FIELD: transport.
SUBSTANCE: invention relates to aerostatic transport systems. Hybrid aircraft comprise airframe, power plant, system of propellers, tail unit, multi-support chassis and nacelle. Nacelle represents an inflatable small-elongation wing with V-wing variable section span. Tail unit consists of inflatable rudder fin with vertical rudder. Two-circuit power plant comprise engine accommodated inside airframe above aforesaid nacelle. System of propellers is arranged on airframe ends and at nose. Multi-support chassis consists of running gear arranged on nacelle and auxiliary chassis arranged on airframe ends. Nacelle accommodates crew cab, passenger and cargo compartments and is secured to airframe from below.
EFFECT: simplified design.
4 dwg
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