An aircraft air conditioning system (10) comprises an ambient air supply line (12) having a first end connected to an ambient air inlet (14) and a second end connected to a mixer (16) of the aircraft air conditioning system (10) so as to supply ambient air to the mixer (16). A first compressor (18) is arranged in the ambient air supply line (12) and is adapted to compress the ambient air flowing through the ambient air supply line (12). A bleed air supply line (52) allows a flow of bleed air bled off from an engine (54) or an auxiliary power unit therethrough. A bleed air turbine (60) is driven by the bleed air flowing through the bleed air supply line (52) and is coupled to the first compressor (18) so as to drive the first compressor (18).


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    Title :

    AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM


    Additional title:

    FLUGZEUGKLIMAANLAGENSYSTEM UND VERFAHREN FÜR DEN BETRIEB EINES FLUGZEUGKLIMAANLAGENSYSTEMS
    SYSTÈME DE CONDITIONNEMENT D'AIR POUR AÉRONEF ET PROCÉDÉ DE FONCTIONNEMENT D'UN SYSTÈME DE CONDITIONNEMENT D'AIR POUR AÉRONEF


    Contributors:

    Publication date :

    2019-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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