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A linkage folding mechanism of a foldable unmanned aerial vehicle and the unmanned aerial vehicle

The application provides a linkage folding mechanism of a foldable unmanned aerial vehicle and the unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles.The linkage folding mechanism of the foldable unmanned aerial vehicle comprises a rotary connecting assembly arranged at the connecting position of a first fuselage section and a second fuselage section and used for realizing rotary folding, a locking structure arranged at the connecting position and used for fixing the fuselage when unfolded, a cantilever end provided with complementary positioning surfaces and fixed structures arranged between the abutting surfaces to fix the cantilever when folded, and a linkage structure arranged between the support and the rotary connecting assembly and used for driving the support to fold synchronously in response to the folding of the fuselage.The linkage folding mechanism of the foldable unmanned aerial vehicle provided by the application can realize the posture switching of the support when the fuselage is folded, automatically and accurately position the cantilever end to prevent collision and fixation, effectively simplify the folding operation, reduce the risk of damage of the cantilever due to loosening, improve the storage stability and safety of the unmanned aerial vehicle, save the storage and transportation space, and significantly improve the portability of the unmanned aerial vehicle.
Owner:WUHAN HAOAO AVIATION TECH CO LTD