An Environmental Control System (ECS) 10 for an aircraft includes a ram air system having a ram inlet 12 and a ram outlet 28. The ECS includes a cabin air compressor motor, a diverter valve 20, and a dedicated outlet 60. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage, The dedicated outlet 60 is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet 28 is connected to the second diverter outlet in a ground mode of operation of the aircraft.


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    Titel :

    Enhanced motor cooling system and method


    Weitere Titelangaben:

    Verbessertes Motorkühlsystem und Verfahren
    Système de refroidissement de moteur amélioré et procédé


    Beteiligte:
    ARMY DONALD E (Autor:in) / MCCORD PATRICK (Autor:in) / SAUTRON DOMINIQUE P (Autor:in) / ZYWIAK THOMAS M (Autor:in)

    Erscheinungsdatum :

    2017-08-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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