A method for operating an air-conditioning system (10) for an aircraft includes compressing ambient air (15) with a compressor (14;102) driven by a shaft (28;108) in communication with a motor (16;102) and a turbine (18;106). The method includes forwarding the compressed air to an aircraft cabin (20) for circulation and removing circulated compressed air from the aircraft cabin (20). The method also includes forwarding the circulated compressed air (20) to the turbine (18;106), depressurizing the circulated compressed air in the turbine (18;106) and capturing energy created by depressurizing the circulated compressed air.
Turbo air compressor with pressure recovery
Turboluftverdichter mit Energierückgewinnung
Turbocompresseur avec dispositif de récupération d'énergie
2021-06-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Engineering Index Backfile | 1921
|Engineering Index Backfile | 1925
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