Described herein is an auxiliary support system for a flap coupled to a wing of an aircraft. The auxiliary support system comprises a base fixable relative to the wing. The auxiliary support system also comprises a first track engagement assembly fixed to the base. The auxiliary support system further comprises a second track engagement assembly fixed to the base. The auxiliary support system additionally comprises a track arm attachable to the flap and comprising a first rail, movably engaged with the first track engagement assembly, and a second rail, movably engaged with the second track engagement assembly. The first rail is spaced apart from and non-parallel to the second rail.
AUXILIARY SUPPORT SYSTEM FOR A FLAP OF AN AIRCRAFT WING
19.09.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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