FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. In compliance with the first version, aircraft comprises fuselage, wing, empennage and engine/engines. Said engine is directed forward-upward relative to aircraft lengthwise axis, or engine thrust source is directed forward-upward relative to aircraft lengthwise axis with due allowance for aircraft aerodynamics. In compliance with the first version, aircraft comprises fuselage, wing, empennage, electric remote control system and engine/engines. Amplifier receives signal from the rudder position selector or that pitch selector and that of engine thrust transducers or that from engine control lever position to vary its gain, or this signal is fed as-scaled to amplifier input.
EFFECT: increased lift.
2 cl, 2 dwg
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