To provide an auxiliary support system for a flap of an aircraft and a flap operating mechanism.SOLUTION: Described herein is an auxiliary support system 150 for a flap 126 coupled to a wing 114 of an aircraft. The auxiliary support system comprises a base 151 fixable relative to the wing. The auxiliary support system also comprises a first track engagement assembly 180A fixed to the base. The auxiliary support system further comprises a second track engagement assembly 180B fixed to the base. The auxiliary support system additionally comprises a track arm 172 attachable to the flap. The track arm comprises a first rail 174A movably engaged with the first track engagement assembly, and a second rail 174B movably engaged with the second track engagement assembly. The first rail is spaced apart from and non-parallel to the second rail.SELECTED DRAWING: Figure 7

    【課題】航空機のフラップの補助支持システム及びフラップ作動機構を提供する。【解決手段】航空機の翼114に連結されたフラップ126の補助支持システム150が開示されている。補助支持システムは、翼に固定可能なベース151を含む。補助支持システムは、さらに、ベースに固定された第1軌条係合部180Aを含む。補助支持システムは、さらに、ベースに固定された第2軌条係合部180Bを含む。加えて、補助支持システムは、フラップに取り付け可能な軌条アーム172を含む。軌条アームは、第1軌条係合部に対して移動可能に係合する第1レール174A、及び、第2軌条係合部に対して移動可能に係合する第2レール174Bを含む。第1レールは、第2レールに対して平行でない状態にて離間している。【選択図】図7


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    Title :

    AUXILIARY SUPPORT SYSTEM FOR FLAP OF AIRCRAFT WING


    Additional title:

    航空機翼のフラップ用補助支持システム


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

    Publication date :

    2019-10-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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