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公开(公告)号：US4706740A
公开(公告)日：1987-11-17
申请号：US24489
申请日：1987-03-11
Applicant: Edward T. Mahefkey
Inventor： Edward T. Mahefkey
CPC classification number: B64G1/506 , B64G1/503 , F28D15/0233 , F28D15/0275 , F28D15/04 , Y10S165/911
Abstract: A system for radiating heat generated by a source of heat aboard a spacecraft or the like is described which comprises a pair of spaced heat pipes and a pair of spaced wall members having inner condensation surfaces and outer heat radiating surfaces bonded to the heat pipes and defining a vapor chamber, a rewet artery of capillary wicking material disposed within the vapor chamber between the heat pipes and extending substantially lengthwise of the vapor chamber, a source of expendable liquid heat exchange medium operatively connected to the rewet artery for maintaining an inventory of heat exchange medium within the vapor chamber, and a pressure relief valve on the vapor chamber for venting vapor overpressure. The condensation surfaces of the wall members include a multiplicity of capillary grooves extending between the rewet artery and the heat pipes to promote vapor condensation, to facilitate flow of condensate toward the heat pipes, and otherwise to maintain a liquid film inventory near the heat radiating surfaces of the wall members.
Abstract translation: 描述了一种用于散发由航天器等上的热源产生的热量的系统，其包括一对间隔开的热管和一对隔开的壁构件，其具有内部冷凝表面和外部散热表面，其结合到热管并且限定 蒸气室，毛细管毛细管材料的再润湿动脉，其设置在热管之间的蒸气室内且基本上沿蒸气室的长度方向延伸;可操作地连接到再润湿动脉的消耗性液体热交换介质源，用于维持热交换库存 蒸汽室内的介质，以及蒸气室上的泄压阀，用于排出蒸气超压。 壁构件的冷凝表面包括在再润湿动脉和热管之间延伸的多个毛细管槽，以促进蒸气冷凝，以促进冷凝物朝向热管的流动，并且以其它方式在热辐射表面附近保持液膜清点 的墙壁成员。
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Patent Agency Ranking
公开(公告)号：US08434225B2
公开(公告)日：2013-05-07
申请号：US13543911
申请日：2012-07-09
Applicant: Edward T. Mahefkey , Louis Chow , Ming Su
Inventor： Edward T. Mahefkey , Louis Chow , Ming Su
CPC classification number: F28D15/046 , F28F2245/02 , Y10T29/49353 , Y10T29/49377
Abstract: A method for manufacturing a heat pipe. Activated particles or particle clusters are formed. The activated particles or particle clusters are contacted with a working fluid in a non-oxidizing environment to form a chemisorbed layer of the working fluid thereon to generate chemisorbed working fluid surfaced activated hydrophilic particles or activated hydrophilic particle clusters which provide a solid-liquid contact angle to working fluid when subsequently added of
Abstract translation: 一种制造热管的方法。 形成活性颗粒或颗粒簇。 活化的颗粒或颗粒簇在非氧化环境中与工作流体接触以在其上形成工作流体的化学吸附层，以产生化学吸附的工作流体表面活化的亲水颗粒或活化的亲水颗粒簇，其提供固 - 液接触角 随后添加<30度的工作流体。 化学吸附的工作流体表面活化的亲水颗粒或亲水颗粒团簇被真空转移并填充在热管内以及额外体积的工作流体。 然后将热管密封。
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公开(公告)号：US4727932A
公开(公告)日：1988-03-01
申请号：US875808
申请日：1986-06-18
Applicant: Edward T. Mahefkey
Inventor： Edward T. Mahefkey
CPC classification number: B64G1/503 , B64G1/50 , F28D15/0266
Abstract: An expandable heat rejection system for radiating heat generated by a source of heat on a spacecraft or like vehicle is described and comprises a fluid heat exchange medium in operative heat exchange contact with the source for absorbing heat by evaporation of the liquid phase of the medium, a thin flexible wall structure having an inlet and an outlet and defining a volume expandable and collapsible between preselected limits and defining an inner condensation surface and an outer heat radiating surface, a multiplicity of capillary grooves on the condensation surface for promoting condensation of vaporous medium and for facilitating flow of condensate along the condensation surface toward the outlet, and a pump for circulating the medium through the system.
Abstract translation: 描述了一种用于在航天器或类似车辆上散发由热源产生的热量的可扩散排热系统，并且包括与源的有效热交换接触的流体热交换介质，用于通过介质的液相的蒸发来吸收热量， 薄的柔性壁结构，其具有入口和出口，并且限定可膨胀和可折叠在预选极限之间并且限定内部冷凝表面和外部散热表面的体积，在冷凝表面上的多个毛细管槽，用于促进蒸气介质的冷凝和 用于促进冷凝物沿着冷凝表面朝向出口的流动，以及用于使介质循环通过系统的泵。
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公开(公告)号：US08235096B1
公开(公告)日：2012-08-07
申请号：US12755797
申请日：2010-04-07
Applicant: Edward T. Mahefkey , Louis Chow , Ming Su
Inventor： Edward T. Mahefkey , Louis Chow , Ming Su
CPC classification number: F28D15/046 , F28F2245/02 , H05K7/20336
Abstract: A heat pipe includes a sealed thermally conductive casing having a length that has a first end for coupling to a heat source to be cooled and a second end for coupling to a heat sink opposite the first end. The casing has an inside surface that defines a thermal control volume above. The thermal control volume includes (i) a plurality of hydrophilic particles or clusters of hydrophilic particles in a size range from nano size to micron size attached as a hydrophilic film to the inside surface or to a wick on the inside surface, wherein the plurality of hydrophilic particles occupy only a portion of an area of the inside surface or an internal pore space of the wick or a surface area of the wick, (ii) a vapor cavity above the hydrophilic film or the wick, and (iii) a heat transfer working fluid contained as a liquid on the hydrophilic film or the wick, and as a vapor in the vapor cavity. The plurality of hydrophilic particles or clusters of hydrophilic particles provide a solid-liquid contact angle for the working fluid when in a liquid state of
Abstract translation: 热管包括密封的导热壳体，该壳体的长度具有用于联接到待冷却的热源的第一端和用于联接到与第一端相对的散热器的第二端。 壳体具有限定上述热控制体积的内表面。 热控制体积包括（i）多个亲水性颗粒或尺寸范围从纳米尺寸至微米尺寸的亲水性颗粒或亲水性颗粒簇作为亲水膜附着到内表面或内表面上的芯，其中多个 亲水性颗粒仅占据芯的内部区域的一部分或芯的内部孔隙或芯的表面积，（ii）亲水膜或芯上方的蒸气腔，和（iii）热传递 工作流体作为液体包含在亲水膜或芯上，以及作为蒸汽腔中的蒸气。 当处于<30度，通常<10度的液体状态时，多个亲水颗粒或亲水颗粒团簇为工作流体提供固 - 液接触角。
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公开(公告)号：US4813476A
公开(公告)日：1989-03-21
申请号：US110809
申请日：1987-10-21
Applicant: Edward T. Mahefkey
Inventor： Edward T. Mahefkey
CPC classification number: B64G1/503 , B64G1/50 , F28D15/0266
Abstract: An expandable heat rejection system for radiating heat generated by a source of heat on a spacecraft or like vehicle is described and comprises a fluid heat exchange medium in operative heat exchange contact with the source for absorbing heat by evaporation of the liquid phase of the medium, a thin flexible wall structure having an inlet and an outlet and defining a volume expandable and collapsible between preselected limits and defining an inner condensation surface and an outer heat radiating surface, a multiplicity of capillary grooves on the condensation surface for promoting condensation of vaporous medium and for facilitating flow of condensate along the condensation surface toward the outlet, and a pump for circulating the medium through the system.
Abstract translation: 描述了一种用于在航天器或类似车辆上散发由热源产生的热量的可扩散排热系统，并且包括与源的有效热交换接触的流体热交换介质，用于通过介质的液相的蒸发来吸收热量， 薄的柔性壁结构，其具有入口和出口，并且限定可膨胀和可折叠在预选极限之间并且限定内部冷凝表面和外部散热表面的体积，在冷凝表面上的多个毛细管槽，用于促进蒸气介质的冷凝和 用于促进冷凝物沿着冷凝表面朝向出口的流动，以及用于使介质循环通过系统的泵。
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公开(公告)号：US4809771A
公开(公告)日：1989-03-07
申请号：US41956
申请日：1987-04-24
Applicant: Elliot B. Kennel , Edward T. Mahefkey , Jerry E. Beam
Inventor： Elliot B. Kennel , Edward T. Mahefkey , Jerry E. Beam
CPC classification number: C09K5/06 , F28D20/023 , Y02E60/145
Abstract: A thermal storage apparatus for use with space-based burst power supplies. Lithium hydride is encapsulated within spherical hollow capsules. Each capsule is made of a three layer hollow shell. The inner layer of each shell is molybdemum, the middle layer silicon carbide, and the outer layer molybedum. The lithium hydride occupies only about sixty percent of the interior volume of each capsule at ambient temperatures to allow for thermal expansion. The outer diameter of each capsule is 3 cm. The thickness of the layers is 0.1 mm for the inner and outer layer, and 0.3-0.5 mm for the middle layer. The capsules are arranged in a packed array for use in heat storage. A heat transfer working fluid, such as lithium, sodium or potassium, transfers heat to and from the packed array.
Abstract translation: 一种与基于空间的突发电源一起使用的储热装置。 氢化锂封装在球形中空胶囊内。 每个胶囊由三层中空壳制成。 每个壳的内层是钼，中层碳化硅和外层钼。 在环境温度下，氢化锂仅占每个胶囊内部体积的约百分之六十，以允许热膨胀。 每个胶囊的外径为3厘米。 内层和外层的层厚度为0.1mm，中间层的厚度为0.3-0.5mm。 胶囊被布置成用于储存的包装阵列。 诸如锂，钠或钾之类的传热工作流体将热量传送到打包阵列并从其排出。
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