MULTI-FUNCTION SHIP STATIONING AIRCRAFT, ITS CONTROLLING AND INDICATING SYSTEM ACCORDING TO AIRCRAFT INCIDENCE ANGLE Russian patent published in 2012 - IPC B64C39/00 B64C9/02 B64D45/00 G09G3/32 

FIELD: aviation.

SUBSTANCE: invention group refers to aviation. The aircraft contains a fuselage, a pilot's cockpit, a foldable wing with the developed mechanization of the front and back edges, vertical and horizontal fins, a power package, an accessory gear-box, control units for the aircraft and the engines, a fuel, hydraulic and air systems, a nose and main landing gears, a retro system. The pilot's cockpit is able to be transformed from a single-seat into a double-seat variant with a tandem arrangement of the pilots under one hood. In the single-seat modification the set-in fuel tank is located in the pilot's cockpit, in its back part. Adaptational noses, swirling shields, wing flaps and end flaperons allows controlling the aircraft. The control system of the aircraft consists in changing the curvature of an aerofoil profile. The indicating system according to the aircraft incidence angle contains three light fields: a central made in the form of a stripe, an upper and a lower one made in the shape of discretely located stripes in the form of rectangles.

EFFECT: takeoff from badly prepared airdromes and/or short flight strips and improving safety of a flight.

37 cl, 12 dwg