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US Patent 11668197 Internally damped airfoiled component
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Patent
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Date Filed
May 20, 2020
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Date of Patent
June 6, 2023
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Patent Application Number
16879274
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Patent Citations
US Patent 7690112 Process and apparatus for producing a turbine component, turbine component and use of the apparatus
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US Patent 7810237 Method for repairing and/or modifying component parts of a gas turbine
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US Patent 7905016 System for forming a gas cooled airfoil for use in a turbine engine
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US Patent 7984547 Method for manufacturing and/or repairing components for gas turbines
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US Patent 7966707 Method for repairing superalloy components using inserts
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US Patent 8240046 Methods for making near net shape airfoil leading edge protection
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US Patent 7300256 Damping arrangement for a blade of an axial turbine
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US Patent 7358457 Nozzle for laser net shape manufacturing
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11668197
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Patent Primary Examiner
Courtney D Heinle
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CPC Code
F01D 5/18
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F01D 5/16
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F01D 25/06
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F05D 2260/96
0
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