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.