The invention discloses a cannon-launched coaxial unmanned rotorcraft airborne firework launching system which comprises a cannon-launched projectile-loaded platform, an unmanned aerial vehicle and a folding type guidable firework launching system. The folding type guidable firework launching system and the unmanned aerial vehicle form an integral system, the integral system is folded and arranged in a bullet cabin, after the unmanned aerial vehicle is launched to the air with a certain height through an air cannon, separation and shelling are completed, the unmanned aerial vehicle and the folding type guidable firework launching system are released, and the launching opportunity and launching direction of fireworks are changed by remotely regulating and controlling a remote control steering engine. Various different complex firework patterns are formed, and large firework show performance is completed. Compared with a traditional firework unmanned aerial vehicle, the flight stability of the unmanned aerial vehicle can be better guaranteed in the flight process of the unmanned aerial vehicle, and the performance safety of the firework unmanned aerial vehicle is improved.
本发明公开了一种炮射共轴旋翼无人机机载烟花发射系统,包括炮射弹载平台、无人机和折叠式可导向烟花发射系统;折叠式可导向烟花发射系统与无人机组成整体系统,折叠置于弹舱中,通过空气炮炮射升至一定高度的空中后完成分离脱壳释放无人机及折叠式可导向烟花发射系统,通过远程调控遥控舵机改变烟花的发射时机以及射向,组成各种不同的复杂的烟花图案,完成大型烟花秀表演。与传统烟花无人机相比,本发明能够地在无人机飞行过程中更好的保障无人机的飞行稳定性,提高烟花无人机表演的安全性。
Airborne firework launching system of cannon-launched coaxial unmanned rotorcraft
一种炮射共轴旋翼无人机机载烟花发射系统
13.05.2025
Patent
Elektronische Ressource
Chinesisch
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