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US Patent 8967967 Propfan engine

Patent 8967967 was granted and assigned to Rolls-Royce on March, 2015 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Current Assignee
Rolls-Royce
Rolls-Royce
Date Filed
January 26, 2012
Date of Patent
March 3, 2015
Patent Application Number
13359194
Patent Citations Received
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US Patent 12103702 Removeable fuselage shield for an aircraft
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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 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 11753144 Unducted propulsion system
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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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US Patent 11834196 System and method for control for unducted engine
0
•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8967967
Patent Primary Examiner
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Igor Kershteyn

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