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US Patent 10344711 System and method of alleviating blade flutter

Patent 10344711 was granted and assigned to Rolls-Royce on July, 2019 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributors
Is a
Patent
Patent
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Current Assignee
‌
Rolls-Royce
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Date Filed
January 11, 2016
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Date of Patent
July 9, 2019
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Patent Applicant
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Rolls-Royce
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Patent Application Number
14992719
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Patent Citations Received
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US Patent 12116929 Bleed flow assembly for a gas turbine engine
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US Patent 11767790 Object direction mechanism for turbofan engine
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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US Patent 12085019 Object direction mechanism for turbofan engine
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US Patent 11480063 Gas turbine engine with inlet pre-swirl features
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US Patent 11655768 High fan up speed engine
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Patent Inventor Names
Kwen Hsu
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10344711
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Patent Primary Examiner
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Jason D Shanske
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