李运泽

教授

教授  博士生导师   硕士生导师 

电子邮箱:

所在单位:航空科学与工程学院

学历:博士研究生

办公地点:沙河校区

在职信息:在职

研究成果

一、代表性授权发明专利:

1)《双量程多通道核热源功率测量系统》,国家发明专利(201310109826.7),授权日期:2016.1,第一发明人;

2)《舱外航天服生保系统二轮能量回收系统》, 国家发明专利(201310066532.0),授权日期:2015.7,第一发明人;

3)《一种基于微重力环境的喷雾冷却回路装置》,国家发明专利(201110446869.5),授权日期:2014.4,第一发明人;

4)《适用于小卫星单相流体热控回路的流量-温度一体化测量装置》,国家发明专利(2010106173542),授权日期:2012.3,第一发明人;

5)《一种基于直接测温的平板型导热热流传感器》,国家发明专利(200910076772.2),授权日期:2010.1,第一发明人;

6)《多电飞行器的机载冷热电联产系统》,国家发明专利(200910085983.2),授权日期:2010.7,第一发明人;

7)《一种适用于纳卫星热控系统的流体回路控制装置》,国家发明专利 200910080237.4,授权日期:2010.8,第一发明人;

8)《飞机富裕液压能存储系统及方法》,国家发明专利(201810771400.0),授权日期:2020.11,第一发明人;

9)《一种利用氮气增压油箱的飞机富裕电力综合系统和方法》,国家发明专利(201811023569.4),授权日期:2020.07,第一发明人;

10)《基于闭式压缩空气循环的富裕发电能力利用系统》,国家发明专利(201811175018.X),授权日期:2020.11,第一发明人;

11)《一种基于飞机液压系统及微型蒸发式制冷循环的分布式热管理系统及方法》,国家发明专利(201811175029.8),授权日期2020.9,第一发明人;

12)《飞机热管理的油箱冷却子系统》,国家发明专利(201811651595.1),授权日期:2020.12.1,第一发明人;

13)《一种具有蓄冷能力的飞机燃油热管理系统及方法》,国家发明专利(201811651645.6),授权日期:2020.11,第一发明人;

14)《基于多孔材料蒸发冷却装置的低空应急主动式热控系统及方法》,国家发明专利(201910182159.2),授权日期:2020.08,第一发明人;

15)《一种用于空间站科学载荷柜的多柔性蒸发器环路热管控温系统及方法》,国家发明专利(201910224149.0),授权日期:2020.03,第一发明人;

16)《一种飞机周期性大功率密度热载荷的喷雾冷却系统》,国家发明专利(201811191797.2),授权日期:2020.12,第一发明人。


二、代表性国际期刊学术论文:

[1]  Ji-Xiang Wang, Yun-Ze Li*, Xi-Kui Yu, Guang-Chao Li, Xin-Yan Ji, “Investigation of heat transfer mechanism of low environmental pressure large-space spray cooling for near-space flight systems”, International Journal of Heat and Mass Transfer, Volume 119, April 2018, Pages 496-507. (SCI、通讯作者、指导教师)

[2]  Shengnan Wang, Yunhua Li, Yun-Ze Li*, Xing Peng, Yufeng Mao, “Exergy based parametric analysis of a cooling and power co-generation system for the life support system of extravehicular spacesuits”, Renewable Energy, Volume 115, January 2018, Pages 1209-1219. (SCI、通讯作者、指导教师

[3]  Ji-Xiang Wang, Yun-Ze Li*, Guang-Chao Li, Kai Xiong, Xianwen Ning, “Investigation of a gravity-immune chip-level spray cooling for thermal protection of laser-based wireless power transmission system”, International Journal of Heat and Mass Transfer, Volume 114, November 2017, Pages 715-726. (SCI、通讯作者、指导教师

[4]  Ji-Xiang Wang, Yun-Ze Li*, Zi-Jian Zhao, Yu-Feng Mao, Xin-Yan Ji, “Comparative Study of the Heating Surface Impact on Porous-material-involved Spray System for Electronic Cooling - an Experimental Approach”, Applied Thermal Engineering, Available online 16 February 2018. (SCI、通讯作者、指导教师

[5]  Shengnan Wang, Yunhua Li, Yun-Ze Li*, Yufeng Mao, Mingliang Zhong, “A forced gas cooling circle packaging with liquid cooling plate for the thermal management of Li-ion batteries under space environment”, Applied Thermal Engineering, Volume 123, August 2017, Pages 929-939.( SCI、指导教师)

[6] Wei Guo, Yunhua Li, Yun-Ze Li*, Ming-Liang Zhong, etal., “A self-driven temperature and flow rate co-adjustment mechanism based on Shape-Memory-Alloy (SMA) assembly for an adaptive thermal control coldplate module with on-orbit service characteristics”, Applied Thermal Engineering, 2017,3, 114(5), pp.744-755. (SCI、通讯作者、指导教师

[7] Wei Guo, Yunhua Li, Yun-Ze Li*, Sheng-Nan Wang, etal., “Construction and experimental verification of a novel flexible thermal control system configuration for the autonomous on-orbit services of space missions”,  Energy Conversion and Management, 2017.4, 138(15), pp.273-285. (SCI、通讯作者、指导教师

[8] Ming-Liang Zhong, Yun-Ze Li*, Wei Guo, Sheng-Nan Wang, etal., “Dynamic in-loop performance investigation and efficiency-cost analysis of dual heat sink thermal control system (DHS-TCS) with a sublimator for aerospace vehicles”, Applied Thermal Engineering, 2017.7 , 121(5), pp. 562-575. (SCI、通讯作者、指导教师

[9] Ming-Liang Zhong, Yun-Ze Li*, Yu-Feng Mao, Yi-Hao Liang, etal., “Coupled optic-thermodynamic analysis of a novel wireless power transfer system using concentrated sunlight for space applications”, Applied Thermal Engineering, 2017.3, 115(25), pp. 1079-1088. (SCI、通讯作者、指导教师

[10]  Shengnan Wang, Yunhua Li, Yun-Ze Li*, Jixiang Wang, etal., “Conception and experimental investigation of a hybrid temperature control method using phase change material for permanent magnet synchronous motors” , Experimental Thermal and Fluid Science, 2017.2, 81, pp.9-20. (SCI、通讯作者)

[11] Xin-Yan Ji; Yun-Ze Li*; Jing Wang; Xiao-Ning Yang; etal., “An integrated tailoring model for thermal cycling tests of spacecraft electronics”, IEEE Transactions on Aerospace and Electronic Systems, Year: 2016.12, 52(6), pp.2685 - 2696, . (SCI、通讯作者、指导教师

[12] Shengnan Wang, Yunhua Li, Yun-Ze Li*, Jixiang Wang, etal., “Transient cooling effect analyses for a permanent-magnet synchronous motor with phase-change-material packaging”, Applied Thermal Engineering, 2016.10, 109(25): pp.251-260. (SCI、通讯作者、指导教师

[13] Ji-Xiang Wang, Yun-Ze Li*, Sheng-Nan Wang , etal. “Experimental investigation of the thermal control effects of phase change material based packaging strategy for on-board permanent magnet synchronous motors”, Energy Conversion and Management, 2016.9, 123(1) , pp. 232-242. (SCI、通讯作者、指导教师

[14] WeiGuo, Yunhua Li, Yun-Ze Li*, etal. “An integrated hardware-in-the-loop verification approach for dual heat sink systems of aerospace single phase mechanically pumped fluid loop”, Applied Thermal Engineering, 2016.8, 106(5),pp. 1403-1414. (SCI、通讯作者)

[15] Ji-Xiang Wang, Yun-Z Li*,  Hong-Sheng Zhang, etal. “A highly self-adaptive cold plate for the single-phase mechanically pumped fluid loop for spacecraft thermal management”, ENERGY CONVERSION AND MANAGEMENT, 2016.3, 111(1), pp: 57-66 . (SCI、通讯作者、指导教师

[16] Yun-Ze Li*, Shun-Jie Zhu, Yunhua Li, Qi Lu, “Temperature Prediction and Thermal Boundary Simulation Using Hardware-in-Loop Method for Permanent Magnet Synchronous Motors”, IEEE/ASME Transactions on Mechatronics. 2016.1, 21(1), pp. 276 – 287. (SCI、通讯作者、指导教师

[17] Hong sheng Zhang, Yunze Li*, Shengnan Wang, etal.“ Ground experimental investigations into an ejected spray cooling system for space closed-loop application”, Chinese Journal of Aeronautics, 29(3), June 2016, pp. 630-638. (SCI、通讯作者、指导教师

[18] Wei Guo, Yunhua Li, Yun-Ze Li*, etal. “Thermal–structural analysis of large deployable space antennaunder extreme heat loads”, JOURNAL OF THERMAL STRESSES, 2016, 39, NO. 8, 887–905. (SCI、通讯作者、指导教师

[19] Ji-Xiang Wang, Yun-Z Li*,  Hong-Sheng Zhang, etal. “Investigation of a spray cooling system with two nozzles for space application”, APPLIED THERMAL ENGINEERING,    2015, 89, pp. 115-124. (SCI、通讯作者、指导教师

[20] Miao Li,Yunze Li*; Hongsheng Zhang, etal. “Study of amplification coefficient in a water-cooling Gardon-type heat power measuring apparatus”, CHINESE JOURNAL OF AERONAUTICS,  2015, 28 (2), pp.410-417. (SCI、通讯作者、指导教师

[21] Jin Wang,Yunze Li;* Jun Wang, “Transient performance and intelligent combination control of a novel spray cooling loop system”, CHINESE JOURNAL OF AERONAUTICS,   2013, 26   (5), pp. 1173-1181. (SCI、通讯作者、指导教师

[22] Su-Jun Dong, Yun-Ze Li*, Jin Wang,etal. “Fuzzy incremental control algorithm of loop heat pipe cooling system for spacecraft applications”, COMPUTERS & MATHEMATICS WITH APPLICATIONS, 2012, 64(5), pp.877. (SCI、通讯作者、指导教师

[23] Yunze Li*,Mingmin Li,KokMeng Lee,“A Dual-driven Intelligent Combination Control of Heat Pipe Space Cooling System”, CHINESE JOURNAL OF AERONAUTICS, 2012, 25 (4), pp. 566-574. (SCI、通讯作者)

[24] Yun-Ze Li*, “Thermodynamic analysis of polymer-electrolyte-membrane fuel-cell performance under varying cooling conditions”, INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2012, 37, pp. 10798-10806. (SCI、通讯作者)

[25]  Yun-Ze Li*, Kok-Meng Lee, “Thermohydraulic Dynamics and Fuzzy Coordination Control of a Microchannel Cooling Network for Space Electronics”, IEEE Transactions on Industrial Electronics, 2011, Vol.58, No.2, pp. 700-708. (SCI、通讯作者)

[26]  Yun-Ze Li*, Kok-Meng Lee, Jun Wang, “Analysis and Control of Equivalent Physical Simulator for Nanosatellite Space Radiator”, IEEE/ASME Transactions on Mechatronics, 2010, Vol. 15, No. 1, pp. 79 – 87. (SCI、通讯作者)

[27]  Yun-Ze Li*, Yu-Ying Wang, Kok-Meng Lee, “Dynamic Modeling and Transient Performance Analysis of a LHP-MEMS Thermal Management System for Spacecraft Electronics”, IEEE Transactions on Components and Packaging Technologies,2010, Vol.3, No. 3, pp. 597–606. (SCI、通讯作者、指导教师

[28]  Yun-Ze Li*, Ming-min Li,Kok-Meng Lee,“A Dual-driven Intelligent Combination Control of Heat Pipe Space Cooling System”,Chinese Journal of Aeronautics,2011, Vol. 25,No. 4,pp.566-574. (SCI、通讯作者)

[29]  Yun-Ze Li*, Chieh-Li Chen, “ Modeling and Analysis of Thermal -management Impacts on Transient Performances of PEM Fuel Cells”, Journal of the Chinese Society of Mechanical Engineers, Vol.32, No.1,13-25. (SCI、通讯作者)

[30]  Xin-Yan Ji, Yun-Ze Li*, Guo-Qing Liu, Jing Wang, “A brief review of ground and flight failures of Chinese spacecraft”,Progress in Aerospace Sciences, Vol.107, 2019, 19-29, (SCI、学生一作、指导教师

[31]  Weishu Wang, Man Yuan, Yun-Ze Li*, Chuang Li, “Numerical investigation on the impact of an on-top sunspace passive heating approach for typical rural buildings in northern China”, Solar Energy, Vol. 186, 2019, 300-310, (SCI、通讯作者、指导教师

[32]  Yu-Feng Mao, Yun-Ze Li*, Ji-Xiang Wang, Jing Wang, Lixiang Jiang, “Numerical investigation and experimental validation of an infrared measurement approach for surface heat flux distribution using a multi-color-reference” , International Journal of Heat and Mass Transfer, Vol. 131, 2019, 675-690, (SCI、通讯作者、指导教师

[33] Ji-Xiang Wang, Yun-Ze Li*, Jia-Xin Li, Chao Li, Xian-Wen Ning, “A gas-atomized spray cooling system integrated with an ejector loop: Ejector modeling and thermal performance analysis”, Energy Conversion and Management, Vol. 180, 2019, 106-118, (SCI、通讯作者、指导教师

[34] Weishu Wang, Chuang Li, Yun-Ze Li*, Man Yuan, “A novel on-top inverse sunspace conception and the passive heating effects on a typical northern China rural house”, Indoor and Built Environment, vol. 28, 2019, 1406-1421., (SCI、通讯作者).


三、代表性国内期刊学术论文

[1] 李运泽,宁献文,王晓明,石晓波,庄达民,王浚.  纳卫星轨道热环境仿真分析[J]. 系统仿真学报,2007,19(14):3166-3175,(EI) 

[2] 李运泽,宁献文,王晓明,石晓波,庄达民.  纳卫星散热面与隔热层的联合设计模型与算法[J]. 北京航空航天大学学报,2007,33(4):681-686,(EI) 

[3] 李运泽,宁献文,王晓明,石晓波,王浚等.  应用EHD热管的微小卫星主动热控建模与仿真[J]. 系统仿真学报.2007,19(3):681-686,(EI) 

[4] 李运泽,王浚. 卫星热平衡试验的温度预测与仿真模型 [J].北京航空航天大学学报2003.9:882-885,(EI)

[5] 李运泽,魏传锋,袁领双,王浚. 应用热电制冷器的微型航天器主动温度控制及仿真[J].机械工程学报,2005.10:149-151,(EI)

[6] 李运泽,魏传锋,袁领双,王浚. 应用PTC加热器的卫星局部温度控制及仿真[J].系统仿真学报,2006.6:1494-1496,(EI)

[7] 李运泽,魏传锋,袁领双,王浚. 卫星热热控系统的动态特性建模与仿真 [J].北京航空航天大学学报,2005.3:372-374,(EI)

[8] 李运泽,马志宏,袁领双,王浚. 直升机砂尘环境风洞的温度控制及仿真[J].航空学报,2005.2:135-138,(EI)

[9] 李运泽,马志宏,袁领双,王浚. 直升机砂尘环境试验风洞的浓度控制策略及仿真[J].系统仿真学报,2005.5:1241-1243,(EI).

[10] 李运泽,杨献勇. 超临界直流锅炉长期动态特性的建模与仿真[J].热能动力工程,2003.1:23-26,(EI).

[11] 李运泽,杨献勇.  汽轮机的长期动态模型与仿真[J]. 清华大学学报,2003.3:281-284, (EI).

[12] 李运泽,杨献勇.  大型锅炉长期动态特性研究中的烟气计算模型[J].热能动力工程,2003.3:170-172.

[13] 李运泽,杨献勇,张勇.罗锐.  超临界及亚临界压力下直流锅炉蒸发过程的模型与仿真[J],清华大学学报,2002,41(8):1117-1120, (EI). 

[14] 李运泽,杨献勇,严俊杰,邓世敏,林万超.  二次再热超临界机组热力系统的三系数线性分析法[J].中国电机工程学报,2002,22(6):132-136, (EI).

[15] 李运泽,杨献勇,罗锐.  二次再热超临界机组热力系统的全方位线性分析法[J].热能动力工程,2002,17(3):258-260, (EI). 

[16] 李运泽,严俊杰,林万超,邓世敏.  压水堆核电机组二回路的反平衡线性单元分析法[J]热能动力工程,2001,16(6):646-649.

[17] 李运泽,严俊杰,林万超,邓世敏.  压水堆核电机组二回路的矩阵分析法[J]. 热力发电,2000,29(5):26-28. 

[18] 李运泽,严俊杰,林万超,邓世敏.  压水堆核电机组二回路的等效热降理论[J].汽轮机技术,2000,42(1):31-35, (EI). 

[19] 李运泽,严俊杰,林万超,邓世敏. 压水堆核电机组二回路的线性单元分析法[J]. 热能动力工程,2000,15(5):544-547.

[20] 毛羽丰、 李运泽、; 王霁翔, 闪沸工况下过热度对水喷雾雾化效果的影响,航空学报,2018,39(S1):722184-1-7,EI,(指导教师).

[21] 王胜男、李运泽、周航、周国栋,舱外航天服生命保障冷电联储系统性能分析,航空学报,2013,34(6):1285-1292,EI,(指导教师).

[22] 刘东晓、李运泽、李淼、李明敏、李运华,微小航天器单相流体回路自主热控地面实验研究,宇航学报,2012,33(3):393-398,EI,(指导教师).

[23] 王瑾、李运泽、宁献文、王浚,感温蜡温控阀对航天器热控系统动态性能的影响,宇航学报,2013,34(5):734-740,EI,(指导教师).

[24] 周航、李运泽、王胜男、周国栋,基于冷热电一体化的舱外航天服生命保障系统性能,航空动力学报,2014,29(3):541-548,EI,(指导教师).

[25] 陈俊光、李运华、李运泽、张红生、钟铭亮,货运飞船智能温湿度测量系统构建和实验,航空动力学报,2015, 30(11):2746-2752,EI,(指导教师)

[26] 钟铭亮、李运泽、刘佳、田少平、张红生,斯特林式空间无线能量传输系统设计与仿真,太阳能学报, 2017,38(1):140-145,EI,(指导教师). 

[27] 毛羽丰、李运泽、王晶、姜利祥、魏传峰,基于红外热成像的热流分布测量技术,红外与激光工程, 2016,45(8):1-8,(指导教师).

[28] 李淼、李运泽、朱舜杰、张红生、李运华,核热源功率测量系统冷端温度控制策略,航空动力学报,2017,32(1):203-212, EI,(指导教师).

[29] 田少平、李运泽、刘佳、钟铭亮、张红生,高强太阳光无线能量传输能量供给平台设计,航空动力学报,2016,31(10):2472-2478, EI,(指导教师).