CONVERTIPLANE Russian patent published in 2020 - IPC B64C37/00 B64C27/28 

FIELD: aviation.

SUBSTANCE: invention relates to the field of aviation, namely to the convertiplane designs. Convertiplane comprises fuselage, control system, wing aerodynamic wing with aerodynamic control surfaces, all-turning front horizontal empennage with aerodynamic control surfaces, tail unit and propeller groups with air screws. Propeller groups with air screws are arranged with the possibility of rotation on the tips of the front horizontal empennage and on the empennage. Convertiplane can match aerodynamic pressure centre and resultant thrust vector with possibility of their mutual dynamic and static scalar control due to operation of aerodynamic control surfaces and control of thrust vector of each of propeller groups.

EFFECT: propeller groups located on tips of front horizontal empennage are made with opposite rotation of propeller and with possibility of providing dynamic displacement of pressure centre, as well as possibility of displacement of rotation axis of front aircraft power plant in plane ZX.

8 cl, 15 dwg