Lin Shifeng
Principal Investigator
Email: linshifeng@@gdiist.cn
Personal Profile
Lin Shifeng, computer thermal engineering research group. Graduated from Harbin Institute of Technology in 2010，majoring in engineering thermophysics. He has been engaged in the design and verification of spacecraft thermal control systems over 10 years, and has participated in the development of thermal control systems for a number of national key aerospace models. He has been honored with China Academy of Sciences (CAS) Outstanding Achievement Award in Science and Technology, and has received several provincial awards including advanced individual in the construction of the Beidou-3 global satellite navigation system. In addition, published 5 related articles and authorized 4 invention patents.
Laboratory of Computer Thermal Engineering
The group focus on the research and development of more advanced and efficient heat dissipation technology. With the support of the national strategic layout and relevant policies, the demand for high-performance computing capabilities in cloud computing, artificial intelligence, block chain and other fields is increasing, the functional density of the server rack and the power density of the chip are constantly improving, and the demand for efficient heat dissipation technology is urgent, our works focus on the diffusion heat of ultra-high power devices and efficient thermal management technology of intelligent computing platform to carry out systematic research, achieve fine thermal management of computing platform, and help the national "carbon peak, carbon neutral" green sustainable development strategy.
Representative publications
1. Lin S., etal. A Method of Temperature Control for Atomic Clock Cabin on Navigation Satellite and Validated l. [J]. Chinese Journal Of Space Science, 2019, 39(3): 381-384.
2. Lin S., etal. Thermal Control Design and Validated for MEO Navigation Satellites. [J]. Chinese Journal Of Space Science, 2022, 42(1): 144-152.
3. Xu H., Lin S.*, etal. Technologies for parallel vacuum thermal test of twin MEO satellites. [J].SPACECRAFT ENVIRONMENT ENGINEERING. 2021.04 ‘Vol. 38, No. 2.
4. Zhang X., Lin S.*, etal. Automatic opt imization design of infrared lamp array based on enhanced particle swarm algorithm.[J].SPACECRAFT ENVIRONMENT ENGINEERING. 2022, 39(5): 501-508.
5. Zhang L., Lin S.*, etal. Two-stage thermal control design of an extravehi-cular load based on TEC. [J]. SPACECRAFT ENVIRONMENT ENGINEERING. 2023, 40(4): 380-386.
Representative patents
1. Lin S., Wu H., Zhu R., A Precise Temperature Control Device and Method, 2023115105791，CN117369551A.
2. Lin S., Wu H., A Continuously Adjustable Gravity Environment Simulation Method and Device, 2023115023607，CN117326106A.
3. Lin S., etal. Thermal Control System of MEO Navigation Satellite, 2020109101677，CN112034873A.
4. Lin S., etal. Temperature Control System and Control Method, 2020108619829，CN111854491A.
5. Lin S., etal. Vacuum Thermal Test Method for Mass Production Satellite Constellation System, 2019105313630，CN110171584A.
6. Lin S., etal. Temperature Stability Control Device for Spacecraft and Control Method Thereof, 2018102232656, CN108490775A.
