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US Patent 10837640 Combustion section of a gas turbine engine

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Patent Citations Received
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US Patent 11859819 Ceramic composite combustor dome and liners
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=108376400
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Patent Citations Received
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US Patent 11353215 Lean burn combustor
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Patent Citations Received
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US Patent 11603993 Combustor with improved aerodynamics
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Infobox
Is a
Patent
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
108376400
Date of Patent
November 17, 2020
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Patent Application Number
154503080
Date Filed
March 6, 2017
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=108376400
Patent Citations
‌
US Patent 10012387 Fuel supply system for a gas turbine engine
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Patent Citations Received
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US Patent 11339970 Combustor with improved aerodynamics
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US Patent 11353215 Lean burn combustor
0
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US Patent 11402099 Combustor with improved aerodynamics
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Patent Primary Examiner
Ehud Halberstam
Ehud Halberstam
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Patent citations received
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US Patent 11402099 Combustor with improved aerodynamics
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10837640
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edited on 9 Jun, 2022
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Patent citations received
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US Patent 11353215 Lean burn combustor
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Patent citations received
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US Patent 11339970 Combustor with improved aerodynamics
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 US Patent 10837640 Combustion section of a gas turbine engine

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10837640
Date of patent
November 17, 2020
Patent application number
15450308
Date Filed
March 6, 2017
Patent citations
‌
US Patent 10012387 Fuel supply system for a gas turbine engine
Patent primary examiner
Ehud Halberstam
Ehud Halberstam

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