An aircraft cabin blower system (100) comprising: a transmission (110) for receiving mechanical power from a gas turbine engine; and a cabin blower compressor (102), an output of the transmission (110) being configured to drive the cabin blower compressor (102); wherein the transmission (110) has a variable gear ratio and the cabin blower compressor (102) has a variable geometry, wherein variation of the gear ratio and the geometry provides a variable output of the cabin blower compressor (102).


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    Title :

    CABIN BLOWER SYSTEM


    Additional title:

    KABINENGEBLÄSESYSTEM
    SYSTÈME DE VENTILATEUR DE CABINE


    Contributors:

    Publication date :

    2020-05-27


    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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