DOUBLE-FLOW TURBOJET ENGINE Russian patent published in 1999 - IPC

Abstract RU 2127370 C1

FIELD: aero-engine manufacture. SUBSTANCE: blade roots of guide vanes are made in form of profiles straightening the flow of air of second loop twisted by fan and having cooling air passages open to second loop. EFFECT: reduction of resistance of air flowing through second loop; reduction of blade mass; reduction of losses. 4 cl, 3 dwg

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RU 2 127 370 C1

Authors

Serkov Anatolij Gavrilovich

Dates

1999-03-10Published

1992-11-24Filed