To provide a spar for an airplane that improves manufacturing, reliability, and/or performance.SOLUTION: A spar 610 for a wing includes a monolithic structure 650 and a strut 652. The monolithic structure includes an upper chord, a lower chord, and a web 628 positioned between the upper chord and the lower chord. The strut 652, distinct and separate from the monolithic structure, is coupled to the monolithic structure between the upper chord and the lower chord and extends across the web.SELECTED DRAWING: Figure 6

    【課題】製造、信頼性及び/又は性能を改善する航空機のスパーを提供する。【解決手段】翼桁610は、モノリス構造650及びストラット652を含む。モノリス構造は、上部翼弦、下部翼弦、及び上部翼弦と下部翼弦との間に配置されたウェブ628を備える。モノリス構造とは別個で独立したストラット652は、上部翼弦と下部翼弦との間でモノリス構造に連結されており、ウェブにわたって延びている。【選択図】図6


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    Title :

    MONOLITHIC SPAR FOR WING


    Additional title:

    モノリス状翼桁


    Contributors:
    FRANK ABADI (author)

    Publication date :

    2020-04-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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