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The A320neo also has a Honeywell 131-9A turboshaft engine located in the rear of the aircraft that is used as an Auxiliary Power Unit (APU).

The A320neo also has a Honeywell 131-9A turboshaft engine located in the rear of the aircraft that is used as an Auxiliary Power Unit (APU). The APU can supply up to

~~3.4\\\\times 10^(5)BT(U)/(h)r

to operate the aircraft's avionics, onboard lighting, galley appliances, and entertainment systems when the aircraft is parked at the gate (it can also draw bleed air from its own compressor to drive the environmental packs used for cabin heating and cooling).\ (a) Determine in kilowatts (kW) the shaft power required to run the PW1100g's fan and the electrical power supplied by the Honeywell APU.\ (b) If the APU operates for 30 minutes, what is the total energy provided by the

APU

, in MJ

image text in transcribed
The A320neo also has a Honeywell 131-9A turboshaft engine located in the rear of the aircraft that is used as an Auxiliary Power Unit (APU). The APU can supply up to 3.4105BTU/hr to operate the aircraft's avionics, onboard lighting, galley appliances, and entertainment systems when the aircraft is parked at the gate (it can also draw bleed air from its own compressor to drive the environmental packs used for cabin heating and cooling). (a) Determine in kilowatts ( kW ) the shaft power required to run the PW1100g's fan and the electrical power supplied by the Honeywell APU. (b) If the APU operates for 30 minutes, what is the total energy provided by the APU, in MJ

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