Disclosed is a cooling circuit for cooling a heat load in an aircraft system, having: a compressor (155); a turbine (135) connected to the compressor by a shaft (160), the turbine configured to drive the compressor via the shaft when RAM air pressure into a turbine inlet is above a first threshold; and a motor (170) connected to the shaft configured to drive the compressor when RAM air pressure at the turbine inlet is below the first threshold to cause the compressor to draw air into the turbine inlet, through the turbine, a heat exchanger (104) in fluid communication with the heat load (102), the compressor, and out of a compressor outlet.


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    Titel :

    REVERSE BOOTSTRAP AIR CYCLE MACHINE


    Weitere Titelangaben:

    REVERSE-BOOTSTRAP-LUFTZYKLUSMASCHINE
    MACHINE À CYCLE D'AIR À AMORÇAGE INVERSE


    Beteiligte:
    DEFRANCESCO GREGORY L (Autor:in) / HO TONY (Autor:in)

    Erscheinungsdatum :

    21.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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