GAS TURBINE COOLED BLADE Russian patent published in 1995 - IPC

Abstract RU 2042833 C1

FIELD: transport engineering. SUBSTANCE: during operation of turbine, cooling air flows to area of fin 1, then it flows through passages 4, cools blade and is discharged from it. Orientation of ribs 2 and 3, introduction of radial rib 5 and V-shaped partitions provide for efficient distribution of coolant flows in passages of blade. EFFECT: efficient distribution of coolant flows in passages of blade. 2 dwg

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RU 2 042 833 C1

Authors

Kobchenko V.K.

Nagoga G.P.

Zikeev V.V.

Mamon Ju.A.

Shtorm E.A.

Terent'Ev A.S.

Dates

1995-08-27Published

1993-06-29Filed