B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 27/00 (2006.01)
Patent
CA 2546207
The invention pertains generally to rotation-wing flying vehicle. It applies to helicopter and flying saucer. The flying vehicle is composed of the frame support 4, the powerplant, the electronic earth compass 11 and laser sensors 8. The powerplant is mainly composed by two propeller assemblies and one steering assembly. The propeller assembly is composed of propeller sliding fork 18, pitch control box 19, propeller shaft 16, Sliding Rod 14, Axis Rod 15 and hollow shaft 17, gearboxes and motors. The steering assembly is composed by steering fork 1, propellers and steering socket 2 which is controlled by servo motors and gearbox. Its first feature is that the powerplant is isolated from frame support 4 for good stabilization. The second feature is that the steering leg 20 of the steering fork 1 slides around the steering socket 2 to get quick response and easy to make. The third feature is that the axis rod 15, which is used to control the pitch angle of the propeller from negative to positive angle, is located inside of the hollow shaft 17. The earth compass sensor 11 and the laser sensors 8 are used to further stabilize the frame by referring to ground for better stabilization.
He Guangming Minc
Na
LandOfFree
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