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航空发动机进气支板裂纹可解释智能声纹诊断-“AI+空天科学”专刊

丁宝庆1,曹智1,肖林海1,王萌2,杨明绥3,王诗彬1,陈雪峰1   

  1. 1. 西安交通大学
    2. 中国航发沈阳发动机研究所
    3. 沈阳发动机设计研究所
  • 收稿日期:2026-02-10 修回日期:2026-06-24 发布日期:2026-06-26
  • 通讯作者: 王诗彬
  • 基金资助:
    航空发动机封严/轮盘界面诱导的振动超标快变时频溯源与控制;航空发动机轴间轴承早期损伤快变特性表征与瞬时频率诊断方法研究;航空发动机进气支板裂纹故障高精准定位识别方法研究

Interpretable intelligent acoustic diagnosis for cracks in intake plates of aero-engine

  • Received:2026-02-10 Revised:2026-06-24 Published:2026-06-26
  • Contact: Shi-Bin WANG

摘要: 航空发动机原位检测是当前定期维修体系下识别早期潜在故障、保障运行安全的关键技术,也是未来视情维修体系下实现精准预测、优化维护决策的重要支撑手段。人工智能赋能的原位检测近来受到学术及工业界广泛关注,然而深度学习“黑箱模型”使得在航空领域应用面临“想用而不敢用”困境。面向进气支板裂纹故障高精准检测的迫切需求,提出可解释智能声纹诊断方法。融合支板裂纹声纹模态响应先验,构建多尺度稀疏表示模型,并将求解优化过程映射为网络结构,使得网络构造有据可依;引入基于对抗训练的异常检测框架,并结合多尺度特征重构开展事后可解释分析,从而实现诊断结论有迹可循。在此基础上,提出时频增强方法提取表征裂纹的敏感声纹特征参数,实现网络输出结果的二次验证,共同助力解决工程应用时虚警与漏检并存问题。最后,通过某型航空发动机进气支板原位检测工程实测数据,验证了提出的可解释智能声纹识别方法在进气支板裂纹故障诊断中的有效性与工程可用性,为进气支板裂纹原位高精准检测提供技术支撑。

关键词: 航空发动机, 进气支板裂纹, 声纹诊断, 可解释异常检测, 稀疏展开网络, 时频增强

Abstract: In-situ inspection of aero-engines is a key technology for identifying potential early faults and ensuring operational safety under the current scheduled maintenance regime. It also serves as a crucial support mechanism for achieving precise prediction and optimizing maintenance decisions within the future condition-based maintenance framework. While AI-enabled in-situ inspection has recently garnered widespread attention from both academia and industry, the “black-box” nature of deep learning models has created a dilemma in aviation applications where operators are “willing but hesitant to deploy.” Addressing the urgent demand for high-precision detection of Intake plates cracks, this paper proposes an interpretable intelligent acoustic signature diagnosis method. By fusing prior knowledge of the modal response of strut crack acoustic signatures, a multi-scale sparse representation model is constructed. The optimization process is then mapped into a network architecture, ensuring the network construction is theoretically grounded. Furthermore, an anomaly detection framework based on adversarial training is introduced, combined with multi-scale feature reconstruction to conduct post-hoc interpretable analysis, making diagnostic conclusions traceable. Based on this, a time-frequency enhancement method is proposed to extract sensitive acoustic signature parameters characterizing cracks, realizing a “secondary verification” of the network outputs. This jointly addresses the coexistence of false alarms and missed detections in engineering applications. Finally, field measurement data from the in-situ inspection of a certain type of aero-engine inlet strut validates the effectiveness and engineering applicability of the proposed method, providing technical support for high-precision in-situ detection of intake plates cracks.

Key words: aero-engine, intake plates crack, acoustic signature diagnosis, interpretable anomaly detection, sparse unrolling network, time-frequency enhancement

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