基本信息
浦健  男    中国科学院工程热物理研究所
电子邮件: pujian@iet.cn
通信地址: 北京市海淀区北四环西路11号
邮政编码:

研究领域

1. 航空发动机/燃气轮机热端部件换热特性与高效冷却技术研发;

2. 涡轮气热环境下先进主动冷却技术与表面热障涂层耦合设计;

3. 叶轮机械气动热力学、气热性能优化与二次空气系统设计;

4. 流-热-固特性先进测量技术与耦合传热数值计算策略;

5. 空天飞行器陶瓷基复合材料热/力性能。


招生信息

叶轮机械气动热力学;工程热物理;CFD,试验技术,包括但不限于红外热像仪、PSP、PIV、TRPIV、PLIF

招生专业
082502-航空宇航推进理论与工程
招生方向
涡轮传热与冷却

教育背景

2009-09--2014-11   中国科学技术大学   工学博士
2005-09--2009-07   南京师范大学   工学学士

工作经历

   
工作简历
2022-09~现在, 中国科学院工程热物理研究所, 副研究员
2016-12~2022-09,中国科学技术大学, 特任副研究员
2014-12~2016-11,中国科学技术大学, 博士后研究员
社会兼职
2022-03-01-今,第五届中国国际 透平会议评审组织者,

专利与奖励

   
奖励信息
(1) 中国科学院青年创新促进会会员, 院级, 2023

出版信息

   
发表论文
(1) Overall Thermal Performances of Double-Wall Effusion Cooling Covered by Simulated Thermal Barrier Coatings, Overall Thermal Performances of Double-Wall Effusion Cooling Covered by Simulated Thermal Barrier Coatings, JOURNAL OF THERMAL SCIENCE, 2022, 第 1 作者
(2) Experimental investigation of hole-geometry effect on unsteady characteristics of film cooling at turbine vane leading edge, INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2022, 通讯作者
(3) Effects of mainstream cross-flow and wall contouring on film cooling effectiveness of cylindrical-holes embedded in elliptical craters, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2022, 通讯作者
(4) Experimental study of cooling air effect on overall cooling of laminated configuration at a turbine vane end-wall, CASE STUDIES IN THERMAL ENGINEERING, 2022, 通讯作者
(5) Overall thermal performances of backward film cooling with simulated surface thermal barrier coatings at various walls, CASE STUDIES IN THERMAL ENGINEERING, 2022, 通讯作者
(6) Visualization and quantitation of unsteadiness of film cooling near stagnation line of a double-wall cooled vane leading edge, JOURNAL OF VISUALIZATION, 2022, 第 1 作者
(7) Effect of length-to-diameter ratio on film cooling and heat transfer performances of simple and compound cylindrical-holes in transverse trenches with various depths, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2022, 通讯作者
(8) Experimental study of combined effects of wall curvature and compound angle on film cooling effectiveness of a fan-shaped film-hole, International Communications in Heat and Mass Transfer, 2022, 第 1 作者
(9) Experimental investigation of inclination angle effect on unsteady film coverage of double-row staggered-holes at vane leading edge using time-resolved quantitative light sheet technique, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 通讯作者
(10) Numerical Investigation of Effects of Blockage, Inclination Angle, and Hole-Size on Film Cooling Effectiveness at Concave Surface, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 通讯作者
(11) Experimental study of transverse trench effect on unsteady film cooling effectiveness of backward cylindrical-holes with various compound angles, INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2021, 通讯作者
(12) 横流下前向与反向复合角沟槽孔气膜冷却效率, Film Cooling Effectiveness of Forward and Backward Compound-Angled Trench-Holes Under Coolant Cross-Flow Effects, 工程热物理学报, 2021, 通讯作者
(13) Exit-shape effect of film holes at pressure side on trailing edge cutback film cooling characteristics, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2021, 第 1 作者
(14) Effect of transverse trench on film cooling performances of typical fan-shaped film-holes at concave and convex walls, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2021, 通讯作者
(15) POD analysis of passage-layout effect on unsteady internal flow in a realistic blade serpentine coolant channel with low aspect ratios, JOURNAL OF VISUALIZATION, 2020, 第 1 作者
(16) Sensitivity analysis of internal layout and coating thickness to overall cooling performances of laminated cooling configurations with surface thermal barrier coatings, APPLIED THERMAL ENGINEERING, 2020, 通讯作者
(17) 改善局部难冷区域的一种导叶层板端壁, Design of a Vane Laminated End-wall to Reduce Local Regions Difficult to Cool, 工程热物理学报, 2020, 通讯作者
(18) Experimental study of free-stream turbulence intensity effect on overall cooling performances and solid thermal deformations of vane laminated end-walls with various internal pin–fin configurations, APPLIED THERMAL ENGINEERING, 2020, 第 1 作者
(19) An experimental investigation on cooling characteristics of a vane laminated end-wall with axial-row layout of film-holes, APPLIED THERMAL ENGINEERING, 2019, 通讯作者
(20) Auxiliary hole influence on internal flow characteristics in bend region of a real investment-casting blade coolant channel, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 通讯作者
(21) 实验研究层板结构对端壁冷却的影响, An Experimental Investigation on Effect of Laminated Structure on Endwall Cooling, 工程热物理学报, 2019, 通讯作者
(22) 一种降低端壁温度的离散气膜孔布置, A Discrete Film-Hole Arrangement to Reduce Endwall Surface Temperature, 工程热物理学报, 2018, 通讯作者
(23) 温比对第一级导叶端壁气膜冷却特性的影响, Effect of temperature ratio on film cooling characteristics at first-stage vane endwall, 航空动力学报, 2018, 通讯作者
(24) An experimental investigation of cooling characteristics at a vane end-wall with a locally enhanced hole-layout, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2018, 通讯作者
(25) The Combined Effects of an Upstream Ramp and Swirling Coolant Flow on Film Cooling Characteristics, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2016, 通讯作者
(26) An experimental investigation of geometric effect of upstream converging slot-hole on end-wall film cooling and secondary vortex characteristics, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2015, 第 1 作者
(27) An experimental investigation of secondary flow characteristics in a linear turbine cascade with upstream converging slot-holes using TR-PIV, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2014, 第 1 作者
(28) An experimental investigation on fluid flow characteristics in a real coolant channel of LP turbine blade with PIV technique, EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2013, 第 1 作者

科研活动

   
科研项目
( 1 ) 薄壁涡轮叶片隔热/气冷一体化 设计中的流/固/热耦合机理研究, 负责人, 国家任务, 2023-01--2026-12
( 2 ) ****下双层壁发汗冷却叶片微 孔出流及与热障涂层耦合换热机理, 负责人, 国家任务, 2021-10--2023-10
( 3 ) 中国科学院青年创新促进会会员项目, 负责人, 中国科学院计划, 2023-01--2026-12
( 4 ) 涡轮叶栅环境下层板冷却与热障涂层耦合传热特性研究, 负责人, 地方任务, 2021-01--2023-12
( 5 ) 涡轮叶片先进冷却技术与热障涂层耦合特性, 负责人, 其他任务, 2020-09--2023-06