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


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    Titel :

    Environmental control systems


    Beteiligte:

    Erscheinungsdatum :

    2024-02-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ENVIRONMENTAL CONTROL SYSTEMS

    RETERSDORF ALAN F | Europäisches Patentamt | 2023

    Freier Zugriff


    Environmental Control Systems

    RETERSDORF ALAN F | Europäisches Patentamt | 2023

    Freier Zugriff

    Environmental control systems

    Hrach, F. | NTRS | 1982


    Environmental Control Systems

    Rosenbush, F. M. | NTRS | 1982