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    Electronics package with radial heat sink and integrated blower
    4.
    发明授权
    Electronics package with radial heat sink and integrated blower 有权
    电子封装带径向散热片和集成风机

    公开(公告)号：US08331091B2

    公开(公告)日：2012-12-11

    申请号：US12873508

    申请日：2010-09-01

    申请人： Scott F. Kaslusky ,  Brian St. Rock

    发明人： Scott F. Kaslusky ,  Brian St. Rock

    IPC分类号： H05K7/20

    CPC分类号： H01L23/467 ,  F04D29/582 ,  F28F3/02 ,  F28F13/08 ,  H01L2924/0002 ,  H05K7/20918 ,  H01L2924/00

    摘要： According to one aspect of the invention, an electronics package includes an enclosure and one or more thermal energy generating components disposed in the enclosure. A radial heat sink is disposed in the enclosure including a blower disposed in the radial heat sink and a plurality of fins extending from a periphery of the blower toward a perimeter of the radial heat sink. The plurality of fins define a plurality of channels having a plurality of channel exits at the perimeter of the radial heat sink. The radial heat sink configured to dissipate thermal energy from the one or more components which are arranged around the heat sink according to heat flux requirements of each component. An air inlet extends through the enclosure and is connected to the blower to direct air to the blower in a direction substantially perpendicular to the first longitudinal face and/or the second longitudinal face.

    摘要翻译： 根据本发明的一个方面，一种电子封装包括外壳和设置在外壳中的一个或多个热能产生元件。 径向散热器设置在外壳中，包括设置在径向散热器中的鼓风机和从鼓风机的周边朝向径向散热器的周边延伸的多个散热片。 多个翅片限定了在径向散热器的周边具有多个通道出口的多个通道。 径向散热器被配置为根据每个部件的热通量要求从布置在散热片周围的一个或多个部件散发热能。 空气入口延伸穿过外壳并且连接到鼓风机以将空气沿基本上垂直于第一纵向面和/或第二纵向面的方向引导到鼓风机。

    Active structures for heat exchanger
    7.
    发明授权
    Active structures for heat exchanger 有权
    热交换器的主动结构

    公开(公告)号：US09140502B2

    公开(公告)日：2015-09-22

    申请号：US12832434

    申请日：2010-07-08

    申请人： Scott F. Kaslusky ,  Brian St. Rock ,  Jaeseon Lee ,  Yirong Jiang

    发明人： Scott F. Kaslusky ,  Brian St. Rock ,  Jaeseon Lee ,  Yirong Jiang

    IPC分类号： F28F13/12 ,  F28F13/06 ,  H05K7/20

    CPC分类号： F28F13/06 ,  F28F13/12 ,  F28F13/125

    摘要： A heat exchanger includes a plurality of channels and one or more active flow disruption members disposed at an entrance to the plurality of channels. The active flow disruption members are configured to induce unsteadiness in a flow through the plurality of channels to increase thermal energy transfer in the plurality of channels. A method for transferring thermal energy from a heat exchanger includes locating one or more active flow disruption members at an entrance to a plurality of channels of the heat exchanger. A flow is directed across the one or more active flow disruption members into the plurality of channels and an unsteadiness is produced in the flow via the one or more active flow disruption members. The unsteadiness in the flow increases the transfer of thermal energy between the heat exchanger and the flow.

    摘要翻译： 热交换器包括多个通道和设置在多个通道的入口处的一个或多个主动流量中断构件。 主动流动破坏构件构造成在通过多个通道的流中引起不稳定，以增加多个通道中的热能传递。 用于从热交换器传递热能的方法包括将一个或多个主动流动破坏构件定位在热交换器的多个通道的入口处。 一个流被引导到一个或多个主动流中断构件进入多个通道中，并且在流中经由一个或多个主动流中断构件产生不稳定性。 流动中的不稳定性增加了热交换器和流量之间的热能传递。

    NON-CIRCULAR RADIAL HEAT SINK
    8.
    发明申请
    NON-CIRCULAR RADIAL HEAT SINK 有权
    非圆形辐射散热片

    公开(公告)号：US20120014064A1

    公开(公告)日：2012-01-19

    申请号：US12838536

    申请日：2010-07-19

    申请人： Brian St. Rock ,  Scott F. Kaslusky

    发明人： Brian St. Rock ,  Scott F. Kaslusky

    IPC分类号： H05K7/20 ,  F28F13/00

    CPC分类号： H01L23/467 ,  H01L2924/0002 ,  H01L2924/00

    摘要： A heat sink includes a blower located in the heat sink and a plurality of fins extending from a periphery of the blower toward a perimeter of the heat sink. The plurality of fins define a plurality of channels each having a channel inlet located at the blower and a channel exit located at the perimeter of the heat sink. The plurality of channels vary in length around the perimeter of the heat sink A velocity of an air flow from the blower at each channel inlet is substantially equal for each channel of the plurality of channels, and a total pressure drop from the channel inlet to the channel exit is substantially equal for each channel of the plurality of channels.

    摘要翻译： 散热器包括位于散热器中的鼓风机和从鼓风机的周边朝向散热器的周边延伸的多个散热片。 多个翅片限定多个通道，每个通道具有位于鼓风机处的通道入口和位于散热器周边的通道出口。 多个通道的长度围绕散热器的周边变化在每个通道入口处的来自鼓风机的空气流的速度对于多个通道中的每个通道基本上相等，并且从通道入口到 通道出口对于多个通道中的每个通道基本相等。

    THERMOELECTRIC DEVICE ARCHITECTURE
    9.
    发明申请
    THERMOELECTRIC DEVICE ARCHITECTURE 有权
    热电装置架构

    公开(公告)号：US20110146740A1

    公开(公告)日：2011-06-23

    申请号：US12642123

    申请日：2009-12-18

    申请人： Brian St. Rock ,  Scott F. Kaslusky

    发明人： Brian St. Rock ,  Scott F. Kaslusky

    IPC分类号： H01L35/34 ,  H01L35/28

    CPC分类号： H01L35/32

    摘要： A thermoelectric device (100, 220) includes a plurality of conductor portions (120-124) including a first angled side portion (134) and a second angled side portion (135). The thermoelectric device (100, 220) also includes a plurality of conductor members (170-174) including a first angled side section (181) and a second angled side section (182). A plurality of P-type thermoelectric members (210-213) interconnect corresponding ones of the first angled side portions (134) with the first angled side sections (181). A plurality of N-type thermoelectric members (200-204) interconnect corresponding ones of the second angled side portions (135) with the second angled side sections (182). Electric flow through the plurality of conductor portions (120-124) and the plurality of conductor members (170-174) passes along a first predefined curvilinear path and a heat flux passes along a second predefined curvilinear path.

    摘要翻译： 热电装置（100,220）包括多个导体部分（120-124），包括第一成角度侧部分（134）和第二倾斜侧部分（135）。 热电装置（100,220）还包括包括第一倾斜侧部分（181）和第二倾斜侧部分（182）的多个导体部件（170-174）。 多个P型热电元件（210-213）将相应的第一成角度侧部（134）与第一倾斜侧部（181）相互连接。 多个N型热电元件（200-204）将相应的第二成角度的侧部（135）与第二倾斜的侧部（182）相互连接。 通过多个导体部分（120-124）和多个导体构件（170-174）的电流沿着第一预定曲线路径通过，并且热通量沿着第二预定曲线路径通过。

    TRANSCRITICAL FLUID COOLING FOR AEROSPACE APPLICATIONS
    10.
    发明申请
    TRANSCRITICAL FLUID COOLING FOR AEROSPACE APPLICATIONS 有权
    用于航空应用的传输流体冷却

    公开(公告)号：US20110005244A1

    公开(公告)日：2011-01-13

    申请号：US12498744

    申请日：2009-07-07

    申请人： Adam M. Finney ,  Young K. Park ,  Scott F. Kaslusky ,  Daniel R. Sabatino

    发明人： Adam M. Finney ,  Young K. Park ,  Scott F. Kaslusky ,  Daniel R. Sabatino

    IPC分类号： F25B9/00 ,  C09K5/04 ,  B60H1/32 ,  F25B1/10 ,  F25B43/00 ,  F25B39/02

    CPC分类号： B64D13/08 ,  B64D2013/0614 ,  B64D2013/0674 ,  F25B1/10 ,  F25B9/008 ,  F25B9/06 ,  F25B2309/061 ,  F25B2400/13 ,  F25B2400/23 ,  Y02T50/44 ,  Y02T50/56

    摘要： A cooling system includes a compressor for compressing a refrigerant from a subcritical state to a supercritical state, a cooler for transferring heat from the refrigerant, an expander for expanding the refrigerant in the supercritical state, an expansion valve for expanding the refrigerant from the supercritical state to the subcritical state and an evaporator for transferring heat from a cooling fluid to the refrigerant in the subcritical state. Work extracted by the expander provides power to the compressor. A method for cooling a vehicle includes compressing a refrigerant from a subcritical state to a supercritical state, cooling the refrigerant, expanding the refrigerant in the supercritical state where work produced by expanding the refrigerant is used to compress the refrigerant, expanding the refrigerant from the supercritical state to the subcritical state, cooling a cooling fluid with the refrigerant in the subcritical state and cooling vehicle components with the cooling fluid.

    摘要翻译： 冷却系统包括用于将制冷剂从亚临界状态压缩至超临界状态的压缩机，用于从制冷剂传递热量的冷却器，用于使处于超临界状态的制冷剂膨胀的膨胀机，用于使制冷剂从超临界状态膨胀的膨胀阀 到亚临界状态的蒸发器和用于将热量从冷却流体传递到亚临界状态的制冷剂的蒸发器。 膨胀机提取的作业为压缩机提供动力。 一种用于冷却车辆的方法包括将制冷剂从亚临界状态压缩至超临界状态，冷却制冷剂，使超临界状态下的制冷剂膨胀，使用膨胀制冷剂制造的工件用于压缩制冷剂，从超临界 状态到亚临界状态，用亚临界状态的制冷剂冷却冷却流体，并用冷却流体冷却车辆部件。