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1. 发明授权

US09914552B2 Integrated control device and integrated control program 有权
公开(公告)号：US09914552B2
公开(公告)日：2018-03-13
申请号：US14915037
申请日：2014-08-28
申请人： Mitsubishi Electric Corporation
发明人： Takehisa Kimura
IPC分类号： B64G3/00 , B64G99/00 , G05B19/042 , G05B23/02
CPC分类号： B64G3/00 , B64G9/00 , G05B19/042 , G05B23/0251
摘要： An integrated control device that assigns a same attribute to plural pieces of status information integrally monitored over at least two or more pieces of equipment, to derive integrated status information and integrate the plural pieces of status information. An integration processor derives the integrated status information such that a group of pieces of preset status information is referenced with respect to plural pieces of status information with a same attribute from among status information of monitoring target functions stored in monitoring data of equipment and provided for each of plural pieces of the equipment to be monitored or an operation applying an operator being set for each attribute to pieces of status information with the same attribute from among status information of monitoring target functions stored in monitoring data of equipment and provided for each of plural pieces of the equipment to be monitored is carried out.

2. 发明申请

US20160288931A1 SATELLITE FRAME AND METHOD OF MAKING A SATELLITE 审中-公开
标题翻译：卫星框架和制作卫星的方法
公开(公告)号：US20160288931A1
公开(公告)日：2016-10-06
申请号：US14675542
申请日：2015-03-31
申请人： WorldVu Satellites Limited
发明人： Daniel W. Field , Armen Askijian , James Grossman , Alexander D. Smith
IPC分类号： B64G99/00 , B29C70/06 , B29C70/30 , B64G1/10 , B64G1/28
CPC分类号： B64G9/00 , B29C70/06 , B29C70/20 , B29C70/30 , B29K2063/00 , B29K2105/06 , B29K2307/04 , B29K2831/00 , B29K2863/00 , B29K2905/00 , B29K2905/02 , B29L2031/3097 , B64G1/10 , B64G1/283 , B64G1/40 , B64G1/402 , B64G1/503 , B64G1/66
摘要： A satellite frame includes a one-piece integrated body defining a plurality of sides for attaching satellite components thereto. Use of the single integrated satellite body minimizes the amount of fasteners and alignment equipment and processes. Use of the single piece frame also allows for the maximum possible specific stiffness by greatly reducing the number of connections and structural interfaces.
摘要翻译：卫星框架包括限定用于将卫星部件附接到其上的多个侧面的一体式整体。使用单个集成卫星体可以最大限度地减少紧固件和对准设备和工艺的数量。使用单片机架也可以通过大大减少连接数量和结构界面来实现最大可能的刚度。

3. 发明申请

US20160251093A1 TRUSS STRUCTURE 审中-公开
标题翻译： TRUSS结构
公开(公告)号：US20160251093A1
公开(公告)日：2016-09-01
申请号：US15053998
申请日：2016-02-25
申请人： Space Systems/Loral, LLC
发明人： Carey Graham Hijmans , Michael Paul Freestone
IPC分类号： B64G99/00 , B29C65/48
CPC分类号： B64G9/00 , B64G1/10 , F16B7/00 , F16B7/185 , F16B11/008 , G06F17/5018
摘要： A spacecraft includes a 3-D closed truss structure including at least four coupling nodes and at least six strut elements, attached together by a plurality of joints, each coupling node including at least two legs, each strut element disposed between and attached with a respective pair of the plurality of coupling nodes. Each coupling node is attached, at respective ones of the plurality of joints, with at least two strut elements. Each strut element is attached at a first end with a first leg of a first coupling node and is attached at a second end with a second leg of a second coupling node, the first leg being substantially longer than the second leg.
摘要翻译：航天器包括一个3-D闭合桁架结构，其包括至少四个耦合节点和至少六个支柱元件，其由多个接头连接在一起，每个耦合节点包括至少两个支腿，每个支柱元件设置在相应的一对多个耦合节点。每个耦合节点在多个关节中的相应的一个处连接有至少两个支柱元件。每个支柱元件在第一端处附接有第一联接节点的第一腿部，并且在第二端处与第二联接节点的第二腿连接，第一腿部基本上长于第二腿部。

4. 发明授权

US09409658B1 Space-based structures and methods of delivering space-sourced materials 有权
标题翻译：空间结构和交付空间材料的方法
公开(公告)号：US09409658B1
公开(公告)日：2016-08-09
申请号：US14218430
申请日：2014-03-18
申请人： Planetary Resources Development Corp.
发明人： Peter H. Diamandis , Eric Anderson , Chris Lewicki , Chris Voorhees
IPC分类号： B64G99/00 , B64G1/24 , E21C51/00 , B64G1/62 , B64G1/00 , C22B9/00
CPC分类号： B64G9/00 , B64G1/00 , B64G1/242 , B64G1/62 , C22B5/20 , C22B11/00 , C22B23/00 , E21C51/00
摘要： A method is provided for processing extraterrestrial metal into a metal foam or gossamer structure in space, and delivering the metal foam or gossamer structure intact to the Earth's surface. Additionally, a structure is provided that is formed in space and consists essentially of an extraterrestrial metal.
摘要翻译：提供了一种用于将外星金属加工成空间中的金属泡沫或游丝结构并将金属泡沫或游丝结构完整地输送到地球表面的方法。另外，提供了一种在空间中形成并且基本上由地外金属组成的结构。

5. 发明申请

US20150230414A1 METHOD FOR MODIFYING ENVIRONMENTAL CONDITIONS WITH RING COMPRISED OF MAGNETIC MATERIAL 审中-公开
标题翻译：用环形材料修饰环境条件的方法
公开(公告)号：US20150230414A1
公开(公告)日：2015-08-20
申请号：US14184624
申请日：2014-02-19
申请人： Dennis Jason Stelmack , Eugene Gerald Stelmack
发明人： Dennis Jason Stelmack , Eugene Gerald Stelmack
IPC分类号： A01G15/00 , B64G1/10
CPC分类号： A01G15/00 , B64G1/1085 , B64G9/00
摘要： A method for modifying environmental conditions is disclosed herein. The method includes the step of deploying a magnetic climate control material to a local area in one of the thermosphere and the exosphere. The magnetic climate control material deflects and absorbs rays of the sun. The magnetic climate control material affects temperature of a local area below the magnetic climate control material and also global temperatures. The method also includes the ability for moving, manipulating, or removal of this ring.
摘要翻译：本文公开了一种改变环境条件的方法。该方法包括将磁性气候控制材料部署到热层和大气层之一的局部区域的步骤。磁性气候控制材料偏转和吸收太阳光线。磁性气候控制材料影响低于磁性气候控制材料的局部区域的温度以及全球温度。该方法还包括移动，操纵或移除该环的能力。

6. 发明授权

US09044566B2 Advanced supported liquid membranes for carbon dioxide control in extravehicular activity applications 有权
标题翻译：先进的支撑液膜在二次空间活动应用中进行二氧化碳控制
公开(公告)号：US09044566B2
公开(公告)日：2015-06-02
申请号：US14195615
申请日：2014-03-03
申请人： Reaction Systems, LLC
发明人： David T. Wickham , Kevin J. Gleason , Scott W. Cowley
IPC分类号： B01D53/22 , A61M16/22 , A62B19/02 , B01D53/00 , B64D13/00 , C01B31/20 , B64G99/00 , A62B19/00
CPC分类号： A61M16/22 , A62B19/00 , A62B19/02 , B01D53/00 , B01D53/1425 , B01D53/1475 , B01D53/228 , B01D61/38 , B01D69/10 , B01D71/06 , B01D2252/204 , B01D2257/504 , B01D2257/80 , B01D2258/06 , B01D2259/4541 , B01D2259/4575 , B64D13/00 , B64G6/00 , B64G9/00 , Y02C10/06 , Y02C10/10
摘要： There is disclosed a portable life support system with a component for removal of at least one selected gas. In an embodiment, the system includes a supported liquid membrane having a first side and a second side in opposition to one another, the first side configured for disposition toward an astronaut and the second side configured for disposition toward a vacuum atmosphere. The system further includes an ionic liquid disposed between the first side and the second side of the supported liquid membrane, the ionic liquid configured for removal of at least one selected gas from a region housing the astronaut adjacent the first side of the supported liquid membrane to the vacuum atmosphere adjacent the second side of the supported liquid membrane. Other embodiments are also disclosed.
摘要翻译：公开了一种便携式生命支持系统，其具有用于去除至少一个选定气体的部件。在一个实施例中，系统包括支撑液膜，其具有彼此相对的第一侧和第二侧，第一侧被配置为朝向宇航员配置，第二侧被配置为朝向真空气氛配置。所述系统还包括设置在所述支撑液膜的所述第一侧和所述第二侧之间的离子液体，所述离子液体构造成用于从邻近所述支撑液膜的所述第一侧的所述宇航员的区域中移除至少一个所选择的气体到邻近负载液膜第二面的真空气氛。还公开了其他实施例。

7. 发明授权

US08991765B1 Satellite predictive avoidance system 有权
标题翻译：卫星预测回避系统
公开(公告)号：US08991765B1
公开(公告)日：2015-03-31
申请号：US13438176
申请日：2012-04-03
申请人： Douglas Edward Chesser , Mario Pio Alleva , Manuel Beltran , Paul H. Smith
发明人： Douglas Edward Chesser , Mario Pio Alleva , Manuel Beltran , Paul H. Smith
IPC分类号： B64G3/00 , B64G1/24
CPC分类号： B64G1/242 , B64G3/00 , B64G9/00 , F41H3/00
摘要： A method and apparatus for generating avoidance data. Strips are generated for a path of a space object. The strips are positioned relative to the path of the space object. The strips have parameters that obscure an identification of the path of the space object to form the avoidance data.
摘要翻译：一种用于产生回避数据的方法和装置。为空间对象的路径生成条带。条带相对于空间物体的路径定位。条带具有遮蔽空间物体的路径的识别以形成回避数据的参数。

8. 发明授权

US08286392B2 Inhabitable space frames 有权
标题翻译：居住空间框架
公开(公告)号：US08286392B2
公开(公告)日：2012-10-16
申请号：US13057132
申请日：2009-06-19
申请人： David Noble , James Chuda
发明人： David Noble , James Chuda
IPC分类号： E04H1/04
CPC分类号： E04B1/19 , B64G9/00 , E04B1/3211 , E04B2001/0053 , E04B2001/3235
摘要： An inhabitable space frame (100) can define and support inhabitable living space within, around and projecting from the exterior of the perimeter of the space frame (100). The space frame (100) includes a vector matrix of strut members (105) that defines a plurality of interconnected basic tetrahedral modules (110) and, optionally, a plurality of prime octahedral modules (115). At least a part of each prime octahedral module (115) in the plurality of prime octahedral modules (115) is adjacent to at least two of the basic tetrahedral modules (110). Use of one or more right triangular faces, or planes, within a repeating geometry of a vector matrix enables an interior of the space frame (100) to be inhabitable, with horizontal floors and vertical walls aligned with associated strut members (105).
摘要翻译：可居住的空间框架（100）可以限定和支撑在空间框架（100）的周边的外部，周围并从其突出的居住的居住空间。空间框架（100）包括限定多个互连的基本四面体模块（110）和可选地多个主八面体模块（115）的支柱构件（105）的向量矩阵。多个主八面体模块（115）中的每个主要八面体模块（115）的至少一部分与至少两个基本四面体模块（110）相邻。在向量矩阵的重复几何形状内使用一个或多个右三角形面或平面使得空间框架（100）的内部可居住，其中水平地板和垂直壁与相关联的支柱构件（105）对准。

9. 发明授权

US08266866B1 Method and apparatus for an inflatable shell 有权
公开(公告)号：US08266866B1
公开(公告)日：2012-09-18
申请号：US13346137
申请日：2012-01-09
申请人： Christopher J. Johnson
发明人： Christopher J. Johnson
IPC分类号： E04B1/00
CPC分类号： B64G9/00 , B64G1/12 , B64G2001/224
摘要： A method of assembling an inflatable shell of a structure comprises folding a plurality of shell sections about a set of fold lines and integrating the plurality of shell sections together with one another to form the shell. In another embodiment, an inflatable shell comprises a plurality of shell sections, each shell section having two pairs of fold lines for folding into stowage comprising a first gore section having a plurality of first gore panels layered and collectively folded about at a first set of fold lines. Each layer of the first gore panels and second gore panels are configured such that, once the first gore panel and second gore panel are attached to one another at the respective side edges of each panel, the lines of attachment forming a second set of fold lines for the shell section. A system and method for fabricating gore panels is also disclosed.

10. 发明申请

US20110180669A1 Inflatable nested toroid structure 有权
公开(公告)号：US20110180669A1
公开(公告)日：2011-07-28
申请号：US11956826
申请日：2007-12-14
申请人： Christopher J. Johnson , Jasen L. Raboin , Gary R. Spexarth
发明人： Christopher J. Johnson , Jasen L. Raboin , Gary R. Spexarth
IPC分类号： B64G1/00 , B64G1/52 , E04H15/20
CPC分类号： B64G1/12 , B64G1/54 , B64G1/56 , B64G9/00 , B64G2001/224
摘要： An inflatable structure comprises at least two generally toroidal, inflatable modules. When in a deployed mode, the first, inner module has a major diameter less than that of a second, outer module and is positioned within the inner circumference of the outer module such that the first module is nested circumferentially alongside the second module. The inflatable structure, in a non-deployed, non-inflated mode, is of compact configuration and adapted to be transported to a site of deployment. When deployed, the inflatable structure is of substantially increased interior volume. In one embodiment, access between the interior of the first module and the second module is provided by at least one port or structural pass-through. In another embodiment, the inflatable structure includes at least one additional generally toroidal module external of and circumferentially surrounding the second module.

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