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Abstract Booklet 2006 - Swanson School of Engineering - University ...

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28-5<br />

A Kinetic Approach to Catalytic Oxidation <strong>of</strong> Mercury in Flue Gas<br />

Evan J. Granite, Albert A. Presto, Henry W. Pennline, Andy Karash, William J.<br />

O’Dowd, Richard A. Hargis, DOE/NETL, USA<br />

Several materials have been examined as catalysts for the oxidation <strong>of</strong> mercury in a<br />

bench-scale packed-bed reactor located at NETL. The catalysts examined include<br />

activated carbon, Thief carbons, precious metals, fly ash, and halogen compounds.<br />

Slipstreams <strong>of</strong> flue gas generated by the NETL 500-lb/hr pilot-scale combustion<br />

facility were contacted with the catalysts. An on-line continuous emissions monitor<br />

(CEM) was employed to measure elemental and oxidized mercury entering and exiting<br />

the bed. The apparent activation energy and reaction order for mercury were<br />

determined for several <strong>of</strong> the catalysts. Future research on catalyst materials will be<br />

conducted in a bench-scale packed-bed reactor employing both simulated and real flue<br />

gas streams generated on-site at NETL. The work presented in this manuscript was<br />

also accepted for publication in Energy & Fuels.<br />

SESSION 29<br />

GAS TURBINES AND FUEL CELLS FOR SYNTHESIS GAS AND<br />

HYDROGEN APPLICATIONS – 1<br />

29-1<br />

Coal IGCC Turbine Technology Improvements for Carbon Free Fuels<br />

Ashok Anand, Benjamin Mancuso, Kevin Collins, Greg Wotzak, GE Energy, USA<br />

Reduction <strong>of</strong> carbon dioxide from Coal-based IGCC Power Plants is rapidly gaining<br />

increased interest in future installations. Studies have shown that IGCC technology is<br />

able to capture and remove carbon dioxide at lower economic penalty as compared to<br />

conventional pulverized coal fired steam plants. Further improvements in IGCC power<br />

plants with carbon capture, is possible though the development <strong>of</strong> specific gas turbine<br />

cycle designs that increase plant efficiency at reduced costs and emissions. The<br />

performance influence <strong>of</strong> a typical heavy-duty gas turbine’s cycle parameters on IGCC<br />

plant with carbon capture is presented. An optimization analysis method is described,<br />

which can be successfully applied to select a gas turbine cycle design to achieve plant<br />

level performance goals.<br />

29-2<br />

Advanced Hydrogen Turbine Development<br />

Ed Bancalari, Ihor S. Diakunchak, Pedy Chan, Siemens Power Generation, Inc., USA<br />

The Advanced Hydrogen Turbine Development Project objective is to design and develop a<br />

fuel flexible (coal derived hydrogen or syngas) advanced gas turbine for Integrated<br />

Gasification Combined Cycle (IGCC) and FutureGen type applications that meets the U.S.<br />

Department <strong>of</strong> Energy (DOE) turbine performance goals. The overall DOE Advanced<br />

Power System goal is to conduct the Research and Development necessary to produce CO 2<br />

sequestration ready coal-based IGCC power systems with high efficiency (45-50% [HHV]),<br />

near zero emissions (< 2 ppm NO x @ 15% O 2 ) and competitive plant capital cost (<<br />

$1000/kW). DOE has awarded Siemens Power Generation a contract for Phases 1 and 2<br />

development work. Phase 1 activities will include identification <strong>of</strong> advanced technologies<br />

required to achieve the Project goals, detailed Research & Development Implementation<br />

Plan preparation and conceptual designs for the new gas turbine components. In Phase 2, the<br />

identified concepts/technologies will be down selected and a detailed design <strong>of</strong> the gas<br />

turbine will be completed. Phase 3, which has not yet been awarded, will involve the<br />

advanced gas turbine and IGCC plant construction and validation/demonstration testing. The<br />

end objective is to validate the advanced gas turbine technology by 2015. The starting point<br />

for this development effort is the SGT6-6000G gas turbine. This gas turbine will be adapted<br />

for operation on coal and biomass derived hydrogen and syngas fuels, as well as natural gas,<br />

while achieving high performance levels and reduced capital costs. This paper describes<br />

Phase 1 activities and accomplishments in the first 9 months since the program was initiated.<br />

29-3<br />

Benefits to IGCC Gas Turbines <strong>of</strong> Advanced Vortex Combustion<br />

Robert Steele, Pete Baldwin, Ramgen Power Systems, USA<br />

Ramgen Power Systems is developing an Advanced Vortex Combustion (AVC) technology<br />

for combustion <strong>of</strong> hydrogen-based fuels which shows tremendous potential for increased<br />

energy efficiency and improved asset utilization. The fundamentals <strong>of</strong> the technology and<br />

the potential advantages <strong>of</strong> incorporating the AVC approach into an IGCC gas turbine will<br />

be presented. The AVC technology can be applied to the efficient and cost-effective<br />

combustion <strong>of</strong> hydrogen-based fuels with sub-3 ppmv NO x emissions while maintaining or<br />

extending simple cycle efficiencies. The AVC technology has the potential for improved<br />

turbine efficiency, lower NO x<br />

emissions, greater flame stability, high flame speed flexibility, increased durability, and<br />

reduced manufacturing costs. This approach can play an important role in the advancement<br />

<strong>of</strong> future Integrated Gasification Combined Cycle (IGCC) power plants that will require<br />

hydrogen-enriched fuel burning gas turbines. The flame speed <strong>of</strong> hydrogen-air mixture is six<br />

times higher than a natural gas-air mixture. Conventional swirl-based combustion systems<br />

25<br />

need customized modifications in order to manage the potential for flame flashback. The<br />

unique insensitivity <strong>of</strong> the AVC approach to high through-put velocities will reduce<br />

hardware modifications and accommodate the extremely fast burning hydrogen-based fuels.<br />

In addition, Ramgen’s AVC technology is cross-cutting and capable <strong>of</strong> delivering benefits to<br />

many <strong>of</strong> the technical areas <strong>of</strong> concern in zero-emissions combustor-based facilities<br />

including the oxy-fuel Rankine cycle system.<br />

29-4<br />

Catalytic Combustion for Ultra-Low NO x Hydrogen Turbines<br />

Benjamin Baird, S. Etemad, Sandeep Alvandi, William C. Pfefferle, H. Karim,<br />

Precision Combustion, Inc., USA<br />

Kenneth O. Smith, W. Nazeer, Solar Turbines, Inc., USA<br />

Precision Combustion, Inc. (PCI), under sponsorship from the U.S. Department <strong>of</strong><br />

Energy, is further developing it’s Rich Catalytic Lean-burn (RCL®) combustion<br />

system for hydrogen fuels. Rich catalytic operation has successfully demonstrated low<br />

single digit ppm NO x and the ability to burn hydrogen fuels in 9 atmosphere subscale<br />

tests. The test data show the potential <strong>of</strong> using rich catalytic combustion for low single<br />

digit emissions. Areas <strong>of</strong> further work to commercialize this technology has been<br />

identified. PCI, in collaboration with Solar Turbines Incorporated and other gas turbine<br />

manufacturers, has a 39 month DOE Fossil Energy Turbine Technology R&D program<br />

to develop and demonstrate a low emission rich catalytic combustion system for fuel<br />

flexible ultra-low NO x megawatt-scale gas turbines that can utilize hydrogen fuel,<br />

facilitate high efficiency operation, and be installed or retr<strong>of</strong>itted into existing turbines.<br />

This paper presents the status <strong>of</strong> the rich catalytic application from the combustion<br />

point <strong>of</strong> view for MW size engine application.<br />

29-5<br />

Development <strong>of</strong> Turbo Machinery for a Zero CO 2 Emissions Oxy-Fuel Cycle<br />

Mohan A. Hebber, Shiv Dinkar, Juan Pablo Gutierrez, Siemens Power Generation, Inc.<br />

Jim Downs, Florida Turbine Technologies, Inc., USA<br />

In 2005 the U.S. Department <strong>of</strong> Energy-National Energy Technology Laboratory (DOE-<br />

NETL) awarded a program to Siemens Power Generation (SPG), Inc. to develop turbo<br />

machinery powered by oxy-fuel combustion, which generates near zero emissions and<br />

provides for economical CO 2 capture capability. (The combustor for this oxy-fuel cycle is to<br />

be developed separately by Clean Energy Systems (CES), Inc. <strong>of</strong> Rancho Cordova,<br />

California.). The new working fluid (a mixture <strong>of</strong> CO 2 and steam) and the desire to<br />

maximize the plant cycle efficiency pose numerous technical challenges not only in<br />

developing the turbine designs and consideration <strong>of</strong> material systems, but also in the<br />

selection <strong>of</strong> a plant cycle. The calculation <strong>of</strong> auxiliary loads for Fuel Processing Plant<br />

(gasifier), Air Separation Unit (ASU), O 2 compression, CO 2 compression, limitations on<br />

metal temperatures and other boundary conditions – all posed difficulties in arriving at<br />

cycles for further consideration. Any turbine design that depends on boundary conditions<br />

higher than the current state-<strong>of</strong>-the-art poses special challenges in the selection <strong>of</strong> materials.<br />

Initial studies indicate that materials in the turbine for the “topping” cycle may have to<br />

tolerate a Turbine Inlet Temperature (TIT) well in excess <strong>of</strong> 1500°C with CO 2 and H 2 O as<br />

working fluid. With regards to the steam turbine in the “bottoming” cycle, major challenges<br />

are anticipated in selecting materials for the turbine casing, rotor, blading, valves, sealing and<br />

bolting. Other challenges include innovative cooling techniques including, but not limited to,<br />

the development <strong>of</strong> serpentine cooling paths; development <strong>of</strong> start-up procedures and<br />

algorithms for controls and life consumption. The paper describes approaches planned to<br />

overcome the technical challenges and develop turbine designs that meet the overall<br />

objectives <strong>of</strong> the program including the efficiency goals. An overall time line is also<br />

identified for key milestones.<br />

SESSION 30<br />

GLOBAL CLIMATE CHANGE: CO 2 CAPTURE – 2:<br />

MEMBRANES AND SOLID SORBENTS<br />

30-1<br />

Experimental Investigation <strong>of</strong> a Molecular Gate Membrane for<br />

Separation <strong>of</strong> Carbon Dioxide for Flue Gas<br />

James H<strong>of</strong>fman, Henry W. Pennline, DOE/NETL, USA<br />

Shingo Kazama, Teruhiko Kai, Takayuki Kouketsu, Shigetoshi Matsui, Koichi<br />

Yamada, RITE, JAPAN<br />

Commercial-sized modules <strong>of</strong> the PAMAM dendrimer composite membrane with high<br />

CO 2 /N 2 selectivity and CO 2 permeance were developed according to the In-situ Modification<br />

(IM) method. This method utilizes the interfacial precipitation <strong>of</strong> membrane materials on the<br />

surface <strong>of</strong> porous, commercially available polysulfone (PSF) ultrafiltration hollow fiber<br />

membrane substrates. A thin layer <strong>of</strong> amphiphilic chitosan, which has a potential affinity for<br />

both hydrophobic PSF substrates and hydrophilic PAMAM dendrimers, was employed as a<br />

gutter layer directly beneath the inner surface <strong>of</strong> the substrate by the IM method. PAMAM<br />

dendrimers were then impregnated into the chitosan gutter layer to form a hybrid active layer<br />

for CO 2 separation. Permeation experiments <strong>of</strong> the PAMAM dendrimer composite<br />

membrane were carried out using a humidified mixed CO 2 / N 2 feed gas at a pressure

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