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复合材料盒段冲击损伤的成像优化 被引量:1

Optimization of impact damage imaging for composite box segments
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摘要 基于压电传感器的Lamb波损伤成像方法已广泛应用于复合材料结构的损伤识别与定位中,但激励传感信号在实际检测中往往会存在电磁干扰等异常扰动,从而出现漏检或者损伤的误报。针对这一问题,研究了损伤概率成像优化方法,改进了基于能量变化的损伤因子。在复合材料盒段结构的冲击损伤现场检测中,采用传统方法的概率成像算法的损伤定位精度为68%,而采用文中改进的概率成像算法的损伤定位精度为82%。 The Lamb wave damage imaging method based on piezoelectric sensor has been widely used in the damage identification and location of composite structures.However,due to the abnormal disturbance such as electromagnetic interference in the actual detection of the excitation sensor signal,there often occur undetected faults or false alarms of damage.Aiming at this problem,the damage probability imaging optimization method is studied,and the damage factor based on energy change is improved,which can have strong anti-interference ability in the field.In the field test of impact damage of composite stiffened wing box structure,the accuracy of damage location is 68% by using the traditional probability imaging method,and 82% by using the improved probability imaging algorithm in this paper.
作者 张华 张倩昀 宁宁 ZHANG Hua;ZHANG Qianyun;NING Ning(Aircraft Strength Research Institute,Xi’an 710065,China;College of Electronic Engineering,Xi’an Aeronautical University,Xi’an 710077,China)
出处 《无损检测》 CAS 2021年第4期20-22,81,共4页 Nondestructive Testing
关键词 压电传感器 复合材料 LAMB波 损伤概率成像 piezoelectric sensor composite material Lamb wave damage probability imaging
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  • 1刘增华,樊军伟,何存富,吴斌.基于概率损伤算法的复合材料板空气耦合Lamb波扫描成像[J].复合材料学报,2015,32(1):227-235. 被引量:32
  • 2Shenfang YUAN, Yingdi XU and Ge PENGThe Smart Materials & Structures Aeronautic Key Laboratory, Nanjing University of Aeronautic and Astronautic, Nanjing 210016, China.New Developments in Structural Health Monitoring Based on Diagnostic Lamb Wave[J].Journal of Materials Science & Technology,2004,20(5):490-496. 被引量:9
  • 3杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1019
  • 4张纪奎,郦正能,程小全,王军.复合材料整体结构在大型民机上的应用[J].航空制造技术,2007,0(9):38-38. 被引量:22
  • 5袁慎芳.结构健康监测.北京:国防工业出版社,2007:1-23.
  • 6Boller C. Next generation structural health monitoring and its integration into aircraft design. International Jour- nal of Systems Science, 2000, 31(11) .. 1333-1349.
  • 7Yuan S, Xu Y, Peng G. New developments in structuralhealth monitoring based on diagnostic Lamb wave. Journal of Material Science and Technology, 2004, 20(5): 490- 496.
  • 8Dertg M X, Warlg Q, Giurgiut:u V. Structural health mo- nitoring using active sensors and wavelet transforms. Pro- ceedings of the SHE, Smart Structures and Materials, 1999.
  • 9Jeong H, Jang Y S. Wavelet analysis of plate wave propa- gation in composite laminates. Composite Structures, 2000, 49(4): 443-450.
  • 10ViktorovI A. Rayleigh and Lamb waves. New York: Ple- num Press, 1967: 67-117.

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