FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering and can be used in soft-wing lifting and manoeuvring in parachutes, kites and soft-wing aircraft. In the technical solution on the method of lifting and manoeuvring with a soft wing in the air, for the convenience of using aircraft with a soft wing, the wing is lifted into the air into the launch position by tightening the slings, and the wing is manoeuvred in flight regardless of the presence of the incoming external air flow (wind). Method of lifting and manoeuvring in flight with a soft wing of an aircraft with an air propeller, which creates an air flow, made with a gas-tight pneumatic frame, filled from a compressed gas source through a flexible gas line and through a relief valve released from gas, with implementation of lifting of soft wing vertically above moved object, with tension by system of slings fixed on moved object, at filling of pneumatic frame of soft wing with gas. At that, air is pumped into the wing gas-tight pneumatic frame, and the airborne wing is lifted to the starting position by the airflow thrust force perpendicular to the ground and the soft wing plane passing through at least one or several holes made in the soft wing created in each of the holes, during rotation of propeller, planted on shaft of electric motor of air propeller, and manoeuvring and horizontal flight of the aircraft is carried out by the value and direction of the air flow thrust force created by the rotating propeller fixed on the shaft of the electric motor of the air propeller, by the value of the motor rpm control unit, and in the direction in the propeller positions from the parallel to the perpendicular to the plane of the wing, with the change in the position of the electric motor on two axes of rotation, fixed parallel to the longitudinal axis of the wing on the circular frame by the electric drive of rotation, when electric power is supplied to an electric motor, via an electric cable from an electric power source fixed on a movable object.
EFFECT: claimed invention enables to implement a method of lifting a wing to a launching position and manoeuvring an aircraft soft wing without using a lifting static Archimedean force of a gas lighter than air, allows to implement method of aircraft soft wing lifting to launch position regardless of external air flow (wind) presence, makes it possible to implement method of soft wing manoeuvring in air flow controlled by magnitude and direction, using air propellers of wing as traction propulsors during lifting, hovering and horizontal flight, provides for collection and storage of soft wing of aircraft in small volume, for example, knapsack or compartment for storage in assembled form.
2 cl, 3 dwg
