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公开(公告)号：US20090288814A1
公开(公告)日：2009-11-26
申请号：US12124092
申请日：2008-05-20
IPC分类号： F28F7/00
CPC分类号： F28F13/003 , F28D9/0062 , F28F21/02 , F28F21/08 , F28F2265/26
摘要： A heat exchanger includes a thermally-conductive fluid barrier having first and second surfaces, at least one first type of foam element placed in thermally-conductive contact with the first surface of the thermally-conductive fluid barrier and having a first coefficient of thermal expansion and at least one second type of foam element placed in thermally-conductive contact with the second surface of the thermally-conductive fluid barrier and having a second coefficient of thermal expansion. The first coefficient of thermal expansion of the first type of foam element and the second coefficient of thermal expansion of the second type of foam element are substantially different.
摘要翻译： 热交换器包括具有第一和第二表面的导热流体屏障，至少一个第一类型的泡沫元件放置成与导热流体屏障的第一表面导热接触并具有第一热膨胀系数， 至少一个第二类型的泡沫元件放置成与导热流体屏障的第二表面导热接触并具有第二热膨胀系数。 第一类泡沫元件的第一热膨胀系数和第二类型泡沫元件的第二热膨胀系数基本上不同。
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公开(公告)号：US20120118345A1
公开(公告)日：2012-05-17
申请号：US12927466
申请日：2010-11-15
申请人： Michael F. Stoia , David W. Kwok , James P. Huang
发明人： Michael F. Stoia , David W. Kwok , James P. Huang
IPC分类号： H01L35/30
CPC分类号： F02C6/18 , F01D5/284 , F02K1/82 , H01L35/30 , Y02T50/673
摘要： Disclosed is an improved thermoelectric component, a method for thermal integration of the improved thermoelectric component in an environment having thermally distinct zones, and a thermoelectric generation system. In general, the thermoelectric component includes a thermoelectric device having opposing surfaces for arrangement in comparatively hot and cold environments, and an extended surface mounted in close proximity to at least one of the opposing surfaces, the extended surface being a layer of porous material having at least a portion immersed in at least one of the hot or cold environments.
摘要翻译： 公开了一种改进的热电组件，在具有热不同区域的环境中热改变的热电组件的热集成方法和热电发电系统。 通常，热电元件包括具有相对表面的热电装置，用于布置在比较热和冷的环境中，以及延伸的表面，其紧邻至少一个相对表面安装，所述延伸表面是多孔材料层， 至少一部分浸没在至少一个热或冷环境中。
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公开(公告)号：US20100192941A1
公开(公告)日：2010-08-05
申请号：US12416207
申请日：2009-04-01
IPC分类号： F24J2/38
CPC分类号： H01L31/0547 , F24S23/77 , F24S30/45 , F24S2023/84 , F24S2023/85 , F24S2023/87 , F24S2023/872 , Y02E10/47 , Y02E10/52
摘要： A solar concentration system including at least one receiver and an array of micro-mirrors connected to a substrate, each micro-mirror of the array being articulateable relative to the substrate, wherein the receiver is positioned relative to the array such that the array directs incoming light to the receiver.
摘要翻译： 一种太阳能集中系统，包括至少一个接收器和连接到衬底的微镜阵列，阵列的每个微镜相对于衬底可铰接，其中接收器相对于阵列定位，使得阵列引导入射 光接收器。
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公开(公告)号：US20090242420A1
公开(公告)日：2009-10-01
申请号：US12058650
申请日：2008-03-28
CPC分类号： C25B1/04 , B64D13/00 , B64D2013/0677 , B64D2041/005 , B64D2211/00 , B64G1/42 , B64G1/44 , B64G1/446 , H01M16/003 , Y02E60/366 , Y02E70/10 , Y02P20/134 , Y02T50/55 , Y02T50/56 , Y02T90/36
摘要： An aerospace platform includes a structure having a cavity and a light-transmissive portion that exposes the cavity to sunlight. The aerospace platform further includes a fluid heating system. The fluid heating system includes a fluid-carrying, thermally absorptive structure within the cavity, and a solar collector for collecting light transmitted through the light-transmissive portion and focusing the collected light onto the absorptive structure. The thermally absorptive structure has a high surface absorptivity that retains thermal energy when exposed to solar irradiance and heats fluid contained therein.
摘要翻译： 航空航天平台包括具有空腔和将空腔暴露于阳光的透光部分的结构。 航空航天平台还包括流体加热系统。 流体加热系统包括空腔内的流体携带的热吸收结构，以及太阳能收集器，用于收集透过透光部分的光并将收集的光聚焦到吸收结构上。 热吸收结构具有高的表面吸收性，当暴露于太阳辐照并且加热其中所含的流体时，其保持热能。
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公开(公告)号：US08957303B2
公开(公告)日：2015-02-17
申请号：US13286202
申请日：2011-10-31
IPC分类号： F24J2/46 , H01L31/042
CPC分类号： H01L31/0422 , B64C2201/021 , B64C2201/042 , B64D2211/00 , H01L31/042 , H02S10/40 , H02S20/00 , Y02B10/20 , Y02E10/50
摘要： In an embodiment of the disclosure, there is provided a strain isolation layer assembly. The assembly has a rigid solar layer; a strain isolation layer having a discontinuous configuration, a vertical rigidity, and a horizontal shear flexibility; and an underlying substrate layer. The strain isolation layer is coupled between the rigid solar layer and the underlying substrate layer to form a strain isolation layer assembly, such that the strain isolation layer isolates the rigid solar layer to reduce one or more strains induced on the rigid solar layer.
摘要翻译： 在本公开的一个实施例中，提供了应变隔离层组件。 该组件具有刚性的太阳能层; 具有不连续构型，垂直刚性和水平剪切挠度的应变隔离层; 和底层基底层。 应变隔离层耦合在刚性太阳能层和下面的基底层之间以形成应变隔离层组件，使得应变隔离层隔离刚性太阳能层以减少在刚性太阳能层上诱发的一种或多种应变。
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公开(公告)号：US08127758B2
公开(公告)日：2012-03-06
申请号：US12058650
申请日：2008-03-28
CPC分类号： C25B1/04 , B64D13/00 , B64D2013/0677 , B64D2041/005 , B64D2211/00 , B64G1/42 , B64G1/44 , B64G1/446 , H01M16/003 , Y02E60/366 , Y02E70/10 , Y02P20/134 , Y02T50/55 , Y02T50/56 , Y02T90/36
摘要： An aerospace platform includes a structure having a cavity and a light-transmissive portion that exposes the cavity to sunlight. The aerospace platform further includes a fluid heating system. The fluid heating system includes a fluid-carrying, thermally absorptive structure within the cavity, and a solar collector for collecting light transmitted through the light-transmissive portion and focusing the collected light onto the absorptive structure. The thermally absorptive structure has a high surface absorptivity that retains thermal energy when exposed to solar irradiance and heats fluid contained therein.
摘要翻译： 航空航天平台包括具有空腔和将空腔暴露于阳光的透光部分的结构。 航空航天平台还包括流体加热系统。 流体加热系统包括空腔内的流体携带的热吸收结构，以及太阳能收集器，用于收集透过透光部分的光并将收集的光聚焦到吸收结构上。 热吸收结构具有高的表面吸收性，当暴露于太阳辐照并且加热其中所含的流体时，其保持热能。
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