首页> 外国专利> Main rotor blade for rotorcraft, has linear type electromagnetic actuator arranged in blade and permitting trailing edge tiltable flap to pivot about virtual hinge axis, where shaft of flap extends perpendicularly to hinge axis

Main rotor blade for rotorcraft, has linear type electromagnetic actuator arranged in blade and permitting trailing edge tiltable flap to pivot about virtual hinge axis, where shaft of flap extends perpendicularly to hinge axis

机译:用于旋翼飞机的主旋翼桨叶,具有线性电磁致动器,布置在桨叶中,并允许后缘可倾斜襟翼绕虚拟铰链轴枢转,其中襟翼轴垂直于铰链轴延伸

摘要

The blade has a trailing edge tiltable flap (5) pivoting about a virtual hinge axis (Y`) extending along a span of the blade (1) and the flap. The flap is provided with a main ball joint (30) having an inner cage (32), an outer cage (33) and a shaft (31) secured to the flap, where a front portion (33`) of the outer cage is connected to an end of a linear type electromagnetic actuator (10) via a single bent connecting rod (46), The actuator is arranged in the blade and permits the flap to pivot about the axis, where the shaft extends perpendicularly to the axis about which the flap pivots.
机译:叶片具有后缘可倾斜的翼片(5),该翼片可绕虚拟的铰链轴线(Y′)枢转,该虚拟的铰链轴线沿叶片(1)和翼片的跨度延伸。襟翼设置有主球窝接头(30),该主球窝接头(30)具有内部保持架(32),外部保持架(33)和固定至襟翼的轴(31),其中,外部保持架的前部(33`)位于其中。通过单个弯曲的连杆(46)连接到线性电磁致动器(10)的一端,该致动器设置在叶片中,并允许风门片绕轴​​枢转,其中轴垂直于该轴延伸襟翼旋转。

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