个人简述:

[1] 大尺寸薄厚度飞机壁板自动装配关键技术与装备. 2015年陕西省科学技术一等奖，排名第1；[2] 复杂产品装配工艺快速设计支持技术研究与应用. 2007年陕西省科学技术二等奖，排名第2；[3] 复杂产品研制协同项目管理技术研究与应用. 2009年陕西省科学技术二等奖，排名第6；[4] 民用飞机数字化集成技术开发与应用. 2013年陕西省科学技术二等奖, 排名第3；[5] 2009年、2011年分别获第十一、十二届“挑战杯”全国大学生课外学术科技作品竞赛优秀指导教师；[6] 陕西省中青年科技创新领军人才（2016年）；[7] 获得陕西青年五四奖章提名奖、西安青年五四奖章。

科研工作:

1. 先进装配与连接2. 结构损伤与疲劳 公开发表论文（代表作）：[1]A novel prediction model forthrust force and torque in drilling interface region of CFRP/Ti stacks. TheInternational Journal of Advanced Manufacturing Technology, online,DOI10.1007/s00170-015-7294-9.Bin Luo, Yuan Li, Kaifu Zhang*, Hui Cheng, ShunuanLiu[2]Effect of workpiece stiffnesson thrust force and delamination in drilling thin composite laminates. Journalof Composite Materials, online, doi: 10.1177/0021998315580449. Bin Luo, YuanLi, Kaifu Zhang*, Hui Cheng, Shunuan Liu[3]Interface damage behaviour duringinterference-fit bolt installation process for CFRP/Ti alloy joining structure.Fatigue & Fracture of Engineering Materials & Structures, online,DOI10.1111/ffe.12313. Jian Li, Yuan Li, Kaifu Zhang*, Ping Liu, Peng Zou.[4]Microscopic mechanism based forceprediction in orthogonal cutting of unidirectional CFRP. The InternationalJournal of Advanced Manufacturing Technology, V79, P1209-1219. Zhenchao Qi,Kaifu Zhang*, Hui Cheng, Dong Wang, Qingxun Meng,[5]Stress distribution modelingfor interference-fit area of each individual layer around composite laminatesjoint . Composites Part B: Engineering, V78, N1, P469-479.Danlong Song, YuanLi, Kaifu Zhang*, Ping Liu, Hui Cheng, Tao Wu[6]An analytical method forpredicting the fluctuation of thrust force during drilling of unidirectionalcarbon fiber reinforced plastics. Journal of Composite Materials, V49, 699-711.QingxunMeng, Kaifu Zhang*, Hui Cheng, Shunuan Liu, and Shoushan Jiang.[7]Analysis of bolt-to-laminateinterface frictionin bolted composite joint with interference-fit. MaterialsResearch Innovations, V19, P42-45. Yuan Xin Duan, Yuan Li, Kaifu Zhang*, PingLiu, Jian Li.[8]Numerical simulation fordelamination during drilling of CFRP/AL stacks. Materials Research Innovations,V19, P98-101. Zhenchao Qi, Kaifu Zhang*, Hui Cheng, Shunuan Liu.[9]Experimental and theoreticalstress analysis for an interface stress model of single-L adhesive jointsbetween CFRP and aluminum components. International Journal of Adhesion andAdhesives, V 50, P37-44.Kaifu Zhang, Lin Li, YuanxinDuan, Yuan Li[10]Critical thrust forcepredicting modeling for delamination-free drilling of metal-FRP stacks.Composite Structures, V107, P 604-609. Zhenchao Qi Kaifu Zhang* Yuan Li,Shunuan Liu, Hui Cheng.[11]A method for predicting thecuring residual stress for CFRP/Al adhesive single-lap joints. InternationalJournal of Adhesion and Adhesives, V46, P 7-13. Kaifu Zhang*, Zhaojun Yang,Yuan Li[12]Based on region division setupplanning for sheet metal assembly in aviation industry. Proceedings of the Institutionof Mechanical Engineers, Part B: Journal of Engineering Manufacture, V227,P153-161. Ping Liu Yuan Li Kaifu Zhang* Hui Cheng.[13]Riveting Process Modeling andSimulating for Deformation Analysis of Aircraft's Thin-walled Sheet-metalParts. Chinese Journal of Aeronautics, V24, P369-377. Kaifu Zhang * Hui ChengYuan Li.[14]An integrated modeling methodof unified tolerance representation for mechanical product. The InternationalJournal of Advanced Manufacturing Technology, V46, P217-226., Kaifu Zhang*Yuan Li Shuilong Tang[15]L型碳纤维增强复合材料/铝合金胶接复合构件剥离应力建模与分析. 机械工程学报，V48, P44-50. 段元欣，张开富*，王中强，马艳艳[16]空间多姿态下自动钻铆托架变形分析与调平方法.西北工业大学学报，V30, P129-137.张开富*，曾佩杰，栾超，牟伟强，李原.？？