A removable closure member is configured to close a female portion received in an external opening formed in the external surface of a nacelle for an aircraft engine. The female portion includes at least one air inlet opening. The closure member includes a base that forms the external contour of the member and that extends beyond the external opening of the nacelle so as to move into abutment against the external surface of the nacelle. The closure member further includes at least one resiliently deformable position retention member that projects from the base and is configured to be inserted into the air inlet opening.


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    Titel :

    REMOVABLE CLOSURE MEMBER FOR A FEMALE PORTION RECEIVED IN AN EXTERNAL OPENING OF AN AIRCRAFT ENGINE NACELLE


    Beteiligte:
    MERIEL OLIVIER (Autor:in) / LUCIENNE VIVIEN (Autor:in)

    Erscheinungsdatum :

    08.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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