- 2081 Baisakh · 10 marks
Gas turbine with 78% effective regenerator
Short answer
Find T2 and T4 using compressor and turbine isentropic efficiencies, then regenerator exit Tx = T2 + 0.78(T4 - T2). Net work is 29.32 kJ/kg and heat input is 248.27 kJ/kg. Thermal efficiency is 11.81%.
In a gas turbine, the compressor takes in air at a temperature of 15°C and compresses it to four times the initial pressure with an isentropic efficiency of 82%. The temperature at the inlet of the turbine is 600°C and the isentropic efficiency of the turbine is 70%. A regenerator having an effectiveness of 78% is also incorporated in the cycle. Determine the thermal efficiency of the cycle. Take cp = 1.005 kJ/kg K and γ = 1.4.
Data: K, , , K, , , kJ/kg K, ; .
+------ Regenerator ------+
| x y |
1 | 2 4 |
--> [C] --> [CC] --3--> [T] ----+
Compressor
Turbine
Regenerator
K K, so heat can be recovered:
Thermal efficiency
(Without the regenerator: kJ/kg, .)
Answer: Thermal efficiency of the cycle = 11.81 %.
✓ Answer checked by Claude Opus 5.5 (high effort)
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