To provide foldable wings to enable an aircraft to fit within a taxiway and/or a gate.SOLUTION: An aircraft includes a fixed wing portion 108, a foldable wing tip 106, and a hinge interface 112 to pivotally couple the foldable wing tip 106 and the fixed wing portion 108. The hinge interface 112 has a first hinge defining a hinge axis 110 that is substantially parallel to a fuselage centerline. The first hinge has a first dimension in a spanwise direction and a second dimension in a chordwise direction. The first dimension is greater than the second dimension.SELECTED DRAWING: Figure 4

    【課題】航空機が誘導路及び/又はゲートの範囲内で適合することを可能とするために、折り畳みが可能な翼を提供する。【解決手段】航空機は、固定翼部分108と、折り畳み可能翼端106と、折り畳み可能翼端106と固定翼部分108とを枢動自在に結合するヒンジ接合部112と、を含む。ヒンジ接合部112は、第1のヒンジを有し、胴体中心線に対して実質的に平行なヒンジ軸110を定める。第1のヒンジは、翼幅方向において第1の寸法を有し、かつ翼弦長方向において第2の寸法を有する。第1の寸法は、第2の寸法よりも大きい。【選択図】図4


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    Title :

    AIRCRAFT HAVING FOLDABLE WINGS


    Additional title:

    折り畳み可能翼を有する航空機


    Contributors:

    Publication date :

    2020-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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