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US Patent 10590867 Method of operating an engine assembly

Patent 10590867 was granted and assigned to Pratt & Whitney Canada on March, 2020 by the United States Patent and Trademark Office.

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Is a
Patent
Patent
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Patent attributes

Patent Applicant
Pratt & Whitney Canada
Pratt & Whitney Canada
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Current Assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
105908670
Patent Inventor Names
Bruno Villeneuve0
Jean Thomassin0
Mike Fontaine0
Date of Patent
March 17, 2020
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Patent Application Number
157089190
Date Filed
September 19, 2017
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Patent Citations Received
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US Patent 11506040 Automated diagnostics of electronic instrumentation in a system for fracturing a well and associated methods
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US Patent 11512642 Direct drive unit removal system and associated methods
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US Patent 11530602 Power sources and transmission networks for auxiliary equipment onboard hydraulic fracturing units and associated methods
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US Patent 12092100 Systems and method for use of single mass flywheel alongside torsional vibration damper assembly for single acting reciprocating pump
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US Patent 11460368 Fuel, communications, and power connection systems and related methods
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US Patent 11466680 Systems and methods of utilization of a hydraulic fracturing unit profile to operate hydraulic fracturing units
...
Patent Primary Examiner
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Patrick D Maines
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Patent abstract

A method of operating a compoundable engine that includes a turbine having a turbine shaft and an intermittent internal combustion engine having an engine shaft. The engine shaft is rotated at a first rotational speed. The turbine is driven by exhaust gases of the intermittent internal combustion engine to rotate the turbine shaft while the engine shaft rotates independently from the turbine shaft. A rotatable load is driven with the turbine shaft. A rotational speed of the engine shaft is increased from the first rotational speed until the turbine shaft reaches a predetermined rotational speed. After the turbine shaft has reached the predetermined rotational speed, the rotational speed of the engine shaft is adjusted until the turbine shaft and the engine shaft are drivingly engageable with each other, and the turbine shaft with the engine shaft are engaged such that both are in driving engagement with the rotatable load.

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