CONVERTIPLANE Russian patent published in 2024 - IPC B64C37/00 B64C29/00 B64C27/28 

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to convertiplane designs. Convertiplane is made according to aerodynamic configuration "canard", contains power plant on the basis of internal combustion engine, fuel tanks of gaseous and liquid types of fuel, electronic control unit. Housing is made in the form of a wing with retractable flaps connected by hinged rods with movable propellers. Thrust vector of the propellers can be changed under the action of the electric drive of the movable posts. Shafts of propellers are rigidly connected to pulleys of electric motor through reduction gear. Turbojet power unit of opposite combustion of gaseous and liquid types of fuel is installed in the housing. Power takeoff pulleys of turbojet power unit are connected by belt transmission with electric motor pulleys, generator charges storage battery and performs additional function of belt tensioner. Propeller strut on a ball bearing is equipped with an electric motor with a planetary reduction gear and a control lever with a hinge joint, and is installed in the tail part of the wing housing.

EFFECT: creation of multifunctional design of convertiplane with powerful power plant using gaseous and liquid types of fuel.

1 cl, 4 dwg