The invention relates to the technical field of unmanned aerial vehicle launching structures, and discloses a brake for an unmanned aerial vehicle launching device and the unmanned aerial vehicle launching device. The brake comprises a brake body, a cutting blade and a friction plate, the brake body is arranged at a gun barrel outlet of a launching device, the cutting blade is arranged on the inner surface of the brake body, the friction plate is arranged on the outer surface of a mover of the launching device, and in the process that the mover and the unmanned aerial vehicle scratch out of the gun barrel, the cutting blade is arranged on the inner surface of the brake body. And the friction plate and the cutting blade interact to realize speed reduction of the rotor. Therefore, it can be guaranteed that the braking effects of all times of launching are basically the same, and then the effectiveness of separation of the rotor and the unmanned aerial vehicle is guaranteed.
本发明涉及无人机发射结构技术领域,公开了一种用于无人机发射装置的制动器及无人机发射装置。其中,该制动器包括制动器本体、切削片和摩擦片,所述制动器本体设置在发射装置的炮筒出口,所述切削片设置在所述制动器本体的内表面上,所述摩擦片设置在所述发射装置的动子外表面上,在所述动子和无人机划出炮筒的过程中,所述摩擦片与所述切削片相互作用实现所述动子减速。由此,可以保证各次发射的制动效果基本相同,进而保证了动子和无人机分离的有效性。
Brake for unmanned aerial vehicle launching device and unmanned aerial vehicle launching device
用于无人机发射装置的制动器及无人机发射装置
05.07.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
Launching device for launching unmanned aerial vehicle
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2024
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