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1. 发明授权

US07687132B1 Ceramic microtruss 有权
标题翻译：陶瓷微桁架
公开(公告)号：US07687132B1
公开(公告)日：2010-03-30
申请号：US12074727
申请日：2008-03-05
申请人： Adam F. Gross , Alan J. Jacobsen , Robert Cumberland
发明人： Adam F. Gross , Alan J. Jacobsen , Robert Cumberland
IPC分类号： B32B3/12
CPC分类号： C04B38/0032 , B22F1/0007 , B22F3/002 , B22F2998/00 , B22F2999/00 , Y10T428/24149 , Y10T428/29 , C04B35/565 , C04B35/58 , B22F1/02 , B22F1/004
摘要： An ordered ceramic microstructure and a method of making the same. In one embodiment, the ceramic microstructure includes a base structure and one or more ceramic layers. The base structure includes a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction, a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction, and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. Here, the first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material, and the base structure is self-supporting. In addition, the ceramic layers coat a surface of at least one truss element of the first truss elements, the second truss elements, or the third truss elements.
摘要翻译：有序的陶瓷微结构及其制造方法。在一个实施例中，陶瓷微结构包括基底结构和一个或多个陶瓷层。基底结构包括由多个第一自传播聚合物波导限定并沿着第一方向延伸的多个第一桁架元件，由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件方向，以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。这里，第一，第二和第三桁架元件在多个节点处相互渗透以形成连续材料，并且基部结构是自支撑的。此外，陶瓷层涂覆第一桁架元件，第二桁架元件或第三桁架元件的至少一个桁架元件的表面。

2. 发明授权

US07938989B1 Composite structures for storing thermal energy 有权
标题翻译：用于储存热能的复合结构
公开(公告)号：US07938989B1
公开(公告)日：2011-05-10
申请号：US12589262
申请日：2009-10-20
申请人： Adam F. Gross , Ronald M. Finnila , Alan J. Jacobsen , Robert Cumberland , Sky L. Skeith
发明人： Adam F. Gross , Ronald M. Finnila , Alan J. Jacobsen , Robert Cumberland , Sky L. Skeith
IPC分类号： G02B1/12
CPC分类号： F28D20/023 , Y02E60/145
摘要： A composite structure for storing thermal energy. In one embodiment, an apparatus for storing thermal energy includes: a thermal storage material and a three-dimensional structure. The three-dimensional structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The thermal storage material occupies at least a portion of the open space, and the three-dimensional structure is self-supporting.
摘要翻译：一种用于储存热能的复合结构。在一个实施例中，用于存储热能的装置包括：热存储材料和三维结构。三维结构包括：由多个第一自传播聚合物波导限定并沿着第一方向延伸的多个第一桁架元件; 由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件; 以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。第一，第二和第三桁架元件在多个节点处相互渗透以形成连续材料。第一，第二和第三桁架元件定义了一个开放空间。储热材料占据开放空间的至少一部分，并且三维结构是自支撑的。

3. 发明授权

US07653276B1 Composite structures for storing thermal energy 失效
标题翻译：用于储存热能的复合结构
公开(公告)号：US07653276B1
公开(公告)日：2010-01-26
申请号：US12075033
申请日：2008-03-06
申请人： Adam F. Gross , Ronald M. Finnila , Alan J. Jacobsen , Robert Cumberland , Sky L. Skeith
发明人： Adam F. Gross , Ronald M. Finnila , Alan J. Jacobsen , Robert Cumberland , Sky L. Skeith
IPC分类号： G02B6/26 , G02B6/255
CPC分类号： F28D20/023 , Y02E60/145
摘要： A composite structure for storing thermal energy. In one embodiment, an apparatus for storing thermal energy includes: a thermal storage material and a three-dimensional structure. The three-dimensional structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The thermal storage material occupies at least a portion of the open space, and the three-dimensional structure is self-supporting.
摘要翻译：一种用于储存热能的复合结构。在一个实施例中，用于存储热能的装置包括：热存储材料和三维结构。三维结构包括：由多个第一自传播聚合物波导限定并沿第一方向延伸的多个第一桁架元件; 由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件; 以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。第一，第二和第三桁架元件在多个节点处相互渗透以形成连续材料。第一，第二和第三桁架元件定义了一个开放空间。储热材料占据开放空间的至少一部分，并且三维结构是自支撑的。

4. 发明授权

US09933213B1 Composite structures with ordered three-dimensional (3D) continuous interpenetrating phases 有权
公开(公告)号：US09933213B1
公开(公告)日：2018-04-03
申请号：US13490376
申请日：2012-06-06
申请人： Alan J. Jacobsen , William B. Barvosa-Carter , Adam F. Gross , Robert Cumberland , Kevin W. Kirby , David Kisailus
发明人： Alan J. Jacobsen , William B. Barvosa-Carter , Adam F. Gross , Robert Cumberland , Kevin W. Kirby , David Kisailus
IPC分类号： B05D3/02 , F28D20/02 , C04B38/00 , B22F1/00
CPC分类号： F28D20/023 , B22F1/0007 , B29D11/00663 , C04B38/0032 , G02B6/12002 , G02B6/138
摘要： A method of forming a three-dimensional (3D) composite structure includes: securing a mask between a collimated light source and a volume of a photo-monomer; directing a collimated light beam from the collimated light source to the mask for a period of exposure time such that a portion of the collimated light beam passes through the mask and is guided by a plurality of apertures into the photo-monomer to form a plurality of waveguides through a portion of the volume of the photo-monomer; removing any uncured photo-monomer to leave behind a three-dimensional ordered open-cellular microstructure to define an open volume and a structure of a first continuous material of the three-dimensional composite material; and placing a second continuous material in the open volume, wherein the second continuous material and the first continuous material share an interface between each other, and wherein the interface is everywhere continuous.

5. 发明授权

US08435438B1 Ceramic microtruss 有权
标题翻译：陶瓷微桁架
公开(公告)号：US08435438B1
公开(公告)日：2013-05-07
申请号：US12705534
申请日：2010-02-12
申请人： Adam F. Gross , Alan J. Jacobsen , Robert Cumberland
发明人： Adam F. Gross , Alan J. Jacobsen , Robert Cumberland
IPC分类号： B29C35/08
CPC分类号： C04B38/0032 , B22F1/0007 , B22F3/002 , B22F2998/00 , B22F2999/00 , Y10T428/24149 , Y10T428/29 , C04B35/565 , C04B35/58 , B22F1/02 , B22F1/004
摘要： An ordered ceramic microstructure and a method of making the same. In one embodiment, the ceramic microstructure includes a base structure and one or more ceramic layers. The base structure includes a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction, a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction, and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. Here, the first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material, and the base structure is self-supporting. In addition, the ceramic layers coat a surface of at least one truss element of the first truss elements, the second truss elements, or the third truss elements.
摘要翻译：有序的陶瓷微结构及其制造方法。在一个实施例中，陶瓷微结构包括基底结构和一个或多个陶瓷层。基底结构包括由多个第一自传播聚合物波导限定并沿着第一方向延伸的多个第一桁架元件，由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件方向，以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。这里，第一，第二和第三桁架元件在多个节点处相互渗透以形成连续材料，并且基部结构是自支撑的。此外，陶瓷层涂覆第一桁架元件，第二桁架元件或第三桁架元件的至少一个桁架元件的表面。

6. 发明授权

US08320727B1 Composite structures with ordered three-dimensional (3D) continuous interpenetrating phases 有权
标题翻译：具有有序三维（3D）连续互穿相的复合结构
公开(公告)号：US08320727B1
公开(公告)日：2012-11-27
申请号：US12008479
申请日：2008-01-11
申请人： Alan J. Jacobsen , William B. Barvosa-Carter , Adam F. Gross , Robert Cumberland , Kevin W. Kirby , David Kisailus
发明人： Alan J. Jacobsen , William B. Barvosa-Carter , Adam F. Gross , Robert Cumberland , Kevin W. Kirby , David Kisailus
IPC分类号： G02B6/10 , E04B1/18 , B29D11/00
CPC分类号： F28D20/023 , B22F1/0007 , B29D11/00663 , C04B38/0032 , G02B6/12002 , G02B6/138
摘要： A three-dimensional (3D) composite structure and a method of making the same. In one embodiment, the 3D composite structure includes a 3D ordered microstructure and a second continuous material. The 3D ordered microstructure includes first truss elements defined by first self-propagating polymer waveguides and extending along a first direction, second truss elements defined by second self-propagating polymer waveguides and extending along a second direction, and third truss elements defined by third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at nodes to form a first continuous material with the three-dimensional ordered microstructure. In addition, the second continuous material has different physical properties than the first continuous material and shares an interface with the three-dimensional ordered microstructure, and wherein the interface is everywhere continuous.
摘要翻译：三维（3D）复合结构及其制作方法。在一个实施例中，3D复合结构包括3D有序微结构和第二连续材料。 3D有序微结构包括由第一自传播聚合物波导限定并沿着第一方向延伸的第一桁架元件，由第二自传播聚合物波导限定并沿第二方向延伸的第二桁架元件，传播聚合物波导并沿着第三方向延伸。第一，第二和第三桁架元件在节点处相互渗透以形成具有三维有序微结构的第一连续材料。此外，第二连续材料具有与第一连续材料不同的物理性能，并且与三维有序微结构共享界面，并且其中界面无处不在。

7. 发明授权

US08679582B2 Tunable variable emissivity materials and methods for controlling the temperature of spacecraft using tunable variable emissivity materials 有权
标题翻译：可调谐的可变辐射率材料和使用可调谐的可变辐射材料来控制航天器的温度的方法
公开(公告)号：US08679582B2
公开(公告)日：2014-03-25
申请号：US12705782
申请日：2010-02-15
申请人： Robert Cumberland , William B. Barvose-Carter , Adam F. Gross
发明人： Robert Cumberland , William B. Barvose-Carter , Adam F. Gross
IPC分类号： B05D3/02
CPC分类号： B64G1/54 , C01G45/1264 , C01P2002/34 , C01P2002/77 , C01P2006/32 , C01P2006/42
摘要： Tunable variable emissivity materials, methods for fabricating tunable variable emissivity materials, and methods for controlling the temperature of a spacecraft using tunable variable emissivity materials have been provided. In an exemplary embodiment, a variable emissivity material has the formula M1(1−(x+y))M2xM3yMnO3, wherein M1 comprises lanthanum, praseodymium, scandium, yttrium, neodymium or samarium, M2 comprises an alkali earth metal, M3 comprises an alkali earth metal that is not M2, and x, y, and (x+y) are less than 1. The material has a critical temperature (Tc) in the range of about 270 to about 320K and a transition width is less than about 30K.
摘要翻译：已经提供了可调谐的可变发射材料，用于制造可调谐的发射率材料的方法以及使用可调谐的发射率材料来控制航天器的温度的方法。在示例性实施例中，可变发射率材料具有式M1（1-（x + y））M2xM3yMnO3，其中M1包括镧，镨，钪，钇，钕或钐，M2包括碱土金属，M3包含碱不属于M2的地球金属，x，y和（x + y）小于1.该材料的临界温度（Tc）在约270至约320K的范围内，并且转变宽度小于约30K 。

8. 发明申请

US20110039035A1 TUNABLE VARIABLE EMISSIVITY MATERIALS AND METHODS FOR CONTROLLING THE TEMPERATURE OF SPACECRAFT USING TUNABLE VARIABLE EMISSIVITY MATERIALS 有权
标题翻译：使用可变电磁材料控制空间温度的可变电磁辐射材料和方法
公开(公告)号：US20110039035A1
公开(公告)日：2011-02-17
申请号：US12705782
申请日：2010-02-15
申请人： Robert Cumberland , William B. Barvose-Carter , Adam F. Gross
发明人： Robert Cumberland , William B. Barvose-Carter , Adam F. Gross
IPC分类号： C23C14/08
CPC分类号： B64G1/54 , C01G45/1264 , C01P2002/34 , C01P2002/77 , C01P2006/32 , C01P2006/42
摘要： Tunable variable emissivity materials, methods for fabricating tunable variable emissivity materials, and methods for controlling the temperature of a spacecraft using tunable variable emissivity materials have been provided. In an exemplary embodiment, a variable emissivity material has the formula M1(1−(x+y))M2xM3yMnO3, wherein M1 comprises lanthanum, praseodymium, scandium, yttrium, neodymium or samarium, M2 comprises an alkali earth metal, M3 comprises an alkali earth metal that is not M2, and x, y, and (x+y) are less than 1. The material has a critical temperature (Tc) in the range of about 270 to about 320K and a transition width is less than about 30K.
摘要翻译：已经提供了可调谐的可变发射材料，用于制造可调谐的发射率材料的方法以及使用可调谐的发射率材料来控制航天器的温度的方法。在示例性实施例中，可变发射率材料具有式M1（1-（x + y））M2xM3yMnO3，其中M1包括镧，镨，钪，钇，钕或钐，M2包括碱土金属，M3包含碱不属于M2的地球金属，x，y和（x + y）小于1.该材料的临界温度（Tc）在约270至约320K的范围内，并且转变宽度小于约30K 。

9. 发明授权

US07691284B2 Tunable variable emissivity materials and methods for controlling the temperature of spacecraft using tunable variable emissivity materials 有权
标题翻译：可调谐的可变辐射率材料和使用可调谐的可变辐射材料来控制航天器的温度的方法
公开(公告)号：US07691284B2
公开(公告)日：2010-04-06
申请号：US11468033
申请日：2006-08-29
申请人： Robert Cumberland , William B. Barvose Carter , Adam F. Gross
发明人： Robert Cumberland , William B. Barvose Carter , Adam F. Gross
IPC分类号： C01G45/12
CPC分类号： B64G1/54 , C01G45/1264 , C01P2002/34 , C01P2002/77 , C01P2006/32 , C01P2006/42
摘要： Tunable variable emissivity materials, methods for fabricating tunable variable emissivity materials, and methods for controlling the temperature of a spacecraft using tunable variable emissivity materials have been provided. In an exemplary embodiment, a variable emissivity material has the formula M1(1−(x+y))M2xM3yMnO3, wherein M1 comprises lanthanum, praseodymium, scandium, yttrium, neodymium or samarium, M2 comprises an alkali earth metal, M3 comprises an alkali earth metal that is not M2, and x, y, and (x+y) are less than 1. The material has a critical temperature (Tc) in the range of about 270 to about 320K and a transition width is less than about 30K.
摘要翻译：已经提供了可调谐的可变发射材料，用于制造可调谐的发射率材料的方法以及使用可调谐的发射率材料来控制航天器的温度的方法。在示例性实施例中，可变发射率材料具有式M1（1-（x + y））M2xM3yMnO3，其中M1包括镧，镨，钪，钇，钕或钐，M2包括碱土金属，M3包含碱不属于M2的地球金属，x，y和（x + y）小于1.该材料的临界温度（Tc）在约270至约320K的范围内，并且转变宽度小于约30K 。

10. 发明授权

US07718227B2 Flexible thermal control coatings and methods for fabricating the same 有权
标题翻译：柔性热控制涂层及其制造方法
公开(公告)号：US07718227B2
公开(公告)日：2010-05-18
申请号：US11465097
申请日：2006-08-16
申请人： Robert Cumberland , William B. Barvosa-Carter , Adam F. Gross
发明人： Robert Cumberland , William B. Barvosa-Carter , Adam F. Gross
IPC分类号： B05D3/02
CPC分类号： C09D5/32
摘要： Flexible thermal control coatings for use on components of spacecraft and methods for fabricating such coatings are provided. In an exemplary embodiment, a flexible thermal control coating comprises a flexible organic binder for disposition on the component and an inorganic material having a radiation absorptance (α) of less than about 0.2 and an emissivity (ε) of at least about 0.6. The inorganic material and the organic binder are oriented relative to each other so that an exterior surface of the coating has a higher concentration of inorganic material than an interior surface of the coating and a lower concentration of organic binder than the interior surface.
摘要翻译：提供了用于航天器部件的柔性热控涂层和制造这种涂层的方法。在示例性实施例中，柔性热控制涂层包括用于配置在组件上的柔性有机粘合剂和具有小于约0.2的辐射吸收率（α）和至少约0.6的发射率（“egr”）的无机材料。无机材料和有机粘合剂相对于彼此定向，使得涂层的外表面具有比内表面更高的无机材料浓度和比内表面更低的有机粘合剂浓度。

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