FIELD: aircraft manufacture. SUBSTANCE: flying vehicle is provided with stabilizer, two similar additional wings, four brackets, two rods, four ball joints, rocker arm and bar; wing is made in form of rectangle whose larger side has form of chord; engine is rigidly secured to leading edge of wing in plane where axis of turn of flying vehicle and central chord of wing lie; engine shaft is mounted at negative angle to central chord. Levers with pedals are arranged in wing and their lower ends are articulated with wing. Axes of articulations are located coaxially relative to each other in parallel with transversal axis of flying vehicle. Stabilizer is rigidly secured to wing before trailing edge in plane where transversal axis of flying vehicle and central chord of wing lie. Elevator is articulated to trailing edge of wing and stabilizer. Ailerons are articulated to trailing edges of wings. Brackets are provided with cylindrical holes. Flying vehicle control stick is connected with end of bar on side of leading edge of wing in such position that axis of articulation is parallel to transversal axis of flying vehicle, elevator is located in plane of stabilizer and control stick is parallel to axis of turn. EFFECT: enhanced economical efficiency and stability of flight. 2 dwg
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Authors
Dates
2002-01-20—Published
1999-12-27—Filed