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相关技术

星载多功能热控制研究

  • 汪衡 ,
  • 田晓丽 ,
  • 杨慧 ,
  • 彭书丽
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  • 中北大学机电工程学院,太原 030051

汪衡(1983-),男,重庆垫江人,硕士研究生,研究方向:制导弹药。

收稿日期: 2009-06-08

  网络出版日期: 2025-05-28

Research on Space-borne Multi-function Thermal Control

  • WANG Heng ,
  • TIAN Xiaoli ,
  • YANG Hui ,
  • PENG Shuli
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  • School of Mechatronics Engineering, North University of China, Taiyuan 030051, China

Received date: 2009-06-08

  Online published: 2025-05-28

摘要

为保证多功能结构内部电子元器件和设备的热可靠性,以及对温度变化的适应能力,利用ANSYS软件中的热分析模块对弹载多功能结构样机——远置单元,进行热传导分析和热应力分析,验证其结构设计的合理性,从而为电子设备的热设计从理论上提供设计依据。通过对样机在上电情况下进行温度循环实验和温度老炼试验,可知样机工作稳定,结构设计合理。

本文引用格式

汪衡 , 田晓丽 , 杨慧 , 彭书丽 . 星载多功能热控制研究[J]. 弹箭与制导学报, 2010 , 30(3) : 243 -246 . DOI: 10.15892/j.cnki.djzdxb.2010.03.010

Abstract

In order to ensure thermal reliability and adaptability to temperature change of the internal electronic components and equipment with multi functional structure, the thermal analysis module was used in ANSYS software to make the analysis of heat conduction and thermal stress analysis for RTU of prototype with multi functional structure used on cartridge, and the rationality of the structure design was verified, which laying the design foundation for thermal design of electronic equipment in theory. Through research on prototypes about circulation experiment in power and the temperature burn in test, it is known that the prototype works steadily and the structural design is reasonable.

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参考文献

[1]
张立华. 有限元法在空间飞行器天线反射器热分析中的应用[J]. 中国空间科学技术, 1999, (2): 32- 37.
[2]
杨邦朝, 张经国. 多芯片组件(MCM)技术及其应用[M]. 成都: 电子科技大学出版社, 2001. 56- 62.
[3]
黄之华, 武宇, 颜肖龙. 多功能结构的热分析[J]. 中国制造业信息化, 2008, 37 (19): 31- 33.
[4]
张朝晖. ANSYS 热分析教程与实例解析[M]. 北京: 中国铁道出版社, 2007.
[5]
Bill Jackson, Kenny Epstein. A reconfigurable multi- functional architecture approach for next-generation nano satellite design[C]// IEEE Aerospace Conference Pro- ceedings, 2000: 185- 193.
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