An integrated electronic engine control and environmental control system bleed control apparatus for use with an aircraft engine. The apparatus comprises an electronic engine controller (18), an environmental control system bleed controller (30) for controlling a flow of bleed air from the aircraft engine (12) to an environmental control system (28) located in an aircraft fuselage (14), and a housing (34) for mounting on or near the aircraft engine (12). The housing (34) contains both the electronic engine controller (18) and the environmental control system bleed controller (30).


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    Title :

    Integrated bleed and engine controller


    Additional title:

    Integrierte Ablauf- und Motorsteuerung
    Contrôleur de purge et moteur intégré


    Contributors:

    Publication date :

    2019-06-05


    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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