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US Patent 11702952 Thermal bias control in turbomachines

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Current Assignee
General Electric
General Electric
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Date Filed
November 11, 2021
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Date of Patent
July 18, 2023
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Patent Applicant
General Electric
General Electric
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Patent Application Number
17524196
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Patent Citations
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US Patent 8918264 Method and device for monitoring a turbine engine of an aircraft
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US Patent 8820046 Methods and systems for mitigating distortion of gas turbine shaft
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US Patent 10508601 Auxiliary drive bowed rotor prevention system for a gas turbine engine
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US Patent 10787933 Low-power bowed rotor prevention and monitoring system
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US Patent 10174678 Bowed rotor start using direct temperature measurement
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US Patent 10443505 Bowed rotor start mitigation in a gas turbine engine
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US Patent 10443507 Gas turbine engine bowed rotor avoidance system
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US Patent 10508567 Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11702952
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Patent Primary Examiner
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Loren C Edwards
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CPC Code
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F01D 25/12
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F05D 2220/323
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F05D 2260/232
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F05D 2260/85
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F05D 2270/112
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F05D 2270/3032
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F02C 7/12
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F02C 7/16
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F02C 7/18
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F02C 7/26
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