According to the cable assembly structure for the aircraft landing gear, the two ends of an internal connecting cable are connected with a first connector and a second connector respectively, the tail of the first connector is provided with a first tail accessory, the tail of the second connector is provided with a second tail accessory, the internal connecting cable is sleeved with multiple sections of hard pipes, and the multiple sections of hard pipes are connected through second pipe joints; the internal connection cable close to the second connector is sleeved with a second hose, the second hose is arranged in the via hole lining in a penetrating mode, and the internal connection cable between the second hose and the second tail accessory is sleeved with a cable protection structure; the two ends of the fixing structure formed by connecting the multiple hard pipes are connected with the corresponding first hoses arranged on the internal connecting cable in a sleeving mode through the corresponding first pipe joints, the first hose close to the first connector is connected with the first tail accessory, and the first hose close to the second connector is connected with the second hose through the third pipe joint. The wire harness is protected to work normally, reliably and safely in a complex environment, and meanwhile the weight requirement is met.
一种飞机起落架用线缆组件结构,内部连接电缆的两端分别连接第一连接器、第二连接器,所述第一连接器尾部设置第一尾附件,第二连接器尾部设置第二尾附件,内部连接电缆上套设多段硬管,多段硬管之间通过第二管接头连接;靠近第二连接器的内部连接电缆上套设第二软管,第二软管穿设在过孔衬套内,第二软管与第二尾附件之间的内部连接电缆套设电缆防护结构;多段硬管连接形成的固定结构两端均通过对应的第一管接头与套设在内部连接电缆上的对应的第一软管连接,靠近第一连接器的第一软管与第一尾附件连接,靠近第二连接器的第一软管通过第三管接头与第二软管连接。本发明保护线束使其在复杂的环境中正常可靠安全工作,同时满足重量要求。
Cable assembly structure for aircraft landing gear
一种飞机起落架用线缆组件结构
2024-03-22
Patent
Electronic Resource
Chinese