PROBLEM TO BE SOLVED: To provide a joint assembly used for joining a wing to an airframe of an aircraft.SOLUTION: A joint assembly 400 for an aircraft is provided. The joint assembly 400 includes: a single main fixture 402 including a first flange 410, a second flange 412, and a third flange; an outer girder component 404 being joined to the first flange 410 by using at least one attachment; an inner girder component 406 being joined to the second flange 412 by using at least one attachment; and a body rib 408 being joined to the third flange by using at least one attachment.SELECTED DRAWING: Figure 5

    【課題】翼を航空機の機体に結合するのに使用される継手アセンブリを提供する。【解決手段】航空機用の継手アセンブリ400が提供される。継手アセンブリ400は、第1フランジ410、第2フランジ412及び第3フランジを含む単一の主取付具402と、少なくとも1つの留具を用いて第1フランジ410に結合された外桁構成部品404と、少なくとも1つの留具を用いて第2フランジ412に結合された内桁構成部品406と、少なくとも1つの留具を用いて第3フランジに結合された本体リブ408とを含む。【選択図】図5


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    Title :

    JOINT ASSEMBLY AND ASSEMBLING METHOD THEREOF


    Additional title:

    継手アセンブリおよびその組立て方法



    Publication date :

    2018-07-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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