US Patent 9759133 Turbofan with variable bypass flow
Patent 9759133 was granted and assigned to Rolls-Royce on September, 2017 by the United States Patent and Trademark Office.
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Patent abstract
A gas turbine engine is disclosed with a bypass flow path having a bypass nozzle positioned downstream of a fan; a core flow path having a compressor, a combustor, a turbine and an exhaust nozzle; an auxiliary duct fluidly connecting the core flow path and the bypass flow path downstream of the turbine; and a control valve operably connected to the auxiliary duct to control fluid flow from the core flow path into the bypass flow path.
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Patent Inventor Names
Dmitriy B. Sidelkovskly0
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US Patent 09759133 Turbofan with variable bypass flow US Patent 9759133 Turbofan with variable bypass flow
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Patent Number
09759133
Patent Number
9759133
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US Patent 09759133 Turbofan with variable bypass flow
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Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
09759133
Date of patent
September 12, 2017
Patent application number
14199237
Date Filed
March 6, 2014
Patent primary examiner
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