FIELD: transport.
SUBSTANCE: invention relates to air-cushion vehicles. Canard configuration hovercraft comprises fuselage with crew cabin, rudder arranged at mid section of fuselage, tail short wing and rudder fin. Fuselage comprises two crew cabins arranged on sides of centre-section with rotary emergency control surface articulated with centre section nose. Inner walls and said cabins and centre section top skin make a flute to accommodate nose and tail airflow blowers. Horizontal rotary flaps are arranged beyond the node blower and equipped with rotary drives to connect airflow portion with said channel. Said channel is arranged between centre section top and bottom skins and rotary shutters articulated therewith.
EFFECT: higher flight safety, perfected aerodynamics.
3 cl, 2 dwg
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