• Optical Communication Technology
  • Vol. 46, Issue 3, 67 (2022)
ZHANG Xin1, CHEN Fang1, WANG Shixin2, GUO Jian2..., HE Zongwei1 and LU Chenghong1|Show fewer author(s)
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.13921/j.cnki.issn1002-5561.2022.03.014 Cite this Article
    ZHANG Xin, CHEN Fang, WANG Shixin, GUO Jian, HE Zongwei, LU Chenghong. Thermal design of laser source for aerospace[J]. Optical Communication Technology, 2022, 46(3): 67 Copy Citation Text show less

    Abstract

    In order to meet the requirements of passive heat dissipation of laser source in aerospace applications, project of heat dissipation solution of high power devices in laser source is proposed. The heat conduction channel from device and printed circuit board to metal structure is designed, which can transfer heat from devices to metal structure efficiently, ensure that the device temperature is within the normal operating range. Efficiency of heat dissipation can be promoted by ways of evolving structure and material of laser soucrce, and by ways of adding or evolving dissipation passages. Simulation results show that, when working in high temperature circumstance, In the heat dissipation optimized scheme, the maximum temperature of chip and laser is reduced by about 100 ℃ and 1 ℃ respectively, the optimized project is effective and viable.