The invention refers to an aircraft comprising a bleed supply architecture (1), the aircraft having a nose section, a central section, and a rear section, and comprising a pneumatic system (2) for supplying compressed bleed air to the different aircraft systems, a bleed supply for providing bleed air to the pneumatic system (2), and an auxiliary power unit (4). The aircraft additionally comprises an electric powered load compressor (5) coupled to the pneumatic system (2) for providing bleed air to said pneumatic system (2). The auxiliary power unit (4) is adapted for feeding electric power to the load compressor (5). The load compressor (5) and the pneumatic system (2) are installed at the same central section of the aircraft to reduce pressure losses.


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    Title :

    AIRCRAFT WITH A BLEED SUPPLY HYBRID ARCHITECTURE


    Additional title:

    FLUGZEUG MIT HYBRIDER DRUCKLUFTVERSORGUNG
    AÉRONEF AVEC UNE ARCHITECTURE HYBRIDE D'ALIMENTATION D'AIR PRESSURISÉ



    Publication date :

    2017-06-28


    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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