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    Integrated modular photovoltaic blanket assembly for space solar array
    2.
    发明授权
    Integrated modular photovoltaic blanket assembly for space solar array 有权

    公开(公告)号：US09620658B1

    公开(公告)日：2017-04-11

    申请号：US13797682

    申请日：2013-03-12

    申请人： Brian R Spence ,  Stephen F White ,  Mark V Douglas ,  Kevin B Schmid ,  Ron S Takeda

    发明人： Brian R Spence ,  Stephen F White ,  Mark V Douglas ,  Kevin B Schmid ,  Ron S Takeda

    IPC分类号： H01L31/044 ,  H02S30/20 ,  H01L31/041

    CPC分类号： B64G1/42 ,  H01L31/041 ,  H02S20/00 ,  H02S30/20 ,  Y02E10/50

    摘要： A modular, lightweight, high-survivable, photovoltaic flexible blanket assembly for a space solar array is disclosed. The modular blanket is an accordion foldable or rollable flexible photovoltaic solar panel blanket assembly comprising a plurality of common photovoltaic modules spaced in an orthogonal pattern. Each module is mechanically attached with multiple low profile fasteners on their backside to an open weave mesh tensioned backplane structure. The backplane forms a tensioned dimensionally stable planar surface in the deployed configuration onto which the modules are suspended. Each module is common and comprised of a rectangular substrate that includes solar cell assemblies, circuitry, exposed electrical contacts for integration of blanket-level harnessing, and frontside and rearside shielding and coatings as required for the mission application. The blanket assembly may be dispersed with an open pattern of compliant and formable material on the backside to provide insulation against the vigorous vibration of the launch environment.

    SOLAR CELL ASSEMBLY, SOLAR CELL PANEL, AND METHOD FOR MANUFACTURING THE SAME
    5.
    发明申请
    SOLAR CELL ASSEMBLY, SOLAR CELL PANEL, AND METHOD FOR MANUFACTURING THE SAME 审中-公开
    太阳能电池组件，太阳能电池板及其制造方法

    公开(公告)号：US20150311372A1

    公开(公告)日：2015-10-29

    申请号：US14793289

    申请日：2015-07-07

    申请人： SolAero Technologies Corp.

    发明人： Cory TOURINO

    IPC分类号： H01L31/05 ,  H01L31/041 ,  H01L31/048

    CPC分类号： H01L31/0508 ,  B64G1/443 ,  B64G1/54 ,  H01L31/041 ,  H01L31/048 ,  H01L31/0512 ,  H02S30/20 ,  Y02E10/50

    摘要： A solar cell assembly, a solar cell array, and a method for manufacturing the same are provided. The solar cell assembly may include a solar cell and an interconnection member, the interconnection member comprising a first portion and a second portion attached to the first portion with an angle formed therebetween. The solar cell array may comprise at least two said solar cell assemblies. In an embodiment, the top surfaces of the first solar cell and the second solar cell are arranged such that the second portion of the first interconnect member and the second portion of the second interconnection member are adjacent to each other, and at least the end portion of the second portion of the first interconnection member is bended together with at least the end portion of the second portion of the second interconnection member.

    摘要翻译： 提供太阳能电池组件，太阳能电池阵列及其制造方法。 太阳能电池组件可以包括太阳能电池和互连构件，所述互连构件包括第一部分和附接到第一部分的第二部分，其间形成有角度。 太阳能电池阵列可以包括至少两个所述太阳能电池组件。 在一个实施例中，第一太阳能电池和第二太阳能电池的顶表面布置成使得第一互连构件的第二部分和第二互连构件的第二部分彼此相邻，并且至少端部 所述第一互连构件的第二部分与所述第二互连构件的第二部分的至少所述端部弯曲在一起。

    Solar cell assembly, solar cell panel, and method for manufacturing the same
    6.
    发明授权
    Solar cell assembly, solar cell panel, and method for manufacturing the same 有权
    太阳能电池组件，太阳能电池板及其制造方法

    公开(公告)号：US09153721B1

    公开(公告)日：2015-10-06

    申请号：US14793289

    申请日：2015-07-07

    申请人： SolAero Technologies Corp.

    发明人： Cory Tourino

    IPC分类号： H01L31/042 ,  H01L31/05 ,  H01L31/048 ,  H01L31/041

    CPC分类号： H01L31/0508 ,  B64G1/443 ,  B64G1/54 ,  H01L31/041 ,  H01L31/048 ,  H01L31/0512 ,  H02S30/20 ,  Y02E10/50

    摘要： A solar cell assembly, a solar cell array, and a method for manufacturing the same are provided. The solar cell assembly may include a solar cell and an interconnection member, the interconnection member comprising a first portion and a second portion attached to the first portion with an angle formed therebetween. The solar cell array may comprise at least two said solar cell assemblies. In an embodiment, the top surfaces of the first solar cell and the second solar cell are arranged such that the second portion of the first interconnect member and the second portion of the second interconnection member are adjacent to each other, and at least the end portion of the second portion of the first interconnection member is bended together with at least the end portion of the second portion of the second interconnection member.

    摘要翻译： 提供太阳能电池组件，太阳能电池阵列及其制造方法。 太阳能电池组件可以包括太阳能电池和互连构件，所述互连构件包括第一部分和附接到第一部分的第二部分，其间形成有角度。 太阳能电池阵列可以包括至少两个所述太阳能电池组件。 在一个实施例中，第一太阳能电池和第二太阳能电池的顶表面布置成使得第一互连构件的第二部分和第二互连构件的第二部分彼此相邻，并且至少端部 所述第一互连构件的第二部分与所述第二互连构件的第二部分的至少所述端部弯曲在一起。

    Radiation Stable Shield
    7.
    发明申请
    Radiation Stable Shield 有权
    辐射稳定盾

    公开(公告)号：US20140007924A1

    公开(公告)日：2014-01-09

    申请号：US13935999

    申请日：2013-07-05

    申请人： Qioptiq Limited

    发明人： Andy GRAY

    IPC分类号： G21F1/06 ,  H01L31/04

    CPC分类号： G21F1/06 ,  G21F1/00 ,  H01L31/041

    摘要： There is disclosed a radiation stable shield for use in space or high altitude applications. The shield comprises a plurality of overlapping planar glass flakes which are held in a lamellar matrix of flexible polymeric material. The flakes are each formed of a radiation stable glass which is suitable for use in space or high altitude applications. The flakes are arranged in alignment with the lamellar direction of the matrix.

    摘要翻译： 公开了一种用于空间或高空应用的辐射稳定屏蔽。 屏蔽包括多个重叠的平面玻璃薄片，其保持在柔性聚合物材料的层状基质中。 薄片各自由适用于空间或高空应用的辐射稳定玻璃形成。 薄片布置成与矩阵的层状方向对齐。

    Electrical discharge countermeasure device
    8.
    发明授权
    Electrical discharge countermeasure device 有权
    放电对策装置

    公开(公告)号：US08014121B2

    公开(公告)日：2011-09-06

    申请号：US12303394

    申请日：2007-06-01

    申请人： Mengu Cho ,  Yuya Sanmaru ,  Satoshi Hosoda ,  Minoru Iwata ,  Tatsuhito Fujita ,  Yasumasa Hisada

    发明人： Mengu Cho ,  Yuya Sanmaru ,  Satoshi Hosoda ,  Minoru Iwata ,  Tatsuhito Fujita ,  Yasumasa Hisada

    IPC分类号： H02H1/00

    CPC分类号： B64G1/52 ,  B64D45/02 ,  B64G1/443 ,  B64G1/546 ,  H01L31/041 ,  Y02E10/50

    摘要： The present invention prevents occurrence of electrical discharge on an electrically conductive structure in an environment in which high-energy electrons impinge onto the structure or on an electronic element mounted to a surface of the structure, which electrical discharge would otherwise occur when the potential of the structure or the electronic element increases in the negative direction due to a negative charge flowing thereinto. An insulating tape bonded to the surface of the electrically conductive structure is partially cut-removed; an electrically conductive adhesive is applied to an exposed portion of the surface of the electrically conductive structure; and an insulating film is bonded to the electrically conductive adhesive, such that the electrically conductive adhesive is exposed to the outside. When encountering higher-energy electrons, the insulating film is charged, so that a strong electric field is applied to the electrically conductive adhesive, and electrons are emitted from the electrically conductive adhesive through field electron emission, to thereby prevent the potential of the electrically conductive structure from increasing in the negative direction.

    摘要翻译： 本发明防止在高能电子撞击到结构上或安装在结构表面上的电子元件的环境中导电结构上的放电发生，否则当电位为 结构或电子元件由于负电荷流入其而在负方向上增加。 结合到导电结构的表面的绝缘带被部分地切除; 将导电粘合剂施加到导电结构的表面的暴露部分; 并且绝缘膜粘合到导电粘合剂上，使得导电粘合剂暴露于外部。 当遇到高能电子时，绝缘膜被充电，使得强电场被施加到导电粘合剂上，并且电子通过场电子发射从导电粘合剂发射，从而防止导电的电位 结构从负方向增加。

    Flexible solar array cell and substrate therefor
    10.
    发明授权
    Flexible solar array cell and substrate therefor 失效
    柔性太阳能阵列电池及其基板

    公开(公告)号：US4755231A

    公开(公告)日：1988-07-05

    申请号：US873895

    申请日：1986-06-13

    申请人： Richard M. Kurland ,  Ira L. Allard ,  Rebecca C. Chaky ,  George T. Inouye, deceased

    发明人： Richard M. Kurland ,  Ira L. Allard ,  Rebecca C. Chaky ,  George T. Inouye, deceased

    IPC分类号： H01L31/0392 ,  H01L31/04 ,  H01L25/02 ,  H01L27/14

    CPC分类号： H01L31/0392 ,  H01L31/03926 ,  H01L31/041 ,  Y02E10/50 ,  Y10S136/292

    摘要： A substrate structure for lightweight, flexible solar cell arrays, in which a plastic substrate is provided with a structure for discharging accumulations of electrons on its rear face and has appropriate heat emmissivity properties. In one embodiment, a Kapton substrate layer is coated with a grounded aluminum layer, which is suitably painted for emissivity. In another embodiment, a poorly conductive Kapton substrate layer, impregnated with carbon, is used to dissipate the charge, and to provide the appropriate emissivity. In a third embodiment, a grounded VDA layer is sandwiched between two Kapton layers.

    摘要翻译： 一种用于轻质柔性太阳能电池阵列的基板结构，其中塑料基板设置有用于在其后表面上排放电子的积聚的结构，并且具有适当的散热特性。 在一个实施例中，Kapton基底层涂覆有接地的铝层，其被适当地用于发射率。 在另一个实施方案中，用碳浸渍的导电不良的Kapton衬底层用于耗散电荷并提供适当的发射率。 在第三实施例中，接地的VDA层夹在两个Kapton层之间。