US Patent 10202863 Seal ring for gas turbine engines
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Patent abstract
An annular ring for sealing a flow includes an inner ring and a tab. The tab extends radially and is configured to restrict axial movement of the seal.
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Patent Inventor Names
Mark F. Zelesky0
Michael G. McCaffrey0
Timothy M. Davis0
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Patent Number
102028630
Date of Patent
February 12, 2019
0Patent Application Number
151620690
Date Filed
May 23, 2016
0Patent Citations Received
Patent Primary Examiner
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US Patent 10202863 Seal ring for gas turbine engines
Infobox
Is a
Patent jurisdiction
Patent number
10202863
Date of patent
February 12, 2019
Patent application number
15162069
Date Filed
May 23, 2016
Patent primary examiner
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