( 教授 、研究生导师 、博士生导师 )
  • 学位:博士学位
  • 专业:未填
  • 职称: 教授 、研究生导师 、博士生导师
  • 单位:航空科学与工程学院飞机系
个人简历

程小全教授简介

单位:北京航空航天大学航空科学与工程学院飞机系
办公室:北航继教楼207室
电话:010-82338215
邮箱:xiaoquan_cheng@buaa.edu.cn

主要研究方向:
 复合材料结构设计技术
 复合材料损伤容限分析与设计技术
 结构修补技术
 结构试验技术
 先进飞行器结构设计技术研究等

招生要求:
 英语写作和口语表达能力强。

个人经历:
1983-1987    就读于西北工业大学飞行器结构强度专业,获学士学位。
1987-1992    中航二集团第602研究所(即中国直升机设计研究所)升力系统室,主要从事直升机主桨和尾桨的强度设计工作。
1992-1998    北京航空航天大学飞行器设计专业先后获硕士和博士学位。
1998-2000    北京航空材料研究院先进复合材料国防科技重点试验室博士后。
2000-2008    北京航空航天大学飞机设计研究所副教授。
2008.7-现在  北京航空航天大学飞机/直升机设计研究所教授。
2010.9-2011  南昌航空大学飞行器工程学院挂职副院长。

科研经历:
       先后承担过科技部国家重大专项、国家863项目、国家自然科学基金、航空科学基金、国防预研基金、国防预研课题等研究工作,以及直-8、直-9、直-10、无人飞机、无人直升机、巡航导弹、战术导弹等多个型号设计分析项目,以及“985工程”学科建设任务。在国内重要学术期刊和国际会议上发表论文200多篇,授权专利6项,教材与专著10部。

近年来发表的论文:

1      Liu Shufeng, Cheng Xiaoquan#, Xu Yunyan, Bao Jianwen, Guo Xin. Study on impact performance of scarf-repaired carbon fiber reinforced polymer laminates [J]. Journal of Reinforced Plastics and Composites, 2015, 34(1): 6071.

2      徐云研,程小全,张纪奎,郦正能. 复合材料蜂窝夹层结构T型接头拉伸性能研究[J]. 工程力学, 2015, 32(7): 243248, 256. (Xu Yunyan, Cheng Xiaoquan, Zhang Jikui, Li Zhengneng. Study on composite honeycomb sandwich structure formed T-joints under tensile load [J]. Engineering Mechanics, 2015, 32(7): 243248, 256.)

3      Wu Pengfei, Cheng Xiaoquan#, Fan Zhou. Buckling performance of composite cylindrical shells subjected to compression loads [C]. 18th International Conference on Composite Structures, 15-18 June, 2015, Lisbon, Portugal.

4      Fan Jingfeng, Cheng Xiaoquan#, Wang Songwei, Guo Xin, Zhang Tao. Experimental and numerical investigation of composite bolted π-joint subjected to bending load [J]. Composites Part B, 2015, 78:324330.

5      杨曼曼,程小全,胡仁伟. 复合材料开缝柱壳压缩屈曲分析与试验[J]. 高科技纤维与应用, 2015, 40(2): 5357, 77. (Yang Man-man, Cheng Xiao-quan, Hu Ren-wei. Analysis and experiments of composite cracked cylindrical shell under axial compression [J]. Hi-Tech Fiber & Application, 2015, 40(2): 5357, 77.)

6      程小全,彭霄婧,胡仁伟,范景峰,刘淑峰. 碳纤维复合材料结构修理用胶粘剂应用研究[J]. 高科技纤维与应用, 2015, 40(5): 1119. (Cheng Xiao-quan, Peng Xiao-jing, Hu Ren-wei, Fan Jing-feng, Liu Shufeng. A review of the studies on adhesively bonded repair to carbon fiber composite structures [J]. Hi-Tech Fiber & Application, 2015, 40(5): 1119.)

7      何斌,孟雷,赵军,胡仁伟,程小全. 复合材料旋翼桨叶固有特性和气弹稳定性分析[J]. 高科技纤维与应用, 2015, 40(6): 4549, 54. (He Bin, Meng Lei, Zhao Jun, Hu Ren-wei, Cheng Xiao-quan. Analysis of natural characteristic and aeroelastic stability with a composite rotor blade [J]. Hi-Tech Fiber & Application, 2015, 40(6): 4549, 54.)

8      Cheng Xiaoquan#, Fan Jingfeng, Liu Shufeng, Guo Xin, Xu Yahong, Zhang Tao. Design and investigation of composite bolted π-joints with an unconventional configuration under bending load [J]. Composites Part B, 2016, 85:5967.

9      Liu Peng, Cheng Xiaoquan#, Wang Songwei, Liu Shufeng, Cheng Yujia. Numerical analysis of bearing failure in countersunk composite joints using 3D explicit simulation method [J]. Composite Structures, 2016, 138: 3039.

10   Liu Shufeng, Cheng Xiaoquan#, Zhang Qian, Zhang Jie, Bao Jianwen, Guo Xin. An investigation of hygrothermal effects on adhesive materials and double lap shear joints of CFRP composite laminates [J]. Composites Part B, 2016, 91:431440.

      11   Wang Songwei, Cheng Xiaoquan#, Guo Xin, Li Xin, Chen Gang. Experimental and finite element analysis of composite to aluminium single lap joints [J]. Experimental Mechanics, 2016, 56: 407417.

12   Cheng Xiaoquan#, Yang Manman, Zhang Jie, Zhang Qian, Yujia Cheng, Zhang Jikui. Thermal Behavior and Tensile Properties of Composite Joints with Bonded Embedded Metal Plate under Thermal Circumstance [J]. Composites Part B, 2016, 99:340347.

13   Qian Zhang, Xiaoquan Cheng#, Jie Zhang, Songwei Wang, Yujia Cheng, Tao Zhang. Experimental and numerical investigations of composite box joint under tensile load [J]. Composites Part B, 2016, 107:7583.

14   Baig, Yasir; Cheng, Xiaoquan#; Hasham, Hasan Junaid; et al. Failure mechanisms of scarf-repaired composite laminates under tensile load [J]. JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2016, 38(7): 2069-2075.

15   刘淑峰,张骞,程小全,李伟东,包建文. 湿热环境下碳纤维复合材料斜面胶接件拉伸试验研究[J]. 高科技纤维与应用, 2016, 41(1): 3439. (Liu Shu-feng, Zhang Qian, Cheng Xiao-quan, Li Wei-dong, Bao Jian-wen. Tensile performance of adhesively bonded carbon/epoxy composite scarf joints subject to hygrothermal environment [J]. Hi-Tech Fiber & Application, 2016, 41(1): 3439.)

16   杜晓渊,张婕,程小全,胡仁伟,包建文. 铺层顺序及补片偏转对挖补层合板低速冲击性能的影响[J]. 高科技纤维与应用, 2016, 41(2): 3237. (DU Xiao-yuan, Zhang Jie, Cheng Xiao-quan, Hu Ren-wei, Bao Jian-wen. Effects of stacking sequence and patch rotation on low-velocity impact properties of scarf-repaired composite laminates [J]. Hi-Tech Fiber & Application, 2016, 41(2): 3237.)

17   刘鹏,程小全,刘淑峰,王松伟,郭鑫. 沉头单钉连接层合板拉伸试验与分析[J]. 哈尔滨工程大学学报, 2016, 37(6): 782787. (Liu Peng, Cheng Xiaoquan, Liu Shufeng, Wang Songwei, Guo Xin. Tensile experiment and numerical analysis of single countersunk bolt composite laminate joints [J]. Journal of Harbin Engineering University, 2016, 37(6): 782787.)

18   张骞,王松伟,马埸浩,张婕,程小全,田春明. 复合材料在现代桥梁工程中的应用[J]. 高科技纤维与应用, 2016, 41(6): 2430. (ZHANG Qian, WANG Song-wei, MA Yi-hao, ZHANG Jie, CHENG Xiao-quan, TIAN Chun-ming. Application of FRP materials in modern bridge engineering [J]. Hi-Tech Fiber & Application, 2016, 41(6): 2430.)

19   Cheng Xiaoquan#, Wang Songwei, Zhang Jie, Huang Wenjun, Cheng Yujia, Zhang Jikui. Effect of damage on failure mode of multi-bolt composite joints using failure envelop method [J]. Composite Structures, 2017, 160: 815.

20   Cheng Xiaoquan#, Li Xiaoqi, Zhang Jie, Zhang Qian, Cheng Yujia, Zeng Benyin. Evaluation of tensile properties of composite-metal joint with a novel metal insert design by experimental and numerical methods [J]. Chinese Journal of Aeronautics, 2017, 30(3): 10041011.

21   Ge Mingming, Cheng Xiaoquan#, Zhang Qian. Compressive test and numerical simulation of center-notched composite laminates with different crack configurations [J]. Polymer Composites, 2017, 38(12): 26312641.

22   陈志刚,吴永康,程小全,张涛. 1/3含口盖复合材料柱壳后屈曲性能[J]. 北京航空航天大学学报, 2017, 43(3): 544550. (Chen Zhigang, Wu Yongkang, Cheng Xiaoquan, Zhang Tao. Post-buckling Performance of 1/3 Composite Cylindrical Shell with Cover [J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(3): 544550.)

23   张祥林,黄文俊,胡仁伟,张纪奎,程小全.飞行器复合材料结构雷击防护研究进展[J]. 高科技纤维与应用, 2017, 42(4): 814. (Zhang Xianglin, Huang Wenjun, Hu Renwei, Zhang Jikui, Cheng Xiaoquan. Investigation progress of lightning protection for aircraft composite structures [J]. Hi-Tech Fiber & Application, 2017, 42(4): 814.)

24   熊蕾,胡仁伟,黄文俊,张纪奎,程小全. 复合材料结构热传导与热性能分析研究进展[J]. 高科技纤维与应用, 2017, 42(4): 1520. (Xiong Lei, Hu Renwei, Huang Wenjun, Zhang Jikui, Cheng Xiaoquan. Research progress on heat transfer analysis and thermal properties of composite structures [J]. Hi-Tech Fiber & Application, 2017, 42(4): 1520.)

25   沙勐,熊欣,许名瑞,曾本银,郭鑫,程小全. 湿热环境对复合材料疲劳性能的影响[J]. 高科技纤维与应用, 2017, 42(4): 3743. (Sha Meng, Xiong Xin, Xu Mingrui, Zeng Benyin, Guo Xin, Cheng Xiaoquan. Effect of hygrothermal environment on fatigue properties of composite materials [J]. Hi-Tech Fiber & Application, 2017, 42(4): 3743.)

26   张羽, 王召娣, 但春明, 黄文俊, 胡仁伟, 程小全. 飞机结构复合材料设计值研究进展[J]. 高科技纤维与应用, 2017, 42(5): 815,23. (Zhang Yu, Wang Zhaodi, Dan Chunming, Huang Wenjun, Hu Renwei, Cheng Xiaoquan. Research progress of aircraft composite structural design values [J]. Hi-Tech Fiber & Application, 2017, 42(5): 815,23.)

27   Xiaoquan Cheng#, Jie Zhang, JianWen Bao, Benyin Zeng, Yujia, Cheng, Renwei Hu. Low-velocity impact performance and effect factor analysis of scarf-repaired composite laminates [J]. International Journal of Impact Engineering, 2018, 111: 8593.

28   Xiaoquan Cheng#, Xiaoyuan Du, Jie Zhang, Jikui Zhang, Xin Guo. Effect of stacking sequence and rotation angle of patch on low velocity impact performance of scarf repaired laminates [J]. Composites Part B, 2018, 133: 7885.

29   Cheng Xiaoquan#, Zhang Jie, Cheng Yujia, Guo Xin, Wu Yongkang, Xu Yahong. Numerical analysis on tensile properties of composite hybrid bolted/bonded joints with flanging [J]. Steel and Composite Structures, 2018, 26(3):265-272.

30   Cheng Xiaoquan#, Liu Shufeng, Zhang Qian, Guo Xin, Bao Jianwen. Hygrothermal effects on mechanical behavior of scarf repaired CFRP laminates subject to axial compression laods: experimental and numerical studies [J]. Polymer Composites, 2018, 39(3):904-914.

31   张婕,程小全,胡仁伟,包建文. 挖补复合材料层合板的拉伸和压缩性能研究现状[J]. 高分子材料科学与工程, 2018, 34(1):178-183.(Zhang Jie, Cheng Xiaoquan, Hu Renwei, Bao Jianwen. Tensile and Compressive Properties of Scarf-Repaired Composite Laminates[J]. Polymer Materials Science and Engineering, 2018, 34(1):178-183)

32   Yihao Ma, Xiaoquan Cheng#, Zhaodi Wang, Xin Guo, Jie Zhang, Yahong Xu. Buckling and post-buckling behaviors of 1/3 composite cylindrical shell with an opening [J]. Steel and Composite Structures, 2018, 27(5):555-566.

33   Qian Zhang, Xiaoquan Cheng#, et al. Investigation of tensile behavior and influence factors of composite-to-metal 2D-scarf bonded joint[J]. Engineering Structures, 2019, 180: 284-294.

34   Xiaoquan Cheng#, Qian Zhang, Jie Zhang, Xin Guo, Zhongrong Niu. Parameters prediction of cohesive zone model for simulating composite/adhesive delamination in hygrothermal environments[J]. Composites Part B, 2019, 166: 710–721.

35   Jikui Zhang, Xianglin Zhang, Xiaoquan Cheng#, Yanwei Hei, Liying Xing, Zhibao Li. Lightning strike damage on the composite laminates with carbon nanotube films: Protection effect and damage mechanism [J]. Composites Part B, 2019, 168: 342―352.

36   Salam Abdus,  Xiaoquan Cheng#, Wenjun Huang, Altaf Ahmed, Renwei Hu. Bearing failure and influence factors analysis of metao-to-composite bolted joints at high temperature[J]. Journal of the Brazilian Society of Mechanical Science and Engineering, 2019, 41: 298.

37   Salam Abdus, Xiaoquan Cheng#, Yujia Cheng, Renwei Hu, Abid Muhammad.Dynamic properties of single and muti-bolted compoaite joints at different bolt-loads and elevated temperature[J]. Australian Jounnal of Mechanical Engineering, 2019, DOI: 10.1080/14484846.2019. 1629188.

38   陈坤,舒茂盛,胡仁伟,郭鑫,程羽佳,程小全#. 带衬套沉头螺栓复合材料/金属接头拉伸性能[J]. 北京航空航天大学学报, 2019, 45(3): 633―640. (Chen Kun, Shu Maosheng, Hu Renwei, Guo Xin, Cheng Yujia, Cheng Xiaoquan. Tensile performance of countersunk bolted composite/metal joints with sleeve [J]. Joural of Beijing University of Aeronautics and Astronautics, 2019, 45(3): 633―640.)

39   邓金鑫,陈少军,张羽,黄文俊,程小全#. 复合材料设计、分析和工艺软件发展现状[J]. 高科技纤维与应用, 2019, (3): 42―51. (Deng Jinxin, Chen Shaojun, Zhang Yu, Huang Wenjun, Cheng Xiaoquan. Development of composite structural design, analysis and manufacturing software [J]. Hi-Tech Fiber & Application, 2019, (3): 42―51.)

40   Jie Zhang, Xiaoquan Cheng#, Xin Guo, Jianwen Bao, Wenjun Huang. Effect of environment conditions on adhesive properties and material selection in composite bonded joints [J]. International Journal of Adhesion and Adhesives, 2020, 96: 102302. 

41   Xiaoqi Li, Xiaoquan Chenga#, Xin Guo, Shufeng Liu, Zhiyong Wang. Tensile properties of a hybrid bonded/bolted joint: Parameter study[J]. Composite Structures, 2020, 245:112329.

42  Yihao Ma, Xiaoquan Cheng#, Jikui Zhang, Dafang Zhao, Wenjun Huang. Prediction of resin pocket geometry around rigid fiber inclusion in composite laminate by hot-pressing of prepregs [J]. Journal of Composite Materials, 2020, 54(15): 1987-1999.

43  Du Xiaoyuan, Cheng Xiaoquan#, Cheng Yujia, Huang Wenjun, Chen Gang. Analysis and design improvement of composite bolted Π-joints under bending load [J]. Journal of the Brazilian Society of Mechanical Science and Engineering, 2020, 42: 384.

44  Jie Zhang, Xiaoquan Cheng#, Yujia Cheng, Xin Guo, Liu Yang. Effect of over-ply on moisture absorption behavior of scarf-repaired composite laminate [J]. International Journal of Adhesion and Adhesives, 2020, 102: 102683.

45  张婕,程小全#,程羽佳,冯振宇. 湿热环境对CCF800/环氧挖补板拉压性能的影响[J]. 北京航空航天大学学报, 2020, 46(6): 1116-1124. (Zhang Jie, Cheng Xiaoquan, Cheng Yujia, Feng Zhenyu. Effect of hygrothermal environment on tensile and compressive properties of CCF800/epoxy scarf-repaired laminates [J]. Joural of Beijing University of Aeronautics and Astronautics, 2020, 46(6): 1116-1124.)

46  周震,程小全#,张涛,陈磊,吴永康. 可收卷复合材料层板大变形弯曲性能研究[J]. 工程力学, 2020, 37(8):213-220, 229. (Zhou Zheng, Cheng Xiaoquan, Zhang Tao, Chen lei, Wu Yongkang. Study on large deformation bending properties of rollable composite laminates [J]. Eigneering Mechanics, 2020, 37(8):213-220, 229.)

47  Jie Zhang, Xiaoquan Cheng#, Jikui Zhang, Xin Guo, Wenjun Huang. Effect of curing condition on bonding quality of scarf-repaired composite laminates [J]. Chinese Journal of Aeronautics, 2020, 33(8): 2257-2267.



       出版的教材与著作

      1.   贾玉红, 程小全主编.《现代民用飞机结构与系统(四系用教材,编写其中22万字). 北京:北京航空航天大学讲义2004.1.

2.     郦正能主编.《飞行器结构学》(编写其中9万多字. 北京: 北京航空航天大学出版社, 2005.1(获2006年北京高等教育精品教材称号,国家教委重点教材).

3.     郦正能主编, 程小全副主编.《飞机部件与系统设计》(编写其中25万字. 北京: 北京航空航天大学出版社, 2006.5(国防重点教材)(获2008年获北京高等教育精品教材称号).

4.      高振荣主编,程小全、薛忠民副主编.《英汉复合材料技术词汇》. 北京:化学工业出版社,2007. 01.

5.      程小全译,Michael, C.Y. Niu.《实用飞机结构工程设计》. 北京:航空工业出版社,2008.10(获航空科技图书出版专项资助).

6.      冯振宇,程小全,张纪奎译. Michael, C.Y. Niu.《实用飞机结构应力分析与尺寸设计》. 北京:航空工业出版社,2009.12(获航空科技图书出版专项资助).

7.      郦正能主编,程小全副主编.《飞行器结构学(第2版)》. 北京: 北京航空航天大学出版社, 2010.03(普通高等教育“十一五”国家级规划教材,201111月获教育部2011年普通高等教育精品教材).

8.      程小全,张纪奎译. Michael, C.Y. Niu.《实用飞机复合材料结构设计与制造》. 北京:航空工业出版社,2010.11.

9.      范金娟,程小全,陶春虎编著.《聚合物基复合材料构件失效分析基础》. 北京:国防工业出版社,2011.06(获国防科技图书出版基金资助).

10.   范金娟,程小全等译,[]L.A. Carlsson, G.A. Kardomateas.《夹层复合材料结构与失效机制》. 北京国防工业出版社,2019.

11.   郦正能,程小全等著.《飞机部件与系统设计(第2版)》.北京:北京航空航天大学出版社,2020.09(教育部高等学校航空航天类专业教学指导委员会推荐教材).


教育理念:

学生是教师的未来,教育真正能够帮助的是那些想提升自己的人。


《飞机结构设计》MOOC课程链接:http://mooc.buaa.edu.cn/courses/course-v1:BUAA+BUAA_FG+2019_T2/about

更多个人介绍可查看:

    https://baike.baidu.com/item/%E7%A8%8B%E5%B0%8F%E5%85%A8/1769002?fr=aladdin  

    http://graduate.buaa.edu.cn/TutorInfo.jsp?id=14863


教育经历
1992.9-1998.6
 北京航空航天大学 | 飞行器设计  | 博士学位 
1983.9-1987.7
 西北工业大学 | 飞机结构强度  | Bachelor's Degree 
工作经历
2000.7-2017.10
 航空科学与工程学院 | 北京航空航天大学 
1998.9-2000.6
 先进复合材料国防重点实验室 | 北京航空材料研究院 
1987.7-1998.8
 升力系统室 | 中国直升机设计研究所  | 室工会主席 
研究概况

研究领域包括:

   — 飞行器结构设计

   — 复合材料结构损伤容限分析与设计

   — 结构试验与评定技术

   — 复合材料结构修理技术

   — 复合材料模具设计

   — 隔热复合材料结构设计等


凡舟新材料结构实验室条件:

  - 美国500kN-INSTRON液压材料试验机一台;

  - 美国250kN-INSTRON(配备有环境箱)液压材料试验机一台;

  - 美国100kN-INSTRON液压材料试验机一台;

  - 2点协调加载系统(两个10吨作动缸)一套;

  - 德国Polytec激光测震设备一套;

  - 复合材料低速冲击试验机一台;

  - 德国进口小裂纹观测设备一套;

  - 台湾宏达10吨和5吨电拉材料试验机各一套,做小的结构试验用;

  - 美国StrainBook616动态应变数据采集分析系统;

  - 超声C扫描无损检测设备一套;

  - 多通道自动数据采集系统一套;

  - 高低温环境箱二套;

  - 水箱一个;

  - 徕卡光学显微镜一套;

  - 徕卡体视显微镜一套。


实验室目标:

根据材料-结构-功能一体化、材料-设计-制造一体化以及结构整体化的发展趋势,通过采用精确的加载和先进的测试手段,使我校飞行器结构设计学科的发展达到国际先进水平,研究成果能够直接转化应用到具体的先进飞行器结构设计中。该实验室拥有多台高精度的加载设备、两作动缸复杂协调加载设备、激光测震设备、微裂纹测试设备、超声C扫描复合材料无损检测设备、多通道应变测量设备以及高低温环境箱等,可以开展复合材料结构与金属结构的加载和破坏试验、智能结构振动试验、结构健康监控试验、结构疲劳试验等等。实验室目前拥有教授2人、高工1人、副教授2人,实验员2人,是一个老中青结合的团队,并且在国内具有一定的影响。

实验室主任:程小全教授。