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11.
公开(公告)号:US6111190A
公开(公告)日:2000-08-29
申请号:US040733
申请日:1998-03-18
Applicant: Mark Joseph O'Neill
Inventor: Mark Joseph O'Neill
IPC: B64G1/44 , B64G1/50 , F24S23/30 , H01L31/052 , H01L31/045 , F24J2/36
CPC classification number: F24J2/085 , B64G1/443 , H01L31/0543 , H01L31/0547 , B64G1/503 , Y02E10/43 , Y02E10/52 , Y10S126/909
Abstract: A novel, high-efficiency, extremely light-weight, inflatable refractive solar concentrator for space power is described. It consists of a flexible Fresnel lens, flexible sides, and a back surface, together enclosing a volume of space which can be filled with low pressure gas to deploy the concentrator on orbit. The back surface supports the energy receiver/converter located in the focal region of the Fresnel lens. The back surface can also serve as the waste heat radiator. Prior to deployment, the deflated flexible lens and sides are folded against the back surface to form a flat, low-volume package for efficient launch into space. The inflatable concentrator can be configured to provide either a line focus or a point focus of sunlight. The new inflatable concentrator approach will provide significant advantages over the prior art in two different space power areas: photovoltaic concentrator arrays and high-temperature solar thermal conversion systems. Photovoltaic concentrator arrays using the new inflatable lens will be much lighter than prior space concentrator arrays. In addition, for photovoltaic concentrator arrays, the new inflatable lens will eliminate the need for a fragile glass superstrate to support the lens, substantially improving robustness of the lens. Solar thermal concentrator arrays using the new inflatable lens will be much lighter than prior art space concentrators which used parabolic mirrors. In addition, for solar thermal applications in space, the new inflatable lens will eliminate the need for high surface accuracy, which has been a significant problem for prior art concentrators.
Abstract translation: 描述了一种用于空间动力的新颖,高效,极轻重量的充气折射式太阳能聚光器。 它由柔性菲涅尔透镜,柔性侧面和后表面组成,共同包围一定量的空间,可以充满低压气体以将集中器部署在轨道上。 后表面支撑位于菲涅尔透镜焦点区域的能量接收器/转换器。 背面也可以作为废热散热器。 在展开之前,放气的柔性透镜和侧面折叠在背面上以形成平坦的低容量包装,以有效地发射到太空中。 可充气聚光器可以被配置成提供阳光的线焦点或点聚焦。 在两个不同的空间电力领域中,新的充气聚光器方法将比现有技术显着优点:光伏聚光器阵列和高温太阳能热转换系统。 使用新的充气镜头的光伏集中器阵列将比以前的空间集中器阵列轻得多。 此外,对于光伏聚光器阵列,新的充气镜头将不需要一个易碎的玻璃底板来支撑透镜,从而显着改善透镜的坚固性。 使用新的充气镜头的太阳能集热器阵列将比使用抛物面镜的现有技术的空间集中器轻得多。 另外,对于空间太阳能热应用,新的充气镜头将消除对高表面精度的需要,这对于现有技术的聚光器来说是一个重大的问题。
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公开(公告)号:US5648873A
公开(公告)日:1997-07-15
申请号:US655578
申请日:1996-05-30
Applicant: Paul A. Jaster , Mark Joseph O'Neill
Inventor: Paul A. Jaster , Mark Joseph O'Neill
CPC classification number: F24J2/062 , F21S11/00 , F24J2/085 , F24J2/15 , G02B19/0028 , G02B19/0042 , G02B19/008 , E04D2013/034 , Y02B10/20 , Y02E10/43
Abstract: An apparatus designed to direct daylight through an aperture toward a target area in a building or other structure is disclosed. A housing provides a base attachable to the building and a support structure for supporting a reflector above the aperture. According to one embodiment of the invention the reflector is in the shape of an inverted cone. A light diffusing lens structure is disposed in the optical path between the reflector and the target area. In use, light is transmitted through the support structure, reflected from the surface of the reflector, and dispersed about the target area by the light diffusing lens structure.
Abstract translation: 公开了一种设计用于将日光通过孔径朝向建筑物或其他结构中的目标区域的装置。 壳体提供可附接到建筑物的基座和用于支撑孔上方的反射器的支撑结构。 根据本发明的一个实施例,反射器为倒锥形。 光漫射透镜结构设置在反射器和目标区域之间的光路中。 在使用中,光通过支撑结构透射,从反射体的表面反射,并通过光漫射透镜结构分散在目标区域周围。
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