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1.发明授权
公开(公告)号：US5578139A
公开(公告)日：1996-11-26
申请号：US368774
申请日：1995-01-03
IPC分类号： B64G1/44 , F24S23/30 , H01L31/045 , H01L31/052
CPC分类号： B64G1/44 , F24J2/085 , H01L31/0543 , H01L31/0547 , H02S30/20 , Y02E10/43 , Y02E10/52 , Y10S136/292
摘要： A stowable and deployable concentrator for solar cells. A substrate mounts a row of solar cells. A row of Fresnel lens elements is mounted to the substrate so as to be deflectable toward the substrate in a stowed configuration and biased away from it in the deployed configuration. The Fresnel lens is linear and flexibly mounted in a shaper which shapes it to a proper curvature in the deployed configuration. A pair of these concentrators can be hinged together to form a conveniently stowed and readily deployed combination.
摘要翻译： 用于太阳能电池的可收起和可部署的集中器。 基板安装一排太阳能电池。 一排菲涅耳透镜元件安装到基板上，以便以收起的构造朝向基板偏转，并在展开构型中偏离它。 菲涅尔透镜线性且柔性地安装在整形器中，其在展开配置中使其成形为适当的曲率。 一对这些集中器可以铰接在一起以形成方便的收纳和容易部署的组合。
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2.发明授权Structures including synchronously deployable frame members and methods of deploying the same 有权包括可同步部署的帧成员的结构及其部署方法公开(公告)号：US07211722B1
公开(公告)日：2007-05-01
申请号：US10117314
申请日：2002-04-05
申请人： David Michael Murphy
发明人： David Michael Murphy
IPC分类号： H01L31/045 , E04H12/18
CPC分类号： H02S30/20 , H02S20/00 , Y02E10/50 , Y10S136/292
摘要： A lightweight structure for space application is deployable from a compact bundle of interconnected struts into a plurality of tiled substantially rectangular bays. Each bay preferably comprises four or six hinged strut members having substantially rectangular cross sections, such that a solar or other suitable blanket may be compactly nested within the bundled struts. In one aspect of the invention, the blanket is attached to two opposed strut members of a six-member strut bundle, such that the blanket is unfolded during deployment of the strut bundle into a substantially rectangular bay. In another aspect of the invention, the blanket is attached to, and held against, a single strut in a strut bundle. After the strut bundle is deployed into a substantially rectangular bay, the blanket is spread across the bay via a cable mechanism or other deployment mechanism.
摘要翻译： 用于空间应用的轻质结构可从紧凑的互连支撑束部署到多个平铺的大致矩形的间隔中。 每个隔间优选地包括具有基本上矩形横截面的四个或六个铰接支柱构件，使得太阳能或其它合适的毯可以紧凑地嵌套在捆扎的支柱内。 在本发明的一个方面，橡皮布被附接到六个支柱束的两个相对的支柱构件，使得在将支柱束展开成基本上矩形的间隔期间，毯被展开。 在本发明的另一方面，橡皮布附着在支柱中并固定在支柱中的单个支柱上。 在将支撑束部署到基本上矩形的隔间中之后，橡皮布经由电缆机构或其他部署机构跨越隔间延伸。
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公开(公告)号：US5024111A
公开(公告)日：1991-06-18
申请号：US428395
申请日：1989-10-30
申请人： Thomas J. Harvey
发明人： Thomas J. Harvey
IPC分类号： F16F15/04
CPC分类号： F16F15/04
摘要： An adjustment system for a suspension system having the property of providing a zero spring rate response to limited vertical excursions from a reference level, the suspension system including a load suspension spring supported from a load spring anchor. The adjustment system includes a rigid reference element below the suspension spring, bi-directional drive means between the load spring and the load spring anchor, and a probe insertable into an aperture in the reference element. Circuit means are responsive to the location of the probe relative to the reference element, to adjust the elevation of the load spring relative to the reference level and thereby to tend to restore the reference element to the reference level.
摘要翻译： 一种用于悬架系统的调节系统，具有从参考水平向限制的垂直偏移提供零弹簧响应响应的特性，所述悬架系统包括从负载弹簧锚固件支撑的负载悬架弹簧。 该调节系统包括悬挂弹簧下面的刚性参考元件，负载弹簧和负载弹簧锚固件之间的双向驱动装置以及可插入参考元件孔中的探针。 电路装置响应于探针相对于参考元件的位置，以相对于基准电平来调整负载弹簧的高度，从而趋于将参考元件恢复到参考电平。
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公开(公告)号：US20060174930A1
公开(公告)日：2006-08-10
申请号：US11249143
申请日：2005-10-11
申请人： David Murphy , Michael Eskenazi , Brian Spence
发明人： David Murphy , Michael Eskenazi , Brian Spence
IPC分类号： H01L31/042
CPC分类号： B64G1/443 , F24S23/77 , F24S25/00 , F24S2023/872 , F24S2030/16 , H01L31/0504 , H01L31/0547 , H02S30/20 , Y02E10/40 , Y02E10/52 , Y10S136/292
摘要： A solar panel for a spacecraft has a base with a face, and at least one row of solar cells and at least one elongated reflector are mounted on the face of said base. The reflectors and the rows are mounted generally parallel to each other in an alternating fashion. The reflector has a first and a second reflecting side when the reflector is in a deployed position. The reflector is mounted so that the first side of the reflector is adjacent to a row of solar cells and reflects radiation incident on the first side onto the adjacent row of solar cells when said reflector is in a deployed position. Preferably, a plurality of rows and a plurality of reflectors are mounted on the face of the base, with at least one of the reflectors being disposed between two adjacent rows of solar cells.
摘要翻译： 用于航天器的太阳能电池板具有带有表面的基座，并且至少一排太阳能电池和至少一个细长的反射器安装在所述基座的表面上。 反射器和行通常以交替的方式彼此平行地安装。 当反射器处于展开位置时，反射器具有第一和第二反射侧。 反射器被安装成使得反射器的第一侧邻近一排太阳能电池并且当所述反射器处于展开位置时将入射在第一侧上的辐射反射到相邻的太阳能电池行上。 优选地，多个行和多个反射器安装在基座的表面上，其中至少一个反射器设置在两个相邻的太阳能电池列之间。
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公开(公告)号：US5961738A
公开(公告)日：1999-10-05
申请号：US903123
申请日：1997-07-30
申请人： Max D. Benton , P. Alan Jones , Brian Spence , Earl McCutcheon , Carl Devillier
发明人： Max D. Benton , P. Alan Jones , Brian Spence , Earl McCutcheon , Carl Devillier
IPC分类号： B64G1/44 , H01L31/042 , H01L31/045 , H01L31/00
CPC分类号： B64G1/44 , H01L31/0508 , H02S30/20 , B64G1/443 , Y02E10/50 , Y10S136/292
摘要： A solar array with a blanket having solar cells incorporated in modules that can readily be removed, replaced, and accordion-folded to a stowed condition. A scissors array having tracks in which scissors linkages are slidingly fitted enables the array to be stowed or deployed from a container in which the module are interleaved with soft, compressed leaves that protect the blanket from inertial forces during handling and launching.
摘要翻译： 具有毯子的太阳能阵列具有并入模块中的太阳能电池，其可以容易地被移除，替换和折叠折叠到收起状态。 具有轨道的剪刀阵列，其中剪刀连杆滑动地装配，使得阵列可以从容器中收起或展开，在该容器中，模块与柔软的压缩叶片交错，在处理和发射过程中保护毯子不受惯性力的影响。
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6.发明授权
公开(公告)号：US5909197A
公开(公告)日：1999-06-01
申请号：US832982
申请日：1997-04-04
CPC分类号： H01Q11/086 , H01Q1/1235 , H01Q1/288
摘要： A compressible and deployable antenna includes a top and a bottom plate. A deployable structure is fitted between the plates which can forcibly separate the plates, and place in tension a plurality of foldable unstretchable cords to provide a rigid antenna structure. An antenna conductor is connected to the plates and is coiled around the structure in a helical shape so its convolutions can be brought closer to one another for stowage, and spaced farther apart in deployment.
摘要翻译： 可压缩和可展开的天线包括顶板和底板。 可展开的结构装配在板之间，这些板可强制地分开板，并且张紧多个可折叠的不可拉伸的绳索以提供刚性的天线结构。 天线导体连接到板上，并以螺旋形的方式卷绕在结构体周围，因此它们的卷绕可以彼此靠近以进行装载，并在展开中间隔更远。
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公开(公告)号：US07301095B2
公开(公告)日：2007-11-27
申请号：US11249143
申请日：2005-10-11
IPC分类号： H01L25/00
CPC分类号： B64G1/443 , F24S23/77 , F24S25/00 , F24S2023/872 , F24S2030/16 , H01L31/0504 , H01L31/0547 , H02S30/20 , Y02E10/40 , Y02E10/52 , Y10S136/292
摘要： A solar panel for a spacecraft has a base with a face, and at least one row of solar cells and at least one elongated reflector are mounted on the face of the base. The reflectors and the rows are mounted generally parallel to each other in an alternating fashion. The reflector has first and second reflecting sides when the reflector is in a deployed position. The reflector is mounted so that the first side of the reflector is adjacent to a row of solar cells and reflects radiation incident on the first side onto the adjacent row of solar cells when the reflector is in a deployed position. Preferably, a plurality of rows and a plurality of reflectors are mounted on the face of the base, with at least one of the reflectors being disposed between two adjacent rows of solar cells.
摘要翻译： 用于航天器的太阳能电池板具有带有表面的基座，并且至少一排太阳能电池和至少一个细长的反射器安装在基座的表面上。 反射器和行通常以交替的方式彼此平行地安装。 当反射器处于展开位置时，反射器具有第一和第二反射面。 反射器被安装成使得反射器的第一侧邻近一排太阳能电池并且当反射器处于展开位置时将入射在第一侧上的辐射反射到相邻行的太阳能电池上。 优选地，多个行和多个反射器安装在基座的表面上，其中至少一个反射器设置在两个相邻的太阳能电池列之间。
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公开(公告)号：US20040016454A1
公开(公告)日：2004-01-29
申请号：US10351454
申请日：2003-01-24
IPC分类号： H01L031/00
CPC分类号： B64G1/443 , F24S23/77 , F24S25/00 , F24S2023/872 , F24S2030/16 , H01L31/0504 , H01L31/0547 , H02S30/20 , Y02E10/40 , Y02E10/52 , Y10S136/292
摘要： A solar panel for a spacecraft has a base with a face, and at least one row of solar cells and at least one elongated reflector are mounted on the face of said base. The reflectors and the rows are mounted generally parallel to each other in an alternating fashion. The reflector has a first and a second reflecting side when the reflector is in a deployed position. The reflector is mounted so that the first side of the reflector is adjacent to a row of solar cells and reflects radiation incident on the first side onto the adjacent row of solar cells when said reflector is in a deployed position. Preferably, a plurality of rows and a plurality of reflectors are mounted on the face of the base, with at least one of the reflectors being disposed between two adjacent rows of solar cells.
摘要翻译： 用于航天器的太阳能电池板具有带有表面的基座，并且至少一排太阳能电池和至少一个细长的反射器安装在所述基座的表面上。 反射器和行通常以交替的方式彼此平行地安装。 当反射器处于展开位置时，反射器具有第一和第二反射侧。 反射器被安装成使得反射器的第一侧邻近一排太阳能电池并且当所述反射器处于展开位置时将入射在第一侧上的辐射反射到相邻的太阳能电池行上。 优选地，多个行和多个反射器安装在基座的表面上，其中至少一个反射器设置在两个相邻的太阳能电池列之间。
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公开(公告)号：US5154027A
公开(公告)日：1992-10-13
申请号：US758266
申请日：1991-08-26
申请人： Robert M. Warden
发明人： Robert M. Warden
CPC分类号： B64G9/00 , E04H12/185
摘要： A deployable and retractable mast which can be rotated while deployed, using only one drive means for all three functions. Flexible longerons carry followers which pass through guides in a storage cannister for transition between a coiled retracted condition and an extended deployed condition. The followers pass through a gate opening, past a gate, and when the mast is rotated, the gates enable or prevent followers from taking the longerons into the retracted condition, and entitles rotation of the mast when retraction is disabled.
摘要翻译： 可部署和可收回的桅杆，可在部署时旋转，仅使用一个驱动装置用于所有三种功能。 柔性长臂带有通过存储罐中的引导件的跟随器，用于在卷绕的缩回状态和扩展的部署状态之间过渡。 跟随者穿过门开口，通过门，当桅杆旋转时，门使得或阻止从动装置将长臂进入缩回状态，并且在缩回被禁用时有权旋转桅杆。
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10.发明授权1-(o-chlorophenyl)-and 1-(o, p-dichlorophenyl)-2-hydrazinopropanes 失效1-（邻氯苯基） - 和1-（邻，对 - 二氯苯基）-2-肼基丙烷
公开(公告)号：US3341591A
公开(公告)日：1967-09-12
申请号：US85754259
申请日：1959-12-07
申请人： UPJOHN CO
发明人： SCHUMANN EDWARD L
IPC分类号： C07C45/00 , C07C49/223 , C07C241/02
CPC分类号： C07C243/18
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