The invention provides an unmanned aerial vehicle wing body quick dismounting and mounting mechanism and an unmanned aerial vehicle with the unmanned aerial vehicle, the unmanned aerial vehicle wing body quick dismounting and mounting mechanism comprises a fuselage joint assembly and a wing joint assembly, and the joint assembly comprises a fuselage joint unit, a first conical lock bolt, a second conical lock bolt, a first guide part, a second guide part and a first elastic element; the fuselage joint unit is provided with a positioning connecting piece through hole, a limiting groove, a first guide groove, a second guide groove, a first lock bolt through hole and a second lock bolt through hole, the joint assembly comprises a wing joint, a top block, a push rod, a deflector rod, a locking element and a pressure spring, and in a locking state, the first conical lock bolt is matched with the first conical groove, and the second conical lock bolt is matched with the second conical groove; the deflector rod is located in the deflector rod guide groove, and the locking element is matched with the limiting groove; and in the unlocking state, the first conical lock bolt is separated from the first conical groove, the second conical lock bolt is separated from the second conical groove, and the locking element is separated from the limiting groove. According to the technical scheme, the technical problem that in the prior art, a fixed wing is complex to disassemble and assemble is solved.
本发明提供了一种无人机翼身快速拆装机构及具有其的无人机,包括机身接头组件和机翼接头组件,接头组件包括机身接头单元、第一、第二锥形锁栓、第一、第二导向件和第一弹性元件,机身接头单元具有定位连接件通孔、限位槽、第一、第二导向槽、第一和第二锁栓通孔,接头组件包括机翼接头、顶块、推杆、拨杆、锁定元件和压簧,当处于锁定状态时,第一锥形锁栓与第一锥形槽配合,第二锥形锁栓与第二锥形槽配合,拨杆位于拨杆导向槽内,锁定元件与限位槽配合;当处于解锁状态时,第一锥形锁栓与第一锥形槽分离,第二锥形锁栓与第二锥形槽分离,锁定元件与限位槽分离。应用本发明的技术方案,以解决现有技术中固定翼机翼拆装复杂的技术问题。
Quick dismounting and mounting mechanism for wing body of unmanned aerial vehicle and unmanned aerial vehicle with same
无人机翼身快速拆装机构及具有其的无人机
2024-02-06
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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