FIELD: transport.
SUBSTANCE: invention relates to dynamic air-cushion vehicles, in particular to hovercrafts. Hovercraft has fuselage, wing, vertical and horizontal fins, power plant and take-off-landing device. Power plant includes at least one engine connected with air propeller. Take-off-landing device has floats connected with wing and pillar mounted on fuselage in front of front wing edge. At least one air propeller is mounted on pillar and furnished with device for gas jet deflection relative to centre-section wing. Planing step is arranged between fuselage stem and wing rear edge. Floats are provided with at least one lateral planing step. Vertical fins are made twin-tailed with dorsal fins and vertical stabiliser. The dorsal fins are formed by extension of fuselage side wall. Fuselage aft is made tapering in vertical plane. Top surface of fuselage aft is provided with hatch connected with fuselage with possibility to move relative to fuselage, and with hatch displacement drive.
EFFECT: invention increases dimensions of cargoes and improves hovercraft maintenance conditions and its take-off-landing characteristics.
8 cl, 8 dwg
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