An aircraft air conditioning system, powered solely using electrical energy, to draw bleed air from outside the aircraft and deliver conditioned air to the aircraft's interior, includes at most three motorized rotary machines, which include: independent first and second motorized turbocompressors, each turbocompressor includes a turbine compressor and an electric motor; and a motor compressor interconnected between the turbocompressors via an interconnection pipe. The motor compressor: generates a primary air flow, which drives a secondary air flow, allowing a breathing air flow to be cooled in a first operation phase, corresponding to a ground operation or at relatively low altitude and relatively low aircraft speed; be at shutdown or at low idle in a second phase of operation at relatively low altitude and relatively high aircraft speed; and, provide a top up breathing air flow in a third phase of operation at relatively high altitude and relatively high aircraft speed.


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    Titel :

    SYSTEME DE CONDITIONNEMENT D'AIR POUR AVION"PLUS ELECTRIQUE"


    Weitere Titelangaben:

    AIR CONDITIONING SYSTEM FOR A "MORE ELECTRIC" AIRPLANE
    KLIMAANLAGE FÜR EIN "MEHR ELEKTRISCHES FLUGZEUG"


    Beteiligte:
    GALZIN GUILLAUME (Autor:in) / GOMEZ VINCENT (Autor:in)

    Erscheinungsdatum :

    29.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

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



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