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公开(公告)号：US20180094583A1
公开(公告)日：2018-04-05
申请号：US15282348
申请日：2016-09-30
Applicant: General Electric Company
CPC classification number: F02C7/14 , F05D2260/213 , F05D2260/22141 , F05D2260/98 , F28D1/0366 , F28D1/0471 , F28D7/005 , F28F1/022 , F28F3/022 , Y02T50/672 , Y02T50/676
Abstract: A surface cooler includes a conduit, a body having an external surface, and a plurality of fin members arranged in an array of fin members. The conduit defines an inlet, an outlet, and an internal flow path extending between the inlet and the outlet. The conduit is configured to channel a flow of fluid to be cooled from the inlet to said outlet. The conduit extends through the body. Each fin member of the array of fin members extends from the external surface of the body. Each fin member is fabricated from a thermally conductive resilient and pliable material.
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公开(公告)号：US09909816B2
公开(公告)日：2018-03-06
申请号：US15271280
申请日：2016-09-21
Applicant: General Electric Company
IPC: H01M10/052 , F28D15/02 , H01M10/659 , F28D15/04 , F28D20/02 , H01L23/34 , H01L23/427 , F28D20/00
CPC classification number: F28D15/0275 , F28D15/02 , F28D15/04 , F28D20/02 , F28D2020/0008 , H01L23/34 , H01L23/4275 , H01M10/052 , H01M10/659 , Y02E60/145
Abstract: A system is disclosed. The system includes a thermally conductive enclosure bounding an interior cavity, a metallic cell wall structure disposed within the cavity, in thermal communication with the enclosure, and defining a plurality of cells, and a phase change material disposed within the cells and in thermal communication with the cell walls. The plurality of cells have a cell width less than about 5 millimeters, and the cell wall thickness of the cell wall structure is in a range from about 0.25 millimeter to about 1 millimeter.
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公开(公告)号：US09903274B2
公开(公告)日：2018-02-27
申请号：US14535614
申请日：2014-11-07
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage , Michael Thomas Kenworthy
IPC: F02C1/00 , F02C7/14 , B64D33/12 , F02C7/18 , F28F27/02 , F28D1/047 , F28D7/08 , F02K3/02 , F28F13/00 , F02K3/06 , F28F1/12 , F28D21/00
CPC classification number: F02C7/14 , B64D33/12 , F02C7/18 , F02K3/025 , F02K3/06 , F05D2250/90 , F05D2300/505 , F28D1/047 , F28D7/08 , F28D2021/0021 , F28D2021/0026 , F28F1/12 , F28F13/00 , F28F27/02 , F28F2255/04 , F28F2280/10 , Y02T50/675
Abstract: A heat exchanger apparatus including a surface cooler and a passive automatic retraction and extension system coupled to the surface cooler. The surface cooler having disposed therein one or more fluid flow channels configured for the passage therethrough of a heat transfer fluid to be cooled. The heat transfer fluid in a heat transfer relation on an interior side of said one or more fluid flow channels. The surface cooler including a plurality of fins projecting from an outer surface thereof. The passive automatic retraction and extension system including a thermal actuation component responsive to a change in temperature of at least one of the heat transfer fluid and a cooling fluid flow so as to actuate a change in a geometry of the surface cooler. Further disclosed is an engine including the heat exchanger apparatus.
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公开(公告)号：US09601951B2
公开(公告)日：2017-03-21
申请号：US14070795
申请日：2013-11-04
Applicant: General Electric Company
Inventor： Ken Ivcar Salas Nobrega , Jeremy Daniel Van Dam , Manoj Ramprasad Shah , William Dwight Gerstler , Tsarafidy Raminosoa , Edward John Flett , Patel Bhageerath Reddy , James Pellegrino Alexander
Abstract: A permanent magnet machine, a rotor assembly for the machine, and a pump assembly. The permanent magnet machine includes a stator assembly including a stator core configured to generate a magnetic field and extending along a longitudinal axis with an inner surface defining a cavity and a rotor assembly including a rotor core and a rotor shaft. The rotor core is disposed inside the cavity and configured to rotate about the longitudinal axis. The rotor assembly further including a plurality of permanent magnets for generating a magnetic field which interacts with the stator magnetic field to produce torque. The permanent magnets configured as one of internal or surface mounted. The rotor assembly also including a plurality of retaining clips configured to retain the plurality of permanent magnets relative to the rotor core. The pump assembly including an electric submersible pump and a permanent magnet motor for driving the pump.
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公开(公告)号：US09572280B2
公开(公告)日：2017-02-14
申请号：US14449452
申请日：2014-08-01
Applicant: General Electric Company
Inventor： Mehmet Arik , William Dwight Gerstler , Ri Li , Earl Ross Nicewarner , Christina Clyde Schroeder , Benjamin Jon Vander Ploeg , Bryan Patrick Whalen
CPC classification number: H05K7/20009 , F24F13/02 , H01L2924/0002 , H05K7/20172 , H05K7/20209 , H01L2924/00
Abstract: A chassis with distributed jet cooling is provided. The chassis includes one or more sidewalls defining a volume configured to substantially surround one or more heat generating components positioned within the volume. The chassis further includes at least one array of fins thermally coupled to a respective one of the one or more sidewalls and at least one synthetic jet assembly comprising a multi-orifice synthetic jet or a number of single orifice synthetic jets disposed on a side of a respective one of the array(s) of fins. The chassis further includes at least one attachment means for attaching a respective one of the at least one synthetic jet assemblies to a respective one of the one or more sidewalls.
Abstract translation: 提供分布式喷射冷却的底盘。 底盘包括限定体积的一个或多个侧壁，所述体积被配置为基本上围绕定位在体积内的一个或多个发热组件。 底盘还包括至少一个热耦合到一个或多个侧壁中的一个或多个侧壁的翅片阵列，以及至少一个合成射流组件，其包括多孔合成射流或多个单孔合成射流， 相应的翅片阵列之一。 底盘还包括至少一个连接装置，用于将至少一个合成射流组件中的相应一个连接到一个或多个侧壁中的相应一个。
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Patent Agency Ranking
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。
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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。
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78.发明申请公开(公告)号：US20150041104A1
公开(公告)日：2015-02-12
申请号：US13963473
申请日：2013-08-09
Applicant: GE Aviation Systems, LLC , General Electric Company
Inventor： Hendrik Pieter Jacobus De Bock , William Dwight Gerstler , Jonathan Mark Dunsdon , Stefano Angelo Mario Lassini , William Earl Gross, JR. , Delbert Warren Flaherty , Randall Lee Neuman , Christina Clyde Schroeder
CPC classification number: B05B17/0653 , F04D33/00 , H05K7/20172
Abstract: A modular synthetic cooling jet apparatus for cooling at least one electronic component and including a first synthetic cooling jet is provided. The first synthetic cooling jet includes a first piezoelectric element, and a first pair of plates coupled to the first piezoelectric element. The first pair of plates includes a first top plate and a first bottom plate. The first synthetic cooling jet also includes a first air gap defined between the first top plate and the first bottom plate. The first flex circuit is coupled to the first piezoelectric element. The first flex circuit is configured to be coupled to an electrical power source and to transmit a first electrical signal to the first piezoelectric element. The first piezoelectric element is configured to actuate at least one of the first top plate and the first bottom plate to induce a first expelling air stream.
Abstract translation: 提供一种用于冷却至少一个电子部件并包括第一合成冷却射流的模块化合成冷却喷射装置。 第一合成冷却射流包括第一压电元件和耦合到第一压电元件的第一对板。 第一对板包括第一顶板和第一底板。 第一合成冷却射流还包括限定在第一顶板和第一底板之间的第一气隙。 第一柔性电路耦合到第一压电元件。 第一柔性电路被配置为耦合到电源并且将第一电信号传输到第一压电元件。 第一压电元件构造成致动第一顶板和第一底板中的至少一个以引导第一排出气流。
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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。
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公开(公告)号：US20140338861A1
公开(公告)日：2014-11-20
申请号：US14449452
申请日：2014-08-01
Applicant: General Electric Company
Inventor： Mehmet Arik , William Dwight Gerstler , Ri Li , Earl Ross Nicewarner , Christina Clyde Schroeder , Benjamin Jon Vander Ploeg , Bryan Patrick Whalen
IPC: H05K7/20
CPC classification number: H05K7/20009 , F24F13/02 , H01L2924/0002 , H05K7/20172 , H05K7/20209 , H01L2924/00
Abstract: A chassis with distributed jet cooling is provided. The chassis includes one or more sidewalls defining a volume configured to substantially surround one or more heat generating components positioned within the volume. The chassis further includes at least one array of fins thermally coupled to a respective one of the one or more sidewalls and at least one synthetic jet assembly comprising a multi-orifice synthetic jet or a number of single orifice synthetic jets disposed on a side of a respective one of the array(s) of fins. The chassis further includes at least one attachment means for attaching a respective one of the at least one synthetic jet assemblies to a respective one of the one or more sidewalls.
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