The invention discloses a wing and fuselage connecting mechanism and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The plurality of driving devices are respectively arranged at the end parts of a plurality of beams of the wing; the plurality of locking rods are respectively arranged at the end parts of the plurality of beams of the machine body and are respectively inserted into the middle parts of the driving devices corresponding to the locking rods, so that the driving devices lock the locking rods corresponding to the driving devices; one end of each locking device is fixed to the skin of the wing, the other end of each locking device is located in the middle of the corresponding driving device, and the locking devices are configured to lock the corresponding driving devices when the locking rods reach preset positions; the stretching piece is connected to the multiple locking devices. Therefore, according to the connecting mechanism for the wings and the fuselage, the wings and the fuselage can be quickly connected and locked, the unnecessary mounting space is reduced, and meanwhile, the mounting and dismounting time of the wings and the fuselage is shortened.
本申请公开了一种机翼与机身的连接机构及无人机,涉及无人机技术领域。多个驱动装置分别设置于机翼的多个梁的端部;多个锁定杆分别设置于机身的多个梁的端部,且被配置为分别插入与之对应的驱动装置的中部,以使驱动装置将与之对应的锁定杆锁定;多个锁紧装置的一端均固定于机翼的蒙皮,另一端位于与之对应的驱动装置的中部,被配置为在多个锁定杆到达预设位置时,锁定与之对应的驱动装置;拉伸件连接于多个锁紧装置。因此,本申请的机翼与机身的连接机构可以快速地将机翼与机身进行连接并锁定,减少不必要的安装空间,同时缩短机翼与机身安装与拆卸时间。
Wing and fuselage connecting mechanism and unmanned aerial vehicle
一种机翼与机身的连接机构及无人机
2024-07-30
Patent
Electronic Resource
Chinese
IPC: | B64U |
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