SEGREGATED COOLING AIR PASSAGES FOR TURBINE VANE
An airfoil for a gas turbine engine includes a cavity including an internal surface of an outer wall. A baffle is disposed within the cavity and spaced apart from the internal surface. A partition is disposed between the baffle and the internal surface to divide a space between the baffle and the in...
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Main Author | |
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Format | Patent |
Language | English |
Published |
11.07.2019
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Subjects | |
Online Access | Get full text |
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