Invention Grant
- Patent Title: Turbine engine, components, and methods of cooling same
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Application No.: US15314341Application Date: 2015-05-28
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Publication No.: US10975731B2Publication Date: 2021-04-13
- Inventor: Robert Francis Manning , Timothy Deryck Stone , Jared Peter Buhler , Victor Hugo Silva Correia , Gregory Michael Laskowski , Robert Carl Murray , Jonathan Russell Ratzlaff , Robert Proctor , John Howard Starkweather , Curtis Walton Stover
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: McGarry Bair PC
- International Application: PCT/US2015/032855 WO 20150528
- International Announcement: WO2016/032585 WO 20160303
- Main IPC: B01D45/16
- IPC: B01D45/16 ; F02C7/05 ; F02C7/052 ; F01D25/32 ; B04C3/06 ; B04C3/00 ; B64D33/08 ; F01D5/08 ; F01D25/12 ; F02C3/04 ; F02C7/18 ; F02C9/18 ; B64D33/02

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.
Public/Granted literature
- US20170101896A1 TURBINE ENGINE, COMPONENTS, AND METHODS OF COOLING SAME Public/Granted day:2017-04-13
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