The aircraft engine can have a core gas path having a first combustor, a second gas path parallel to the core gas path, the second gas path having a second combustor, a turbine driven by the second gas path, a gearbox driven by the turbine, and a valve configured for selectively opening and closing the second gas path.


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    Titel :

    AIRCRAFT ENGINE AND METHOD OF OPERATING SAME


    Weitere Titelangaben:

    MOTEUR D`AERONEF ET SON PROCEDE DE FONCTIONNEMENT


    Beteiligte:

    Erscheinungsdatum :

    06.12.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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