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基于Gap度量的分布式航空发动机故障诊断方法(ICGNC增刊)

叶力豪1,许宇航1,郭黎2,姜斌3   

  1. 1. 南京航空航天大学
    2. 安徽工程大学电气工程学院
    3. 南京航空航天大学自动化学院
  • 收稿日期:2026-05-25 修回日期:2026-07-27 出版日期:2026-07-30 发布日期:2026-07-30
  • 通讯作者: 姜斌
  • 基金资助:
    国家自然科学基金;江苏省自然科学基金;中央基本科研业务费;直升机动力学全国重点实验室-开放基金;中国航空科学基金;中国航空学会青年科学家基;直升机动力学全国重点实验室专项基金

A Gap-Metric-Based Method for Distributed Aero-Engine Fault Diagnosis

  • Received:2026-05-25 Revised:2026-07-27 Online:2026-07-30 Published:2026-07-30
  • Supported by:
    National Natural Science Foundation of China

摘要: 航空装备的安全运行对保障飞行安全具有重要意义,而航空发动机作为其核心部件,其故障诊断研究具有重要价值。然而,航空发动机运行数据通常由不同机构分别持有,受保密性与隐私保护限制难以集中共享,形成数据孤岛问题。联邦学习通过在各节点本地训练模型并进行参数聚合,可在不共享原始数据的条件下实现全局模型训练,为分布式航空发动机数据环境下的故障诊断提供了一种有效途径。然而,多源航空发动机数据通常呈现非独立同分布特性,容易导致联邦模型性能下降。针对该问题,提出一种基于Gap度量的联邦学习故障诊断方法,通过Gap几何度量评估各客户端模型贡献,从而提升非均衡数据环境下的诊断性能。实验采用航空发动机数据集,并与独立训练、FedAvg和FedProx方法进行对比。结果表明,所提出方法在分布式数据环境下具有较好的诊断性能与稳定性。

关键词: 故障诊断, 分布式, Gap度量, 联邦学习, 航空发动机

Abstract: The safe operation of aviation equipment is essential for flight safety, and aero-engine fault diagnosis is of great importance because the engine is the core power unit of aircraft. In practical engineering scenarios, monitoring data of aero-engines are usually held by different institutions or test platforms. Due to confidentiality and privacy constraints, such data are difficult to collect centrally, resulting in a typical data-island problem. Federated learning provides a feasible way to train a global diagnostic model through local model updating and server-side parameter aggregation without sharing raw data. However, multi-source aero-engine data often follow non-independent and non-identically distributed patterns, which may reduce the performance and stability of conventional federated models. To address this problem, this paper proposes a Gap-metric-based federated aggregation method for distributed aero-engine fault diagnosis. The proposed method evaluates client contributions from the geometric structure of the feature space by considering intra-class compactness and inter-class separability, and then adaptively adjusts aggregation weights. Experiments on an aero-engine dataset, compared with Direct CNN, FedAvg, and FedProx, demonstrate that the proposed method achieves better diagnostic accuracy and stable training performance in distributed non-IID scenarios.

Key words: fault diagnosis, distributed, Gap metric, federated learning, aero-engine

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