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公开(公告)号：US20170101894A1
公开(公告)日：2017-04-13
申请号：US15314487
申请日：2015-05-27
Applicant: General Electric Company
Inventor： Phebe Helena PREETHI , William Thomas BENNETT , John Howard STARKWEATHER , Timothy Deryck STONE
CPC classification number: F01D25/12 , F01D5/189 , F01D9/041 , F01D11/08 , F02C7/12 , F05D2220/32 , F05D2240/127 , F05D2240/35 , F05D2250/38 , F05D2260/201 , F05D2260/202 , F05D2260/22141 , F23R3/002 , F23R2900/03044 , Y02T50/673 , Y02T50/676
Abstract: An engine component assembly is provided for impingement cooling including discrete cooling features. An insert is located opposite and adjacent to a cooled surface of the engine component and includes a plurality of angled impingement air holes. A cooling fluid flow path is flowing on one side the cooled surface of the engine component and adjacent to the insert and passes through the angled cooling holes of the insert in order to cool the cooled surface of the engine component. Additionally, a plurality of discrete cooling features may be located along the cooled surface of the engine component opposite the plurality of cooling holes in the insert.
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公开(公告)号：US20230226476A1
公开(公告)日：2023-07-20
申请号：US17993082
申请日：2022-11-23
Applicant: General Electric Company
Inventor： Timothy Deryck STONE , Gregory Michael LASKOWSKI , Robert PROCTOR , Curtis STOVER , Robert Francis Manning , Victor Hugo Silva CORREIA , Jared Peter BUHLER , Robert Carl MURRAY , Corey BOURASSA , Byron Andrew PRITCHARD, JR. , Jonathan Russell RATZLAFF
CPC classification number: B01D45/16 , B04C3/06 , F01D5/189 , F01D9/065 , F02C6/08 , F02C7/18 , F02C7/052 , B04C2003/003 , F05D2260/607
Abstract: A turbine engine having a compressor section, a combustor section, a turbine section, and a rotatable drive shaft that couples a portion of the turbine section and a portion of the compressor section. A bypass conduit couples the compressor section to the turbine section while bypassing at least the combustion section. At least one particle separator is located in the turbine engine having a separator inlet that receives a bypass stream, a separator outlet that receives a reduced-particle stream flows, and a particle outlet that receives a concentrated-particle stream comprising separated particles. A conduit, fluidly coupled to the particle outlet, extends through an interior of at least one stationary vane.
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公开(公告)号：US20210275951A1
公开(公告)日：2021-09-09
申请号：US17325650
申请日：2021-05-20
Applicant: General Electric Company
Inventor： Timothy Deryck STONE , Gregory Michael LASKOWSKI , Robert PROCTOR , Curtis STOVER , Robert Francis Manning , Victor Hugo Silva CORREIA , Jared Peter BUHLER , Robert Carl MURRAY , Corey BOURASSA , Byron Andrew PRITCHARD, JR. , Jonathan Russell RATZLAFF
Abstract: A turbine engine having an inducer assembly. The inducer assembly includes a centrifugal separator fluidly coupled to an inducer with an inducer inlet and an inducer outlet. The centrifugal separator includes a body, an angular velocity increaser to form a concentrated-particle stream and a reduced-particle stream, a flow splitter, and an exit conduit fluidly coupled to the body to receive the reduced-particle stream and define a separator outlet.
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Patent Agency Ranking
公开(公告)号：US20250010231A1
公开(公告)日：2025-01-09
申请号：US18442719
申请日：2024-02-15
Applicant: General Electric Company
Inventor： Timothy Deryck STONE , Gregory Michael LASKOWSKI , Robert PROCTOR , Curtis STOVER , Robert Francis Manning , Victor Hugo Silva CORREIA , Jared Peter BUHLER , Robert Carl MURRAY , Corey BOURASSA , Byron Andrew PRITCHARD, Jr. , Jonathan Russell RATZLAFF
IPC: B01D45/16 , B04C3/00 , B04C3/06 , F01D5/18 , F01D9/06 , F02C6/08 , F02C7/052 , F02C7/18 , F02K3/04
Abstract: A turbine engine having a compressor section, a combustor section, a turbine section, and a rotatable drive shaft. A bypass conduit couples the compressor section to the turbine section. At least one centrifugal separator is fluidly coupled to the bypass stream, where the at least one centrifugal separator includes a body, a center body, a separator inlet, and a separator outlet fluidly coupled with the turbine section to output a reduced-particle stream that is provided to the turbine section for cooling. The centrifugal separator includes an angular velocity increaser, a flow splitter, a first outlet passage defined by an inner annular wall that receives the reduced-particle stream, and an angular velocity decreaser located downstream of the flow splitter. A second outlet passage receives the concentrated-particle stream.
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公开(公告)号：US20180274370A1
公开(公告)日：2018-09-27
申请号：US15522830
申请日：2015-10-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ronald Scott BUNKER , Timothy Deryck STONE
CPC classification number: F01D5/186 , F05D2250/181 , F05D2250/184 , F05D2250/24 , F05D2250/292 , F05D2250/294 , F05D2250/51 , F05D2250/70 , F05D2260/202 , F23R3/002 , F23R3/005 , F23R3/06 , F23R2900/03042 , Y02T50/672 , Y02T50/676
Abstract: An engine component for a gas turbine engine includes a film-cooled wall having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. The wall includes one or more film holes that have an outlet provided on the hot surface and a contoured inlet provided on the cooling surface. A contoured portion in the cooling surface encompasses the inlets for two or more film holes in the wall.
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公开(公告)号：US20170114720A1
公开(公告)日：2017-04-27
申请号：US15314536
申请日：2015-05-29
Applicant: General Electric Company
Inventor： Timothy Deryck STONE , Gregory Michael LASKOWSKI , Robert PROCTOR , Curtis STOVER , Robert Francis Manning , Victor Hugo Silva CORREIA , Jared Peter BUHLER , Robert Carl MURRAY , Corey BOURASSA, Jr. , Byron Andrew PRITCHARD , Jonathan Russell RATZLAFF
CPC classification number: B01D45/16 , B04C3/06 , B04C2003/003 , B04C2003/006 , F02C6/08 , F02C7/18 , F05D2260/607 , Y02T50/675
Abstract: A turbine engine having a bypass fluid conduit coupled to the turbine section includes at least one particle separator located within the bypass fluid conduit to separate particles from a bypass fluid stream prior to the bypass stream reaching the turbine section for cooling. A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser, a particle outlet, an angular velocity decreaser downstream of the angular velocity increaser, and a bend provided between the angular velocity increaser and the angular velocity decreaser.
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公开(公告)号：US20170101896A1
公开(公告)日：2017-04-13
申请号：US15314341
申请日：2015-05-28
Applicant: GENERAL ELECTRIC COMPANY
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
CPC classification number: F01D25/32 , B01D45/16 , B04C3/00 , B04C3/06 , B04C2003/003 , B04C2003/006 , B64D33/08 , B64D2033/022 , B64D2033/024 , B64D2033/0246 , F01D5/08 , F01D25/12 , F02C3/04 , F02C7/05 , F02C7/052 , F02C7/18 , F02C9/18 , F05D2220/32 , F05D2240/35
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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公开(公告)号：US20150345397A1
公开(公告)日：2015-12-03
申请号：US14717547
申请日：2015-05-20
Applicant: General Electric Company
Inventor： Ronald Scott BUNKER , Jason Randolph ALLEN , Ryan Nicholas PORTER , Byron Andrew PRITCHARD , Christopher Joseph GREENWELL , Timothy Deryck STONE , Andrew Stephen Pritchard
CPC classification number: F01D5/188 , F01D5/186 , F01D5/189 , F01D9/04 , F01D25/12 , F02C7/18 , F05D2220/32 , F05D2240/35 , F05D2250/38 , F05D2260/201 , F05D2260/202 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044 , Y02T50/676
Abstract: An engine component with particulate mitigation features is provided. The engine component comprises an internal engine component surface having a cooling flow path on one side thereof and a second component adjacent to the first component. The second component, for example an insert, may have a plurality of openings forming an array wherein the openings extend through the second component at a non-orthogonal angle to the surface of the second component.
Abstract translation: 提供了具有微粒减轻特征的发动机部件。 发动机部件包括内部发动机部件表面，该内部发动机部件表面具有在其一侧上的冷却流动路径和与第一部件相邻的第二部件。 第二部件，例如插入件，可以具有形成阵列的多个开口，其中开口以与第二部件的表面成非正交角延伸穿过第二部件。
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