An aircraft including a flap support assembly for a flap support. An aircraft includes a fuselage comprising a pressure deck, where at least a portion the pressure deck is substantially horizontal. The aircraft further includes a wing extending from the fuselage, where the wing includes a leading edge and a trailing edge. The wing additionally includes a flap assembly on the trailing edge of the wing, where the flap assembly is configured to move between an extended position and a retracted position. The aircraft further includes a flap support coupled to the flap assembly comprising a plurality of load-bearing connection points, where at least one of the load-bearing connection points is coupled to the pressure deck.
Aircraft wing flap support
2022-02-22
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
FLAP SUPPORT FOR SUPPORTING FLAP OF WING FOR AIRCRAFT
Europäisches Patentamt | 2021
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