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

机译:用于提高飞机翼横向控制表面的有效性的迷你扰流板

摘要

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.
机译:描述了用于增强飞机翼的侧向控制表面的有效性的迷你扰流板。示例飞行器包括机翼(800),横向控制表面,横向控制表面,横向控制表面(132),FLAPERON或扰流板,以及迷你扰流板(808)。横向控制表面可移动地连接到机翼。横向控制表面可在空档位置,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。迷你扰流板位于侧向控制表面上或前方。迷你扰流板可在缩回位置和展开位置之间移动。迷你扰流板构造成基于从中立位置移动到或朝向第一向上偏转位置的横向控制表面从缩回位置移动到展开位置。

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