US Patent 10337404 Preferential cooling of gas turbine nozzles
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Patent abstract
Turbine nozzle assemblies include a plurality of circumferentially spaced first components and second components, which are designed to provide different amounts of cooling. The second components, which are generally aligned with an opening of transition pieces, are designed to provide more cooling than the first components, which are generally aligned with interfaces between the transition pieces.
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Patent Inventor Names
Joseph V. Citeno0
Kevin Weston McMahan0
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Official Website
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US Patent 10337404 Preferential cooling of gas turbine nozzles
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Is a
Patent jurisdiction
Patent number
10337404
Date of patent
July 2, 2019
Patent application number
12719674
Date Filed
March 8, 2010
Patent primary examiner
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