摘要
针对空间受限的大功率老练设备的散热问题,本文给出了一种散热系统的设计方法,包括散热系统的构成以及各部分的设计计算方法,并通过基于ICEPAK的热仿真技术进行分析和试验验证。结果表明,仿真分析的结论与试验的结果是一致的,从而证明该设计方法的有效性和可行性。
This paper presents an design method of cooling system that is proposed by taking into account the heat dissipation of the space constraints of high power equipment. The approach includes the choice of cooling technology and the calculation of thermal performance. Meanwhile, a simulation model of cooling system is constructed by ICEPAK which is based on the theoretical calculation results and a high-power aging equipment is produced to verify the method. Finally, the experiment results and the simulation results are consistent. This means that the design method of cooling system is effective and practical.
出处
《航天制造技术》
2014年第4期64-66,共3页
Aerospace Manufacturing Technology
关键词
散热系统
热计算
热仿真
cooling system
thermal calculation
thermal simulation
