A securement assembly for securing a vertical tail fin assembly to an aircraft includes a first lug member secured to the vertical tail fin assembly. The securement assembly further includes a first clevis member. The first clevis member includes a first end portion of the first clevis member is engaged to the first lug member. A second end portion of the first clevis member is secured to a first fuselage frame constructed of a composite material with a first fastener 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:

    CHASSIS DE FUSELAGE DE RESINE POLYMERE EN FIBRE DE CARBONE ET FIXATION A LA DERIVE DE L'EMPENNAGE VERTICAL


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

    Publication date :

    2022-02-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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