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.


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    Title :

    AUXILIARY SUPPORT SYSTEM FOR A FLAP OF AN AIRCRAFT WING


    Additional title:

    HILFSTRÄGERSYSTEM FÜR EINE KLAPPE EINES FLUGZEUGFLÜGELS
    SYSTÈME DE SUPPORT AUXILIAIRE POUR UN VOLET D'AILE D'AÉRONEF


    Contributors:
    BOWERS BRET A (author) / ISIC MIRELA (author)

    Publication date :

    2020-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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