ATPL: In a gas turbine engine, compressor blades, which are not rigidly fixed in position when the engine is stationary, take up a rigid position when the engine is running due to:

Home > Archivio Quiz di Esame > Quiz ATPL - Test di esame Airline Transport Pilot license > Aircraft General Knowledge - Airframe, Systems, Powerplant > In a gas turbine engine, compressor blades, which are not rigidly fixed in position when the engine is stationary, take up a rigid position when the engine is running due to:

Domanda 431, Aircraft General Knowledge - Airframe, Systems, Powerplant - ATPL - Airline Transport Pilot license

Oil Pressure.

The resultant of aerodynamic and centrifugal forces.

Blade creep.

Thermal Expansion.

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