The invention discloses a universal
cycloid spindle blade rotor lifting device, and relates to the technical field of unmanned aerial vehicles. The universal
cycloid spindle
paddle rotor wing lifting device comprises a shell, a main shaft, a main taper sleeve, a main
paddle, an auxiliary
paddle and a universal adjusting mechanism. The universal adjusting mechanism comprises a conical fluted disc, a paddle connecting shaft, a driven
bevel gear, an electromagnetic telescopic sleeve A, an electromagnetic telescopic sleeve B and a driving control module; the main paddle and the auxiliary paddle are installed at the two ends of the paddle connecting shaft, each paddle is of a spindle-shaped structure with the surface being a
cycloid curved surface, the middle of each paddle is thickened, and the edge of each paddle is provided with a flow guide edge protruding outwards. The driving control module controls the two groups of electromagnetic telescopic sleeves to synchronously
push and pull to force the paddle connecting shaft to axially translate so as to drive the driven
bevel gear to be instantly meshed with or separated from the
bevel gear disc on the main shaft; transient micro-adjustment of the
attack angle of the blade is achieved through a pure mechanical structure of rigid meshing of the
electromagnetic clutch and the gear, the cycloid gradual change pneumatic curved surface is matched,
response delay is effectively overcome, blade tip vortex is restrained, and the anti-
crosswind stability and the
heavy load structure rigidity under complex turbulence are improved.