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A sunlight to microwave power transmission module prototype for space solar power.

机译:用于太空太阳能的日光到微波功率传输模块原型。

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摘要

The prospect of effectively limitless, continuous electricity from orbiting satellites for use on earth has captured many people's interest for decades. The proposed approach typically entails collection of solar energy, its conversion to microwave energy, and the wireless transmission of the microwaves to the earth. This offers the benefit of providing baseload power while avoiding diurnal cycle and atmospheric losses associated with terrestrial solar power. Proponents have contended that the implementation of such systems would offer energy security, environmental, and broad technological advantages to those who would undertake their development, while critics have pointed out economic, political, and logistical barriers. Niche applications, such as provision of power to remote military bases, might better tolerate the higher energy costs associated with early operational systems.;Among recent implementations commonly proposed for solar power satellites, highly modular concepts have received considerable attention. Each employs an array of modules for performing conversion of sunlight into microwaves for transmission to earth. This work details results achieved in the design, development, integration, and testing of photovoltaic arrays, power electronics, microwave conversion electronics, and antennas for 2.45 GHz microwave-based "sandwich" module prototypes. Prototypes were fabricated and subjected to the challenging conditions inherent in the space environment, including solar concentration levels in which an array of modules might be required to operate. This testing of sandwich modules for solar power satellites in vacuum represents the first such effort.;The effort culminated with two new sandwich module designs, "tile" and "step", each having respectively area-specific masses of 21.9 kg/m2 and 36.5 kg/m2, and mass-specific power figures of 4.5 W/kg at minimum one sun and 5.8 W/kg at minimum 2.2 suns (AM0) simulated solar illumination. The total combined sunlight to microwave efficiency of the modules was shown to be on the order of 8% and 7% for vacuum operation in the 10-6 torr regime. These represent the highest reported combined sandwich module efficiencies under either ambient or vacuum conditions, nearly quadrupling the previous efficiency record. The novel "step" concept was created to address thermal concerns and resulted in a patent publication.;Results from module characterization are presented in context and compared with figures of merit, and practical thresholds are formulated and applied. The results and discussion presented provide an empirical basis for assessment of solar power satellite economic models, and point to several opportunities for improvements in area-specific mass, mass-specific power, and combined conversion efficiency of future prototypes.
机译:数十年来,轨道卫星为地球使用的有效无限,连续电力的前景吸引了许多人的兴趣。提出的方法通常需要收集太阳能,将其转换为微波能量以及将微波无线传输到地球。这提供了提供基本负载功率的好处,同时避免了与地面太阳能相关的昼夜循环和大气损失。支持者争辩说,这样的系统的实施将为那些进行开发的人们提供能源安全,环境和广泛的技术优势,而批评者指出了经济,政治和后勤方面的障碍。利基应用,例如为偏远的军事基地供电,可能会更好地忍受与早期作战系统相关的更高的能源成本。在最近为太阳能卫星普遍提出的实现中,高度模块化的概念受到了相当大的关注。每个模块都采用一系列模块,用于将太阳光转换为微波以传输到地球。这项工作详细介绍了在基于2.45 GHz微波“三明治”模块原型的光伏阵列,电力电子设备,微波转换电子设备和天线的设计,开发,集成和测试中获得的结果。制造原型并使其经受空间环境固有的挑战性条件,包括可能需要运行一系列模块的太阳能集中度。这项在真空中用于太阳能卫星的夹层模块的测试代表了第一个此类工作。该工作最终以两种新的夹心模块设计为“平铺”和“阶梯”式设计,每种设计的面积比重分别为21.9 kg / m2和36.5。 kg / m2的模拟太阳照度(至少0个太阳时为4.5 W / kg,最小2.2个太阳(AM0)时为5.8 W / kg)。在10-6托的真空条件下,模块的总的日光对微波效率的总和显示为8%和7%左右。这些代表了在环境或真空条件下最高的组合三明治模块效率报告,几乎是以前效率记录的四倍。创建了新颖的“阶梯”概念以解决热问题,并获得了专利公布。;模块表征的结果在上下文中进行了介绍,并与优点进行了比较,并制定并应用了实际阈值。提出的结果和讨论为评估太阳能卫星经济模型提供了经验基础,并指出了一些改进区域特定质量,特定质量功率以及未来原型的组合转换效率的机会。

著录项

  • 作者

    Jaffe, Paul Iven.;

  • 作者单位

    University of Maryland, College Park.;

  • 授予单位 University of Maryland, College Park.;
  • 学科 Engineering Electronics and Electrical.;Engineering Aerospace.;Alternative Energy.;Energy.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 144 p.
  • 总页数 144
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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