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<strong>An</strong> <strong>Absorption</strong> <strong>Chiller</strong> <strong>in</strong> a <strong>Micro</strong> <strong>BCHP</strong> <strong>Application</strong>:<br />

Model based Design and Performance <strong>An</strong>alysis<br />

Hongxi Y<strong>in</strong><br />

<strong>Carnegie</strong> Mellon University<br />

School of Architecture<br />

Ph.D. Committee<br />

Prof. Volker Hartkopf, Ph.D. (Chair)<br />

Prof. David Archer, Ph.D.<br />

Prof. David Claridge, Ph.D.


Copyright Declaration<br />

I hereby declare that I am the sole author of this thesis.<br />

I authorize <strong>Carnegie</strong> Mellon University, Pittsburgh, Pennsylvania to lend this thesis to other<br />

<strong>in</strong>stitutions or <strong>in</strong>dividuals for the purpose of scholarly research.<br />

I authorize <strong>Carnegie</strong> Mellon University, Pittsburgh, Pennsylvania to reproduce this thesis by photo<br />

copy<strong>in</strong>g or by other means, <strong>in</strong> total or <strong>in</strong> part, at the request of other <strong>in</strong>stitutions or <strong>in</strong>dividuals for the<br />

purpose of scholarly research.<br />

Copyright © 2006 by Hongxi Y<strong>in</strong><br />

i


Acknowledgment<br />

It has been a long journey to complete my Ph.D. thesis with the objective of mak<strong>in</strong>g myself more<br />

capable of deal<strong>in</strong>g with the <strong>in</strong>creas<strong>in</strong>g complexity of build<strong>in</strong>g-related technical issues. The scientific<br />

research <strong>in</strong> the Intelligent Workplace (IW) starts my academic career and a brand new professional<br />

practice. In the future, I shall see myself as an “eng<strong>in</strong>eered architect”, who could help the build<strong>in</strong>g<br />

<strong>in</strong>dustry create healthy, efficient, and economical and ultimately susta<strong>in</strong>able environments.<br />

I wish to express my s<strong>in</strong>cere appreciation and gratitude to my advisor, Professor Volker Hartkopf, for<br />

his <strong>in</strong>valuable vision, support, and encouragement. His enthusiasm and <strong>in</strong>spiration were essential to<br />

the success of this research, and his wisdom and <strong>in</strong>sights will serve as a source of ideas for my future<br />

endeavors.<br />

Let me extend my profound gratitude to Professor David Archer who has played a pivotal role <strong>in</strong> this<br />

thesis. He has far exceeded his duty as an advisor, a loyal colleagues and an enthusiastic partner <strong>in</strong> this<br />

endeavor. Furthermore, and more importantly, he has given me a deep understand<strong>in</strong>g of build<strong>in</strong>g<br />

energy systems, and has also implanted his rigorous method of th<strong>in</strong>k<strong>in</strong>g and effective way of work<strong>in</strong>g.<br />

I would like to thank Mr. Zhang Yue, CEO of Broad Air Condition<strong>in</strong>g Co., and his colleagues for their<br />

generous support, diligent work, and warm cooperation over the past several years. Mr. Zhang Yue<br />

spent much time on the design, test, and commercialization of this chiller. His strong motivation and<br />

ability to convert scientific research <strong>in</strong>to commercial products is one of the essential lessons he taught<br />

me.<br />

It gives me great pleasure to thank Professor David Claridge of Texas A&M University for provid<strong>in</strong>g<br />

valuable suggestions and clarifications and Professor Richard Christensen of Ohio State University for<br />

his careful review of the draft and his constructive critique of this work.<br />

I also voice my appreciation to Nancy G. Berkowitz for her diligent guidance on writ<strong>in</strong>g skills and<br />

edit<strong>in</strong>g efforts. Above all are these life-long experiences that are important for my future endeavors. I<br />

am <strong>in</strong>debted to my colleague and lovely wife, M<strong>in</strong>g Qu, who gave me unconditional support and took<br />

the responsibility for car<strong>in</strong>g for our baby, Ryan, who fills us with joys every day. This thesis is also<br />

dedicated to my parents <strong>in</strong> their confidence, their high expectations, and their hearty bless<strong>in</strong>g.<br />

ii


<strong>An</strong> <strong>Absorption</strong> <strong>Chiller</strong> <strong>in</strong> a <strong>Micro</strong> <strong>BCHP</strong> <strong>Application</strong>:<br />

Model based Design and Performance <strong>An</strong>alysis<br />

iii


Table of Contents<br />

Copyright © 2006 by Hongxi Y<strong>in</strong>.........................................................................................................i<br />

Acknowledgment.................................................................................................................................ii<br />

List of Figures...................................................................................................................................viii<br />

List of Tables........................................................................................................................................x<br />

Abstract...............................................................................................................................................xi<br />

1 Introduction ....................................................................................................................... 1<br />

1.1 Background and Motivation .................................................................................................2<br />

1.1.1 CHP Systems ....................................................................................................................3<br />

1.1.2 <strong>BCHP</strong> Systems..................................................................................................................3<br />

1.1.3 Heat Utilization.................................................................................................................4<br />

1.2 Overview of <strong>Absorption</strong> <strong>Chiller</strong> Technology........................................................................5<br />

1.2.1 <strong>Absorption</strong> Cycle <strong>An</strong>alysis ...............................................................................................6<br />

1.2.2 <strong>Absorption</strong> Refrigeration Work<strong>in</strong>g Fluids ........................................................................8<br />

1.2.3 <strong>Absorption</strong> Refrigeration Operat<strong>in</strong>g Conditions...............................................................9<br />

1.2.4 <strong>Absorption</strong> <strong>Chiller</strong> Cycle Modifications...........................................................................9<br />

1.3 Research Objectives............................................................................................................ 11<br />

1.4 Research Approach .............................................................................................................12<br />

1.4.1 The Plann<strong>in</strong>g and Installation of Experimental Equipment ............................................12<br />

1.4.2 The Test Program and Experimental Data ......................................................................13<br />

1.4.3 The Development of Computational Performance Model..............................................13<br />

1.4.4 The <strong>An</strong>alysis of the Experimental Data ..........................................................................14<br />

1.5 Current <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Studies ....................................................................14<br />

1.5.1 <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Approaches ......................................................................14<br />

1.5.2 The Insufficiencies of Current <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Studies ............................15<br />

1.6 The Comprehensive Performance Model and its <strong>Application</strong>s...........................................16<br />

1.6.1 The <strong>Chiller</strong> Model Description .......................................................................................16<br />

1.6.2 <strong>Application</strong>s of the <strong>Chiller</strong> Performance Design Model.................................................18<br />

1.6.2.1 Prelim<strong>in</strong>ary Design Computations..............................................................................18<br />

iv


1.6.2.2 Detailed Design and Performance Computations .......................................................19<br />

1.6.3 Data analysis ...................................................................................................................20<br />

1.7 Chapter Overview...............................................................................................................20<br />

2 <strong>Chiller</strong> Test System and Program .................................................................................. 22<br />

2.1 <strong>Absorption</strong> <strong>Chiller</strong> ..............................................................................................................22<br />

2.1.1 System Descriptions........................................................................................................22<br />

2.1.2 Evaporator and Chilled-Water Pump ..............................................................................26<br />

2.1.3 Absorber and Solution Pump ..........................................................................................27<br />

2.1.4 High-Temperature Regenerator.......................................................................................27<br />

2.1.5 Low-Temperature Regenerator .......................................................................................29<br />

2.1.6 Condenser .......................................................................................................................29<br />

2.1.7 Heat Recovery Devices...................................................................................................30<br />

2.1.8 Cool<strong>in</strong>g Tower ................................................................................................................30<br />

2.1.9 Vacuum System...............................................................................................................31<br />

2.2 <strong>Absorption</strong> <strong>Chiller</strong> Test Systems ........................................................................................32<br />

2.2.1 System Description .........................................................................................................32<br />

2.2.1.1 Steam Supply System..................................................................................................33<br />

2.2.1.2 Variable Cool<strong>in</strong>g Load System ...................................................................................34<br />

2.2.2 Instrumentation, Control, and Data Acquisition System.................................................35<br />

2.2.2.1 Structure of Instrumentation Control System .............................................................35<br />

2.2.2.2 Data Acquisition and Display .....................................................................................36<br />

2.2.2.3 Instrumentation for the <strong>Chiller</strong>....................................................................................38<br />

2.2.2.4 Instrumentation for the Auxiliary Systems .................................................................40<br />

2.2.2.5 Instrumentation Calibration ........................................................................................40<br />

2.2.3 Controls for the <strong>Chiller</strong> ...................................................................................................41<br />

2.3 <strong>Chiller</strong> Performance and Test Program...............................................................................43<br />

2.3.1 <strong>Chiller</strong> Test<strong>in</strong>g.................................................................................................................43<br />

2.3.2 Conduct of the Test<strong>in</strong>g Program .....................................................................................45<br />

2.4 <strong>Chiller</strong> Performance............................................................................................................45<br />

2.4.1 <strong>Chiller</strong> Performance Calculations ...................................................................................46<br />

2.4.2 <strong>Chiller</strong> Performance under Design Condition.................................................................47<br />

2.4.3 <strong>Chiller</strong> Performance at Reduced Capacity Condition .....................................................51<br />

v


2.5 Further Information from <strong>Chiller</strong> Test<strong>in</strong>g ...........................................................................54<br />

3 <strong>Chiller</strong> Design and Performance Model........................................................................ 55<br />

3.1 Flow Diagram .....................................................................................................................55<br />

3.2 Dűhr<strong>in</strong>g Chart Representation ............................................................................................57<br />

3.3 T-Q Diagram.......................................................................................................................59<br />

3.4 Calculation Procedure.........................................................................................................59<br />

3.4.1 Mass Balance ..................................................................................................................60<br />

3.4.2 Energy Balance ...............................................................................................................60<br />

3.4.3 Thermodynamic Property and Equilibrium Relations ....................................................61<br />

3.4.4 Heat Transfer Models......................................................................................................61<br />

3.4.5 Overall Heat Transfer Coefficient Model .......................................................................62<br />

3.4.6 Mass Transfer Models.....................................................................................................65<br />

3.4.7 Model Assumptions ........................................................................................................65<br />

3.5 Model Steps ........................................................................................................................66<br />

4 Model-based Experimental Data <strong>An</strong>alysis.................................................................... 69<br />

4.1 <strong>An</strong>alytical Method ..............................................................................................................69<br />

4.1.1 Statistical <strong>An</strong>alysis Procedure.........................................................................................70<br />

4.1.2 <strong>Absorption</strong> Cycle at Design Condition ...........................................................................72<br />

4.1.3 Overall Deviation............................................................................................................74<br />

4.2 Model <strong>An</strong>alysis ...................................................................................................................75<br />

4.2.1 <strong>An</strong>alysis of Cool<strong>in</strong>g-Load Variation ...............................................................................75<br />

4.2.2 Performance Curve .........................................................................................................77<br />

4.2.3 Flow Rate Variations.......................................................................................................79<br />

4.2.4 Temperature Variations ...................................................................................................81<br />

4.2.5 Composition Variations...................................................................................................82<br />

4.2.6 Vapor Quality Variations.................................................................................................83<br />

4.2.7 Heat Transfer Area Variations.........................................................................................84<br />

4.2.8 Deviation Variations........................................................................................................85<br />

4.2.9 <strong>An</strong>alysis of Other Test Data ............................................................................................86<br />

vi


5 Contributions and Areas of Future Research............................................................... 87<br />

5.1 Contributions ......................................................................................................................87<br />

5.2 Areas of Future Research....................................................................................................89<br />

5.2.1 Extended <strong>Chiller</strong> Model for Multi-Heat Resources ........................................................89<br />

5.2.1.1 Hot Water <strong>Absorption</strong> <strong>Chiller</strong> .....................................................................................90<br />

5.2.1.2 Natural Gas <strong>Absorption</strong> <strong>Chiller</strong>...................................................................................90<br />

5.2.1.3 Exhaust Gas <strong>Absorption</strong> <strong>Chiller</strong>..................................................................................91<br />

5.2.2 System Integration and <strong>Application</strong>................................................................................91<br />

5.2.2.1 <strong>Chiller</strong> Performance Tables for Build<strong>in</strong>g Simulation Tools........................................92<br />

5.2.2.2 Cost Model..................................................................................................................92<br />

References ............................................................................................................................... 93<br />

Appendix 1A ........................................................................................................................... 97<br />

Appendix 2A ......................................................................................................................... 102<br />

Appendix 2B ..........................................................................................................................118<br />

Appendix 3A ......................................................................................................................... 130<br />

Appendix 4A ......................................................................................................................... 150<br />

Acronyms .............................................................................................................................. 194<br />

vii


List of Figures<br />

Figure 1-1: Gross estimation of annual rejected heat <strong>in</strong> the U.S., 2004 ..................................................2<br />

Figure 1-2: Conceptual Diagram for System Integration <strong>in</strong> Build<strong>in</strong>gs....................................................3<br />

Figure 1-3: Schematic diagram of <strong>BCHP</strong> systems...................................................................................4<br />

Figure 1-4: Basic vapor compression chiller cycle..................................................................................7<br />

Figure 1-5: Basic LiBr absorption chiller cycle.......................................................................................7<br />

Figure 1-6: Typical two-stage parallel flow absorption chiller configuration .......................................10<br />

Figure 1-7: Typical two-stage series flow absorption chiller configuration .......................................... 11<br />

Figure 2-1: <strong>Absorption</strong> chiller <strong>in</strong>stalled <strong>in</strong> the IW.................................................................................22<br />

Figure 2-2: Schematic diagram of the absorption chiller.......................................................................23<br />

Figure 2-3: Structure of the absorption chiller.......................................................................................25<br />

Figure 2-4: Configuration of the lower vessel .......................................................................................26<br />

Figure 2-5: Configuration of the upper vessel .......................................................................................28<br />

Figure 2-6: Configuration of cool<strong>in</strong>g tower...........................................................................................31<br />

Figure 2-7: Simplified flow diagram of the chiller test system .............................................................33<br />

Figure 2-8: Site views of the absorption chiller test system ..................................................................34<br />

Figure 2-9: Control and <strong>in</strong>strumentation structure.................................................................................36<br />

Figure 2-10: <strong>Absorption</strong> chiller monitor<strong>in</strong>g software ............................................................................37<br />

Figure 2-11: Test system monitor<strong>in</strong>g software.......................................................................................38<br />

Figure 2-12: PI&D diagram of the absorption chiller............................................................................39<br />

Figure 2-13: Typical start-up of the chiller test system .........................................................................47<br />

Figure 2-14: Steady-state operation of the chiller under design load condition ....................................48<br />

Figure 2-15: Steady-state operation of the chiller under design load condition ....................................49<br />

Figure 2-16: <strong>Chiller</strong> performance under various load conditions..........................................................53<br />

Figure 2-17: <strong>Chiller</strong> power consumption under various load conditions...............................................53<br />

Figure 2-18: Comparison of chiller performance ..................................................................................54<br />

Figure 3-1: Simplified flow diagram for chiller model .........................................................................56<br />

Figure 3-2: Dűhr<strong>in</strong>g chart at design condition.......................................................................................58<br />

Figure 3-3: T-Q diagram for the heat transfer components....................................................................59<br />

Figure 3-4: Steps <strong>in</strong> the use of the performance model .........................................................................67<br />

Figure 3-5: Structure of the design model .............................................................................................68<br />

Figure 3-6: Structure of performance model .........................................................................................68<br />

viii


Figure 4-1: Data analytical procedure flow diagram .............................................................................70<br />

Figure 4-2: <strong>Absorption</strong> cycle at design load condition ..........................................................................73<br />

Figure 4-3: Dűhr<strong>in</strong>g chart at 55% design load condition.......................................................................76<br />

Figure 4-4: <strong>Absorption</strong> cycle variations with load changes...................................................................77<br />

Figure 4-5: <strong>Chiller</strong> performance curve under various load conditions ..................................................78<br />

Figure 4-6: Heat transfer load on each component under various load conditions................................78<br />

Figure 4-7: Steam supply flow rate under various load conditions .......................................................79<br />

Figure 4-8: Sorbent solution flow rate under various load conditions...................................................80<br />

Figure 4-9: Sorbent solution split ratio under various load conditions..................................................80<br />

Figure 4-10: Refrigerant regeneration rate under various load conditions ............................................81<br />

Figure 4-11: Refrigerant vaporization temperature under various load conditions ...............................82<br />

Figure 4-12: Sorbent solution composition changes under various load conditions .............................82<br />

Figure 4-13: Refrigerant vapor quality leav<strong>in</strong>g the LTRG under various load conditions ....................83<br />

Figure 4-14: UA changed for the 5 major components under various load conditions .........................84<br />

Figure 4-15: Surface contact area changes under various load conditions............................................85<br />

Figure 4-16: Overall and weighted deviations under various load conditions ......................................86<br />

Figure 5-1: Simplified HTRG configurations for natural-gas-driven absorption chiller.......................91<br />

ix


List of Tables<br />

Table 1-1: Power generation equipment rejected heat temperature ranges..............................................5<br />

Table 1-2: Water-LiBr absorption chiller thermal energy types and temperature ranges ........................5<br />

Table 2-1: Component names and correspond<strong>in</strong>g abbreviations ...........................................................23<br />

Table 2-2: Specifications of the absorption chiller ................................................................................25<br />

Table 2-4: Control po<strong>in</strong>ts of the chiller..................................................................................................41<br />

Table 2-3: Instrumentations of the chiller test systems..........................................................................42<br />

Table 2-5: Input and primary output of the test program.......................................................................45<br />

Table 2-6: Measurement data of the chiller under design condition......................................................50<br />

Table 2-7: Comparison of chiller performance under design conditions...............................................51<br />

Table 2-8: Primary measurement for chiller <strong>in</strong>put and output...............................................................52<br />

Table 3-1: <strong>Chiller</strong> model state po<strong>in</strong>t descriptions ..................................................................................57<br />

Table 3-2: Physical features of heat and mass transfer components......................................................63<br />

Table 3-3: Heat and mass transfer correlations used <strong>in</strong> the performance model ...................................64<br />

Table 4-1: Measured values and model calculations for 100% and 55% of design load conditions .....71<br />

Table 5-1: Heat transfer features of the HTRG of different heat<strong>in</strong>g media ...........................................90<br />

x


Abstract<br />

Developments <strong>in</strong> absorption cool<strong>in</strong>g technology present an opportunity to achieve significant<br />

improvements <strong>in</strong> microscale build<strong>in</strong>g cool<strong>in</strong>g, heat<strong>in</strong>g, and power (<strong>BCHP</strong>) systems for residential and<br />

light commercial build<strong>in</strong>gs that are effective, energy efficient, and economic. However, model based<br />

design and performance analysis methods for micro scale absorption chillers and their applications<br />

have not been fully developed; particularly consider<strong>in</strong>g that thermal energy from a wide variety of<br />

sources might be used to drive the chiller <strong>in</strong> a residential or light commercial build<strong>in</strong>g. This thesis<br />

contributes important knowledge and methods for design<strong>in</strong>g and <strong>in</strong>tegrat<strong>in</strong>g absorption chillers <strong>in</strong><br />

<strong>BCHP</strong> systems that reduce energy consumption, decrease operational costs, and improve<br />

environmental benefits <strong>in</strong> residential and light commercial build<strong>in</strong>gs.<br />

To be more specific, this thesis contributes the development and application of absorption chiller and<br />

the computational model <strong>in</strong> the follow<strong>in</strong>g areas:<br />

1) establishment of a unique experimental environment and procedures for absorption chiller<br />

tests under various conditions<br />

2) conduct of a comprehensive test<strong>in</strong>g program on a microscale absorption chiller<br />

3) construction of a comprehensive chiller model based on the pert<strong>in</strong>ent scientific and<br />

eng<strong>in</strong>eer<strong>in</strong>g pr<strong>in</strong>ciples adapted to the design of a chiller and to the analysis of extensive,<br />

detailed test data obta<strong>in</strong>ed from the test program<br />

4) analysis of the measured data, ref<strong>in</strong>ement of the model, and improvement of the chiller design<br />

on the basis of the data analysis process<br />

The model is now be<strong>in</strong>g used as a tool to adapt the chiller to various heat sources and s<strong>in</strong>ks and to<br />

carry out performance simulations of micro <strong>BCHP</strong> system.<br />

xi


1 Introduction<br />

In the United States, residential and commercial build<strong>in</strong>gs – more than 107 million households (2001)<br />

[1] and 71.7 billion square feet of commercial floor space (2003) [2] – account for more than one-third<br />

of the total energy consumption of the country. Significant energy efficiency improvements <strong>in</strong> heat<strong>in</strong>g,<br />

ventilation, air condition<strong>in</strong>g and refrigeration (HVAC&R) systems for residential and light<br />

commercial build<strong>in</strong>gs might be achieved by the application of microscale heat-driven absorption<br />

chillers for space and ventilation air cool<strong>in</strong>g.<br />

<strong>Absorption</strong> chillers are key components <strong>in</strong> a build<strong>in</strong>g cool<strong>in</strong>g heat<strong>in</strong>g and power (<strong>BCHP</strong>) system to<br />

cool space <strong>in</strong> build<strong>in</strong>gs. They can be driven directly by the thermal energy and heat recovered from<br />

various sources, <strong>in</strong>clud<strong>in</strong>g power generation equipment and solar receiv<strong>in</strong>g devices. The comb<strong>in</strong>ation<br />

of heat recovery equipment and heat-driven absorption chillers provides significantly <strong>in</strong>creased overall<br />

energy efficiency. Most of today’s heat<strong>in</strong>g and cool<strong>in</strong>g technologies for build<strong>in</strong>gs, however, are not<br />

designed to make use of rejected heat. Performance model<strong>in</strong>g studies of heat-driven absorption chillers<br />

are accord<strong>in</strong>gly limited, contribut<strong>in</strong>g to the difficulty of prepar<strong>in</strong>g and apply<strong>in</strong>g build<strong>in</strong>g simulation<br />

programs for <strong>BCHP</strong> system design and performance analysis.<br />

This thesis contributes important knowledge and methods for design<strong>in</strong>g and <strong>in</strong>tegrat<strong>in</strong>g absorption<br />

chillers <strong>in</strong> <strong>BCHP</strong> systems that reduce energy consumption, decrease operational costs, and improve<br />

environmental benefits <strong>in</strong> residential and light commercial build<strong>in</strong>gs.<br />

The gap between experiment and simulation is closed <strong>in</strong> this thesis because of the availability of a<br />

unique microscale absorption chiller and an associated experimental setup. By develop<strong>in</strong>g and<br />

apply<strong>in</strong>g a numerical performance model, a ref<strong>in</strong>ed understand<strong>in</strong>g of a particular chiller and its<br />

operation can provide improved design and model<strong>in</strong>g tools for heat-driven absorption chillers <strong>in</strong><br />

general. The approach developed <strong>in</strong> this thesis will allow developers to simulate the <strong>in</strong>teraction of the<br />

<strong>BCHP</strong> components as a system along with its <strong>in</strong>teractions with:<br />

• power and other energy supply systems<br />

• electricity grids<br />

• <strong>in</strong>door air conditions<br />

• various load profiles<br />

1


The model<strong>in</strong>g tool will also allow eng<strong>in</strong>eers to assess different operat<strong>in</strong>g strategies of such a system to<br />

f<strong>in</strong>d the most economic operat<strong>in</strong>g conditions, based on the idealized nonl<strong>in</strong>ear systems with only a few<br />

degrees of freedom.<br />

1.1 Background and Motivation<br />

In the United States, approximately two-thirds of the energy of the fuel used to generate electricity is<br />

wasted as rejected heat. <strong>An</strong>nually, 28.8 to 34.0 quadrillion Btu of thermal energy are rejected to the<br />

atmosphere, lakes, and rivers from power generation, build<strong>in</strong>g equipment operations, and <strong>in</strong>dustrial<br />

processes, Figure 1-1, [3, 4].<br />

Figure 1-1: Gross estimation of annual rejected heat <strong>in</strong> the U.S., 2004<br />

National<br />

total energy<br />

consumption<br />

(99.74 Quads)<br />

Power<br />

generation<br />

(40.77 Quads)<br />

Residential<br />

sector<br />

(6.92 Quads)<br />

Commercial<br />

sector<br />

(4.02 Quads)<br />

Industrial<br />

sector<br />

(21.18 Quads)<br />

Transportation<br />

(27.79 Quads)<br />

Electricity<br />

(14.2 Quads)<br />

HVAC, light<strong>in</strong>g, and others<br />

(4.84-5.54 Quads)<br />

HVAC, light<strong>in</strong>g, and others<br />

(2.81-3.21 Quads)<br />

Manufactur<strong>in</strong>g processes<br />

(16.94-19.06 Quads)<br />

Power production<br />

waste heat<br />

(24.5 -26.5 Quads)<br />

Residential sector<br />

waste heat<br />

(1.38-2.08 Quads)<br />

Commercial sector<br />

waste heat<br />

(0.8-1.2 Quads)<br />

Industrial sector<br />

waste heat<br />

(2.12-4.24 Quads)<br />

National total<br />

waste heat<br />

(28.8-34.02 Quads)<br />

Rejected heat from power generation can be used for build<strong>in</strong>g operations. Renewable energy sources<br />

(such as solar thermal energy to drive absorption chillers and boilers) comb<strong>in</strong>ed with advanced<br />

distributed electric energy generation can also be used <strong>in</strong> build<strong>in</strong>gs. Figure 1-2 illustrates the system<br />

<strong>in</strong>tegration concepts that Volker Hartkopf put forward for the first time [5], for the opportunities of<br />

simultaneously achiev<strong>in</strong>g energy conservation, us<strong>in</strong>g renewable resource, and deploy<strong>in</strong>g distributed<br />

electricity generation technologies. The build<strong>in</strong>g of the future is conceived as a power plant (BAPP)<br />

that would generate more energy on site than is brought to it <strong>in</strong> the form of non-renewable resources.<br />

The surplus of energy (power, heat<strong>in</strong>g, and cool<strong>in</strong>g) could export to the utility grids or neighbor<strong>in</strong>g<br />

build<strong>in</strong>gs.<br />

2


Figure 1-2: Conceptual Diagram for System Integration <strong>in</strong> Build<strong>in</strong>gs<br />

Resource conservation:<br />

Energy, water,<br />

material, and so forth<br />

Source: Volker Hartkopf [5]<br />

1.1.1 CHP Systems<br />

Renewables: solar, w<strong>in</strong>d, bio-gas,<br />

day-light<strong>in</strong>g, natural ventilation,<br />

passive/active heat<strong>in</strong>g/cool<strong>in</strong>g<br />

System<br />

Integration<br />

Distributed generation:<br />

eng<strong>in</strong>e generator,<br />

gas turb<strong>in</strong>e, and fuel cell<br />

Comb<strong>in</strong>ed heat<strong>in</strong>g and power (CHP) systems are based on the concept of produc<strong>in</strong>g electrical energy<br />

and recover<strong>in</strong>g rejected heat for useful purposes. Compared with conventional power plants, CHP<br />

systems can improve overall energy efficiency from 30% to 70% or more. CHP is effective <strong>in</strong> largescale<br />

<strong>in</strong>dustrial plants, hospitals, university campuses, and urban district energy systems. Recent<br />

developments <strong>in</strong> small-scale power generation, heat recovery, and heat-driven refrigeration<br />

technologies make possible the <strong>in</strong>stallation and effective operation of CHP <strong>in</strong> residential and small<br />

commercial applications.<br />

1.1.2 <strong>BCHP</strong> Systems<br />

In <strong>BCHP</strong> systems, the electrical energy generated on site is used to meet the demands of light<strong>in</strong>g and<br />

electrical equipment. The rejected heat <strong>in</strong> power generation is used to provide space ventilation,<br />

cool<strong>in</strong>g, heat<strong>in</strong>g, dehumidification, and domestic hot water for the build<strong>in</strong>g, Figure 1-3.<br />

Various technologies can be used to configure a <strong>BCHP</strong> system. The power generation equipment, as<br />

illustrated at the top of the figure, could be a steam turb<strong>in</strong>e, combustion turb<strong>in</strong>e, reciprocat<strong>in</strong>g spark<br />

ignition, Diesel eng<strong>in</strong>e, or fuel cell. These power generators produce power and reject heat <strong>in</strong> various<br />

quantities at various temperatures that can be used for the build<strong>in</strong>g operation. Heat recovery<br />

exchangers/boilers, absorption chillers, and desiccant dehumidifiers are equipment that can deliver<br />

heat<strong>in</strong>g, cool<strong>in</strong>g, or ventilation to the build<strong>in</strong>g space. As <strong>in</strong>dicated <strong>in</strong> Figure 1-3, the thermal <strong>in</strong>put can<br />

also be provided directly from solar thermal receivers. F<strong>in</strong>ally, a capable, robust control system is<br />

needed to <strong>in</strong>tegrate the operation of all equipment to meet the needs of the build<strong>in</strong>g and its occupants<br />

3


and to achieve the full benefits of system efficiency and economy. Heat-driven absorption chiller<br />

technology plays a prom<strong>in</strong>ent role <strong>in</strong> mak<strong>in</strong>g use of the reject as well as solar energy, for space and<br />

ventilation air cool<strong>in</strong>g, and thus <strong>in</strong> the design and operation of overall <strong>BCHP</strong> systems.<br />

Figure 1-3: Schematic diagram of <strong>BCHP</strong> systems<br />

Traditionally, CHP systems with power generation capacities below 500 kW are categorized as<br />

microscale systems. With the development of compact, microscale absorption chillers, more reliable,<br />

lower-emitt<strong>in</strong>g reciprocat<strong>in</strong>g eng<strong>in</strong>es, and high-temperature fuel cell power supplies, <strong>BCHP</strong> is feasible<br />

for packaged systems <strong>in</strong> residential and light commercial build<strong>in</strong>gs hav<strong>in</strong>g power requirements less<br />

than 15 kW. This <strong>in</strong>troduction of micro-<strong>BCHP</strong> systems presents many technical and commercial<br />

challenges, but the production of heat-driven absorption chillers and their <strong>in</strong>tegration <strong>in</strong> <strong>BCHP</strong><br />

systems can assist the nation <strong>in</strong><br />

• <strong>in</strong>creas<strong>in</strong>g energy efficiency<br />

• <strong>in</strong>tegrat<strong>in</strong>g renewable forms of energy<br />

• elim<strong>in</strong>at<strong>in</strong>g transmission and distribution costs and losses<br />

• <strong>in</strong>creas<strong>in</strong>g reliability by comb<strong>in</strong><strong>in</strong>g distributed with centralized utility power supplies<br />

1.1.3 Heat Utilization<br />

Table 1-1 illustrates the temperature range of rejected thermal energy from typical power generators<br />

and heat recovery units. Among them, a solid oxide fuel cell (SOFC) gives the highest exhaust gas<br />

4


temperature for heat recovery and utilization. The hot water temperature from solar collectors varies<br />

with the type of collector. Solar collectors with parabolic trough reflectors can generate hot water up<br />

to 180 o C; <strong>in</strong>tegrated compound parabolic collectors, ICPC’s, 140 to 160 o C; flat plate collectors, 65 to<br />

90 o C.<br />

Table 1-1: Power generation equipment rejected heat temperature ranges<br />

No. Power Generation Equipment, Waste Stream Temperature ( o F) Temperature ( o C)<br />

1 Solid Oxide Fuel Cell Exhaust 1300 700-800<br />

2 Reciprocal Eng<strong>in</strong>e Exhaust 1100-1200 600-650<br />

3 Molten Carbonate Fuel Cell Exhaust 1100 600<br />

4 Gas Turb<strong>in</strong>e Exhaust 950-1000 510-540<br />

5 <strong>Micro</strong>turb<strong>in</strong>e Exhaust 450-600 230-315<br />

6 HRSG Exhaust 350 175<br />

7 Reciprocal Eng<strong>in</strong>e Jacket Water 180-200 80-95<br />

8 Phosphoric Acid Fuel Cell 180 80<br />

9 Solar Thermal Collector 150-250 65-180<br />

Table 1-2 shows typical temperature ranges for the heat<strong>in</strong>g medium to drive a water-lithium bromide<br />

(LiBr) absorption chiller [6]. A s<strong>in</strong>gle-stage hot-water-driven chiller can use heat at a temperature as<br />

low as 75 o C. Tables 1-1 and 1-2 show that an absorption chiller can be found to use heat from a wide<br />

range of sources. Because of its higher thermal efficiency, this study focuses on a two-stage absorption<br />

chiller and its appropriate sources of rejected heat.<br />

Table 1-2: Water-LiBr absorption chiller thermal energy types and temperature ranges<br />

No. Heat-driven <strong>Absorption</strong> <strong>Chiller</strong> Type Pressure (kPa) Temperature ( o C)<br />

1 Direct-fired fossil fuel (natural gas, oil, LPG etc.) - 1,000 – 1,800<br />

2 Double-stage exhaust gas - 400 - 600<br />

3 S<strong>in</strong>gle-stage exhaust gas - 230 - 350<br />

4 Double-stage steam 400 – 1,000 144 - 180<br />

5 S<strong>in</strong>gle-stage steam 100 - 400 103 - 133<br />

6 Double-stage hot water 350 – 1,100 140 - 200<br />

7 S<strong>in</strong>gle-stage hot water 40 - 200 75 - 120<br />

8 Other fuel/steam/hot water/exhaust gas Same as above Same as above<br />

1.2 Overview of <strong>Absorption</strong> <strong>Chiller</strong> Technology<br />

<strong>An</strong> absorption chiller is a mach<strong>in</strong>e that, driven by heat, produces chilled water for space and<br />

ventilation air cool<strong>in</strong>g. Little or no mechanical energy is consumed <strong>in</strong> an absorption chiller, and little<br />

or no electric power is required. A great variety of hot media, gases and liquids, over a broad range of<br />

temperatures above ambient can be used. The chiller must also reject an amount of heat equal to that<br />

provided <strong>in</strong> driv<strong>in</strong>g it plus that absorbed <strong>in</strong> produc<strong>in</strong>g the chilled water. Ammonia-water (NH3-H2O)<br />

5


absorption refrigeration technology has been used for more than 150 years. As a refrigerant, ammonia<br />

has high latent heat and excellent heat transfer characteristics, but its toxicity has limited its use <strong>in</strong> this<br />

technology.<br />

S<strong>in</strong>ce 1945, water-LiBr absorption chillers have achieved widespread use. This trend reached its peak<br />

<strong>in</strong> the 1960s, and then dim<strong>in</strong>ished <strong>in</strong> the late 1970s. The technology has s<strong>in</strong>ce revived <strong>in</strong> Asia, because<br />

the rapidly <strong>in</strong>creas<strong>in</strong>g electricity demand has limited the application of electrically driven vapor<br />

compression chillers. The sales data of a lead<strong>in</strong>g absorption chiller manufacturer, presented <strong>in</strong><br />

appendix 1A, shows several new developments <strong>in</strong> the current absorption chiller market. Today, water-<br />

LiBr absorption chiller technology is return<strong>in</strong>g to the United States with the <strong>in</strong>creas<strong>in</strong>g application of<br />

CHP systems.<br />

In the past three years, heat-driven water-LiBr absorption chillers have been used widely both <strong>in</strong> large<br />

commercial build<strong>in</strong>gs comb<strong>in</strong>ed with advanced power generation equipment and <strong>in</strong> <strong>in</strong>dividual houses<br />

driven directly by fossil fuels or by other heat sources. The cool<strong>in</strong>g capacity of chillers can vary from<br />

greater that 1,000 refrigeration ton (3,561.85 kW) to as low as a microscale, 4.5 refrigeration ton (16<br />

kW). This thesis will focus on microscale water-LiBr absorption chiller research, development, and<br />

demonstration <strong>in</strong> residential and light commercial applications.<br />

1.2.1 <strong>Absorption</strong> Cycle <strong>An</strong>alysis<br />

A chiller produces chilled water by remov<strong>in</strong>g heat from it and transferr<strong>in</strong>g this heat to a vaporiz<strong>in</strong>g<br />

refrigerant. The process is illustrated <strong>in</strong> Figure 1-4 for a conventional vapor compression chiller and<br />

<strong>in</strong> Figure 1-5 for an absorption chiller. In both, the refrigerant liquid flows <strong>in</strong>to an evaporator,<br />

evaporates at a reduced pressure and temperature, and absorbs heat from chilled water flow<strong>in</strong>g <strong>in</strong> a<br />

tube through the evaporator. In the vapor compression process, the refrigerant vapor is compressed<br />

and condensed at a high-pressure and temperature, transferr<strong>in</strong>g heat to cool<strong>in</strong>g water or to the<br />

surround<strong>in</strong>gs <strong>in</strong> a condenser. The high-pressure condensed refrigerant is then returned through the<br />

expansion valve to a low-pressure evaporator, once aga<strong>in</strong> to absorb heat from the chilled-water flow.<br />

6


Figure 1-4: Basic vapor compression chiller cycle<br />

Refrigerant<br />

expansion valve<br />

P<br />

Evaporator<br />

Heat absorbed<br />

from chilled water<br />

T<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

Condenser<br />

Compressor<br />

In the absorption process shown <strong>in</strong> Figure 1-5, the refrigerant vapor from the evaporator is absorbed at<br />

low pressure <strong>in</strong>to a sorbent solution <strong>in</strong> the absorber. Heat is released as the refrigerant vapor is<br />

absorbed. This heat is removed by cool<strong>in</strong>g water flow<strong>in</strong>g through the absorber. The sorbent solution<br />

is then pumped to the regenerator, where refrigerant vapor is driven from the sorbent solution by the<br />

addition of heat at high temperature and pressure. The refrigerant vapor is condensed at high pressure<br />

and temperature with the removal of heat to ambient or to cool<strong>in</strong>g water. The liquid refrigerant is<br />

returned to the evaporator through the expansion valve.<br />

Figure 1-5: Basic LiBr absorption chiller cycle<br />

P<br />

Refrigerant<br />

expansion valve<br />

Heat absorbed<br />

from chilled water<br />

T<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

Condenser<br />

Solution<br />

pump<br />

Evaporator Absorber<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

Work<br />

Heat <strong>in</strong>put<br />

Regenerator<br />

Solution<br />

expansion valve<br />

7


This basic absorption chiller cycle shown <strong>in</strong> Figure 1-5 is similar to the traditional vapor compression<br />

chiller cycle <strong>in</strong> Figure 1-4 <strong>in</strong> that<br />

• refrigerant vapor is condensed at high pressure and temperature, reject<strong>in</strong>g heat to the<br />

surround<strong>in</strong>gs<br />

• refrigerant vapor is vaporized at low pressure and temperature, absorb<strong>in</strong>g heat from the chilled<br />

water flow<br />

The chiller cycles differ <strong>in</strong> that<br />

• the pumped circulation of a sorbent solution replaces the compression of the refrigerant vapor<br />

The energy, work, required by the pump is significantly less than that required by the<br />

compressor<br />

• heat must be supplied <strong>in</strong> the regenerator to release refrigerant vapor at high pressure for<br />

condensation, and heat must be removed from the absorber<br />

From the standpo<strong>in</strong>t of thermodynamics, the vapor compression chiller is a heat pump, us<strong>in</strong>g<br />

mechanical energy and work, to move heat from a low to a high temperature. <strong>An</strong> absorption chiller is<br />

the equivalent of a heat eng<strong>in</strong>e – absorb<strong>in</strong>g heat at a high temperature, reject<strong>in</strong>g heat at a lower<br />

temperature, produc<strong>in</strong>g work – driv<strong>in</strong>g a heat pump.<br />

1.2.2 <strong>Absorption</strong> Refrigeration Work<strong>in</strong>g Fluids<br />

<strong>An</strong> absorption chiller requires two work<strong>in</strong>g fluids, a refrigerant and a sorbent solution of the<br />

refrigerant. In a water-LiBr absorption chiller, water is the refrigerant; and water-LiBr solution, the<br />

sorbent. In the absorption chiller cycle the water refrigerant undergoes a phase change <strong>in</strong> the<br />

condenser and evaporator; and the sorbent solution, a change <strong>in</strong> concentration <strong>in</strong> the absorber and<br />

evaporator.<br />

Water is an excellent refrigerant; it has high latent heat. Its cool<strong>in</strong>g effect, however, is limited to<br />

temperatures above 0 o C because of freez<strong>in</strong>g. The sorbent, LiBr, is nonvolatile, so a vapor phase <strong>in</strong><br />

the absorption chiller is always H2O. The sorbent solution, water-LiBr, has a low H2O vapor pressure<br />

at the temperature of the absorber and high H2O vapor pressure at the temperature of the regenerator,<br />

facilitat<strong>in</strong>g design and operation of the chiller. The advantage of the water-LiBr pair <strong>in</strong>cludes its<br />

stability, safety, and high volatility ratio. It has no associated environmental hazard, ozone depletion,<br />

or global warm<strong>in</strong>g potential.<br />

8


1.2.3 <strong>Absorption</strong> Refrigeration Operat<strong>in</strong>g Conditions<br />

The choice of the refrigerant, water, and sorbent, water-LiBr solution, along with the designation of a<br />

chilled-water outlet temperature and cool<strong>in</strong>g-water <strong>in</strong>let temperature determ<strong>in</strong>es the operat<strong>in</strong>g<br />

temperatures and pressures <strong>in</strong> the evaporator, absorber, regenerator, and condenser of the LiBr<br />

absorption chiller as illustrated <strong>in</strong> Figure 1-5.<br />

• In the evaporator, low operat<strong>in</strong>g temperature and pressure are required to vaporize refrigerant<br />

to absorb heat from the chilled water.<br />

• In the absorber, the cool<strong>in</strong>g-water temperature determ<strong>in</strong>es the composition of the sorbent<br />

solution so that it absorbs the refrigerant vapor, as required, at the pressure determ<strong>in</strong>ed by the<br />

evaporator.<br />

• In the regenerator, the pressure is that of the condenser. <strong>An</strong> elevated value is required to<br />

condense the refrigerant vapor at the temperature of the cool<strong>in</strong>g water. The temperature <strong>in</strong> the<br />

absorber is that required to vaporize the refrigerant from the sorbent solution.<br />

The low operat<strong>in</strong>g pressure <strong>in</strong> the evaporator and absorber requires high equipment volume and a<br />

special means for reduc<strong>in</strong>g pressure loss <strong>in</strong> the refrigerant vapor flow. Prevent<strong>in</strong>g the leakage of air<br />

<strong>in</strong>to the evaporator and the absorber is one of the ma<strong>in</strong> issues <strong>in</strong> operat<strong>in</strong>g an absorption chiller. A<br />

special purge device removes air and other noncondensable gases, and an external vacuum pump is<br />

used periodically to ma<strong>in</strong>ta<strong>in</strong> low operat<strong>in</strong>g pressure. The high operat<strong>in</strong>g pressure <strong>in</strong> the regenerator<br />

and condenser requires the use of heavy-walled equipment and a pump to deliver the sorbent solution<br />

from the low-pressure absorber to the high-pressure regenerator. Crystallization, the deposition of<br />

LiBr from the sorbent solution at high concentrations and low temperatures, can block the sorbent<br />

flow and cause the chiller to shut down. Controls are usually necessary to prevent crystallization.<br />

1.2.4 <strong>Absorption</strong> <strong>Chiller</strong> Cycle Modifications<br />

Several modifications can be made <strong>in</strong> the basic absorption chiller cycle to reduce the heat required to<br />

operate the chiller and to reduce the extent of heat transfer surface <strong>in</strong>corporated <strong>in</strong> the mach<strong>in</strong>e.<br />

• Countercurrent heat <strong>in</strong>terchange can be arranged between the two sorbent solution flows<br />

connect<strong>in</strong>g the low-temperature absorber and the high-temperature regenerator. This<br />

<strong>in</strong>terchange can significantly reduce the heat quantities <strong>in</strong>volved <strong>in</strong> the operation of both; less<br />

heat will need to be supplied to the regenerator, and less heat will need to be removed form the<br />

absorber.<br />

9


• The refrigerant vapor leav<strong>in</strong>g the high-temperature and -pressure regenerator can be used to<br />

vaporize an equal quantity of refrigerant from the sorbent solution <strong>in</strong> a second regenerator<br />

operat<strong>in</strong>g at a lower temperature and pressure. This second stage of regeneration reduces the<br />

heat requirement of the absorption chiller by a factor approach<strong>in</strong>g 2.<br />

• Heat transfer between the vaporiz<strong>in</strong>g refrigerant and the chilled water <strong>in</strong> the evaporator can be<br />

facilitated by recirculat<strong>in</strong>g the refrigerant liquid over the heat transfer surface, reduc<strong>in</strong>g the<br />

temperature difference and the heat transfer area.<br />

Figure 1-6: Typical two-stage parallel flow absorption chiller configuration<br />

Refrigerant<br />

comb<strong>in</strong>er<br />

Refrigerant<br />

expansion valve<br />

P<br />

Recirculation<br />

pump<br />

Heat absorbed<br />

from chilled water<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

T<br />

Condenser<br />

Solution<br />

splitter<br />

Solution<br />

pump<br />

Evaporator Absorber<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

Condenser<br />

Heat to<br />

LTRG<br />

Low-temp.<br />

regenerator<br />

Low-temp.<br />

heat exchanger<br />

Solution<br />

comb<strong>in</strong>er<br />

Solution<br />

expansionvalve<br />

Heat <strong>in</strong>put<br />

Regenerator<br />

High-temp.<br />

heat exchanger<br />

The revised flow diagrams illustrat<strong>in</strong>g these absorption chiller flow diagrams are shown <strong>in</strong> Figures 1-6<br />

and 1-7. The flow of the sorbent solution from the absorber to the two regenerators can be either<br />

parallel or <strong>in</strong> series. In a parallel flow arrangement, the dilute solution from the absorber is pumped to<br />

both the high-temperature and the lower-temperature regenerators <strong>in</strong> parallel, as shown <strong>in</strong> Figure 1-6.<br />

Concentrated solutions from both regenerators are recomb<strong>in</strong>ed and returned to the absorber. In a<br />

series flow arrangement, the solution from the absorber is first pumped to the high-temperature, highpressure<br />

regenerator; and the partially concentrated sorbent solution then flows to the lower-pressure,<br />

lower-temperature regenerator, as shown <strong>in</strong> Figure 1-7.<br />

10


Figure 1-7: Typical two-stage series flow absorption chiller configuration<br />

P<br />

Refrigerant<br />

comb<strong>in</strong>er<br />

Refrigerant<br />

expansion valve<br />

Recirculation<br />

pump<br />

Heat absorbed<br />

from chilled water<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

T<br />

Condenser<br />

Solution<br />

Pump<br />

Evaporator Absorber<br />

Heat rejected<br />

to cool<strong>in</strong>g water<br />

Condenser<br />

Heat to<br />

LTRG<br />

Low-temp.<br />

heat exchanger<br />

High-temp.<br />

heat exchanger<br />

Low-temp.<br />

regenerator<br />

Solution<br />

expansion valve<br />

Heat <strong>in</strong>put<br />

Regenerator<br />

A parallel flow configuration has several advantages over the series flow configuration. The sorbent<br />

solution flow <strong>in</strong> each heat <strong>in</strong>terchanger is only half that of the series flow configuration. In general,<br />

the parallel configuration has a lower heat <strong>in</strong>put requirement than the series flow configuration.<br />

1.3 Research Objectives<br />

The objective of this research is to develop methods for the effective design and evaluation of<br />

absorption chiller-based micro-<strong>BCHP</strong> systems that reduce energy consumption, decrease operational<br />

costs, and improve environmental benefits <strong>in</strong> residential and light commercial build<strong>in</strong>gs. The methods<br />

demonstrated <strong>in</strong> the thesis can be widely used <strong>in</strong> build<strong>in</strong>g energy system design and evaluation; they<br />

can also be broadly applied <strong>in</strong> an absorption chiller and other <strong>BCHP</strong> system equipment design, and <strong>in</strong><br />

system <strong>in</strong>tegration. The analytical methods also provide the basis for diagnos<strong>in</strong>g and optimiz<strong>in</strong>g the<br />

operation of absorption chiller-based micro-<strong>BCHP</strong> systems.<br />

Four research areas are <strong>in</strong>volved <strong>in</strong> this work on microscale absorption chiller system evaluation and<br />

performance simulation:<br />

11


1) establishment of a unique experimental environment and procedures for absorption chiller<br />

tests under various conditions<br />

2) conduct of a comprehensive test<strong>in</strong>g program on a microscale absorption chiller<br />

3) construction of a comprehensive chiller model based on the pert<strong>in</strong>ent scientific and<br />

eng<strong>in</strong>eer<strong>in</strong>g pr<strong>in</strong>ciples adapted to the design of a chiller and to the analysis of extensive,<br />

detailed test data obta<strong>in</strong>ed from the test program<br />

4) analysis of the measured data, ref<strong>in</strong>ement of the model, and improvement of the chiller design<br />

on the basis of the data analysis process<br />

The model is now be<strong>in</strong>g used as a tool to adapt the chiller to various heat sources and s<strong>in</strong>ks and to<br />

carry out performance simulations of micro <strong>BCHP</strong> system. In both its theoretical and practical aspects,<br />

this study contributes important knowledge for the development and application of micro-<strong>BCHP</strong><br />

systems <strong>in</strong> residential and light commercial build<strong>in</strong>gs. The improvements <strong>in</strong> <strong>BCHP</strong> system analytical<br />

methods lay the groundwork for develop<strong>in</strong>g of overall <strong>BCHP</strong> system performance assessment tool; the<br />

practical progress <strong>in</strong> microscale-<strong>BCHP</strong> system experiment and evaluation setups establishes the<br />

threshold for an efficient and <strong>in</strong>tegrated microscale build<strong>in</strong>g energy supply, distribution, and delivery<br />

system. These contributions are made possible by close cooperation <strong>in</strong> research and development<br />

(R&D) with a lead<strong>in</strong>g manufacturer; <strong>in</strong> turn, some of the research achievements of this study have<br />

been promptly <strong>in</strong>corporated <strong>in</strong>to the emerg<strong>in</strong>g technology and product.<br />

1.4 Research Approach<br />

To achieve the research objectives, this thesis focuses on equipment <strong>in</strong>stallation and test, model<br />

development, data analysis, and system simulation of a microscale, steam-driven, two-stage LiBr<br />

absorption chiller for an energy supply system <strong>in</strong> <strong>Carnegie</strong> Mellon University (CMU)’s Robert L.<br />

Preger Intelligent Workplace (IW). Experimental data and a computational model are the two basic<br />

components of this work. The experience ga<strong>in</strong>ed provides the framework for other <strong>BCHP</strong> component<br />

studies and system <strong>in</strong>tegration. The research has been carried out <strong>in</strong> the follow<strong>in</strong>g several steps: some<br />

<strong>in</strong> parallel, others sequentially:<br />

1.4.1 The Plann<strong>in</strong>g and Installation of Experimental Equipment<br />

A microscale <strong>BCHP</strong> energy supply system (ESS) has been designed for the IW, a 6,500 ft 2 office<br />

environment at CMU, to provide power and space cool<strong>in</strong>g heat<strong>in</strong>g, and ventilation. As the first stage<br />

<strong>in</strong> realiz<strong>in</strong>g this overall system, a 16kW steam-driven water-LiBr absorption chiller was <strong>in</strong>stalled <strong>in</strong><br />

the south section of the IW. This chiller<br />

12


• is driven by steam, reduc<strong>in</strong>g summer electrical peak demands and level<strong>in</strong>g the year round<br />

demand for natural gas and other fuels<br />

• is flexible <strong>in</strong> adapt<strong>in</strong>g to thermal recovery equipment associated with various prime movers<br />

• provides a cool<strong>in</strong>g capacity and compactness appropriate for residential, small commercial, and<br />

<strong>in</strong>stitutional build<strong>in</strong>gs<br />

• <strong>in</strong>corporates a cool<strong>in</strong>g tower to reject the heat from its operation as required<br />

The chiller was <strong>in</strong>stalled together with its auxiliary steam and chilled-water supply, and test load<br />

systems <strong>in</strong> the IW. A web-based chiller automation system (CAS) was also <strong>in</strong>stalled to operate the<br />

chiller with its auxiliary systems, monitor the overall system status, and collect the experimental data.<br />

In this test-bed the absorption chiller was also <strong>in</strong>tegrated <strong>in</strong>to the IW and campus chilled-water system,<br />

so when the test was over, the chiller could provide chilled water to the IW and the campus.<br />

Experiments were carried out under a broad range of system operat<strong>in</strong>g parameters.<br />

In this work, both equipment test<strong>in</strong>g and mathematical model simulation of the chiller were comb<strong>in</strong>ed<br />

to provide a detailed understand<strong>in</strong>g of the equipment, to analyze the test data, to discover possible<br />

chiller design improvements and modifications, and to provide a method to design and evaluate<br />

overall <strong>BCHP</strong> systems.<br />

1.4.2 The Test Program and Experimental Data<br />

The chiller was tested by vary<strong>in</strong>g six operat<strong>in</strong>g parameters <strong>in</strong> turn: the chilled-water return temperature<br />

and flow rate, the cool<strong>in</strong>g-water supply temperature and flow rate, and the steam pressure. In the test<br />

program, only one parameter was adjusted at a time, and the others were kept at design conditions.<br />

Additional sensors were <strong>in</strong>stalled <strong>in</strong> the chiller beyond those provided by the manufacturer to operate<br />

the chiller and its auxiliary system to calculate chiller performance such as the coefficient of<br />

performance (COP) and cool<strong>in</strong>g capacity, and to observe chiller <strong>in</strong>ternal conditions. Experimental data<br />

obta<strong>in</strong>ed from 11 temperature sensors <strong>in</strong> the chiller were used to verify the predictions of the<br />

performance model.<br />

1.4.3 The Development of Computational Performance Model<br />

On the basis of scientific and eng<strong>in</strong>eer<strong>in</strong>g pr<strong>in</strong>ciples and the specific configurations of the chiller, a<br />

detailed computational performance model was constructed to evaluate the chiller performance under<br />

various operat<strong>in</strong>g conditions. This model was developed for the chiller to further ref<strong>in</strong>e the<br />

13


understand<strong>in</strong>g of the pr<strong>in</strong>ciples of the chiller, to analyze the experiment data from the test program, to<br />

assist <strong>in</strong> the equipment design, and to evaluate the performance of <strong>BCHP</strong> systems.<br />

The basic equation types <strong>in</strong>corporated <strong>in</strong> the model <strong>in</strong>clude: mass and energy balances,<br />

thermodynamic property relations, thermal and phase equilibrium relations, and heat and mass transfer<br />

coefficient correlations. The variables <strong>in</strong> these equations are the operat<strong>in</strong>g conditions – pressures,<br />

temperatures, compositions, and flows – throughout the chiller. The model <strong>in</strong>cludes 416 variables and<br />

409 equations. If seven operat<strong>in</strong>g conditions are specified, the model can be solved and all the<br />

operat<strong>in</strong>g conditions throughout chiller can be calculated.<br />

1.4.4 The <strong>An</strong>alysis of the Experimental Data<br />

To assess the performance data collected, an analytical method was developed that m<strong>in</strong>imizes the<br />

deviations between the experimental measurements and the model solutions. Several model<br />

assumptions were adjusted to improve the agreement between the experimental measurements and the<br />

model calculations. These adjustments significantly improved the agreement between the calculated<br />

and measured variables.<br />

1.5 Current <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Studies<br />

The microchiller performance model is one of the major efforts of this research. The literature for<br />

absorption chiller model studies has been reviewed; the exist<strong>in</strong>g model studies are categorized and<br />

summarized <strong>in</strong> the follow<strong>in</strong>g sections.<br />

1.5.1 <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Approaches<br />

In the past decades, computer models have been developed to <strong>in</strong>vestigate the performance of various<br />

water-LiBr absorption chiller cycles. Among these models, some [8, 9] are system specific for<br />

particular mach<strong>in</strong>es, flow configurations, and work<strong>in</strong>g materials. Others [10, 11, 12] are generic to<br />

handle various potential absorption cycles with one modularized model. The system specific models<br />

are performance models aimed at simulat<strong>in</strong>g a specific design and <strong>in</strong>vestigat<strong>in</strong>g its performance under<br />

various operation conditions; the generic models are aimed at explor<strong>in</strong>g novel absorption cycles and<br />

evaluat<strong>in</strong>g their performance under various boundary conditions.<br />

The advantage of system specific or performance models is that the model simulates the configuration<br />

of absorption chiller systems <strong>in</strong> detail. Thermodynamic cycle, heat, and mass transfer characteristics<br />

can be <strong>in</strong>vestigated on the basis of the physical details of the chiller. In these studies the simulation<br />

14


esults are verifiable through the chiller operations under various conditions. The difficulty of this type<br />

of model is that the accurate details of chiller configuration and design are not always available from<br />

the manufacturer. In most cases a simplified approach is adopted to solve the models, such as a<br />

specified heat transfer coefficient of specific chiller components provided by the manufacturer.<br />

The advantage of the generic cycle model is that programm<strong>in</strong>g effort is reduced by modular structure.<br />

A generic model is normally developed on the basis of the thermodynamic theory to <strong>in</strong>vestigate the<br />

performance of different absorption cycles and work<strong>in</strong>g fluids. This type of model is used <strong>in</strong> the<br />

conceptual design of an absorption mach<strong>in</strong>e. It can be used effectively to predict the performance of<br />

different design configurations, but because of its generic characteristics, it is difficult to <strong>in</strong>vestigate<br />

the details of the physical configuration of the chiller and its components.<br />

Beyond absorption cycle simulations, model<strong>in</strong>g efforts [13, 14, 15, 16, 17] focus ma<strong>in</strong>ly on chiller<br />

component design. Numerous model<strong>in</strong>g studies and experimental efforts have been made on comb<strong>in</strong>ed<br />

heat and mass transfer, work<strong>in</strong>g fluid additives, noncondensable gas measures, and other features of<br />

absorption chillers. These studies have advanced the capability for model<strong>in</strong>g absorption chillers. Some<br />

simulation results were found to be <strong>in</strong> good agreement with the experiments. On the basis of the<br />

experiments, some empirical correlations for comb<strong>in</strong>ed heat and mass transfer have been proposed for<br />

several typical absorber configurations and work<strong>in</strong>g fluids. The methods and results of these prior<br />

studies have been applied <strong>in</strong> the model<strong>in</strong>g efforts of this thesis.<br />

1.5.2 The Insufficiencies of Current <strong>Absorption</strong> <strong>Chiller</strong> Model<strong>in</strong>g Studies<br />

First, the exist<strong>in</strong>g simulation models of water-LiBr absorption chillers focus on relatively large-scale<br />

<strong>in</strong>stallations for commercial build<strong>in</strong>gs or for district energy centers. None of the studies consider<br />

microscale absorption chillers with a cool<strong>in</strong>g capacity less than 17 kW for residential or light<br />

commercial applications. There are, theoretically, no dist<strong>in</strong>ctions between the large-scale and the<br />

microscale absorption chillers <strong>in</strong> terms of scientific and eng<strong>in</strong>eer<strong>in</strong>g pr<strong>in</strong>ciples, but the design criteria<br />

and operat<strong>in</strong>g conditions for microscale absorption chillers are different from those for the large<br />

capacity chillers. For <strong>in</strong>stance, microscale absorption chillers for residential application must provide a<br />

more compact design and <strong>in</strong>clude a heat rejection unit, such as a cool<strong>in</strong>g tower.<br />

Second, at present, nearly all performance models of absorption chillers have been numerical<br />

simulations without significant experimental validation under design and off-design conditions. It has<br />

been difficult to <strong>in</strong>stall a commercial absorption chiller <strong>in</strong> a university laboratory because of their large<br />

capacity. The requirements for operation and test of commercial chillers and their limited<br />

15


<strong>in</strong>strumentations greatly restrict their accessibility for the experiments. The small cool<strong>in</strong>g capacity of a<br />

microscale chiller, however, makes it possible to provide a test cool<strong>in</strong>g load and to simulate a wide<br />

range of operation conditions for the chiller.<br />

Third, the model validation method has been simplified <strong>in</strong> the past studies. The deviations between<br />

the experimental and the performance simulation results for the COP and the cool<strong>in</strong>g capacity at a<br />

s<strong>in</strong>gle given operational condition are used to judge the overall quality of the model.<br />

F<strong>in</strong>ally, the available packaged absorption chiller models lack the flexibility to be <strong>in</strong>tegrated <strong>in</strong>to<br />

build<strong>in</strong>g simulation tools to support the design and analysis of absorption chiller-based <strong>BCHP</strong> systems.<br />

The work reported <strong>in</strong> this thesis addresses these <strong>in</strong>sufficiencies.<br />

1.6 The Comprehensive Performance Model and its <strong>Application</strong>s<br />

In this work, a steady-state performance model has been developed for the Broad BCT16 absorption<br />

chiller to further ref<strong>in</strong>e the understand<strong>in</strong>g of the pr<strong>in</strong>ciples of this chiller, to analyze the experiment<br />

data from the test program, to assist <strong>in</strong> the equipment design, and to evaluate the performance of<br />

<strong>BCHP</strong> systems.<br />

1.6.1 The <strong>Chiller</strong> Model Description<br />

In the model, the absorption chiller is composed of the follow<strong>in</strong>g components:<br />

• an evaporator: a countercurrent two-phase coiled tube heat exchanger<br />

• an absorber: a countercurrent two-phase coiled tube mass and heat exchanger<br />

• two regenerators: one high temperature, one <strong>in</strong>termediate temperature: well mixed, two-phase<br />

boil<strong>in</strong>g coiled tube heat exchangers<br />

• a condenser: a countercurrent heat exchanger<br />

• two plate heat <strong>in</strong>terchangers: countercurrent s<strong>in</strong>gle-phase heat exchangers<br />

• two tube and shell heat recovery exchangers: countercurrent s<strong>in</strong>gle-phase exchangers<br />

• three pumps: a sorbent pump, a refrigerant pump, and a chilled-water pump<br />

• associated spray nozzles, trap, valves, and pipe fitt<strong>in</strong>gs<br />

The cool<strong>in</strong>g tower associated with this chiller <strong>in</strong>cludes the follow<strong>in</strong>g components:<br />

• a countercurrent plate column two-phase mass and heat exchanger<br />

16


• a cool<strong>in</strong>g-water pump<br />

• an air fan<br />

The complete steady-state chiller model is composed of the follow<strong>in</strong>g nonl<strong>in</strong>ear algebraic equations<br />

applicable to each of the above chiller and cool<strong>in</strong>g-tower components:<br />

• two mass balances, water and LiBr<br />

• an energy balance<br />

• thermodynamic property relations for stream enthalpies as a function of pressure, temperature,<br />

and composition<br />

• phase equilibrium relations among pressure, temperature, and compositions of the coexist<strong>in</strong>g<br />

phases<br />

• the appropriate heat transfer (and for the absorber and cool<strong>in</strong>g tower, mass transfer) relations<br />

• correlations of overall heat and mass transfer coefficients, U and K, for the respective<br />

components based on their specific design and operat<strong>in</strong>g conditions, (see chapter 3)<br />

• work computations for the pumps and fan<br />

These equations <strong>in</strong>volve, as variables, the properties – pressure, temperature, composition, and flow –<br />

of all the phases present <strong>in</strong> and flows among the chiller components. The completed chiller model<br />

<strong>in</strong>terrelates variables of all these equations based on the configuration and the flow diagram, of the<br />

chiller. In general it has been assumed that:<br />

• The properties of a stream leav<strong>in</strong>g a component to an <strong>in</strong>terconnected component are those of<br />

eithera liquid or a vapor, thus the quality of the stream is either 1.0 or 0.0<br />

• There is no pressure loss and no heat loss/ga<strong>in</strong> <strong>in</strong> the l<strong>in</strong>es connect<strong>in</strong>g the components<br />

• Tthe sorbent solution charged to the chiller has a concentration of 55% LiBr. Once the chiller<br />

operates under design conditions, the concentration difference of the sorbent solutions flow <strong>in</strong><br />

and out of the high-temperature regenerator is roughly at 5%; that of the <strong>in</strong>termediate<br />

temperature regenerator is approximately 4%. Dilute sorbent is distributed to the two<br />

regenerators <strong>in</strong> approximately equal quantities.<br />

The completed chiller model <strong>in</strong>volves 416 variables and 409 nonl<strong>in</strong>ear algebraic equations. Solv<strong>in</strong>g<br />

the model and determ<strong>in</strong><strong>in</strong>g values for all the chiller variables therefore requires specify<strong>in</strong>g values for<br />

seven operat<strong>in</strong>g parameters. In this work, the specified operat<strong>in</strong>g parameters are: the chilled water<br />

17


<strong>in</strong>let and outlet temperatures and flow, the cool<strong>in</strong>g-water supply temperature and flow, the steam<br />

supply pressure and flow.<br />

1.6.2 <strong>Application</strong>s of the <strong>Chiller</strong> Performance Design Model<br />

This chiller performance model has been used <strong>in</strong> various forms for various applications: prelim<strong>in</strong>ary<br />

design, detailed design, and performance data analysis by<br />

• exclud<strong>in</strong>g or <strong>in</strong>clud<strong>in</strong>g various model equations<br />

• mak<strong>in</strong>g various assumptions relat<strong>in</strong>g to the model equations<br />

• specify<strong>in</strong>g various <strong>in</strong>put and correspond<strong>in</strong>g output variables or operat<strong>in</strong>g conditions<br />

1.6.2.1 Prelim<strong>in</strong>ary Design Computations<br />

The steam flow and the pump work for a given cool<strong>in</strong>g load – chilled-water <strong>in</strong>let and outlet<br />

temperatures and flow – and the <strong>in</strong>ternal operat<strong>in</strong>g conditions throughout the chiller can conveniently<br />

be estimated from a simplified form of the model by<br />

• exclud<strong>in</strong>g heat and mass transfer relations and correlations<br />

• fix<strong>in</strong>g the composition of the circulat<strong>in</strong>g sorbent solution<br />

• assum<strong>in</strong>g that<br />

o the operat<strong>in</strong>g temperatures (and the correspond<strong>in</strong>g equilibrium pressures) of the<br />

evaporator, absorber, high and <strong>in</strong>termediate temperature regenerators, respectively, are<br />

those of the outlet chilled water, the <strong>in</strong>let cool<strong>in</strong>g water, the steam supply, the condens<strong>in</strong>g<br />

temperature of the refrigerant vapor from the high-temperature regenerator.<br />

o the operat<strong>in</strong>g pressure of the condenser (with its correspond<strong>in</strong>g pressure) is that of the<br />

<strong>in</strong>termediate temperature regenerator.<br />

o heat transfer <strong>in</strong> the countercurrent <strong>in</strong>terchangers and heat recovery exchangers is<br />

maximized by equal stream temperatures at one end of the exchanger.<br />

Prelim<strong>in</strong>ary design computations have proved useful <strong>in</strong> explor<strong>in</strong>g the effects of various chiller<br />

configurations, component characteristics, and external operat<strong>in</strong>g conditions on the heat<strong>in</strong>g and<br />

cool<strong>in</strong>g requirements, <strong>in</strong>ternal conditions, and power requirements of a chiller.<br />

A prelim<strong>in</strong>ary design model was programmed to estimate the heat/mass transfer areas of the chiller<br />

components; this was a first step <strong>in</strong> construct<strong>in</strong>g a comprehensive performance model. If the design<br />

18


conditions, the desired performance, the specific configuration, and the reasonable assumptions are<br />

<strong>in</strong>corporated <strong>in</strong> the model, the heat transfer area, UA, of chiller components can be calculated. The UA<br />

is def<strong>in</strong>ed as the product of overall heat transfer coefficient (U) and the total <strong>in</strong>ternal contact area (A):<br />

• The design conditions are these specified conditions (temperature, pressure, and flow) of<br />

chilled water, cool<strong>in</strong>g water, and heat sources at a specified load condition<br />

• The performance parameters are the values of COP and cool<strong>in</strong>g capacity<br />

• The operat<strong>in</strong>g parameters are the conditions (temperature, pressure, and flow) of chilled water,<br />

cool<strong>in</strong>g water, and heat source at any operat<strong>in</strong>g conditions<br />

• The specific chiller configuration <strong>in</strong>cludes the <strong>in</strong>formation such as one-stage or two-stage,<br />

parallel- or series-sorbent flow (for a two-stage absorption chiller), heat source types, work<strong>in</strong>g<br />

fluids, and other details of the chiller<br />

1.6.2.2 Detailed Design and Performance Computations<br />

On the basis of the design model, the performance model was constructed to predict chiller<br />

performance and to analyze the measured experimental data. First, the performance model took the<br />

<strong>in</strong>itial UA estimations from the design model to predict chiller performance under design conditions;<br />

then, the actual Us and As were calculated from the actual chiller physical configurations and from the<br />

heat and mass transfer correlations from the literature. The heat transfer correlations were corrected by<br />

compar<strong>in</strong>g the actual Us and As and the UA solutions from the design model, and then, the corrected<br />

UA correlations were used to predict the chiller performance for design and off-design operations.<br />

Heat (and mass) transfer areas required <strong>in</strong> the various components of the chiller can be estimated by<br />

the performance model by<br />

• apply<strong>in</strong>g known conditions for steam flow, pump work, etc.<br />

• <strong>in</strong>clud<strong>in</strong>g heat and mass transfer relations and correlations from the literature <strong>in</strong> the model<br />

• fix<strong>in</strong>g the composition of the circulat<strong>in</strong>g sorbent solution<br />

• assum<strong>in</strong>g “approach” temperatures (and pressures) for heat (and mass) transfer occurr<strong>in</strong>g <strong>in</strong><br />

each of the various chiller components.<br />

The calculated transfer area values for the given design values of the external operat<strong>in</strong>g conditions –<br />

the chilled-water <strong>in</strong>let and outlet temperatures and flow, the steam conditions (temperature and<br />

pressure), the cool<strong>in</strong>g water <strong>in</strong>let temperature and flow – can then be used <strong>in</strong> the model to determ<strong>in</strong>e<br />

the effects of off design external operat<strong>in</strong>g conditions on chiller performance.<br />

19


1.6.3 Data analysis<br />

The outputs of performance model were also compared with test data under various conditions by<br />

chang<strong>in</strong>g the operation parameters. Based on the performance model, the accuracy and reliability of<br />

the experimental data were assessed, and the model assumptions were validated.<br />

Measured chiller external and <strong>in</strong>ternal operat<strong>in</strong>g conditions can be used to compare those calculated<br />

from the chiller model with the results when the model is supplied with the external operat<strong>in</strong>g<br />

conditions and component areas.<br />

These comparisons can be used to evaluate the accuracy of measurements and to consider the validity<br />

of the model <strong>in</strong>clud<strong>in</strong>g the assumptions on which the model is based. Such comparisons and<br />

conclusions based on those comparisons are discussed <strong>in</strong> detail <strong>in</strong> chapter 3. Several measurements<br />

that differ significantly from model predicted values have been analyzed, and the procedures for<br />

correct<strong>in</strong>g these measurements have been proposed and applied.<br />

On the basis of the model developed <strong>in</strong> this thesis, the validated model can then be extended to<br />

<strong>in</strong>corporate the follow<strong>in</strong>g heat sources:<br />

• hot water from solar thermal or heat recovery equipment<br />

• natural gas<br />

• exhaust gas from gas turb<strong>in</strong>e, eng<strong>in</strong>e generator, and fuel cells<br />

The validated models, as a tool, can be <strong>in</strong>tegrated with the IW model to evaluate overall <strong>BCHP</strong> system<br />

performance <strong>in</strong>corporat<strong>in</strong>g with a cost model.<br />

1.7 Chapter Overview<br />

This thesis conta<strong>in</strong>s five chapters followed by references, and appendixes, and list of abbreviations.<br />

Chapter 1, Introduction <strong>in</strong>troduces the background and motivation of this dissertation and<br />

summarizes the research objectives of this chapter. The emerg<strong>in</strong>g features of the modern absorption<br />

chiller <strong>in</strong>dustry are summarized <strong>in</strong> appendix 1A.<br />

Chapter 2, <strong>Chiller</strong> Test System and Performance <strong>in</strong>troduces the chiller and exam<strong>in</strong>es the overall<br />

experimental system setups. It presents detailed <strong>in</strong>formation concern<strong>in</strong>g the <strong>in</strong>strumentation and<br />

control for the chiller and its auxiliary systems. The chiller test<strong>in</strong>g program, measured experimental<br />

20


data, and chiller performance are presented. The chiller <strong>in</strong>ternal control pr<strong>in</strong>ciples and the system<br />

operation <strong>in</strong>structions are presented <strong>in</strong> appendixes 2A and 2B, respectively.<br />

Chapter 3, Computational Model describes the framework of the performance model with<strong>in</strong> which<br />

the absorption chiller component modules are developed. It provides an <strong>in</strong>-depth presentation of the<br />

govern<strong>in</strong>g equations and model<strong>in</strong>g assumptions. The computational and numerical issues are<br />

addressed <strong>in</strong> the various stages of the absorption chiller component model<strong>in</strong>g <strong>in</strong> appendix 3A; the<br />

source code of the performance model is attached <strong>in</strong> appendix 3B.<br />

Chapter 4, Model-based Data <strong>An</strong>alysis assesses the model calculations and experimental data<br />

accuracy and reliability to learn how to validate the model as well as improve the equipment designs.<br />

The analysis results presented regard the test programs that vary for five operat<strong>in</strong>g parameters: chilledwater<br />

supply temperature and flow, cool<strong>in</strong>g-water supply temperature and flow, and steam supply<br />

pressure. When analyz<strong>in</strong>g the experimental data, opportunities to improve the accuracy of the model<br />

became apparent. Consequently, the adjustments to model assumptions significantly improved the<br />

agreement between the calculated and the measured variables.<br />

Chapter 5, Contributions and Areas for Future Research summarizes the contributions of this<br />

thesis and suggests future areas for research and the issues <strong>in</strong>volved, <strong>in</strong>clud<strong>in</strong>g: extension of the<br />

validated steam-driven absorption chiller model to several other heat sources: hot water, natural gas,<br />

and exhaust gases. The chiller performance models can be <strong>in</strong>tegrated and evaluated <strong>in</strong>to overall <strong>BCHP</strong><br />

system configurations on an annual basis.<br />

21


2 <strong>Chiller</strong> Test System and Program<br />

As a first step <strong>in</strong> provid<strong>in</strong>g an energy supply system for CMU’s IW, a 16kW, steam-driven, two-stage<br />

absorption chiller was <strong>in</strong>stalled together with an auxiliary steam supply and a variable load for the<br />

chiller test and performance evaluation. A web-based data acquisition and control system was<br />

developed to operate the chiller and its auxiliary equipment while stor<strong>in</strong>g and display<strong>in</strong>g the test<br />

measurement data. The chiller was tested at various operat<strong>in</strong>g conditions <strong>in</strong> accordance with a test<br />

program. In the future, the chiller and its control system will be <strong>in</strong>corporated <strong>in</strong> the cool<strong>in</strong>g system of<br />

the IW and connected with the campus chilled-water supply system.<br />

2.1 <strong>Absorption</strong> <strong>Chiller</strong><br />

2.1.1 System Descriptions<br />

The absorption chiller <strong>in</strong>stalled <strong>in</strong> the IW is a steam-driven, two-stage, water-LiBr, parallel-sorbentflow<br />

series-cool<strong>in</strong>g-water flow chiller with a cool<strong>in</strong>g tower. This chiller, provided by Broad Co., has a<br />

16kW rated cool<strong>in</strong>g capacity. It is the smallest absorption chiller available <strong>in</strong> the exist<strong>in</strong>g market and<br />

the only steam-driven absorption chiller of such capacity <strong>in</strong> the world.<br />

Figure 2-1 shows the absorption chiller <strong>in</strong>stalled on<br />

a platform adjacent to the IW. The chilled-water<br />

supply and return, steam supply, condensate return,<br />

power, and city water l<strong>in</strong>es connect with the chiller<br />

at the bottom left. Figure 2-2 is a schematic flow<br />

diagram recreated from the manufacturer’s brochure<br />

for a commercial natural-gas direct-fired chiller; this<br />

flow diagram shows all the heat and mass transfer<br />

components, pumps, and pipe fitt<strong>in</strong>gs. It also<br />

<strong>in</strong>dicates the design values for temperatures<br />

throughout the chiller. The measurement and<br />

control features of the chiller will be discussed <strong>in</strong><br />

conjunction with a detailed process and<br />

<strong>in</strong>strumentation (P&I) diagram <strong>in</strong> the section that<br />

follows. The components and parts <strong>in</strong>dicated <strong>in</strong><br />

Figure 2-2 are listed <strong>in</strong> Table 2-1.<br />

Figure 2-1: <strong>Absorption</strong> chiller <strong>in</strong>stalled <strong>in</strong> the IW<br />

22


Figure 2-2: Schematic diagram of the absorption chiller<br />

Table 2-1: Component names and correspond<strong>in</strong>g abbreviations<br />

Abbreviation Name Abbreviation Name<br />

ABS Absorber EVP Evaporator<br />

BPHX By-pass heat exchanger HTRG High-temperature regenerator<br />

CHSV Cool<strong>in</strong>g/heat<strong>in</strong>g switch valve HRHX Heat recovery heat exchanger<br />

CHWBPV Chilled-water by-pass valve HTHX High-temperature heat exchanger<br />

CHWP Chilled-water pump LTHX Low-temperature heat exchanger<br />

COND Condenser LTRG Low-temperature regenerator<br />

CT Cool<strong>in</strong>g tower RBPSV Refrigerant by-pass solenoid valve<br />

CTOF City-water overflow RP Refrigerant pump<br />

CTWS City-water switch RPH Refrigerant pump heater<br />

CWBPV Cool<strong>in</strong>g-water by-pass valve SF Steam filter<br />

CWDD Cool<strong>in</strong>g-water dra<strong>in</strong> device SP Solution pump<br />

CWDV Cool<strong>in</strong>g-water detergent valve ST Steam trap<br />

CTF Cool<strong>in</strong>g-tower fan SV Steam valve<br />

CWP Cool<strong>in</strong>g-water pump<br />

23


The absorption chiller <strong>in</strong> Figure 2-2 consists of five major and four m<strong>in</strong>or heat transfer components,<br />

three pumps, a cool<strong>in</strong>g tower, an automatic <strong>in</strong>ert gas purge device, and the associated valves and pipe<br />

fitt<strong>in</strong>gs. Specifically, the five major components are:<br />

• an evaporator, a countercurrent two-phase heat exchanger<br />

• an absorber, a countercurrent two-phase heat and mass exchanger<br />

• a high-temperature regenerator (HTRG), a well-mixed, two-phase, boil<strong>in</strong>g heat exchanger<br />

• a low-temperature regenerator (LTRG), a well-mixed, two-phase boil<strong>in</strong>g heat exchanger<br />

• a condenser, a countercurrent heat exchanger<br />

The four m<strong>in</strong>or components are:<br />

• a high-temperature heat <strong>in</strong>terchanger (HTHX), a countercurrent, s<strong>in</strong>gle-phase heat exchanger<br />

• a low-temperature heat <strong>in</strong>terchanger (LTHX), a countercurrent, s<strong>in</strong>gle-phase heat exchanger<br />

• a heat recovery heat exchanger (HRHX), a countercurrent, s<strong>in</strong>gle-phase heat exchanger<br />

• a refrigerant by-pass heat exchanger (BPHX), a countercurrent, s<strong>in</strong>gle-phase heat exchanger<br />

The three pumps are:<br />

• a solution pump (SP), a variable-speed pump<br />

• a chilled-water pump (CHWP), a s<strong>in</strong>gle-speed pump<br />

• a refrigerant pump (RP), a s<strong>in</strong>gle-speed pump<br />

The cool<strong>in</strong>g tower (CT) <strong>in</strong>cludes:<br />

• a countercurrent vertical plate column; a two-phase, mass and heat exchanger<br />

• a cool<strong>in</strong>g-water pump (CWP); a s<strong>in</strong>gle-speed pump<br />

• a cool<strong>in</strong>g-tower fan (CTF); a three-speed air fan<br />

• associated valves and dra<strong>in</strong> devices<br />

Other associated components <strong>in</strong>clude:<br />

• an automatic gas purge device (AGPD)<br />

• associated valves, spray nozzles, and pipe fitt<strong>in</strong>gs<br />

24


Figure 2-3: Structure of the absorption chiller<br />

The physical arrangement of the absorption chiller is shown <strong>in</strong> Figure 2-3. The ma<strong>in</strong> body of the<br />

chiller consists of two sealed vessels: the upper one at an elevated pressure, the lower vessel at a high<br />

vacuum. The upper vessel <strong>in</strong>cludes the HTRG, the LTRG, and the condenser. The lower vessel<br />

<strong>in</strong>cludes the absorber, the evaporator, the BPHX, the LTHX, and the HTHX. The flows of sorbent<br />

solutions, refrigerant, and cool<strong>in</strong>g water penetrate the vessel walls <strong>in</strong> pipes between the two vessels.<br />

The high vacuum <strong>in</strong> the lower vessel is ma<strong>in</strong>ta<strong>in</strong>ed by the AGPD and a manual vacuum pump<br />

<strong>in</strong>dependent of the chiller. The chilled water and cool<strong>in</strong>g water are circulated by the CHWP and the<br />

CWP, respectively. The <strong>in</strong>clusion of the cool<strong>in</strong>g tower enables chiller <strong>in</strong>stallation where cool<strong>in</strong>g water<br />

may be unavailable.<br />

Table 2-2: Specifications of the absorption chiller<br />

Chilled water<br />

Steam<br />

Power<br />

Solution<br />

Name Quantity Unit<br />

Cool<strong>in</strong>g capacity 16 kW<br />

Chilled-water return temperature 14<br />

o<br />

C<br />

Chilled-water supply temperature 7<br />

Chilled-water flow rate 2 m 3 /h<br />

Chilled-water pump head 8 mH2O<br />

Rated steam pressure, absolute 0.7 mPa<br />

Steam pressure limit, absolute 0.9 mPa<br />

Maximum steam consumption 24 kg/h<br />

Power voltage 220 V<br />

Power frequency 60 Hz<br />

Maximum power consumption 1 kW<br />

Water-LiBr sorbent solution mass 65 Kg<br />

Water-LiBr sorbent concentration 55 %<br />

o C<br />

25


Table 2-2 lists the chiller specifications from the manufacturer; these are the only published<br />

performance data for this unique chiller. A test program was developed to <strong>in</strong>vestigate chiller<br />

performance and to provide additional measurements of chiller operat<strong>in</strong>g conditions. The chiller<br />

specification data are useful <strong>in</strong> evaluat<strong>in</strong>g the results of the chiller tests. The chiller work<strong>in</strong>g pr<strong>in</strong>ciples<br />

are described <strong>in</strong> the follow<strong>in</strong>g sections.<br />

2.1.2 Evaporator and Chilled-Water Pump<br />

The evaporator of the chiller, shown <strong>in</strong> Figures 2-2 and 2-4, occupies the lower vessel. The evaporator<br />

tube bank comprises two parallel tubes spiral<strong>in</strong>g 18 times from the bottom to the top of the coil. Water<br />

refrigerant is distributed evenly over the tubes <strong>in</strong> the bank by nozzles spray<strong>in</strong>g water from the<br />

condenser. Water that was not evaporated <strong>in</strong> the first pass collects <strong>in</strong> the refrigerant tray at the base of<br />

the evaporator and is recirculated by the refrigerant pump. The refrigerant vaporizes <strong>in</strong> the evaporator<br />

at low pressure, about 0.8-1.0 kPa, and low temperature, about 3-4 o C. The vaporization absorbs heat<br />

from the chilled water flow<strong>in</strong>g through the evaporator coil, cool<strong>in</strong>g this flow from 14 o C to 7 o C.<br />

Figure 2-4: Configuration of the lower vessel<br />

26


At a constant flow rate of 2 m 3 /h and a head of 8 mH2O to overcome the pressure loss, the evaporator<br />

functions as a countercurrent, two-phase heat exchanger. The steam flow to the HTRG is adjusted to<br />

ma<strong>in</strong>ta<strong>in</strong> a constant refrigerant level water tray reservoir; a low level requires an <strong>in</strong>crease <strong>in</strong> the steam<br />

flow to provide more refrigerant. The chiller control system is discussed <strong>in</strong> appendix 2.A<br />

2.1.3 Absorber and Solution Pump<br />

The absorber, shown <strong>in</strong> Figures 2-2 and 2-4, ma<strong>in</strong>ta<strong>in</strong>s the low operat<strong>in</strong>g pressure required <strong>in</strong> the<br />

evaporator. It is a spiral tube bank, consist<strong>in</strong>g of two tubes spiral<strong>in</strong>g from the bottom to the top. The<br />

coil surrounds the evaporator but is separated from it by a chevron separator to prevent carryover of<br />

refrigerant liquid. Concentrated water-LiBr sorbent solution is distributed evenly over the tubes of the<br />

absorber coil by nozzles spray<strong>in</strong>g sorbent from the two regenerators, cooled <strong>in</strong> the HTHX and the<br />

LTHX. The water refrigerant vapor from the evaporator passes through the chevron separator, enters<br />

the absorber, and is absorbed <strong>in</strong> the water-LiBr sorbent flow<strong>in</strong>g 5 m 3 /h over the coil. The heat released<br />

by the sorption of the refrigerant <strong>in</strong> the sorbent is transferred to the cool<strong>in</strong>g water flow<strong>in</strong>g <strong>in</strong> the tubes<br />

of the coil, <strong>in</strong>creas<strong>in</strong>g its temperature of 30 o C. The cool<strong>in</strong>g water circulates to the condenser and then<br />

to the cool<strong>in</strong>g tower of the chiller where the sorption heat is rejected to the surround<strong>in</strong>gs by<br />

evaporation. The concentrated sorbent solution becomes dilute by absorb<strong>in</strong>g the refrigerant vapor. The<br />

dilute sorbent solution, collected <strong>in</strong> the solution reservoir at the bottom of the lower vessel, is pumped<br />

back to the HTRG and LTRG with pressure about 10 kPa and 100 kPa, respectively, either <strong>in</strong> series or<br />

<strong>in</strong> parallel by the solution pump for regeneration.<br />

2.1.4 High-Temperature Regenerator<br />

The water-LiBir sorbent solution, diluted by absorbed water refrigerant vapor, is pumped <strong>in</strong> the Broad<br />

chiller to the two regenerators <strong>in</strong> parallel: the HTRG and the LTRG. In each regenerator, the<br />

refrigerant water vapor added to the sorbent <strong>in</strong> the absorber is removed by evaporation at elevated<br />

temperature and pressure. Approximately equal quantities of sorbent solution are fed to each<br />

regenerator controlled by a flow restriction device <strong>in</strong> the pipe leav<strong>in</strong>g the solution pump. In the<br />

HTRG, steam <strong>in</strong> a coil is used to boil off refrigerant vapor from the sorbent. The temperature and<br />

pressure of the refrigerant vapor produced <strong>in</strong> the HTRG is high enough to generate an approximately<br />

equal quantity of refrigerant vapor from the sorbent <strong>in</strong> the LTRG operat<strong>in</strong>g at a lower temperature and<br />

pressure. The driv<strong>in</strong>g heat provided to the HTRG is thus cascaded and used twice. This makes the<br />

absorption cycle a two-stage process. The generation of additional refrigerant from a given heat <strong>in</strong>put,<br />

improves significantly the cycle performance.<br />

27


The design of the HTRG differs depend<strong>in</strong>g both on the heat<strong>in</strong>g medium, gas, or liquid, and on its<br />

temperature. Many forms of thermal energy can be used <strong>in</strong> the HTRG to drive a two-stage absorption<br />

chiller, such as steam, hot water, exhaust gas, natural gas, oil, and liquid pressurized gas. In this<br />

section, only the steam-driven HTRG is discussed; other k<strong>in</strong>ds of heat sources - natural gas, hot water,<br />

and exhaust gas - are discussed <strong>in</strong> the sections that follow.<br />

The water-LiBr sorbent, reconcentrated <strong>in</strong> the regenerators, returns to the absorber through flow<br />

restrictions that assist <strong>in</strong> ma<strong>in</strong>ta<strong>in</strong><strong>in</strong>g appropriate liquid levels to submerge the heat transfer coils <strong>in</strong> the<br />

regenerators. The solution pump frequency is adjusted to ma<strong>in</strong>ta<strong>in</strong> a constant level <strong>in</strong> the HTRG.<br />

Both the HTRG and the LTRG use water vapor as<br />

a heat resource; they have similar functions and<br />

structure. The heat transfer process <strong>in</strong>cludes<br />

condensation <strong>in</strong>side the tubes and boil<strong>in</strong>g on the<br />

outer surface of these tubes.<br />

The configuration of the upper vessel for the<br />

absorption chiller <strong>in</strong>stalled <strong>in</strong> the IW is similar to<br />

that of a natural gas direct-fired absorption chiller<br />

of the same capacity shown <strong>in</strong> Figure 2-5. The<br />

combustion chamber and convection chamber of<br />

the natural-gas-fired HTRG are replaced by a<br />

spiral tube bank <strong>in</strong> the steam-driven HTRG to<br />

vaporize water refrigerant from the water-LiBr<br />

sorbent.<br />

Figure 2-5: Configuration of the upper vessel<br />

The major part of the HTRG is a spiral tube bank with three parallel tubes spiral<strong>in</strong>g eleven rounds<br />

from the top to the bottom. Steam supply flows <strong>in</strong> parallel through the tubes from top to bottom. The<br />

dilute sorbent solution is pumped <strong>in</strong>to the HTRG from the bottom of the tank, and the concentrated<br />

sorbent solution leaves the HTRG from the bottom of the tank at a distant po<strong>in</strong>t. The vigorous mix<strong>in</strong>g<br />

result<strong>in</strong>g from the boil<strong>in</strong>g <strong>in</strong> the regenerator m<strong>in</strong>imizes sorbent concentration differences <strong>in</strong> the HTRG.<br />

While mass transfer is <strong>in</strong>volved as water diffuses to and is evaporated from the sorbent-vapor<br />

<strong>in</strong>terface, the vigorous mix<strong>in</strong>g m<strong>in</strong>imizes mass transfer resistance. The HTRG thus functions as a<br />

well-mixed two-phase boil<strong>in</strong>g heat exchanger.<br />

28


At design conditions, the HTRG requires a steam supply at 0.7 mPa; the maximum steam supply<br />

pressure is 0.9 mPa, and the maximum flow rate is 24 kg/h. <strong>An</strong> elevated pressure, typically at a<br />

saturated vapor pressure of 100 kPa, is ma<strong>in</strong>ta<strong>in</strong>ed <strong>in</strong> the HTRG to provide a condens<strong>in</strong>g temperature<br />

of about 100 o C.<br />

2.1.5 Low-Temperature Regenerator<br />

The LTRG is a staggered tube bank with 14 parallel tubes circulat<strong>in</strong>g once around. Vapor from the<br />

HTRG enters at one end of each parallel tube, and condensate leaves the other end of the tubes and<br />

enters the condenser. One end of each tube is connected to the HTRG, the other, to the condenser. The<br />

refrigerant, water, and vapor from the HTRG passes through the LTRG tubes and transfers the heat of<br />

condensation to the sorbent solution surround<strong>in</strong>g the tube bank. The dilute sorbent solution enters the<br />

LTRG on the top; the concentrated sorbent solution leaves from the bottom. Refrigerant vapor is<br />

boiled off; the dilute sorbent solution is concentrated. Similar to the HTRG, the boil<strong>in</strong>g process <strong>in</strong> the<br />

LTRG is violent; bubbles stir the sorbent solution. The concentration of the sorbent <strong>in</strong> the LTRG is<br />

therefore nearly uniform, close to the exit value, and mass transfer is not a limit<strong>in</strong>g process. Similar to<br />

the HTRG, the LTRG functions as a well-mixed, two-phase boil<strong>in</strong>g heat exchanger.<br />

The LTRG has a lower boil<strong>in</strong>g temperature and pressure than the HTRG. At design conditions, a<br />

medium pressure, typically at a saturated vapor pressure of 10 kPa, is ma<strong>in</strong>ta<strong>in</strong>ed to provide an<br />

evaporat<strong>in</strong>g temperature of about 45 o C. The LTRG has no solution level control like the HTRG, but<br />

the maximum solution level is measured <strong>in</strong> the LTRG to prevent crystallization <strong>in</strong> the LTHX. The<br />

details of the control pr<strong>in</strong>ciples are discussed <strong>in</strong> appendix 2.A.<br />

2.1.6 Condenser<br />

The condenser and the LTRG are housed <strong>in</strong> the same vessel with the HTRG, and they operate at the<br />

same <strong>in</strong>termediate pressure. The condensate from the LTRG flashes <strong>in</strong>to the condenser operat<strong>in</strong>g at<br />

<strong>in</strong>termediate pressure. The condenser then condenses both the vapor produced <strong>in</strong> this flash<strong>in</strong>g and the<br />

water vapor from the LTRG, transferr<strong>in</strong>g heat <strong>in</strong>to cool<strong>in</strong>g water flow<strong>in</strong>g <strong>in</strong>to the condenser coil. This<br />

condensate is returned to the evaporator.<br />

The condenser is a spiral copper tube bank with three parallel tubes spiral<strong>in</strong>g three rounds from the<br />

bottom to the top. The cool<strong>in</strong>g water flow<strong>in</strong>g from the absorber enters the condenser from the bottom<br />

and leaves the condenser to the cool<strong>in</strong>g tower at the top. The liquid condensed from the vapor as a<br />

29


film on the surface of tube bank drips down to a dra<strong>in</strong> pan that separates the condenser from the LTRG.<br />

The condenser functions as a two-phase, countercurrent heat exchanger.<br />

2.1.7 Heat Recovery Devices<br />

In Figure 2-2, the four m<strong>in</strong>or heat transfer components <strong>in</strong> the chiller are used to recover thermal<br />

energy by heat exchange between the various refrigerant, sorbent, and steam condensate streams. All<br />

these exchangers are s<strong>in</strong>gle-phase, countercurrent heat exchangers that recover heat from a hot stream<br />

and deliver it to a cold stream. One is the LTHX, and the other is the HTHX. These <strong>in</strong>terchangers<br />

reduce the heat requirements of the regenerators and the cool<strong>in</strong>g requirement of the absorber.<br />

In the chiller, the temperature of the condensate leav<strong>in</strong>g the HTRG is high enough to be used to<br />

preheat the dilute solution from the LTHX before it enters the LTRG. A heat recovery exchanger<br />

between the steam condensate and the sorbent stream enter<strong>in</strong>g the LTRG reduces the heat requirement<br />

of the LTRG and the temperature of the steam condensate, avoid<strong>in</strong>g its flash<strong>in</strong>g <strong>in</strong> the condensate tank.<br />

A heat recovery exchanger between the water refrigerant leav<strong>in</strong>g the condenser and the sorbent pool <strong>in</strong><br />

the absorber, called the by-pass heat exchanger (BPHX), <strong>in</strong>creases cool<strong>in</strong>g <strong>in</strong> the evaporator. Broad<br />

terms it an elbow-heat exchanger. In the elbow, the liquid refrigerant condensed from the condenser<br />

releases a small amount of heat to the dilute solution <strong>in</strong> the absorber.<br />

2.1.8 Cool<strong>in</strong>g Tower<br />

A cool<strong>in</strong>g tower is widely used to dissipate reject heat from a water-cooled air-condition<strong>in</strong>g system to<br />

the surround<strong>in</strong>gs. This Broad absorption chiller has a built-<strong>in</strong> cool<strong>in</strong>g tower, as shown <strong>in</strong> Figures 2-2<br />

and 2-6. Its compact design facilitates chiller <strong>in</strong>stallation and operation. The cool<strong>in</strong>g water <strong>in</strong> the<br />

chiller flows <strong>in</strong> series through the absorber, the condenser, and then through the cool<strong>in</strong>g tower. This<br />

arrangement provides for a m<strong>in</strong>imum operat<strong>in</strong>g temperature <strong>in</strong> the absorber that is required to achieve<br />

a low chilled-water temperature; the high flow <strong>in</strong> both the absorber and the condenser provides for<br />

high heat transfer coefficients <strong>in</strong> these components. The recirculat<strong>in</strong>g cool<strong>in</strong>g water flows down<br />

vertical plates <strong>in</strong> countercurrent contact with upward-flow<strong>in</strong>g ambient air.<br />

Evaporation of a small portion of the water flow<strong>in</strong>g downward through the cool<strong>in</strong>g tower reduces its<br />

temperature; makeup water added to the cool<strong>in</strong>g tower replaces that evaporated. The air temperature is<br />

also reduced, but the humidity <strong>in</strong>creases markedly. Thus, the cool<strong>in</strong>g tower functions as a two-phase<br />

countercurrent heat and mass exchanger.<br />

30


As illustrated <strong>in</strong> Figure 2-6, the cool<strong>in</strong>g tower attached<br />

to the chiller comprises spray nozzles, vertical PVC<br />

plates, a PVC mist collector, a cool<strong>in</strong>g-water tank, a<br />

cool<strong>in</strong>g-water pump, a cool<strong>in</strong>g-water by-pass valve,<br />

and a cool<strong>in</strong>g-air fan along with devices for water<br />

dra<strong>in</strong> and city-water supply and detergent addition.<br />

The major components of the cool<strong>in</strong>g tower are the<br />

PVC vertical plates (a heat and mass transfer medium)<br />

that <strong>in</strong>crease water/air contact surface as well as the<br />

duration of contact. The closely packed vertical PVC<br />

plates are spaced with staggered bars <strong>in</strong>stalled below<br />

the spray nozzles <strong>in</strong> the air path. At design conditions,<br />

the cool<strong>in</strong>g water is distributed from the top of the<br />

tower through spray nozzles at a temperature of 35.5<br />

o<br />

C. The speed of the cool<strong>in</strong>g tower air fan is varied to<br />

ma<strong>in</strong>ta<strong>in</strong> the cool<strong>in</strong>g-water supply to the chiller at 30<br />

o C.<br />

Figure 2-6: Configuration of cool<strong>in</strong>g tower<br />

From chiller<br />

City water<br />

To chiller<br />

CWP<br />

Dra<strong>in</strong><br />

CWBPV<br />

CWDV<br />

CTWS<br />

CWDD<br />

Air outlet<br />

Air <strong>in</strong>let<br />

PVC mist<br />

collector<br />

Spray<br />

nozzles<br />

PVC Plates<br />

CTF<br />

Water tank<br />

As illustrated <strong>in</strong> Figure 2-6, the cool<strong>in</strong>g tower attached to the chiller comprises spray nozzles, vertical<br />

PVC plates, a PVC mist collector, a cool<strong>in</strong>g-water tank, a cool<strong>in</strong>g-water pump, a cool<strong>in</strong>g-water bypass<br />

valve, and a cool<strong>in</strong>g-air fan along with devices for water dra<strong>in</strong> and city-water supply and<br />

detergent addition. The major components of the cool<strong>in</strong>g tower are the PVC vertical plates (a heat and<br />

mass transfer medium) that <strong>in</strong>crease water/air contact surface as well as the duration of contact. The<br />

closely packed vertical PVC plates are spaced with staggered bars <strong>in</strong>stalled below spray nozzles <strong>in</strong> the<br />

air path. At design conditions, the cool<strong>in</strong>g water is distributed from the top of the tower through spray<br />

nozzles at a temperature of 35.5 o C. The speed of the cool<strong>in</strong>g-tower air fan is varied to ma<strong>in</strong>ta<strong>in</strong> the<br />

cool<strong>in</strong>g-water supply to the chiller at 30 o C.<br />

2.1.9 Vacuum System<br />

The pressure of the evaporator and the absorber is significantly below atmospheric pressure, and air<br />

can leak <strong>in</strong>to the absorption chiller. Corrosion can also occur <strong>in</strong> the chiller, generat<strong>in</strong>g another<br />

noncondensable gas, H2. Air and other noncondensable gases <strong>in</strong> the evaporator and absorber can<br />

seriously reduce the rate of heat and mass transfer processes there and thus reduce the overall cool<strong>in</strong>g<br />

31


capability of the chiller. <strong>An</strong> appropriate means for remov<strong>in</strong>g noncondensable gases is essential to the<br />

operation of microscale absorption chillers.<br />

<strong>An</strong> automatic gas purge device (AGPD) has been provided <strong>in</strong> the chiller to cont<strong>in</strong>uously remove<br />

noncondensable gases from the absorber and the evaporator to ma<strong>in</strong>ta<strong>in</strong> the required vacuum. The<br />

vacuum can be ma<strong>in</strong>ta<strong>in</strong>ed through the AGPD and/or by periodic manual vacuum removal. The<br />

advantage of us<strong>in</strong>g the AGPD is that the noncondensable gases are cont<strong>in</strong>uously removed from the<br />

refrigerant vapor, so the pressure <strong>in</strong> the absorber and the evaporator vessel rema<strong>in</strong>s constant until the<br />

storage chamber is full. Noncondensable gas is generated <strong>in</strong> the upper vessel (the HTRG and the<br />

LTRG), but is hard to remove through the AGPD. Even if an automatic purge unit is <strong>in</strong>stalled,<br />

therefore, manual vacuum removal is still required to purge the noncondensable gas from the storage<br />

chamber and the upper vessel. The detailed mechanisms for controll<strong>in</strong>g noncondensable gas are<br />

described <strong>in</strong> appendix 2.A.<br />

2.2 <strong>Absorption</strong> <strong>Chiller</strong> Test Systems<br />

2.2.1 System Description<br />

A system was set up to test the Broad BCT 16 absorption chiller and to evaluate its performance under<br />

a wide range of external and <strong>in</strong>ternal operat<strong>in</strong>g conditions. This test system, shown <strong>in</strong> Figure 2-7,<br />

comprises the follow<strong>in</strong>g equipment <strong>in</strong> addition to the chiller:<br />

• a steam supply<br />

• a variable cool<strong>in</strong>g load<br />

• an <strong>in</strong>strumentation, control, and data acquisition system<br />

In Figure 2-7, the absorption chiller is <strong>in</strong> the middle. It is connected with the steam supply system on<br />

the left and the variable cool<strong>in</strong>g load system on the right. The necessary control and <strong>in</strong>strumentation<br />

for the overall system has been <strong>in</strong>stalled to operate this test system and to process the data it provides.<br />

The measurement data are used both to monitor the system status and to calculate chiller performance.<br />

32


Figure 2-7: Simplified flow diagram of the chiller test system<br />

CTW<br />

WS BFT<br />

<strong>Absorption</strong> chiller<br />

2.2.1.1 Steam Supply System<br />

BFP<br />

P7 T25<br />

ESB<br />

Steam supply system<br />

P4<br />

CR<br />

T22<br />

SS<br />

T23<br />

P5<br />

ALC<br />

Additional<br />

sensors to<br />

chiller<br />

F2 P3 T21<br />

<strong>Absorption</strong><br />

chiller<br />

F1<br />

Cool<strong>in</strong>g loads Steam supply<br />

T20<br />

P2<br />

BHWSV<br />

HWS<br />

IV5<br />

IV2<br />

HWR<br />

TLHX<br />

IV4<br />

IV3<br />

Variable cool<strong>in</strong>g load<br />

To conduct the tests, steam is generated on site by a steam supply system. The CMU campus has a<br />

steam supply grid, but the closest possible po<strong>in</strong>t of connection is remote from the chiller (six floors<br />

below). The campus steam supply is used ma<strong>in</strong>ly for the build<strong>in</strong>g heat<strong>in</strong>g system; the steam supply<br />

pressure is high <strong>in</strong> the w<strong>in</strong>ter, about 0.7 mPa, but low <strong>in</strong> the summer, about 0.4 mPa – lower than that<br />

specified to operate the chiller, 0.7 mPa. <strong>An</strong> electric steam boiler (ESB) was procured and <strong>in</strong>stalled<br />

along with its auxiliaries to supply steam for test<strong>in</strong>g the chiller. The boiler auxiliaries, shown <strong>in</strong><br />

Figure 2-7, <strong>in</strong>clude:<br />

• a boiler feed receiver tank (BFT)<br />

• a boiler feed pump (BFP)<br />

• a boiler blowdown separator (BBDS)<br />

• a boiler system chemical feeder (BSCF)<br />

• a water softener<br />

• a boiler chemical treater (BCT)<br />

The ESB is capable of provid<strong>in</strong>g steam at a maximum pressure of 1.0 mPa; its rated capacity is 24<br />

kW. The boiler capacity and pressure range is sufficient to drive the absorption chiller with a rated<br />

cool<strong>in</strong>g capacity of 16 kW. Steam pressure is adjusted by on/off control of the two horizontal<br />

33


electrical heaters mounted <strong>in</strong> the base of the boiler. The water level <strong>in</strong> the boiler is ma<strong>in</strong>ta<strong>in</strong>ed around<br />

a set po<strong>in</strong>t that submerges the heaters by on/off control of the boiler feed pump that delivers<br />

condensate from the receiver. A water level set po<strong>in</strong>t <strong>in</strong> the receiver controls the <strong>in</strong>put of water from<br />

the tap through an ion exchange water treatment system. Chemicals are added to the condensate <strong>in</strong> a<br />

treater to avoid corrosion and deposits <strong>in</strong> the system.<br />

At design conditions, the ESB provides steam with a pressure of 0.7 mPa to the absorption chiller. In<br />

the chiller, the steam is condensed <strong>in</strong> the HTRG; and the condensate subcooled <strong>in</strong> the HRHX at 0.1<br />

mPa. The condensate from the chiller is then collected <strong>in</strong> the BFT at atmospheric pressure to serve as<br />

feedwater to the boiler. The other source of feedwater <strong>in</strong> the BFT is city water, which is pretreated<br />

through the water softener. The water softener <strong>in</strong>cludes two water treatment tanks filled with ion<br />

exchange res<strong>in</strong> and a sodium chloride salt tank. The ion exchange res<strong>in</strong> <strong>in</strong> each of the tanks is<br />

regenerated periodically by the sodium chloride salt solution. The boiler feedwater is delivered to the<br />

ESB by the BFP.<br />

Figure 2-8: Site views of the absorption chiller test system<br />

2.2.1.2 Variable Cool<strong>in</strong>g Load System<br />

Systematic test<strong>in</strong>g of the chiller requires a load that can be adjusted <strong>in</strong>dependently and ma<strong>in</strong>ta<strong>in</strong>ed<br />

constant dur<strong>in</strong>g a test run. This load is provided by a shell-and-tube heat exchanger fed with water at<br />

34


80 o C to the shell from the build<strong>in</strong>g hot water grid. The flow of chilled water from the chiller outlet to<br />

the tubes of the load exchanger is controlled by a valve to achieve a desired flow set po<strong>in</strong>t. The flow<br />

of hot water to the exchanger is also controlled by a valve (BHWSV) to ma<strong>in</strong>ta<strong>in</strong> a desired set po<strong>in</strong>t<br />

temperature for the chilled water at the <strong>in</strong>let to the chiller. Under design conditions, the chilled water<br />

flows <strong>in</strong> the chiller at a rate at 2 m 3 /h and a temperature of 14 o C. The chiller cools the chilled water to<br />

7 o C. Figure 2-8 shows photographs of the overall system. The photo on the left <strong>in</strong>dicates the ESB,<br />

BFT, and some chilled-water supply and return pipes. The photo on the top right shows the absorption<br />

chiller <strong>in</strong>stalled on the deck adjacent to the IW. The picture on the bottom right shows the variable<br />

cool<strong>in</strong>g load system.<br />

2.2.2 Instrumentation, Control, and Data Acquisition System<br />

For operation of the chiller test system, an <strong>in</strong>strumentation, control, and data acquisition<br />

system has been provided by the Automated Logic Co. (ALC). It collects the measurement data<br />

from the operation of the absorption chiller and the auxiliary steam supply and cool<strong>in</strong>g-load systems to<br />

evaluate the chiller under various conditions and to assess chiller <strong>in</strong>ternal work<strong>in</strong>g conditions. The<br />

system also displays the operational data <strong>in</strong> various forms such as trends and bar charts, and stores<br />

data for future analysis. The ALC system is a web-based control and data display system, so the<br />

operators can operate the system and access the experimental data via the Internet.<br />

2.2.2.1 Structure of Instrumentation Control System<br />

The structure of the overall control and <strong>in</strong>strumentation system is illustrated <strong>in</strong> Figure 2-9. The left<br />

side is the <strong>in</strong>ternal control system from the chiller manufacturer, and the right side is the ALC control<br />

system for the steam supply and variable cool<strong>in</strong>g load systems. The additional sensors used to monitor<br />

the chiller <strong>in</strong>ternal conditions were also implemented through the ALC control system. The ALC<br />

control system is one of the basic platforms for build<strong>in</strong>g an <strong>in</strong>tegrated <strong>BCHP</strong> system. It can not only<br />

perform regular control and data acquisition functions, but it can also perform more complicated tasks<br />

such as system diagnostics and optimization when the overall system becomes more complicated.<br />

With this automation control system, the overall chiller test system can be started up, shut down, and<br />

adjusted automatically or manually through a computer. The operat<strong>in</strong>g conditions can be displayed on<br />

a graphic <strong>in</strong>terface, and the measured data can be collected for further analysis.<br />

35


Figure 2-9: Control and <strong>in</strong>strumentation structure<br />

The sensors <strong>in</strong>stalled through the ALC system <strong>in</strong>clude:<br />

• the additional sensors (surface type) for the chiller<br />

• the sensors for the steam supply system<br />

• the sensors for the variable cool<strong>in</strong>g load system<br />

The chiller <strong>in</strong>ternal control system receives the measurement signals from the sensors and sends<br />

commands to the control po<strong>in</strong>ts (components) through the chiller control panel. The control algorithm<br />

provides for startup, shutdown, and operation of the chiller on the basis of the sensor <strong>in</strong>formation. The<br />

chiller control will be discussed <strong>in</strong> appendix 2.A. The chiller operational status is monitored through a<br />

remote control device or a computer; the measurement data are stored <strong>in</strong> the computer.<br />

2.2.2.2 Data Acquisition and Display<br />

User friendly <strong>in</strong>terfaces are important to operate the chiller, the auxiliary steam supply, and the<br />

variable cool<strong>in</strong>g load systems. The operators can operate the chiller automatically or manually <strong>in</strong><br />

startup, shutdown, and adjustment of the system. The measurement data are displayed <strong>in</strong>stantaneously<br />

on the monitor and are stored <strong>in</strong> the computer for future analysis.<br />

The chiller monitor<strong>in</strong>g <strong>in</strong>terface is illustrated <strong>in</strong> Figure 2-10. The monitor<strong>in</strong>g <strong>in</strong>terface is a small and<br />

<strong>in</strong>dependent software package with data collection functions. It is a good tool for monitor<strong>in</strong>g the status<br />

of the chiller <strong>in</strong>stantly and display<strong>in</strong>g the <strong>in</strong>formation graphically. Through the <strong>in</strong>terface, the operator<br />

36


can perform startup, shutdown, and other operational actions to the chiller automatically and can<br />

adjust chiller operational parameters such as set po<strong>in</strong>ts. The chiller operation status (on or off) is<br />

displayed <strong>in</strong> the top row; the temperature measurements are displayed on the left of the <strong>in</strong>terface. The<br />

solution level <strong>in</strong> the HTRG and the solution pump status are displayed <strong>in</strong> the middle of the <strong>in</strong>terface,<br />

and the valve positions and other pump states are displayed at the lower part of the <strong>in</strong>terface. On the<br />

right of the <strong>in</strong>terface are warn<strong>in</strong>g and alarm<strong>in</strong>g messages.<br />

Figure 2-10: <strong>Absorption</strong> chiller monitor<strong>in</strong>g software<br />

Parallel to the computer monitor<strong>in</strong>g <strong>in</strong>terface, an on-site key pad monitor<strong>in</strong>g system is mounted near<br />

the chiller. This system has the same functions as the control software <strong>in</strong>stalled <strong>in</strong> the central computer<br />

<strong>in</strong> Figure 2-10 that can save the measurement data <strong>in</strong> an Excel spreadsheet.<br />

The ALC control software is called the web control server (WCS). As an example, Figure 2-11<br />

displays additional sensor measurements for the chiller and for the steam supply and variable load<br />

systems through the ALC WCS data display system.<br />

The WCS plots historical data <strong>in</strong> various forms, such as graphics, trends, and spreadsheets. The<br />

measurement data can be sampled <strong>in</strong> any time step from a second to a year. The ALC control system<br />

has the potential to communicate with the chiller control module directly through a standard<br />

37


communication port; this function is usually called “the third party <strong>in</strong>tegration”. Third-party<br />

equipment, like the absorption chiller, becomes a subsystem that can receive commands such as<br />

startup and shutdown from the WCS, a primary control system. The manufacturer of the absorption<br />

chiller, however, uses nonstandard control protocol, so a software driver to translate the chiller control<br />

protocol <strong>in</strong>to a commercial standard was required to implement “the third party <strong>in</strong>tegration”. The<br />

chiller control system and the ALC control system were <strong>in</strong>stalled and worked as two <strong>in</strong>dependent<br />

systems <strong>in</strong> parallel.<br />

Figure 2-11: Test system monitor<strong>in</strong>g software<br />

2.2.2.3 Instrumentation for the <strong>Chiller</strong><br />

Figure 2-12 is the process and <strong>in</strong>strumentation (P&I) diagram for the chiller. This figure illustrates<br />

chiller components, pip<strong>in</strong>g, and the measurement and control po<strong>in</strong>ts. The chiller components and<br />

configurations have been described <strong>in</strong> Figure 2-2, Table 2-1, and section 2.1. This section discussed<br />

the <strong>in</strong>strumentation and control of the chiller. The absorption chiller has its own controls and<br />

<strong>in</strong>strumentation from the manufacturer; additional sensors are <strong>in</strong>stalled for the chiller by the ALC<br />

dur<strong>in</strong>g chiller <strong>in</strong>stallation to study its <strong>in</strong>ternal operation conditions. In Figure 2-12, the sensors from<br />

38


the manufacturer are <strong>in</strong>dicated <strong>in</strong> green. The temperature sensors and flow meter provided by the ALC<br />

are <strong>in</strong>dicated <strong>in</strong> blue. The red l<strong>in</strong>es <strong>in</strong>dicate the control po<strong>in</strong>ts of the chiller from the manufacturer,<br />

and the p<strong>in</strong>k ones refer to the controls for the steam supply and cool<strong>in</strong>g-load systems.<br />

The <strong>in</strong>struments and sensors <strong>in</strong>stalled <strong>in</strong> the chiller by its manufacturer <strong>in</strong>dicate chiller operat<strong>in</strong>g<br />

conditions. These temperature, level, flow, and electric power measurements are listed <strong>in</strong> Table 2-3.<br />

There was a total of 16 measurements from the chiller manufacturer. The configurations and the<br />

functions of these sensors are discussed <strong>in</strong> appendix 2.A.<br />

Figure 2-12: PI&D diagram of the absorption chiller<br />

To auxilary system<br />

ME-LGR 25<br />

Steam<br />

Condensate<br />

CHWS<br />

CHWR B1 T1 B2<br />

Dra<strong>in</strong><br />

City water<br />

T9 T2<br />

T6<br />

T10<br />

Controller<br />

T7<br />

SF<br />

T14<br />

P1<br />

SV<br />

T8<br />

RBPSV<br />

HRHX<br />

L2<br />

RP<br />

CHWP<br />

L3<br />

CHSV<br />

T11<br />

CTWS<br />

Evaporator<br />

T33 T13<br />

RPH<br />

SP<br />

LTRG<br />

HTRG<br />

Condenser<br />

T19<br />

HTHX LTHX<br />

Absorber<br />

T12<br />

T3<br />

T17 T18<br />

T5<br />

L1<br />

T15<br />

T32<br />

L4<br />

CWP<br />

T16<br />

L5<br />

F6<br />

CWBPV<br />

DV<br />

CWDD<br />

Hot Humid Air<br />

CTF<br />

Air<br />

CWF<br />

39


The ALC <strong>in</strong>stalled 11 additional temperature sensors and a flow meter <strong>in</strong> the chiller for this study to<br />

obta<strong>in</strong> further <strong>in</strong>formation on its operation, Table 2-3. The temperature sensors were mounted on the<br />

surface of the chiller vessel and pip<strong>in</strong>g. This is an economical and convenient method, but the heat<br />

conduction through the pipe and heat loss to the surround<strong>in</strong>gs affects the accuracy of the<br />

measurements.<br />

Serious consideration was given to <strong>in</strong>stall<strong>in</strong>g of three pressure sensors to <strong>in</strong>dicate pressure levels <strong>in</strong> the<br />

evaporator and <strong>in</strong> each of the two regenerators of the chiller. Broad advised aga<strong>in</strong>st penetrat<strong>in</strong>g the<br />

chiller hous<strong>in</strong>g because of the possible <strong>in</strong>troduction of air leakage or corrosion at the po<strong>in</strong>t of sensor<br />

<strong>in</strong>stallation.<br />

2.2.2.4 Instrumentation for the Auxiliary Systems<br />

The steam supply system and the variable cool<strong>in</strong>g-load system were discussed <strong>in</strong> sections 2.2.1 and<br />

2.2.2. The system configuration is <strong>in</strong>dicated <strong>in</strong> Figure 2-7. Table 2-3 lists the seven measurements of<br />

the steam system provided by the ALC system, which are also <strong>in</strong>dicated <strong>in</strong> Figure 2-7. Among these<br />

sensors, the steam flow rate, steam supply temperature, and condensate return temperature are used to<br />

calculate the quantity of heat <strong>in</strong>put to the chiller. These sensors measure the fluid directly.<br />

Table 2-3 also lists the six sensors <strong>in</strong>stalled for the variable cool<strong>in</strong>g load system. There are a total of<br />

six temperature sensors, two flow meters, and four pressure transducers. Among these sensors, the<br />

chilled-water flow rate (F1), chilled-water supply temperature (T21), and chilled-water return<br />

temperature (T20) were used to calculate the cool<strong>in</strong>g capacity of the chiller. All these sensors and<br />

meters measure the fluid directly.<br />

2.2.2.5 Instrumentation Calibration<br />

These sensors provided by the ALC were calibrated on site by the follow<strong>in</strong>g methods:<br />

• the temperature sensor read<strong>in</strong>gs were calibrated <strong>in</strong> ice water and boil<strong>in</strong>g water.<br />

• the condensate from the chiller was collected <strong>in</strong> a barrel; the weight of the condensate was<br />

measured every 15 m<strong>in</strong>utes for 2 hours. The weight of condensate was compared with the<br />

measured values of the steam flow meter.<br />

• the chilled-water flow meter pip<strong>in</strong>g configuration was sent back to the flow meter<br />

manufacturer for calibration; the suggested deviation has been applied to the chilled-water flow<br />

measurement.<br />

40


The calibration results are <strong>in</strong>dicated <strong>in</strong> the last column of Table 2-3. The accuracies of the resistance<br />

temperature detectors (RTD) type temperature sensors are with<strong>in</strong> ± 0.2%. The surface temperature<br />

sensors calibrated <strong>in</strong> ice water are accurate to ± 1.5% but have an accuracy of ± 0.5% <strong>in</strong> boil<strong>in</strong>g<br />

water. The calibration offset values are assigned to the sensors listed <strong>in</strong> the last column of Table 2-3.<br />

The steam flow meter gives higher accuracy at high flow rate and pressure. On average, when the<br />

steam flow rate is higher than 12 kg/h, the steam flow meter accuracy is with<strong>in</strong> 10%, but when the<br />

steam flow rate drops below 12 kg/h, the steam flow meter accuracy is with<strong>in</strong> roughly 50%. At design<br />

condition, the steam flow meter <strong>in</strong>dicates a value only 2% lower than the condensate weight. Because<br />

of these <strong>in</strong>accuracies, the chiller heat <strong>in</strong>put was calculated by measur<strong>in</strong>g the power <strong>in</strong>put to the boiler.<br />

Accord<strong>in</strong>g to the manufacturer, the boiler efficiency is 98% to 99% under design load and off-design<br />

load conditions. In calculat<strong>in</strong>g the chiller performance, therefore, the power measurements of the<br />

boiler are more reliable than the steam flow measurements.<br />

2.2.3 Controls for the <strong>Chiller</strong><br />

On the basis of sensor <strong>in</strong>puts, the chiller control algorithms determ<strong>in</strong>e the outputs to the actuators and<br />

control po<strong>in</strong>ts on various system components. The chiller has a total of 12 control components listed <strong>in</strong><br />

Table 2-4, and the sensor locations, types, and the configurations are <strong>in</strong>dicated <strong>in</strong> Figure 2-12. The<br />

features of these control components are discussed <strong>in</strong> appendix 2.A.<br />

Table 2-3: Control po<strong>in</strong>ts of the chiller<br />

Abbrev. Name Signal Category<br />

CHWP Chilled-water pump Digital On/off<br />

CWP Cool<strong>in</strong>g-water pump Digital On/off<br />

SP Solution pump <strong>An</strong>alog Quantity control<br />

RP Refrigerant pump Digital Quantity control<br />

CTF Cool<strong>in</strong>g-tower fan <strong>An</strong>alog Temperature control<br />

SV Steam valve <strong>An</strong>alog Operation time control<br />

RBPSV Refrigerant by-pass valve Digital On/off<br />

CTS City-water switch Digital Quantity control<br />

CWDD Cool<strong>in</strong>g-water dra<strong>in</strong> device Digital On/off<br />

CWDV Cool<strong>in</strong>g-water detergent valve Digital On/off<br />

CWBPV Cool<strong>in</strong>g-water by-pass valve <strong>An</strong>alog Temperature control<br />

CTF Cool<strong>in</strong>g-tower fan <strong>An</strong>alog Temperature control<br />

RPH Refrigerant-pump heater Digital Temperature control<br />

41


Table 2-4: Instrumentation of the chiller test systems<br />

<strong>Absorption</strong> <strong>Chiller</strong> (manufacturer)<br />

<strong>Absorption</strong> <strong>Chiller</strong> (ALC)<br />

Steam System<br />

Cool<strong>in</strong>g Load System<br />

Temp.<br />

Level<br />

Power Flow<br />

Temp.<br />

Misc.<br />

Temp.<br />

Pres.<br />

Misc.<br />

Temp.<br />

Flow<br />

Pres.<br />

Label Sensor location Medium Range Manufacturer<br />

Accuracy<br />

T1 Chilled-water return Water (-15 o C) to 110 o C ± 0.1%<br />

T2 Chilled-water supply Water (-15 o C) to 110 o C ± 0.1%<br />

T3 Cool<strong>in</strong>g-water supply Water (-15 o C) to 110 o C ± 0.1%<br />

T5 High-temperature regenerator Solution (-15 o C) to 210 o C ± 0.1%<br />

T6 Ambient Air (-15 o C) to 110 o C ± 0.1%<br />

T7 Steam supply Steam (-15 o C) to 210 o C ± 0.1%<br />

T8 Condensate return Water (-15 o C) to 210 o C ± 0.1%<br />

T9 Chilled-water return 2 Water (-15 o C) to 110 o C ± 0.1%<br />

L1 HTRG solution level probe Solution 4 p<strong>in</strong>s<br />

L3 LTRG upper-limit level probe Solution 1 p<strong>in</strong><br />

L4 Auto<br />

probe<br />

vacuum device level Solution 1 p<strong>in</strong><br />

L5 Cool<strong>in</strong>g-water level probe Water 1 p<strong>in</strong><br />

B1 Chilled-water flow detector Water on/off<br />

B2 Chilled-water flow detector Water on/off<br />

D1 Solution pump frequency, Electricity<br />

amps, and voltage<br />

On-site<br />

Calibration<br />

T11 Condensate after HTRG Surface 0-400 o F ± 0.1% 0.5 o F<br />

T12 Solution <strong>in</strong> Absorber Surface 0-400 o F ± 0.1% 0.5 o F<br />

T13 Solution enter<strong>in</strong>g HRHX Surface 0-400 o F ± 0.1% 2 o F<br />

T14 Solution leav<strong>in</strong>g HRHX Surface 0-400 o F ± 0.1% 1.5 o F<br />

T15 Cool<strong>in</strong>g water after absorber Surface 0-400 o F ± 0.1% 1.5 o F<br />

T16 Cool<strong>in</strong>g water after condenser Surface 0-400 o F ± 0.1% 1.0 o F<br />

T17 Low-temperature<br />

(LTRG)<br />

regenerator Surface 0-400 o F ± 0.1% 0.3 o F<br />

T18 Refrigerant after condenser Surface 0-400 o F ± 0.1% 1.5 o F<br />

T19 Refrigerant from evaporator Surface 0-400 o F ± 0.1% 2.0 o F<br />

T32 Cool<strong>in</strong>g water after cool<strong>in</strong>g<br />

tower<br />

Surface 0-400 o F ± 0.1% 0.0 o F<br />

T33 HTRG temperature Surface 0-400 o F ± 0.1% 1.5 o F<br />

F6 Cool<strong>in</strong>g-water flow Water 0 to 30 gpm ± 1% -15%<br />

E1 Electric power of absorption<br />

chiller<br />

Electricity 0-2400 amps ± 1% 0.0%<br />

T22 Steam-supply temperature Steam (50 o F) to 250 o F ± 0.1% 0.0 o F<br />

T23 Condensate-return<br />

Water (50 o F) to 250 o F ± 0.1% 0.0 o F<br />

temperature<br />

T25 Feed-water temperature Water (50 o F) to 250 o F ± 0.1% 0.0 o F<br />

P4 Steam supply pressure Steam 0 to 40 gpm ± 0.13%<br />

P5 Condensate return pressure Water 0 to 100 psi ± 0.13%<br />

P7 Feed-water pressure Water 0 to 50 psi ± 0.13%<br />

F2 Steam flow Steam 0 to 75 lb/h ± 0.5% 0-10%<br />

E2 Electric power of steam boiler Electricity 0-2400 amps ± 1% 0.0%<br />

T20 Chilled-water supply Water (-10 o F) to 110 o F ± 0.1% 0.6 o F<br />

T21 Chilled-water return Water (-10 o F) to 110 o F ± 0.1% -0.4 o F<br />

T31 Ambient temperature Air (-58 o F) to122 o F ± 0.1%<br />

P2 Chilled-water <strong>in</strong>let Water 0 to 100 psi ± 0.13%<br />

P3 Chilled-water outlet Water 0 to 50 psi ± 0.13%<br />

F1 Chilled water Water 0 to 20 gpm ± 1% 0%<br />

42


Compared to traditional pneumatic or electric controls, the use of electronic controls with advanced<br />

control algorithms makes the complicated absorption chiller more efficient and reliable. Control<br />

categories for the chiller are:<br />

• startup and shutdown<br />

• chilled-water supply temperature control<br />

• cool<strong>in</strong>g-water supply temperature control<br />

• vacuum ma<strong>in</strong>tenance<br />

• crystallization judgment and de-crystallization<br />

• safety and diagnostics<br />

The details of the chiller control pr<strong>in</strong>ciples of the six categories are discussed <strong>in</strong> appendix 2.A.<br />

Knowledge of the chiller controls greatly improves the understand<strong>in</strong>g of the chiller, which, <strong>in</strong> turn,<br />

assists <strong>in</strong> improv<strong>in</strong>g the accuracy of the computational model discussed <strong>in</strong> chapter 3.<br />

With the control, <strong>in</strong>strumentation, and data acquisition systems, the absorption chiller can be tested<br />

under various load conditions. On the basis of a test program, the chiller performance was <strong>in</strong>vestigated<br />

by vary<strong>in</strong>g the operational parameters <strong>in</strong>dividually. The test<strong>in</strong>g approaches and results will be<br />

discussed <strong>in</strong> the follow<strong>in</strong>g sections.<br />

2.3 <strong>Chiller</strong> Performance and Test Program<br />

The chiller was first tested at design condition and then under off-design conditions on the basis of a<br />

test program.<br />

2.3.1 <strong>Chiller</strong> Test<strong>in</strong>g<br />

2.3.1.1 <strong>Chiller</strong> Test<br />

<strong>An</strong> <strong>in</strong>dividual chiller test was conducted by sett<strong>in</strong>g the six operat<strong>in</strong>g conditions that are the primary<br />

<strong>in</strong>put to the test system, all external to the chiller:<br />

• the pressure of the saturated steam supply<br />

• the flow rate, <strong>in</strong>let , and outlet temperature of the chilled water<br />

• the flow rate and <strong>in</strong>let temperature of the cool<strong>in</strong>g water. Ord<strong>in</strong>arily, the chiller cool<strong>in</strong>g- water<br />

pump ma<strong>in</strong>ta<strong>in</strong>s a constant flow; and the air fan ma<strong>in</strong>ta<strong>in</strong>s a constant supply temperature by<br />

vary<strong>in</strong>g its speed <strong>in</strong> response to the cool<strong>in</strong>g load and the ambient air conditions. To test the<br />

43


chiller over a broader range of operat<strong>in</strong>g conditions, however, measures adjust cool<strong>in</strong>g-water<br />

flow and temperature were taken<br />

The chilled-water outlet temperature sett<strong>in</strong>g <strong>in</strong> the chiller control system was ma<strong>in</strong>ta<strong>in</strong>ed constant at 7<br />

o<br />

C throughout the test program. While this sett<strong>in</strong>g rema<strong>in</strong>ed constant, the measured value of chilledwater<br />

outlet temperature varied ±2 o C from the set po<strong>in</strong>t, depend<strong>in</strong>g on the test conditions. At a given<br />

sett<strong>in</strong>g of operat<strong>in</strong>g conditions, the chiller was allowed to reach steady-state operation. Three primary<br />

performance conditions were measured:<br />

• the chilled-water outlet temperature<br />

• the steam flow<br />

• the power consumption of the chiller <strong>in</strong> its pumps, fan, heater, and controls<br />

Steady-state was established by observ<strong>in</strong>g that these conditions had a constant average value over a<br />

period of 20 m<strong>in</strong>utes or longer. The chiller load, COP, and power consumption were calculated for the<br />

test. The chiller load is the product of the chilled-water flow, the temperature difference between the<br />

<strong>in</strong>let and outlet chilled-water temperature, and the specific heat of the chilled water. The COP is the<br />

quotient of the chiller load and the enthalpy difference of the <strong>in</strong>let steam and the outlet condensate<br />

from the chiller. In addition, all the <strong>in</strong>put data from sensors and output signals to actuators <strong>in</strong> the<br />

chiller, steam supply, and variable load for each test were recorded and stored <strong>in</strong> the data acquisition<br />

system for further consideration and analysis as described <strong>in</strong> chapter 3.<br />

2.3.1.2 The <strong>Chiller</strong> Test Program<br />

A chiller test program was planned and executed. Each of the six operat<strong>in</strong>g conditions, identified<br />

above, was varied one at a time over a range of design values, as <strong>in</strong>dicated <strong>in</strong> Table 2-5. With<strong>in</strong> its<br />

range each operat<strong>in</strong>g condition was tested at 5 to 10 values. Ranges of each of these six variables are<br />

<strong>in</strong>dicated <strong>in</strong> Table 2-5. Each test collected 20 to 200 data sets obta<strong>in</strong>ed at 2-m<strong>in</strong>ute <strong>in</strong>tervals dur<strong>in</strong>g<br />

steady-state operation of the chiller. A total of 38 tests were conducted over an estimated 220 hours of<br />

chiller operation.<br />

The results of these tests <strong>in</strong> terms of the steam flow and chilled-water outlet temperature, the chiller<br />

load and the coefficient of performance, is reported and discussed <strong>in</strong> subsection 2.4 below.<br />

44


Table 2-5: Input and primary output of the test program<br />

CHW<br />

return T<br />

CHW<br />

flow<br />

Inputs Primary Outputs Calculated performance<br />

CW<br />

supply T<br />

CW<br />

flow<br />

Steam<br />

pressure<br />

Steam<br />

Flow<br />

CHW<br />

supply COP<br />

Cool<strong>in</strong>g<br />

load<br />

o C kg/s o C kg/s kPa kg/s o C kW<br />

Design<br />

condition 13.9 0.5616 30.78 1.546 600 0.00727 7 1.03 16.63<br />

CHW<br />

0.00382–<br />

return T 8–14 Design Design Design Design 0.00771 6.25–6.9 0.95–1.03 9–18<br />

CHW<br />

0.531–<br />

0.00705– 6.42–<br />

flow Design 0.864 Design Design Design 0.00771 8.97 0.93–1.02 16.56–17.96<br />

CW<br />

0.00609– 6.13–<br />

supply T Design Design 27.5–36 Design Design 0.00764 9.26 1.11–0.91 19.22–13.29<br />

0.784–<br />

0.00618–<br />

CW flow Design Design Design 1.547 Design 0.00709 7.52–9 0.81–0.98 11.73–15.23<br />

Steam<br />

0.00556– 6.34–<br />

pressure Design Design Design Design 360–700 0.00748 10.27 0.65–0.99 8.41–17.47<br />

2.3.2 Conduct of the Test<strong>in</strong>g Program<br />

In the test<strong>in</strong>g program, various procedures were used to adjust the six operat<strong>in</strong>g conditions.<br />

• The chilled-water return temperature was varied by adjust<strong>in</strong>g the hot water supply flow to the<br />

variable load.<br />

• The chilled-water flow was varied by adjust<strong>in</strong>g a ball valve <strong>in</strong> the chilled-water supply pipe,<br />

but when the chilled-water flow was reduced below the design flow rate for the chiller, a<br />

“water cut” warn<strong>in</strong>g was reported, and the chiller automatically executed its shutdown<br />

procedure. Only design and higher chilled-water flows have been tested.<br />

• The cool<strong>in</strong>g-water supply temperature was varied by adjust<strong>in</strong>g the air fan speed.<br />

• The cool<strong>in</strong>g-water flow rate was varied by block<strong>in</strong>g a portion of the cool<strong>in</strong>g-water filter<br />

located at the bottom of the cool<strong>in</strong>g tower.<br />

• The steam supply pressure was varied by adjust<strong>in</strong>g the pressure set po<strong>in</strong>t <strong>in</strong> the boiler control<br />

system.<br />

Fewer tests have been performed at operat<strong>in</strong>g conditions that result <strong>in</strong> loads below the design values.<br />

When the cool<strong>in</strong>g load is below 50% of the design load, it has proved difficult to obta<strong>in</strong> stable data for<br />

analysis because of on-off cycl<strong>in</strong>g of the steam valve.<br />

2.4 <strong>Chiller</strong> Performance<br />

The chiller performance has been calculated on the basis of the result<strong>in</strong>g measurements. The chiller<br />

performance has been compared with the chiller specification data Broad provided. Results show that<br />

45


the chiller cool<strong>in</strong>g capacity is higher than its rated capacity of 16 kW. The chiller has a COP of 1.0,<br />

slightly below its specified value.<br />

2.4.1 <strong>Chiller</strong> Performance Calculations<br />

The performance of an absorption chiller is determ<strong>in</strong>ed by its cool<strong>in</strong>g capacity, coefficient of<br />

performance, and electric power consumption. These quantities are def<strong>in</strong>ed <strong>in</strong> the follow<strong>in</strong>g equations<br />

The cool<strong>in</strong>g capacity or chiller load is<br />

cool<strong>in</strong>g<br />

CHW<br />

p<br />

( T T )<br />

Q = m&<br />

× C × −<br />

(Equation 2-1)<br />

CHWR<br />

CHWS<br />

Where m& CHW is the flow rate of the chilled water<br />

T CHWR is the temperature of the chilled water enter<strong>in</strong>g the chiller<br />

T is the temperature of the chilled water leav<strong>in</strong>g the chiller<br />

CHWS<br />

C is the specific heat of water.<br />

The COP of the chiller is conventionally<br />

thermal<br />

p<br />

Q<br />

Q<br />

cool<strong>in</strong>g<br />

COP = (Equation 2-2)<br />

heat<br />

Where, Q m × ( h − h )<br />

heat<br />

= & = the heat delivered to the chiller by steam<br />

steam<br />

steam<br />

condensate<br />

condensation; this quantity can also be estimated from the electrical power<br />

consumption <strong>in</strong> the steam boiler.<br />

m& steam is the flow rate of the steam supply<br />

h steam and h condensate are the enthalpies of the steam supply and the condensate,<br />

respectively.<br />

<strong>An</strong> overall COP can be def<strong>in</strong>ed that <strong>in</strong>cludes both the thermal and the electrical energy supplied to the<br />

chiller<br />

Q<br />

COP = (Equation 2.3)<br />

energy<br />

cool<strong>in</strong>g<br />

overall<br />

Qenergy<br />

Q Q + E<br />

= (Equation 2-3)<br />

heat<br />

E =<br />

V * I<br />

power<br />

power<br />

power<br />

power<br />

46


Where, the power consumed <strong>in</strong> the pumps, fan, heater, and control of the chiller.<br />

The power consumption of the chiller is approximately 8% of the total energy supplied; the thermal<br />

COP ( COP thermal ), usually used to represent chiller performance. is therefore only slightly greater than<br />

the (COPoverall ).<br />

2.4.2 <strong>Chiller</strong> Performance under Design Condition<br />

The chiller has been tested under the design conditions <strong>in</strong>dicated <strong>in</strong> Table 2-5. In the test, the chiller<br />

was started up and operated for a period of time before the steam supply system was started. This<br />

procedure is called a “cold” start of the chiller. The “cold” start of the chiller provides an opportunity<br />

to check the accuracy of the sensors. For example, there are two measurements of the cool<strong>in</strong>g water<br />

temperature: at the cool<strong>in</strong>g tower outlet after the absorber and after the condenser. In the “cold” start,<br />

these two sensors should <strong>in</strong>dicate the same, ambient temperature. Similarly, the sorbent solutions <strong>in</strong><br />

the absorber and the high-temperature and low-temperature regenerators should be equal. Figure 2-13,<br />

show<strong>in</strong>g a typical cold start, startup, and steady-state operation of a chiller test, confirms these<br />

expectations. Once the steam supply system is provided, all these stream temperatures diverge as<br />

steady-state operation is approached.<br />

Figure 2-13: Typical start-up of the chiller test system<br />

47


The steady state is def<strong>in</strong>ed by observ<strong>in</strong>g the monitor<strong>in</strong>g <strong>in</strong>terface. Figure 2-14 shows steady-state<br />

measurement data over a period of 1 hour and 45 m<strong>in</strong>utes. The time step for the measurements was<br />

preset at 2 m<strong>in</strong>utes; a total of 67 data samples were collected for this design load test.<br />

The steam flow fluctuated around an average value with<strong>in</strong> ± 20%<br />

. A drop <strong>in</strong> steam flow occurs<br />

because the boiler feed pump periodically feeds condensate to the boiler at a temperature lower than<br />

the boil<strong>in</strong>g po<strong>in</strong>t. The boiler temperature, pressure, and steam flow are consequently reduced until the<br />

electrical elements of the boiler heat its water content to the preset boil<strong>in</strong>g pressure. This periodic<br />

action of the boiler feed system repeats as shown <strong>in</strong> Figure 2-14. The cool<strong>in</strong>g capacity of the chiller is<br />

rather stable around 17.5 kW; but the calculated thermal COPthermal, directly dependent on the steam<br />

flow, fluctuates around an average value of 1.0.<br />

Figure 2-14: Steady-state operation of the chiller under design load condition<br />

Steam supply flow rate (kg/h),<br />

Cool<strong>in</strong>g load (kW)<br />

30<br />

25<br />

20<br />

15<br />

10<br />

5<br />

0<br />

Cool<strong>in</strong>g load (Q cool<strong>in</strong>g)<br />

Steam flow rate (F1)<br />

COP thermal<br />

21:30 21:38 21:46 21:54 22:02 22:10 22:18 22:26 22:34 22:42 22:50 22:58 23:06 23:14<br />

Steam supply flow rate Cool<strong>in</strong>g load COP<br />

Figure 2-15 shows the stream temperatures for the same test as Figure 2-14. The data <strong>in</strong>dicate the<br />

chilled-water supply and return temperatures at the bottom of the chart. The chilled-water supply<br />

temperature is very stable compared with the steam supply temperature on the top of the chart and the<br />

cool<strong>in</strong>g water temperatures <strong>in</strong> the middle. The sorbent solutions <strong>in</strong> both regenerators are affected by<br />

the temperature of steam supply. The refrigerant temperature after the condenser is plotted also; this<br />

temperature is apparently affected by the temperature of the steam supply, but the curve is flatter than<br />

the sorbent solution <strong>in</strong> the HTRG and the LTRG.<br />

4<br />

3<br />

2<br />

1<br />

0<br />

Time<br />

3.5<br />

2.5<br />

1.5<br />

0.5<br />

Cofficient of Performance (COP)<br />

48


The cool<strong>in</strong>g water fluctuates some because of the operation of the cool<strong>in</strong>g-tower fan. The cool<strong>in</strong>gwater<br />

supply temperature is consistently ma<strong>in</strong>ta<strong>in</strong>ed at 30 o C with<strong>in</strong> ± 1<br />

o C deviations. Although the<br />

conditions of the outside stream (steam, cool<strong>in</strong>g water, chilled water) vary as <strong>in</strong>dicated <strong>in</strong> Figure 2-14,<br />

the absorption chiller reduces these effects by its <strong>in</strong>ternal control system. As a result, it is more<br />

convenient to use the temperatures <strong>in</strong> the chiller as an <strong>in</strong>dicator of steady-state operation.<br />

Figure 2-15: Steady-state operation of the chiller under design load condition<br />

Temperature ( o C)<br />

180<br />

160<br />

140<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

HTRG sorbent<br />

LTRG sorbent<br />

Cool<strong>in</strong>g water supply and return<br />

Refrigerant after Condenser<br />

Steam supply<br />

Chilled water supply<br />

Chilled water return<br />

21:30 21:38 21:46 21:54 22:02 22:10 22:18 22:26 22:34 22:42 22:50 22:58 23:06 23:14<br />

CHWR CHWS SS<br />

CWS CW after ABS CW after COND<br />

LTRG HTRG Refrigerant after COND<br />

Table 2-6 presents the average measured data of the chiller operat<strong>in</strong>g at design condition before and<br />

after sensor calibration. Before the calibration means that the test data were collected prior to the<br />

<strong>in</strong>strumentation processes, and after the calibration means that the test data were collected after the<br />

sensor were relocated, well <strong>in</strong>sulated, and the offsets of calibration are applied through the data<br />

acquisition systems. The differences of the measurement values between the two tests are small<br />

because the sensor calibration offset values <strong>in</strong> Table 2-6 are relatively small.<br />

Table 2-6 shows that all temperature data collected from the data acquisition system of the absorption<br />

chiller that Broad provided (T1 to T9) show only small differences from similar measurements<br />

collected from the ALC system (T11 to T33). The chiller performance has been calculated on the<br />

basis of the measurement data from the ALC system. The measurements <strong>in</strong> bold are those used <strong>in</strong><br />

calculat<strong>in</strong>g the chiller performance. It is notable that T11 and T33 have higher deviations before and<br />

after the calibration, about 6.5 and 3 o C, respectively.<br />

Time<br />

49


Table 2-6: Measurement data of the chiller under design condition<br />

<strong>Absorption</strong> chiller (manufacturer)<br />

<strong>Absorption</strong> chiller (ALC)<br />

Steam system<br />

Cool<strong>in</strong>g load system<br />

Temp.<br />

Level<br />

Flow<br />

Ele.<br />

Temp.<br />

Flow<br />

Temp.<br />

Pres.<br />

Flow<br />

Temp.<br />

Pres.<br />

Flow<br />

Label Sensor location Medium Unit Before calib. After calib.<br />

T1 Chilled-water return Water<br />

o<br />

C - 13.83<br />

T2 Chilled-water supply Water<br />

T3 Cool<strong>in</strong>g-water supply Water<br />

T5 High-temperature regenerator Solution<br />

T6 Ambient Air<br />

T7 Steam supply Steam<br />

T8 Condensate return Water<br />

T9 Chilled-water return 2 Water<br />

L1 HTRG solution level probe Solution<br />

L3 LTRG upper-limit level probe Solution<br />

L4 Auto vacuum device level probe Solution<br />

L5 Cool<strong>in</strong>g-water level probe Water<br />

B1 Chilled-water flow detector Water<br />

B2 Chilled-water flow detector Water<br />

E1 Solution pump frequency, amps, and voltage Electricity<br />

T11 Condensate after HTRG Surface<br />

T12 Solution <strong>in</strong> absorber Surface<br />

T13 Solution enter<strong>in</strong>g HRHX Surface<br />

T14 Solution leav<strong>in</strong>g HRHX Surface<br />

T15 Cool<strong>in</strong>g water after absorber Surface<br />

T16 Cool<strong>in</strong>g water after condenser Surface<br />

T17 Low-temperature regenerator (LTRG) Surface<br />

T18 Refrigerant after condenser Surface<br />

T19 Refrigerant from evaporator Surface<br />

T32 Cool<strong>in</strong>g water after cool<strong>in</strong>g tower Surface<br />

T33 HTRG temperature Surface<br />

o C - 6.65<br />

o C - 30.01<br />

o C - 154.87<br />

o C - 24.26<br />

o C - 158.56<br />

o C - 99.00<br />

o C - 6.58<br />

o C 151.23 157.65<br />

o C 36.7 36.63<br />

o C 74.99 75.02<br />

o C 90.54 90.37<br />

o C 37.46 37.7<br />

o C 40.06 40<br />

o C 92.71 93.21<br />

o C 43.29 44.08<br />

o C 127.78 129.24<br />

o C 30.78 30.74<br />

o C 150.54 153.44<br />

F6 Cool<strong>in</strong>g-water flow Water kg/s 1.55 1.45<br />

T22 Steam-supply temperature Steam<br />

T23 Condensate-return temperature Water<br />

T25 Feedwater temperature Water<br />

o<br />

C 163.56 164.31<br />

o<br />

C 99.43 99.3<br />

o C 70.09 59.1<br />

P4 Steam supply pressure Steam psi 698.04 713.87<br />

P5 Condensate return pressure Water psi 101.75 100.04<br />

P7 Feedwater pressure Water psi<br />

F2 Steam flow Steam kg/s 0.00727 0.00734<br />

T20 Chilled-water supply Water<br />

T21 Chilled-water return Water<br />

T31 Ambient temperature Air<br />

o C 13.9 13.88<br />

o C 6.83 6.39<br />

o C 28.49 23.2<br />

P2 Chilled-water <strong>in</strong>let Water psi 298.58 154.23<br />

P3 Chilled-water outlet Water psi 372.32 233.33<br />

F1 Chilled water Water kg/s 0.56 0.56<br />

50


Broad specified and measured chiller performance data at design conditions are presented <strong>in</strong> Table 2-<br />

7. The chiller specified cool<strong>in</strong>g capacity is 16 kW, but the cool<strong>in</strong>g capacity of the chiller after the<br />

calibration is calculated to be 17.6 kW. The measured steam flow is about 10% higher than<br />

specifications; but the load is also 10% higher. The COPthermal of the chiller, <strong>in</strong> either case, is 1.03. The<br />

power consumption of the chiller is 0.82 kW. The results of the two tests, before and after the<br />

calibration of sensors, are quite similar; they confirm the specifications provided by the manufacturer.<br />

Table 2-7: Comparison of chiller performance under design conditions<br />

Chilled water<br />

Steam<br />

Power<br />

Perform.<br />

Name Unit Specification Before calibration After calibration<br />

Cool<strong>in</strong>g capacity kW 16 16.62 17.62<br />

Chilled-water return temperature<br />

o<br />

C 14 13.9 13.88<br />

Chilled-water supply temperature<br />

o C 7 6.83 6.39<br />

Chilled-water flow rate m 3 /h 2 2.02 2.02<br />

Chilled-water pump head mH2O 8 7.9 7.9<br />

Rated steam pressure, absolute mPa 0.7 0.698 0.714<br />

Steam consumption* kg/h 24 26.18 26.43<br />

Power voltage V 220 220 220<br />

Power frequency Hz 60 60 60<br />

Power consumption* kW 1 0.856 0.823<br />

COP (Thermal) 0.98 1.038<br />

COP (overall) 0.93 0.99<br />

* The maximum values for the specification data.<br />

2.4.3 <strong>Chiller</strong> Performance at Reduced Capacity Condition<br />

The chiller performance at the design condition is reported <strong>in</strong> subsection 2.4.2 above. To obta<strong>in</strong> chiller<br />

test data at reduced capacity, the chilled-water return temperature was decreased from 14 o C to 8 o C <strong>in</strong><br />

a series of n<strong>in</strong>e tests. In these tests the chilled- and cool<strong>in</strong>g-water flows and the cool<strong>in</strong>g water <strong>in</strong>let<br />

temperature were ma<strong>in</strong>ta<strong>in</strong>ed constant. The test conditions and results are summarized <strong>in</strong> Table 2-8.<br />

As the chilled-water return temperature and, thus, the chiller capacities were reduced, the saturated<br />

steam pressure and temperature to the chiller were also reduced. This reduction was imposed to avoid<br />

on-off cycl<strong>in</strong>g of the steam valve of the chiller and the consequent erratic chiller conditions that were<br />

observed if the steam supply pressure was ma<strong>in</strong>ta<strong>in</strong>ed at 700 kPa.<br />

Figure 2-16 shows the COP of the chiller as the cool<strong>in</strong>g capacity (load) was varied from 21% to 100%<br />

of the capacity at design conditions. As the cool<strong>in</strong>g load was varied from 4 kW to 18 kW, the thermal<br />

51


COP varied from 0.7 to 1.04. The overall COP, which considers the power consumption of the chiller,<br />

is, on average, less than the thermal COP by 5%.<br />

Figure 2-17 shows the power consumption of the chiller at various loads. The bold curve is the<br />

measured value for the chiller, and the second curve is the data from Broad’s brochure for a naturalgas-driven<br />

chiller with the same cool<strong>in</strong>g capacity and a similar configuration.<br />

Figure 2-18 compares the measured heat <strong>in</strong>put, Qheat, of this steam-driven chiller with the<br />

manufacturer’s specified heat <strong>in</strong>put from the heat of combustion of the fuel <strong>in</strong> their natural-gas-driven<br />

chiller. The ord<strong>in</strong>ate is the actual heat <strong>in</strong>put, and the abscissa is the actual cool<strong>in</strong>g load. In the figure,<br />

the bold curve is the steam-driven chiller measured <strong>in</strong> the IW, and the curve below is the rated<br />

performance curve from the manufacturer. The two curves have similar trends, but the steam-driven<br />

chiller uses more thermal energy than does the natural-gas-driven chiller.<br />

Table 2-8: Primary measurement for chiller <strong>in</strong>put and output<br />

Chilled-<br />

water<br />

flow<br />

Measurement values for chiller <strong>in</strong>puts Measurement values for chiller outputs<br />

Cool<strong>in</strong>g-<br />

water<br />

flow<br />

Chilled-<br />

water return<br />

temp.<br />

Cool<strong>in</strong>g-<br />

water supply<br />

temp.<br />

Steam<br />

supply<br />

temp.<br />

Condensate<br />

return<br />

temp.<br />

Steam<br />

flow<br />

Chilled-<br />

water supply<br />

temp.<br />

Cool<strong>in</strong>g<br />

load<br />

Test F1 F6 T20 T32 T22 T23 F2 T21 Q cool<strong>in</strong>g COP<br />

No. m 3 /h kg/s<br />

o C<br />

o C<br />

o C<br />

o C kg/h<br />

o C kW<br />

1 2.02 1.45 13.88 30.72 164.33 99.31 27.42 6.40 18.91 1.04<br />

2 2.01 1.45 14.12 30.71 164.57 99.33 25.90 6.74 17.61 1.01<br />

3 2.01 1.45 13.26 30.56 164.68 99.31 23.10 6.36 16.12 0.99<br />

4 2.00 1.46 12.85 30.35 158.63 99.23 20.60 6.57 15.25 1.01<br />

5 2.02 1.46 11.67 30.38 153.17 92.32 19.44 6.15 13.59 1.03<br />

6 2.01 1.46 10.41 30.96 150.30 76.34 15.56 5.72 10.69 0.99<br />

7 2.02 1.46 10.54 30.40 140.34 69.46 12.04 7.09 8.14 0.87<br />

8 2.02 1.46 9.60 30.51 138.72 61.58 9.96 6.89 6.40 0.80<br />

9 2.04 1.47 8.02 30.24 133.03 54.07 5.30 6.39 3.86 0.67<br />

52


Figure 2-16: <strong>Chiller</strong> performance under various load conditions<br />

Coefficient of Performance (COP) .<br />

1.3<br />

1.2<br />

1.1<br />

1.0<br />

0.9<br />

0.8<br />

0.7<br />

0.6<br />

0.5<br />

0.4<br />

Thermal COP<br />

(measurement)<br />

Overall COP<br />

(measurement)<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Thermal COP (measurement) Overall COP (measurement)<br />

Figure 2-17: <strong>Chiller</strong> power consumption under various load conditions<br />

<strong>Chiller</strong> power consumption (kW) .<br />

2.0<br />

1.6<br />

1.2<br />

0.8<br />

0.4<br />

0.0<br />

Measured power consumption<br />

for natural gas and hot water<br />

Measured power consumption<br />

for steam driven chiller<br />

Actual cool<strong>in</strong>g load (kW)<br />

Rated power consumption for<br />

natural gas driven chiller<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100% 110%<br />

Steam chiller<br />

Natural gas & hot water chiller<br />

Natural gas chiller<br />

Actual load / design load<br />

53


Figure 2-18: Comparison of chiller performance<br />

Actual heat <strong>in</strong>put (kW) .<br />

20<br />

16<br />

12<br />

8<br />

4<br />

0<br />

Steam-driven chiller<br />

Natural-gas-driven chiller<br />

0 4 8 12 16 20<br />

Steam-driven chiller Natural gas-driven chiller Actual cool<strong>in</strong>g load (kW)<br />

2.5 Further Information from <strong>Chiller</strong> Test<strong>in</strong>g<br />

The performance curves for the chiller at part-load conditions, result<strong>in</strong>g from varied chilled-water<br />

return temperatures, have been plotted and compared with Broad’s published <strong>in</strong>formation <strong>in</strong> the<br />

figures above. The chiller performance based on vary<strong>in</strong>g others of the primary operat<strong>in</strong>g condition<br />

parameters <strong>in</strong> Table 2-4 has also been determ<strong>in</strong>ed us<strong>in</strong>g the test approach <strong>in</strong>dicated <strong>in</strong> subsections<br />

2.3.1 and 2.3.2; the results are summarized <strong>in</strong> appendix 2.B. The data on chiller <strong>in</strong>ternal conditions at<br />

the various operat<strong>in</strong>g conditions will be used and analyzed <strong>in</strong> the next two chapters based on a<br />

comprehensive performance model.<br />

54


3 <strong>Chiller</strong> Design and Performance Model<br />

As described <strong>in</strong> the previous chapter, the chiller was tested at various operat<strong>in</strong>g conditions, and chiller<br />

performance was calculated on the basis of the measurements. This chapter describes how we<br />

developed a comprehensive performance model to further ref<strong>in</strong>e our understand<strong>in</strong>g of the pr<strong>in</strong>ciples of<br />

the chiller, to analyze the experimental data from the test program, to assist <strong>in</strong> equipment design, and<br />

to evaluate the performance of various <strong>BCHP</strong> systems. This model is a set of equations consist<strong>in</strong>g of<br />

mass balances, energy balances, relations describ<strong>in</strong>g the heat and mass transfer, and equations for the<br />

thermophysical properties of the work<strong>in</strong>g fluids.<br />

The model can be solved when appropriate assumptions and a certa<strong>in</strong> number of operat<strong>in</strong>g parameters<br />

are assigned, so that the conditions – pressure, temperature, composition, and flow – at each po<strong>in</strong>t<br />

with<strong>in</strong> the chiller can be calculated. The model solutions have been used to evaluate the accuracy of<br />

the measurement data and the test program. Heat and mass transfer correlations have been <strong>in</strong>tegrated<br />

<strong>in</strong>to the model so that the model cannot evaluate the chiller performance at design conditions only, but<br />

at various off-design conditions also. For the manufacturer and equipment designer, the model can be<br />

used to size the chiller components and to determ<strong>in</strong>e configurations; and for the build<strong>in</strong>g system<br />

eng<strong>in</strong>eer and architect, the model can be used to predict chiller performance under various design<br />

conditions <strong>in</strong> build<strong>in</strong>gs.<br />

3.1 Flow Diagram<br />

On the basis of the schematic flow diagram <strong>in</strong> Figure 2-2, we constructed a simplified flow diagram<br />

labeled with correspond<strong>in</strong>g numbered state po<strong>in</strong>ts as illustrated <strong>in</strong> Figure 3-1. Each state po<strong>in</strong>t is<br />

represented by its pressure, temperature, composition, and flow rate. The bold l<strong>in</strong>es represent the water<br />

refrigerant (vapor/liquid); the other l<strong>in</strong>es refer to the sorbent water-LiBr solutions. Table 3-1 describes<br />

each state po<strong>in</strong>t.<br />

55


Figure 3-1: Simplified flow diagram for chiller model<br />

12<br />

Refrigerant<br />

comb<strong>in</strong>er<br />

13<br />

Refrigerant<br />

spray nozzle<br />

17<br />

Evaporator<br />

Sorbent solution<br />

Refrigerant<br />

State po<strong>in</strong>ts: pressure, temperature,<br />

composition, flow of streams<br />

enter<strong>in</strong>g/leav<strong>in</strong>g chiller components<br />

Equilibrium states: thermal and vapor<br />

liquid equilibrium between streams<br />

leav<strong>in</strong>g a chiller component Cool<strong>in</strong>g<br />

water<br />

14<br />

16<br />

18<br />

BPHX<br />

RP<br />

Condenser<br />

Solution<br />

Splitter<br />

2<br />

1<br />

42 43<br />

Heat to<br />

Absorber<br />

32 31 42 41<br />

11<br />

SP<br />

Chilled water CHWP Cool<strong>in</strong>g water<br />

<strong>Chiller</strong><br />

25<br />

3<br />

10<br />

Steam<br />

trap<br />

9<br />

91<br />

24<br />

53<br />

HRHX<br />

4<br />

Absorber<br />

54<br />

LTHX<br />

7<br />

LTRG<br />

(<strong>in</strong>side)<br />

52<br />

Heat to<br />

LTRG<br />

Low-temp. heat exchanger<br />

5<br />

19<br />

23<br />

LTRG (outside)<br />

Solution<br />

8 comb<strong>in</strong>er<br />

Solution<br />

spray nozzle<br />

92<br />

Low-temp. regenerator<br />

6<br />

To HRHX<br />

52<br />

20 21<br />

High-temp. heat exchanger<br />

46<br />

HTHX<br />

22<br />

43<br />

Steam<br />

51<br />

High temp. regenerator<br />

HTRG<br />

from<br />

Condenser<br />

44 41 to<br />

Absorber<br />

45 47<br />

CWP<br />

Air City water<br />

Cool<strong>in</strong>g tower<br />

In Figure 3-1, the model for each chiller component consists of equations represent<strong>in</strong>g mass balances<br />

for water and LiBr, the energy balance, the work<strong>in</strong>g fluids property relations, and the heat and mass<br />

transfer relations <strong>in</strong>volv<strong>in</strong>g the state po<strong>in</strong>t conditions of the streams enter<strong>in</strong>g and leav<strong>in</strong>g the<br />

component. Once these equations are assembled for all the chiller components and solved, all the state<br />

po<strong>in</strong>t conditions of the chiller <strong>in</strong> terms of temperature, composition, pressure, flow rate, and other<br />

thermodynamic properties will have been determ<strong>in</strong>ed. The state po<strong>in</strong>t conditions of the water<br />

refrigerant and the water-LiBr sorbent solutions can be plotted on a Dűhr<strong>in</strong>g diagram as illustrated <strong>in</strong><br />

Figure 3-2. Such a plot lacks only the flow quantities to serve as a complete description of the state<br />

po<strong>in</strong>ts throughout the chiller.<br />

56


Table 3-1: <strong>Chiller</strong> model state po<strong>in</strong>t descriptions<br />

No. Stream description No. Stream description<br />

1 Sorbent solution <strong>in</strong> the absorber 2 Sorbent solution leav<strong>in</strong>g the solution pump<br />

3 Sorbent solution enter<strong>in</strong>g the LTHX 4 Solution leav<strong>in</strong>g the LTHX and enter<strong>in</strong>g the HRHX<br />

5 Sorbent solution enter<strong>in</strong>g the LTRG 6 Sorbent solution leav<strong>in</strong>g the LTRG and enter<strong>in</strong>g the LTHX<br />

7 Sorbent solution leav<strong>in</strong>g the LTHX 8 Sorbent solution after solution comb<strong>in</strong>er<br />

9 Sorbent solution pass<strong>in</strong>g spray nozzles 10 Refrigerant vapor leav<strong>in</strong>g the LTRG <strong>in</strong>to the condenser<br />

11 Refrigerant liquid leav<strong>in</strong>g condenser 12 Refrigerant liquid leav<strong>in</strong>g the BPHX<br />

13 Refrigerant liquid after refrigerant comb<strong>in</strong>er 14 Refrigerant leav<strong>in</strong>g spray nozzles<br />

15 Empty 16 Refrigerant liquid enter<strong>in</strong>g refrigerant pump<br />

17 Refrigerant liquid leav<strong>in</strong>g refrigerant pump 18 Refrigerant vapor leav<strong>in</strong>g evaporator<br />

19 Sorbent solution enter<strong>in</strong>g the HTHX 20 Sorbent solution enter<strong>in</strong>g the HTRG<br />

21 Sorbent solution leav<strong>in</strong>g the HTRG 22 Sorbent solution leav<strong>in</strong>g the HTHX<br />

23 Refrigerant vapor leav<strong>in</strong>g the HTRG 24 Refrigerant leav<strong>in</strong>g the LTRG<br />

25 Refrigerant enter<strong>in</strong>g the condenser<br />

31 Chilled-water return 32 Chilled-water supply<br />

41 Cool<strong>in</strong>g-water supply 42 Cool<strong>in</strong>g-water leav<strong>in</strong>g absorber<br />

43 Cool<strong>in</strong>g-water return 44 Cool<strong>in</strong>g-water enter<strong>in</strong>g cool<strong>in</strong>g water pump<br />

45 Ambient air enter<strong>in</strong>g cool<strong>in</strong>g tower 46 Exhaust air leav<strong>in</strong>g cool<strong>in</strong>g tower<br />

51 Steam supply enter<strong>in</strong>g the HTRG 52 Condensate leav<strong>in</strong>g the HTRG<br />

53 Condensate leav<strong>in</strong>g the HRHX 54 Condensate leav<strong>in</strong>g steam trap<br />

91 Refrigerant vapor after the spay nozzle 92 Sorbent solution after the spray nozzle<br />

3.2 Dűhr<strong>in</strong>g Chart Representation<br />

On the basis of model solutions, Figure 3-3 shows an absorption cycle at design condition with state<br />

po<strong>in</strong>ts <strong>in</strong>dicated on the Dűhr<strong>in</strong>g chart, which visualizes the absorption cycle and associated design<br />

parameters. The ord<strong>in</strong>ate of this plot is the equilibrium vapor pressure of water (kPa), and the abscissa<br />

is correspond<strong>in</strong>g temperature ( o C). The <strong>in</strong>cl<strong>in</strong>ed l<strong>in</strong>e on the left of the plot represents vapor pressuretemperature<br />

relation for the water refrigerant. The parallel l<strong>in</strong>es with<strong>in</strong> the plot represent the water<br />

vapor pressure of the sorbent solution at various concentrations and temperature. A crystallization l<strong>in</strong>e<br />

is located at the bottom of the chart. If the state po<strong>in</strong>t of solution drops below this l<strong>in</strong>e, sorbent<br />

solution will tend to deposit LiBr solid crystals.<br />

The Dűhr<strong>in</strong>g chart is a tool to rapidly perform a number of checks on the measurement data or model<br />

solutions. In such a plot, many design parameters can be illustrated, such as the heat rejection<br />

temperatures, solution concentrations, equilibrium pressures, and p<strong>in</strong>ch po<strong>in</strong>t of each heat transfer<br />

component. In Figure 3-2, the connected bold l<strong>in</strong>es <strong>in</strong> the middle of the figure are the water-LiBr<br />

sorbent solution, and the bold dash l<strong>in</strong>es represent the refrigerant. The l<strong>in</strong>es are connected to form two<br />

complete cycles: the sorbent solution cycle and the refrigerant cycle. The state po<strong>in</strong>ts <strong>in</strong>dicated on the<br />

57


cycles are identical to those used <strong>in</strong> the flow diagram <strong>in</strong> Figure 3-2. The major chiller components are<br />

<strong>in</strong>dicated on the diagram by dashed ellipses.<br />

In the Dűhr<strong>in</strong>g chart, a p<strong>in</strong>ch po<strong>in</strong>t is one of the notable features of the heat exchanger. The<br />

temperature p<strong>in</strong>ch po<strong>in</strong>t is the po<strong>in</strong>t of m<strong>in</strong>imum temperature difference between the fluids <strong>in</strong>volved <strong>in</strong><br />

the heat transfer process. The p<strong>in</strong>ch po<strong>in</strong>t usually occurs at either the <strong>in</strong>let or the outlet of the heat<br />

exchanger. Small temperature differences at the p<strong>in</strong>ch po<strong>in</strong>t require large heat transfer areas <strong>in</strong> the<br />

exchanger.<br />

Figure 3-2: Dűhr<strong>in</strong>g chart at design condition<br />

Evaporator<br />

20<br />

T31<br />

Steam, cool<strong>in</strong>g water, and chilled water<br />

Water-LiBr sorbent solution<br />

Refrigerant<br />

Condenser<br />

T11<br />

T43<br />

T42 40<br />

T41<br />

30<br />

P<strong>in</strong>ch po<strong>in</strong>t<br />

REFRIGERANT TEMPERATURE, C<br />

50<br />

60<br />

57.39 %<br />

70<br />

61.68 %<br />

80<br />

90<br />

0<br />

30%<br />

40%<br />

T3210<br />

evaporator<br />

1<br />

5<br />

1 7<br />

Pl<br />

T18 0<br />

91 22<br />

10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180<br />

P<strong>in</strong>ch po<strong>in</strong>t<br />

for absorber<br />

Absorber<br />

P<strong>in</strong>ch po<strong>in</strong>t<br />

Condenser<br />

LTHX<br />

4<br />

P<strong>in</strong>ch po<strong>in</strong>t for LTHX<br />

P<strong>in</strong>ch po<strong>in</strong>t for HTHX<br />

o<br />

LTRG<br />

5<br />

T53<br />

110<br />

T54<br />

6<br />

100<br />

T1 T91 T7 T4 T5 T6<br />

T20<br />

T21<br />

T22<br />

50%<br />

HTHX<br />

57.39 %<br />

P<strong>in</strong>ch po<strong>in</strong>t<br />

for LTRG<br />

60%<br />

HRHX<br />

120<br />

70%<br />

62.81 %<br />

o<br />

SOLUTION TEMPERATURE, C<br />

Equlibrium Chart for A queous Lithium Bromide Solutions<br />

20<br />

HTRG<br />

T52<br />

21<br />

T51<br />

Ph<br />

P<strong>in</strong>ch po<strong>in</strong>t<br />

for HTRG<br />

Pm<br />

200<br />

150<br />

100<br />

50<br />

40<br />

30<br />

20<br />

10<br />

5<br />

4<br />

3<br />

2<br />

58<br />

SATUATION PRESSURE (P), kPa


3.3 T-Q Diagram<br />

The temperature heat (T-Q) diagram is another tool to <strong>in</strong>dicate the p<strong>in</strong>ch po<strong>in</strong>ts of each heat transfer<br />

component. The T-Q diagram for heat transfer components <strong>in</strong> this chiller are illustrated <strong>in</strong> Figure 3-3.<br />

The ord<strong>in</strong>ate is the stream temperatures along the length of the heat exchanger. The abscissa is the<br />

quantity of heat transferred between the streams up to any given po<strong>in</strong>t along the length of the<br />

exchanger.<br />

Figure 3-3: T-Q diagram for the heat transfer components<br />

o<br />

C<br />

160<br />

140<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

22<br />

1<br />

HTHX<br />

51<br />

21<br />

20<br />

HTRG<br />

20<br />

LTRG<br />

52<br />

23<br />

0<br />

0 5 10 15 20 25 30<br />

7<br />

1<br />

6<br />

5<br />

4<br />

53<br />

LTHX HRHX<br />

3.4 Calculation Procedure<br />

5<br />

43<br />

35<br />

24<br />

Condenser<br />

9<br />

11<br />

42<br />

Absorber<br />

31<br />

18<br />

32<br />

14<br />

40 45 50 55 60 65 70 75 80 85 kW<br />

1<br />

41<br />

Evaporator<br />

This steady-state chiller model is a set of nonl<strong>in</strong>ear algebraic equations, described <strong>in</strong> subsection 3.1.1<br />

above, programmed <strong>in</strong> the Eng<strong>in</strong>eer<strong>in</strong>g Equation Solver (EES), which relate state-po<strong>in</strong>t conditions –<br />

pressure, temperature, composition, and flow rates, and equipment design parameters throughout the<br />

chiller. The EES equations of each component with equation type, <strong>in</strong>clud<strong>in</strong>g mass balance, energy<br />

balance, heat transfer equations, thermal property functions, phase equilibrium equations, and the<br />

assumptions, are annotated <strong>in</strong> appendix 3A.<br />

The procedure for the EES calculation is straightforward: first, the algebraic equations are entered <strong>in</strong>to<br />

EES. Enough state-po<strong>in</strong>t conditions are entered so that the number of equations is equal to the number<br />

of the rema<strong>in</strong><strong>in</strong>g, unknown state-po<strong>in</strong>t conditions. Reasonable estimates are entered for all these<br />

59


unknown conditions. The properties, such as the enthalpy and equilibrium functions, are related to the<br />

pressure, temperature, composition, and vapor quality of water/steam and sorbent solutions by<br />

equations <strong>in</strong> the EES. The EES then solves the equations by adjust<strong>in</strong>g the estimates to reach a solution<br />

of the equations. The chiller model comprises 416 variables, state-po<strong>in</strong>t operat<strong>in</strong>g conditions, and 409<br />

equations express<strong>in</strong>g basic eng<strong>in</strong>eer<strong>in</strong>g pr<strong>in</strong>ciples. The equations can be solved when seven variable<br />

<strong>in</strong>puts are provided. Once the model has been solved, the conditions of each state po<strong>in</strong>t <strong>in</strong> the flow<br />

diagram are known. The solutions can be used to check the measurement data from the test program.<br />

3.4.1 Mass Balance<br />

For each chiller component, the steady-state total mass balance equation for refrigerant, chilled water,<br />

cool<strong>in</strong>g water, steam and condensate, and LiBr can be expressed as:<br />

where, m& = mass flow rate.<br />

∑ m& <strong>in</strong> = ∑ m&<br />

out<br />

.<br />

(Equation 3 - 1)<br />

In equation 3-1, subscripts <strong>in</strong> and out mean the streams enter<strong>in</strong>g and leav<strong>in</strong>g each of the chiller<br />

components. The mass balance of LiBr associated with absorption and regeneration processes can be<br />

expressed <strong>in</strong> the follow<strong>in</strong>g equation:<br />

∑<br />

Solution<br />

∑<br />

m& ∗ x = m&<br />

∗ x<br />

(Equation 3 - 2)<br />

<strong>in</strong><br />

<strong>in</strong><br />

Solution<br />

where, x = the weight concentration of the water-LiBr sorbent solution.<br />

3.4.2 Energy Balance<br />

out<br />

out<br />

As the basic format of energy, heat, and external work associated with the fluids are observed when<br />

they cross the boundaries of each chiller component. In the chiller, except for three pumps, no work is<br />

<strong>in</strong>volved <strong>in</strong> the components. The steady-state energy balance for each chiller component is expressed<br />

<strong>in</strong> the equation below:<br />

Q& −W& shaft + ∑ m&<br />

jh<br />

j = 0<br />

(Equation 3 - 3)<br />

where Q& is the quantity of heat transfer to or from the system; Wshaft & is the quantity of shaft work<br />

done by the system; m& is the mass flow of each stream; and h is the enthalpy of each stream.<br />

60


For <strong>in</strong>stance, the cycle <strong>in</strong>volv<strong>in</strong>g with absorb process, the energy balance us<strong>in</strong>g equation 3-3 can be<br />

written <strong>in</strong> the follow<strong>in</strong>g equation:<br />

Q + m&<br />

h + m&<br />

h = m&<br />

h<br />

(Equation 3 - 4)<br />

water<br />

water<br />

conc<br />

conc<br />

dilute<br />

dilute<br />

3.4.3 Thermodynamic Property and Equilibrium Relations<br />

Fluid properties are used widely <strong>in</strong> the model. In EES, the states and properties of specific fluid can be<br />

related by <strong>in</strong>ternal functions. For pure water and steam, the follow<strong>in</strong>g functions are often used to<br />

provide equilibrium states.<br />

Thermal property relation:<br />

j<br />

( water steam,<br />

T = T P P )<br />

h = enthalpy / , =<br />

(Equation 3 - 5)<br />

Phase equilibrium for saturated liquid and vapor <strong>in</strong> equilibrium:<br />

j<br />

( water / steam P Pj<br />

)<br />

( water / steam T Tj<br />

)<br />

( water steam,<br />

h = h P P )<br />

j<br />

T = T _ SAT<br />

, =<br />

(Equation 3 - 6)<br />

P = P _ SAT<br />

, =<br />

(Equation 3 - 7)<br />

j<br />

q = quality / , =<br />

(Equation 3 - 8)<br />

j<br />

For the cool<strong>in</strong>g-tower model, moist air properties can be evaluated by the follow<strong>in</strong>g relations <strong>in</strong> EES:<br />

3.4.4 Heat Transfer Models<br />

j<br />

= Enthalpy(Air<br />

, P = P , T = T , R = RH )<br />

(Equation 3 - 9)<br />

h j<br />

H2O j j<br />

j<br />

j<br />

= Wetbulb(Air<br />

, T = T , P = P , R = RH ) (Equation 3 - 10)<br />

Tj -wb<br />

H2O j j<br />

j<br />

RH =<br />

, T = T , P = P , w = w )<br />

(Equation 3 - 11)<br />

j<br />

Relhum(AirH2O j j<br />

j<br />

Heat transfer, <strong>in</strong> some components, coupled with mass transfer, occurs throughout the absorption<br />

chiller. Although a full understand<strong>in</strong>g of both the heat and mass transfer process <strong>in</strong> the absorber is<br />

necessary and critical, it is usually more convenient to analyze them respectively with heat transfer<br />

study <strong>in</strong> the first step and coupled mass transfer next. This allows us to handle the problems from the<br />

simple to the complex.<br />

j<br />

61


In the model, the UA-LMTD (UA-log mean temperature difference) values are used to evaluate the<br />

follow<strong>in</strong>g heat transfer components: absorber, evaporator, condenser, HTRG, LTRG, HRHX, and<br />

BPHX.<br />

In the log-mean temperature difference (UA-LTMD) approach, f<strong>in</strong>d<strong>in</strong>g the product of the overall heat<br />

transfer coefficient and the heat exchanger surface area is convenient for specify<strong>in</strong>g the size and<br />

performance of a heat exchanger.<br />

Q<br />

UA = (Equation 3 - 12)<br />

∆T<br />

LMTD<br />

In equation (3-12), Q is the quantity of heat transferred <strong>in</strong> the components. ∆ TLMTD<br />

is the log-mean<br />

temperature difference; it is expressed below as:<br />

( T − T ) − ( T − T )<br />

hot,<br />

<strong>in</strong> cold , out hot,<br />

out cold , <strong>in</strong><br />

∆ TLMTD<br />

=<br />

(Equation 3 - 13)<br />

Thot,<br />

<strong>in</strong> − Tcold<br />

, out<br />

ln<br />

T<br />

hot,<br />

out<br />

− T<br />

cold , <strong>in</strong><br />

In equation (3-13), subscripts hot and cold refer to the hot and cold streams, respectively; the<br />

subscripts <strong>in</strong> and out refer to the <strong>in</strong>let and outlet of a stream.<br />

The other two m<strong>in</strong>or heat exchangers (HTHX and LTHX) are evaluated by the heat transfer<br />

effectiveness method. For effectiveness-type heat exchanger models, the effectiveness, ε , is def<strong>in</strong>ed<br />

as the ratio of the actual heat transfer, Q actual , to the maximum potential heat transfer, Q max , below:<br />

Q<br />

( Tcold<br />

, out − Tcold<br />

, <strong>in</strong> )<br />

( T − T )<br />

or<br />

( Thot,<br />

<strong>in</strong> − Tcold<br />

, out )<br />

( T − T )<br />

actual ε = =<br />

(Equation 3 - 14)<br />

Qmax<br />

hot,<br />

<strong>in</strong> cold , <strong>in</strong><br />

hot,<br />

<strong>in</strong> cold , <strong>in</strong><br />

The def<strong>in</strong>ition of effectiveness <strong>in</strong> terms only of the temperatures makes it a convenient heat exchanger<br />

performance parameter.<br />

3.4.5 Overall Heat Transfer Coefficient Model<br />

In practice, the overall heat transfer coefficient, U, is not a constant variable <strong>in</strong> describ<strong>in</strong>g the heat<br />

exchanger but is a function of flow rate, temperature, pressure, and other properties. Physical<br />

<strong>in</strong>formation on the heat exchanger configuration and the characteristics of flow <strong>in</strong> and out of the heat<br />

exchanger must be known to calculate the overall heat transfer coefficient and heat exchanger surface<br />

62


area. Table 3-3 summarizes heat and mass transfer correlations for the various chiller components. The<br />

values of U <strong>in</strong> the HTRG adapt for different heat<strong>in</strong>g media as listed <strong>in</strong> the table.<br />

Table 3-2: Physical features of heat and mass transfer components<br />

Steam<br />

<strong>Chiller</strong> Tube bank Surface Inside<br />

Component Material Type Treatment Media Process Media Process<br />

Evaporator Copper Spiral tube Grooved Refrigerant Evaporation Chilled water Convection<br />

Absorber Copper Spiral tube Smooth LiBr Convection Cool<strong>in</strong>g water Convection<br />

Condenser Copper Spiral tube Smooth Refrigerant Condensation Cool<strong>in</strong>g water Convection<br />

LTRG Copper Straight tube Grooved LiBr Boil<strong>in</strong>g Water vapor Condensation<br />

HTRG Copper Spiral tube Grooved LiBr Boil<strong>in</strong>g Steam Condensation<br />

Hot water HTRG Copper Straight tube Grooved LiBr Boil<strong>in</strong>g Hot water Convection<br />

Natural gas<br />

HTRG Steel Comb. chamber Grooved LiBr Boil<strong>in</strong>g Combustion gases Radiation<br />

Steel Straight tube Grooved LiBr Boil<strong>in</strong>g Combustion gases Convection<br />

Exhaust gas HTRG Steel Straight tube Grooved LiBr Boil<strong>in</strong>g Exhaust gases Convection<br />

The overall heat transfer coefficient calculated for circular tube is a function of two heat-transfer<br />

coefficients, hi and h o :<br />

UA<br />

overall<br />

=<br />

1<br />

h A<br />

<strong>in</strong><br />

<strong>in</strong><br />

1<br />

ln out +<br />

2πkL<br />

( d d )<br />

<strong>in</strong><br />

+<br />

h<br />

out<br />

1<br />

A<br />

out<br />

(Equation 3 - 15)<br />

The subscripts <strong>in</strong> and out refer to the <strong>in</strong>side and outside of the tube. A<strong>in</strong> refers to the <strong>in</strong>side surface and<br />

Aout refers to the outside surface of the tube. In this model, the heat transfer resistance of the tube wall<br />

is neglected. The area difference between the tube <strong>in</strong>side surface and outside surface is very small, so<br />

the outside surface area of the tube is used as heat exchanger area A. Heat transfer coefficients<br />

h<strong>in</strong> and hout can be calculated by the empirical equations <strong>in</strong> Table 3-3 that relate to steam states, fluid<br />

properties, and physical configurations.<br />

Heat transfer areas, A, sometimes are not constant when partial load operation is considered. For<br />

<strong>in</strong>stance, concentrated solution spray from nozzles on the surface of the absorber tube bank and the<br />

refrigerant from nozzles on the surface of the evaporator tube banks may not cover the tubes at low<br />

flow conditions. In this model all the heat transfer areas, A, are assumed to be constants.<br />

63


Table 3-3: Heat and mass transfer correlations used <strong>in</strong> the performance model<br />

Component Reference Process Equation Comment<br />

Evaporator<br />

Absorber<br />

Condenser<br />

HTRG<br />

LTRG<br />

Cool<strong>in</strong>g<br />

Tower<br />

HTRG<br />

HTRG<br />

HTRG<br />

Chun and<br />

Seban<br />

Dittus and<br />

Boelter<br />

Water film on<br />

2<br />

1 3<br />

⎛ v ⎞<br />

hevp− film⎜<br />

⎟ 3<br />

evp−<br />

film evp−<br />

tube surface ( ) ( ) 65 . 0<br />

4 . 0<br />

3 −<br />

= . 8×<br />

10 Re Pr<br />

Chilled water <strong>in</strong><br />

tube<br />

Vliet et al. LiBr solution film<br />

on tube surface<br />

Dittus and<br />

Boelter<br />

Cool<strong>in</strong>g water <strong>in</strong><br />

tube<br />

Vliet et al. Vapor absorption<br />

rate on tube<br />

surface<br />

Nagaoka et al. Vapor absorption<br />

coefficient on<br />

tube surface<br />

Kern D. Q. Condensation<br />

film on tube<br />

surface<br />

Dittus and<br />

Boelter<br />

Jakob and<br />

Hawk<strong>in</strong>s<br />

Cool<strong>in</strong>g water <strong>in</strong><br />

tube<br />

Nucleate boil<strong>in</strong>g<br />

Kern D. Q. Condensation<br />

film <strong>in</strong> tube<br />

Jakob and<br />

Hawk<strong>in</strong>s<br />

h<br />

⎜ g k ⎟<br />

⎝ ⋅ ⎠<br />

d<br />

3 film<br />

evp−chw<br />

30<br />

0.<br />

8 0.<br />

3<br />

= 0. 023Reevp−chw<br />

Prevp−chw<br />

k30<br />

− 1<br />

3<br />

0.<br />

46 1.<br />

5 91 91<br />

− 0.<br />

30 Re − 91 2 ⎟<br />

91<br />

⎟<br />

⎛ µ Γ ⎞<br />

h =<br />

k ⎜<br />

abs film<br />

abs film ⎜ ρ g<br />

h<br />

d<br />

abs−<br />

cw 40 0.<br />

8 0.<br />

4<br />

= . 023Reabs−cw<br />

Prabs−<br />

k40<br />

0 cw<br />

⎝<br />

⎠<br />

For vertical tube<br />

Equation summarized for the ¾-<br />

<strong>in</strong>ch (19 mm) smooth tube bank<br />

with Octhyl Alcohol surfactant<br />

0.<br />

46 q&<br />

abs<br />

m&<br />

abs−<br />

vapor = 0. 30 Reabs−<br />

film<br />

h fg<br />

Equation summarized for the ¾-<br />

<strong>in</strong>ch (19 mm) smooth tube bank<br />

with Octhyl Alcohol surfactant<br />

k abs = 29.571Γ<br />

91 + 0.405<br />

Equation summarized for the ¾-<br />

<strong>in</strong>ch (19 mm) smooth tube bank<br />

with Octhyl Alcohol surfactant<br />

hcond− film<br />

h<br />

2 ⎛ v ⎞<br />

⎜ 11 ⎟<br />

⎜ 3 ⎟<br />

⎝ k11g<br />

⎠<br />

d<br />

1 3<br />

= 1.<br />

51Re<br />

−1<br />

3<br />

11<br />

cond − cw<br />

k49<br />

49 0.<br />

8 0.<br />

4<br />

= 0. 023 Recond<br />

−cw<br />

Prcond<br />

−cw<br />

htrg −nucleate<br />

51 21<br />

0.<br />

4<br />

3⎛<br />

p ⎞ h<br />

⎜<br />

⎟<br />

p0<br />

1<br />

on tube surface h = 1042(<br />

T −T<br />

)<br />

Nucleate boil<strong>in</strong>g<br />

Kern D. Q. Condensation<br />

film <strong>in</strong> tube<br />

Jakob and<br />

Hawk<strong>in</strong>s<br />

Dittus and<br />

Boelter<br />

Jakob and<br />

Hawk<strong>in</strong>s<br />

hhtrg− film<br />

2 ⎛ v ⎞<br />

⎜ 51 ⎟<br />

⎜ 3 ⎟<br />

⎝ k51g<br />

⎠<br />

1 3<br />

= 1.<br />

51Re<br />

1<br />

on tube surface h = ( T − T )<br />

Nucleate boil<strong>in</strong>g<br />

ltrg −nucleate<br />

⎝<br />

−1<br />

3<br />

51<br />

0.<br />

4<br />

3<br />

1042 24 6 ⎟<br />

0<br />

⎟<br />

⎛ p ⎞ m<br />

⎜<br />

p<br />

2<br />

1 3<br />

−1<br />

3<br />

4<br />

24<br />

24<br />

− 1.<br />

51<br />

3<br />

⎟<br />

24<br />

24<br />

⎟<br />

⎛ v ⎞ ⎛ Γ ⎞<br />

h ⎜ ⎟ = ⎜<br />

ltrg film⎜<br />

k g ⎟ µ<br />

NTU =<br />

⎝<br />

ln<br />

⎠<br />

⎝<br />

( hs43<br />

− h46<br />

) − ( hs44<br />

− h45<br />

)<br />

( ( hs − h − δ ) ( hs − h − δ ) )<br />

43<br />

46<br />

(h<br />

46<br />

ct<br />

- h<br />

1<br />

on tube surface h = 1042(<br />

T −T<br />

)<br />

Hot water <strong>in</strong> tube<br />

Nucleate boil<strong>in</strong>g<br />

Hottel, et al. Combustion<br />

process <strong>in</strong><br />

chamber<br />

Hausen Exhaust gas <strong>in</strong><br />

tube<br />

Jakob and<br />

Hawk<strong>in</strong>s<br />

htrg −nucleate<br />

h<br />

htrg −hw<br />

k<br />

55<br />

d<br />

55<br />

=<br />

51<br />

21<br />

⎝<br />

45<br />

3<br />

)<br />

44<br />

⎠<br />

⎠<br />

⎠<br />

45<br />

0.<br />

4<br />

⎛ p ⎞ h<br />

⎜<br />

⎟<br />

⎝ p0<br />

⎠<br />

0.<br />

8 0.<br />

3<br />

0. 023Rehtrg<br />

−hw<br />

Prhtrg<br />

−hw<br />

1<br />

on tube surface h = 1042(<br />

T −T<br />

)<br />

Nucleate boil<strong>in</strong>g<br />

J. P. Holman Exhaust gas <strong>in</strong><br />

tube<br />

htrg −nucleate<br />

Q<br />

h<br />

51<br />

21<br />

3<br />

0.<br />

4<br />

⎛ p ⎞ h<br />

⎜<br />

⎟<br />

⎝ p0<br />

⎠<br />

4<br />

4<br />

( T ) σT<br />

α ( T ) σ<br />

radiation = ε g g g − g w Tw<br />

Acc<br />

htrg − gas<br />

k<br />

d 0.<br />

0668<br />

= 3.<br />

66 +<br />

1+<br />

0.<br />

04<br />

1<br />

on tube surface h = ( T − T )<br />

htrg −nucleate<br />

h<br />

htrg −exgas<br />

k<br />

55<br />

d<br />

55<br />

( )<br />

[ ( ) ] 3 2<br />

d L Red<br />

Pr<br />

d L Re Pr<br />

1042 21<br />

d<br />

0.<br />

4<br />

3<br />

⎟<br />

0<br />

⎟<br />

g<br />

⎛ p ⎞ h<br />

⎜<br />

p<br />

=<br />

0.<br />

8<br />

0.<br />

4<br />

0. 023Rehtrg<br />

−exgas<br />

Prhtrg<br />

−exgas<br />

⎝<br />

⎠<br />

ct<br />

Steam as heat<strong>in</strong>g medium<br />

See paper<br />

Hot water as heat<strong>in</strong>g medium<br />

Natural gas as heat<strong>in</strong>g medium<br />

Lam<strong>in</strong>ar flow<br />

Exhaust as heat<strong>in</strong>g medium<br />

Turbulent flow<br />

64


3.4.6 Mass Transfer Models<br />

The process of mass transfer is complicated by coupled heat transfer and by the properties of the<br />

work<strong>in</strong>g fluids. Mass transfer occurs <strong>in</strong> the absorber, the HTRG, and the LTRG. The boil<strong>in</strong>g processes<br />

<strong>in</strong> the LTRG and HTRG, however, mix the solution well, and therefore the mass transfer effects are<br />

m<strong>in</strong>imized. In the model only the mass transfer <strong>in</strong> the absorber is considered. Numerous model<strong>in</strong>g and<br />

experimental studies found that the absorption process is controlled by the mass transfer resistance on<br />

the liquid side. This is because the refrigerant vapor absorbed at the liquid <strong>in</strong>terface transfers slowly<br />

<strong>in</strong>to the bulk of the liquid. The absorption of additional refrigerant is <strong>in</strong>hibited. The energy released at<br />

the liquid <strong>in</strong>terface causes an <strong>in</strong>crease <strong>in</strong> temperature there, and this energy must also transfer through<br />

the liquid film to the bulk of the liquid.<br />

A coupled mass and heat transfer model for the absorber is developed on the basis of a correlation<br />

given by Cosenza and Vliet [4]. They found that the mass transfer rate is a l<strong>in</strong>ear relation to the heat<br />

transfer rate. They also observed this relation by experiment on a ¾ -<strong>in</strong>ch (19mm) tube bank. The<br />

details of their studies and how this relation is implemented <strong>in</strong> the model<strong>in</strong>g will be discussed further<br />

<strong>in</strong> appendix 3A.<br />

3.4.7 Model Assumptions<br />

The follow<strong>in</strong>g assumptions are employed to properly represent the absorption cycle:<br />

• The control of streams between components allows only all liquid or all gaseous flows. The<br />

system operates at steady-state conditions. There is no accumulation/depletion of mass or<br />

energy at any po<strong>in</strong>t with<strong>in</strong> the system.<br />

• The overall system is considered a three-pressure system:<br />

o The high-pressure, P h , is determ<strong>in</strong>ed by the equilibrium water vapor pressure and the<br />

temperature enter<strong>in</strong>g the condenser. The pressures <strong>in</strong> the HTRG and <strong>in</strong> the heat<strong>in</strong>g tubes<br />

of the LTRG are at this high pressure.<br />

o The <strong>in</strong>termediate-pressure, P m , is determ<strong>in</strong>ed by the equilibrium water vapor pressure<br />

and temperature of the refrigerant leav<strong>in</strong>g the condenser. The pressure of sorbent solution<br />

<strong>in</strong> the LTRG is at this <strong>in</strong>termediate pressure.<br />

o The low-pressure, P l , is determ<strong>in</strong>ed by the equilibrium of water vapor pressure and<br />

temperature of the refrigerant <strong>in</strong> the evaporator. The sorbent solution <strong>in</strong> the absorber is at<br />

65


this same pressure. The pressure difference due to flow from the evaporator to the<br />

absorber is small enough to be neglected. (Herold, Radermacher, and Kle<strong>in</strong> consider the<br />

equilibrium pressure of refrigerant at state po<strong>in</strong>t 18 as represent<strong>in</strong>g the low pressure <strong>in</strong> the<br />

absorber and the evaporator.)<br />

• The dilute solution leav<strong>in</strong>g the absorber is <strong>in</strong> phase equilibrium at the same water vapor<br />

pressure as the refrigerant from the evaporator.<br />

• The temperatures of superheated vapors leav<strong>in</strong>g two regenerators have the same temperature<br />

as the concentrated solution leav<strong>in</strong>g the HTRG and the LTRG. (Koeppel, Kle<strong>in</strong>, and Mitchell<br />

took the follow<strong>in</strong>g po<strong>in</strong>t of view, that refrigerant vapor leav<strong>in</strong>g the regenerator has the<br />

equilibrium temperature of the weak solution at regenerator pressure.)<br />

• The steam <strong>in</strong>put is saturated vapor, and the condensate after the steam trap is saturated liquid.<br />

• There is no liquid carryover between the evaporator and the absorber.<br />

• Flow restrictors, such as expansion valves, spray nozzles, and the steam trap are adiabatic.<br />

• Pump work is isentropic. There are no pressure changes except for flow restrictors and pumps.<br />

Flow head losses <strong>in</strong> the pip<strong>in</strong>g system are negligible.<br />

• There are no convection and radiation heat losses through surfaces to ambient.<br />

3.5 Model Steps<br />

Figure 3-4 illustrates the steps <strong>in</strong> the use of the performance model to deal with the chiller<br />

performance for design and off-design conditions. These steps are listed below:<br />

1. Estimate the chiller cool<strong>in</strong>g capacity, COP, and heat source conditions theoretically on the<br />

basis of desired sorbent composition, chilled water, and cool<strong>in</strong>g-water conditions.<br />

2. Estimate the UA values (heat transfer areas) of the n<strong>in</strong>e heat transfer components <strong>in</strong> a design<br />

model when the design operat<strong>in</strong>g conditions and the approach temperatures are taken <strong>in</strong>to the<br />

design model. The heat transfer areas can be estimated for design condition.<br />

3. Construct a performance model for design and off-design conditions, the actual U (heat<br />

transfer coefficient) and A (heat transfer surface area) of five major heat exchangers can be<br />

calculated from the chiller physical configurations (from the manufacturer) and heat and mass<br />

transfer correlations. These heat transfer correlations are corrected by the comparison of the<br />

actual U, A, and the solution from the design model.<br />

4. <strong>An</strong>alyze the accuracy of the measurements and validate the model at design and off-design<br />

conditions. The corrected UA values from step 2 are used to construct a performance model<br />

66


that can predict the chiller performance under design and off-design operation conditions. The<br />

analytical method and results <strong>in</strong> this last step will be discussed further <strong>in</strong> chapter 4.<br />

Figure 3-4: Steps <strong>in</strong> the use of the performance model<br />

The design model and the performance model both use the same equations and assumptions; they are<br />

identical except for the structure of calculation. The design model estimates UA values of the n<strong>in</strong>e heat<br />

transfer components on the basis of desired chiller performance for the design condition; the structure<br />

of a design model is illustrated <strong>in</strong> Figure 3-5. In the design model, appropriate UA values are<br />

determ<strong>in</strong>ed from assumed p<strong>in</strong>ch-po<strong>in</strong>t temperatures for heat transfer components.<br />

The performance model uses the U and A values by detailed heat transfer coefficient correlations from<br />

the literature and the chiller <strong>in</strong>formation from the manufacturer. The U and A values are corrected on<br />

the basis of <strong>in</strong>itial estimation of UA values from the design model. The structure of the performance<br />

model is illustrated <strong>in</strong> Figure 3-6. In the performance model, the UA solutions of different heat<br />

transfer components replace the p<strong>in</strong>ch-po<strong>in</strong>t temperatures <strong>in</strong> the design model. Up to now, both the<br />

design model and the performance model represent the chiller performance under design conditions.<br />

67


Off-design conditions can be modeled when the physical-mathematical model of heat and mass<br />

transfer characteristics are described <strong>in</strong> the performance model.<br />

Figure 3-5: Structure of the design model Figure 3-6: Structure of performance model<br />

Once the heat and mass transfer characteristics of the chiller are described <strong>in</strong> the performance model,<br />

the model can be used to represent the off-design conditions as the chiller tested on the basis of the test<br />

program. The simulation outputs are used to compare with the test data. Discrepancies are acquired to<br />

identify measurement that may be <strong>in</strong>accurate. The performance model will be validated by m<strong>in</strong>imiz<strong>in</strong>g<br />

the deviations between the model solutions and the test data. <strong>An</strong> experimental data-driven model<br />

approach will be used to tune up the performance model, particularly those uncerta<strong>in</strong>ties that exist <strong>in</strong><br />

the model assumptions.<br />

68


4 Model-based Experimental Data <strong>An</strong>alysis<br />

The comprehensive model developed for the chiller <strong>in</strong> chapter 3 has been used to analyze the<br />

experimental data from the test program. The computational model has been used to calculate all<br />

chiller <strong>in</strong>ternal work<strong>in</strong>g conditions from a limited number of measurements. The discrepancies<br />

between the measurements and the model calculations have been m<strong>in</strong>imized by adjust<strong>in</strong>g the model<br />

assumptions. The discrepancies between the measurements and the model solutions are <strong>in</strong>troduced<br />

ma<strong>in</strong>ly by the follow<strong>in</strong>g:<br />

• <strong>in</strong>accurate stream flow temperature measurements from sensors mounted on the external pipe<br />

surface<br />

• fluctuat<strong>in</strong>g measurements of steam flow due to periodic feedwater addition to the boiler<br />

• imprecise cool<strong>in</strong>g water flow measurements due to space limitations <strong>in</strong> mount<strong>in</strong>g the flow<br />

sensor<br />

• <strong>in</strong>accurate assumptions regard<strong>in</strong>g the quality of the refrigerant flow from various chiller<br />

components<br />

• <strong>in</strong>accurate values of heat transfer coefficients calculated from available correlations<br />

The absorption cycle on a Dűhr<strong>in</strong>g diagram for each test has been plotted on the basis of the model<br />

calculations. The variation trends of temperature, pressure, and composition of critical state po<strong>in</strong>ts<br />

have been summarized symmetrically on the Dűhr<strong>in</strong>g diagram and other plots. On the basis of the<br />

model analysis results, the strategies to improve the chiller performance (particularly at the partial load<br />

conditions) have been devised and the model has been validated to calculate chiller performance under<br />

various operat<strong>in</strong>g conditions.<br />

4.1 <strong>An</strong>alytical Method<br />

Figure 4-1 illustrates the analytical method used <strong>in</strong> the model-based data analysis process. First, when<br />

a set of steady-state test data is available, the outlier data are removed. Second, the experimental data<br />

from the chiller test are averaged. Third, the seven operat<strong>in</strong>g parameters from the averaged data are<br />

used as the model <strong>in</strong>put to solve the model. The seven <strong>in</strong>put parameters for the model are listed <strong>in</strong><br />

Table 4-1 <strong>in</strong> bold; the values of the measured values are listed under the “sensor” column. The values<br />

of 11 measured operat<strong>in</strong>g parameters used for check<strong>in</strong>g model calculations are also listed <strong>in</strong> Table 4-1.<br />

In the table, two sets of number<strong>in</strong>g systems are used, one for the sensor, the values under the “sensor”<br />

column be<strong>in</strong>g the average value of steady-state data, and the other number<strong>in</strong>g system for the model<br />

69


state po<strong>in</strong>ts, the calculated values be<strong>in</strong>g those listed <strong>in</strong> the “model” columns. The measured values<br />

from the chiller tests are compared with the same operat<strong>in</strong>g parameters calculated by the eng<strong>in</strong>eer<strong>in</strong>g<br />

equation solver, EES, from the chiller model.<br />

Figure 4-1: Data analytical procedure flow diagram<br />

The differences between the calculated and measured values of the 11 operat<strong>in</strong>g parameters are<br />

weighted and summed <strong>in</strong> a statistical procedure to arrive at a measure of the data accuracy and model<br />

validity. If this measure is unsatisfactory, the data are exam<strong>in</strong>ed for possible errors and discrepancies,<br />

and the model assumptions are adjusted to reduce the discrepancies <strong>in</strong> calculated and measured<br />

operat<strong>in</strong>g conditions. If the statistical measure is satisfactory, the calculated and test data are plotted on<br />

a Dűhr<strong>in</strong>g chart.<br />

This analytical method is used throughout the data analysis process for all test data. The statistical<br />

analysis procedure and the results of the analysis are presented <strong>in</strong> the follow<strong>in</strong>g sections.<br />

4.1.1 Statistical <strong>An</strong>alysis Procedure<br />

The statistical analysis procedure <strong>in</strong>troduced <strong>in</strong> Figure 4-1 is used to evaluate the deviations between<br />

the model calculations and the test measurements. The statistical model is based on the follow<strong>in</strong>g<br />

equation:<br />

2<br />

n ⎛ ∆X<br />

⎞ n<br />

∑ ⎜<br />

⎟<br />

1<br />

=<br />

⎝ X n<br />

σ<br />

⎠ , (Equation 4 - 1)<br />

n −1<br />

70


Table 4-1: Measured values and model calculations for 100% and 55% of design load conditions<br />

Temperature<br />

Flow<br />

Pressure<br />

Power<br />

Calculation<br />

Stream name Label 100% 55%<br />

Condensate after HTRG * T11 T52<br />

Solution <strong>in</strong> absorber * T12 T1<br />

Solution enter<strong>in</strong>g HRHX * T13 T4<br />

Solution leav<strong>in</strong>g HRHX * T14 T5<br />

Cool<strong>in</strong>g-water after absorber * T15 T42<br />

Cool<strong>in</strong>g-water after condenser * T16 T43<br />

Solution leav<strong>in</strong>g LTRG * T17 T6<br />

Refrigerant after condenser * T18 T11<br />

Solution enter<strong>in</strong>g HTRG * T19 T20<br />

Chilled-water return T20 T31<br />

Chilled-water supply T21 T32<br />

Steam <strong>in</strong>put T22 T51<br />

Condensate return * T23 T54<br />

Cool<strong>in</strong>g-water supply T32 T41<br />

Solution leav<strong>in</strong>g HTRG * T33 T21<br />

Sensor Model Unit Sensor Model<br />

Absolute<br />

Deviation<br />

Relative<br />

Deviation Weight Sensor Model<br />

Absolute<br />

Deviation<br />

Relative<br />

Deviation Weight<br />

o C 157.5 157.5 0.0 0.0% 10% 133.7 133.7 0.0 0.0% 10%<br />

o C 36.6 36.1 0.5 1.5% 8% 33.8 33.4 0.4 1.1% 8%<br />

o C 75.1 75.1 0.0 0.0% 10% 66.1 66.1 0.0 0.0% 10%<br />

o C 90.5 90.5 0.0 0.0% 10% 81.3 81.4 -0.1 -0.1% 10%<br />

o C 37.7 36.1 1.6 4.3% 6% 33.8 33.8 0.0 0.0% 6%<br />

o C 40.0 38.2 1.8 4.6% 6% 34.9 34.9 0.0 0.1% 6%<br />

o C 93.3 92.7 0.6 0.6% 10% 79.6 79.6 0.0 0.1% 10%<br />

o C 44.1 44.1 0.0 0.0% 20% 37.2 37.2 0.0 0.0% 20%<br />

o C 129.3 128.8 0.5 0.4% 10% 113.8 113.5 0.3 0.3% 10%<br />

o C 13.9 13.9 0.0 -0.1% 0% 10.5 10.6 0.0 -0.1% 0%<br />

o C 6.4 6.4 0.0 0.8% 0% 7.1 7.1 0.0 0.5% 0%<br />

o C 164.3 164.0 0.3 0.2% 0% 140.2 140.0 0.2 0.2% 0%<br />

o C 99.3 100.0 -0.7 -0.7% 2% 69.0 70.2 -1.2 -1.7% 2%<br />

o C 30.7 31.5 -0.8 -2.5% 0% 30.4 31.5 -1.1 -3.6% 0%<br />

o C 153.5 155.8 -2.3 -1.5% 8% 131.7 132.8 -1.1 -0.9% 8%<br />

Chilled-water supply F1 m31 kg/s 0.56 0.55 0.0 2.14% 0% 0.56 0.55 0.0 2.06% 0%<br />

Steam supply F2 m51 kg/s 0.00713 0.00730 -0.00017 -2.33% 0% 0.00334 0.00385 -0.00050 -15.06% 0%<br />

Cool<strong>in</strong>g-water supply F6 m41 kg/s 1.45 1.15 0.3 20.64% 0% 1.46 1.15 0.3 21.09% 0%<br />

Chilled water <strong>in</strong>let P2 P31 kPa 54.2 84.5<br />

Chilled water outlet P3 P32 kPa 133.3 164.1<br />

Steam <strong>in</strong>let P4 P51 kPa 709.8 683.1 26.7 3.8% 0% 370.4 361.2 9.2 2.5% 0%<br />

Condensate after chiller P5 P54 kPa 101.8 101.3 0.5 0.5% 0% 101.3 101.3 0.0 0.0% 0%<br />

Power for the chiller E1 kW 1.34 1.14<br />

Power for the boiler E2 kW 20.02 10.96<br />

Thermal COP 1.02 1.10 -0.08 -7.9% 0.86 0.91 -0.05 -5.9%<br />

Cool<strong>in</strong>g load 17.39 17.17 0.22 1.3% 8.07 7.89 0.18 2.2%<br />

Overall deviation (σ )<br />

5.0% 5.9%<br />

Weighted deviation (σ ')<br />

1.67% 0.48%<br />

* The 11 measurements <strong>in</strong>side chiller to check with model calculations<br />

71


where σ is an overall deviation; ∆X n is the deviation between the measured value of a chiller<br />

operat<strong>in</strong>g condition value X n'<br />

and the model calculated value X n :<br />

∆ X = X −<br />

n<br />

n<br />

X<br />

n<br />

'<br />

, (Equation 4 - 2)<br />

where the subscript “n” corresponds to each of the 11 test measurements listed <strong>in</strong> Table 4-1.<br />

A weighted error, σ ' , has also been considered; the weight of each measurement is assigned on the<br />

basis of its perceived accuracy:<br />

∑ ⎟ ⎟<br />

2<br />

n ⎛<br />

⎞<br />

⎜ ⎛ ∆X<br />

⎞ n<br />

σ '= ε<br />

⎜ ⎜<br />

⎟<br />

n *<br />

(Equation 4 - 3)<br />

1 ⎝ ⎝ X n ⎠ ⎠<br />

The summation of weights of all the measurement conditions has been set at 1.<br />

n<br />

∑ ε n = 1<br />

(Equation 4 - 4)<br />

1<br />

The weights of measured conditions are given on the basis of eng<strong>in</strong>eer<strong>in</strong>g judgment. Higher weights<br />

are assigned to more accurate measurements. All the sensors used <strong>in</strong> the test program have been<br />

calibrated as presented <strong>in</strong> chapter 2. The accuracy of the measurement of the sensors discussed <strong>in</strong> this<br />

chapter is affected by external factors such as location and <strong>in</strong>stallation of the sensor. The effects of<br />

these external factors can be m<strong>in</strong>imized when the weights are assigned. If, for <strong>in</strong>stance, a sensor shows<br />

a small discrepancy consistently for all operat<strong>in</strong>g conditions, we can conclude that this measurement is<br />

less affected by the external factors. This sensor is treated as an accurate sensor. By us<strong>in</strong>g the weights<br />

<strong>in</strong> the model, the overall deviation between the model solutions and the measurements is less affected<br />

by the uncerta<strong>in</strong>ties of the measurements.<br />

4.1.2 <strong>Absorption</strong> Cycle at Design Condition<br />

The model solution can best represent the absorption cycle at various loads. The model solutions of<br />

major state po<strong>in</strong>ts for a 100% design load condition are presented <strong>in</strong> Table 4-1; the solutions are<br />

mapped <strong>in</strong> the Dűhr<strong>in</strong>g chart <strong>in</strong> Figure 4-2 to form a complete absorption cycle.<br />

72


Figure 4-2: <strong>Absorption</strong> cycle at design load condition<br />

T32<br />

T31<br />

13.9<br />

20<br />

Steam, cool<strong>in</strong>g water, and chilled water<br />

Water-LiBr sorbent solution<br />

Refrigerant<br />

Model solution<br />

Measurement<br />

+ 5 C<br />

o<br />

T43<br />

38.2<br />

T42 40<br />

36.11<br />

T41<br />

31.5<br />

30<br />

T1 T91 T7 T4 T5 T6<br />

T20<br />

T21<br />

36.1<br />

T11<br />

44.11<br />

10<br />

6.35<br />

1<br />

5 m 1 7<br />

18 =0.007513 kg/s<br />

Pl, 0.7665 kPa<br />

T18 0<br />

91 22<br />

3.154 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180<br />

57.39 %<br />

45.75<br />

REFRIGERANT TEMPERATURE, C<br />

50<br />

T22<br />

46.22<br />

61.68 %<br />

48.1<br />

60<br />

70<br />

m 10 =0.003315 kg/s<br />

1<br />

6<br />

m =0.09622 kg/s<br />

m =0.04434 kg/s<br />

4<br />

o<br />

75.1<br />

80<br />

4<br />

99.97<br />

100<br />

95.26<br />

90<br />

0<br />

30%<br />

40%<br />

m =0.04765 kg/s<br />

T53<br />

109.6<br />

110<br />

T54<br />

5<br />

6<br />

90.65 92.7<br />

50%<br />

57.39 %<br />

60%<br />

120<br />

m =0.0042 kg/s<br />

24<br />

m =0.04857 kg/s<br />

70%<br />

m =0.0073 kg/s<br />

51<br />

62.81 %<br />

128.8<br />

o<br />

SOLUTION TEMPERATURE, C<br />

Equlibrium Chart for A queous Lithium Bromide Solutions<br />

21<br />

20<br />

21<br />

m =0.04437 kg/s<br />

T52<br />

157.5<br />

21<br />

156.2<br />

T51<br />

164<br />

200<br />

150<br />

100<br />

Ph, 85.34 kPa<br />

Pm, 9.155 kPa<br />

The chart visualizes the sorbent solution cycle, the refrigerant cycle, and the conditions of steam,<br />

condensate, cool<strong>in</strong>g water, chilled water, and sorbent solutions at the major state po<strong>in</strong>ts <strong>in</strong>dicated <strong>in</strong><br />

Figure 4-2. In the figure, the measurements of the 11 temperature sensors <strong>in</strong>side the chiller are also<br />

plotted. The discrepancies are displayed between the model solution and the measurements. The 11<br />

dotted circles are centered at model solutions with a radius of 5 o C. This is a convenient way to<br />

illustrate the discrepancies between the model solutions and the measurement values. The flow rates of<br />

the sorbent solution and the refrigerant are directly labeled <strong>in</strong> the Dűhr<strong>in</strong>g chart above each stream<br />

l<strong>in</strong>e.<br />

Among the 11 measurements, the sorbent solution leav<strong>in</strong>g the HTRG at state po<strong>in</strong>t 21 (T21) shows the<br />

highest deviation to be about 2.3 o C, where the model solution gives a higher value than the<br />

measurement. The cool<strong>in</strong>g-water temperatures after the absorber (T42) and the condenser (T43) show<br />

50<br />

40<br />

30<br />

20<br />

10<br />

5<br />

4<br />

3<br />

2<br />

73<br />

SATUATION PRESSURE (P), kPa


deviations of about 1.6 o C and 1.8 o C, respectively, where the actual measured values are even higher<br />

if surface temperature measurement are used here. Other sensors agree with the model solutions<br />

with<strong>in</strong> ± 1<br />

o C.<br />

Figure 4-2 shows an average concentration of 60% between the concentrated and dilute water-LiBr<br />

sorbent solutions. The concentration differences between the concentrated solutions and the dilute<br />

solutions are 5.4% and 4.3% for the HTRG and LTRG, respectively. These data check well with the<br />

design conditions Broad provided. The chiller was <strong>in</strong>itially charged with a total of 65 kg sorbent<br />

solution at 55%. The concentration of sorbent solution at the different state po<strong>in</strong>ts depends on the<br />

<strong>in</strong>ventories of water <strong>in</strong> the water tray of the evaporator, the dra<strong>in</strong> pan of the condenser, and the pipes.<br />

We have estimated that, at design conditions, 5 kg of refrigerant water are held up <strong>in</strong> the reservoir of<br />

the evaporator, the condenser, and the pipes. The average concentration of the sorbent solution is then<br />

about 60%.<br />

At off-design conditions, less refrigerant circulates <strong>in</strong> the chiller. The average sorbent solution <strong>in</strong> the<br />

chiller may then be more dilute than at design conditions. The sorbent solution concentration changes<br />

correspond<strong>in</strong>g to the chiller load variations will be discussed <strong>in</strong> the next section.<br />

The dilute sorbent solution flow ratio to the HTRG and to the LTRG is another key variable that<br />

deserves closer consideration. At design condition, the model shows that the flow distribution ratio is<br />

roughly 0.5, which means that the flow is equally distributed to each regenerator. Broad has<br />

confirmed this result for the design condition. The model shows 17 kW cool<strong>in</strong>g load, the same as the<br />

measurements. The model, however, shows higher COP, about 1.10, than the measured value of 1.02.<br />

4.1.3 Overall Deviation<br />

<strong>An</strong> <strong>in</strong>itial standard and weighted error is calculated by the statistical analysis procedure and then<br />

model assumptions are adjusted one by one to reduce standard and weighted errors. New assumptions<br />

are then applied to the n<strong>in</strong>e test data sets. If consistent improvements are found for all n<strong>in</strong>e tests, the<br />

new assumption is adopted. This has proved effective <strong>in</strong> improv<strong>in</strong>g the model and <strong>in</strong> identify<strong>in</strong>g ways<br />

<strong>in</strong> which the chiller performance might be improved.<br />

Overall deviations are calculated on the basis of the statistical analysis procedure (subsection 4.1.1) to<br />

evaluate the model accuracy. Table 4-1 shows the results of the procedures for calculat<strong>in</strong>g the absolute<br />

and weighted deviations. The absolute deviations between the two columns are calculated <strong>in</strong> the third<br />

74


column. The relative deviation is calculated on the fourth column. The weights assigned to each of the<br />

11 measurement po<strong>in</strong>ts, the cool<strong>in</strong>g capacity, and the COP are listed <strong>in</strong> the bottom of the table.<br />

The 100% on the first row means the cool<strong>in</strong>g capacity full load is 17.17 kW; partial-load percentage is<br />

calculated by compar<strong>in</strong>g its cool<strong>in</strong>g capacity with this full-load capacity. The measurement data,<br />

model solutions, and the analysis for the 55% cool<strong>in</strong>g-load conditions are also listed <strong>in</strong> Table 4-2. At<br />

design condition, the overall deviations between the measurements and the model solutions are about<br />

5%, the weighted overall deviation is 1.67%. The major deviation is <strong>in</strong>troduced by the steam flow<br />

meter and the cool<strong>in</strong>g-water flow meter. By us<strong>in</strong>g the weights, the systematic deviations <strong>in</strong>troduced by<br />

the two flow meters are deemphasized.<br />

4.2 Model <strong>An</strong>alysis<br />

Once the deviations between the measurements and the model solution for the design condition are<br />

reduced satisfactorily, the model is used to analyze all the experimental data from the test program by<br />

the same analytical method. The test data for the cool<strong>in</strong>g-load variations are analyzed <strong>in</strong> the follow<strong>in</strong>g<br />

subsections.<br />

4.2.1 <strong>An</strong>alysis of Cool<strong>in</strong>g-Load Variation<br />

In the cool<strong>in</strong>g-load variation test, the chiller cool<strong>in</strong>g load was changed <strong>in</strong> the model by adjust<strong>in</strong>g the<br />

chilled-water return temperature with a fixed chilled-water supply temperature and flow rate. The<br />

cool<strong>in</strong>g loads were varied <strong>in</strong> 9 steps from 100% to 35%. The test data were obta<strong>in</strong>ed us<strong>in</strong>g the same<br />

method as described <strong>in</strong> chapter 2. As an example of off-design condition analysis, Table 4-1 also<br />

shows the measured values, the model solutions, and the analysis results for a 55% design load<br />

condition. Similarly, the absorption cycle of 55% design load condition is mapped <strong>in</strong> a Dűhr<strong>in</strong>g<br />

diagram <strong>in</strong> Figure 4-3.<br />

If we compare the 55% of design load with the 100% of design load condition <strong>in</strong> Figure 4-2, the<br />

pressures <strong>in</strong> the HTRG, LTRG, and the evaporator all decrease significantly. The concentration of<br />

dilute sorbent solution does not change appreciably, but the concentrated sorbent solutions from the<br />

two regenerators become more dilute. The flow rates of total sorbent solution and refrigerant are<br />

decreased. The dilute sorbent flow distribution ratio to the HTRG and the LTRG is about 0.6. At 55%<br />

design load condition, less refrigerant circulates <strong>in</strong> the chiller; the average concentration of the dilute<br />

sorbent solution <strong>in</strong> the chiller is estimated at 58%, which is lower than that of the design condition at<br />

60%. The model calculated COP for the 55% design load condition is 0.91, which is higher than the<br />

75


measured COP at 0.86. The overall deviation of the measurements and the model solutions is about<br />

5.9%, and the weighted overall deviation is about 0.48%.<br />

Figure 4-3: Dűhr<strong>in</strong>g chart at 55% design load condition<br />

REFRIGERANT TEMPERATURE, C<br />

60<br />

70<br />

o<br />

80<br />

90<br />

0<br />

30%<br />

40%<br />

50<br />

T11<br />

T43<br />

10<br />

T42 40<br />

Pm, 6.352 kPa<br />

T41<br />

30<br />

5<br />

4<br />

3<br />

20<br />

T31<br />

2<br />

T3210<br />

5<br />

0<br />

10 20 30 40 50 60 70 80 90 100 110 120 130 140 150<br />

1<br />

Pl, 0.6871 kPa<br />

160 170 180<br />

m =0.04701 kg/s<br />

18<br />

Steam, cool<strong>in</strong>g water, and chilled water<br />

Water-LiBr sorbent solution<br />

Refrigerant<br />

Model solution<br />

Measurement<br />

T1 T22<br />

T91 T7<br />

4<br />

56.89 % m =0.03305 kg/s<br />

T54<br />

m =0.01436 kg/s<br />

10<br />

6<br />

59.47 % m =0.03162 kg/s<br />

T4<br />

100<br />

50%<br />

110<br />

56.89 % m =0.04958 kg/s<br />

60%<br />

T6 T5 T20<br />

20<br />

120<br />

m =0.02012 kg/s<br />

59.29 % m =0.04756 kg/s<br />

70%<br />

T21<br />

o<br />

SOLUTION TEMPERATURE, C<br />

Equlibrium Chart for A queous Lithium Bromide Solutions<br />

23<br />

21<br />

m =0.03848 kg/s<br />

51<br />

T52 T51<br />

Ph, 54.4 kPa<br />

Other test data for the cool<strong>in</strong>g-load conditions are analyzed us<strong>in</strong>g the same method. Figure 4-4 shows<br />

the model output of the 9 steady-state tests at various load conditions. The trends of the major state<br />

po<strong>in</strong>ts illustrate the variation of composition, temperature, and equilibrium pressure with the change of<br />

the operat<strong>in</strong>g load conditions. The Dűhr<strong>in</strong>g plot illustrates the conditions of the chiller under various<br />

loads <strong>in</strong> one diagram, but it does not <strong>in</strong>dicate the flow rate of each stream, the quantity of heat<br />

transferred, or the heat transfer coefficients <strong>in</strong> each component. Other plots are needed to supplement<br />

the Dűhr<strong>in</strong>g chart.<br />

200<br />

150<br />

100<br />

50<br />

40<br />

30<br />

20<br />

76<br />

SATUATION PRESSURE (P), kPa


Figure 4-4: <strong>Absorption</strong> cycle variations with load changes<br />

20<br />

Steam, cool<strong>in</strong>g water, and chilled water<br />

Water-LiBr sorbent solution<br />

Model solution for 100%, 83%,<br />

67%, and 34% of design load<br />

Chilled/cool<strong>in</strong>g water<br />

supply temperature set po<strong>in</strong>t<br />

Po<strong>in</strong>t 4340<br />

Po<strong>in</strong>t 41<br />

30<br />

REFRIGERANT TEMPERATURE, C<br />

50<br />

60<br />

70<br />

o<br />

80<br />

100<br />

Po<strong>in</strong>t 54<br />

90<br />

0<br />

30%<br />

40%<br />

Po<strong>in</strong>t 31<br />

10<br />

Po<strong>in</strong>t 32<br />

5<br />

0<br />

10 20<br />

Po<strong>in</strong>t 1<br />

30 40<br />

Po<strong>in</strong>t 7<br />

Po<strong>in</strong>t 22<br />

Po<strong>in</strong>t 5091 60 70 80 90 100 110 120 130 140 150 160 170<br />

1<br />

180<br />

4.2.2 Performance Curve<br />

Po<strong>in</strong>t 4<br />

Po<strong>in</strong>t 5<br />

50%<br />

Po<strong>in</strong>t 6<br />

110<br />

60%<br />

120<br />

Po<strong>in</strong>t 20<br />

70%<br />

o<br />

SOLUTION TEMPERATURE, C<br />

Equlibrium Chart for A queous Lithium Bromide Solutions<br />

Po<strong>in</strong>t 51<br />

Po<strong>in</strong>t 21<br />

Figure 4-5 shows that the chiller COP calculated by the model is, on average, higher than the<br />

measurement by 8%. The reason for the discrepancy is the calculation of the heat <strong>in</strong>put. The model<br />

and the measurement share the same steam <strong>in</strong>let pressure/temperature and the flow, but <strong>in</strong> the<br />

measurement the condensate from the chiller is assumed to be saturated water at atmospheric pressure.<br />

The model solution, however, shows that the condensate is partially vaporized when it leaves the<br />

chiller above an 82% design load. In the model, the heat <strong>in</strong>put is def<strong>in</strong>ed by the summation of the heat<br />

transferred to the HTRG and the HRHX. The model, therefore, predicts lower quantity of heat<br />

transferred to the chiller than the measurements. Below 82% load conditions, the model predicts<br />

higher condensate return temperature than the measurements. Theoretically, the performance curve<br />

calculated by the model is a better representation of the chiller performance.<br />

200<br />

150<br />

100<br />

50<br />

40<br />

30<br />

20<br />

10<br />

5<br />

4<br />

3<br />

2<br />

77<br />

SATUATION PRESSURE (P), kPa


Figure 4-5: <strong>Chiller</strong> performance curve under various load conditions<br />

Coefficient of Performance (COP) .<br />

1.30<br />

1.20<br />

1.10<br />

1.00<br />

0.90<br />

0.80<br />

0.70<br />

0.60<br />

0.50<br />

0.40<br />

Thermal COP<br />

(model)<br />

Overall COP<br />

(measurement)<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Thermal COP (measurement) Overall COP (measurement)<br />

Thermal COP (model)<br />

Thermal COP<br />

(measurement)<br />

Figure 4-6: Heat transfer load on each component under various load conditions<br />

Heat transfer on chiller component (kW) .<br />

32<br />

28<br />

24<br />

20<br />

16<br />

12<br />

8<br />

4<br />

Actual cool<strong>in</strong>g load (kW)<br />

0<br />

HRHX<br />

BPHX<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Cool<strong>in</strong>g tower Absorber Evaporator HTRG<br />

LTRG Condenser HTHX LTHX<br />

HRHX BPHX<br />

Cool<strong>in</strong>g tower<br />

Absorber<br />

Evaporator<br />

HTRG<br />

LTRG<br />

HTHX<br />

Condenser<br />

LTHX<br />

Actual cool<strong>in</strong>g load (kW)<br />

The quantity of heat transferred <strong>in</strong> each component <strong>in</strong> the chiller is illustrated <strong>in</strong> Figure 4-6. The load<br />

<strong>in</strong> the 5 major heat transfer components is l<strong>in</strong>early related to the cool<strong>in</strong>g load. The heat transferred on<br />

the 4 m<strong>in</strong>or heat recovery exchangers, the HTHX, LTHX, HRHX, and BPHX, are relatively constant.<br />

The heat transfer <strong>in</strong> the BPHX is negligible.<br />

78


4.2.3 Flow Rate Variations<br />

The steam flow rate is an <strong>in</strong>put parameter to the chiller model; the flow rate has been calculated on the<br />

basis of the power <strong>in</strong>put measurement to the steam boiler. In the chiller operation, the outlier data are<br />

ma<strong>in</strong>ly <strong>in</strong>troduced by the steam flow meter. The read<strong>in</strong>gs of the steam flow meter may be zero or very<br />

low when the feedwater pump operates to supply feedwater to the boiler; these low read<strong>in</strong>gs reduce<br />

the average steam flow measurement below the actual value. In this case, the measured steam flow<br />

meter is not very reliable, so the actual steam flow is calculated us<strong>in</strong>g the power measurements to the<br />

steam boiler. The calculated steam flow agrees well with the condensate return measured after the<br />

chiller. The comparison of the calculated steam flow and the measurement read<strong>in</strong>gs under various<br />

operation conditions are presented <strong>in</strong> Figure 4-7. The manufacturer has calibrated the steam flow<br />

orifice meter at design conditions with 700 kPa saturated steam.<br />

Figure 4-7: Steam supply flow rate under various load conditions<br />

Steam flow rate (kg/s)<br />

0.008<br />

0.007<br />

0.006<br />

0.005<br />

0.004<br />

0.003<br />

0.002<br />

0.001<br />

0<br />

Steam flow calculated<br />

from power<br />

Measured steam flow<br />

Measured steam flow<br />

(corrected by the desnsity)<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Steam flow calculated from power measurement<br />

Measured steam flow<br />

Measured steam flow (corrected)<br />

Actual cool<strong>in</strong>g load (kW)<br />

Figure 4-8 shows the flow rates of the dilute sorbent solution from the absorber to the HTRG and<br />

LTRG at various load conditions. The dilute solution flow <strong>in</strong> the HTRG rema<strong>in</strong>s relatively constant.<br />

The sorbent solution flow rates to the LTRG decrease with the drop of cool<strong>in</strong>g loads. This result is<br />

consistent with the chiller control pr<strong>in</strong>ciple that the variable frequency solution pump ma<strong>in</strong>ta<strong>in</strong>s the<br />

sorbent solution level <strong>in</strong> the HTRG. Figure 4-9 shows the sorbent solution split ratio that is def<strong>in</strong>ed by<br />

the dilute sorbent solution flow to the HTRG over the total solution flow from the absorber. The<br />

chiller does not control sorbent solution distribution ratio, the ratio is preset roughly at 0.5 at design<br />

79


load condition by predeterm<strong>in</strong><strong>in</strong>g the pipe diameters of each sorbent stream. In this case, when the<br />

cool<strong>in</strong>g load decreases, the pressure drops <strong>in</strong> the HTRG faster than <strong>in</strong> the LTRG, so more sorbent<br />

solution flows <strong>in</strong>to the HTRG than the LTRG, and the sorbent solution split ratio <strong>in</strong>creases the value<br />

above 0.5.<br />

Figure 4-8: Sorbent solution flow rate under various load conditions<br />

Sorbent solution flow, kg/s .<br />

0.12<br />

0.1<br />

0.08<br />

0.06<br />

0.04<br />

0.02<br />

0<br />

Sorbent solution<br />

to the LTRG<br />

Sorbent solution<br />

from the absorber<br />

Sorbent solution<br />

to the HTRG<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Sorbent solution from absorber<br />

Sorbent solution to HTRG<br />

Sorbent solution to LTRG<br />

Actual cool<strong>in</strong>g load (kW)<br />

Figure 4-9: Sorbent solution split ratio under various load conditions<br />

Dilute sorbent solution distribution ratio, R .<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

Split ratio, R<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Sorbent solution distribution ratio<br />

Actual cool<strong>in</strong>g load (kW)<br />

80


Figure 4-10 shows that the refrigerant flow vaporized <strong>in</strong> the evaporator is proportional to the cool<strong>in</strong>gload<br />

condition. The HTRG consistently generates more refrigerant than the LTRG. This result agrees<br />

well with the chiller control pr<strong>in</strong>ciple <strong>in</strong> which, under lower load conditions, the refrigerant level <strong>in</strong> the<br />

water tray of the evaporator drops, and the refrigerant pump is on/off less frequently than at the higher<br />

load conditions.<br />

Figure 4-10: Refrigerant regeneration rate under various load conditions<br />

Refrigerant flow (kg/s)<br />

0.01<br />

0.008<br />

0.006<br />

0.004<br />

0.002<br />

0<br />

Refrigerant vaporized<br />

<strong>in</strong> the evaporator<br />

Refrigerant produced<br />

from the HTRG<br />

Refrigerant produced<br />

from the LTRG<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Referigerant from LTRG<br />

Refrigerant vaporizaed <strong>in</strong> evaporator<br />

Refrigerant from HTRG<br />

Actual cool<strong>in</strong>g load (kW)<br />

4.2.4 Temperature Variations<br />

In Figure 4-11, the refrigerant vaporization temperature <strong>in</strong> the evaporator is plotted aga<strong>in</strong> to illustrate<br />

state po<strong>in</strong>t 18 more clearly. The refrigerant vaporization temperature is <strong>in</strong> equilibrium with the vapor<br />

pressure <strong>in</strong> the absorber. The refrigerant has a higher vaporization temperature, around 3.2 o C at<br />

design conditions; this temperature drops to 0.5 o C at 34% design load conditions. The result agrees<br />

with the chiller control pr<strong>in</strong>ciple that when the cool<strong>in</strong>g load drops too low, ice may form <strong>in</strong> the<br />

evaporator. Ice formation affects chiller operation by block<strong>in</strong>g the spray nozzles; the problem may be<br />

solved automatically when the chiller stops for a short while. To avoid the hazard of ice formation <strong>in</strong><br />

the recirculation pump, an electrical heater <strong>in</strong>stalled <strong>in</strong> the evaporator is turned on to protect the<br />

refrigerant pump from freez<strong>in</strong>g.<br />

81


Figure 4-11: Refrigerant vaporization temperature under various load conditions<br />

Vaporization temperature, T18, ( o C ) .<br />

4<br />

3.5<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

T18<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Vaporization temperature <strong>in</strong> the evaporator<br />

Actual cool<strong>in</strong>g load (kW)<br />

Figure 4-12: Sorbent solution composition changes under various load conditions<br />

Sorbent solution concentration (%) .<br />

64<br />

62<br />

60<br />

58<br />

56<br />

54<br />

4.2.5 Composition Variations<br />

Sorbent from HTRG<br />

Sorbent from Absorber<br />

Sorbent from LTRG<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Sorbent form absorber<br />

Sorbent from HTRG<br />

Sorbent from LTRG<br />

Actual cool<strong>in</strong>g load (kW)<br />

Figure 4-12 illustrates the composition changes of the sorbent solutions with the variations of the load<br />

conditions. The sorbent solution leav<strong>in</strong>g the HTRG shows higher concentration than that of the LTRG<br />

at design load conditions. With the load decrease, the concentration of sorbent leav<strong>in</strong>g the LTRG<br />

becomes higher than that of the HTRG. This result is <strong>in</strong>troduced by sorbent solution split ratio changes<br />

from design load to partial load condition. The concentrations of the dilute solution do not change<br />

82


appreciably. The average concentration of the sorbent solution approaches 57% from the design load<br />

condition to lower load condition. This result checks well with the design parameter from Broad<br />

<strong>in</strong>dicat<strong>in</strong>g when the chiller is off, the concentration of the dilute solution is 57%.<br />

The composition differences between the dilute sorbent solution and the concentrated solutions<br />

variations reflect the chiller performance. The wider the discrepancies between the dilute and<br />

concentrated sorbent solution are, the higher the COP values will be.<br />

4.2.6 Vapor Quality Variations<br />

The vapor qualities of the chiller <strong>in</strong>ternal conditions at different state po<strong>in</strong>ts are assumed <strong>in</strong> the model.<br />

The refrigerant vapor from the HTRG at state po<strong>in</strong>t 23 was <strong>in</strong>itially assumed to be completely<br />

condensed <strong>in</strong> the LTRG, so only saturated water enters the condenser at state po<strong>in</strong>t 24, q 0 . This<br />

assumption results <strong>in</strong> generat<strong>in</strong>g high COP values because the LTRG recovers most of the latent heat<br />

by the condensation process. This assumption, however, produces higher overall and weighted<br />

deviations for all 9 data sets. The values of vapor quality q24 have been adjusted as shown <strong>in</strong> Figure 4-<br />

13. The overall and weighted deviations are reduced dramatically by us<strong>in</strong>g these new q24 values. The<br />

chiller performance can be improved by an appropriate measure reduc<strong>in</strong>g the vapor carryover.<br />

Figure 4-13: Refrigerant vapor quality leav<strong>in</strong>g the LTRG under various load conditions<br />

Vapor quality (q 24) .<br />

0.4<br />

0.35<br />

0.3<br />

0.25<br />

0.2<br />

0.15<br />

0.1<br />

0.05<br />

0<br />

Vapor quality of<br />

refrigerant enter<strong>in</strong>g<br />

Condenser<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Vapor quality of refrigerant enter<strong>in</strong>g condenser<br />

Actual cool<strong>in</strong>g load (kW)<br />

24 =<br />

83


4.2.7 Heat Transfer Area Variations<br />

The UA values of the 5 major heat transfer components are plotted <strong>in</strong> Figure 4-14. The overall heat<br />

transfer coefficients (Us) of the 5 major heat transfer components are functions of the mass flow rates,<br />

<strong>in</strong>let and outlet temperature of streams on both sides of the tubes; the effects of the stream flow rates<br />

and temperature are presented <strong>in</strong> appendix 4A. The model <strong>in</strong>itially assumes that the contact area (As)<br />

of each heat transfer component rema<strong>in</strong>s constant. The model analysis, however, shows that the<br />

decrease <strong>in</strong> surface contact areas for the heat transfer components <strong>in</strong> the evaporator, and the LTRG<br />

under partial load conditions may contribute to the decrease of UA values. The variations of contact<br />

areas <strong>in</strong> the evaporator and the LTRG are due to the significant flow rate changes. Figure 4-15 shows<br />

the estimations of the area changes <strong>in</strong> the evaporator and the LTRG on the basis of the overall<br />

deviations between the measured values and the model solutions.<br />

Figure 4-14: UA changed for the 5 major components under various load conditions<br />

UA, kW/ o C<br />

4<br />

3.5<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

UA for Condenser<br />

UA for Evaporator<br />

UA for Absorber<br />

UA for LTRG<br />

UA for HTRG<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Absorber Evaporator HTRG LTRG Condenser Actual cool<strong>in</strong>g load (kW)<br />

The surface area for the evaporator is <strong>in</strong>dicated <strong>in</strong> Figure 4-15, The surface contact areas decrease at<br />

partial load conditions by 30-50%. The reason for this change is the significant refrigerant flow<br />

decrease. For <strong>in</strong>stance, Figure 4-10 <strong>in</strong>dicates that this drops from 0.0075 kg/s at design load condition<br />

to 0.0016 kg/s at 34% of design load condition.<br />

The surface variations also exist <strong>in</strong> the LTRG because of the flow decrease from the design load<br />

condition to the partial load condition. Figure 4-8 <strong>in</strong>dicates that the sorbent solution distributed to the<br />

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LTRG drops from 0.048 kg/s at design load condition to 0.022 kg/s at 34% of design load condition.<br />

The chiller controls the solution levels <strong>in</strong> the HTRG but not <strong>in</strong> the LTRG. The total contact area of the<br />

LTRG is estimated to decrease by 20-30% from the design load to 34% of design load conditions. This<br />

means that under the lower load conditions, some of the tubes <strong>in</strong> the LTRG may be exposed to the<br />

refrigerant vapor.<br />

The surface contact areas of the HTRG, condenser, and absorber are not significantly affected by the<br />

load variations. First, the control system ma<strong>in</strong>ta<strong>in</strong>s the solution level <strong>in</strong> the HTRG. Figure 4-8<br />

<strong>in</strong>dicates that the solution sorbent solution flow rate is relatively constant for all load conditions;<br />

second, the absorber contact area does not vary much from the design load condition to the partial load<br />

condition because, as Figure 4-8 <strong>in</strong>dicates, the dilute sorbent solution circulation rate does not change<br />

significantly for all load conditions; third, the condenser contact area does not change much because<br />

the tubes are consistently exposed <strong>in</strong> the refrigerant vapor.<br />

Figure 4-15: Surface contact area changes under various load conditions<br />

Surface area, m 2<br />

1.6<br />

1.4<br />

1.2<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

4.2.8 Deviation Variations<br />

0<br />

Contact area of<br />

LTRG<br />

Contact area of<br />

Evaporator<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Evaporator surface area LTRG surface area<br />

Sorbent solution flow (kg/s)<br />

The overall deviations and the weighted deviations of the measurements and the model solutions are<br />

plotted <strong>in</strong> Figure 4-16. The overall deviations are below 6% when the cool<strong>in</strong>g loads are below 60% of<br />

the design condition. When the load drops below 60%, the overall deviations <strong>in</strong>crease fast to 13% at<br />

34% of design load condition. The dramatic <strong>in</strong>crease of overall deviation is due to the <strong>in</strong>accuracy of<br />

85


steam flow measurements and the relative <strong>in</strong>creas<strong>in</strong>g discrepancy of condensate return temperature<br />

between the measured values and the model solutions.<br />

Figure 4-16: Overall and weighted deviations under various load conditions<br />

Overall and weighted deviations .<br />

16%<br />

14%<br />

12%<br />

10%<br />

8%<br />

6%<br />

4%<br />

2%<br />

0%<br />

Weighted deviation<br />

Overall deviation<br />

0 2 4 6 8 10 12 14 16 18 20<br />

Overall deviationr Weighted deviation<br />

Actual cool<strong>in</strong>g load (kW)<br />

4.2.9 <strong>An</strong>alysis of Other Test Data<br />

Only the results of the cool<strong>in</strong>g-load variation tests are presented <strong>in</strong> this chapter. The analyses of other<br />

test data are implemented <strong>in</strong> the follow<strong>in</strong>g order:<br />

• chilled-water supply temperature variation<br />

• chilled-water flow rate variation<br />

• cool<strong>in</strong>g-water supply temperature<br />

• cool<strong>in</strong>g-water supply flow rate<br />

• steam supply temperature<br />

The results of the analysis are presented <strong>in</strong> the appendix 4A.<br />

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5 Contributions and Areas of Future Research<br />

5.1 Contributions<br />

This thesis develops methods for the effective design and evaluation of an absorption chiller for<br />

micro-<strong>BCHP</strong> systems that reduce energy consumption, decrease operational costs, and improve<br />

environmental benefits <strong>in</strong> residential and light commercial build<strong>in</strong>gs.<br />

1) Establishment of a unique experimental environment for the equipment tests under various<br />

conditions.<br />

A 16 kW steam-driven, two-stage absorption chiller was <strong>in</strong>stalled together with an auxiliary steam<br />

supply and a variable load for the chiller test and performance evaluation. We developed a web-based<br />

data acquisition and control system to operate the chiller and its auxiliary equipment while stor<strong>in</strong>g and<br />

display<strong>in</strong>g the test measurement data. We tested the chiller at various operat<strong>in</strong>g conditions <strong>in</strong><br />

accordance with a test program. On the basis of the test program, the effects of chilled water, cool<strong>in</strong>g<br />

water, and steam <strong>in</strong>put operat<strong>in</strong>g conditions on the chiller performance were exam<strong>in</strong>ed systematically.<br />

The chiller performance was calculated and presented on the basis of the measurement data gathered<br />

<strong>in</strong> the test program. The calculated chiller performance data under various load conditions checked and<br />

supplemented the performance data from manufacturer publications. In the future, the chiller and its<br />

control system will be <strong>in</strong>corporated <strong>in</strong> the cool<strong>in</strong>g system of the IW and connected with other <strong>BCHP</strong><br />

components and the campus chilled-water supply system.<br />

2) Construction of a comprehensive chiller model for the analysis of extensive, detailed test data<br />

obta<strong>in</strong>ed from the absorption chiller<br />

A comprehensive computational model was developed to further ref<strong>in</strong>e the understand<strong>in</strong>g of the<br />

pr<strong>in</strong>ciples of the chiller, to analyze the experimental data from the test program, to assist <strong>in</strong> equipment<br />

design, and to evaluate the performance of various <strong>BCHP</strong> systems. This model is a set of equations<br />

consist<strong>in</strong>g of: mass balances, energy balances, relations describ<strong>in</strong>g heat and mass transfer, and<br />

equations for the thermophysical properties of the work<strong>in</strong>g fluids. The model can be solved when<br />

appropriate assumptions and a certa<strong>in</strong> number of operat<strong>in</strong>g parameters are assigned, so that the<br />

conditions – pressure, temperature, composition, and flow – at each po<strong>in</strong>t with<strong>in</strong> the chiller can be<br />

calculated. Heat and mass transfer correlations have been <strong>in</strong>tegrated <strong>in</strong>to the model so that it can<br />

evaluate the chiller performance not only at design conditions, but also at various off-design<br />

conditions.<br />

87


3) <strong>An</strong>alysis of the measured data, ref<strong>in</strong>ement of the model, and improvement of the chiller design on<br />

the basis of the data analysis process<br />

The comprehensive model has been used to assess the accuracy of the experimental data from the test<br />

program. The discrepancies between the measurements and the model calculations were reduced by<br />

adjust<strong>in</strong>g the model assumptions. The discrepancies between the measurements and the model<br />

solutions are <strong>in</strong>troduced ma<strong>in</strong>ly by the follow<strong>in</strong>g factors:<br />

• <strong>in</strong>accurate stream flow temperature measurements from sensors mounted on the external pipe<br />

surface<br />

• fluctuat<strong>in</strong>g measurements of steam flow due to periodic feedwater addition to the boiler<br />

• imprecise cool<strong>in</strong>g-water flow measurements because of space limitations <strong>in</strong> mount<strong>in</strong>g the flow<br />

sensor<br />

• <strong>in</strong>accurate assumptions regard<strong>in</strong>g the quality of the refrigerant flow from various chiller<br />

components<br />

• <strong>in</strong>accurate values of heat transfer coefficients calculated from available correlations<br />

The absorption cycle for each test has been plotted on a Dűhr<strong>in</strong>g diagram based on the model<br />

calculations. The trends of temperature, pressure, and composition of critical state po<strong>in</strong>ts for each<br />

group of operat<strong>in</strong>g parameter tests have been summarized on the Dűhr<strong>in</strong>g diagram and other plots. We<br />

have devised a strategy to improve the chiller performance (particularly at partial load conditions) on<br />

the basis of model analysis results and have validated the model for the calculation of chiller<br />

performance under various operat<strong>in</strong>g conditions.<br />

These research efforts have provided a solid basis for future studies on microscale absorption chiller<br />

design, application, and simulation. Current work can be extended <strong>in</strong>to the follow<strong>in</strong>g research areas <strong>in</strong><br />

the future:<br />

• Extension of the validated model to various heat sources and s<strong>in</strong>ks and thermal capacities <strong>in</strong><br />

microscale <strong>BCHP</strong> system design evaluations<br />

o The model can be extended to heat sources <strong>in</strong>clud<strong>in</strong>g natural gas, hot water, and exhaust gases<br />

from eng<strong>in</strong>es and gas turb<strong>in</strong>es<br />

88


o The model can also be adapted to air cool<strong>in</strong>g, but this adaptation may reduce the capital and<br />

ma<strong>in</strong>tenance costs, although the rated COP may drop when compared with the water-cooled<br />

system.<br />

• Integration of the chiller performance and cost models <strong>in</strong>to overall simulations of microscale<br />

<strong>BCHP</strong> systems to optimize overall system performance and operat<strong>in</strong>g strategies<br />

o A cost model <strong>in</strong>clud<strong>in</strong>g capital cost, operational cost, and ma<strong>in</strong>tenance cost can be <strong>in</strong>tegrated<br />

with build<strong>in</strong>g load simulation tools to evaluate absorption chiller economic performance under<br />

various types of build<strong>in</strong>gs and weather conditions.<br />

o A guidel<strong>in</strong>e for apply<strong>in</strong>g the microscale absorption chiller <strong>in</strong> build<strong>in</strong>gs can be proposed on the<br />

basis of the simulation results of the economical evaluation model.<br />

o As a simulation tool, the model should provide a graphic user <strong>in</strong>terface (GUI) and standard<br />

output sheets that can assist the system designers <strong>in</strong> implant<strong>in</strong>g <strong>BCHP</strong> system design and<br />

evaluation.<br />

The field of computational support for build<strong>in</strong>g an energy system is extensive, and this thesis has<br />

illustrated significant concepts <strong>in</strong> design<strong>in</strong>g, analyz<strong>in</strong>g, and model<strong>in</strong>g of microscale absorption chiller<br />

systems and of analyz<strong>in</strong>g extensive test data sets with the support of a detailed model. Some of the<br />

future areas of study have been <strong>in</strong>vestigated prelim<strong>in</strong>arily <strong>in</strong> this thesis along with the chiller<br />

equipment tests and the experimental data analysis processes. The methods and some of the results are<br />

summarized <strong>in</strong> the follow<strong>in</strong>g sections.<br />

5.2 Areas of Future Research<br />

5.2.1 Extended <strong>Chiller</strong> Model for Multi-Heat Resources<br />

Many types of fuel and thermal heat sources can be used to drive a double-effect absorption chiller,<br />

such as steam, hot water, exhaust gas, natural gas, oil, and LPG. Among them the most widely used<br />

heat<strong>in</strong>g media are natural gas, steam, and hot water. From the manufacturer’s perspective, the chiller<br />

can be adapted to any heat source with m<strong>in</strong>or changes on the HTRG and <strong>in</strong>ternal control system.<br />

From a research perspective, the validated chiller model, based on a modularized structure, allows for<br />

the flexible extension of one specific chiller to other types of chillers with similar flow configurations<br />

but different heat<strong>in</strong>g media. The extended absorption chiller models us<strong>in</strong>g various heat sources can<br />

meet the total cool<strong>in</strong>g demand of build<strong>in</strong>gs and can better <strong>in</strong>tegrate with other <strong>BCHP</strong> components,<br />

such as solar collectors and various power generators.<br />

89


Compared with the steam-driven chiller model, the major difference <strong>in</strong> the new types of chiller is <strong>in</strong><br />

the calculation of heat transfer coefficients for the HTRG. In the steam-driven chiller, the condensate<br />

after the HTRG is recovered by the HRHX. In the other types of chiller, however, this HRHX does not<br />

exist. The heat transfer features of the HTRG for the four types of chiller are listed <strong>in</strong> Table 5-1. The<br />

common feature of the four HTRGs is the boil<strong>in</strong>g process of LiBr solution. The detailed<br />

configurations of the HTRGs are summarized <strong>in</strong> Tables 3-2 and 3A-1. The heat transfer coefficient<br />

equations applied for the HTRGs are listed <strong>in</strong> Table 3-3.<br />

Table 5-1: Heat transfer features of the HTRG of different heat<strong>in</strong>g media<br />

Outside tube (combustion chamber)<br />

Heat<strong>in</strong>g medium Reference Process Medium<br />

All types Jakob and Hawk<strong>in</strong>s Boil<strong>in</strong>g Water-LiBr sorbent solution<br />

Inside tube (combustion chamber)<br />

Steam Kern D. Q. Condensation Steam, condensate<br />

Hot water Dittus and Boelter Convection Water<br />

Exhaust gas J. P. Holman Convection Combustion gases<br />

Natural gas Hottel, et al. Radiation, convection Combustion gases<br />

5.2.1.1 Hot Water <strong>Absorption</strong> <strong>Chiller</strong><br />

The HTRG us<strong>in</strong>g hot water comprises a spiral circular tube bundle with 3 parallel tubes spiral<strong>in</strong>g 8<br />

rounds down to the bottom; hot water is split <strong>in</strong>to three streams at the <strong>in</strong>let located at the top and<br />

comb<strong>in</strong>ed <strong>in</strong>to one stream on the bottom of the HTRG. The hot water flow is regulated by a motorized<br />

hot water valve. The hot water supply temperature is 160 o C, and the temperature difference between<br />

the hot water <strong>in</strong>let and the outlet is 10-20 o C. When the hot water leaves the HTRG, it can be reheated<br />

by external heat sources such as solar collectors or other heat recovery systems.<br />

5.2.1.2 Natural Gas <strong>Absorption</strong> <strong>Chiller</strong><br />

In a natural-gas-driven absorption chiller, the HTRG <strong>in</strong> Figure 5-1 comprises a combustion chamber<br />

(burner) cooled by a radiation convection section and an exhaust gas. The combustion gases exit at the<br />

far end of the combustion chamber at a temperature significantly lower than the adiabatic temperature.<br />

The combustion gases are cooled further <strong>in</strong> the exhaust gas convector, so that the exhaust gas<br />

temperature approaches the sorbent solution temperature <strong>in</strong> the HTRG with<strong>in</strong> 30 o C. The natural gas<br />

flow to the burner is regulated by a flow switch. The control logic of natural gas flow is similar to that<br />

of steam, but the natural gas burner has only two stages, high flame and low flame.<br />

90


Figure 5-1: Simplified HTRG configurations for natural-gas-driven absorption chiller<br />

Combustion<br />

Chamber<br />

Fuel ejector<br />

200<br />

400<br />

200 200<br />

Exhaust gas<br />

25 Exit<br />

5.2.1.3 Exhaust Gas <strong>Absorption</strong> <strong>Chiller</strong><br />

Exhaust gas<br />

Convector<br />

Us<strong>in</strong>g exhaust gas directly from a power generator, such as an eng<strong>in</strong>e, gas turb<strong>in</strong>e, or solid oxide fuel<br />

cell, is one of the latest practices <strong>in</strong> the application of absorption chillers. The structure of the HTRG<br />

for an exhaust-gas-driven absorption chiller is similar to that of the gas convector <strong>in</strong> the natural-gasdriven<br />

chiller. It is comprises a staggered tube bundle with 22 circular grooved copper tubes; the<br />

exhaust gas is split <strong>in</strong>to 22 streams at the <strong>in</strong>let located at one side and comb<strong>in</strong>ed <strong>in</strong>to one stream on the<br />

other side of the HTRG. High-temperature exhaust gas can be supplied at 520 o C from an eng<strong>in</strong>e or a<br />

reciprocated gas turb<strong>in</strong>e, 755 o C directly from a solid oxide fuel cell. When the exhaust gas leaves the<br />

tube bundles, its temperature is usually higher than the solution temperature by 30 to 50 o C.<br />

5.2.2 System Integration and <strong>Application</strong><br />

Many cogeneration concepts are conceivable with absorption chiller systems, but the selection of one<br />

over another requires detailed study of long-term technical and economic performance. On the basis of<br />

the chiller models developed <strong>in</strong> this thesis, the design and analysis of an <strong>in</strong>dividual absorption chiller<br />

can be expanded to overall <strong>BCHP</strong> systems. <strong>An</strong> <strong>in</strong>tegrated design, control, and operation strategy can<br />

be developed to maximize the overall efficiency while lower<strong>in</strong>g the capital cost and later the<br />

associated operation and ma<strong>in</strong>tenance fees. <strong>An</strong> annual simulation us<strong>in</strong>g TRNSYS tools with ref<strong>in</strong>ed<br />

build<strong>in</strong>g <strong>in</strong>formation can be conducted for several simplified system configurations associated with the<br />

four heat sources for an absorption chiller and a cost model to comprehensively analyze the effects of<br />

build<strong>in</strong>g occupancy and weather variations on system overall efficiencies and economic benefits.<br />

91


5.2.2.1 <strong>Chiller</strong> Performance Tables for Build<strong>in</strong>g Simulation Tools<br />

TRNSYS build<strong>in</strong>g simulation tools can, <strong>in</strong> pr<strong>in</strong>ciple, directly <strong>in</strong>tegrate the <strong>in</strong>puts and outputs of<br />

detailed EES models for system and plant equipment, but this method is not very convenient because<br />

the iteration of build<strong>in</strong>g load calculations requires an iterated solution of the mathematical calculation.<br />

Computation times are <strong>in</strong>creased greatly by us<strong>in</strong>g this method, particularly when the equipment model<br />

becomes more and more complex. As an alternative, chiller performance tables based on <strong>in</strong>put<br />

operat<strong>in</strong>g conditions and output performance from solutions of a computational model are more<br />

appropriate for use <strong>in</strong> overall system simulation. The performance tables generated from this thesis can<br />

greatly enrich the limited component library of TRNSYS simulation tools.<br />

5.2.2.2 Cost Model<br />

The purpose of a comprehensive cost model is to support the decision-mak<strong>in</strong>g process <strong>in</strong> design<strong>in</strong>g an<br />

absorption chiller-based <strong>BCHP</strong> system. As the basis of economical analysis, a cost model can be<br />

developed to forecast the cost of chilled water of different system configurations. The model will<br />

make use of capital costs, operation costs (grid electricity and steam, natural gas, hot water, and<br />

exhaust gas), <strong>in</strong>terest rates, expected return-on-<strong>in</strong>vestment, system efficiency, and ma<strong>in</strong>tenance cost to<br />

predict the system economical performance.<br />

92


References<br />

[1] “Residential Consumption of Electricity by End Use,” Energy Information Adm<strong>in</strong>istration, 2001.<br />

[2] “Commercial Build<strong>in</strong>gs Energy Consumption Survey,” Overview of Commercial Build<strong>in</strong>g<br />

Characteristics, Energy Information Adm<strong>in</strong>istration, 2003.<br />

[3] “<strong>An</strong>nual Energy Review” 2004 Report, Energy Information Adm<strong>in</strong>istration, No. DOE/EIA-0384,<br />

2004.<br />

[4] Broad absorption chiller catalog for the US market, 2004.<br />

[5] Volker Hartkopf, Vivian Loftness, “Global relevance of total build<strong>in</strong>g performance,” Automation <strong>in</strong><br />

construction, pp. 377-393, 1999<br />

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[8] Eric A. Koeppel, Sanford A. Kle<strong>in</strong>, and John W. Mitchell, “Commercial <strong>Absorption</strong> <strong>Chiller</strong> Models<br />

For Evaluation of Control Strategies,” Desiccant <strong>Absorption</strong> Cool<strong>in</strong>g, ASHRAE Technical Data<br />

Bullet<strong>in</strong>, Volume 11, Number 2, pp. 71-80, January 1995<br />

[9] G. C. Vliet, M. B. Lawson, and R. A. Lithgow, “Water-Lithium Bromide Two-stage <strong>Absorption</strong><br />

Cool<strong>in</strong>g Cycle <strong>An</strong>alysis, ” ASHRAE Transaction, 88, Part1, 811-823, 1982<br />

[10] Keith E. Herold, Re<strong>in</strong>hard Radermacher, Sanford A. Kle<strong>in</strong>, 1996, <strong>Absorption</strong> <strong>Chiller</strong>s and Heat<br />

Pumps, CPC Press, Inc., Boca Raton, FL.<br />

[11] K. Gommed and G. Grossman, “Performance <strong>An</strong>alysis of Staged <strong>Absorption</strong> Heat Pumps: Water-<br />

LiBr Systems,” ASHRAE Transactions, Vol. 96, Part 1, pp.1590-1598, 1990.<br />

[12] G. Grossman and E. Michelson, “A Modular Computer Simulation of <strong>Absorption</strong> Systems,”<br />

ASHRAE Transactions, Vol91, Part 2B, pp.1808-1827, 1985.<br />

[13] F. Cosenza, G. C.Vliet, “<strong>Absorption</strong> <strong>in</strong> Fall<strong>in</strong>g Water-LiBr Films on Horizontal Tubes,” ASHRAE<br />

Transactions 96910, pp693-701, 1990.<br />

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[14] <strong>An</strong>dberg, J. W., and Vliet, G. C. “<strong>Absorption</strong> of Vapors <strong>in</strong>to Liquid Films Flow<strong>in</strong>g over cooled<br />

Horizontal Tubes,” Proceed<strong>in</strong>gs of the ASME/JSME Jo<strong>in</strong>t Thermal Eng<strong>in</strong>eer<strong>in</strong>g Conference, Vol. 2,<br />

pp. 533-541, March, 1987.<br />

[15] Ick-Soo Kyung, Keith E. Herold, “Performance of Horizontal Smooth Tube Absorber with and<br />

without 2-Ethyl-Hexanol,” Journal of Heat Transfer, Vol 124, pp.177-183, February 2002.<br />

[16] I. Greiter, A. Wagner, V. Weiss, and Georg Alefeld, “Experimental Investigation of Heat and Mass<br />

Transfer <strong>in</strong> A Horizontal-tube Fall<strong>in</strong>g-film Absorber with Aqueous Solutions,” International<br />

<strong>Absorption</strong> Heat Pump Conference, AES Vol. 31, pp. 225-232, ASME, 1993.<br />

[17] Y. Nagaoka, N. Nishiyama, K.Ajisaka, and M. Nakamura, et al., “Absorber of <strong>Absorption</strong><br />

Refrigerat<strong>in</strong>g Mach<strong>in</strong>e (Enhancement of heat and mass transfer <strong>in</strong> fall<strong>in</strong>g film absorbers by surface<br />

configuration),” Proceed<strong>in</strong>gs of the 17th International Congress of Refrigeration, pp. 990-995, 1987.<br />

[18] J. P. Holman, “Heat transfer”, 8 th edition, the McGraw-Hill Companies, Inc., 1997<br />

[19] R.E. Sonntag, C. Borgnakke, and G. J. Van Wylen, Fundamentals of Thermodynamics, 5 th edition,<br />

John Wiley & Sons, Inc., 1998.<br />

[20] Volker Hartkopf, David Archer, and Hongxi Y<strong>in</strong>, “A Fuel Cell based Energy Supply System for a<br />

Multi Purpose Build<strong>in</strong>g”, the Ideaction 2003 Conference, FMA Australia, Sydney 2003<br />

[21] D.H. Archer, Volker Hartkopf, and Hongxi Y<strong>in</strong>; 2003, Advanced Build<strong>in</strong>g System Integration<br />

Consortium (ABSIC) annual meet<strong>in</strong>g; “<strong>An</strong> Energy Supply System for the Intelligent Workplace,<br />

IWESS,” Proceed<strong>in</strong>gs of ABSIC 2003, Wash<strong>in</strong>gton DC; June, 2003<br />

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Consortium (ABSIC) annual meet<strong>in</strong>g; “<strong>An</strong> Energy Supply System for the Intelligent Workplace,<br />

IWESS,” Proceed<strong>in</strong>gs of ABSIC 2004, Wash<strong>in</strong>gton DC; June, 2004<br />

[23] Archer, Hartkopf, and Y<strong>in</strong>, December 2003, DOE Proposal for Research, Development, and<br />

Demonstration of <strong>Micro</strong> CHP for Residential <strong>Application</strong>s (DE-PS36-03-GO93014), <strong>Carnegie</strong> Mellon<br />

University, Pittsburgh, PA<br />

[24] Chun, K.R., and R. A. Seban, “Heat Transfer to Evaporat<strong>in</strong>g Liquid Films,” Journal of Heat<br />

Transfer, 91c, page 391-396, 1971"<br />

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Horizontal Tube Evaporator,” AIChE Journal, Vol. 34, No.9, page 1539-1549, September 1988<br />

[26] M. C., Chyu and A.e. Berles, “<strong>An</strong> <strong>An</strong>alytical and Experimental Study of Fall<strong>in</strong>g-Film Evaporation<br />

on a Horizontal Tube,” AIChE Journal, Vol. 34, No.9, page 1539-1549, September 1988<br />

[27] Dittus, F. W., and L. M. K. Boelter: University California Berkeley Pub. Eng., Vol. 2, p.443, 1930.<br />

[28] Kern, Q. Donald, 1950, “Chapter 12, Condensation of s<strong>in</strong>gle vapors,” Process Heat Transfer, pp.<br />

252-312, McGraw-HIill Book Company<br />

[29] Kern, Q. Donald, 1958, “Mathematical Development of Load<strong>in</strong>g <strong>in</strong> Horizontal Condensers,”<br />

AIChe Journal, 4, pp. 157-160<br />

[30] Hausen, H.: Darstellung des Warmeuberganges <strong>in</strong> Rohren durch verallgeme<strong>in</strong>erte<br />

Potenzbeziehungen, VDIZ., no. 4, p. 91, 1943.<br />

[31] H. C. Hottel, 1967, “Chapter 6, Gas Emissivities and Absorptivities,” Radiative Transfer, pp. 234,<br />

McGraw-HIill, Inc.<br />

[32] Alefeld, G., Radermacher, R., 1994, Heat Conversion Systems, CRC Press Inc., Boca Raton, FL<br />

[33] U.S. Department of Energy 2001, “National CHP Roadmap, Doubl<strong>in</strong>g Comb<strong>in</strong>ed Heat and Power<br />

Capacity <strong>in</strong> the United States by 2010,” Wash<strong>in</strong>gton, D.C.<br />

[34] Grossman G. and K. Gommed, “A Computer Model for Simulation of <strong>Absorption</strong> Systems <strong>in</strong><br />

Flexible and Modular Form”, ASHRAE Transactions, Vol.93, Part 2, pp.2389-2428, 1987.<br />

[35] Braun J.E., S.A. Kle<strong>in</strong>, W.A. Beckman and J.W. Mitchell, “Methodologies for Optimal Control of<br />

Chilled-Water Systems without Storage”, ASHRAE Transactions, Vol. 95, Part 1, pp.652-662, 1989<br />

[36] EERE, U.S. Department of Energy, May 2003, Thermally Activated Technology, “Technology<br />

Roadmap, Develop<strong>in</strong>g New Ways to use Thermal Energy to meet the Energy Needs of Homes,<br />

Offices, Factories, and Communities,” Wash<strong>in</strong>gton, D.C.<br />

[37] V. Hartkopf, D. Archer, and V. Loftness, “Build<strong>in</strong>g as Power Plant,” Smart and Susta<strong>in</strong>able Built<br />

Environments, Black publish<strong>in</strong>g, Ltd. pp. 55-74, 2005<br />

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[38] ASHRAE Handbooks 2000, HVAC Systems and Equipment, Atlanta: American Society of<br />

Heat<strong>in</strong>g, Refrigerat<strong>in</strong>g and Air-Condition<strong>in</strong>g Eng<strong>in</strong>eers, Inc.<br />

[39] ASHRAE Handbooks 2001, Fundamentals, Atlanta: American Society of Heat<strong>in</strong>g, Refrigerat<strong>in</strong>g<br />

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[40] ASHRAE Handbooks 2002, Refrigeration, Atlanta: American Society of Heat<strong>in</strong>g, Refrigerat<strong>in</strong>g<br />

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[41] ASHRAE Handbooks 2003, HVAC <strong>Application</strong>s, Atlanta: American Society of Heat<strong>in</strong>g,<br />

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[42] “<strong>Absorption</strong> <strong>Chiller</strong>s Guidel<strong>in</strong>e,” Southern California Gas Company New Build<strong>in</strong>g Institute<br />

Advanced Design Guidel<strong>in</strong>e Series, 1998<br />

[43] J<strong>in</strong>, Kaiwen, Broad Co., BCT16 Installation, Operation, and Ma<strong>in</strong>tenance Guides, 2004,<br />

Changsha, Ch<strong>in</strong>a.<br />

[44] Chen, Xiaoyong, Broad Co., BCT16 Commission<strong>in</strong>g Instruction and Explanation Notes, 2004,<br />

Changsha, Ch<strong>in</strong>a.<br />

96


Appendix 1A<br />

97


Appendix 2A<br />

102


Appendix 2B<br />

118


Appendix 3A<br />

130


Appendix 4A<br />

150


Acronyms<br />

ACEEE: American Council for Energy Efficient Economy<br />

ALC: Automated Logic Co.<br />

BAPP: build<strong>in</strong>g as power plant<br />

BAS: build<strong>in</strong>g automation system<br />

<strong>BCHP</strong>: build<strong>in</strong>g cool<strong>in</strong>g heat<strong>in</strong>g and power<br />

CHP: comb<strong>in</strong>ed heat<strong>in</strong>g and power<br />

CHW: chilled water<br />

CHWS: chilled-water supply<br />

CHWR: chilled-water return<br />

COCHW: cost of chilled water<br />

COP: coefficient of performance<br />

CMU: <strong>Carnegie</strong> Mellon University<br />

CW: cool<strong>in</strong>g water<br />

CWS: cool<strong>in</strong>g-water supply<br />

CWR: cool<strong>in</strong>g-water return<br />

EES: eng<strong>in</strong>eer<strong>in</strong>g equation solver<br />

EIA: energy <strong>in</strong>formation adm<strong>in</strong>istration.<br />

ESS: energy supply system<br />

GUI: graphic user <strong>in</strong>terface<br />

HVAC&R: heat<strong>in</strong>g ventilat<strong>in</strong>g air condition<strong>in</strong>g and refrigerat<strong>in</strong>g<br />

HTRG: high-temperature regenerator<br />

HTHX: high-temperature heat exchanger<br />

HRHX: heat recovery heat exchanger<br />

IW: the <strong>in</strong>telligent workplace<br />

ICPC: <strong>in</strong>tegrated compound parabolic collectors<br />

LiBr: lithium bromide<br />

LPG: liquid pressurized gas<br />

LTRG: low-temperature regenerator<br />

LTHX: low-temperature heat exchanger<br />

SOFC: solid oxide fuel cell<br />

TRNSYS: transient systems simulation program<br />

WCS: web control server<br />

194

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