Module 15 Gas Turbine Engine Practice Questions - Aircraft Maintenance Licence (AML) Category B Module 15 Gas Turbine Engine Exam

Which of the following correctly describes the thermodynamic stages of the Brayton cycle in a gas turbine engine?

Constant volume combustion followed by constant temperature expansion Adiabatic compression, isobaric combustion, adiabatic expansion, isobaric heat rejection Isochoric compression, isothermal expansion, isobaric combustion, adiabatic exhaust Isothermal compression, isobaric combustion, isothermal expansion, isochoric exhaust

Correct Answer:

Adiabatic compression, isobaric combustion, adiabatic expansion, isobaric heat rejection

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