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US Patent 9845692 Turbine component connection with thermally stress-free fastener
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Patent
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Date Filed
May 5, 2015
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Date of Patent
December 19, 2017
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Patent Application Number
14704406
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Patent Citations Received
US Patent 11939886 Aircraft engine having stator vanes made of different materials
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US Patent 12091178 Aircraft engine with stator having varying geometry
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US Patent 12017782 Aircraft engine with stator having varying pitch
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Patent Inventor Names
Joshua Brian Jamison
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
9845692
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Patent Primary Examiner
Igor Kershteyn
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