PROPULSOR Russian patent published in 1998 - IPC

Abstract RU 2120396 C1

FIELD: aeronautical engineering. SUBSTANCE: propulsor is provided with air intake mounted on tail section of fuselage and slotted exit nozzles mounted in nose section of fuselage at the top and on the wing. Engine is mounted in fuselage with turbine forward in way of flight and with compressor opposite to flight. Entire gas flow is fed to slotted nozzles mounted along leading edge of wing and over perimeter of upper portion of fuselage frame. EFFECT: enhanced efficiency of use of fuel. 3 dwg

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RU 2 120 396 C1

Authors

Duchenko Nikolaj Aleksandrovich

Dates

1998-10-20—Published

1997-01-06—Filed