US Patent 10100672 Fluid-cooled seal arrangement for a gas turbine engine
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Patent abstract
A component for a gas turbine engine includes a compartment housing that redirects oil from at least one passage in a rotational component onto a backside of a seal land.
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Patent Inventor Names
Garth J Vdoviak, Jr.0
Gary L Grogg0
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Patent Number
101006720
Date of Patent
October 16, 2018
0Patent Application Number
147718670
Date Filed
March 7, 2014
0Patent Citations Received
Patent Primary Examiner
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US Patent 10100672 Fluid-cooled seal arrangement for a gas turbine engine
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10100672
Date of patent
October 16, 2018
Patent application number
14771867
Date Filed
March 7, 2014
Patent primary examiner
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