-
公开(公告)号：US09086573B2
公开(公告)日：2015-07-21
申请号：US14578748
申请日：2014-12-22
申请人： HELIOFOCUS LTD.
发明人： Yanir Blumenthal , Oren Gadot , Thomas Keck , Wolfgang Schiel , Hristo Zlatanov
CPC分类号： G02B26/0816 , F24S23/77 , F24S25/00 , F24S30/40 , F24S30/452 , F24S2020/23 , F24S2023/874 , F24S2030/115 , F24S2030/145 , G02B7/183 , G02B19/0019 , G02B19/0042 , Y02E10/47
摘要： A plural axis sun tracking system, including a base, a spatial structure assembly, and a rotating system mounted on the base for rotating the spatial structure assembly, where the spatial structure assembly includes a frame having a lower portion at a first peripheral end of the spatial structure assembly and an upper portion at a second peripheral end of the spatial structure assembly, the lower portion being more proximal to the rotating system than the upper portion, and an anchoring location for anchoring the spatial structure assembly to the rotating system, the anchoring location located at the lower portion, where the mass of the frame increasingly recedes as the distance from the anchoring location towards the upper portion increases.
摘要翻译： 一种多轴太阳跟踪系统，包括基座，空间结构组件和安装在基座上的用于旋转空间结构组件的旋转系统，其中空间结构组件包括框架，该框架在第一外围端处具有下部 空间结构组件和在空间结构组件的第二外周端处的上部，下部比上部更靠近旋转系统，以及用于将空间结构组件锚定到旋转系统的锚定位置，锚定 位于下部的位置，随着距离锚固位置朝向上部的距离的增加，框架的质量逐渐减小。
-
公开(公告)号：US09377217B2
公开(公告)日：2016-06-28
申请号：US14373376
申请日：2013-01-21
申请人： HELIOFOCUS, LTD.
CPC分类号： F24S50/20 , F24S23/70 , F24S23/71 , F24S25/00 , F24S30/452 , F24S80/00 , F24S2023/876 , F24S2030/115 , F24S2030/145 , G02B7/183 , Y02E10/42 , Y02E10/47
摘要： A solar concentrating system for concentrating sunlight by tracking the sun, including concentrator support structure, an annular track mounted on an upper surface of a base, the center of mass of the concentrator support structure being off-axis relative to curvature center of annular track, enclosures provided at comers and comprising a wheel positioned on the track, the enclosure connected to a piston connected to a guiding element placed on the track; a fastening element that when moved towards the track, the guiding element is fastened to the track, and when the fastening element is moved away from the track, the guiding element is released, when the first piston elongates or contracts, the first guiding element is fastened to the track, the second guiding element is released, the wheels of the enclosures rotate from a first location on the track to a second location, thereby rotating the concentrator support structure.
摘要翻译： 一种用于通过跟踪太阳来集中太阳的太阳能集中系统，包括集中器支撑结构，安装在基座的上表面上的环形轨道，聚光器支撑结构的质心相对于环形轨道的弯曲中心离轴， 设置在角落处并且包括定位在轨道上的轮的外壳，所述外壳连接到连接到放置在轨道上的引导元件的活塞; 紧固元件，当向轨道移动时，引导元件紧固到轨道上，并且当紧固元件远离轨道移动时，引导元件被释放，当第一活塞伸长或收缩时，第一引导元件是 固定到轨道上，第二引导元件被释放，外壳的轮从轨道上的第一位置旋转到第二位置，从而旋转集中器支撑结构。
-
公开(公告)号：US20140352686A1
公开(公告)日：2014-12-04
申请号：US14373376
申请日：2013-01-21
申请人： HELIOFOCUS, LTD.
IPC分类号： F24J2/38
CPC分类号： F24S50/20 , F24S23/70 , F24S23/71 , F24S25/00 , F24S30/452 , F24S80/00 , F24S2023/876 , F24S2030/115 , F24S2030/145 , G02B7/183 , Y02E10/42 , Y02E10/47
摘要： A solar concentrating system for concentrating sunlight by tracking the sun, including concentrator support structure, an annular track mounted on an upper surface of a base, the center of mass of the concentrator support structure being off-axis relative to curvature center of annular track, enclosures provided at comers and comprising a wheel positioned on the track, the enclosure connected to a piston connected to a guiding element placed on the track; a fastening element that when moved towards the track, the guiding element is fastened to the track, and when the fastening element is moved away from the track, the guiding element is released, when the first piston elongates or contracts, the first guiding element is fastened to the track, the second guiding element is released, the wheels of the enclosures rotate from a first location on the track to a second location, thereby rotating the concentrator support structure.
摘要翻译： 一种用于通过跟踪太阳来集中太阳的太阳能集中系统，包括集中器支撑结构，安装在基座的上表面上的环形轨道，聚光器支撑结构的质心相对于环形轨道的弯曲中心离轴， 设置在角落处并且包括定位在轨道上的轮的外壳，所述外壳连接到连接到放置在轨道上的引导元件的活塞; 紧固元件，当向轨道移动时，引导元件紧固到轨道上，并且当紧固元件远离轨道移动时，引导元件被释放，当第一活塞伸长或收缩时，第一引导元件是 固定到轨道上，第二引导元件被释放，外壳的轮从轨道上的第一位置旋转到第二位置，从而旋转集中器支撑结构。
-
-
搜索结果
3 条记录 (耗时 0.009 秒)
