Aircraft with "s"-rotor/"c" blades folding to the "o"-wing

Details Aircraft with "s"-rotor/"c" blades folding to the "o"-wing Aircraft with "s"-rotor/"c" blades folding to the "o"-wing

B - Operations, Transporting

64

C

B64C 27/24 (2006.01)

Patent

CA 2141481

The present invention provides an aircraft which has the capabilities of the vertical takeoff, landing, hovering operations and flying with supersonic speed utilizing the "S"-shaped rotor-wing as a conventional helicopter rotating wing After transition to forward flight, following the takeoff, the "C"-shaped blades of the "S"-shaped rotor-wing arc pivoted and become a wing of the "O" configuration. The axle of the rotor- wing is designed to be tilted its all directions. The aircraft utilizes two jet engines for rotating the rotor-wing and propulsive force; and four small rocket nozzles, installed on both sides at equal length from the rotor axis at the middle and at the rear of the fuselage, for yaw control at low speed.

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