【課題】様々な飛行状態における航空機の効率および性能を高めるために航空機の翼上で使用され得る揚力調整可能な揚力修正翼端を提供する。【解決手段】調整可能な揚力修正翼端500は、航空機のベースライン翼に取り付けられ、制御面506を含む水平部分502と、この水平部分に連結される垂直部分504とを備える。垂直部分は、水平部分に実質的に垂直であり得る軸を中心に移動する。制御面および垂直部分は、ともに調整されて、ある飛行状態で翼効率を高める。【選択図】図5

    An adjustable lift modification wingtip may be attached to a baseline wing of an aircraft. The adjustable lift modification wingtip may comprise a horizontal portion including a control surface and a vertical portion coupled to the horizontal portion. The vertical portion may move about an axis that may be substantially perpendicular to the horizontal portion. The control surface and the vertical portion may be adjusted in conjunction to increase wing efficiency at a flight condition.


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    Title :

    ADJUSTABLE LIFT MODIFICATION WINGTIP


    Additional title:

    調整可能な揚力修正翼端


    Contributors:

    Publication date :

    2015-08-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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