Quick-release rotor unmanned aerial vehicle
The utility model relates to the related technical field of unmanned aerial vehicles, in particular to a quick-release rotor unmanned aerial vehicle. Comprising a fuselage and a skid type undercarriage, the skid type undercarriage comprises an arch beam and two sliding pipes, and the two sliding pip...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model relates to the related technical field of unmanned aerial vehicles, in particular to a quick-release rotor unmanned aerial vehicle. Comprising a fuselage and a skid type undercarriage, the skid type undercarriage comprises an arch beam and two sliding pipes, and the two sliding pipes are connected with the arch beam through sliding pipe sleeves arranged at the lower end of the arch beam; a quick-release connector A is arranged at the bottom of the machine body, and a quick-release connector B is arranged at the top of the arched beam; the quick-release connector A is provided with a concave cavity allowing the quick-release connector B to enter, the concave cavity is provided with more than two blocking pieces, and the quick-release connector B is provided with clamping blocks matched with the blocking pieces; by arranging the quick-release connector A and the quick-release connector B, the fuselage and the undercarriage of the unmanned aerial vehicle can be quickly disassembled and assemble |
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