The invention discloses a self-locking type unmanned aerial vehicle hinged arm which at least comprises a longitudinal middle shaft, a detachable side arm, movable side arms and a radial lock body. Each hinged side arm comprises a hollow shell-shaped middle shell, and further comprises an external lantern ring, an internal mandrel and a side arm body. The radial lock body comprises an input assembly, a cone pulley assembly, a worm assembly, a worm gear assembly and an elastic lock cylinder. The self-locking type unmanned aerial vehicle hinged arm further comprises an axial lock body, a telescopic lock head and an adjusting assembly.
本申请公开一种自锁式无人机铰接臂,至少包括:纵置中轴、可拆侧臂、活动侧臂、径向锁体。所述铰接侧臂包括空心壳体状的中置壳体,还包括外置套环、内置芯轴、侧臂本体;所述径向锁体包括输入组件、锥轮组件、蜗杆组件、蜗轮组件、弹性锁芯。还包括轴向锁体、伸缩锁头、调节组件。
Pre-adjusting method of self-locking type unmanned aerial vehicle hinged arm
一种自锁式无人机铰接臂的预调节方法
2020-12-08
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Angle adjusting method of self-locking unmanned aerial vehicle articulated arm
European Patent Office | 2020
Unmanned aerial vehicle wing locking device and unmanned aerial vehicle
European Patent Office | 2022
|Vehicle-mounted unmanned aerial vehicle self-adjusting charging platform
European Patent Office | 2025
|