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US Patent 10267237 Return flow powered turbine

Patent 10267237 was granted and assigned to Rolls-Royce on April, 2019 by the United States Patent and Trademark Office.

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Patent Citations Received
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US Patent 11959423 Modulating fuel for a turbine engine
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US Patent 11946420 Fuel systems having thermal recirculation
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Patent Citations Received
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US Patent 11859552 Flow recirculative power system
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Patent abstract

A fuel system for an aircraft is provided having an improved fluid circuit and method of operation. Un-burnt fuel is directed via a return loop towards a fuel tank reservoir. A turbine is located in the return loop and upstream from the fuel tank. The pressurized un-burnt fuel energizes the turbine and the fuel passes to the fuel tank. The turbine is harnessed to a generator for providing a power.

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Patent Inventor Names
Andrew J. Pool0
Joel M. Rubel0
Perry J. Patzer0
Stephen E. Hollander0
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10267237
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Patent Citations Received
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US Patent 11629652 Metering pump system
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Patent citations received
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US Patent 11396848 Modulating fuel for a turbine engine
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10267237
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 US Patent 10267237 Return flow powered turbine

Infobox
Is a
Patent
Patent
Patent applicant
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Rolls-Royce
Current assignee
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Rolls-Royce
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10267237
Date of patent
April 23, 2019
Patent application number
15067921
Date Filed
March 11, 2016
Patent primary examiner
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Jesse S Bogue

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