A securement assembly (24) for securing a vertical tail fin assembly (16) to an aircraft includes a first lug member (46) secured to the vertical tail fin assembly. The securement assembly further includes a first clevis member (52). The first clevis member includes a first end portion of the first clevis member which is engaged to the first lug member. A second end portion of the first clevis member is secured to a first fuselage frame (20a) constructed of a composite material with a first fastener (70) which extends through the second end portion and the first fuselage frame in a first direction transverse to the first fuselage frame.


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    Titel :

    CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN


    Weitere Titelangaben:

    CFRP-RUMPFRAHMEN MIT SICHERUNG AN VERTIKALES LEITWERK
    CADRE DE FUSELAGE EN POLYMÈRE À RENFORT FIBRE DE CARBONE AVEC FIXATION SUR DÉRIVE VERTICALE


    Beteiligte:
    DIEP PAUL (Autor:in) / PHAM PHIYEN T (Autor:in)

    Erscheinungsdatum :

    2022-02-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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