Mini-spoilers for enhancing the effectiveness of lateral-control surfaces of aircraft wings are described. An example aircraft includes a wing (800), a lateral-control surface in the form of an aileron (132), a flaperon or a spoiler, as well as a mini-spoiler (808). The lateral-control surface is movably coupled to the wing. The lateral-control surface is movable between a neutral position, a first upward deflected position, and a second upward deflected position extending beyond the first upward deflected position. The mini-spoiler is located on or forward of the lateral-control surface. The mini-spoiler is movable between a retracted position and a deployed position. The mini-spoiler is configured to be moved from the retracted position to the deployed position based on the lateral-control surface being moved from the neutral position to or toward the first upward deflected position.

    描述了用于增强飞机机翼的侧向操纵面的效能的微型扰流翼。示例飞机包括机翼、侧向操纵面和微型扰流翼。侧向操纵面可移动地联接至机翼。侧向操纵面可在中立位置、第一向上偏转位置和延伸超过第一向上偏转位置的第二向上偏转位置之间移动。微型扰流翼位于侧向操纵面上或前方。微型扰流翼可在缩回位置和展开位置之间移动。微型扰流翼被配置为基于侧向操纵面从中立位置移动至第一向上偏转位置或朝向第一向上偏转位置移动而从缩回位置移动至展开位置。


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    Titel :

    MINI-SPOILERS FOR ENHANCING THE EFFECTIVENESS OF LATERAL-CONTROL SURFACES OF AIRCRAFT WINGS


    Weitere Titelangaben:

    用于增强飞机机翼的侧向操纵面的效能的微型扰流翼


    Beteiligte:

    Erscheinungsdatum :

    2021-05-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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