The invention provides movable aircraft main wheel mounting equipment. The mounting equipment comprises an inner bearing structure, an outer supporting structure and a lifting structure. The inner bearing structure comprises an inner main frame, a fork rod, a limiting groove and a self-locking disc. The inner main frame is a square-ring-shaped frame body, a left fork rod cavity and a right fork rod cavity are formed in a lower bottom ring body of the square-ring-shaped frame body, and openings of the fork rod cavities face the front face of the inner bearing structure. The number of the fork rods is two, and the two fork rods are inserted into the two fork rod cavities respectively. A through limiting groove is formed in the position, close to the back face of the inner bearing structure,in an inner cavity body of the fork rod cavity, and the self-locking disc is arranged on the back face of the inner bearing structure and penetrates through the limiting groove to be connected with the fork rod in the fork rod cavity. By means of the arrangement, the efficient, safe and high-quality installation requirements of the aircraft main wheel are met, the installation efficiency and installation safety of the aircraft main wheel are improved, and the product damage rate is reduced.
本发明提出了一种可移动式飞机主机轮安装设备,所述安装设备包括内承重结构、外支撑结构、升降结构;所述内承重结构包括内主框架、叉杆、限位槽、自锁盘;所述内主框架为方环形架体,所述方环形架体的下底环体设置左右两个叉杆腔,所述叉杆腔开口朝向内承重结构的正面;所述叉杆设置两根,两根叉杆分别插入在两个叉杆腔中;所述叉杆腔的内部腔体中靠近内承重结构背面的内部上设置贯穿的限位槽所述自锁盘设置在内承重结构的背面,且穿过限位槽与叉杆腔内的叉杆连接。本发明通过上述设置满足了飞机主机轮高效、安全、高质量安装需求,实现飞机主机轮安装效率、安装安全性的提高以及产品损坏率的降低。
Movable aircraft main wheel mounting equipment
一种可移动式飞机主机轮安装设备
2020-11-06
Patent
Elektronische Ressource
Chinesisch
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