3-4 Isentropic expansion (in a turbine)
4-1 Constant-pressure heat rejection
The T-sand P-vdiagrams of an ideal Brayton cycle are shown in Fig. 9–31.
Notice that all four processes of the Brayton cycle are executed in steady-
flow devices; thus, they should be analyzed as steady-flow processes. When
the changes in kinetic and potential energies are neglected, the energy bal-
ance for a steady-flow process can be expressed, on a unit–mass basis, as
(9–15)
Therefore, heat transfers to and from the working fluid are
(9–16a)
and
(9–16b)
Then the thermal efficiency of the ideal Brayton cycle under the cold-air-
standard assumptions becomes
Processes 1-2 and 3-4 are isentropic, and P 2 P 3 and P 4 P 1. Thus,
Substituting these equations into the thermal efficiency relation and simpli-
fying give
hth,Brayton 1 (9–17)
1
r^1 pk^1 2>k
T 2
T 1
a
P 2
P 1
b
1 k 1 2>k
a
P 3
P 4
b
1 k 1 2>k
T 3
T 4
hth,Brayton
wnet
qin^1
qout
qin^1
cp 1 T 4 T 12
cp 1 T 3 T 22
1
T 11 T 4 >T 1 12
T 21 T 3 >T 2 12
qouth 4 h 1 cp 1 T 4 T 12
qinh 3 h 2 cp 1 T 3 T 22
1 qinqout 2 1 winwout 2 hexithinlet
508 | Thermodynamics
Compressor
wnet
Turbine
Combustion
chamber
Fresh
air
Exhaust
(^1) gases
2
3
4
Fuel
FIGURE 9–29
An open-cycle gas-turbine engine.
Compressor Turbine
1
2
3
Heat^4
exchanger
Heat
exchanger
wnet
qin
qout
FIGURE 9–30
A closed-cycle gas-turbine engine.
P
s s = const.
= const.
2
1 4
3
s
T
2
3
4
1
P = const.
P = const.
(a) T-s diagram
(b) P-v diagram
qout
qin
qout
qin
v
FIGURE 9–31
T-sand P-vdiagrams for the ideal
Brayton cycle.