To solve the problem of a landing gear often subjected to extremely high loads, especially in landing and braking, for instance.SOLUTION: Aircraft main landing gear drag brace backup fitting assemblies and related methods are described herein. An example aircraft wing disclosed herein includes a rear spar having a rear side and a front side opposite the rear side, a side-of-body rib coupled to the rear spar, a rib post disposed on the front side of the rear spar, where the rib post is to couple a second rib to the rear spar, a side-of-body fitting coupled to the side-of-body rib, an intercostal member coupled between the side-of-body fitting and the rib post, and a drag brace fitting disposed on the rear side of the rear spar. The drag brace fitting is coupled to the rib post and the side-of-body fitting via a first plurality of fasteners extending through the rear spar.SELECTED DRAWING: Figure 2

    【課題】ランディングギアは、たとえば、特に着陸時および制動時にきわめて高い荷重を受けることが多い。【解決手段】航空機のメインランディングギアのドラッグブレースのバックアップ取付具アセンブリおよび関連方法が本出願で説明されている。本出願で開示されている航空機翼例は、後側と後側の反対側の前側とを有する後桁と、後桁に接続される胴体側リブと、後桁の前側に配置されるリブ支柱であって、リブ支柱は後桁に第2のリブを接続する、リブ支柱と、胴体側リブに接続される胴体側取付具と、胴体側取付具とリブ支柱との間で接続されるインタコスタル部材と、後桁の後側に配置されるドラッグブレース取付具とを含む。ドラッグブレース取付具はリブ支柱および胴体側取付具に、後桁を貫通して延伸する第1の複数の締め具により接続される。【選択図】図2


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    Title :

    AIRCRAFT MAIN LANDING GEAR DRAG BRACE BACKUP FITTING ASSEMBLIES AND RELATED METHODS


    Additional title:

    航空機のメインランディングギアのドラッグブレースのバックアップ取付具アセンブリおよび関連方法



    Publication date :

    2020-10-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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