A multi-rotor-wing unmanned aerial vehicle landing protection device is composed of an unmanned aerial vehicle 1, a connecting table 2, a fixing frame 3, a gas bag bin 4, a gas pipeline 5, a high-pressure gas cylinder 6, gas columns 7 and a gas release valve 8, wherein the connecting table 2 is arranged at the bottom end of the unmanned aerial vehicle 1, the high-pressure gas cylinder 6 is arranged at the bottom end of the connecting table 2, the gas bag bin 4 is arranged at the bottom end of the high-pressure gas cylinder 6 which is fixedly connected with the gas bag bin 4 through the fixing frame 3, the gas pipeline 5 is arranged between the high-pressure gas cylinder 6 and the gas bag bin 4, the gas columns 7 are arranged in the gas bag bin 4 and are in the shape of a honeycomb, and the gas release valve 8 is arranged at the bottom end of the gas bag bin 4. The multi-rotor-wing unmanned aerial vehicle landing protection device can achieve stable grounding and is prevented from turning one side, and has the advantages of being recycled, reset and reused.
Multi-rotor-wing unmanned aerial vehicle landing protection device
03.02.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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