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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 />

Figure: 1 Schematic flow diagram <strong>of</strong> Co-Generation Cycle<br />

In the present system ambient air is coming to air compressor and after compression its temperature and pressure<br />

is increased. This compressed air is passed through regenerator. In regenerator compressed air is entering from<br />

one side and combustion gases coming out <strong>of</strong> gas turbine from the other. High temperature combustion gases<br />

transfer their heat to the compressed air. After gaining heat this compressed air comes to combustion chamber<br />

and fuel is added in it. After burning in air chemical energy <strong>of</strong> fuel is converted into thermal energy.<br />

Temperature <strong>of</strong> combustion products coming out <strong>of</strong> combustion chamber depends upon turbine inlet temperature.<br />

Combustion product temperature is controlled by making A/F mixture a lean mixture. Gasses coming out from<br />

gas turbine are having a large amount <strong>of</strong> thermal energy. Some part <strong>of</strong> this thermal energy is transferred to<br />

compressed air in regenerator and remaining part is absorbed by high pressure water in steam generator. Flue gas<br />

temperature coming out <strong>of</strong> steam generator is dependent upon the dew point temperature <strong>of</strong> flue gases. This dew<br />

point temperature decides the temperature at which flue gases must enter the stack. Each component is modeled<br />

by mass and energy balances. If the system operates in a steady-state, steady flow condition and all the<br />

nonreacting gases are arbitrarily assigned as zero thermo mechanical enthalpy, entropy, and exergy at the<br />

condition <strong>of</strong> ambient pressure and temperature regardless <strong>of</strong> their chemical composition, then the entropy <strong>of</strong><br />

mixing different gaseous components can be neglected, and the general exergy-balance equation is given by<br />

For single stream flow<br />

Specific exergy is given by<br />

. n . . . .<br />

∑ ∑ ∑<br />

E = ( E ) i + me − me − E<br />

W Q D<br />

i=<br />

1<br />

in out<br />

. . . . .<br />

E = ( E ) + me − me − me<br />

W Q in out D<br />

⎛ T T ⎞ <br />

P ⎡<br />

<br />

⎛1+<br />

wa<br />

⎞<br />

( ) 1 ln (1 ) ln (1 )ln <br />

⎛ w ⎞⎤<br />

e = C<br />

pa<br />

+ wC<br />

pv<br />

Ta ⎜ − − ⎟ + + w RaTa + RaTa<br />

⎢ + w ⎜ wln<br />

T 1 ⎟ + ⎜ ⎟⎥<br />

⎝ a<br />

Ta ⎠ Pa<br />

⎢⎣<br />

⎝ + w ⎠ ⎝ wa<br />

⎠⎥⎦<br />

Where w = 1.608w<br />

The mass, energy, and exergy balances <strong>of</strong> the component <strong>of</strong> the plant are given below.<br />

2.1. Air Compressors<br />

The inlet and outlet humidity ratios will be the same. The energy balance yields the compressor work<br />

compressor outlet temperature.<br />

w<br />

ai<br />

= w<br />

ao<br />

Wc<br />

and<br />

T<br />

T<br />

a o<br />

a i<br />

=<br />

[ r ]<br />

c<br />

γ c − 1<br />

γ cη<br />

c<br />

W<br />

c<br />

= h<br />

a o<br />

− h<br />

a i<br />

The exergy balance for the compressor gives the exergy destruction e DC as following<br />

e = W + ( e − e )<br />

DC C ai ao<br />

181

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