An aircraft air conditioning device provided in an aircraft includes: a plurality of base units (U1 to U6) each of which is provided with two electric compressors (1, 3, 4, 6) connected in series to an air flow path; a temperature controller (A) which is configured to adjust a temperature of air discharged from a compressor (4) of the two electric compressors; and a control device (S) which is configured to control the plurality of base units (U1 to U6) and the temperature controller (A) and each of the plurality of base units (U1 to U6) is configured to supply compressed air discharged from the temperature controller (A) to an air-conditioned space (X) as conditioned air.


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    Title :

    AIRCRAFT AIR CONDITIONING DEVICE


    Additional title:

    FLUGZEUGKLIMAANLAGE
    DISPOSITIF DE CLIMATISATION D'AÉRONEF


    Contributors:

    Publication date :

    2024-05-22


    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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