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.
CFRP FUSELAGE FRAME WITH SECUREMENT TO VERTICAL TAIL FIN
CHASSIS DE FUSELAGE DE RESINE POLYMERE EN FIBRE DE CARBONE ET FIXATION A LA DERIVE DE L'EMPENNAGE VERTICAL
2022-02-12
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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