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US Patent 10352824 Method for evaluating turbine engine system stability
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Patent
Date Filed
November 12, 2014
Date of Patent
July 16, 2019
Patent Application Number
14538996
Patent Citations Received
US Patent 11506571 System and method for gathering flight load data
US Patent 11022524 Stochastic configuration network based turbofan engine health parameter estimation method
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Patent Inventor Names
Kenneth William Simon
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Dean Frederick Long
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Grant August Radinzel
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Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
10352824
Patent Primary Examiner
Leslie J. Evanisko
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