Provided is an inlet bulkhead for large diameter aircraft engines. The inlet bulkhead, in certain examples, includes an annular body having an outer flange, an inner flange, and a web having a first side and an opposing second side. The web extends from the outer flange to the inner flange. The bulkhead also includes at least one annular stiffener disposed on the first side, and multiple radial stiffeners disposed on the first side, each of which extend from the outer flange to the inner flange. The annular and radial stiffeners may be integrally formed with the web.


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    Titel :

    INLET BULKHEADS FOR LARGE DIAMETER AIRCRAFT ENGINES


    Weitere Titelangaben:

    CLOISONS D`ENTREE POUR MOTEURS D`AERONEF DE GRAND DIAMETRE


    Beteiligte:
    WIJESINGHE JANAKA (Autor:in) / ROCHA ANDREW G (Autor:in) / ZIMNEY ERIC J (Autor:in)

    Erscheinungsdatum :

    2021-01-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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