The invention relates to the technical field of moving structures, and discloses an integral moving structure of a helicopter, which comprises a first baffle plate, a connecting mechanism, a second baffle plate and a skid tube, the connecting mechanism is arranged on the first baffle plate, the first baffle plate is arranged on the skid tube, the second baffle plate is arranged on the skid tube, and the connecting mechanism is arranged on the second baffle plate. A carrying wheel is arranged on the back face of the first baffle, the connecting mechanism comprises a core shaft and a first positioning hole, and the core shaft is inserted into the first positioning hole. According to the integral moving structure of the helicopter, after the core shaft is fixed to the first baffle through the fixing rivet, the core shaft is fixed to the skid pipe through the locking bolt and the locking nut to form a component, the connecting shaft is inserted into the core shaft, and rapid mounting of a carrying wheel is achieved; according to the invention, short-distance transition of the helicopter can be realized, the phenomenon that the helicopter is inconvenient to move when a skid tubular undercarriage is adopted is avoided, and the limitation of a site on the movement of the helicopter is reduced.
本发明涉及移动结构技术领域,且公开了一种直升机的整体移动结构,包括第一挡板、连接机构、第二挡板和滑撬管,所述连接机构设置在第一挡板上,所述第一挡板设置在滑撬管上,所述第二挡板设置在滑撬管上,所述第一挡板的背面设置有搬运轮,所述连接机构包括芯轴和第一定位孔,所述芯轴插接在第一定位孔的内部。该一种直升机的整体移动结构,通过固定铆钉将芯轴固定在第一挡板上后,在使用锁紧螺栓和锁紧螺母固定在滑撬管上组成部件,其将连接轴插接到芯轴的内部,实现搬运轮的快速安装,通过对该装置增加搬运轮后,可实现直升机短距离的转场,避免了采用滑橇管式起落架时,直升机不方便进行移动的现象出现,降低了场地对直升机移动的限制。
Integral moving structure of helicopter
一种直升机的整体移动结构
2023-07-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Integral Helicopter Cargo Restraint System
NTIS | 1969
|Helicopter Operations to Moving Decks
British Library Conference Proceedings | 2001
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