南京航空航天大学智能材料与结构航空科技重点实验室
纸质出版:2008
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[1]王强,袁慎芳.航空结构健康监测的压电夹层设计[J].传感器与微系统,2008(07):72-74.
WANG Qiang, YUAN Shen-fang. PZTs layer technique for aerocraft structure health monitoring[J]. 2008, (7): 72-74.
[1]王强,袁慎芳.航空结构健康监测的压电夹层设计[J].传感器与微系统,2008(07):72-74. DOI: 10.13873/j.1000-97872008.07.006.
WANG Qiang, YUAN Shen-fang. PZTs layer technique for aerocraft structure health monitoring[J]. 2008, (7): 72-74. DOI: 10.13873/j.1000-97872008.07.006.
根据智能夹层思想和真实航空飞行器结构特点
研究了面向航空结构健康监测的压电夹层技术
并将该技术应用到了某无人机机翼盒段结构健康监测验证实验中。实验结果表明:压电夹层工作性能稳定
寿命长
压电元件的一致性良好
抗干扰、串扰能力较好
该技术对于结构健康监测技术实用化具有推动作用。
Based on the ideal of smart layer and the structure characterastic of aviation flyer
PZTs Layer technique for aerocraft structure health monitoring(SHM)is studied and used in the SHM validation experiment for a testbox of an UAV wing.The experiment result proves that the PZTs layer works stably and has long service life
and the PZTs have good consistency
low interference.All of these indicate that the PZTs layer technique is helpful for the practicality of SHM.
压电智能夹层及其特性分析 [J]. 唐守锋,熊克,李刚. 传感器技术 . 2005(07)
用于结构健康监测的智能夹层研究进展 [J]. 唐守锋,熊克,梁大开,李东升. 实验力学 . 2005(02)
基于主动监测技术的结构冲击损伤BP神经网络识别 [J]. 彭鸽,袁慎芳. 仪器仪表学报 . 2005(06)
Damage Localization on Two-Dimensional Structure Based on Wavelet Transform and Active Lamb Wave-Based Method [J] . Peng Ge,Yuan Shen Fang. Materials Science Forum . 2005 (475)
Detection of bolt load loss in hybrid composite/metal bolted connections [J] . Vincent Caccese,Richard Mewer,Senthil S. Vel. Engineering Structures . 2004 (7)
Health monitoring of a composite wingbox structure [J] . S Grondel,J Assaad,C Delebarre,E Moulin. Ultrasonics . 2004 (1)
Next generation structural health monitoring and its integration into aircraft design [J] . C. Boller. International Journal of Systems Science . 2000 (11)
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