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基于超声导波的航空发动机薄壁导管应力测量

Stress measurement of aero-engine thin-walled catheter based on ultrasonic guided wave.

作者信息

Ma Huiping, Ding Yibo, Liu Yongmeng

机构信息

Center of Ultra-precision Optoelectronic Instrument Engineering, Harbin Institute of Technology, Harbin 150080, China.

Key Lab of Ultra-precision Intelligent Instrumentation Engineering (Harbin Institute of Technology), Ministry of Industry and Information Technology, Harbin 150080, China.

出版信息

Rev Sci Instrum. 2023 Oct 1;94(10). doi: 10.1063/5.0165170.

Abstract

A pipeline system made of catheters is used for liquid-gas transportation in aero-engines. It is important to measure the residual stresses, such as the assembly stress in this system, as they influence performance and lifetime. Compared to other testing techniques, ultrasonic measurement methods based on acoustic-elastic effects can better solve problems. For the above requirements, this paper researches an aero-engine thin-wall catheter's assembly stress measurement method based on ultrasonic guided waves's acoustic, elastic effect. The propagation and dispersion characteristics of guided ultrasonic waves in the catheter were studied. Then, the excitation frequency, guided wave mode, and single-mode excitation mode of the simulation model were determined. Next, a finite element simulation model was established for simulation experiments. In order to reduce the influence of sampling rate and working environment noise on the measurement accuracy of assembly stress, the ultrasonic guided wave signal was processed by the wavelet threshold method. A good noise reduction effect was obtained by determining the wavelet base and the number of decomposition layers. Finally, an experimental platform was built to measure the assembly stress of thin-walled catheters. The maximum measurement error of the assembly stress of a thin-walled catheter was 21.1 MPa, which verified the feasibility of the measurement method. This study provides a promising method for accurately measuring the assembly stress of thin-walled catheters in aero-engines.

摘要

一种由导管制成的管道系统用于航空发动机中的液气传输。测量残余应力很重要,比如该系统中的装配应力,因为它们会影响性能和寿命。与其他测试技术相比,基于声弹性效应的超声测量方法能更好地解决问题。针对上述需求,本文研究了一种基于超声导波声弹性效应的航空发动机薄壁导管装配应力测量方法。研究了导波在导管中的传播和频散特性。然后,确定了仿真模型的激励频率、导波模式和单模激励模式。接下来,建立了有限元仿真模型进行仿真实验。为了降低采样率和工作环境噪声对装配应力测量精度的影响,采用小波阈值法对超声导波信号进行处理。通过确定小波基和分解层数,获得了良好的降噪效果。最后,搭建了实验平台来测量薄壁导管的装配应力。薄壁导管装配应力的最大测量误差为21.1MPa,验证了该测量方法的可行性。本研究为准确测量航空发动机薄壁导管的装配应力提供了一种很有前景的方法。

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