560 ENGINEERING THERMODYNAMICS
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\M-therm\Th15-2.pm5
(iv)Brake thermal efficiency :
Brake thermal efficiency =
W
hhf
brake
1 − 3
=
225
3037 6 428.8. −
= 0.086 or 8.6%. (Ans.)
(v)Relative efficiency :
Relative efficiency on the basis of indicated work
=
W
hh
W
hh
f
f
indicated
1
1
3
3
−
−
=
W
W
indicated = 281 25
495 8
.
. = 0.567 or 56.7%. (Ans.)
Relative efficiency on the basis of brake work
=
W
hh
W
hh
f
f
indicated
()
()
1
1
3
3
−
−
=
W
W
brake =^225
495 8. = 0.4538 or 45.38%. (Ans.)
Example 12.11. Superheated steam at a pressure of 10 bar and 400°C is supplied to a
steam engine. Adiabatic expansion takes place to release point at 0.9 bar and it exhausts into a
condenser at 0.3 bar. Neglecting clearance determine for a steam flow rate of 1.5 kg/s :
(i)Quality of steam at the end of expansion and the end of constant volume operation.
(ii)Power developed.
(iii)Specific steam consumption.
(iv)Modified Rankine cycle efficiency.
Solution. Fig. 12.14 shows the p-V and T-s diagrams for modified Rankine cycle.
From steam tables :
- At 10 bar, 400°°°°°C : h 1 = 3263.9 kJ/kg, v 1 = 0.307 m^3 /kg, s 1 = 7.465 kJ/kg K
2. At 0.9 bar : ts 2 = 96.7°C, hg 2 = 2670.9 kJ/kg, sg 2 = 7.3954 kJ/kg K,
vg 2 = 1.869 m^3 /kg - At 0.3 bar : hf 3 = 289.3 kJ/kg, vg 3 = 5.229 m^3 /kg
(i) Quality of steam at the end of expansion, Tsup2 :
For isentropic expansion 1-2, we have
s 1 = s 2
= sg 2 + cp loge
T
T
sup
s
2
2
7.465 = 7.3954 + 2.1 loge
Tsup 2
()96.7 273+
465 3954
1
F −
HG
I
KJ
= loge
Tsup 2
369 7.
or loge
Tsup 2
369 7.
= 0.0033
Tsup 2
369 7.
= 1.0337 or Tsup 2 = 382 K