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US Patent 8459035 Gas turbine engine with low fan pressure ratio

Patent 8459035 was granted and assigned to United Technologies on June, 2013 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Current Assignee
United Technologies
United Technologies
Date Filed
December 30, 2011
Date of Patent
June 11, 2013
Patent Application Number
13340761
Patent Citations Received
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US Patent 12071896 Air-to-air heat exchanger potential in gas turbine engines
3
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US Patent 11988099 Unducted thrust producing system architecture
4
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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
5
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US Patent 12065989 Gas turbine engine with third stream
6
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US Patent 11781447 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
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US Patent 11781505 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
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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
7
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US Patent 11834954 Gas turbine engine with third stream
8
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US Patent 11834995 Air-to-air heat exchanger potential in gas turbine engines
9
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US Patent 11859516 Gas turbine engine with third stream
10
•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8459035
Patent Primary Examiner
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Phutthiwat Wongwian

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