Disclosed is an air cycle machine (ACM) having: a turbine (210); a compressor (200); a compressor shaft (255) connected to the compressor and configured to receive rotational energy from a gearbox (75); and a turbine shaft (260) connected to the turbine and configured to provide rotational energy to the gearbox; wherein the turbine shaft and the compressor shaft operate at different rotational speeds.


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    Title :

    AIRCRAFT SYSTEM


    Additional title:

    LUFTFAHRZEUGSYSTEM
    SYSTÈME D'AVION


    Contributors:

    Publication date :

    2023-04-26


    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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