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Rotor blade coupling device and rotor head for rotorcraft.

机译:旋翼飞机的旋翼桨叶耦合装置和旋翼头。

摘要

In a rotor blade coupling apparatus (2) for coupling to a rotor mast (9) to form a rotor head (1) of a rotorcraft, in particular a helicopter or helicopter, comprising a rotor head central piece (7), at least two on Rotorkopfzentralstück (7) attached to the rotor blade mounts (4) for receiving at least two in a rotor plane (RE) lying rotor blades (3), and at least one connecting means between adjacent rotor blade mounts (4), to a simplified structure of the rotor blade coupling apparatus (2) can be achieved, and the rotor blade coupling apparatus (2) to allow an agile control , This is achieved in that the rotor blade coupling apparatus (2) as the connecting means comprises at least one closed ring (10), said ring (10) arranged at least all rotor blade mounts (4), crossing in each case at least one connection location and all the rotor blade mounts (4) together indirectly connecting is.
机译:在用于连接至旋翼桅杆(9)以形成旋翼飞机,特别是直升飞机或直升飞机的旋翼飞机的旋翼头(1)的旋翼叶片联接装置(2)中,包括至少两个旋翼头中心件(7)。安装在转子叶片支座(4)上的Rotorkopfzentralstück(7)上,用于容纳至少两个位于转子平面(RE)上的转子叶片(3),以及在相邻转子叶片支座(4)之间的至少一个连接装置。转子叶片联接装置(2)的结构可以简化,并且转子叶片联接装置(2)可以进行灵活的控制。这通过如下方式实现:转子叶片联接装置(2)作为连接装置至少包括一个闭合的环(10),所述环(10)至少布置所有转子叶片座(4),在每种情况下都至少穿过一个连接位置,并且所有转子叶片座(4)间接地连接在一起。

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