560 ENGINEERING THERMODYNAMICSdharm
\M-therm\Th15-2.pm5(iv)Brake thermal efficiency :Brake thermal efficiency =W
hhfbrake
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
hhffindicated
1133−−=W
Windicated = 281 25
495 8.. = 0.567 or 56.7%. (Ans.)
Relative efficiency on the basis of brake work=W
hh
W
hhffindicated
()()1133−−=W
Wbrake =^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
Tsup
s2
2
7.465 = 7.3954 + 2.1 loge
Tsup 2
()96.7 273+465 3954
1F −
HGI
KJ
= logeTsup 2
369 7.
or logeTsup 2
369 7.
= 0.0033Tsup 2
369 7.= 1.0337 or Tsup 2 = 382 K