An environmental control system (ECS) (200) for a multi-engine aircraft includes a controller (201) configured to switch the ECS between a plurality of operating modes. The plurality of operating modes includes a first operating mode configured to receive bleed air from each engine (209a, 209b, 209c, 209d) of the aircraft in a first environmental condition, wherein the pressure of the bleed air is about equal from each engine. The plurality of operating modes includes a second operating mode configured to receive bleed air from at least one engine of the aircraft in a second environmental condition, wherein the pressure of the bleed air is different between at least two engines.


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    Titel :

    ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT


    Weitere Titelangaben:

    UMGEBUNGSKÜHLSYSTEME FÜR FLUGZEUGE
    SYSTÈMES DE REFROIDISSEMENT ENVIRONNEMENTAL POUR AÉRONEF


    Beteiligte:
    SABNIS JAYANT (Autor:in) / BRUNO LOUIS J (Autor:in)

    Erscheinungsdatum :

    2019-07-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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