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US Patent 11774098 Combustor for a gas turbine engine

Patent 11774098 was granted and assigned to General Electric on October, 2023 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Current Assignee
General Electric
General Electric
Date Filed
June 7, 2021
Date of Patent
October 3, 2023
Patent Applicant
General Electric
General Electric
Patent Application Number
17340585
Patent Citations
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US Patent 8307656 Gas turbine engine systems involving cooling of combustion section liners
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US Patent 7246993 Coolable segment for a turbomachine and combustion turbine
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US Patent 7726131 Floatwall dilution hole cooling
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US Patent 7802431 Combustor liner with reverse flow for gas turbine engine
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US Patent 8109099 Flow sleeve with tabbed direct combustion liner cooling air
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US Patent 8276391 Combustor liner cooling at transition duct interface and related method
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US Patent 9010121 Combustion chamber
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US Patent 9182122 Combustor and method for supplying flow to a combustor
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US Patent 9310079 Combustion liner with open cell foam and acoustic damping layers
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US Patent 9718735 CMC turbine components and methods of forming CMC turbine components
•••
Patent Inventor Names
Ravindra Shankar Ganiger
Shai Birmaher
Saket Singh
Pradeep Naik
Hiranya Kumar Nath
Rimple Rakeshkumar Rangrej
Narasimha Chiranthan R
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11774098
Patent Primary Examiner
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Gerald L Sung
CPC Code
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F23M 5/085
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F23R 3/346
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F23R 3/16
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F05D 2260/2212
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F23R 3/002
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F23R 3/08
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F23R 3/06

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