The application discloses a helicopter universal traction structure and a
traction method thereof, and relates to the technical field of traction vehicles. The application comprises a
traction frame, one end of the
traction frame is provided as a U-shaped structure, and a helicopter front
landing gear is internally installed, one end of the helicopter front
landing gear is symmetrically connected with a connecting roller in a rotating mode, one end of the
traction frame is symmetrically provided with a connecting groove, the connecting roller is internally installed in the connecting groove, one end of the connecting groove is provided with a connecting
assembly, the other end of the traction frame is provided with a mounting block, and the top of the mounting block is rotatably connected with a steering
handle. The spring one, the
damper and the braking
assembly are used in cooperation, so that when the helicopter front
landing gear is suddenly stopped, the spring one and the
damper absorb and buffer the inertial thrust received by the traction frame, and the braking
assembly is used in cooperation to increase the friction between the traction frame and the ground, so that the
braking distance of the traction frame is shortened, and the use safety of the traction vehicle is effectively improved.