-
公开(公告)号：US10036319B2
公开(公告)日：2018-07-31
申请号：US14867379
申请日：2015-09-28
Applicant: General Electric Company
Inventor： Robert Carl Murray , Corey Bourassa , David Vickery Parker , Byron Andrew Pritchard, Jr. , Jonathan Russell Ratzlaff , William Collins Vining , Erich Alois Krammer
CPC classification number: F02C7/052 , B01D45/12 , B01D45/16 , B01D50/002 , B04C3/00 , B04C3/04 , B04C3/06 , B04C2003/006
Abstract: A separator assembly for removing entrained particles from a fluid stream passing through a gas turbine engine includes a first particle separator for separating the fluid stream into a reduced-particle stream and a particle-laden stream, and emitting the particle-laden stream through a scavenge outlet. Another particle remover is fluidly coupled to the scavenge outlet to remove more particles from the air stream.
-
公开(公告)号：US20170128867A1
公开(公告)日：2017-05-11
申请号：US14933749
申请日：2015-11-05
Applicant: General Electric Company
Inventor： William Collins Vining , Robert Francis Manning , Victor Hugo Silva Correia , Corey Bourassa , Jared Peter Buhler , Hojjat Nasr
CPC classification number: B01D45/04 , B01D45/08 , B01D46/0002 , B01D46/0004 , B01D46/0005 , B01D50/002 , B01D2265/06
Abstract: A filter system and method use a filter housing that defines an interior chamber and that includes an inlet opening extending into the interior chamber. The outer air flow housing has an outlet conduit through which a flow of air having particles is directed toward the inlet opening of the filter housing along a flow direction toward the interior chamber of the filter housing. The outer air flow housing engages the filter housing such that the filter housing is separated from the outer air flow housing along the flow direction to permit at least some of the air to pass around an exterior of the filter housing and exit the outer air flow housing while the particles in the at least some of the air pass into the interior chamber of the filter housing through the inlet opening.
-
公开(公告)号：US09512780B2
公开(公告)日：2016-12-06
申请号：US13955107
申请日：2013-07-31
Applicant: General Electric Company
Inventor： Corey Bourassa , William Dwight Gerstler
CPC classification number: F02C7/12 , F02C7/32 , F05D2260/213 , Y02T50/676 , Y10T29/49826
Abstract: A heat transfer assembly for controlling heat transfer of a turbine engine is provided. The turbine engine includes a housing and includes a compressor, a combustor and a turbine located within the housing. The heat transfer assembly includes a flow control device having a sidewall coupled to the turbine, the sidewall is in flow communication with a compressor vane. The sidewall is configured to define a first flow path from the compressor vane to a turbine vane and a second flow path from the compressor vane to a turbine blade. A heat exchanger is coupled to the housing and located between the compressor and the turbine, wherein the heat exchanger is in flow communication with at least one of the first flow path and the second flow path. A fluid supply device is coupled to the housing and in flow communication with the heat exchanger.
Abstract translation: 提供了一种用于控制涡轮发动机的传热的传热组件。 涡轮发动机包括壳体并且包括位于壳体内的压缩机，燃烧器和涡轮机。 传热组件包括具有连接到涡轮机的侧壁的流量控制装置，该侧壁与压缩机叶片流动连通。 侧壁被构造成限定从压缩机叶片到涡轮叶片的第一流动路径和从压缩机叶片到涡轮机叶片的第二流动路径。 热交换器耦合到壳体并且位于压缩机和涡轮机之间，其中热交换器与第一流动路径和第二流动路径中的至少一个流动连通。 流体供应装置联接到壳体并与热交换器流动连通。
-
公开(公告)号：US09249730B2
公开(公告)日：2016-02-02
申请号：US13755500
申请日：2013-01-31
Applicant: General Electric Company
Inventor： Corey Bourassa , William Dwight Gerstler
CPC classification number: F02C7/185 , F01D5/189 , F05D2240/129 , F05D2250/185 , F05D2260/201 , F05D2260/213 , F28D7/0058 , F28D2021/0026 , F28F13/06 , F28F2250/02
Abstract: An integrated inducer heat exchanger is provided. The integrated inducer heat exchanger includes multiple airfoil devices disposed in an annular array within an inner circular casing and an outer circular casing forming multiple passages for allowing a flow of fluid from a forward side to an aft side of the integrated inducer heat exchanger. The integrated inducer heat exchanger also includes multiple annular manifolds arranged about the outer circular casing configured for supplying a flow of coolant at low temperature from one or more coolant sources and returning the flow of coolant at high temperature to the one or more coolant sources via an external heat exchanger for dissipating heat and multiple transfer tubes connecting the multiple annular manifolds with the multiple airfoil devices for transferring the flow of coolant within the airfoil devices for exchanging heat between the coolant and the fluid passing through the multiple passages.
Abstract translation: 提供了一种综合的导流器热交换器。 集成导流器热交换器包括多个设置在内部圆形壳体内的环形阵列中的翼型装置和形成多个通道的外部圆形壳体，用于允许流体从一体式导流换热器的前侧流向后侧。 集成导流器热交换器还包括围绕外部圆形壳体布置的多个环形歧管，其构造成用于在低温下从一个或多个冷却剂源供应冷却剂流，并将高温下的冷却剂流通过一个或多个冷却剂源经由 用于散热的外部热交换器和将多个环形歧管与多个翼型装置连接的多个传输管，用于传递在翼型装置内的冷却剂流，以在冷却剂和通过多个通道的流体之间进行热交换。
-
公开(公告)号：US20150033761A1
公开(公告)日：2015-02-05
申请号：US13955107
申请日：2013-07-31
Applicant: General Electric Company
Inventor： Corey Bourassa , William Dwight Gerstler
CPC classification number: F02C7/12 , F02C7/32 , F05D2260/213 , Y02T50/676 , Y10T29/49826
Abstract: A heat transfer assembly for controlling heat transfer of a turbine engine is provided. The turbine engine includes a housing and includes a compressor, a combustor and a turbine located within the housing. The heat transfer assembly includes a flow control device having a sidewall coupled to the turbine, the sidewall is in flow communication with a compressor vane. The sidewall is configured to define a first flow path from the compressor vane to a turbine vane and a second flow path from the compressor vane to a turbine blade. A heat exchanger is coupled to the housing and located between the compressor and the turbine, wherein the heat exchanger is in flow communication with at least one of the first flow path and the second flow path. A fluid supply device is coupled to the housing and in flow communication with the heat exchanger.
Abstract translation: 提供了一种用于控制涡轮发动机的传热的传热组件。 涡轮发动机包括壳体并且包括位于壳体内的压缩机，燃烧器和涡轮机。 传热组件包括具有连接到涡轮机的侧壁的流量控制装置，该侧壁与压缩机叶片流动连通。 侧壁被构造成限定从压缩机叶片到涡轮叶片的第一流动路径和从压缩机叶片到涡轮机叶片的第二流动路径。 热交换器耦合到壳体并且位于压缩机和涡轮机之间，其中热交换器与第一流动路径和第二流动路径中的至少一个流动连通。 流体供应装置联接到壳体并与热交换器流动连通。
-
Patent Agency Ranking
公开(公告)号：US12031501B2
公开(公告)日：2024-07-09
申请号：US16698287
申请日：2019-11-27
Applicant: General Electric Company
CPC classification number: F02K1/822 , F02K7/10 , F28D7/163 , F05D2220/10 , F05D2240/14 , F05D2260/213 , F28D2021/0021 , F28D2021/0026
Abstract: A cooling system includes a conduit extending from an upstream end to a downstream end and retains a gas. A heat exchanger is fluidly coupled with and disposed within a surface of the conduit. A portion of the gas is directed into the heat exchanger via one or more passages extending between the conduit and the heat exchanger, and a portion of the gas is directed out of the heat exchanger via the one or more passages. The heat exchanger directs cooling fluid in one or more directions within the heat exchanger along one or more passageways of plural passageways. The heat exchanger directs the portion of the gas in one or more directions within the heat exchanger along one or more other passageways of the plural passageways. The heat exchanger cools the gas by exchanging heat from the gas to the cooling fluid within the heat exchanger.
-
公开(公告)号：US11918943B2
公开(公告)日：2024-03-05
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
IPC: B01D45/16 , B04C3/00 , B04C3/06 , F01D5/18 , F01D9/06 , F02C6/08 , F02C7/052 , F02C7/18 , F02K3/04
CPC classification number: B01D45/16 , B04C3/06 , F01D5/189 , F01D9/065 , F02C6/08 , F02C7/052 , F02C7/18 , B04C2003/003 , B04C2003/006 , F02K3/04 , F05D2260/607 , Y02T50/60
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.
-
公开(公告)号：US11815019B2
公开(公告)日：2023-11-14
申请号：US17230095
申请日：2021-04-14
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
CPC classification number: F02C7/052 , F02C3/06 , F02C9/18 , B01D45/08 , F05D2220/32 , F05D2260/607
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
-
公开(公告)号：US11541340B2
公开(公告)日：2023-01-03
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
IPC: B01D45/16 , F02C7/18 , B04C3/06 , B04C3/00 , F02C6/08 , F01D5/18 , F01D9/06 , F02C7/052 , F02K3/04
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.
-
公开(公告)号：US20210388763A1
公开(公告)日：2021-12-16
申请号：US17230095
申请日：2021-04-14
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
-
-
-
-
-
-
-
-
-
Search Results
48
records
(took 0.017 seconds)
