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OCTOBER 19-20, 2012 - YMCA University of Science & Technology

OCTOBER 19-20, 2012 - YMCA University of Science & Technology

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Proceedings <strong>of</strong> the National Conference on<br />

Trends and Advances in Mechanical Engineering,<br />

<strong>YMCA</strong> <strong>University</strong> <strong>of</strong> <strong>Science</strong> & <strong>Technology</strong>, Faridabad, Haryana, Oct <strong>19</strong>-<strong>20</strong>, <strong>20</strong>12<br />

∆ m )<br />

w<br />

= (<br />

1<br />

− ω1′<br />

m a<br />

ω (12)<br />

where ω<br />

1<br />

is the humidity ratio <strong>of</strong> air after cooling, The partial pressure <strong>of</strong> water vapour can be found from the<br />

respective relative humidity (φ ) by:<br />

P<br />

= φ<br />

(13)<br />

v<br />

P sat<br />

where P and<br />

sat<br />

P are the saturation pressures <strong>of</strong> water for the corresponding temperature. Pressure loss in the<br />

sat<br />

adiabatic mixing is neglected.<br />

The enthalpy, entropy, and exergy can be determined at each state point using mass and energy balances. The<br />

performance parameters required for the thermodynamic analysis <strong>of</strong> retr<strong>of</strong>itted systems are given below:<br />

Thermal Efficiency (η Th ): Thermal efficiency <strong>of</strong> a thermal system is defined as the ratio <strong>of</strong> net work output<br />

W & ) to the total heat input ( Q & ) <strong>of</strong> the fuel.<br />

f<br />

W&<br />

net<br />

=<br />

Th<br />

Q&<br />

(<br />

net<br />

η (14)<br />

f<br />

Generation Efficiency (η Gen ): Generation efficiency <strong>of</strong> a thermal system is defined as the ratio <strong>of</strong> electrical<br />

power output (W el ) to the total heat input <strong>of</strong> the fuel(Q f ).<br />

W<br />

el<br />

η =<br />

(15)<br />

Gen<br />

Q<br />

f<br />

Heat-Rate (HR in kJ/s/kW): Heat rate is defined as the ratio <strong>of</strong> heat produced by the fuel (<br />

W &<br />

Q&<br />

W&<br />

power output (<br />

HR<br />

el<br />

el<br />

) <strong>of</strong> the thermal system.<br />

Q & ) to the electrical<br />

f<br />

= (16)<br />

Specific Fuel-Consumption (SFC): Specific fuel–consumption <strong>of</strong> a thermal system is defined as the ratio <strong>of</strong><br />

mass <strong>of</strong> fuel to the net work output. It is reciprocal <strong>of</strong> specific net work (W spec ).<br />

SFC<br />

m&<br />

W&<br />

f<br />

= (17)<br />

net<br />

First–Law Efficiency (<br />

): The ratio <strong>of</strong> all the useful energy extracted from the system (electricity and process<br />

heat) to the energy <strong>of</strong> fuel input is known as first-law efficiency. First-law efficiency is also known as fuel<br />

utilization efficiency or utilization factor or energetic efficiency. By definition,<br />

where<br />

( W& + Q&<br />

)<br />

el Pr o<br />

η =<br />

(18)<br />

I<br />

Q&<br />

f<br />

is process heat rate.<br />

Second–Law Efficiency (<br />

): Since exergy is more valuable than energy according to the second law <strong>of</strong><br />

thermodynamics, it is useful to consider both output and input in terms <strong>of</strong> exergy. The amount <strong>of</strong> exergy supplied<br />

in the product to the amount <strong>of</strong> exergy associated with the fuel is a more accurate measure <strong>of</strong> thermodynamic<br />

performance <strong>of</strong> a system, which is called second-law efficiency. It is also called exergetic efficiency<br />

(effectiveness or rational efficiency). By definition,<br />

( W& + E&<br />

)<br />

el pro<br />

η =<br />

(<strong>19</strong>)<br />

II<br />

E&<br />

f<br />

where is the exergy content <strong>of</strong> process heat and is the exergy content <strong>of</strong> fuel input.<br />

E &<br />

Exergy-Destruction Rate (<br />

DR<br />

)-The component exergy destruction rate can be compared to the total exergy<br />

destruction rate within the system.<br />

E&<br />

E&<br />

D<br />

E& = (<strong>20</strong>)<br />

DR<br />

D, tot<br />

Results and Discussion<br />

In the present study following configurations with retr<strong>of</strong>itting have been studied in comparison to simple gas<br />

turbine cycle:<br />

(i) Simple gas turbine cycle with inlet air cooling (IAC)<br />

f<br />

<strong>19</strong>9

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