欢迎登录材料期刊网

材料期刊网

高级检索

本文针对宽频带超声换能器的设计,对采用非一致层厚的多层铁电单晶结构的特性进行了研究和优化.建立了基于复材料参数的多层压电结构的理论模型,运用模拟退火全局优化算法对多层铌镁酸铅-钛酸铅结构的层厚进行了优化,并分析了各层厚度变化对多层压电结构频率响应特性的影响.理论仿真和实验结果证明非一致层厚的多层铁电单晶结构能够用于设计和制造高性能宽频带超声换能器.

参考文献

[1] Goldberg R.L.;Smith S.W. .Multilayer piezoelectric ceramics for two-dimensional arraytransducers[J].IEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control,1994(5):761-771.
[2] Hossack J.A.;Auld B.A. .Improving the characteristics of a transducer using multiple piezoelectric layers[J].IEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control,1993(2):131-139.
[3] Greenstein M.;Kumar U. .Multilayer piezoelectric resonators for medical ultrasoundtransducers[J].IEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control,1996(4):620-622.
[4] Aneela Abrar;Sandy Cochran .Mathematical Optimization of Multilayer Piezoelectric Devices with Nonnuniform Layers by Simulated Annealing[J].IEEE Transactions on Ultrasonics,Ferroelectrics,and Frequency Control,2007,54:1920-1929.
[5] Z.Wu;A.Abrar;G.McRobbie.Implementation of Multilayer Ultrasonic Transducer Structures with Optimized Non-Uniform Layer Thicknesses[A].:1292-1295.
[6] W.P.Mason .Equivalent Electromechanical Representation of Trapped Energy Transducers[J].Proceedings of the IEEE,1969,57(10):1723-1734.
[7] Stewart Sherrit;Sean P.Leary;Benjamin P.Dolgin.Comparison of the Mason and KLM Equivalent Circuits for Piezoelectric Resonators in the Thickness Mode[A].,1999:921-926.
[8] Kervel;Thijssen.A Calculation Scheme for the Optimum Design of Ultrasonic Transducers[J].Ultrasonics,1983:134-140.
[9] Dong, Y.,Wu, Z.,Hu, H.,Wu, B.,Xu, G. .A novel method for characterization of piezoelectric material parameters by simulated annealing optimization[J].IEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control,2010(12):2613-2615.
[10] Ewart;McLaughlin.Mechanical and Electromechanical Properties of PMN-PT Single Crystals for Naval Sonar Transducers[A].,2007:553-556.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%