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US Patent 12110801 Turbine shroud segment and its manufacture

Patent 12110801 was granted and assigned to Rolls-Royce PLC on October, 2024 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Rolls-Royce PLC
Rolls-Royce PLC
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Date Filed
August 10, 2023
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Date of Patent
October 8, 2024
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Patent Applicant
Rolls-Royce PLC
Rolls-Royce PLC
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Patent Application Number
18447740
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Patent Citations
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US Patent 9988936 Shroud assembly for a gas turbine engine
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US Patent 10422235 Angled impingement inserts with cooling features
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US Patent 10690055 Engine components with impingement cooling features
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US Patent 10815828 Hot gas path components including plurality of nozzles and venturi
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US Patent 10822986 Unitary body turbine shrouds including internal cooling passages
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US Patent 10989068 Turbine shroud including plurality of cooling passages
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US Patent 11598222 Turbine engine hanger
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US Patent 11525401 Impingement baffle for gas turbine engine
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US Patent 7665962 Segmented ring for an industrial gas turbine
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US Patent 9556795 Integrated heat shield
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•••
Patent Inventor Names
Rupert J. Taylor
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Carlos Javier Diaz Rodriguez
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James Revell
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Grant Mathieson
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Ryan R. Allen
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Dinesh Perumalsamy
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Ngungunyana Mhlanga
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
12110801
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Patent Primary Examiner
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Jesse S Bogue
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CPC Code
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F05D 2260/201
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F01D 25/12
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F01D 25/24
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