US Patent 9863538 Gas turbine engine brush seal with supported tip
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Patent abstract
As assembly is provided for a gas turbine engine. This assembly includes a component and a brush seal. The component includes a first surface and a second surface. The brush seal includes an annular bundle of bristles which extends longitudinally along an axis to a bundle tip. The bundle of bristles axially contacts the first surface at the bundle tip. The bundle of bristles proximate the bundle tip axially overlaps the second surface, and the bundle of bristles is operable to radially contact the second surface.
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Patent Inventor Names
Brian Duguay0
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US Patent 09863538 Gas turbine engine brush seal with supported tip US Patent 9863538 Gas turbine engine brush seal with supported tip
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Patent Number
098635380
Patent Number
98635380
Edits on 27 Mar, 2023
Golden AI
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Patent Applicant
Patent Jurisdiction
Patent Number
098635380
Date of Patent
January 9, 2018
0Patent Application Number
146971040
Date Filed
April 27, 2015
0Patent Primary Examiner
Edits on 16 Jan, 2022
Golden AI
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US Patent 09863538 Gas turbine engine brush seal with supported tip
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
09863538
Date of patent
January 9, 2018
Patent application number
14697104
Date Filed
April 27, 2015
Patent primary examiner
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