柔性光伏板的仿真指导设计

S. Athreya, R. Sharma, K. Kauffmann, L. López, Jie Feng
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引用次数: 1

摘要

光伏(PV)模块是使用各种光伏电池技术制造的。每种光伏技术的封装要求各不相同,并取决于其固有的热机械性能和电池的环境稳定性。相对于-à-vis刚性和脆性的竞争对手,薄膜光伏具有相对的灵活性优势。本文讨论了使用有限元分析(FEA)来开发一个框架,用于指导利用薄膜光伏电池的柔性建筑集成光伏(BIPV)瓦的设计。选择微玻璃(0.2-0.3 mm厚的玻璃)作为顶部阻挡层,以利用薄膜PV材料的柔韧性。然而,微玻璃本身并不能为瓦板提供足够的保护,以满足法规的抗冲击要求。本文讨论了利用有限元分析来指导增强聚合物层的选择及其在微玻璃周围的放置,以使微玻璃基柔性层压板能够承受冰雹的冲击。采用有限元分析方法指导增强聚合物的选择及其在层压板结构中的位置。冰雹冲击建模为静态压痕,并计算了层压板各层的应力。该模型用于比较大约50种通过系统改变聚合物力学性能和层压板设计而产生的层压板。通过对微玻璃层和其他层的应力分析,发现最优的层压板设计是在微玻璃层上加一层弹性增强层,在其下加一层刚性聚合物层。在弹性体层之上的另一层刚性聚合物可以进一步减小层压板中的应力;然而,相对较大的厚度的这一层可能需要得到任何显著的应力降低。已确定刚性增强层的理想位置是在单元和底部阻隔层之间。模型预测已通过冰雹冲击试验得到部分验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Simulation guided design of flexible photovoltaic laminates
Photovoltaic (PV) modules are manufactured using various PV cell technologies. The packaging requirements vary for each of the PV technologies and depend on their inherent thermo-mechanical properties and environmental stability of the cell. Thin film PV has the relative advantage of flexibility vis-à-vis their rigid and brittle competitors. This paper discusses the use of Finite Element Analysis (FEA) to develop a framework for guiding the design of flexible Building Integrated Photovoltaic (BIPV) shingles utilizing thin film PV cells. Microglass (0.2-0.3 mm thick glass) was chosen as the top barrier layer to exploit the flexibility of the thin film PV material. However, microglass alone does not provide sufficient protection to the shingle to meet regulatory impact resistance requirements. This paper discusses the use of FEA to guide the selection of reinforcing polymer layers and their placement around the microglass to enable microglass-based flexible laminates to sustain hail impact. FEA was used to guide the selection of reinforcing polymers and their placement in the laminate structure. Hail impact was modeled as static indentation and stresses were calculated in all layers of the laminate. This model was used to compare around 50 laminates generated through systematic variation of the polymer mechanical properties and laminate designs. Based on the analysis of the stresses generated in the microglass and other layers in these laminates, it is found that the optimal laminate design would consist of an elastomeric reinforcing layer above the microglass and a rigid polymer layer below it. An additional layer of a rigid polymer above the elastomeric layer can further reduce stresses in the laminate; however, relatively large thickness of this layer might be needed to get any significant stress reduction. The ideal location for the rigid reinforcing layer has been identified to be between the cell and the bottom barrier layer. The model predictions have been partially validated through hail impact testing.
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