Independent suspension damping device of nozzle for unmanned aerial vehicle
A technology of independent suspension and shock-absorbing devices, which is applied to unmanned aircraft, devices for catching or killing insects, launching devices, etc. It can solve the problems that the landing gear cannot be retracted, the aircraft is lost, and it is easy to trip over other things.
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[0031] 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.
[0032] see Figure 1-Figure 8, the present invention provides a technical scheme of an independent suspension damping device for a nozzle of a drone: its structure includes a fixed mounting plate 1, a main shaft 2, a fixed base 3, a support arm 4, a spiral wing motion mechanism 5, and a support arm motion mechanism 6. The fixed mounting plate 1 is connected to the main shaft 2 by riveting bolts, the main shaft 2 is connected between the fixed mounting plate 1 and the three-way bushing 21 by riveting bolts, and the fixed base 3 is engaged by threads Connected to both ends of the cantilever 22, the support arm 4 is connected to the outside of the fixed base 3 by bolt riveting, the screw wing movement mechanism 5 is embedded in the inside of the scre...
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