張建宇，男，漢族，黑龍江人，1973年12月生，博士，重慶大學航空航天學院教授。 研究工作圍繞飛行器結構疲勞可靠性這個主題展開，作為項目負責人主持了30多個科研項目，主持項目的契約經費累計1500萬元以上；作為主要成員參與10多個科研項目；科研經費到款1300餘萬元。主持科研項目包括：國家自然科學基金面上項目2項，國家863重大項目子課題1項，大型客機預研和型號攻關百萬以上項目2項。獲航空科技進步一等獎和北航科技進步二等獎各一項。在國內外學術期刊/會議上發表和錄用論文130餘篇，SCI期刊論文28篇，WOS引用88次；EI/ISTP收錄85篇。以第一享有人申請國家發明專利6項，已授權2項。
基本介紹
- 中文名：張建宇
- 畢業院校：北京航空航天大學
- 學位/學歷：博士
- 專業方向：飛行器設計與套用力學
人物經歷,教育經歷,工作經歷,科研項目,學術兼職,社會服務,研究方向,代表論文,
人物經歷
教育經歷
1991.09-1995.07北京航空航天大學飛行器設計與套用力學系學士
1994.09-1997.07北京航空航天大學飛行器設計與套用力學系碩士
1997.09-2000.09北京航空航天大學飛行器設計與套用力學系博士
工作經歷
2000.10-2007.07北京航空航天大學飛行器設計與套用力學系/航空科學與工程學院講師
2003.09-2004.03日本九州大學工學院航空宇航工程專業訪問學者
2004.09-2005.09北京航空航天大學人事處掛職副處長
2005.09-2007.11北京航空航天大學人事處副處長
2007.11-2008.11北京航空航天大學人才交流中心主任
2007.12-2008.07國防科工委發展研究中心綜合計畫部部長（借調）
2009.04-2009.08英國南安普頓大學工學院訪問學者
2001.10-2015.01北京航空航天大學疲勞斷裂實驗室主任
2007.07-2015.01北京航空航天大學航空科學與工程學院副教授
2015.01-今重慶大學航空航天學院研究員
科研項目
- 國家自然科學基金面上項目：金屬材料多軸-高周疲勞載入軟性係數研究（項目負責人，68萬元）
- 國家自然科學基金面上項目：碳纖維增強複合材料多向層板疲勞分層擴展行為研究（項目負責人，86萬元）
- 國家863重大項目：先進輕質複合材料成形技術與裝備開發與典型套用（北航課題負責人，107萬元）
- 大型客機預研項目：大型客機蒙皮連線結構多部位損傷分析評定技術（項目技術負責人，北航課題負責人，2008.12-2011.07，北航經費：190萬元）
- ARJ21型號攻關項目：ARJ21-700飛機02架飛機製造中代料偏離補充試驗（項目負責人，160萬元）
- C919型號攻關係列項目：加工工藝對鋁鋰合金疲勞性能影響對比研究，鋁鋰合金力學性能及結構件疲勞性能測試，噴丸成形對材料性能影響研究（項目負責人，共159萬元）
- 航空金屬材料和結構疲勞/斷裂性能測試與分析系列項目：大寬板疲勞裂紋擴展測試與分析，鈦合金薄板疲勞及裂紋擴展性能試驗研究，鋼製螺栓元件力學性能測試，航空材料的腐蝕與譜載裂紋擴展測試，航空材料的焊接及腐蝕疲勞與裂紋擴展性能測試，2E12等航空鋁合金的腐蝕與譜載裂紋擴展性能試驗研究，鋁合金疲勞與裂紋擴展門檻值測試等（項目負責人，共約500萬元）
學術兼職
北京力學會固體力學專業委員會委員；複合材料學會高級會員；Composite Structures (IF: 3.120, Q1)、Materials & Design (IF: 3.171, Q1)、IJ Solids Structures (IF: 2.035, Q1)、IJ Mechanical Sciences (IF: 2.061, Q1)、Meccanica (IF: 1.815, Q1)、J Aerospace Engineering (IF: 0.926, Q1)、J Composite Materials (IF: 1.257, Q2)、力學學報、力學季刊、套用力學學報、實驗力學等期刊評審人。
社會服務
作為疲勞專家參與多個型號飛行器的研製方案、試驗總任務書及首飛等評審，參與多個在役、在研飛行器型號的故障分析、故障歸零工作，參與載人航天工程三期材料選型評審。
研究方向
金屬多軸疲勞：開展了金屬材料多軸高周疲勞研究，提出了疲勞軟性係數這個力學量作為多軸疲勞失效模式的判據，並進行了系統驗證，解決了多軸高周疲勞失效模式判據缺失問題。相關工作已在國際期刊IJ Fatigue上發表了系列論文，被法國、葡萄牙、波蘭等國同行多次引用。
複合材料疲勞斷裂：通過理論和實驗研究，揭示了多向界面分層擴展阻力的形成機制，建立了阻力修正的分層疲勞擴展模型，可以準確地描述多向層板的分層擴展規律。這些成果已在Composite Structures, IJ Fatigue, Journal of Composite Materials等期刊發表系列論文，並被美國、荷蘭、西班牙等國同行多次引用。
疲勞可靠性工程：圍繞Jxx系列飛機機翼、尾翼的復材主結構開展研究，建立了復材結構外場損傷性能評價技術體系，完成了關鍵構件的試驗驗證，在Jxx-B疲勞定壽和Jxx-D型號選材中獲得了直接套用。幫助航天主機院所完成了多個型號的疲勞壽命評定，在實踐中逐步建立起飛彈疲勞壽命評定的技術體系。在疲勞可靠性工程方面的研究成果已套用于飛機、飛彈、衛星等11個型號，取得了重大軍事和經濟效益。
代表論文
1.Zhao L, Wang Y,Zhang J(Corresponding author), et al. XFEM-based model for simulating zigzag delamination growth in laminated composites under mode I loading[J]. Composite Structures, 2017, 160:1155-1162.
2.Zhao L, Gong Y,Zhang J(Corresponding author), et al. A novel interpretation of fatigue delamination growth behavior in CFRP multidirectional laminates[J]. Composites Science & Technology, 2016, 133:79-88.
3.Zhao L, Wang Y,Zhang J(Corresponding author), et al. An interface-dependent model of plateau fracture toughness in multidirectional CFRP laminates under mode I loading[J]. Composites Part B Engineering, 2017, 131.
4.Gong Y, Zhao L,Zhang J(Corresponding author),, et al. Delamination propagation criterion including the effect of fiber bridging for mixed-mode I/II delamination in CFRP multidirectional laminates[J]. Composites Science & Technology, 2017, 151.
5.Zhao, L., Shan, M., Hong, H., Qi, D.,Zhang J(Corresponding author), & Hu, N.. A residual strain model for progressive fatigue damage analysis of composite structures.Composite Structures, 2016，169.
6.Zhang Jianyu (Corresponding author), Shi Xinhong, Fei Binjun. High cycle fatigue and fracture mode analysis of 2A12-T4 aluminum alloy under out-of-phase axial-torsion constant amplitude loading. International Journal of Fatigue. 2012, 38:144-154.
7.Zhang Jianyu (Corresponding author), Shi Xinhong, Bao Rui and Fei Binjun. Tension-torsion high-cycle fatigue failure analysis of 2A12-T4 aluminum alloy with different stress ratios. International Journal of Fatigue. 2011,33(8):1066-1074.
8.Zhang Jianyu (Corresponding author), Peng Lei, Zhao Libin, Fei Binjun.Fatigue Delamination Growth Rates and Thresholds of Composite Laminates under Mixed Mode Loading.International Journal of Fatigue. 2012, 40:7-15.
9.Zhang Jianyu (Corresponding author), Liu Fengrui, Zhao Libin, Fei Binjun. A novel characteristic curve for failure prediction of multi-bolt composite joints. Composite Structures. 2014, 108:129-136.
10.Zhang Jianyu (Corresponding author), Liu Fengrui, Libin Zhao, Chen Yuli, Fei Binjun. A progressive damage analysis based characteristic length method for multi-bolt composite joints. Composite Structures. 2014, 108:915-923.
11.Zhang Jianyu,ZhaoLibin, Qin Tianliang, Fu Yue, Fei Binjun.Influence ofpoverlaminates on the mechanical behavior of all-composite adhesively bondedpjoints.Journal of Reinforced Plastics and Composites 2014, 33(10):923-934.
12.Zhang Jianyu(Corresponding author), Xiao Qingshan, Shi Xinhong, Fei Binjun. Effect of Mean Shear Stress on Torsion Fatigue Failure Behavior of 2A12-T4 Aluminum Alloy. International Journal of Fatigue. 2014, 67:173-182.
13.Peng Lei (Ph.D. Candidate),Zhang Jianyu (Corresponding author), Zhao Lilin, Bao Rui, Yang Hongqin, Fei Binjun.Mode I Delamination Growth of Multidirectional Composite Laminates under Fatigue Loading.Journal of Composite Materials. 2011, 45(10):1077-1090.
14.Zhang Jianping (Ph.D. Candidate),Zhang Jianyu (Corresponding author), Bao Rui, Zheng Xiaoling. Study of Methods for Evaluating the Probability of Multiple Site Damage Occurrences. Science China Physics, Mechanics & Astronomy. 2014, 57(1):65-73.
15.Qin Tianliang(Ph.D. Candidate), Zhao Libin,Zhang Jianyu (Corresponding author). Fastener effects on mechanical behaviors of double-lap composite joints. Composite Structures. 2013, 100:413-423.
16.Zhao Libin, Zhang Xiaoxiao,Zhang Jianyu (Corresponding author),Huang Hai, Liang Xianzhu.Failure Analysis of Woven Composite Π Joint under Bending Load.Advanced Science Letters. 2011, 4(8-10):2752-2758.
17.Chen Yuli, Wang Shengtao, Pan Fei,Zhang Jianyu (Corresponding author). A numerical study on electrical percolation of polymer matrix composites with hybrid fillers of carbon nanotubes and carbon black. Journal of Nanometerials. 2014, 2014: 614797.
18.Zhao Libin, Gong Yu,Zhang Jianyu (Corresponding author), Chen Yuli, Fei Binjun. Simulation of delamination growth in multidirectional laminates under mode I and mixed mode I/II loadings using cohesive elements. Composite Structures. 2014, 116:509-522.
19.Zhao Libin, Qin Tianliang,Zhang Jianyu (Corresponding author), Shan Meijuan, Fei Binjun. Determination method of stress concentration relief factors for failure prediction of composite multi-bolt joints. Journal of Composite Materials. 2014.
20.Fu Yue (Ph.D. Candidate),Zhang Jianyu,Zhao Libin. Strength Prediction of Composite Π Joint under Bending Load and Study of Geometric and Material Variations Effects.Journal of Composite Materials. 2013, 47(8):1029-1038.
21.Tian Hailing, Bao Rui,Zhang Jianyu,Zheng Xiaoling, Fei Binjun. The Influence of Low Load Truncation Level on Crack Growth for Al 2324-T39 and Al 7050-T7451. Chinese J. of Aeronautics. 2009, 22(4):401-406.
22.Zhao Libin, Qin Tianliang,ShenoiRamanandAjit,Zhang Jianyu,Liang Xianzhu, Huang Hai. Strength Prediction of Composite Π Joint Under Tensile Load. Journal of Composite Materials. 2010,44(23):2759-2778.
23.Yang Hongqin (Ph.D. Candidate), Bao Rui,Zhang Jianyu, Peng Lei, Fei Binjun. Crack Growth Behaviour of a Nickel-based Powder Metallurgy Superalloy under Elevated Temperature. International Journal of Fatigue. 2011, 33(4):632-641.
24.Yang Hongqin (Ph.D. Candidate), Bao Rui,Zhang Jianyu, Peng Lei, Fei Binjun. Creep-fatigue crack growth behaviour of a nickel-based powder metallurgy superalloy under high temperature. Engineering Failure Analysis. 2011, 18(4):1058-1066.
25.Liu Hao (Ph.D. Candidate), Bao Rui,Zhang Jianyu, Fei Binjun. A creep-fatigue crack growth model containing temperature and interactive effects. International Journal of Fatigue. 2014, 59:34-42.
26.Zhao Libin, Qin Tianliang, Chen Yuli,Zhang Jianyu.Three dimensional progressive damage models for cohesively bonded composite π joint.Journal of Composite Materials. 2014, 48(6): 707-721.
27.Bao Rui, Yang Hongqin,Zhang Jianyu, Peng Lei, Fei Binjun. Fatigue crack growth measurement in a superalloy at elevated temperature.International Journal of Fatigue. 2013, 47:189-195.
28.Liu Fengrui (Ph.D. Candidate), Zhao Libin, Mehmood Saqib,Zhang Jianyu, Fei Binjun. A modified failure envelope method for failure prediction of multi-bolt composite joints. Composites Science and Technology. 2013, 83:54-63.
29.Zhao Libin, Gong Yu, Qin Tianliang, Mehmood Saqib,Zhang Jianyu. Failure prediction of out-of-plane woven composite joints using cohesive element. Composite Structures.2013, 106:407-416.
30.Zhao Libin, Qin Tianliang,Zhang Jianyu, Shenoi Ramanand Ajit. Modified Maximum Stress Failure Criterion for Composite π Joints. Journal of Composite Materials. 2013, 47(23):2995-3008.
(SCI:000329545100001,IF: 1.257, 2013 JCRMaterials Science, CompositesQ2, 9/23)
31.Peng Lei, Xu Jifeng,Zhang Jianyu, Zhao Libin. Mixed mode delamination growth of multidirectional composite laminates under fatigue loading. Engineering Fracture Mechanics. 2012, 96:676-686.
