航空功能涂层表界面完整性参数超声检测反演原理及其应用

doi:10.3901/JME.2023.08.001

机械工程学报 ›› 2023, Vol. 59 ›› Issue (8): 1-8.doi: 10.3901/JME.2023.08.001

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航空功能涂层表界面完整性参数超声检测反演原理及其应用

林莉¹, 马志远¹, 孙珞茗¹, 罗忠兵¹, 雷明凯²

1. 大连理工大学无损检测研究所大连 116024;
2. 大连理工大学材料科学与工程学院大连 116024

收稿日期:2022-01-15 修回日期:2022-10-28 出版日期:2023-04-20 发布日期:2023-06-16
通讯作者: 马志远,男,1986年出生,博士,副教授,硕士研究生导师。主要研究材料无损检测与评价。E-mail:zhiyma@dlut.edu.cn
作者简介:林莉,女,1970年出生,博士,教授,博士研究生导师。主要研究方向为材料无损检测、表征与评价。E-mail:linli@dlut.edu.cn
基金资助:
国家自然科学基金(52075078,51805072); 兴辽英才计划(XLYC1902082); 国家重点研发计划(2019YFA0708900)资助项目

Inversion Principle and Application of Ultrasonic Detecting Surface or Interface Integrity Parameters of Aviation Functional Coatings

LIN Li¹, MA Zhi-yuan¹, SUN Luo-ming¹, LUO Zhong-bing¹, LEI Ming-kai²

1. NDT & E Laboratory, Dalian University of Technology, Dalian 116024;
2. School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024

Received:2022-01-15 Revised:2022-10-28 Online:2023-04-20 Published:2023-06-16

摘要/Abstract

摘要： 热障涂层、吸波涂层等航空功能涂层缺陷、几何、结构、性能等表界面完整性参数的精准控制,对于兼顾、平衡其综合性能至关重要。提出航空功能涂层表界面完整性多参数的超声检测反演原理。原理基于超声波在涂层多界面结构中的作用机制,将模型正则化、数据正则化与灵敏度矩阵分析相结合,提出面向材料的特征检测信号正则化策略,并依据特征检测信号与表界面完整性多参数的相关性,发展了基于灵敏度矩阵(Sensitivity matrix, SM)的涂层表界面完整性多参数超声反演方法。以等离子体喷涂Al₂O₃涂层多个弹性常数的超声检测为例,阐述超声检测原理的实施效果。结果表明Al₂O₃涂层弹性常数C11、C13、C33、C44的反演结果分别为158.9 GPa、44.1 GPa、244.1 GPa、31.6 GPa,其中C44的反演结果与试验结果之间相对误差不超过4.5%。所提出的超声检测反演原理为基于传统“试错法”超声检测难以解决的多参数复杂无损检测问题提供有效解决途径。

关键词: 涂层, 表界面完整性, 超声检测, 参数反演, 灵敏度矩阵

Abstract: Accurate control of surface/interface integrity parameters included defect, geometry, structure, and property of thermal barrier coatings, absorbing coatings, and other aviation functional coatings is of great importance to balance their comprehensive performance. A new principle of ultrasonic detecting surface/interface integrity parameters of aviation functional coatings is presented.Based on the response mechanism of ultrasonic propagation in multi-interface coating structure, a material-oriented regularization strategy of characteristic detection signal is proposed, which includes model regularization, data regularization, and sensitivity matrix analysis. A sensitivity matrix based inversion method of ultrasonic detecting surface/interface integrity parameters is developed according to the correlation between characteristic detection signal and surface/interface integrity parameters. Taking the ultrasonic detection of elastic constants of plasma sprayed Al₂O₃ coating as an example, the validity of proposed ultrasonic detection principle is illustrated.Resultsshow that the inversed elastic constants C11, C13, C33, and C44 of Al₂O₃ coating are 158.9 GPa, 44.1 GPa, 244.1GPa, and 31.6 GPa, respectively, and the relative errors between them and the experimental results are less than 4.5 %. The proposed ultrasonic inversion principle provides an effective path for solving the complex ultrasonic non-destructive detecting problems with multiple unknown parameters which are difficult for traditional “trial-and-error” ultrasonic detecting methods.

Key words: coating, surface/interface integrity, ultrasonic detection, parameter inversion, sensitivity matrix

中图分类号:

TQ174

林莉, 马志远, 孙珞茗, 罗忠兵, 雷明凯. 航空功能涂层表界面完整性参数超声检测反演原理及其应用[J]. 机械工程学报, 2023, 59(8): 1-8.

LIN Li, MA Zhi-yuan, SUN Luo-ming, LUO Zhong-bing, LEI Ming-kai. Inversion Principle and Application of Ultrasonic Detecting Surface or Interface Integrity Parameters of Aviation Functional Coatings[J]. Journal of Mechanical Engineering, 2023, 59(8): 1-8.

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航空功能涂层表界面完整性参数超声检测反演原理及其应用

Inversion Principle and Application of Ultrasonic Detecting Surface or Interface Integrity Parameters of Aviation Functional Coatings

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