GATE ME 2024 Set 1 — Question 45
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Thermodynamics → Power Cycles → Brayton Cycle
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Question
Consider an air-standard Brayton cycle with adiabatic compressor and turbine, and a regenerator, as shown in the figure. Air enters the compressor at 100 kPa and 300 K and exits the compressor at 600 kPa and 550 K. The air exits the combustion chamber at 1250 K and exits the adiabatic turbine at 100 kPa and 800 K. The exhaust air from the turbine is used to preheat the air in the regenerator. The exhaust air exits the regenerator (state 6) at 600 K. There is no pressure drop across the regenerator and the combustion chamber. Also, there is no heat loss from the regenerator to the surroundings. The ratio of specific heats at constant pressure and volume is . The thermal efficiency of the cycle is _________ % (answer in integer).

Correct answer
40 to 40
Solution
Given state points:
1: Compressor inlet ( K)
2: Compressor outlet ( K)
3: Regenerator outlet (air side)
4: Combustion chamber outlet ( K)
5: Turbine outlet ( K)
6: Regenerator outlet (gas side) ( K)Work done by compressor:
Work done by turbine:
Net work output: In the regenerator, heat lost by hot gas = heat gained by cold air (since no heat loss to surroundings):
KHeat input in combustion chamber: Thermal efficiency: .
1: Compressor inlet ( K)
2: Compressor outlet ( K)
3: Regenerator outlet (air side)
4: Combustion chamber outlet ( K)
5: Turbine outlet ( K)
6: Regenerator outlet (gas side) ( K)Work done by compressor:
Work done by turbine:
Net work output: In the regenerator, heat lost by hot gas = heat gained by cold air (since no heat loss to surroundings):
KHeat input in combustion chamber: Thermal efficiency: .
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