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US Patent 11306654 Gas turbine engine system wear reduction

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
November 26, 2019
Date of Patent
April 19, 2022
Patent Application Number
16695290
Patent Citations
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US Patent 10125691 Bowed rotor start using a variable position starter valve
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US Patent 10174678 Bowed rotor start using direct temperature measurement
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US Patent 10208629 Piezo-electric motor for bowed rotor mitigation
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US Patent 10221774 Speed control during motoring of a gas turbine engine
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US Patent 10358936 Bowed rotor sensor system
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US Patent 10436064 Bowed rotor start response damping system
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US Patent 10443507 Gas turbine engine bowed rotor avoidance system
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US Patent 10539079 Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
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US Patent 10718231 Method and system for mitigating bowed rotor operation of gas turbine engine
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US Patent 10760498 System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11306654
Patent Primary Examiner
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Katheryn A Malatek

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