FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft comprises fuselage, crew cabin, wing with developed front and rear edges, vertical and horizontal fins, power plant, box of aircraft assembly units, aircraft and engine control unit, fuel, hydraulic and air systems, front and primary legs and landing braking system. Crew cabin allows conversion from single-seat into two-seat version and tandem location of pilots in front and rear compartments in common sealed zone under cockpit canopy. In single-seat version, rear compartment accommodates removable fuel tank. Adaptive wing tips deflect automatically in all flight conditions. Said deflection is performed in compliance with preset law. Incidence indication system incorporates three light fields: central strip-like, top and bottom fields arranged in the row of discrete rectangular strips.
EFFECT: expended performances.
37 cl, 11 dwg
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Authors
Dates
2012-02-27—Published
2010-06-10—Filed