US Patent 11066955 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 Number
110669550
Date of Patent
July 20, 2021
0Patent Application Number
161275240
Date Filed
September 11, 2018
0Official Website
Patent Citations
Patent Primary Examiner
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Patent Number
110669550
Date of Patent
July 20, 2021
0Patent Application Number
161275240
Date Filed
September 11, 2018
0Official Website
Patent Citations
Patent Primary Examiner
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US Patent 11066955 Fluid-cooled seal arrangement for a gas turbine engine
Infobox
Is a
Patent jurisdiction
Patent number
11066955
Date of patent
July 20, 2021
Patent application number
16127524
Date Filed
September 11, 2018
Patent citations
Patent primary examiner
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