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DEVICE FOR INCREASING LIFT FORCE, WING AND DEVICE FOR REDUCING NOISE USED WITH DEVICE FOR INCREASING LIFT FORCE

机译:提升力的装置,机翼以及用于降低提升力的装置的降噪装置

摘要

1. A device for increasing the lift, containing: the main element of the flap, installed with the possibility of releasing and retracting relative to the main wing; and a protruding member having a smooth contour and located near at least one end portion of a positive pressure surface of the flap main member, projecting outwardly from the flap main member. The apparatus of claim 1, wherein said protruding element extends along an end portion of the flap main element, the leading edge and trailing edge end portions of the protruding element being narrower in the direction of span of the flap main element compared to the substantially central portion of the protruding element. ... The apparatus of claim 1, wherein the projecting element extends along an end portion of the flap main element, the length of the projecting element in the direction of span of the flap main element being substantially constant. A wing containing: a main wing; and a device for increasing lift according to any one of claims 1 to 3, installed with the possibility of release and retract relative to the trailing edge of the main wing. A noise reduction device comprising: a detachable main element adapted to be attached to the end portion of the main flap element and detachable from the end portion of the main flap element, which is retractable and retractable relative to the main wing; and a protruding element having a smooth contour and protruding from the surface of the removable main element on the side of the positive pressure surface of the main element
机译:1.一种增加升力的装置,包括:襟翼的主要元件,安装成可能相对于主翼释放和缩回;突出部件具有平滑的轮廓,并位于挡板主体的正压表面的至少一个端部附近,并且从挡板主体向外突出。 2.根据权利要求1所述的设备,其中,所述突出元件沿着所述襟翼主元件的端部延伸,与所述大致中央部相比,所述突出元件的前缘和后缘端部在所述襟翼主元件的跨度方向上更窄。突出元件的一部分。 2.根据权利要求1所述的设备,其中,所述突出元件沿着所述襟翼主元件的端部延伸,所述突出元件在所述襟翼主元件的跨度方向上的长度基本恒定。机翼,机翼: 4.根据权利要求1至3中任一项所述的用于增加升力的装置,其安装成相对于所述主翼的后缘可释放和缩回。一种降噪装置,包括:可拆卸的主元件,其适于附接到所述主襟翼元件的端部并且可从所述主襟翼元件的端部拆卸,并且相对于所述主翼可伸缩。突出元件具有平滑的轮廓,并且从可移除主元件的在主元件的正压力表面一侧上的表面突出。

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