FIELD: aviation.
SUBSTANCE: proposed flying vehicle has fuselage, propeller rotating in horizontal plane for creating lifting force and horizontal thrust, engine for driving the propeller and control surfaces. Fuselage is provided with through vertical passage where control surfaces are secured on frame; propeller is made in form of upper disk and lower ring with curvilinear air intake blades located in between them. Upper disk of propeller is rigidly secured on shaft kinematically linked with output shaft of engine. Upper surface of disk is provided with stiffeners on which bow-shaped wind shield is secured over periphery.
EFFECT: simplified construction; enhanced operational reliability.
2 dwg
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