US Patent 10830154 Gas turbine engine having fan shaft stiffness ratio
Patent 10830154 was granted and assigned to Rolls-Royce on November, 2020 by the United States Patent and Trademark Office.
Is a
Current Assignee
Date Filed
March 3, 2020
Date of Patent
November 10, 2020
Patent Applicant
Patent Application Number
16807786
Patent Citations Received
Patent Jurisdiction
Patent Number
Patent Primary Examiner
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