Stacked cooling assembly for gas turbine combustor
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United States of America Patent
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Jul 30, 2024
Grant Date -
Apr 6, 2023
app pub date -
Oct 6, 2021
filing date -
Oct 6, 2021
priority date (Note) -
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Abstract
Stacked cooling assemblies and combustor bead ends are provided. A stacked cooling assembly includes an inlet plate defining an inlet to a coolant circuit, an outlet plate defining an outlet of the coolant circuit, and an intermediate plate disposed between the inlet plate and die outlet plate. The intermediate plate defines an intermediate cavity. A downstream surface of the inlet plate, an upstream surface of the outlet plate, and the intermediate cavity collectively define a connecting channel that fluidly couples the inlet to the outlet.
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