首页> 外国专利> Rotorcraft rotor blade, has fastener tongue with swiveling points at trailing edge, and tiltable trailing-edge flap with outer cage integrated to points, where flap pivots around virtual hinge axis extending along span of blade

Rotorcraft rotor blade, has fastener tongue with swiveling points at trailing edge, and tiltable trailing-edge flap with outer cage integrated to points, where flap pivots around virtual hinge axis extending along span of blade

机译:旋翼航空器旋翼桨叶,具有在后缘具有旋转点的紧固件舌片,以及可倾斜的后缘襟翼,其中外笼集成到各个点,襟翼围绕虚拟铰链轴线枢转,并沿着叶片的跨度延伸

摘要

The blade (1) has a tiltable trailing-edge flap (5) for pivoting around a virtual hinge axis (Y`) extending along a span of the blade and the flap (5). The flap (5) has two fastener ball joints (30), each provided with an inner cage (32), an outer cage (33) and a pin (31) integrated to the flap (5). The blade has a fastener tongue (20) with swiveling points (21) provided at its trailing edge (BF), where the outer cage is integrated to the points.
机译:叶片(1)具有可倾斜的后缘襟翼(5),该后缘襟翼用于绕虚拟的铰链轴线(Y′)枢转,该假想的铰链轴线沿叶片和襟翼(5)的跨度延伸。翼片(5)具有两个紧固件球窝接头(30),每个均具有内笼(32),外笼(33)和与翼片(5)成一体的销钉(31)。叶片具有在其后缘(BF)处设置有旋转点(21)的紧固件舌片(20),在该处,外笼被整合到这些点上。

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