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    • 24. 发明授权
    • Application of carbon fiber mesh for space and airborne platform applications
    • 碳纤维网应用于空间和机载平台应用
    • US06547190B1
    • 2003-04-15
    • US10139934
    • 2002-05-06
    • Brian D. ThompsonWah L. Lim
    • Brian D. ThompsonWah L. Lim
    • H01L2500
    • B64G1/443Y10S136/292Y10T428/249924Y10T428/249928Y10T428/249986
    • A solar array including a carbon fiber mesh substrate is provided. The solar panels including a series of hybrid structures formed along the common and continuous substrate by sandwiching the substrate between a series of discontinuous upper and lower support layers. In order to construct the solar panels having such hybrid structure, a series of top support layers or upper face sheets is disposed on a upper surface of the substrate and between the folding sections. The solar cells are placed on top of the upper face sheets. Similarly, a series of lower support layers or lower face sheets are disposed on a bottom surface of the substrate and between the folding sections. The folding sections are the regions where the upper and lower face sheets discontinue and expose the underlying substrate. The solar array can be folded along the folding section when a bending force is applied over one of the hybrid structures.
    • 提供了包括碳纤维网状基材的太阳能电池阵列。 太阳能电池板包括通过将衬底夹在一系列不连续的上部和下部支撑层之间沿着共同和连续衬底形成的一系列混合结构。 为了构造具有这种混合结构的太阳能电池板,在衬底的上表面和折叠部之间设置一系列顶部支撑层或上表面片。 太阳能电池放置在上表面的顶部。 类似地,一系列下支撑层或下表面片设置在基底的底表面和折叠部分之间。 折叠部分是上下面板中断并暴露下面的基底的区域。 当弯曲力施加在混合结构之一上时,太阳能阵列可以沿着折叠部折叠。