劉豐睿(北京航空航天大學副教授碩士生導師)

劉豐睿，北京航空航天大學宇航學院航天飛行器技術系副教授、碩士生導師，兼任黨支部副書記及北京力學會力學與工程結合委員會副主任。2003年進入北京航空航天大學學習，獲飛行器設計專業學士與固體力學博士學位，期間赴加拿大西安大略大學開展博士後研究。2016年起任教於北航，2020年晉升副教授。

長期從事飛行器結構設計與複合材料力學研究，聚焦複合材料連線結構失效機理及最佳化算法，開發了多螺栓接頭失效分析模型，成果套用於重型運載火箭、超聲速飛行器等型號研製。主持國家自然科學基金青年項目等科研課題，發表SCI論文30餘篇，獲授權發明專利5項。主講《飛行器結構力學》等課程，獲宇航學院人才培養貢獻獎、優秀畢業設計指導教師等教學榮譽。

基本介紹

• 中文名：劉豐睿
• 國籍：中國
• 民族：蒙古族
• 出生地：內蒙古自治區開魯縣
• 出生日期：1984年7月25日
• 畢業院校：北京航空航天大學
• 學位/學歷：博士/研究生
• 職業：教師
• 專業方向：飛行器設計
• 電子信箱：[email protected]

人物經歷

工作經歷

2020.7-今 北京航空航天大學 飛行器設計 副教授

2016.10-2020.6 北京航空航天大學 飛行器設計 講師

2015.9-2016.9 WesternUniversity 複合材料力學 博士後

2014.4-2016.10 北京航空航天大學 複合材料力學 博士後

學習經歷

2009.9-2014.7 北京航空航天大學 固體力學博士

2007.9-2009.7 北京航空航天大學 飛行器設計 碩博連讀

2003.9-2007.7 北京航空航天大學 飛行器設計 學士

研究方向

飛行器結構設計，複合材料結構力學

主講課程

飛行器結構力學

飛行器結構概論與3D列印套用

高等結構分析與設計

航空航天材料與結構實驗

榮譽及獎勵

[1]北京力學會第24屆學術年會青年力學工作者優秀學術論文獎

[2]2018 年宇航學院本科生人才培養貢獻獎

[3]2019 年宇航學院本科生人才培養貢獻獎

[4]獲宇航學院2019年院級“優秀本科畢業設計”指導教師

[5]北航學院2018學年“優秀班主任”稱號

[6]北航學院2019學年“優秀導師”稱號

研究成果

[1] Fengrui Liu, Wanting Yao, Libin Zhao, Hao Wud, Xi Zhang, JianyuZhang. An improved 2D finite element model for bolt loaddistribution analysis of composite multi-bolt single-lap joints. CompositeStructures, 2020; 253: 112770.

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

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

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

[5] Fengrui Liu, Meijuan Shan, Libin Zhao, Jianyu Zhang.Probabilistic bolt load distribution analysis of composite single-lapmulti-bolt joints considering random bolt-hole clearances and tighteningtorques. Composite Structures, 2018; 194: 12-20.

[6] Fengrui Liu, Xuheng Lu, Libin Zhao, Jianyu Zhang,Jifeng Xu, Ning Hu. Investigation of bolt load redistribution and its effect onfailure prediction in double-lap, multi-bolt composite joints. CompositeStructures, 2018; 202: 397-405.

[7] Fengrui Liu, Jianyu Zhang, Libin Zhao, An Xin, Longwei Zhou. Ananalytical joint stiffness model for load transfer analysis in highly torquedmulti-bolt composite joints with clearances. Composite Structures, 2015; 131:625-636.

[8] Fengrui Liu, Libin Zhao, Saqib Mehmood, Jianyu Zhang, BinjunFei. A modified failure envelope method for failure prediction of multi-boltcomposite joints. Composites Science and Technology, 2013; 83: 54-63.

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

[10] W.M.Mahdy, Libin Zhao, Fengrui Liu, Rong Pian, Huiping Wang, JianyuZhang. Buckling and stress-competitive failure analyses ofcomposite laminated cylindrical shell under axial compression and torsionalloads. Composite Structures, 2021; 255: 112977.

[11] KangkangWang, Fengrui Liu, Haiming Hong. Shear failure mechanisms and influences ofoverlaminate configuration on the failure of composite π joints. Results inPhysics, 2019; 12: 934-942.

[12] YanaWang, Ruodi Jia, Fengrui Liu. A ply-by-ply discretized 2D FEAapproach with the integrated XFEM-CE strategy for predicting multiple failuresin laminated composite structures. CMES-Computer Modeling in Engineering &Sciences, 2019; 120(1): 215-234.

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

[14] XinhongShi, Yana Wang, Ruodi Jia, Fengrui Liu, Jianyu Zhang. Experimentalinvestigations on microstructures and mechanical properties of white yak horns sheath.Results in Physics, 2019; 13: 102174.

[15] LibinZhao, Kangkang Wang, Fan Ding, Tianliang Qin, Jifeng Xu, Fengrui Liu, Jianyu Zhang. A post-buckling compressive failure analysisframework for composite stiffened panels considering intra-, inter-laminardamage and stiffener debonding. Results in Physics, 2019; 13: 102205.

[16] YunfengDong, Xiaona Wei, Fengrui Liu. Novel collaborative optimizationframework using a negotiation model for satellite system design. EngineeringOptimization, 2018; 50(8): 1395-1414.

[17] MeijuanShan, Fengrui Liu, Ziang Fang, Libin Zhao, Jianyu Zhang. Abi-material property based FE modelling method for progressive damage analysesof composite double-lap bolted joints. Results in Physics, 2018; 11: 674-683.

[18] LongweiZhou, Libin Zhao, Fengrui Liu, Jianyu Zhang. Amicromechanical model for longitudinal compressive failure in unidirectionalfiber reinforced composite. Results in Physics, 2018; 10: 841-848.

[19] YunfengDong, Xiaona Wei, Lu Tian, Fengrui Liu, Guangde Xu. A novel double clusteranalysis and principal component analysis based optimization method for theorbit design of Earth observation satellites. International Journal of AerospaceEngineering, 2017; Article ID 6396032.

[20] MeijuanShana, Libin Zhao, Fengrui Liu, Dexuan Qi,Jianyu Zhang. Revealing the competitive fatigue failure behaviourof CFRP-aluminum twobolt, double-lap joints. Composite Structures, 2020; 244:112166.

[21] TianliangQin, Libin Zhao, Jifeng Xu, FengruiLiu, JianyuZhang. Model of CEL for 3D elements in PDMs of unidirectional compositestructures. Computer Modeling in Engineering & Sciences, 2019; 118 (1): 157-176.

[22] MeijuanShan, Libin Zhao, Haiming Hong, FengruiLiu, Jianyu Zhang.A progressive fatigue damage model for composite structures in hygrothermalenvironments. International Journal of Fatigue, 2018; 111: 299-307.

[23] LibinZhao, Meijuan Shan, Fengrui Liu, Jianyu Zhang.A probabilistic model for strength analysis of composite double-lap single-boltjoints. Composite Structures, 2017; 161: 419-427.

[24] LongweiZhou, Donghua Zhang, Libin Zhao, Xiaohong Zhou, Jianyu Zhang, Fengrui Liu. Design and analysis of a novel bolted composite π joint underbending load. Materials and Design, 2016; 98: 201-208.

[25] LibinZhao, An Xin, Fengrui Liu, Jianyu Zhang, Ning Hu. Secondary bending effectsin progressively damaged single-lap, single-bolt composite joints. Results inPhysics, 2016; 6: 704-711.

[26] JianyuZhang, Fengrui Liu, Libin Zhao, Jie Zhi, Longwei Zhou, Binjun Fei.Influence of end distances on the failure of composite bolted joints. Journalof Reinforced Plastics and Composites, 2015; 34: 388-404.

[27] JianyuZhang, Fengrui Liu, Libin Zhao, Meijuan Shan. Investigation oncharacteristic length testing methods for failure prediction of compositemulti-bolt joints. Journal of Reinforced Plastics and Composites, 2015; 34: 636-648.

[28] JianyuZhang, Fengrui Liu, Libin Zhao,Yuli Chen, Binjun Fei. A progressive damage analysis based characteristiclength method for multi-bolt composite joints. Composite Structures, 2014; 108:915-923.

[29] JianyuZhang, Fengrui Liu, Libin Zhao,Binjun Fei. A novel characteristic curve for failure prediction of multi-boltcomposite joints. Composite Structures, 2013; 108: 129-136.

[30] 劉豐睿, 駢瑢, 趙麗濱, 張建宇. 一種考慮過濾的短纖維複合材料RVE 建模方法. 北京航空航天大學學報, 2019; 45(2): 277-282.

[31] 劉豐睿, 趙麗濱, 韓邦成, 房建成. 磁懸浮控制力矩陀螺框架結構的拓撲最佳化設計. 北京航空航天大學學報, 2010; 36: 455-458+499.

[32] 張武昆, 閆偉, 王會平, 趙麗濱, 劉豐睿. 不同環境下寬徑比對碳纖維增強環氧樹脂複合材料開孔層壓板壓縮失效的影響. 複合材料學報, 2020; 37(2): 267-275.

[33] 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最佳化的兩步式策略. 西安交通大學學報, 2020; 54(11): 74-80.

[34] 張建宇, 劉豐睿, 山美娟, 趙麗濱. 複合材料多釘連線釘載矢量感測器. 複合材料學報, 2015; 32:1420-1427.