Construction of PZT-5H mechano-electric model based on strain rate dependence and its numerical simulation in overload igniter application

被引:11
作者
Wang, Ruizhi [1 ]
Tang, Enling [1 ,2 ]
Yang, Guolai [1 ]
Sun, Quanzhao [1 ]
Han, Yafei [2 ]
Chen, Chuang [2 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
[2] Shenyang Ligong Univ, Key Lab Transient Phys Mech & Energy Convers Mat, Shenyang 110159, Liaoning, Peoples R China
基金
中国国家自然科学基金;
关键词
PZT-5H; Dynamic mechano-electric model; Strain rate; Overload igniter; CONSTITUTIVE MODEL; BEHAVIOR;
D O I
10.1016/j.mechmat.2021.103837
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Although the force-electricity relationship of piezoelectric ceramics under pulse stress is found to be nonlinear, there is still lacking a reliable model describing this relationship. To bridge this research gap, the mechanical and electrical responses of PZT-5H (Pb1?0[Zr0?49Ti0?46(Nb0?25Sb0.75)0.05]1.0O3) under different strain rates were investigated through uniaxial compression tests and split-Hopkinson pressure bar (SHPB) experiments with an additional electrical output measurement system. With reference to the nonlinear viscoelastic constitutive equation and the piezoelectric equation, a PZT-5H mechano-electric model considering the strain rate effects was built based on the experimental data. The incremental form of the mechano-electric model was established based on the Piola-Kirchhoff stress tensor and Green strain tensor theory. The model was numerically simulated with a user-defined material subroutine in the explicit finite element software ABAQUS. The accuracy of the material subroutine was verified with finite element models of the uniaxial quasi-static compression and the high strain rate SHPB tests. The finite element simulation results were verified with the experimental results, and the two agreed well. The material subroutine was then adopted to predict the mechanical and electrical response of the piezoelectric ceramics inside the overload igniter during projectile launch and impact. The analysis results show that the overload igniter can be stably activated within 200 ?s under the launch overload and successfully ignited within 5 ?s at speed as low as 50 m/s under the impact overload.
引用
收藏
页数:13
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