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US Patent 9335050 Gas turbine engine combustor

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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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Patent abstract

A swirler assembly for a gas turbine engine includes an outer annular injector which at least partially surrounds an inner injector. In sonic embodiments, a combustor section for a gas turbine engine comprises an inner injector which defines an axis, an outer annular injector which surrounds said inner injector, and a combustor vane along said axis.

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US Patent 11767766 Turbomachine airfoil having impingement cooling passages
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US Patent 09335050 Gas turbine engine combustor US Patent 9335050 Gas turbine engine combustor

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Patent Number
0933505000
Patent Number
933505000
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=0933505000
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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
093350500
Date of Patent
May 10, 2016
0
Patent Application Number
136276880
Date Filed
September 26, 2012
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=093350500
Patent Primary Examiner
Ehud Halberstam
Ehud Halberstam
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edited on 24 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
093350500
Date of Patent
May 10, 2016
0
Patent Application Number
136276880
Date Filed
September 26, 2012
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=093350500
Patent Primary Examiner
Ehud Halberstam
Ehud Halberstam
0
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=09335050
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 US Patent 09335050 Gas turbine engine combustor

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
09335050
Date of patent
May 10, 2016
Patent application number
13627688
Date Filed
September 26, 2012
Patent primary examiner
Ehud Halberstam
Ehud Halberstam

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