A rapid folding mechanism for multi-rotor UAV landing gear
A technology of a multi-rotor unmanned aerial vehicle and a folding mechanism, applied in the field of unmanned aerial vehicles, can solve the problems of inconvenience to carry, occupy a large space, and the landing gear cannot be folded, and achieve convenient carrying, reduced space occupation, good economic benefits and social benefits. effect of benefit
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[0025] In order to make the technical solution, creative features, objectives and beneficial effects of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0026] figure 1 A schematic diagram of the local structure of the landing gear, image 3 It is a schematic diagram of the structure of the motor base. First, the landing gear is installed on the lug 9 of the motor base through the rotating shaft 4 . will fold down the lower housing 13 of the control assembly, as figure 2 As shown, insert the motor base in the direction of the chute 10, install two U-shaped guide posts, the limit block 7 and the return spring 5 in the lower housing in sequence, and the two ends of the limit spring are respectively installed on the two U-shaped guide posts. On the boss 6. In order to prevent accidental ejection of the spring during use, insert the upper clamping plate into the lower...
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