An aircraft propulsion system (20) includes a gas turbine engine; an environmental control system (ECS) (22); and a bleed flowpath (600) from the gas turbine engine through the ECS (22). A turbine (28) is along the bleed flowpath (600) and a propulsion fan (26) is mechanically coupled to the turbine (28) to be driven by the turbine (28).


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    Title :

    ENVIRONMENTAL CONTROL SYSTEMS


    Additional title:

    KLIMAREGELUNGSSYSTEME
    SYSTÈMES DE COMMANDE ENVIRONNEMENTALE


    Contributors:

    Publication date :

    2023-08-23


    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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