王克成, 马聪, 孙亮. 载人飞船仪表板的热仿真分析[J]. 真空与低温, 2016, 22(2): 90-94. DOI: 10.3969/j.issn.1006-7086.2016.02.006
引用本文: 王克成, 马聪, 孙亮. 载人飞船仪表板的热仿真分析[J]. 真空与低温, 2016, 22(2): 90-94. DOI: 10.3969/j.issn.1006-7086.2016.02.006
WANG Ke-cheng, MA Cong, SUN Liang. THERMAL ANALYSIS FOR A SPACEFLIGHT INSTRUMENT PANEL[J]. VACUUM AND CRYOGENICS, 2016, 22(2): 90-94. DOI: 10.3969/j.issn.1006-7086.2016.02.006
Citation: WANG Ke-cheng, MA Cong, SUN Liang. THERMAL ANALYSIS FOR A SPACEFLIGHT INSTRUMENT PANEL[J]. VACUUM AND CRYOGENICS, 2016, 22(2): 90-94. DOI: 10.3969/j.issn.1006-7086.2016.02.006

载人飞船仪表板的热仿真分析

THERMAL ANALYSIS FOR A SPACEFLIGHT INSTRUMENT PANEL

  • 摘要: 航天器产品热设计的对象是电子产品整机,将宇宙空间作为热沉,有效将热量排放到外空间是航天器热设计的主要任务。而对于舱内电子产品热设计任务主要是将元器件的热功耗有效传递给底板、设备外壳及舱壁上,确保元器件在允许的工作温度范围内可靠的工作。运用有限元分析软件FloTHERM,对航天电子产品设计阶段进行热仿真,对其热控方案进行调整和优化,实现电子元器件能够安全、可靠的工作。

     

    Abstract: Spacecraft is a complete machine of electronic products,astrospace is used as heat sink. Discharging heat out to external space effectively is the primary mission of spacecraft thermal design. But for electronic products inboard, the mission is mainly transmitting thermal power dissipation to baseplate,enclosure and bulkhead,make sure that components work reliably in the range of allowable working temperature. Apply finite element analysis software FloTHERM to conduct thermal analysis during spacecraft electronic products design period,adjust and optimize the thermal control scheme to make electronic components work safely and reliably.

     

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