Mounting apparatus to secure solar panel rails to flat tile roofs

    公开(公告)号:US09954479B1

    公开(公告)日:2018-04-24

    申请号:US15667421

    申请日:2017-08-02

    CPC classification number: H02S20/24 F24S25/00 F24S25/35 F24S25/636 H02S30/10

    Abstract: A mounting apparatus to secure a pair of solar panel rails to a flat tile roof and minimize penetrations or damage to the roof's rafter is provided. The mounting apparatus includes a lower hook assembly with a plurality of arm members continuously connected together, the plurality of arm members having a first end coupled to the rafter of the flat tile roof and a second end, and an upper arm assembly coupled to the second end of the plurality of arms of the lower hook assembly, the upper arm assembly having a generally U-shaped member comprising a first symmetric half member and a second symmetric half member, each symmetric half member having a slot to receive a fastener that secures one of the pair of solar panel rails thereto, thereby permitting the mounting apparatus to support the pair of solar panel rails above the flat tile roof.

    Solar assembly and method of forming same
    10.
    发明授权
    Solar assembly and method of forming same 有权
    太阳能组件及其形成方法

    公开(公告)号:US09595910B2

    公开(公告)日:2017-03-14

    申请号:US13551799

    申请日:2012-07-18

    Abstract: Various aspect provide for a solar assembly. The solar assembly may be a mechanical structure that allows many small solar cells to be integrated into the wing design of an aircraft without placing them on the surface area of the wing or the vehicle. Additional aspects may provide for an adjustable solar assembly. The adjustable solar assembly may be configured to be installed into a structure having a structural profile. When installed, the solar assembly may conform to the structural profile such that the structural profile is maintained. The solar assembly may further comprise an adjustable carrier system comprising a plurality of solar cells attached thereto. The adjustable carrier system may be configured to dynamically adjust the orientation of the solar cells so as to maintain an optimal angle with respect to an external light source.

    Abstract translation: 各种方面提供太阳能组件。 太阳能组件可以是机械结构,其允许许多小型太阳能电池被集成到飞机的机翼设计中而不将它们放置在机翼或车辆的表面区域上。 另外的方面可以提供可调太阳能组件。 可调节的太阳能组件可以被配置成安装到具有结构轮廓的结构中。 当安装时,太阳能组件可以符合结构轮廓,使得维持结构轮廓。 太阳能组件还可以包括可调节的载体系统,其包括附接到其上的多个太阳能电池。 可调节载体系统可以被配置为动态地调整太阳能电池的取向,以便相对于外部光源保持最佳角度。

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