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Chapter 13 Gas Turbine Power Plants

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in the cycle 1-2-3-4-1, the cycle is called the ideal Brayton cycle.<br />

The thermal efficiency of the ideal Brayton cycle is a function of<br />

pressure ratio pjpi, and its value is the highest possible efficiency<br />

for any Brayton cycle at a given pressure ratio.<br />

The thermal efficiency of any cycle is defined by (5.30). In the<br />

Brayton cycle the net work is the algebraic sum of the turbine<br />

work W t , which is positive, and the compressor work W c , which is<br />

negative; thus, the thermal efficiency is written as<br />

W +Wc<br />

'<br />

QA<br />

(<strong>13</strong>.1)<br />

where Q A is the energy added to the flowing gas in the combustor<br />

as a result of the exothermic chemical reaction which occurs as<br />

the fuel burns in air.<br />

In the following sections the methods for computing W t , W c ,<br />

and Q A will be shown for the ideal Brayton cycle, the standard<br />

Brayton cycle, and for variations on the Brayton cycle which involve<br />

the use of heat exchangers. Finally, the combined cycle,<br />

Brayton plus Rankine, is considered.<br />

<strong>13</strong>.2 Ideal Brayton Cycle<br />

For the ideal cycle we can assume that the working fluid is cold<br />

air, i.e., a gas having a molecular weight of 28.96 and a ratio of<br />

specific heats y of 1 .4, and that the air behaves as a perfect gas.<br />

The compression and expansion processes are isentropic for the<br />

ideal cycle. According to (5.21) work for compression is given by<br />

W c =h ol -h m (<strong>13</strong>.2)<br />

where any change in potential energy is assumed negligible, and<br />

the solid boundaries of the compressor are assumed to be adiabatic.<br />

Assuming that the working substance is a perfect gas and

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