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US Patent 8397487 Environmental control system supply precooler bypass

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
February 28, 2011
Date of Patent
March 19, 2013
Patent Application Number
13036534
Patent Citations Received
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US Patent 12116929 Bleed flow assembly for a gas turbine engine
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US Patent 11834995 Air-to-air heat exchanger potential in gas turbine engines
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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
0
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US Patent 12071896 Air-to-air heat exchanger potential in gas turbine engines
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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 11773742 Cooled cooling air for blade air seal through outer chamber
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US Patent 11773780 Intercooled cooling air with selective pressure dump
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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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 Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8397487
Patent Primary Examiner
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William H. Rodriguez

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