US Patent 10429070 Combustor assembly
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Patent abstract
A combustor assembly for a gas turbine engine includes a combustor dome and a combustion chamber liner formed integrally of a ceramic matrix composite material. The combustor dome defines a plurality of openings for receiving a respective plurality of fuel air injector hardware assemblies and may extend continuously along a circumferential direction.
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Patent Inventor Names
David Andrew Hannwacker0
Stephen John Howell0
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Patent Number
104290700
Date of Patent
October 1, 2019
0Patent Application Number
150533690
Date Filed
February 25, 2016
0Official Website
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US Patent 10429070 Combustor assembly
Infobox
Is a
Patent jurisdiction
Patent number
10429070
Date of patent
October 1, 2019
Patent application number
15053369
Date Filed
February 25, 2016
Patent primary examiner
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