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US Patent 10578028 Compressor bleed auxiliary turbine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
August 18, 2015
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Date of Patent
March 3, 2020
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Patent Application Number
14828542
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Patent Citations
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US Patent 10100744 Aircraft bleed air and engine starter systems and related methods
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US Patent 10267153 Gas turbine, gas turbine control device, and gas turbine cooling method
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Patent Citations Received
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US Patent 12135076 Fluid device(s) for supporting rotating structure(s) of a turbine engine
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US Patent 11939926 Selective power distribution for an aircraft propulsion system
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US Patent 12060829 Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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US Patent 12071896 Air-to-air heat exchanger potential in gas turbine engines
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US Patent 12078107 Gas turbine engine
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US Patent 10920602 Tip clearance control system
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US Patent 11073091 Gas turbine engine with integrated air cycle machine
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US Patent 11680530 Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
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US Patent 11834995 Air-to-air heat exchanger potential in gas turbine engines
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US Patent 11834992 Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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Patent Inventor Names
Thomas Lee Becker, Jr.
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10578028
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Patent Primary Examiner
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William H Rodríguez
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