The invention belongs to the technical field of tilt-rotor aircrafts, and discloses a universal joint pin universal hinge propeller hub for a tilt-rotor aircraft and a working method of the universal joint pin universal hinge propeller hub. The universal joint pin universal hinge propeller hub for the tilt rotor aircraft comprises a universal joint pin universal hinge, a propeller hub elastic bearing and a variable pitch hinge, the universal joint pin universal hinge comprises a universal joint pin, a universal hinge lock yoke, a first connecting piece, a second connecting piece and a propeller hub shell trifurcate piece. The propeller hub elastic bearing is used for being fixedly installed on the propeller hub shell trifurcate piece, and the propeller hub elastic bearing is located above the cross shaft; the variable pitch hinge is used for being installed on three supporting arms of a propeller hub shell trifurcate piece of the universal joint pin universal hinge. The universal joint pin universal hinge propeller hub disclosed by the invention is particularly a semi-hinged propeller hub structure, can meet the requirements of aircrafts with larger take-off weight levels, and can prolong the service life of the aircrafts and improve the reliability of the aircrafts.
本发明属于倾转旋翼飞行器技术领域,公开了一种用于倾转旋翼飞行器的十字轴万向铰桨毂及其工作方法;所述用于倾转旋翼飞行器的十字轴万向铰桨毂包括:十字轴万向铰、桨毂弹性轴承和变距铰;其中,所述十字轴万向铰包括十字轴、万向铰锁轭、第一连接件、第二连接件和桨毂外壳三叉件;所述桨毂弹性轴承用于固定安装于所述桨毂外壳三叉件上,所述桨毂弹性轴承处于所述十字轴的上方;所述变距铰用于安装于所述十字轴万向铰的桨毂外壳三叉件的三个支臂上。本发明公开的十字轴万向铰桨毂具体是一种半铰接式桨毂构型,能够覆盖更大起飞重量级别飞行器的需求,可提高飞行器使用寿命和可靠性。
Universal joint pin universal hinge propeller hub for tilt-rotor aircraft and working method of universal joint pin universal hinge propeller hub
用于倾转旋翼飞行器的十字轴万向铰桨毂及其工作方法
2024-08-09
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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