US Patent 10533437 Inner diffuser case for a gas turbine engine
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Patent abstract
A combustor section of a gas turbine engine has a diffuser case with a structural cone having variable wall thicknesses strategically located for reducing localized stress in the cone.
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Patent Inventor Names
Swati G. Bhanderi0
Timothy Dale0
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Patent Number
105334370
Date of Patent
January 14, 2020
0Patent Application Number
150294740
Date Filed
October 31, 2014
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US Patent 10533437 Inner diffuser case for a gas turbine engine
Infobox
Is a
Patent jurisdiction
Patent number
10533437
Date of patent
January 14, 2020
Patent application number
15029474
Date Filed
October 31, 2014
Patent primary examiner
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