Tiltrotor With jet-driven rotors, rotor RUN THROUGH THROUGH swash control levers do not require additional controls

摘要

1. convertiplane comprising a: a fuselage (1), the stabilizer (3) and the keel (4) arranged to maintain the sideslip in airplane mode and located in the tail section of the fuselage (1), the console (2) mounted near the center gravity (17) on either side of the fuselage (1) and connected to it by hinges (18), providing the possibility of changing the angle of rotation of 100 to -10 ° relative to the horizon independently; fairings (19); column (12), rigidly connected to the consoles (2) and a closed fairing (19), the rotors (6) comprise moving if (5) having a blade (7) with jet engines (8) rigidly connected to the columns (12), arms (2) by means of torsion bars (9) mounted on a freely rotating shaft (10) columns (12), in bearings ( 11), thrusters (8) disposed in the arm portion of the blades (7) having a nozzle oriented towards the rear edge-propulsion blades (7), the swash plate (14) arranged to change the total and cyclic-propulsion blades (7) by changing the installation angle of said propulsor blades (7); sound control means detecting (16) adapted to change and total cyclic pitch of said rotor blades (6) .2 (7). Convertiplane according to claim 1, characterized in that therein the aforementioned air-jet propulsors (5) are formed integrally with the rotor (6) and the aforementioned blades (7), wherein the aforementioned blade (7) comprise a common input device (13) located near the rotor shaft (10), a longitudinal duct blades (7) disposed inside the heat exchanger (21) for the evaporation of the cryogenic fuel and the engine combustion chamber (8) with the rea