Rotary-wing miniature gyro helicopter

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/02 (2006.01) A63H 27/00 (2006.01)

Patent

CA 2607188

There is provided a gyro helicopter generally comprising a fuselage, a rotor mast extending upwardly from the top of the fuselage, a rotor adapted to autorotate when the gyro helicopter moves forward, and drive means mounted to the fuselage for driving the gyro helicopter in at least a forward direction and for causing the gyro helicopter to perform yawing motions. The rotor of the gyro helicopter includes a hub mounted to the rotor mast, at least two rotor arms extending radially from the hub, and at least two corresponding lifting blades, a leading edge of each of the lifting blades fixedly mounted to a corresponding one of the rotor arms. The rotor arms are adapted to twist in a first direction while an upward force is applied to the blades, raising the trailing edge of the blades above the plane of the rotor, and the rotor arms are adapted to twist in a second direction while a downward force is applied to the blades, the twisting in a second direction lowering the trailing edge of the blades below the plane of the rotor.

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