A method for operating an air-conditioning system for an aircraft including receiving an available power level from a control system of the aircraft, forwarding air from a first compressed air source to an aircraft cabin and forwarding air from a second compressed air source to the aircraft cabin if the available power level exceeds a threshold value.
Turbo air compressor
2015-12-08
Patent
Electronic Resource
English
Engineering Index Backfile | 1921
|Engineering Index Backfile | 1925
|Contra-flow turbo-compressor tests
TIBKAT | 1951
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