基于水浸超声技术的涡轮叶片裂纹损伤检测方法研究OA
Research on Crack Damage Detection Method for Turbine Blades Based on Immersion Ultrasonic Technology
针对某型航空发动机涂层涡轮叶片表面微裂纹损伤难以检测的问题,提出一种基于一维卷积神经网络与水浸超声技术的涡轮叶片裂纹损伤检测方法.分析检测过程中的异常信号特性,设计包含所有特征映射的新型连接结构搭建缺陷一维卷积检测网络,建立了适用于涡轮叶片水浸超声信号的缺陷特征自适应提取模块.针对实际检测场景损伤样本稀缺的情况,通过数据增强方法增加伪样本,提升网络模型对涡轮叶片检测样本的检测精度.研发了涡轮叶片专用工装并搭建了超声水浸检测实验平台,验证并优化所提检测模型.实验结果表明,涡轮叶片损伤检测精度为96.8%,优于常用检测模型,为涂层涡轮叶片表面微裂纹检测提供了一种新方法.
To address the difficulty in detecting surface micro-crack damage on coated turbine blades of a certain aero-engine,a crack detection method is proposed based on a one-dimensional convolutional neural network(1D-CNN)and water immersion ultrasonic testing.By analyzing the characteristics of abnormal signals during detection,a novel defect detection network is constructed using a 1D-CNN architecture that incorporates all feature mappings,along with an adaptive defect feature extraction module tailored for water immersion ultrasonic signals of turbine blades.To overcome the scarcity of real damage samples in practical detection scenarios,a data augmentation approach is employed to generate synthetic samples,thereby improving the detection accuracy of the network model for turbine blade inspection.Specialized tooling for turbine blades is developed,and an experimental platform for water immersion ultrasonic testing is established to validate and optimize the proposed detection model.Experimental results demonstrate that the proposed method achieves a detection accuracy of 96.8%for turbine blade damage,outperforming conventional detection models.This provides a novel solution for detecting surface micro-cracks in coated turbine blades.
张浩喆;黄刘伟;冯萍;何喜;方雨婷;陈振华;卢超;蔡苏阳
中国航发动力股份有限公司,西安 710021南昌航空大学无损检测技术教育部重点实验室,南昌 330063中国航发动力股份有限公司,西安 710021中国航发动力股份有限公司,西安 710021南昌航空大学无损检测技术教育部重点实验室,南昌 330063南昌航空大学无损检测技术教育部重点实验室,南昌 330063南昌航空大学无损检测技术教育部重点实验室,南昌 330063南昌航空大学无损检测技术教育部重点实验室,南昌 330063
矿业与冶金
水浸超声涡轮叶片深度学习微裂纹损伤无损检测
immersion ultrasoundturbine bladedeep learningmicrocrack damagenon-destructive testing
《机电工程技术》 2026 (4)
14-19,6
国家自然科学基金(12464059)航发技术委托项目(HFDL-KYZ-JSZ-202308-40)南昌航空大学博士启动基金(EA202408166)江西省早期人才项目(20244BCE52109)
评论