Dynamic load-bearing launcher for drones

Abstract

The invention discloses a dynamic load-bearing launching device for an unmanned aerial vehicle, belonging to the technical field of unmanned aerial vehicles, comprising a launching component, a load-bearing component, a shock absorbing component and a power mechanism. The launching part includes an ejection end, a pipe body, a loading and unloading end and an object to be launched. The load-bearing member includes a first support arm and a second support arm. The shock absorbing component includes a first limit rod, a second limit rod, a first elastic component and a second elastic component. The first elastic component is sleeved on the outside of the first limit rod, and the second elastic component is sleeved on the outside of the second limit rod. The power mechanism includes a first steering gear and a second steering gear. The first steering gear includes a first casing and a first rotating shaft; the second steering gear includes a second casing and a second rotating shaft. The invention achieves the technical effect that the drone can be shot at any time in various flight attitudes; the damage to the drone caused by the recoil force is reduced, the flying attitude of the drone is stabilized, and the technical effect of helping trapped persons to escape in time is facilitated.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a dynamic load-bearing launching device for unmanned aerial vehicles. Background technique [0002] Unmanned UAV, referred to as "UAV", is an unmanned UAV controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary UAV under radio remote control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. [0003] For the unmanned aerial vehicle, the unmanned aerial vehicle fuselage in the prior art is ...

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is that the UAV cannot shoot the glass doors and windows at any time in various flight attitudes; if the glass doors and windows are shot, the recoil force of the shooting will damage the UAV and interfere with the UAV's flight attitude , so that the UAV cannot help the trapped people to escape in time

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