US Patent 10228136 Combustor assembly
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Patent abstract
A combustor assembly for a gas turbine engine is includes a liner and a combustor dome formed of a ceramic matrix composite material. The combustor dome and liner together define at least in part a combustion chamber. The combustor dome extends along a circumferential direction and defines one or more openings, the combustor dome is configured to receive one or more fuel-air injector hardware assemblies in or through the one or more openings.
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Patent Inventor Names
David Andrew Hannwacker0
Stephen John Howell0
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Patent Jurisdiction
Patent Number
102281360
Date of Patent
March 12, 2019
0Patent Application Number
150533980
Date Filed
February 25, 2016
0Patent Primary Examiner
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US Patent 10228136 Combustor assembly
Infobox
Is a
Patent jurisdiction
Patent number
10228136
Date of patent
March 12, 2019
Patent application number
15053398
Date Filed
February 25, 2016
Patent primary examiner
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