Cooled turbo-machine vane
AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
InventorsXavier G. A. Coudray, Mischael F. L. Derrien, Philippe M. P. Pichon
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Abstract
A turbo-machine vane having a plurality of internal cavities for the flow of a cooling fluid, and a plurality of openings through the outer wall of the vane for communicating the internal cavities with the outside of the vane. Two rows of openings are provided in the leading edge of the vane, one row on each side of the central line of the leading edge end extending parallel with the central line, and each opening of each row is oriented to direct cooling fluid which flows through it from the interior of the vane away from the central line relative to the rows.
Claims6
A turbo-machine vane, comprising:
- an outer wall defining a hollow interior,
- a plurality of internal walls dividing said hollow interior into a plurality of internal cavities for the flow of a cooling fluid, and said outer wall having a plurality of openings for communicating at least some of said internal cavities with the exterior of said vane, said vane having a foot end and a head end and defining a longitudinal axis between said foot end and said head end, and said outer wall defining an intrados face, an extrados face and a leading edge portion of said vane separating said intrados face and said extrados face, said leading edge portion having a central line on which tangents to said outer wall and lying in planes perpendicular to said longitudinal axis of said vane are perpendicular to the principal direction of the flow of gases which, in use, come into contact with said vane, wherein said plurality of openings include two first rows of openings in said leading edge portion of said vane on opposite sides of said central line and substantially parallel to said central line, the orientation of each opening in said two first rows being such as to direct cooling fluid which flows through said opening from said interior of said vane away from said central line relative to said rows, and each said opening of said two first rows having a cross-section of an oblong shape arranged at an angle relative to said central line, wherein said plurality of internal cavities include a first longitudinal cavity in the region of said leading edge of said vane and in direct communication with said openings of said two first rows of openings, a first series of longitudinal ducts adjacent and defined partly by the portion of said outer wall defining said intrados face of said vane, and a second series of longitudinal ducts adjacent and defined partly by the portion of said outer wall defining said extrados face of said vane wherein each opening in said two first rows of openings is oriented relative to said longitudinal axis of said vane such that the inner end of each of said openings is closer to said foot of said vane than the respective outer end of each of said openings such that cooling fluid which flows through said openings is directed away from said foot toward said head of said vane and wherein the cross-section of each of said openings in said first two rows of openings increases uniformly in side from the inner end of said opening to the outer end thereof.
Dependencies are inferred from the claim text.