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US Patent 8307657 Combustor liner cooling system

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US Patent 12092330 Gas turbine combuster
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US Patent 12085283 Combustor for a gas turbine engine
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US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture
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US Patent 11994292 Impingement cooling apparatus for turbomachine
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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 11859818 Systems and methods for variable microchannel combustor liner cooling
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US Patent 11774098 Combustor for a gas turbine engine
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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
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US Patent 08307657 Combustor liner cooling system US Patent 8307657 Combustor liner cooling system

Infobox
Patent Number
0830765700
Patent Number
830765700
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Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
083076570
Date of Patent
November 13, 2012
0
Patent Application Number
124015300
Date Filed
March 10, 2009
0
Patent Primary Examiner
Ehud Halberstam
Ehud Halberstam
0
Edits on 27 Sep, 2022
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edited on 27 Sep, 2022
Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
083076570
Date of Patent
November 13, 2012
0
Patent Application Number
124015300
Date Filed
March 10, 2009
0
Patent Primary Examiner
Ehud Halberstam
Ehud Halberstam
0
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created this topic on 15 Dec, 2021
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 US Patent 08307657 Combustor liner cooling system

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
08307657
Date of patent
November 13, 2012
Patent application number
12401530
Date Filed
March 10, 2009
Patent primary examiner
Ehud Halberstam
Ehud Halberstam

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