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    THERMAL MANAGEMENT SYSTEM AND METHOD
    54.
    发明申请
    THERMAL MANAGEMENT SYSTEM AND METHOD 审中-公开
    热管理系统和方法

    公开(公告)号：US20170040242A1

    公开(公告)日：2017-02-09

    申请号：US15298677

    申请日：2016-10-20

    Applicant: General Electric Company

    Inventor： Mehmet Arik ,  William Dwight Gerstler ,  Ri Li ,  Pradeep Chandra Babu Salapakkam ,  Bryan Patrick Whalen

    IPC: H01L23/467 ,  B23P15/26 ,  H01L21/48 ,  H05K7/20

    CPC classification number: H01L23/467 ,  B23P15/26 ,  B23P2700/10 ,  H01L21/4882 ,  H01L23/4735 ,  H01L2924/0002 ,  H05K7/20172 ,  Y10T29/4935 ,  H01L2924/00

    Abstract: A thermal management system is provided. The thermal management system includes at least one heat sink including one or more respective fins, wherein the one or more fins include one or more respective cavities. The thermal management system also includes a synthetic jet stack including at least one synthetic jet mounted within each of the respective cavities employing at least one engaging structure to provide a rigid positioning of the synthetic jet stack within the fins, wherein the synthetic jet includes at least one orifice through which a fluid is ejected.

    Abstract translation: 提供热管理系统。 热管理系统包括至少一个散热器，其包括一个或多个相应的散热片，其中所述一个或多个散热片包括一个或多个相应的空腔。 热管理系统还包括合成射流堆叠，其包括安装在每个相应空腔内的至少一个合成喷射器，其采用至少一个接合结构，以提供合成射流堆叠在翅片内的刚性定位，其中合成射流至少包括 一个孔，喷射流体。

    THERMAL MANAGEMENT SYSTEM
    55.
    发明申请
    THERMAL MANAGEMENT SYSTEM 有权
    热管理系统

    公开(公告)号：US20160169591A1

    公开(公告)日：2016-06-16

    申请号：US14570204

    申请日：2014-12-15

    Applicant: General Electric Company

    Inventor： Naveenan Thiagarajan ,  Hendrik Pieter Jacobus de Bock ,  William Dwight Gerstler

    IPC: F28D15/02

    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.

    Abstract translation: 公开了一种系统。 该系统包括界定内腔的导热外壳，设置在空腔内的金属电池壁结构，与外壳热连通，并且限定多个电池，以及设置在电池内并与电池内部热连通的相变材料 细胞壁。 多个电池具有小于约5毫米的电池宽度，电池壁结构的电池壁厚度在约0.25毫米至约1毫米的范围内。

    Systems and methods for control of an adaptive-cycle engine with power-thermal management system
    56.
    发明授权
    Systems and methods for control of an adaptive-cycle engine with power-thermal management system 有权
    使用电力热管理系统控制自适应循环发动机的系统和方法

    公开(公告)号：US09354621B2

    公开(公告)日：2016-05-31

    申请号：US14305063

    申请日：2014-06-16

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Eric Richard Westervelt ,  Benjamin Paul Breig ,  Mustafa Tekin Dokucu ,  Neil Richard Garrigan ,  William Dwight Gerstler ,  Javier Armando Parrilla

    IPC: G05B13/02 ,  G05B15/02 ,  G05D23/19

    CPC classification number: G05B13/026 ,  G05B15/02 ,  G05D23/1917

    Abstract: A control system for an adaptive-power thermal management system of an aircraft having at least one adaptive cycle gas turbine engine includes a real time optimization solver that utilizes a plurality of models of systems to be controlled, the plurality of models each being defined by algorithms configured to predict changes to each system caused by current changes in input to each system. The real time optimization solver is configured to solve an open-loop optimal control problem on-line at each of a plurality of sampling times, to provide a series of optimal control actions as a solution to the open-loop optimal control problem. The real time optimization solver implements a first control action in a sequence of control actions and at a next sampling time the open-loop optimal control problem is re-posed and re-solved.

    Abstract translation: 用于具有至少一个自适应循环燃气涡轮发动机的飞机的自适应功率热管理系统的控制系统包括利用要控制的多个系统模型的实时优化求解器，所述多个模型各自由算法 配置为预测由每个系统的输入的当前变化引起的每个系统的变化。 实时优化求解器被配置为在多个采样时间中的每一个在线解决开环最优控制问题，以提供作为开环最优控制问题的解决方案的一系列最佳控制动作。 实时优化求解器在控制动作序列中实现第一控制动作，并且在下一个采样时间，重新提出并解决了开环最优控制问题。

    METHOD AND APPARATUS FOR DECONGEALING A LUBRICATING FLUID IN A HEAT EXCHANGER APPARATUS
    57.
    发明申请
    METHOD AND APPARATUS FOR DECONGEALING A LUBRICATING FLUID IN A HEAT EXCHANGER APPARATUS 有权
    用于在热交换器装置中分解润滑油的方法和装置

    公开(公告)号：US20160090863A1

    公开(公告)日：2016-03-31

    申请号：US14502750

    申请日：2014-09-30

    Applicant: General Electric Company

    Inventor： Carlos Enrique Diaz ,  William Dwight Gerstler ,  Michael Ralph Storage

    IPC: F01D25/18 ,  F01D17/02

    CPC classification number: F01D25/18 ,  F02C7/00 ,  F28D20/003

    Abstract: A decongealing channel for use in a heat exchanger apparatus, including a supersaturated solution contained therein and an actuation component in fluid communication with a lubricating fluid coupled to the decongealing channel. The actuation component is responsive to a change in pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution. The heat exchanger apparatus is disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a manifold portion, one or more flow through openings extending therethrough the manifold portion to define one or more flow through channels having contained therein the lubricating fluid. In addition, the manifold portion including one or more additional openings extending therethrough to define one or more decongealing channels. Further disclosed is an engine including the heat exchanger apparatus and a method of decongealing a lubricating fluid in the heat exchanger apparatus.

    Abstract translation: 一种在热交换器装置中使用的去饱和通道，包括其中所含的过饱和溶液和与连接到去饱和通道的润滑流体流体连通的致动部件。 致动部件响应于润滑流体施加在其上的压力变化，以便致动过饱和溶液中的放热响应。 热交换器装置设置在飞机发动机的旁路风扇管道中。 所述热交换器装置包括歧管部分，一个或多个流过所述歧管部分的流过开口以限定一个或多个通过其中包含润滑流体的通道。 此外，歧管部分包括一个或多个延伸穿过其中的附加开口，以限定一个或多个去饱和通道。 还公开了一种发动机，其包括热交换器装置和在热交换器装置中使润滑流体退热的方法。

    MODULAR PERMANENT MAGNET MOTOR AND PUMP ASSEMBLY
    58.
    发明申请
    MODULAR PERMANENT MAGNET MOTOR AND PUMP ASSEMBLY 有权
    模块式永磁电机和泵组件

    公开(公告)号：US20150123506A1

    公开(公告)日：2015-05-07

    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

    IPC: H02K1/27 ,  H02K16/02 ,  H02K5/132

    CPC classification number: H02K1/274 ,  H02K1/276 ,  H02K1/278 ,  H02K5/132 ,  H02K16/02 ,  Y02E20/16

    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.

    Abstract translation: 永磁机，用于机器的转子组件和泵组件。 永磁体机器包括定子组件，该定子组件包括定子铁心，该定子铁心构造成产生磁场并且沿纵向轴线延伸，内表面限定空腔，转子组件包括转子芯和转子轴。 转子芯设置在空腔内并且构造成围绕纵向轴线旋转。 转子组件还包括多个永磁体，用于产生与定子磁场相互作用以产生转矩的磁场。 永久磁铁被配置为内部或表面安装的一个。 转子组件还包括多个保持夹，其构造成相对于转子芯保持多个永磁体。 泵组件包括用于驱动泵的电潜泵和永磁电动机。

    FLOW CONTROL ASSEMBLY AND METHODS OF ASSEMBLING THE SAME
    59.
    发明申请
    FLOW CONTROL ASSEMBLY AND METHODS OF ASSEMBLING THE SAME 有权
    流量控制组件及其组装方法

    公开(公告)号：US20150033729A1

    公开(公告)日：2015-02-05

    申请号：US13955096

    申请日：2013-07-31

    Applicant: General Electric Company

    Inventor： Corey Bourassa ,  William Dwight Gerstler ,  Bruce Philip Biederman

    IPC: F02C7/18

    CPC classification number: F02C7/18 ,  F02C9/16 ,  Y02T50/671 ,  Y02T50/675 ,  Y10T29/49323

    Abstract: A flow control assembly for controlling cooling flow of a turbine engine is provided. The flow control assembly includes a first flow control device having a first sidewall and a second sidewall. The first sidewall is coupled to a compressor vane and is configured to define a first flow path from a compressor to a turbine vane. The second sidewall is coupled to a compressor vane and is configured to define a second flow path from the compressor to a turbine blade. A second flow control device is coupled to the compressor and includes an orifice device coupled to the compressor vane and a meter device coupled to the orifice, wherein the orifice is configured to direct a cooling flow to the meter device. A controller is configured to control the meter device to facilitate regulating the cooling flow into at least one of the first flow path and the second flow path.

    Abstract translation: 提供了一种用于控制涡轮发动机的冷却流量的流量控制组件。 流量控制组件包括具有第一侧壁和第二侧壁的第一流量控制装置。 第一侧壁联接到压缩机叶片并且构造成限定从压缩机到涡轮叶片的第一流动路径。 第二侧壁联接到压缩机叶片并且构造成限定从压缩机到涡轮叶片的第二流动路径。 第二流量控制装置联接到压缩机并且包括联接到压缩机叶片的孔装置和联接到孔口的仪表装置，其中孔口被配置成将冷却流引导到仪表装置。 控制器被配置为控制仪表装置以便于调节进入第一流动路径和第二流动路径中的至少一个的冷却流。

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