A bogie beam for an aircraft landing gear assembly is provided. The bogie beam includes an elongated hub having a first end and a second end. The hub can be rotatably mounted to a shock strut of a landing gear assembly. The first leg extends radially from the first end of the hub in a first direction. The first leg has an inner side facing the second end of the hub and is configured to have a first wheel rotatably mounted to the inner side of the first leg about a first wheel axis. The second leg extends radially from the second end of the hub in a second direction and has an inner side facing the first end of the hub. The second leg is configured to have a second wheel rotatably mounted to an inner side of the second leg about a second wheel axis.
提供了一种用于飞行器起落架组件的转向架梁。转向架梁包括具有第一端和第二端的细长毂。该毂能够可旋转地安装到起落架组件的减震支柱。第一支腿从毂的第一端沿第一方向径向地延伸。第一支腿具有面向毂的第二端的内侧,并构造成具有第一轮,该第一轮围绕第一轮轴线可旋转地安装到第一支腿的内侧。第二支腿从毂的第二端沿第二方向径向地延伸,并具有面向毂的第一端的内侧。第二支腿构造成具有第二轮,该第二轮围绕第二轮轴线可旋转地安装到第二支腿的内侧。
Staggered wheel landing gear bogie beam
交错轮起落架转向架梁
25.04.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |