赵丽滨 河北工业大学教授

赵丽滨，分别于1996年和2001年于北京航空航天大学获得学士学位和博士学位，现为河北工业大学机械工程学院院长，教授，博士生导师，国家级高层次人才。多年来主要先进复合材料结构失效和破坏理论研究开展工作，在先进复合材料结构设计与分析方面有丰富的工程实践经验。主持863课题4项，工信部民机专项2项，航空航天院所型号预研与攻关项目60余项。发表发表SCI论文70余篇，EI论文50余篇；获授权发明专利20余项、软件著作权10余项。出版专著一部，参编两部。被聘为中国力学学会理事、中国复合材料学会监事会秘书、北京力学会副秘书长、国际华人计算力学学会执行委员会委员、工程计算方法联络委员会委员等。

教育经历工作经历

1992.09-1996.07   北京航空航天大学，飞行器设计与应用力学系，本科

1996.09-1998.07   北京航空航天大学，飞行器设计与应用力学系，提前攻博博士

1998.09-2001.04   北京航空航天大学，飞行器设计与应用力学系，博士

2001.05-2003.09   清华大学工程力学系，博士后

2003.10-2004.07   北京航空航天大学宇航学院，讲师

2004.08-2009.07   北京航空航天大学宇航学院，副教授

2008.10-2009.09   英国南安普顿大学工程科学学院，访问学者

2009.08-2013.07   北京航空航天大学宇航学院，副教授、博导

2010.11-2011.11   中国商飞北京民用飞机技术研究中心，挂职锻炼

2013.08-2021.04   北京航空航天大学宇航学院，教授、博导、副主任

2021.04至今       河北工业大学机械工程学院，院长、教授、博导

2019.11-2019.12  法国图卢兹第三大学，访问教授

 

 

 

研究方向 

飞行器结构分析与优化设计、复合材料结构的破坏理论和力学设计、多场条件下多功能结构设计研究成果。 

近3年主持和参与的科研项目：

1.       国家自然科学基金面上项目“先进复合材料连接渐进失效机理及大型飞机典型连接结构强度预测理论研究”，项目编号：11372020，2014~2017，主持

2.       工业和信息化部民用飞机专项科研项目子课题“远程宽体客机复合材料重要结构设计和分析关键技术研究”，2014~2015，主持

3.       国家自然科学基金面上项目“纤维增强复合材料结构多尺度多模式损伤耦合扩展的渐进失效行为研究”，项目编号：11772028，2018~2021，主持

4.       国家自然科学基金面上项目“亚、超临界载荷下含缺陷/损伤复合材料加筋结构多重损伤演化机理研究”，项目编号：12072005，2021~2024，主持

5.       主持企业横向课题“多场耦合环境下后体结构设计及分析”，2016.10-2018.12，项目经费：158万元

6.       主持企业横向课题“重型整流罩开口影响分析及补强结构优化研究项目”，2019.08-2019.12，项目经费：45万元

       近3年授权专利与软著：

[1]    赵丽滨，路绪恒，张建宇，黄伟，刘丰睿. 一种间接测定复合材料多钉连接结构破坏历程中钉载分配比例的试验方法. 发明专利

[2]    张建宇，赵丽滨，王雅娜，龚愉，路绪恒. 一种归一化CFRP多向层合板疲劳分层扩展速率预测方法. 发明专利

[3]    赵丽滨，刘丰睿，房子昂，张建宇. 一种采用均匀钉载进行复合材料螺栓连接结构最终失效载荷预测的方法. 发明专利

[4]    赵丽滨，龚愉，肖鑫，张建宇. 一种改进B-K准则用于含纤维桥接影响复合材料多向层板分层预测的方法. 发明专利

[5]    赵丽滨，杨赟辉，山美娟，刘丰睿. 一种变相对密度octet点阵结构的设计方法. 发明专利

[6]    赵丽滨，贾若迪，王雅娜，王康康，龚愉. 一种复合材料I型分层桥联法则确定方法. 发明专利

[7]    赵丽滨，王雅娜，贾若迪，龚愉，王康康. 一种CFRP层板任意层间界面I型分层断裂韧度稳定值的预测方法. 发明专利

[8]    刘丰睿，姚婉婷，赵丽滨. 基于四折线刚度模型的复合材料螺栓连接钉载分配预测方法，

[9]    赵丽滨，杨文，曹天成，陈奎儒. 一种基于渐近损伤模型的全SiC复合材料多钉连接结构失效分析方法. 发明专利

        发表的学术论文：

[1]     Kangkang Wang, Libin Zhao*, Haiming Hong, Jianyu Zhang, Yu Gong. Parameter studies and evaluation principles of delamination damage in laminated composites, Chinese Journal of Aeronautics (2021),

[2]     Yu Gong*, Libin Zhao*, Jianyu Zhang*, Ning Hu, Chuanzeng Zhang. Development of a standardized test procedure and an improved data reduction method for the mixed-mode I/II delamination in composite laminates. Composites Science and Technology, 2021, 201: 108488.

[3]     Ruixue Ji, Libin Zhao, Kangkang Wang, Fengrui Liu, Yu Gong, Jianyu Zhang. Effects of debonding defects on the postbuckling and failure behaviors of composite stiffened panel under uniaxial compression. Composite Structures, 2021, 256：113121.

[4]     W.M. Mahdy, Libin Zhao, Fengrui Liu*, Rong Pian, Huiping Wang, Jianyu Zhang*. Buckling and stress-competitive failure analyses of composite laminated cylindrical shell under axial compression and torsional loads. Composite Structures, 2021, 255: 112977.

[5]     Fengrui Liu,Wanting Yao, Libin Zhao*, Hao Wu, Xi Zhang, Jianyu Zhang*. An improved 2D finite element model for bolt load distribution analysis of composite multi-bolt single-lap joints. Composite Structures, 2020, 253: 112700.

[6]     Yu Gong*, Libin Zhao*, Jianyu Zhang*, Ning Hu. Crack closure in the fatigue delamination of composite multidirectional DCB laminates with large-scale fiber bridging. Composite Structures, 2020, 244: 112220.

[7]     Meijuan Shan, Libin Zhao*, Fengrui Liu, Dexuan Qi, Jianyu Zhang*. Revealing the competitive fatigue failure behaviour of CFRP-aluminum two-bolt, double-lap joints. Composite Structures, 2020, 243: 112147.

[8]     Meijuan Shan, Libin Zhao*, Wei Huang, Fengrui Liu, Jianyu Zhang*. Effect Mechanisms of Hygrothermal Environments on Failure of Single-Lap and Double-Lap CFRP-Aluminum Bolted Joints. CMES-Computer Modeling in Engineering & Sciences, 2020, 123(1), 101–127.

[9]     Fengrui Liu, Wanting Yao, Xinhong Shi*, Libin Zhao and Jianyu Zhang*. Bearing failure optimization of composite double-lap bolted joints based on a three-step strategy marked by feasible region reduction and model decoupling. Computers, Materials & Continua, 2020, 62(2): 977–999.

[10] Yu Gong*, Xinjian Chen, Junan Tao, Libin Zhao*, Jianyu Zhang*, NingHu. A simple procedure for determining the mode I bridging stress of composite DCB laminates without measuring the crack opening displacement. Composite Structures, 2020, 244: 112166.

[11] Tiancheng Cao, Libin Zhao*, Yu Gong, Xiaojing Gong, Jianyu Zhang*. An enhanced beam theory based semi-analytical method to determine the DCB mode I bridging-traction law. Composite Structures, 2020, 245: 112306.

[12] Yu Gong*, Yixin Hou, Libin Zhao*, Wangchang Li, Jianyu Zhang*, NingHu. A modified mode I cohesive zone model for the delamination growth in DCB laminates with the effect of fiber bridging. International Journal of Mechanical Sciences, 2020, 276: 105514.

[13] Yu Gong*, Libin Zhao*, Jianyu Zhang*, Ning Hu, Chuanzeng Zhang. An insight into three approaches for determining fatigue delamination resistance in DCB tests on composite laminates Composites Part B, 2019, 176: 107206.

[14] Shihao Yin, Yu Gong*, Wangchang Li, Libin Zhao*, Jianyu Zhang*, Ning Hu. A novel four-linear cohesive law for the delamination simulation in composite DCB laminates. Composites Part B, 2020, 180: 107526.

[15] Yunhui Yang, Meijuan Shan, Libin Zhao*, Dexuan Qi, Jianyu Zhang*. Multiple strut-deformation patterns based analytical elastic modulus of sandwich BCC lattices. Materials and Design, 2019, 181: 107916.

[16] Kangkang Wang, Libin Zhao*, Haiming Hong, Jianyu Zhang*, Ning Hu. An extended analytical model for predicting the compressive failure behaviors of composite laminate with an arbitrary elliptical delamination. International Journal of Solids and Structures, 2020, 185-186; 439-447.

[17] Fengrui Liu, Ziang Fang, Libin Zhao*, Jianyu Zhang*, Ning Hu. A failure-envelope-based method for the probabilistic failure prediction of composite multi-bolt double-lap joints. Composites Part B, 2019, 172: 593-602.

[18] Libin Zhao, Ziang Fang, Fengrui Liu*, Meijuan Shan, Jianyu Zhang*. A modified stiffness method considering effects of hole tensile deformation on bolt load distribution in multi-bolt composite joints. Composites Part B, 2019, 171: 264-271.

[19] Kangkang Wang, Libin Zhao*, Haiming Hong, Yu Gong, Jianyu Zhang*, Ning Hu. An analytical model for evaluating the buckling, delamination propagation, and failure behaviors of delaminated composites under uniaxial compression. Composite Structures, 2019, 223: 110937.

[20] Yu Gong*, Bing Zhang, Libin Zhao*, Jianyu Zhang*, Ning Hu, Chuanzeng Zhang. R-curve behaviour of the mixed-mode I/II delamination in carbon/epoxy laminates with unidirectional and multidirectional interfaces. Composite Structures,2019,223:110949

[21] Libin Zhao, Kangkang Wang, Fan Ding, Tianliang Qin, Jifeng Xu, Fengrui Liu*, Jianyu Zhang*.A post-buckling compressive failure analysis framework for composite stiffened panels considering intra-, inter-laminar damage and stiffener debonding. Results in Physics,2019,13:102205.

[22] Tianliang Qin, Libin Zhao*, Jifeng Xu, Fengrui Liu, Jianyu Zhang. Model of CEL for 3D elements in PDMs of unidirectional composite  structures. Computer Modelling in Engineering & Sciences, 2019, 118: 157-176.

[23] Kangkang Wang, Fengrui Liu*, Haiming Hong. Shear failure mechanisms and influences of overlaminate configuration on the failure of composite π joints. Results in Physics, 2019, 12: 934-942.

[24] Yunhui Yang, Libin Zhao*, Dexuan Qi, Meijuan Shan, Jianyu Zhang*. A fuzzy optimization method for octet lattice structures. Rapid Prototyping Journal, 2019, Online.

[25] Meijuan Shan, Fengrui Liu*, Ziang Fang, Libin Zhao, Jianyu Zhang*. A bi-material property based FE modelling method for progressive damage analyses of composite double-lap bolted joints. Results in Physics, 2018, 11: 674-683.

[26] Yu Gong, Libin Zhao*, Jianyu Zhang*, Ning Hu. A novel model for determining the fatigue delamination resistance in composite laminates from a viewpoint of energy. Composites Science and Technology, 2018, 167: 489-496.

[27] Libin Zhao*, Wen Yang, Tiancheng Cao, Haibo Li, Baorui Liu, Chao Zhang, Jianyu Zhang*. A progressive failure analysis of all-C/SiC composite multi-bolt joints. Composite Structures, 2018, 202: 1059-1068.

[28] Libin Zhao*, Yaling Liu, Haiming Hong, Kangkang Wang, Jie Zhao. Compressive failure analysis for low length-width ratio composite laminates with embedded delamination. Composites Communications. 2018, 9l: 17-21.

[29] Fengrui Liu, Xuheng Lu, Libin Zhao*, Jianyu Zhang*, Jifeng Xu, Ning Hu. Investigation of bolt load redistribution and its effect on failure prediction in double-lap, multi-bolt composite joints. Composite Structures, 2018, 202: 397-405.

[30] Longwei Zhou, Libin Zhao, Fengrui Liu*, Jianyu Zhang*. A micromechanical model for longitudinal compressive failure in unidirectional fiber reinforced composite. Results in Physics, 2018, 10: 841-848.

[31] Kangkang Wang, Libin Zhao*, Haiming Hong, Jianyu Zhang*. A strain-rate-dependent damage model for evaluating the low velocity impact induced damage of composite laminates. Composite Structures, 2018, 201: 995-1003.

[32] Fengrui Liu, Meijuan Shan, Libin Zhao*, Jianyu Zhang*. Probabilistic bolt load distribution analysis of composite single-lap multi-bolt joints considering random bolt-hole clearances and tightening torques. Composite Structures, 2018, 194: 12-20.

[33] Meijuan Shan, Libin Zhao*, Haiming Hong, Fengrui Liu, Jianyu Zhang*. A progressive fatigue damage model for composite structures in hygrothermal environments. International Journal of Fatigue, 2018, 111: 299-307.

[34] Fengrui Liu, Xuheng Lu, Libin Zhao*, Jianyu Zhang*, Ning Hu, Jifeng Xu. An interpretation of the load distributions in highly torqued single-lap composite bolted joints with bolt-hole clearances. Composites Part B. 2018, 138: 194-205.

[35] Yu Gong, Libin Zhao*, Jianyu Zhang*, Ning Hu. An improved power law criterion for the delamination propagation with the effect of large-scale fiber bridging in composite multidirectional laminates. Composite Structures, 2018, 184: 961-968.

[36]  Libin Zhao*, Yang Li, Jianyu Zhang*, Longwei Zhou, Ning Hu. A novel material degradation model for unidirectional CFRP composites. Composites Part B. 2018, 135: 84-94.

[37]  山美娟，赵丽滨*．基于可靠性的 CFRP 螺栓连接优化设计方法研究[J]．北京航空航天大学学报. Online

[38]  张娇蕊，山美娟，黄伟，赵丽滨*. 湿热环境对CFRP-铝合金螺栓连接结构静力失效的影响[J]. 复合材料学报, 2020, 37(0): 1-10

[39]  山美娟，赵丽滨*. CFRP 螺栓连接失效载荷不确定性的评估方法[J]．复合材料学报. Online.

[40]  李重华，刘丰睿*，叶振信，赵丽滨. 考虑横截面形状和几何尺寸的弹簧优化的两步式策略. 西安交通大学学报. 2020,54(11),74-80

 

[41]  张武昆，闫伟，王会平，赵丽滨，刘丰睿*．不同环境下宽径比对T800/X850复合材料开孔层压板压缩失效的影响．复合材料学报. 2020,37(02),267-275

 

[42]  房子昂，赵丽滨*，刘丰睿，张建宇．碳纤维/树脂基复合材料多钉连接钉载系数测试方法. 复合材料学报. 2019,36(12),2795-2804

 

[43]  周龙伟，赵丽滨*. 基于失效机制的单向纤维增强树脂基复合材料退化模型. 复合材料学报. 2019,36(06),1389-1397

 

[44]  赵丽滨*，龚愉，张建宇. 纤维增强复合材料层合板分层扩展行为研究进展. 航空学报. 2019,40(1): 522509.

 

[45]  刘丰睿*，骈瑢，赵丽滨，张建宇. 一种考虑过滤的短纤维复合材料RVE建模方法. 北京航空航天大学学报. 2018, 45(2): 277-282.

 

 

 

联系邮箱： lbzhao@buaa.edu.cn