轻小型、紧凑型机载光电吊舱散热技术

Thermal Management Technology of Light, Small, and Compact Airborne Photo-Electric Pod

  • 摘要: 为满足机载光电吊舱轻小型、紧凑型要求,解决光电吊舱散热问题,采用了热传导和风机内循环对流结合的散热方式,用金属结构件将发热元器件与壳体接触建立热传导通道,用风机内循环强化内部对流建立低热阻的对流换热通道,通过ICEPAK热仿真软件对该散热方式建模仿真计算表明:静止条件下吊舱核心处理芯片DSP、FPGA、SoC温升分别为:29.1℃、29.2℃、33.8℃,相比无风机时别降低:5.2℃、3.5℃、4.4℃;飞行条件下温升分别为:11.9℃、9.1℃、15.5℃;静止条件下,在风机内循环作用下,舱内最高环境温度较无风机内循环时降低约5.5℃。通过与同等条件下高温试验数据比较,仿真温度与测试温度相差3.1℃。该散热方式可有效降低舱内环境和器件的温升,满足吊舱使用要求,结构简单占用空间小,适用于轻小型、紧凑型机载光电吊舱。

     

    Abstract: To meet the development trend of light, small, and compact airborne photoelectric pods and solve the heat dissipation problem of photoelectric pods, a combination of cooling and fan circulation convection heat dissipation was used. The contact heat components with the cabin using a metal structure were employed to establish a heat conduction channel. The internal air was circulated by a fan to strengthen the internal convection and establish a low-thermal-resistance convection heat-transfer channel. Modeling simulation was performed by ICEPAK thermal simulation software, and a high-temperature working test was also conducted. The results show that the maximum temperature rise of the key processors DSP, FPGA, SoC is respectively 29.1℃, 29.2℃, 33.8℃ under static conditions and 5.2℃, 3.5℃, 4.4℃ lower than the case without fans. And the maximum temperature rise is respectively 11.9℃, 9.1℃, 15.5℃ under flight conditions. At the same time, under the action of internal air circulation by the fan, the maximum ambient temperature in the cabin was reduced by approximately 5.5℃. The maximum temperature deviation between test and simulation at the same conditions is 3.1℃. The thermal management method can effectively reduce the temperature increase in the internal environment and devices inside the cabin, satisfy the requirements of pod use with a simple structure, and occupy a small space. Thus, it is suitable for light, small, and compact airborne photo-electric pods.

     

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