- 专利标题: Turbine engine, components, and methods of cooling same
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申请号: US15314341申请日: 2015-05-28
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公开(公告)号: US10975731B2公开(公告)日: 2021-04-13
- 发明人: 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
- 申请人: GENERAL ELECTRIC COMPANY
- 申请人地址: US NY Schenectady
- 专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人地址: US NY Schenectady
- 代理机构: McGarry Bair PC
- 国际申请: PCT/US2015/032855 WO 20150528
- 国际公布: WO2016/032585 WO 20160303
- 主分类号: B01D45/16
- IPC分类号: 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
摘要:
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.
公开/授权文献
- US20170101896A1 TURBINE ENGINE, COMPONENTS, AND METHODS OF COOLING SAME 公开/授权日:2017-04-13
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