SHROUD ASSEMBLY FOR A TURBINE ENGINE
A shroud assembly for a turbine section of a turbine engine includes a shroud plate in thermal communication with a hot combustion gas flow and a baffle overlying the shroud plate to define a region. One or more shaped cooling features are located along the region such that a cooling fluid flow pass...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
30.06.2016
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Subjects | |
Online Access | Get full text |
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Summary: | A shroud assembly for a turbine section of a turbine engine includes a shroud plate in thermal communication with a hot combustion gas flow and a baffle overlying the shroud plate to define a region. One or more shaped cooling features are located along the region such that a cooling fluid flow passing through the region encounters the shaped cooling features to increase the turbulence of the cooling fluid flow. |
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Bibliography: | Application Number: US201514879277 |