The invention relates to a multi-rotor aircraft. The multi-rotor aircraft comprises a fuselage, a pod and a locking structure, the bottom of the fuselage is recessed to form a mounting groove, the pod can be slidably mounted in the mounting groove through the guide rail assembly in the first direction, the locking structure has a locking state and an unlocking state, when the pod is mounted in the mounting groove, the locking structure can be in the locking state so as to fix the pod in the mounting groove, and when the locking structure is in the unlocking state, the pod is locked in the mounting groove. The pod can be detached in a sliding mode relative to the mounting groove, and the locking structure can be switched from the locking state to the unlocking state by pressing the locking structure. Compared with the prior art, the multi-rotor aircraft has the advantage of being fast to disassemble and assemble, extra tools are not needed to unlock the locking structure, so that the pod is disassembled, the multi-rotor aircraft is very convenient to use, and during installation, only the pod needs to be installed in the installation groove in a sliding mode.
本发明涉及一种多旋翼飞行器,包括机身、吊舱以及锁定结构;机身底部凹陷形成有安装槽,吊舱通过导轨组件可沿第一方向滑动地安装到安装槽中,锁定结构具有锁定状态和解锁状态,当吊舱安装于安装槽中时,锁定结构可处于锁定状态以将吊舱固定在安装槽中,锁定结构处于解锁状态时,吊舱可相对安装槽滑动拆卸,通过按压锁定结构,可将锁定结构从锁定状态切换到解锁状态。本发明多旋翼飞行器具有快速拆装的特点,无需使用额外的工具对锁定结构进行解锁,从而将吊舱进行拆卸,使用起来十分方便,安装时,只需将吊舱滑动装入安装槽即可。
Multi-rotor aircraft
一种多旋翼飞行器
2025-03-28
Patent
Electronic Resource
Chinese