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US Patent 8876465 Gas turbine engine

Patent 8876465 was granted and assigned to Rolls-Royce on November, 2014 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Rolls-Royce
Rolls-Royce
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Date Filed
April 15, 2011
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Date of Patent
November 4, 2014
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Patent Application Number
13087877
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Patent Citations Received
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US Patent 12071896 Air-to-air heat exchanger potential in gas turbine engines
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US Patent 12018575 Turbine engine with a cowl door
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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 12065989 Gas turbine engine with third stream
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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 11834992 Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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US Patent 11834954 Gas turbine engine with third stream
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US Patent 11834995 Air-to-air heat exchanger potential in gas turbine engines
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•••
Patent Inventor Names
Richard G. Stretton
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
8876465
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Patent Primary Examiner
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Edward Look
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