航空学报 > 2026, Vol. 47 Issue (15): 633304-633304   doi: 10.7527/S1000-6893.2026.33304

航空发动机智能控制与健康管理专栏

基于向导优化算法的航空发动机部件退化评估

张翔欣, 吕福慧, 邹毅, 黄向华()   

  1. 南京航空航天大学 能源与动力学院,南京 210016
  • 收稿日期:2025-12-30 修回日期:2026-01-26 接受日期:2026-02-28 出版日期:2026-03-24 发布日期:2026-03-16
  • 通讯作者: 黄向华 E-mail:xhhuang@nuaa.edu.cn
  • 基金资助:
    航空科学基金(2023L060052001)

Aero-engine component degradation assessment based on engine physics-guided optimization algorithm

Xiangxin ZHANG, Fuhui LYU, Yi ZOU, Xianghua HUANG()   

  1. College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • Received:2025-12-30 Revised:2026-01-26 Accepted:2026-02-28 Online:2026-03-24 Published:2026-03-16
  • Contact: Xianghua HUANG E-mail:xhhuang@nuaa.edu.cn
  • Supported by:
    Aeronautical Science Foundation of China(2023L060052001)

摘要:

为提升航空发动机视情维修的经济性、可靠性,需实现部件健康状态的精准量化评估。针对现有方法评估层次局限、精度不足且物理可解释性差的现状,提出一种基于向导优化(EPGO)算法的部件退化评估框架。该框架以退化因子高精度提取为目标,通过构建线性影响矩阵,将部件退化因子与多传感器响应的复杂关系转化为可计算的物理引导信号,动态生成发动机向导矢量,在复杂参数空间中实现精准、稳定的退化因子提取。为验证方法有效性,以涡轴发动机为研究对象,利用仿真数据与实际飞行数据验证算法核心机理与工程适用性。仿真数据验证结果表明:与传统粒子群优化算法相比,基于向导优化算法提取的部件退化因子平均均方根误差降低36.69%,平均决定系数提升29.75%。飞行数据验证结果表明:向导优化算法提取的退化因子所呈现的退化趋势,符合部件性能退化的物理机理,展现出向导优化算法在部件退化因子提取中具有良好的工程解释性与鲁棒性。研究为航空发动机部件退化评估提供了一种高精度、高可靠性的解决方案。

关键词: 航空发动机, 部件退化, 退化评估, 粒子群算法, 健康管理

Abstract:

To enhance the economic efficiency and reliability of condition-based maintenance for aero-engines, it is crucial to achieve accurate quantitative assessment of component health. Addressing the current limitations of existing methods—such as constrained assessment levels, insufficient accuracy, and weak physical interpretability—this paper proposes a component degradation assessment framework based on the Engine Physics-Guided Optimization (EPGO) algorithm. Aimed at high-precision extraction of degradation factors, the framework transforms the complex relationship between component degradation factors and multi-sensor responses into a computable, physics-guided signal by constructing a linear influence matrix. It dynamically generates an ‘engine-guide’ vector to achieve precise and stable extraction of degradation factors within the complex parameter space. To validate the effectiveness of the method, a turboshaft engine is selected as the research object, and both simulation data and actual flight data are employed to verify the core mechanism and engineering applicability of the algorithm. Verification results using simulation data show that, compared with the traditional particle swarm optimization algorithm, the EPGO-based method reduces the average root mean square error of extracted component degradation factors by 36.69% and increases the average correlation coefficient by 29.75%. Results from flight data indicate that the degradation trends revealed by the factors extracted via the EPGO algorithm align with the physical mechanisms of component performance degradation, demonstrating the algorithm’s good engineering interpretability and robustness in degradation factor extraction. This study provides a high-precision and highly reliable solution for aero-engine component degradation assessment.

Key words: aero-engine, component degradation, degradation assessment, particle swarm optimization, health management

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