The invention relates to a helicopter coaxial double-cone rotor parallel manual device, which includes a rotor group, a parallel mechanism, a forward and reverse rotation mechanism, a variable cone mechanism and a spring; the rotor group includes a core rod, an inner and outer jacket, a tie
rod group, an upper and The lower blade set, the upper and lower connecting rod sets, the upper and lower rings; the upper and lower blade sets are rotationally connected with the inner and upper ends of the jacket; the parallel mechanism is connected in parallel with the rotor set, and the hand-operated
crank drives the rotor set to swing and
telescope; forward and reverse The rotating mechanism drives the coaxial double-linked rotor to rotate forward and reverse through the inner and outer jackets, upper and lower large gears, intermediate wheels and upper and lower gears; the cone-changing mechanism drives the core rod, upper and lower rings and upper and lower connecting rod groups. Changing the angle between the blades and the axis of the rotor group changes the lift and
flight speed. The control mechanism of the invention is simple and lightweight, and can change the
flight direction, speed and lift flight. It has the characteristics of
fast speed, large rotor lift, balanced anti-torque, simple structure, short
fuselage, centered center of gravity, aerodynamic symmetry, small rotation
diameter, Good stability and other advantages.