DEVICE FOR PROTECTION OF INNER FLOW OF DOUBLE-FLOW TURBOJET ENGINE AGAINST FOREIGN MATTER Russian patent published in 1995 - IPC

Abstract RU 2045451 C1

FIELD: aeronautical engineering. SUBSTANCE: device is mounted after last-stage impeller of fan rotor. Device has blades inclined towards rotation of rotor of guide vane assembly of last-stage fan, outer and inner housings of fan. EFFECT: enhanced reliability. 2 dwg

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RU 2 045 451 C1

Authors

Alekseev V.B.

Evdokimov A.I.

Novitskij S.M.

Fedorko G.V.

Dates

1995-10-10Published

1992-03-05Filed