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Solar ray collection rate fluctuation analysis with Monte Carlo Ray Tracing method for space solar power satellite

机译:太空太阳能卫星蒙特卡罗射线追踪法的太阳射线收集率波动分析。

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摘要

According to the ideal optical design, the spherical concentrator made by the semi-transparent and semi-reflecting thin film is used in SSPS-OMEGA system. To obtain the continuous power, the PV array should rotate around the spherical concentrator to point the sun when SSPS-OMEGA rotate around the earth on GEO. However, considering the in-orbit assembly, the concentrator is assembled by many planar elements to be approximate to the ideal spherical concentrator. The solar ray collection rate fluctuates in certain scope because the original solar ray path is changed. In addition, planar element is deformed easily by the rotating PV array, which also lead to the fluctuation because the position of the planar element is changed. In this paper, the spherical concentrator is divided into many planar elements by using equal latitude and longitude method. It is studied that the relationship between the number of division layers and the collection rate fluctuation by using Monte Carlo Ray Tracing method. The simulation results indicate that with increasing dividing layers, the collection rate increases and the fluctuation amplitude decreases, which ranges 80.72-83.70% (2.98%) of 24-layers concentrator, ranges 88.45-89.91% (1.47%) of 48-layers concentrator, and ranges 92.46-93.80% (1.33%) of 72-layers concentrator. To solve the deformation of the concentrator, the flexible multibody dynamics model of SSPS-OMEGA is established. Combing the deformation and Monte Carlo Ray Tracing method, it is studied that the relationship between the deformation of the concentrator and the collection rate. The simulation results indicate that the stiffness of 72-layers concentrator is better than 24-layers concentrator and 48-layers concentrator, and the reduction of the collection rate of 72-layers concentrator, which is 0.4%, is less than 24-layers concentrator (1.57%) and 48-layers concentrator (0.81%).
机译:根据理想的光学设计,在SSPS-OMEGA系统中使用由半透明和半反射薄膜制成的球形聚光器。为了获得连续功率,当SSPS-OMEGA在GEO上绕地球旋转时,PV阵列应绕球形聚光器旋转以指向太阳。然而,考虑到在轨组装,该集中器由许多平面元件组装成近似于理想球形集中器。由于原始太阳光线的路径发生了变化,因此太阳光线的收集率会在一定范围内波动。另外,平面元件容易由于旋转的PV阵列而变形,这也由于平面元件的位置改变而导致波动。本文采用经纬度相等的方法将球形聚光器分为许多平面单元。利用蒙特卡洛射线追踪法研究了分离层数与收集率波动之间的关系。仿真结果表明,随着层数的增加,收集率增加,波动幅度减小,其中24层浓缩器的范围为80.72-83.70%(2.98%),48层浓缩器的范围为88.45-89.91%(1.47%) ,范围为72层浓缩器的92.46-93.80%(1.33%)。为了解决集中器的变形问题,建立了SSPS-OMEGA的柔性多体动力学模型。结合变形和蒙特卡洛射线追踪法,研究了聚光器的变形与收集率之间的关系。仿真结果表明,72层选矿机的刚度好于24层选矿机和48层选矿机,而72层选矿机的捕集率下降0.4%,小于24层选矿机。 (1.57%)和48层浓缩器(0.81%)。

著录项

  • 来源
    《Solar Energy》 |2019年第6期|235-244|共10页
  • 作者单位

    Xidian Univ, Shaanxi Key Lab Space Solar Power Stn Syst, Xian 710071, Shaanxi, Peoples R China|Xidian Univ, Minist Educ, Key Lab Elect Equipment Struct Design, Xian 710071, Shaanxi, Peoples R China;

    Xidian Univ, Shaanxi Key Lab Space Solar Power Stn Syst, Xian 710071, Shaanxi, Peoples R China|China Acad Space Technol, Qian Xuesen Lab Space Technol, Beijing 100094, Peoples R China|Xidian Univ, Minist Educ, Key Lab Elect Equipment Struct Design, Xian 710071, Shaanxi, Peoples R China;

    Xidian Univ, Shaanxi Key Lab Space Solar Power Stn Syst, Xian 710071, Shaanxi, Peoples R China|Xidian Univ, Minist Educ, Key Lab Elect Equipment Struct Design, Xian 710071, Shaanxi, Peoples R China;

    Xidian Univ, Shaanxi Key Lab Space Solar Power Stn Syst, Xian 710071, Shaanxi, Peoples R China|Xidian Univ, Minist Educ, Key Lab Elect Equipment Struct Design, Xian 710071, Shaanxi, Peoples R China;

    China Acad Space Technol, Qian Xuesen Lab Space Technol, Beijing 100094, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Space solar power satellite; Concentrator; Flexible multibody dynamics; Solar ray collection rate; Monte Carlo Ray Tracing method;

    机译:空间太阳能卫星聚光器灵活的多体动力学太阳能收集率蒙特卡罗射线追踪法;

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