空天多层异构结构压电导波传播特性仿真

doi:10.7527/S1000-6893.2025.32366

Abstract

Abstract:

To address the urgent demand for active guided wave damage monitoring of multilayer heterogeneous structures of aerospace vehicles under complex service conditions， we conduct a simulation study on piezoelectric guided waves in multilayer heterogeneous structures. By establishing a high-precision simulation model of multi-physics field coupling， the propagation characteristics and attenuation laws of guided waves in multilayer heterogeneous structures are revealed， which provides a design basis for the implementation of guided wave monitoring methods. Firstly， a multi-physics field coupling finite element model considering material attenuation characteristics is established， and the attenuation effect of viscoelastic layers on guided waves is simulated by Rayleigh damping. Secondly， the meshing strategy of multilayer heterogeneous structures is optimized to balance the calculation accuracy and efficiency. Experimental verification shows that the proposed method accurately simulates the attenuation behavior and propagation phase of guided waves， significantly improving the simulation accuracy. After introducing the damping model， the amplitude attenuation errors of S₀ and A₀ modes in the structure are reduced from 122.3% and 78.1% to 3.4% and 3.6% respectively； the mesh optimization reduces the element degrees of freedom by 66.6% while keeping the phase error within 0.6%. This research provides a high-precision simulation method and theoretical basis for damage monitoring of aerospace multilayer heterogeneous structures， which has important engineering value for ensuring the safe service of aerospace vehicles.

Key words: multilayer heterogeneous structures of aerospace vehicles, piezoelectric guided wave, finite element simulation, damping model, dispersion characteristics

CLC Number:

V214

Junxian SHEN, Yahui YANG, Shenfang YUAN. Simulation of piezoelectric guided wave propagation characteristics in multilayer heterogeneous structures for aerospace vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(21): 532366.

Figures/Tables 14

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References 30

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部件	6061铝合金	隔热瓦	应变隔离垫	耐高温硅橡胶
密度/（g·cm^-3）	2.75	0.350	0.150	1.18
弹性模量/GPa	70.0	0.283	0.005 23	1.00
泊松比	0.330	0.180	0.310	0.370

参数	相对介电常数/（10^-10 C·N^-1）		压电常数			柔度系数/（10^-12 m²·N^-1）
参数	ε₁₁	ε₃₃	d₃₁	d₃₃	d₁₅	s₁₁	s₁₂	s₁₃	s₃₃	s₅₅	s₆₆
数值	1 730	1 700	-1.71	3.74	5.84	16.4	-5.74	-7.22	18.8	4.75	4.43

导波模式	β/10^-6
导波模式	硅橡胶层	应变隔离垫
S₀模式	8.00	9.00
A₀模式	1.00	1.48

导波模式	信号来源	主承力-隔热瓦结构直达波幅值/V	主承力结构直达波幅值/V	直达波幅值衰减程度/%	误差/%
S₀	实验	1.933	2.521	-23.3
	引入阻尼前仿真	0.606	0.576	5.2	122.3
	引入阻尼后仿真	0.437	0.576	-24.1	3.4
A₀	实验	4.701	6.506	-27.7
	引入阻尼前仿真	1.413	1.505	-6.1	78.1
	引入阻尼后仿真	1.073	1.505	-28.7	3.6

导波模式	信号来源	相位/μs	误差/%
S₀	实验	63.467
	网格优化前	63.283	0.29
	网格优化后	63.367	0.11
A₀	实验	90.567
	网格优化前	89.067	1.70
	网格优化后	88.983	0.60

Simulation of piezoelectric guided wave propagation characteristics in multilayer heterogeneous structures for aerospace vehicles

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