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US Patent 10975731 Turbine engine, components, and methods of cooling same

Patent 10975731 was granted and assigned to General Electric on April, 2021 by the United States Patent and Trademark Office.

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Is a
Patent
Patent
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Patent attributes

Patent Applicant
General Electric
General Electric
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Current Assignee
General Electric
General Electric
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
109757310
Patent Inventor Names
Timothy Deryck Stone0
Victor Hugo Silva Correia0
Curtis Walton Stover0
Gregory Michael Laskowski0
Jared Peter Buhler0
John Howard Starkweather0
Jonathan Russell Ratzlaff0
Robert Carl Murray0
...
Date of Patent
April 13, 2021
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Patent Application Number
153143410
Date Filed
May 28, 2015
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Patent Citations Received
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US Patent 11541340 Inducer assembly for a turbine engine
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US Patent 11918943 Inducer assembly for a turbine engine
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Patent Primary Examiner
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Scott J Walthour
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Patent abstract

A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser configured to increase the angular velocity of a fluid stream, a flow splitter configured to split the fluid stream to form a concentrated-particle stream and a reduced-particle stream, and an exit conduit configured to receive the reduced-particle stream. An inducer assembly for a turbine engine includes an inducer with a flow passage having an inducer inlet and an inducer outlet in fluid communication with a turbine section of the engine, and a particle separator, which includes a particle concentrator that receives a compressed stream from a compressor section of the engine and a flow splitter. A turbine engine includes a cooling air flow circuit which supplies a fluid stream to a turbine section of the engine for cooling, a particle separator located within the cooling air flow circuit, and an inducer forming a portion of the cooling air flow circuit in fluid communication with the particle separator. A method of cooling a rotating blade of a turbine engine having an inducer includes directing a cooling fluid stream from a portion of turbine engine toward the rotating blade, separating particles from the cooling fluid stream by passing the cooling fluid stream through a inertial separator, accelerating a reduced-particle stream emitted from the inertial separator to the speed of the rotating blade, and orienting the reduced-particle stream by emitting the reduced-particle stream from the inertial separator into a cooling passage in the inducer.

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