APU Flashcards
Frequently, an aircraft’s auxiliary power unit (APU) generator
Is identical to engine driven generators
Fuel is normally supplied to an APU from
The airplanes main fuel supply
An APU is usually rotated during start by
Electric starter
The function of an APU air inlet plenum is to
Stabilize the pressure of the air before it enters the compressor
When in operation, the speed of an APU
Remains at or near rated speed regardless of the load condition
Generally, when maximum APU shaft output power is being used in conjunction with pneumatic power
Pneumatic loading will be automatically modulated to maintain a safe EGT.
When necessary, APU engine cooling before shutdown may be accomplished by
Closing the bleed air valves
Usually, most of the load placed on an APU occurs when
Bleed air valves opened
Fuel scheduling during APU start and under varying pneumatic bleed and electrical loads is maintained
Automatically by the APU fuel control system
On APU’s equipped with a free turbine and load compressor, the primary function of the load
compressor is to
Provide bleed air for aircraft pneumatic systems