Aircraft wing and wing parts movable adjacent to the aircraft wing
    43.
    发明授权
    Aircraft wing and wing parts movable adjacent to the aircraft wing 有权
    飞机机翼和机翼部件可在飞机机翼附近移动

    公开(公告)号:US06910662B1

    公开(公告)日:2005-06-28

    申请号:US09959707

    申请日:2000-05-02

    CPC classification number: B64B1/20 B64C3/48 Y02T50/14

    Abstract: Wing parts (20, 21) which influence the lift of aircraft wings (1), especially wings (1) with a cross section and an angle of attack which is suitable for high-speed flight, which parts can be moved out of an aerodynamically inactive servicing position within the aircraft fuselage (30) or out of chambers (40) mounted on the wings (1) into an aerodynamically efficient active position and from the active position back into the servicing position, are assigned to the wings (1). These wing parts (20, 21) in their active position are located on the top (3) and optionally also on the bottom (4) of the wings (1) and are shaped for example such that the wing parts (21) located in their active position on the bottom (4) of the wings (1) jointly with the wing parts (20) located in their active position on the top (3) of the wings (1) increase the lift and optionally at the same time change the angle of attack of the wing.

    Abstract translation: 影响飞机机翼(1)的升力的翼部件(20,21),特别是适用于高速飞行的横截面和迎角的翼(1),这些部件可以从空气动力学中移出 将安装在机翼(1)上的飞行器机身(30)内或室外(40)内的不正常的维修位置分配成空气动力学有效的主动位置并从主动位置返回维修位置。 这些翼部件(20,21)处于其主动位置,位于机翼(1)的顶部(3)上并且任选地位于底部(4)上,并且成形为例如使翼部件(21)位于 它们与翼(1)的底部(4)的主动位置与位于机翼(1)的顶部(3)上的主动位置的翼部件(20)共同增加升力并且可选地同时改变 机翼的攻角。

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