Chapter 13 Gas Turbine Power Plants
Chapter 13 Gas Turbine Power Plants
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