基本信息
安柏涛 男 硕导 中国科学院工程热物理研究所
email: anbt@mail.etp.ac.cn
address: 北四环西路11号
postalCode: 100190
email: anbt@mail.etp.ac.cn
address: 北四环西路11号
postalCode: 100190
招生信息
招生专业
080701-工程热物理080703-动力机械及工程
招生方向
燃气透平传热与冷却
教育背景
2002-12--2004-12 中国科学院工程热物理研究所 博士后1998-09--2002-10 哈尔滨工业大学 博士学位1996-09--1998-07 哈尔滨工业大学 硕士学位1988-09--1992-07 哈尔滨工业大学 学士学位
工作经历
工作简历
2005-01~现在, 中国科学院工程热物理研究所, 副研究员2002-12~2004-12,中国科学院工程热物理研究所, 博士后1998-09~2002-10,哈尔滨工业大学, 博士学位1996-09~1998-07,哈尔滨工业大学, 硕士学位1992-08~1996-09,哈尔滨汽轮机有限责任公司, 技术员1988-09~1992-07,哈尔滨工业大学, 学士学位
专利与奖励
专利成果
( 1 ) 一种冷却结构, 2023, 第 1 作者, 专利号: CN114198154B( 2 ) 一种冷却结构, 2023, 第 1 作者, 专利号: CN114198155B( 3 ) 一种涡轮叶片强化扰流柱冷却结构, 2023, 第 2 作者, 专利号: CN115585022A( 4 ) 透平叶片前缘气膜冷却结构, 2022, 第 1 作者, 专利号: 2022091300337470( 5 ) 透平叶片前缘气膜冷却结构, 2022, 第 1 作者, 专利号: CN115045720A( 6 ) 一种冷却结构, 2022, 第 1 作者, 专利号: CN114198154A( 7 ) 一种冷却结构, 2022, 第 1 作者, 专利号: CN114198155A( 8 ) 一种涡轮叶片及用于涡轮叶片内冷通道的V型凹陷肋结构, 2020, 第 3 作者, 专利号: CN211715180U( 9 ) 陶瓷-金属相结合的透平导向叶片及其燃气轮机, 2020, 第 2 作者, 专利号: CN211058869U( 10 ) 一种透平叶片尾缘冷却结构, 2020, 第 2 作者, 专利号: CN111412020A( 11 ) 具有槽形截面气膜孔排的带肋横流通道, 2020, 第 1 作者, 专利号: CN111120009A( 12 ) 一种横向扩张子午收缩槽形气膜孔, 2020, 第 1 作者, 专利号: CN111042872A( 13 ) 一种用于涡轮叶片内冷通道的V型凹陷肋结构, 2020, 第 3 作者, 专利号: CN111005769A( 14 ) 一种离散气膜冷却孔结构, 2018, 第 1 作者, 专利号: CN106437866B( 15 ) 一种透平叶片冷却结构, 2018, 第 2 作者, 专利号: CN207879399U( 16 ) 一种双层壁冷却与气膜冷却组合式透平叶片结构, 2018, 第 2 作者, 专利号: CN108425705A( 17 ) 一种离散气膜冷却孔结构, 2017, 第 1 作者, 专利号: CN106437866A( 18 ) 一种离散气膜冷却孔, 2015, 第 1 作者, 专利号: CN104747242A( 19 ) 一种离散气膜冷却孔型, 2013, 第 1 作者, 专利号: CN103244196A( 20 ) 一种考虑进口热斑的燃气透平导向器, 2013, 第 1 作者, 专利号: CN103061826A( 21 ) 一种提高离散孔气膜冷却效率的结构, 2011, 第 1 作者, 专利号: CN102140964A( 22 ) 强化换热装置, 2008, 第 3 作者, 专利号: CN201093913Y
出版信息
发表论文
(1) Film-Cooling effectiveness of combined hole slot geometries on a turbine rotor blade surface, Applied Thermal Engineering, 2024, (2) Film Cooling Effectiveness on Pressure Surface and Suction Surface of Turbine Guide Vane with Diffusion Slot Holes, JOURNAL OF TURBOMACHINERY, 2023, 第 2 作者 通讯作者(3) Experimental Investigation on Overall Effectiveness of Flat Plate Combined Impingement Cooling with Film-Cooling of Diffusion Slot Holes, ASME Turbo Expo, 2023, 第 1 作者 通讯作者(4) Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 第 2 作者(5) Experimental Investigation of Film Cooling Performance on Blade Endwall With Diffusion Slot Holes and Stator-Rotor Purge Flow, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 第 4 作者(6) 垂直横流通道内槽型截面孔气膜冷却特性数值研究, Numerical Investigation on Film Cooling Characteristics of Slot-Sectional Holes in Perpendicular Cross-Flow Channels, 推进技术, 2020, 第 3 作者(7) Numerical investigation on film cooling characteristics of slot-sectional diffusion holes combined with an internal cross-flow channel, APPLIED THERMAL ENGINEERING, 2020, 第 2 作者 通讯作者(8) Experimental investigation of film cooling effectiveness on a gas turbine blade pressure surface with diffusion slot holes, APPLIED THERMAL ENGINEERING, 2020, 第 3 作者 通讯作者(9) NUMERICAL INVESTIGATION OF THE EFFECT OF INLET FLOW ANGLE ON FILM COOLING PERFORMANCE FOR THE BLADE TIP WITH SUCTION SURFACE SQUEALER RIM, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5A, 2019, 第 4 作者(10) The investigations of slot film outflow used on the laminated cooling configuration, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 第 3 作者(11) Effects of Mainstream Turbulence Intensity and Coolant-to-Mainstream Density Ratio on Film Cooling Effectiveness of Multirow Diffusion Slot Holes, JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2019, 第 1 作者 通讯作者(12) Numerical investigation of the film cooling effectiveness on the suction surface squealer tip with different film-hole arrangements, ACGT, 2018, 第 1 作者(13) Numerical Investigation on Film Cooling Performance of Fusiform Diffusion Holes, JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 第 1 作者 通讯作者(14) Effects of Inclination Angle, Orientation Angle, and Hole Length on Film Cooling Effectiveness of Rectangular Diffusion Holes, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 第 1 作者 通讯作者(15) 燃气轮机透平叶片流-热-固耦合分析及蠕变寿命预测, Fluid-thermal-mechanical Coupling Analysis and Creep Life Prediction of Gas Turbine Blade, 燃气轮机技术, 2018, 第 4 作者(16) Performance of differential synthetic aperture ladar versus phase-gradient autofocus at large phase errors and low return levels, OPTICAL ENGINEERING, 2018, (17) Numerical Investigation on Diffusion Slot Hole With Various Cross-Sectional End Shapes, JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2017, 第 1 作者 通讯作者(18) A TWO-DIMENSIONAL ANALYTICAL METHOD FOR TURBINE BLADE COOLING DESIGN, PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2B, 2017, 第 3 作者(19) Geometrical Parameter Effects on Film-Cooling Effectiveness of Rectangular Diffusion Holes, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2017, 第 1 作者 通讯作者(20) Experimental demonstration of tri-aperture Differential Synthetic Aperture Ladar, OPTICS COMMUNICATIONS, 2017, (21) Investigation on Cooling Effectiveness and Aerodynamic Loss of a Turbine Cascade with Film cooling, JOURNAL OF THERMAL SCIENCE, 2016, 第 4 作者(22) The influences of element layout and coolant ejection angle on overall cooling effectiveness of laminated cooling configuration, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2016, 第 3 作者(23) Film cooling effectiveness measurements of a near surface streamwise diffusion hole, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2016, 第 1 作者 通讯作者(24) Calculation of Film-Cooling Effectiveness and Aerodynamic Losses Using DES/SAS and RANS Methods and Compared With Experimental Results, 2016, (25) 平板气膜冷却气动损失影响实验研究, 2015年中国工程热物理学会气动学学术年会, 2015, 第 3 作者(26) 主流马赫数对不同气膜孔结构冷却效果及气动损失影响研究, Influence of Mainstream Mach Number on Cooling Effectiveness and Aerodynamic Losses of Different Film Cooling Configurations, 燃气轮机技术, 2015, 第 3 作者(27) Thermo-Elastc Analysis on the Flat-Plate Film-Cooling, ASME, 2014, 第 2 作者(28) 吹风比对不同气膜孔结构冷却效率及损失影响研究, 2014年工程热物理学会, 2014, 第 2 作者(29) Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes, JOURNAL OF THERMAL SCIENCE, 2013, 第 4 作者(30) Film Cooling of Cylindrical Hole With a Downstream Short Crescent-Shaped Block, JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2013, 第 1 作者 通讯作者(31) Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes, Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes, 热科学学报:英文版, 2013, (32) 三流程蛇形冷却通道导流优化设计研究, 中国工程热物理学会, 2012, 第 3 作者(33) 气冷涡轮叶片传统热分析中热边界条件的影响, Influence of Thermal Boundary Conditions in Conventional Heat Transfer Analysis of an Air-Cooled Turbine Vane, 工程热物理学报, 2012, 第 4 作者(34) 多级轴流透平气动特性计算方法研究, Investigation on the Computational Method of Axial Turbine Aerodynamic Characteristics Based on 1.5 Dimensional Euler Equations, 工程热物理学报, 2011, 第 3 作者(35) 复合角双射流气膜冷却的研究, Study of the Air-film Cooling of a Dual-jet-flow with a Composite Angle, 热能动力工程, 2011, 第 3 作者(36) Effects of Axial Row-Spacing for Double-Jet Film-Cooling on the Cooling Efectiveness, ASME, 2011, 第 3 作者(37) 基于单色捕捉技术的透平导叶传热系数测量, Heat Transfer Coefficients Measurement of Turbine Guide Vane Based on Single-Color Capture Technology, 工程热物理学报, 2011, 第 3 作者(38) 基于1.5维欧拉方程的多级轴流透平气动特性计算方法研究, 中国工程热物理学会(热机气动热力学), 2010, 第 3 作者(39) Leading Edge Film Cooling Enhancement for an Inlet Guide Vane with Fan- Shaped Holes, Leading Edge Film Cooling Enhancement for an Inlet Guide Vane with Fan- Shaped Holes, JOURNAL OF THERMAL SCIENCE, 2010, 第 2 作者(40) 非均匀有理B样条曲线及节点插入算法在透平叶片优化设计中的应用, Application of non-uniform rational B-spline curve and knot insertion algorithm to turbine blade optimization, 航空动力学报, 2010, 第 3 作者(41) 基于窄带液晶单色捕捉技术的透平导叶全表面传热系数测量, 中国工程热物理学会(热机气动热力学), 2010, 第 3 作者(42) Numerical Investigation on Unsteady Effects of Hot Streak on Flow and Heat Transfer in a Turbine Stage, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 第 1 作者 通讯作者(43) 静叶前缘气膜冷却特性的数值模拟及改进设计, Numerical simulation and design improvement of leading-edge film cooling in an inlet guide vane, 航空动力学报, 2009, 第 2 作者(44) 交替大小肋片方腔通道内换热性能的数值模拟, Numerical simulation on heat transfer in duct roughened by periodic alternate scale ribs, 航空动力学报, 2008, 第 4 作者(45) 内部结构对空冷叶片换热性能的影响, The lnfluence of Inner Structures on the Heat Exchange Performance of Air-cooled Blades, 热能动力工程, 2008, 第 4 作者(46) 透平导叶闭式蒸汽冷却方案研究, INVESTIGATION ON COLSED-LOOP STEAM COOLING SCHEMES OF A GAS TURBINE GUIDE-VANE, 工程热物理学报, 2008, 第 4 作者(47) 复杂空冷叶片换热特性研究, Calculations of Heat Transfer in an Air-cooled Blade, 燃气涡轮试验与研究, 2008, 第 4 作者(48) Simulation of 3D flow in turbine blade rows including the effects of coolant ejection, JOURNAL OF THERMAL SCIENCE, 2008, 第 2 作者(49) Numerical Investigation of Fluid Flow and Heat Transfer in a Turbine Blade With Serpentine Passage and Latticework Cooling, PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B, 2008, (50) 非对称蛇形旋转通道换热及流场数值研究, CALCULATIONS OF HEAT TRANSFER AND FLUID FLOW IN AN UNSYMMETRICAL RIB-ROUGHENED BRANCH OF A ROTATING TWO-PASS DUCT, 工程热物理学报, 2007, 第 3 作者(51) 内冷涡轮叶栅三维气热耦合数值模拟, Numerical simulation of conjugate heat transfer for an internally cooled 3-D turbine blade, 航空动力学报, 2007, 第 3 作者(52) 空冷透平静叶气膜冷却数值研究, 工程热物理学报, 2005, 第 1 作者(53) 4级空气冷却透平气动性能三维数值研究, 3D Numerical Investigation on the Aerodynamic Performance of an Air Cooled 4 - Stage Turbine, 航空发动机, 2005, 第 1 作者(54) 前置导叶对两种涡轮导向器及涡系结构的影响, Effects of front guide blade on performance and vortices structure in two turbine low pressure guide vanes, 推进技术, 2004, 第 1 作者(55) 涡轮导向器几何与气动参数对通道涡影响的实验与数值研究, Experimental and Numerical Investigation on Effects of Turbine Guide Vane Geometric and Aerodynamic Parameters on Passage Vortex, 航空学报, 2004, 第 1 作者(56) 几何参数对涡轮低压导向器变工况性能的影响, Effects of Geometry Parameters on Incidence Characteristics of Turbine Low Pressure Guide Vane, 航空动力学报, 2004, 第 1 作者(57) 涡轮低压导向器优化前后气动性能对比实验研究, Comparison of Turbine Low Pressure Guide Vane before and After Optimization, 航空动力学报, 2004, 第 4 作者(58) 流道几何参数对低压导向器气动性能的影响, The Impact of Flow-passage Geometric Parameters on the Aerodynamic Performance of a Low-pressure Guide Vane Assembly, 热能动力工程, 2003, 第 1 作者
科研活动
参与会议
(1)Numerical Investigation of the Effect of Inlet Flow Angle on Film Cooling Performance for the Blade Tip with Suction Surface Squealer Rim 2019-06-08(2)Numerical investigation of the film cooling effectiveness on the suction squealer tip with different film-hole arrangements 2018-10-18(3)Numerical investigation of the film cooling effectiveness on the suction squealer tip with different film-hole arrangements 2018-10-18(4)A TWO-DIMENSIONAL ANALYTICAL METHOD FOR TURBINE BLADE COOLING DESIGN 2017-06-13(5)Numerical Investigation on Unsteady Effects of Hot Streak on Flow and Heat Transfer in a Turbine Stage An Bai-Tao, Liu Jian-Jun, Jiang Hong-De 2008-06-09(6)Three-Dimensional Flow Analysis and Design Improvement of Leading-Edge Film-Cooling in An Inlet Guide Vane An Bai-Tao, Liu Jian-Jun, Jiang Hong-De 2006-05-08