FIELD: canard configuration aircraft.
SUBSTANCE: proposed aircraft has wing 1, horizontal nose plane consisting of lower plane 2 and upper plane 3, fuselage 4, wheeled landing gear including main support 5 and two side supports 6 and engine plant 7. Main support 5 of wheeled landing gear is located behind aircraft CG. Upper plane 3 of horizontal nose plane is shifted backwards relative to lower plane 2. Movable surface of upper plane 3 of horizontal nose plane is kinematically linked with aircraft control system by pitching and is used as elevator 8. Movable surface of lower plane 2 is kinematically linked with control system of wing high-lift devices; it may move downward only and is used as flap 9.
EFFECT: reduced sizes of aircraft.
2 dwg
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