The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle launching device which comprises a launching cylinder, and a miniature gas generator is detachably connected into the tail end of the launching cylinder; the projectile support is arranged in the launch canister in a clearance fit mode, one end of the projectile support abuts against the micro gas generator, and the other end of the projectile support is used for abutting against the canister launch type unmanned aerial vehicle; the folding type supporting assembly is arranged on the launching cylinder, and the folding type supporting assembly is attached to the launching cylinder after being folded; the guide assembly is arranged at the head end of the launching cylinder. According to the unmanned aerial vehicle, the miniature gas generator which instantly generates one-way high-pressure gas is matched with the missile support, catapult-assisted take-off power is provided for the barrel-shooting type unmanned aerial vehicle, and the barrel-shooting type unmanned aerial vehicle is guided and limited through the guide assembly, so that the barrel-shooting type unmanned aerial vehicle cannot roll and/or deflect at the launching moment; the launching device for launching the unmanned aerial vehicle is further optimized, and the requirements for portability and launching guiding are met.
本发明涉及无人机技术领域,具体涉及一种无人机发射用发射装置,包括发射筒,微型气体发生器可拆卸连接在发射筒的尾端内;弹托间隙配合设置在发射筒内,所述弹托的一端与所述微型气体发生器抵靠,所述弹托的另一端用于与筒射式无人机抵靠;折叠式支撑组件设置在所述发射筒上,所述折叠式支撑组件折叠后与所述发射筒贴合;导向组件设置在所述发射筒的首端。本发明,通过瞬间产生单向的高压气体的微型气体发生器配合弹托,向筒射式无人机提供弹射起飞的动力,并通过导向组件对筒射式无人机进行导向限位,使得筒射式无人机在发射瞬间不能够进行翻滚和/或偏转,对无人机发射用发射装置进一步进行了优化,满足了便携性和发射导向的需求。
Launching device for launching unmanned aerial vehicle
一种无人机发射用发射装置
2024-07-16
Patent
Electronic Resource
Chinese
IPC: | B64U |
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