考虑维修干扰的涡轴发动机气路性能预测
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作者单位:

1南京航空航天大学民航学院,南京 211106;2中国人民解放军93145部队,上海 200231

作者简介:

通讯作者:

蔡景,男,副教授,E-mail:caijing@nuaa.edu.cn。

中图分类号:

V263

基金项目:

航空科学基金(2024L042052001)。


Prediction for Gas Path Performance of Turboshaft Engines Considering Maintenance Interference
Author:
Affiliation:

College of Civil Aviation, Nanjing University of Aeronautics & Astronautics, Nanjing 211106,China;2Unit 93145 of the Chinese People’s Liberation Army,Shanghai 200231,China

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    摘要:

    针对涡轴发动机性能建模过程中存在的工况复杂、稳态与瞬态数据难以有效区分、维修活动干扰性能退化建模等关键技术难题,提出一种基于试车数据的涡轴发动机气路性能预测方法。首先,采用Pearson相关性分析对试车数据进行降维处理,剔除冗余信息以提升建模效率;其次,通过构建滑动窗口结合变异系数阈值判定准则,实现试车数据中稳态数据的精准提取,解决稳态与瞬态数据混淆的问题;然后,基于相对退化量分析识别数据中维修活动的发生时间点,构建性能退化分段建模策略,有效排除维修活动对退化建模的干扰;最后,利用随机森林算法拟合发动机气路参数间的非线性多耦合关系,完成涡轴发动机气路性能的精准预测。为验证所提方法的有效性,采用3段试车数据进行重复验证,结果表明,各预测指标的平均相对误差均小于1.09%。该方法可有效实现涡轴发动机气路性能退化趋势的精准预测,为发动机故障诊断、健康状态监测及性能预测等工程实践提供可靠的技术支撑。

    Abstract:

    To address the key technical challenges in turboshaft engine performance modeling, such as complex operating conditions, difficulty in effectively distinguishing steady-state and transient data, and interference of maintenance activities on degradation modeling, a gas path performance prediction method for turboshaft engines based on test run data is proposed. First, Pearson correlation analysis is adopted to reduce the dimensionality of test run data, eliminating redundant information to improve modeling efficiency. Second, a sliding window combined with a coefficient of variation threshold criterion is constructed to accurately extract steady-state data from test run data, solving the problem of confusion between steady-state and transient data. Third, based on relative degradation analysis, the occurrence time of maintenance activities in the data is identified, and a segmented modeling strategy for performance degradation is established to effectively eliminate the interference of maintenance activities on degradation modeling. Finally, the random forest algorithm is used to fit the nonlinear multi-coupling relationship between engine gas path parameters, so as to achieve accurate prediction of turboshaft engine gas path performance. To verify the effectiveness of the proposed method, three segments of test run data are used for repeated verification. The results show that the average relative error of each prediction index is less than 1.09%. This method can effectively realize the accurate prediction of the degradation trend of turboshaft engine gas path performance, and provide reliable technical support for engineering practices such as engine fault diagnosis, health condition monitoring and performance prediction.

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邱朝阳,蔡景,陈颖.考虑维修干扰的涡轴发动机气路性能预测[J].南京航空航天大学学报,2026,58(3):615-626

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  • 收稿日期:2025-12-16
  • 最后修改日期:2026-03-20
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  • 在线发布日期: 2026-06-18
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