万方义

的个人主页 http://teacher.nwpu.edu.cn/fwan

  被浏览次数:17752

基本信息 The basic information

万方义

航空学院

博士研究生毕业

工学博士

副教授

副院长

航空宇航科学与技术

工作经历 Work Experience

2003.12-2006.12,西北工业大学,博士后

2005.12-2006.6,美国弗吉尼亚州立理工学院(Virginia Tech),访问学者

2013.3-2014.3,比利时列日大学(ULg),访问学者

2007.1-至今,  西北工业大学,副教授 

教育经历 Education Experience

1992.9-1996.7,西安理工大学,水利电力动力工程,本科生

1996.9-1999.4,西安理工大学,印刷工程(印刷机械),硕士生

1999.3-2003.12,西安交通大学,力学,博士生 

教育教学 Education And Teaching

1. 生命保障技术,本科生课程,48学时

2. 飞行器健康管理原理与技术,本科生课程,24学时

3. 飞行器救生技术,硕士生课程,40学时

4. 飞行器故障诊断与健康管理理论与应用,硕士生课程,40学时

5. 飞行器结构系统健康管理技术,硕士生课程,40学时 

招生信息 Admission Information

研究方向

1) 飞行器综合测试与健康管理

2) 飞行器结构/机构健康管理及演示实验

3)  无人机综合测试与控制

4) 飞行器安全性分析与设计 

硕士研究生招生学科

1.飞行器设计
2.飞行器控制与信息工程
3. 航空航天安全工程

4. 航空工程


荣誉获奖 Awards Information

      2019年度西北工业大学“三育人”先进个人

      2018年度西北工业大学校级优秀教学成果奖二等奖

2018年“创青春”全国大学生创业大赛国家级铜奖指导老师

2017年第四届粤港澳台大学生创新创业大赛亚军指导老师

2017(洛阳)直通硅谷创新创业大赛优秀创业导师

2016年度第二届江西省互联网+”大学生创新创业大赛(金奖)优秀指导老师

2016年度航空学院本科生最满意教师、学院保密工作先进个人、学院先进个人

航空学院2015年度,2016年度教学工作先进个人、科研工作先进个人

2013年度,2014年度,2015年度陕西省三秦人才奖

2010年省部级科技二等进步奖1项(排名第三)



科学研究 Scientific Research

2005CG010001

科研项目(国家自然科学基金青年项目)

8.0

2005-01-01到2005-12-31

2007DN010001

科研项目(国家863项目)

20.0

2007-08-01到2008-06-30

2008DN010001

科研项目(国家863项目)

20.0

2008-08-01到2009-07-30

2009DH010001

科研项目(国家863项目)

30.0

2009-08-01到2010-07-30

2010DH010001

科研项目(国家863项目)

20.0

2010-08-01到2011-06-30

2011DH010001

科研项目(国家863项目)

30.0

2011-08-01到2012-06-30

2012DH010001

科研项目(国家863项目)

60.0

2012-08-01到2013-06-30

2013DH010005

科研项目(国家863项目)

50.0

2013-08-01到2014-06-30

2014KC010161

健康管理系统试验研究(国家863项目)

60.0

2014-06-01到2015-09-30

2014MC010048

数据包络分析研究

10.2

2013-01-03到2014-05-30

2015KC010181

健康管理试验(国家863项目)

50.0

2015-08-01到2016-06-30

2016MC010064

连接匹配设计及试验研究

65.35

2016-06-20到2017-07-30

2016MC010119

机电系统通用自动化测试方法研究

20.0

2016-05-23到2017-11-01

2016ME010057

应急撤离人员轨迹测试与分析系统开发

35.0

2016-06-15到2017-12-31

2016ME010060

可用性评估指标研究项目

45.0

2016-06-15到2017-04-30

2017KE010217

长航时工业无人机及测绘系统产业化

10.0

2017-01-01到2018-12-31

2017MC010035

翼身连接开口密封带研发试验

48.0

2017-01-01到2017-12-30

2017MC010064

人机工效评估验证系统

30.0

2017-03-01到2017-12-01

2017MC010197

某人机功效仿真评价优化系统

84.9

2017-06-01到2019-06-01

2017MC100079

PHM软件验证设备

394.0

2017-09-10到2018-09-09

2018MC010229

陆战舱室人-机-环系统效能提升虚拟优化技术

19.8

2018-09-05到2018-12-30

2018ME010284

直升机驾驶舱人机工效试验与评估

35.0

2018-11-10到2018-12-30


学术成果 Academic Achievements

期刊论文/ Journals Articles

[1]  Wan, F.; Tran, M.-P.; Leblanc, C.; Béchet, E.; Plougonven, E.; Léonard, A.; Detrembleur, C.; Noels, L.; Thomassin, J.-M.; Nguyen, V.-D. Experimental and computational micro-mechanical investigations of compressive properties of polypropylene/multi-walled carbon nanotubes nanocomposite foams[J]. Mechanics of Materials, 2015, 91: 95-118. (WOS:000366774400008, EI: 20153501210245, DOI: 10.1016/j.mechmat.2015.07.004)

[2]  万方义,宋笔锋,许庆余,喻天翔.非线性裂纹转子系统碰摩故障时参变特性的研究 [J]. 机械强度,2006, 28(5):633-638. (EI20064910289870).

[3]  万方义,宋笔锋,许庆余,万婧,郝俊霞. 裂纹转子系统虚拟状态监测[J]. 机械科学与技术,200524(12):1469-1471.

[4]  Fangyi Wan, Qingyu Xu, Songtao Li, Vibration Analysis of Cracked Rotor–Sliding-Bearing System with Rotor-Stator Rubbing by Harmonic Wavelet Transform [J]. Journal of Sound and Vibration, 2004,271(3-5), 507~518. (WOS:000220284900002EI2004158110320,它引27) DOI: 10.1016/S0022-460X(03)00277-3

[5]  万方义,许庆余,宋笔锋,张小龙. 滑动轴承_转子系统非线性裂纹故障特征及其实验研究[J]. 应用力学学报200421(3): 3842. (EI2004478470817)

[6]  万方义,许庆余,李松涛.谐波小波变换在转子—轴承系统多故障监测中的应用[J]. 工程力学,200421(1):102~106. (EI04238201581)

[7]  万方义,许庆余,张小龙,许清源. 油膜支承转子系统动静件碰摩特征分析[J]. 应用力学学报,2003,20(2):1721. (EI03337594734)

[8]  万方义,华军,许庆余. 二维小波变换及其在机械碰摩故障诊断中的应用[J]. 机械强度,2002,24(2):168171. (EI02397117987)

[9]  万方义,许庆余,华军.非线性油膜支承裂纹转子动力特性分析[J].航空学报,2002,23(3):237240.

[10]      万方义,许庆余. 柔性递纸机构的动态设计方法研究[J].机械科学与技术.200120(3)239241. (EI01216514584)

 

[11]      Chunlin Zhang, Yuling Liu, Fangyi Wan et al. Multi-faults diagnosis of rolling bearings via adaptive customization of flexible analytical wavelet bases [J]. Chinese Journal of Aeronautics.  (DOI: https://doi.org/10.1016/j.cja.2019.03.014)

[12]      Chunlin Zhang ; Yuling Liu ; Fangyi Wan ; Binqiang Chen ; Jie Liu. Isolation and identification of compound faults in rotating machinery via windowed correlated kurtosis enhanced by modified empirical wavelet transform [J]. IEEE Access. (DOI: 10.1109/ ACCESS.2019.2924273)

[13]      Guo,Qing; Wan, Fangyi. Complete synchronization of the global coupled dynamical network induced by Poisson noises[J]. PLoS ONE, 2017, 12(12): e0188632. (WOS:000417337800032, DOI : 10.1371/journal.pone.0188632)

[14]      Guo,Qing; Guo, Peirong; Wan, Fangyi. Strong convergence in the pth-mean of an averaging principle for two-time-scales SPDEs with jumps[J]. Advances In Difference Equations, 2017. (WOS:000410027300002, DOI: 10.1186/s13662-017-1333-9)

[15]      于琦,万方义,郭英男,赵阳. 故障注入技术在飞行器非电系统中的应用进展[J]. 航空工程进展, 2013, 4(3):261-267.

[16]      秦增,万方义. 基于杆件柔性的舱门机构动力学特性影响分析[J]. 机械与电子,2013,(11): 15-19.

[17]      李鹏飞,万方义,崔卫民,宋笔锋. FBG传感器在飞行器结构健康监控中的可行性研究[J]. 机械强度, 2011, 33(4): 624-628.

[18]      郝俊霞,万方义,宋笔锋.基于小概率事件的飞行器结构健康监控[J].机械设计与制造, 2007, (12):87-88

[19]      张茂,万方义,宋笔锋. 基于小波包的碰摩信号能量特征辨识[J]. 机械设计与制造,2006, (9):143-145.

[20]      万婧,万方义,宋笔锋,冯蕴雯. 虚拟仪器技术在飞机燃油系统健康监控中的应用[J]. 机械设计与制造,2005(11):153-154.

[21]      Jun Hua, Fangyi Wan, Qingyu Xu. Numerical and Experimental Studies on Nonlinear Dynamic Behaviors of a Rotor-Fluid Film Bearing System with Squeeze Film Dampers [J]. Trans. ASME J. of Vibration and Acoustics. 2001,123(3),297302 (WOS:000170090400002).

 

[22]      尚柏林, 宋笔锋, 万方义. 光纤传感器在飞行器结构健康监测中的应用[J]. 光纤与电缆及其应用技术, 2008,(03):7-10

[23]      尚柏林, 宋笔锋, 万方义. 飞行器结构健康监控系统研究进展及关键技术[J]. 测控技术,2008, 27(7): 1-3

[24]      喻天翔,宋笔锋,万方义,冯蕴雯. 机械可靠性试验技术研究现状和展望[J].机械强度,2007, 29(2):256-263. EI20071910595182

[25]      喻天翔,宋笔锋,万方义,冯蕴雯. 零件多失效模式可靠度计算理论研究[J]. 机械强度,2006, 28(4):508-511. EI20064910289844

[26]      李松涛,许庆余,万方义等,宫密封不平衡子转子动力系统的稳定性与分岔[J]. 应用数学与力学,2003,24(11),11411150.

[27]      LI Song-taoXU Qing-yuWAN Fang-yi et al. Stability and Bifurcation of Unbalance Rotor/Labyrinth Seal System[J]. Applied Mathematics and Mechanics, 2003,24(11),12901301. (SCI三区:766RZ) (EI04148103033)

[28]      李松涛,许庆余,万方义,迷宫密封转子系统非线性动力稳定性的研究[J]. 应用力学学报,2002,19(2), 2730. (EI02417136211)

[29]      张劲夫,许庆余,万方义等,考虑摩擦的机械手逆动力学问题的研究[J].工程力学,2002, 19(4), 104108.

[30]      侯乔乔,崔卫民,喻天翔,万方义. 考虑弹性变形的开环机构运动精度分析[J]. 机械强度, 2013, 35(1): 111-115.



会议论文/ Conference Proceedings

[1]  Jiangni Lei,Fangyi Wan, Weimin Cui, Wenheng Li. Testability Modeling of Hydraulic System Based on Multi-signal Flow Model[C]. 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control (SDPC). p361-366, 16-18 Aug. 2017, Shanghai, China. (DOI: 10.1109/SDPC.2017.75)

[2]  Wenhao Zong; Fangyi Wan; Yishui Wei. Real-time monitoring for the actuator mechanism of the aileron[C]. 2017 Prognostics and System Health Management Conference (PHM- Harbin), p1-5, 9-12 July 2017, Harbin, China. (DOI: 10.1109/PHM.2017.8079309, EI: 20180204617715)

[3]  Wan Fangyi,Yu, Xingliang,Yu, Qi. Research on Optimal Sensor Placement for Aircraft Structural Health Management [C]. 2017 IEEE International Conference on Prognostics and Health Management, ICPHM 2017, p160-166, June 19 - 21, 2017, Dallas, TX, United states. (DOI: 10.1109/ICPHM.2017.7998322, EI: 20173604113002 )

[4]  YU xingliang, WAN Fangyi, GUO yingnan. Micromechanics Modeling of Skin Panel with Pitting Corrosion for Aircraft Structural Health Monitoring [C]. 2016 IEEE International Conference on Prognostics and Health Management, p1-8, June 20-22, 2016, Ottawa, ON, Canada. (DOI: 10.1109/ICPHM.2016.7542831, EI: 20163702788923)

[5]  YANG Hui, WAN Fangyi, CUI Weimin. Failure simulation and identification of shock absorber in carrier-based aircraft landing gear [C]. 2016 IEEE International Conference on Prognostics and Health Management, p1-6, June 20 -22, 2016, Ottawa, ON, Canada. (DOI: 10.1109/ICPHM.2016.7542833, EI: 20163702788925)

[6]  Yu Qi, Wan Fangyi, Guo Yingnan, Cui Weimin. A model-based fault injection system for aerocraft wing structure[C], 2014 International Conference on Prognostics and Health Management,p1-6, June 22-25, 2014, Cheney, WA, USA (DOI: 10.1109/ ICPHM. 2014. 7036378, EI: 20152100874751)

[7]  Wan Fangyi, Qin, Zeng. Virtual health monitoring system for wing structure[C].  Advanced Materials Research, 2013 International Conference on MEMS and Mechanics, MEMSM 2013, March 15-16, 2013, Wuhan, China. (DOI: 10.4028/www.scientific.net/AMR.705.534, EI: 20132816492577)

[8]  Guo Yingnan, Wan Fangyi. Research on Modal Parameters Identification of Wing Structures with NExT-ERA[C]. 2012 3rd International Conference on Applied Mechanics and Mechanical Engineering, ICAMME 2012, November 14- 15, 2012, Macau, China. Applied Mechanics and Materials, 249-259(201): 1025-1029. (DOI: 10.4028/ www.scientific.net/ AMM.249-250.1025,EI: 20130515974471)

[9]  Sun Mingming, Wan Fangyi, Qin Zeng. Health monitoring for propagating crack faults[C]. Proceedings of IEEE 2012 Prognostics and System Health Management Conference, PHM-2012. P1-6, May 23-25, 2012, Beijing, China. (DOI:10.1109/PHM.2012.6228803, EI: 20123815449178).

[10]      Wang Haifeng, Song Bifeng, WAN Fangyi. Research on fault pattern recognition for aircraft fuel system with its performance simulation[C]. 2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011 - Proceedings, p 4231-4235, 2011, August 8-10, 2011, Zhengzhou, China (DOI:10.1109/ AIMSEC.2011.6010100, EI: 20114014387121)

[11]      Hou Qiaoqiao, Cui Weimin,Yu Tianxiang, Wan  Fangyi, Song  Bifeng. An analysis of mechanism kinematics accuracy based on linear elastic [C]. Proceedings of 2011 9th International Conference on Reliability, Maintainability and Safety, p 404-408, ICRMS'2011.  June 12 - 15, 2011. Guiyang, China. (DOI: 10.1109/ICRMS.2011.5979302,EI: 20113714317607)

[12]      Wang Haifeng, Song Bifeng, WAN Fangyi. A simulation software of prognostics and health management for aircraft fuel system[C]. Proceedings of 2011 international conference on Quality, Reliability. Risk, Maintenance and Safety Engineer, DOI: 10.1109/ICQR2MSE.2011.5976660, June 17-19, 2011, Xi’an, China. EI20113614308962

[13]      Yingnan GUO, Fangyi WAN, Ling WU, Hanjie JIANG. Research of Structural Health Monitoring Based on Mode Analysis for UAV Wings[C]. 2011 Prognostics and system heath Management Conference. DOI: 10.1109/PHM.2011.5939521, May 23-25, Shenzhen, China. EI20113114201560.

[14]      Yun WU, FangYi WAN, MingMing SUN. Simulation on the faults mechanism of wing structure[C]. 2011 Prognostics and system heath Management Conference. P 1 - 7, May 23-25, Shenzhen, China. DOI: 10.1109/PHM.2011.5939522 ,EI20113114201561.

[15]      Xuhui CUI, Fangyi WAN, Mingming SUN. Virtual Damages Simulation of the Metallic Thermal Protection System Panel[C]. 2011 Prognostics and system heath Management Conference.  DOI: 10.1109/PHM.2011.5939523; May 24-25, 2011,Shenzhen, China. EI20113114201562.

[16]      Ting SHEN, Fangyi WAN, Bifeng SONG, Yun WU. Damage Location and Identification of the Wing Structure with Probabilistic Neural Networks[C]. 2011 Prognostics and system heath Management Conference. P1 - 6, May 23-25, Shenzhen, China. DOI: 10.1109/PHM.2011.5939524 ,EI20113114201563.

[17]      Weimin CUI, Fangyi WAN, TianxiangYU, Bifeng SONG. Optimization Design of Sensor Logic Structure for Safety Monitoring Systems[C]. 2011 Prognostics and system heath Management Conference. May 23-25, Shenzhen, China.

[18]      Ting SHEN, Fangyi WAN, Weimin CUI, Bifeng SONG. Application of Prognostic and Health Management Technology on Aircraft Fuel System[C]. 2010 Prognostics and system heath Management Conference. DOI:10.1109/PHM.2010.5413340, Jan 12-14, Macau, China.WOS:000283804700064, EI20101512847345.

[19]      Fangyi WAN, Weiping YANG, Ting SHEN, Bifeng SONG. Application of Harmonic Wavelet Transform on Aerocraft Structure Health Monitoring[C]. Asia Pacific Symposium on Safety 2009 Conference Proceedings :206-209. Oct.20-23 Osaka, Japan

[20]      Weimin CUI, Tianxiang YU, Fangyi WAN, Bifeng SONG. A New Method of Reliability Test and Assessment in High Reliability Design of Valves[C]. Asia Pacific Symposium on Safety 2009 Conference Proceedings :143-146. Oct.20-23 Osaka, Japan

[21]      Yu Tianxiang, Song Bifeng, Feng Yunwen, Wan Fangyi, Research on the Accelerated Reliability Growth Model (ARGM) in Constant Stress[C]. Asia Pacific Symposium on Safety 2005 Conference Proceedings :1991-1996. Nov.2-4 Shaoxing, China(WOS:000233802701126)

[22]      Yu Tianxiang, Song Bifeng, Wan Fangyi, Feng Yunwen. Simulation Validation of Reliability Growth Model for Multi-Systems Development Testing[C]. Asia Simulation Conf./ the 6th Int. Conf. on System Simulation and Scientific Computing, Conference Proceedings : 1299-1303. Oct. 24-27, 2005,Beijing, ChinaWOS:000234109200278, EI: 20142617855285

[23]      Wan Fang-yi, Song Bi-feng, Xu qing-yu, Yu Tian-xiang. Based on virtual instrument to monitor cracked rotor-bearing system by harmonic wavelet transform[C]. ISTM/2005: 6TH International Symposium On Test And Measurement, Vols 1-9, Conference Proceedings : 1166-1169, June 1-4, 2005, Dalian: WOS:000232030701042

[24]      万方义,许庆余. 裂纹转子-滑动轴承系统动静件碰摩故障的谐波小波分析[C]. 2002年全国振动工程技术及应用学术会议论文集,北京:111116.

[25]      F.Y.Wan, Q.Y.Xu, L.Zhang. Research on Dynamic Characteristics of Flexible Transfer Mechanism [C]. Proceedings of International Conference Advanced Problems in Vibration Theory and Application , June 2000, Xi’an707710.

专利及软件著作权/ Patents and software copyrights

[1]   结构PHM故障仿真软件[简称:故障注入软件]V1.0   登记号:2019SR0615904

[2]   结构PHM故障诊断软件[简称:故障诊断软件]V1.0    登记号:2019SR0614438

[3]   万方义 戴维 李文衡 崔卫民 郭英男 郭庆 李陶; 一种基于模块化组合涵道式旋翼无人机 (Modular combined duct type rotor wing unmanned aerial vehicle ), 申请号: CN201711110910.5

[4]  郭腾 崔卫民 万方义 雷江妮 李文衡 符超 秦大顺 王景卓;一种航空舱门锁变加载试验装置(Aerial cabin door lock variable loading test device),申请号:201810876642.6




学术文献 Academic Literature

1. Application of Prognostic and Health Management Technology on Aircraft Fuel System , IEEE,2010,,415-421 ,DOI:10.1109/PHM.2010.5413340, ISSN:
2. A Simulation Software of Prognostics and Health Management for Aircraft Fuel System , IEEE,2011,,492-496 ,DOI:10.1109/ICQR2MSE.2011.5976660, ISSN:
3. 基于小波包的碰摩信号能量特征辨识 , 2006,(9),143-145 ,DOI:10.3969/j.issn.1001-3997.2006.09.062, ISSN:1001-3997
4. 基于小概率事件的飞行器结构健康监控 , 2007,(12),87-88 ,DOI:10.3969/j.issn.1001-3997.2007.12.037, ISSN:1001-3997
5. 故障注入技术在飞行器非电系统中的应用进展 , 2013,4(3),261-267 ,DOI:10.3969/j.issn.1674-8190.2013.03.001, ISSN:1674-8190
6. FBG传感器在飞行器结构健康监控中的可行性研究 , 2011,33(4),624-628 ,DOI:, ISSN:1001-9669
7. 考虑弹性变形的开环机构运动精度分析 , 2013,35(1),111-115 ,DOI:, ISSN:1001-9669
8. 裂纹转子系统虚拟状态监测 , 2005,24(12),1469-1471,1501 ,DOI:10.3321/j.issn:1003-8728.2005.12.023, ISSN:1003-8728
9. Research on calculating the reliability of mechanical component with correlated failure modes , Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(4),508-511 ,DOI:, ISSN:10019669
10. A model-based fault injection system for aerocraft wing structure , Institute of Electrical and Electronics Engineers Inc.,2015, ,DOI:10.1109/ICPHM.2014.7036378, ISSN:9781479959426
11. Simulation validation of reliability growth model for multi-systems development testing , INTERNATIONAL ACADEMIC PUBLISHERS LTD,2005,,1299-1303 ,DOI:, ISSN:
12. Research on the characteristics of variable parameters in nonlinear cracked rotor system with rub-impact faults , Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(5),633-638 ,DOI:, ISSN:10019669
13. Research of structural health monitoring based on mode analysis for UAV wings , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.5939521, ISSN:9781424479511
14. Damage location and identification of the wing structure with Probabilistic Neural Networks , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.5939524, ISSN:9781424479511
15. Simulation on the faults mechanism of wing structure , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.5939522, ISSN:9781424479511
16. Health monitoring for propagating crack faults , IEEE Computer Society, 2001 L Street N.W., Suite 700, Washington, DC 20036-4928, United States,2012, ,DOI:10.1109/PHM.2012.6228803, ISSN:
17. Research on modal parameters identification of wing structures with NExT-ERA , Trans Tech Publications, P.O. Box 1254, Clausthal-Zellerfeld, D-38670, Germany,2013,249-250,1025-1029 ,DOI:10.4028/www.scientific.net/AMM.249-250.1025, ISSN:9783037855577
18. Virtual damages simulation of the metallic thermal protection system panel , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.5939523, ISSN:9781424479511
19. Present state and prospects for mechanical reliability testing technique study , Journal of Mechanical Strength, Zhengzou, Henan, China,2007,29(2),256-263 ,DOI:, ISSN:10019669
20. Research on accelerated reliability growth model (ARGM) in constant stress , SCIENCE PRESS BEIJING,2005,5,1991-1996 ,DOI:, ISSN:
21. Based on virtual instrument to monitor cracked rotor-bearing system by harmonic wavelet transform , INTERNATIONAL ACADEMIC PUBLISHERS LTD,2005,,1166-1169 ,DOI:, ISSN:
22. Virtual health monitoring system for wing structure , Trans Tech Publications Ltd, Kreuzstrasse 10, Zurich-Durnten, CH-8635, Switzerland,2013,705,534-539 ,DOI:10.4028/www.scientific.net/AMR.705.534, ISSN:9783037856994
23. Research on fault pattern recognition for aircraft fuel system with its performance simulation , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011,,4231-4235 ,DOI:10.1109/AIMSEC.2011.6010100, ISSN:9781457705366
24. An analysis of mechanism kinematics accuracy based on linear elastic , IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011,,404-408 ,DOI:10.1109/ICRMS.2011.5979302, ISSN:9781612846644
25. 滑动轴承-转子系统非线性裂纹故障特征及其实验研究 , 2004,21(3),38-42 ,DOI:10.3969/j.issn.1000-4939.2004.03.008, ISSN:1000-4939
26. 基于杆件柔性的舱门机构动力学特性影响分析 , 2013,(11),15-19 ,DOI:10.3969/j.issn.1001-2257.2013.11.004, ISSN:1001-2257
27. 飞行器结构健康监控系统研究进展及关键技术 , 2008,27(7),1-3,14 ,DOI:10.3969/j.issn.1000-8829.2008.07.001, ISSN:1000-8829
28. 机械可靠性试验技术研究现状和展望 , Journal of Mechanical Strength, Zhengzou, Henan, China,2007,29(2),256-263 ,DOI:10.3321/j.issn:1001-9669.2007.02.017, ISSN:1001-9669
29. 机械零件多失效模式相关可靠度算法研究 , Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(4),508-511 ,DOI:10.3321/j.issn:1001-9669.2006.04.008, ISSN:1001-9669
30. 非线性裂纹转子系统碰摩故障参变特性研究 , Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(5),633-638 ,DOI:10.3321/j.issn:1001-9669.2006.05.001, ISSN:1001-9669
31. 虚拟仪器技术在飞机燃油系统健康监控中的应用 , 2005,(11),153-154 ,DOI:10.3969/j.issn.1001-3997.2005.11.072, ISSN:1001-3997
32. 光纤传感器在飞行器结构健康监测中的应用 , 2008,(3),7-10 ,DOI:10.3969/j.issn.1006-1908.2008.03.003, ISSN:1006-1908
33. 基于自然激励技术与本征系统实现算法的飞行器结构健康监测研究 , 2012,(中国陕西西安),1 ,DOI:, ISSN:

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