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US Patent 10436122 Fuel-air ratio control of gas turbine engines

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
April 7, 2015
Date of Patent
October 8, 2019
Patent Application Number
14680369
Patent Citations Received
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US Patent 11480112 Acceleration of a gas turbine
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US Patent 11988098 Increasing surge margin and compression efficiency via shaft power transfer
0
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US Patent 12006880 High bandwidth control of turbofan/turboprop thrust response using embedded electric machines
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US Patent 12060834 Hybrid electric idle and braking for an aircraft
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US Patent 11268454 Preventing surge
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US Patent 11326526 Deceleration of a gas turbine
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US Patent 11384696 Reducing low flight mach number fuel consumption
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10436122
Patent Primary Examiner
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Thai-Ba Trieu

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