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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    Title :

    CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN


    Additional title:

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


    Contributors:
    DIEP PAUL (author) / PHAM PHIYEN T (author)

    Publication date :

    2024-10-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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