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US Patent 10107128 Cooling channels for gas turbine engine component

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US Patent 12085283 Combustor for a gas turbine engine
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US Patent 12066187 Plank hanger structure for durable combustor liner
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US Patent 11994294 Combustor liner
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US Patent 11959643 Combustor for a gas turbine engine
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US Patent 11920796 Combustor for a gas turbine engine
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US Patent 11885495 Combustor for a gas turbine engine including a liner having a looped feature
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US Patent 11867398 Hollow plank design and construction for combustor liner
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US Patent 11859824 Combustor with a dilution hole structure
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US Patent 11859823 Combustor chamber mesh structure
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Patent abstract

A gas turbine engine component includes a wall portion and a leading edge cooling channel that extends through the wall portion. The leading edge cooling channel includes at least one first cooling passage separated from at least one serpentine cooling passage.

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US Patent 11788416 Gas turbine engine components having interlaced trip strip arrays
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edited on 4 Oct, 2023
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US Patent 11774098 Combustor for a gas turbine engine
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Patent Inventor Names
Dmitriy A. Romanov0
Dominic J. Mongillo, Jr.0
Matthew A. Devore0
Edits on 29 Apr, 2023
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Patent Citations Received
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US Patent 10533454 Turbine shroud cooling
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Edits on 6 Apr, 2023
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edited on 6 Apr, 2023
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Patent Citations Received
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US Patent 10570773 Turbine shroud cooling
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Edits on 3 Apr, 2023
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Infobox
Is a
Patent
Patent
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Patent Applicant
United Technologies
United Technologies
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
101071280
Date of Patent
October 23, 2018
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Patent Application Number
148308120
Date Filed
August 20, 2015
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Patent Citations Received
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US Patent 10344620 Air cooled component for a gas turbine engine
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US Patent 10502093 Turbine shroud cooling
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US Patent 10533454 Turbine shroud cooling
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US Patent 10570773 Turbine shroud cooling
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US Patent 10837315 Turbine shroud including cooling passages in communication with collection plenums
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US Patent 10989068 Turbine shroud including plurality of cooling passages
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US Patent 11274569 Turbine shroud cooling
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US Patent 11365645 Turbine shroud cooling
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US Patent 11371701 Combustor for a gas turbine engine
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US Patent 11549686 Combustor for a gas turbine engine
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Patent Primary Examiner
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Woody Lee, Jr.
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Edits on 1 Apr, 2023
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Edits on 31 Mar, 2023
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edited on 31 Mar, 2023
Infobox
Patent Citations Received
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US Patent 11365645 Turbine shroud cooling
0
Edits on 29 Mar, 2023
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edited on 29 Mar, 2023

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