HEAT EXCHANGER
    64.
    发明申请

    公开(公告)号:US20170131034A1

    公开(公告)日:2017-05-11

    申请号:US14937259

    申请日:2015-11-10

    Abstract: A heat exchanger is disclosed including an array of interlaced conduits. The conduit array includes a first plurality of conduits connected to a first inlet header at one end of the first plurality of conduits and to a first outlet header at an opposite end of the first plurality of conduits. This first plurality of conduits provides a first fluid flow path from the first inlet header through the first plurality of conduits to the first outlet header. The conduit array also includes a second plurality of conduits crossing and interlaced with the first plurality of conduits. First and second fluid flow paths are provided through the first and second pluralities of conduits, and a third fluid flow path is through open spaces between the crossed interlaced first and second pluralities of conduits.

    COMPACT HEAT EXCHANGER
    65.
    发明申请
    COMPACT HEAT EXCHANGER 审中-公开
    紧凑型热交换器

    公开(公告)号:US20160282061A1

    公开(公告)日:2016-09-29

    申请号:US14669202

    申请日:2015-03-26

    Abstract: A compact heat exchanger is provided and includes a first manifold defining an inlet for receiving from a component a fluid to be cooled and an outlet for returning the cooled fluid to the component to cool the component. A second manifold is disposed spaced from the first manifold. A core extends between and fluidly communicates with the manifolds and includes hexagonal channels. Each channel is formed by mini-tubes defining respective triangular passages. A cross-section of the core defines an irregular-cross structure. The fluid enters the inlet of the first manifold, makes a first pass through the mini-tubes to the second manifold, makes a second pass through the mini-tubes to the first manifold such that the fluid is cooled across the mini-tubes, exits the first manifold through the outlet, and returns to the component to cool the component. A method of manufacturing the heat exchanger is provided also.

    Abstract translation: 提供了紧凑的热交换器,并且包括限定用于从部件接收待冷却的流体的入口的第一歧管和用于将冷却的流体返回到部件以冷却部件的出口。 第二歧管与第一歧管间隔设置。 芯部与歧管之间延伸并与流体连通并且包括六边形通道。 每个通道由限定相应的三角形通道的微型管形成。 芯的横截面限定了不规则交叉结构。 流体进入第一歧管的入口,首先通过微型管到第二歧管,使第二通过微型管到第一歧管,使得流体在微型管,出口 通过出口的第一个歧管,并返回到组件以冷却组件。 还提供制造热交换器的方法。

    SHELL AND TUBE HEAT EXCHANGER
    66.
    发明申请
    SHELL AND TUBE HEAT EXCHANGER 审中-公开
    壳和热交换器

    公开(公告)号:US20160146542A1

    公开(公告)日:2016-05-26

    申请号:US14552748

    申请日:2014-11-25

    CPC classification number: F28D7/106 F28D7/16 F28D15/02 F28D2021/0021 F28F9/22

    Abstract: A heat exchanger is provided that includes a shell defining a first fluid space and one or more tubes within the first fluid space having interiors fluidly isolated therefrom. The tubes define a second fluid space and are configured to permit thermal energy transfer between the first fluid space and the second fluid space. One or more heat pipes are disposed within one of the first fluid space and the second fluid space and are configured to transfer thermal energy within the respective fluid space.

    Abstract translation: 提供了一种热交换器,其包括限定第一流体空间的外壳和在第一流体空间内的一个或多个管,其具有与其流体隔离的内部。 管限定第二流体空间并且构造成允许第一流体空间和第二流体空间之间的热能传递。 一个或多个热管布置在第一流体空间和第二流体空间之一内,并且被配置成在相应的流体空间内传递热能。

    BALANCED HEAT EXCHANGER SYSTEMS AND METHODS
    67.
    发明申请
    BALANCED HEAT EXCHANGER SYSTEMS AND METHODS 有权
    平衡热交换器系统和方法

    公开(公告)号:US20160131432A1

    公开(公告)日:2016-05-12

    申请号:US14537311

    申请日:2014-11-10

    Abstract: A heat exchanger is provided having a first fluid circuit defining a first volume and configured to permit a first fluid to flow therethrough with a first fluid supply. The heat exchanger includes a second fluid circuit defining a second volume separate from the first volume and sharing at least one common wall with the first enclosed volume, and configured to permit a second fluid to flow therethrough from a second fluid supply. One or more thermal transfer sheets having one or more channels therein are configured in structural and thermal contact with both the first and second fluid circuits, the channels having a thermodynamic fluid disposed therein and configured to transfer heat between the first fluid circuit and the second fluid circuit. A thermal transfer rate through the at least one common wall is less than a thermal transfer rate of the one or more thermal transfer sheets.

    Abstract translation: 提供了一种热交换器,其具有限定第一容积的第一流体回路并且构造成允许第一流体通过第一流体供应流过其中。 热交换器包括第二流体回路,其限定与第一容积分离的第二容积并与第一封闭容积共享至少一个公共壁,并且构造成允许第二流体从第二流体供应流过。 其中具有一个或多个通道的一个或多个热转印片被构造成与第一和第二流体回路结构和热接触,通道具有设置在其中的热力学流体并且构造成在第一流体回路和第二流体之间传递热量 电路。 通过至少一个公共壁的热传递速率小于一个或多个热转印片材的热转印速率。

    HIGH-TEMPERATURE ENVIRONMENT ELECTRONIC CHASSIS
    68.
    发明申请
    HIGH-TEMPERATURE ENVIRONMENT ELECTRONIC CHASSIS 有权
    高温环境电子基座

    公开(公告)号:US20150124407A1

    公开(公告)日:2015-05-07

    申请号:US14192096

    申请日:2014-02-27

    CPC classification number: H05K5/0213 H05K7/20 H05K7/20263

    Abstract: An electrical chassis for use in high temperature environments is disclosed. The electrical chassis may be employed, for example, in close proximity to the combustion chamber of a jet engine. The electrical chassis is constructed with a substrate formed from a material with low thermal conductivity and low electrical conductivity, such as polyetheretherketone. A reflective surface may be disposed on a housing containing the substrate to reduce the absorption of radiation. A heat sink and fluid inlet and outlet may also be arranged to remove heat generated by the electrical components.

    Abstract translation: 公开了一种用于高温环境的电气底盘。 电底盘可以例如紧靠喷气发动机的燃烧室使用。 电气底盘由具有低导热性和低导电性的材料(例如聚醚醚酮)形成的基底构成。 反射表面可以设置在包含衬底的壳体上以减少辐射的吸收。 散热器和流体入口和出口也可以被布置成去除由电气部件产生的热量。

    FLUID COOLING ARRANGEMENT FOR A GAS TURBINE ENGINE AND METHOD
    69.
    发明申请
    FLUID COOLING ARRANGEMENT FOR A GAS TURBINE ENGINE AND METHOD 有权
    用于气体涡轮发动机的流体冷却装置和方法

    公开(公告)号:US20150023776A1

    公开(公告)日:2015-01-22

    申请号:US13945070

    申请日:2013-07-18

    Abstract: A fluid cooling arrangement in a gas turbine engine for aerospace propulsion includes an inner structure. Also included is an outer structure disposed radially outwardly of the inner structure, the outer structure and the inner structure defining a bypass flow path. Further included is at least one strut operatively coupling the inner structure to the outer structure. Yet further included is at least one cooling tube formed within the at least one strut, the at least one cooling tube configured to cool a fluid passing through the at least one cooling tube upon convective cooling of the at least one strut as air passes through the bypass flow path and over the at least one strut.

    Abstract translation: 用于航空航天推进的燃气涡轮发动机中的流体冷却装置包括内部结构。 还包括设置在内部结构的径向外侧的外部结构,外部结构和内部结构限定旁路流动路径。 还包括至少一个支柱,其可操作地将内部结构联接到外部结构。 还包括至少一个形成在所述至少一个支柱内的冷却管,所述至少一个冷却管构造成当空气通过所述至少一个支柱时对所述至少一个支柱进行对流冷却时,冷却通过所述至少一个冷却管的流体 旁路流路和至少一个支柱上。

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