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.
CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN
CFRP-RUMPFRAHMEN MIT SICHERUNG AN VERTIKALES LEITWERK
CADRE DE FUSELAGE EN POLYMÈRE À RENFORT FIBRE DE CARBONE AVEC FIXATION SUR DÉRIVE VERTICALE
2022-02-16
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN
Europäisches Patentamt | 2022
|CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN
Europäisches Patentamt | 2022
|CFRP fuselage structures - postbuckling permitted
Online Contents | 2001
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