Vertical take off and landing and the aerodynamics the horizontal flight hybrid aircraft which becomes independent

摘要

(57) Abstract As for this invention, there was a front part of the aircraft, it was connected to the main engine of the aircraft at least is locked offer the feather propeller/the rotor (2 and 12) which it is located on the rear section of the propulsion unit and the aircraft which at least being 1 where auxiliary engines (3 and 13), gradually inclined possibility, at the same time is revolution possible to include with the auxiliary engine (3 and 13) which with two restriction position namely the respective vertical position and horizontal position, the cockpit (4 and 14) and the passenger compartment (5 and 15) each flight aspect namely the takeoff and movement aspect and horizontal direction flightAs between, or the horizontal position of the between floor and the ceiling of the opposite maintained vis-a-vis the land parallel continually, it is executed it takes off in vertical attitude (as revolving possible module, with front part as upper part,) it modifies attitude gradually with the engine of auxiliary inclined possibility the rear section, reaches to horizontal attitude completely, being between vertical attitude of landing returns, vertical take off and landing and the aerodynamics it becomes independent, it regards the hybrid aircraft (1 and 11) which flies horizontally.