The invention relates to a landing gear, an aircraft including the landing gear and a method of distributing a landing gear load. An aircraft (2) has a landing gear (10) with a main support (20) supporting one or more wheels (76). The landing gear has at least two side struts (30, 32) through which landing gear loads can be propagated from the landing gear (10) to the body (3) of the aircraft (2). The side struts (30, 32) are attached at one end to the rotatable yoke (40) via a joint allowing relative movement between the side struts (30, 32) and the yoke (40) such that the yoke (40) is rotatable about a yoke axis (42). Rotation of the yoke (40) about the yoke axis (42) permitted by the joint may help distribute load between the two side struts (30, 32) and/or eliminate negative effects, e.g., caused by adverse tolerance superimposition during assembly.
本发明涉及起落架、包括起落架的飞行器和分配起落架载荷的方法。飞行器(2)具有起落架(10),该起落架具有支承一个或更多个轮(76)的主支承件(20)。该起落架具有至少两个侧撑杆(30、32),起落架载荷能够通过侧撑杆从起落架(10)传播至飞行器(2)的本体(3)。侧撑杆(30、32)在一个端部处经由接头附接至可旋转的轭(40),接头允许侧撑杆(30、32)与轭(40)之间的相对运动,使得轭(40)能够围绕轭轴线(42)旋转。所述接头所允许的轭(40)围绕轭轴线(42)的旋转可以有助于在两个侧撑杆(30、32)之间分配载荷以及/或者消除例如在组装期间由不利的公差叠加导致的负面影响。
Landing gear, aircraft comprising landing gear and method of distributing load of landing gear
起落架、包括起落架的飞行器和分配起落架载荷的方法
2023-11-21
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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