TURBINE ENGINE SHROUD WITH NEAR WALL COOLING
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United States of America Patent
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Issued Date -
Sep 19, 2024
app pub date -
May 29, 2024
filing date -
Feb 9, 2017
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Abstract
An apparatus for a shroud assembly for a turbine engine and a method of manufacturing such can include the shroud assembly having one or more shroud segments having an inner face in a circumferential organization around a rotating blade assembly. A near wall cooling passage can be provided in the shroud assembly to cool the inner face of the shroud. The near wall cooling passage can exhaust to a purge cavity, a split line, or at the inner face.
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