| CPL技术在空间飞行器上的应用 |
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| 引用本文： | 张加迅,侯增祺.CPL技术在空间飞行器上的应用[J].工程热物理学报,2001,22(3):34-37. |
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| 作者姓名： | 张加迅 侯增祺 |
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| 作者单位： | 北京空间飞行器总体设计部, |
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| 基金项目： | 国家863航天领域重点基金资助项目（No．863－2－2－3－1） |
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| 摘 要： | 本文对ＣＰＬ技术进行了简要概述，介绍了其工作原理与工作特性，并讨论了ＣＰＬ技术在空间飞行器上的可能应用方式。其中，对ＣＰＬ技术应用于空间设备的散热进行了全面阐述，并给予理论分析；此外，对ＣＰＬ技术应用于空间设备的主动热控制，也作了简要介绍；对ＣＰＬ技术未来有发展前景的应用方式进行了展望。
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| 关 键 词： | 毛细抽吸 热控制 热管 |
| 文章编号： | 0253-231(2001)03-034-04 |
| 修稿时间： | 2001年2月8日 |
THE APPLICATION OF CPL TECHNIQUE IN SPACECRAFT |
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| ZHANG Jia-Xun HOU Zeng-Qi.THE APPLICATION OF CPL TECHNIQUE IN SPACECRAFT[J].Journal of Engineering Thermophysics,2001,22(3):34-37. |
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| Authors: | ZHANG Jia-Xun HOU Zeng-Qi |
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| Abstract: | The general concept of the CPL technique is introduced in the paper. The principle and characteristics of the CPL are also introduced in the paper, moreover, the possible applications in the spacecraft are discussed. The application of CPL in the heat transfer of the equipment in space is illustrated in full with the support of theoretical analysis; additionally, the application of CPL in active thermal control for equipment in space is also discussed summarily. Finally, the promising application of CPL is also depicted. |
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| Keywords: | capillary pumped loop thermal control heat pipe |
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