Vertical take-off and landing (vtol) tilt rotor aircraft with tandem rotors

摘要

Tilt rotor aircraft has the following features: - the lateral hulls, which are connected at the front, form a single body.,. - the wings, which is in the upper part of the hulls and are located between two fence, generate the lifting force for horizontal flight. - between two hulls are two opposite direction and tandem was applied stroke - thrust - rotors placed in position, a turning the degree of 0° - 95°. [0030] figs - on the lower part of the gondolas are controllable double valves, which serve for stabilizing system. Fig.4 (1a, 2a). - basic mechanisms, main components are doubled, and placed on two hulls are - the stabilizing system comprises flight made possible even in the case of the turbulent atmosphere and yawing, pitching, and lateral flight.