Cooled turbine vane

Rotary kinetic fluid motors or pumps – Including heat insulation or exchange means – Working fluid on at least one side of heat exchange wall

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Details

415DIG1, 416 96R, F01D 518

Patent

active

040800954

ABSTRACT:
A cooled vane for a gas turbine engine in which the coolant channels have an arcuate component, convex outwardly towards the surface of the vane to establish centrifugal force in the coolant flowing therethrough and thereby induce a secondary flow to the coolant, promote mixing and reduce the outer boundary layer of the coolant to enhance the heat transfer characteristics to the coolant and thereby more efficiently maintain the vane within acceptable temperature limitations.

REFERENCES:
Hodge, R. I. and Johnston, I. H., "A Review of Blade-Cooling Systems," The Gas Turbine (Feb., 1958), pp. 396-398.

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