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
HILFSTRÄGERSYSTEM FÜR EINE KLAPPE EINES FLUGZEUGFLÜGELS
SYSTÈME DE SUPPORT AUXILIAIRE POUR UN VOLET D'AILE D'AÉRONEF
2020-09-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |