Patent ID: 6979176

Claim:
Cooled turbine component for film cooling in a gas turbine engine comprising: a main body; a film cooling hole which is formed in the main body, and the hole further includes an inlet opening which is provided on an inlet side surface of the main body and an spurt out opening which is provided on an outlet side surface of the main body, and compressed air which is bled from a compressor or a fan introduces to the cooling hole from the inlet opening for providing cooling air, and the cooling air spurt out from the spurt out opening, and the cooling hole is slanted to the thickness direction of the component body so that the cooling air form a cooling film which coats and protects the surface of the main body; and a partition wall which is provided on the bottom surface of the outlet side of the film cooling hole, and the partition wall is extended from the outlet side of the cooling hole to the inlet side of the cooling hole being viewed from the side opposing to the spurt out opening.