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US Patent 10371383 Unitary flow path structure

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
January 27, 2017
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Date of Patent
August 6, 2019
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Patent Application Number
15417602
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Patent Citations Received
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US Patent 11428160 Gas turbine engine with interdigitated turbine and gear assembly
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US Patent 11286799 Methods and assemblies for attaching airfoils within a flow path
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US Patent 12110802 Full hoop ceramic matrix composite vane endwall integration with turbine shroud ring and mounting thereof
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US Patent 11859819 Ceramic composite combustor dome and liners
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US Patent 11879362 Segmented ceramic matrix composite vane endwall integration with turbine shroud ring and mounting thereof
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US Patent 11384651 Methods and features for positioning a flow path inner boundary within a flow path assembly
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US Patent 11391171 Methods and features for positioning a flow path assembly within a gas turbine engine
Patent Inventor Names
Brandon ALlanson Reynolds
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Aaron Michael Dziech
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Andrew Scott Bilse
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Ernesto Andres Vallejo Ruiz
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Jonathan David Baldiga
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Mark Eugene Noe
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Michael Todd Radwanski
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10371383
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Patent Primary Examiner
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Jason H Duger
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