The invention relates to a helicopter coaxial twin-rotor two-turn and three-shift parallel drive device, which includes a rotor mechanism, a moving platform, a
machine base, two PSS-type drive rods, a PUU-type drive rod, two rotating transmission shafts, two engines and Spring; rotor mechanism includes moving platform, spindle, inner and outer jackets, tie
rod group, upper and lower blade groups, upper and lower connecting rod groups, gear group and auxiliary electric rod; upper and lower blade groups and coaxial inner and outer jackets The convex circular table is rotationally connected, and the moving table is rotationally connected with the inner and outer jackets; the two ends of the three driving rods are hinged with the moving table and the
machine base, driving the rotor mechanism to swing and
telescope; the engine is fixedly connected with the
machine base, and the two ends of the rotating transmission shaft are connected to the engine. The input shaft of the shaft and gear set drives the inner and outer casings to rotate forward and reverse; the auxiliary electric rod drives the blade set to self-tilt through the screw, core rod, tie
rod group and connecting
rod group; the spring driven platform diverts the rotor load to the machine base. The invention has the advantages of
fast speed, large lift, balanced reaction torque, the engine is installed on the base, simple structure and good stability.