Catapult device for small unmanned aerial vehicle
A technology for small unmanned aerial vehicles and ejection devices, which can be applied to launch/drag transmission devices, unmanned aerial vehicles, motor vehicles, etc., and can solve the problems of incapable of ejecting mobile orbits, fixed position, reduced use value, and imperfect technology.
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[0017] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.
[0018] see figure 1 , figure 2 , the present invention provides a technical solution for a small unmanned aerial vehicle ejection device: its structure includes a fixing device 1, a rear drive motor 2, a rear connection block 3, a rear power connection block 4, anti-skid lines 5, an ejection moving track 6, and an ejection booster 7, baffle plate 8, front power connector 9, front connection block 10, rotating shaft 11, front drive motor 12, the front end of the rear drive motor 2 is connected to the inside of the rear connection block 3, and the front end of the rear connection block 3 is connected to the rear The power connection block 4 is internally mechanically connected, the side of the rear power connection block 4 is flexibly connected to...
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