趙麗濱，分別于1996年和2001年于北京航空航天大學獲得學士學位和博士學位，現為河北工業大學機械工程學院院長，教授，博士生導師，國家級高層次人才。多年來主要先進復合材料結構失效和破壞理論研究開展工作，在先進復合材料結構設計與分析方面有豐富的工程實踐經驗。主持863課題4項，工信部民機專項2項，航空航天院所型號預研與攻關項目60余項。發表發表SCI論文70余篇，EI論文50余篇；獲授權發明專利20余項、軟件著作權10余項。出版專著一部，參編兩部。被聘為中國力學學會理事、中國復合材料學會監事會秘書、北京力學會副秘書長、國際華人計算力學學會執行委員會委員、工程計算方法聯絡委員會委員等。

教育經歷工作經歷

1992.09-1996.07   北京航空航天大學，飛行器設計與應用力學系，本科

1996.09-1998.07   北京航空航天大學，飛行器設計與應用力學系，提前攻博博士

1998.09-2001.04   北京航空航天大學，飛行器設計與應用力學系，博士

2001.05-2003.09   清華大學工程力學系，博士后

2003.10-2004.07   北京航空航天大學宇航學院，講師

2004.08-2009.07   北京航空航天大學宇航學院，副教授

2008.10-2009.09   英國南安普頓大學工程科學學院，訪問學者

2009.08-2013.07   北京航空航天大學宇航學院，副教授、博導

2010.11-2011.11   中國商飛北京民用飛機技術研究中心，掛職鍛煉

2013.08-2021.04   北京航空航天大學宇航學院，教授、博導、副主任

2021.04至今       河北工業大學機械工程學院，院長、教授、博導

2019.11-2019.12  法國圖盧茲第三大學，訪問教授

 

 

 

研究方向 

飛行器結構分析與優化設計、復合材料結構的破壞理論和力學設計、多場條件下多功能結構設計研究成果。 

近3年主持和參與的科研項目：

1.       國家自然科學基金面上項目“先進復合材料連接漸進失效機理及大型飛機典型連接結構強度預測理論研究”，項目編號：11372020，2014~2017，主持

2.       工業和信息化部民用飛機專項科研項目子課題“遠程寬體客機復合材料重要結構設計和分析關鍵技術研究”，2014~2015，主持

3.       國家自然科學基金面上項目“纖維增強復合材料結構多尺度多模式損傷耦合擴展的漸進失效行為研究”，項目編號：11772028，2018~2021，主持

4.       國家自然科學基金面上項目“亞、超臨界載荷下含缺陷/損傷復合材料加筋結構多重損傷演化機理研究”，項目編號：12072005，2021~2024，主持

5.       主持企業橫向課題“多場耦合環境下后體結構設計及分析”，2016.10-2018.12，項目經費：158萬元

6.       主持企業橫向課題“重型整流罩開口影響分析及補強結構優化研究項目”，2019.08-2019.12，項目經費：45萬元

       近3年授權專利與軟著：

[1]    趙麗濱，路緒恒，張建宇，黃偉，劉豐睿. 一種間接測定復合材料多釘連接結構破壞歷程中釘載分配比例的試驗方法. 發明專利

[2]    張建宇，趙麗濱，王雅娜，龔愉，路緒恒. 一種歸一化CFRP多向層合板疲勞分層擴展速率預測方法. 發明專利

[3]    趙麗濱，劉豐睿，房子昂，張建宇. 一種采用均勻釘載進行復合材料螺栓連接結構最終失效載荷預測的方法. 發明專利

[4]    趙麗濱，龔愉，肖鑫，張建宇. 一種改進B-K準則用于含纖維橋接影響復合材料多向層板分層預測的方法. 發明專利

[5]    趙麗濱，楊赟輝，山美娟，劉豐睿. 一種變相對密度octet點陣結構的設計方法. 發明專利

[6]    趙麗濱，賈若迪，王雅娜，王康康，龔愉. 一種復合材料I型分層橋聯法則確定方法. 發明專利

[7]    趙麗濱，王雅娜，賈若迪，龔愉，王康康. 一種CFRP層板任意層間界面I型分層斷裂韌度穩定值的預測方法. 發明專利

[8]    劉豐睿，姚婉婷，趙麗濱. 基于四折線剛度模型的復合材料螺栓連接釘載分配預測方法，

[9]    趙麗濱，楊文，曹天成，陳奎儒. 一種基于漸近損傷模型的全SiC復合材料多釘連接結構失效分析方法. 發明專利

        發表的學術論文：

[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，趙麗濱*．基于可靠性的 CFRP 螺栓連接優化設計方法研究[J]．北京航空航天大學學報. Online

[38]  張嬌蕊，山美娟，黃偉，趙麗濱*. 濕熱環境對CFRP-鋁合金螺栓連接結構靜力失效的影響[J]. 復合材料學報, 2020, 37(0): 1-10

[39]  山美娟，趙麗濱*. CFRP 螺栓連接失效載荷不確定性的評估方法[J]．復合材料學報. Online.

[40]  李重華，劉豐睿*，葉振信，趙麗濱. 考慮橫截面形狀和幾何尺寸的彈簧優化的兩步式策略. 西安交通大學學報. 2020,54(11),74-80

 

[41]  張武昆，閆偉，王會平，趙麗濱，劉豐睿*．不同環境下寬徑比對T800/X850復合材料開孔層壓板壓縮失效的影響．復合材料學報. 2020,37(02),267-275

 

[42]  房子昂，趙麗濱*，劉豐睿，張建宇．碳纖維/樹脂基復合材料多釘連接釘載系數測試方法. 復合材料學報. 2019,36(12),2795-2804

 

[43]  周龍偉，趙麗濱*. 基于失效機制的單向纖維增強樹脂基復合材料退化模型. 復合材料學報. 2019,36(06),1389-1397

 

[44]  趙麗濱*，龔愉，張建宇. 纖維增強復合材料層合板分層擴展行為研究進展. 航空學報. 2019,40(1): 522509.

 

[45]  劉豐睿*，駢瑢，趙麗濱，張建宇. 一種考慮過濾的短纖維復合材料RVE建模方法. 北京航空航天大學學報. 2018, 45(2): 277-282.

 

 

 

聯系郵箱： lbzhao@buaa.edu.cn