电气工程学报 ›› 2023, Vol. 18 ›› Issue (4): 188-198.doi: 10.11985/2023.04.021

• 电力电子与电力传动 • 上一篇    下一篇

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飞机主电源系统关键器件健康状态评估研究

李小宁1(), 高朝晖1(), 王爽2, 汤孝3, 李一卓1   

  1. 1.西北工业大学自动化学院 西安 710129
    2.中国商飞上海飞机设计研究院 上海 201210
    3.中航长沙设计研究院有限公司 长沙 410014
  • 收稿日期:2022-11-05 修回日期:2023-07-05 出版日期:2023-12-25 发布日期:2024-01-12
  • 作者简介:李小宁,女,1997年生,硕士研究生。主要研究方向为飞机电力系统健康管理。E-mail:2020262627@mail.nwpu.edu.cn
    高朝晖,女,1971年生,博士,副教授,硕士研究生导师。主要研究方向为电力电子及飞机电力系统仿真、飞机电力系统健康管理。E-mail:holly@nwpu.edu.cn

Research on Health Assessment Method of Key Components in Aircraft Main Power System

LI Xiaoning1(), GAO Zhaohui1(), WANG Shuang2, TANG Xiao3, LI Yizhuo1   

  1. 1. School of Automation, Northwestern Polytechnical University, Xi’an 710129
    2. COMAC Shanghai Aircraft Design and Research Institute, Shanghai 201210
    3. AVIC Changsha Design and Research Institute, Changsha 410014
  • Received:2022-11-05 Revised:2023-07-05 Online:2023-12-25 Published:2024-01-12

摘要:

采用数据驱动的方法实现飞机主电源系统关键器件的健康状态评估。选取飞机主电源系统中故障率较高的旋转整流器整流二极管和调压器功率(Metal oxide semiconductor field effect transistor, MOSFET)管作为系统关键器件,并分析确定了关键器件的老化特性;利用仿真数据筛选出励磁机的励磁电压平均值和励磁电流平均值作为表征系统关键器件健康状态的电源系统特征变量;采用主成分分析法对系统特征变量数据进行解耦,得到可以分别表征两个关键器件健康状态的特征参数;利用高斯混合模型建立了关键器件的健康基准模型,并计算系统老化模型与健康基准模型的马氏距离;将马氏距离结果经过K-means聚类分析得到包含关键器件健康状态等级信息的训练样本集数据,将样本集数据经过神经网络训练得到系统关键器件的健康状态评估分类函数。采用蒙特卡罗仿真获取大量数据对分类函数进行验证,关键器件不同健康状态等级数据的原始分类和分类函数评估结果的匹配度达到90%以上,说明了该健康评估方法的有效性。

关键词: 飞机主电源系统, 健康状态评估, 主成分分析, K-means聚类, BP(Back propagation)神经网络

Abstract:

Data-driven method is used to evaluate the health status of the key components in the aircraft main power system. The rectifier diodes in the rotating rectifier and the metal oxide semiconductor field effect transistor(MOSFET) in the voltage regulator are selected as the key components of the aircraft main power system with high failure rate, and their aging characteristics are analyzed and determined. Using the simulation data, the average excitation voltage and the average excitation current of the exciter are selected as the characteristic variables of the power system to represent the health status of the key components of the system. Principal component analysis(PCA) is used to decouple the data of system characteristic variables, and the characteristic parameters which can represent the aging status of two key components are obtained. The Gaussian mixture model is used to establish the health reference model of key components, and the Mahalanobis distance between the system aging model and the health reference model is calculated. The Mahalanobis distance data is processed by K-means clustering analysis to obtain the data training sample set containing the health status level information of key components, and neural network is used to train the data of the sample set to obtain the health status evaluation classification functions of the key components of the system. Monte Carlo simulation is used to obtain a large amount of data to verify the classification function. The matching degree between the original data and the evaluation results of the classification function of different health status level data of key components is more than 90%, which shows the effectiveness of this health assessment method.

Key words: Aircraft main power system, health assessment, principal component analysis, K-means clustering, back propagation neural network

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