US Patent 10352566 Gas turbine engine combustor liner panel
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Patent abstract
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a hemi-spherical protuberance.
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Patent Number
103525660
Date of Patent
July 16, 2019
0Patent Application Number
148965760
Date Filed
April 14, 2014
0Official Website
Patent Primary Examiner
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Patent Applicant
Patent Jurisdiction
Patent Number
103525660
Date of Patent
July 16, 2019
0Patent Application Number
148965760
Date Filed
April 14, 2014
0Official Website
Patent Primary Examiner
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US Patent 10352566 Gas turbine engine combustor liner panel
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10352566
Date of patent
July 16, 2019
Patent application number
14896576
Date Filed
April 14, 2014
Patent primary examiner
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