FIELD: aviation.
SUBSTANCE: the mode of flying is based on creation of a flow with propulsion propellers for continuous streamline circulation of the flow around the wing. The flow is deflected in vertical plane with tilting of the propellers. The part of the flow is withdrawn into the wing's cavity fulfilled with a smooth contour of the cross-section and brought out into the open in round direction along the contour of the wing through lengthwise tangential grooves along the whole wing span. A propeller-driven aircraft has a wing, propellers and a power-plant for propellers. The power-plant has a fuel bunker and a gas-generator with a pyrolysis chamber, a furnace , an evaporator and a condenser. The wing and the blades of the propellers are fulfilled with a volumetric contour of the cylinder type cross-section with an aperture for drawing of air from the braking zone of the flow into the inner cavity and with longitudinal exit tangential grooves along the contour on the whole length. The propellers are connected with the gas-generator with pipes. The furnace is placed in the fuel bunker.
EFFECT: expanding the range of changing the speed of the flight.
2 cl, 2 dwg
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Authors
Dates
2005-05-20—Published
2003-05-13—Filed