US Patent 10955140 Combustor for gas turbine engine
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Patent abstract
A gas turbine engine comprises a combustor. The combustor comprises an annular combustor chamber formed between an inner liner and an outer liner spaced apart from the inner liner. An annular fuel manifold has fuel nozzles distributed circumferentially on the fuel manifold, the fuel manifold and fuel nozzles positioned entirely inside the combustion chamber.
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Patent Number
109551400
Date of Patent
March 23, 2021
0Patent Application Number
153634180
Date Filed
November 29, 2016
0Official Website
Patent Primary Examiner
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Patent Jurisdiction
Patent Number
109551400
Date of Patent
March 23, 2021
0Patent Application Number
153634180
Date Filed
November 29, 2016
0Official Website
Patent Primary Examiner
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US Patent 10955140 Combustor for gas turbine engine
Infobox
Is a
Patent jurisdiction
Patent number
10955140
Date of patent
March 23, 2021
Patent application number
15363418
Date Filed
November 29, 2016
Patent primary examiner
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