A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum

The load spectrum serves as the foundation for the life analysis of aero-engine turbine disks. To enhance the accuracy of life assessments for turbine disks, this study compiles a time-varying load spectrum for turbine disks. Firstly, a surrogate model for transient processes at the critical points...

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Main Authors: Shunyu Yao, Xuming Niu, Zhigang Sun, Yingdong Song
Format: Article
Language:English
Published: MDPI AG 2025-05-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/12/5/423
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author Shunyu Yao
Xuming Niu
Zhigang Sun
Yingdong Song
author_facet Shunyu Yao
Xuming Niu
Zhigang Sun
Yingdong Song
author_sort Shunyu Yao
collection DOAJ
description The load spectrum serves as the foundation for the life analysis of aero-engine turbine disks. To enhance the accuracy of life assessments for turbine disks, this study compiles a time-varying load spectrum for turbine disks. Firstly, a surrogate model for transient processes at the critical points of turbine disks is established, enabling the rapid evaluation of the transient temperature and thermal stress at these points under complex loading histories. Secondly, a performance degradation model is established based on real engine test data, explicitly describing the general trend of performance degradation characteristics with respect to the cycle number and engine power. Finally, a time-varying load spectrum for turbine disks is compiled, considering both short-term transient processes and long-term performance degradation. The life of turbine disks at the fir-tree slot root and disk bore is assessed using the Manson–Coffin equation, Wilshire equation, and linear damage accumulation rule. The results indicate that neglecting transient processes leads to conservative life assessment results while neglecting performance degradation leads to dangerous life assessment results. Compared with traditional methods, the time-varying load spectrum significantly improves the accuracy and scientific nature of turbine disk life assessment.
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spelling doaj-art-1f0e34125de34d62864c4eb2b7d5cccc2025-08-20T03:47:49ZengMDPI AGAerospace2226-43102025-05-0112542310.3390/aerospace12050423A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load SpectrumShunyu Yao0Xuming Niu1Zhigang Sun2Yingdong Song3Key Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaKey Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaKey Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaKey Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaThe load spectrum serves as the foundation for the life analysis of aero-engine turbine disks. To enhance the accuracy of life assessments for turbine disks, this study compiles a time-varying load spectrum for turbine disks. Firstly, a surrogate model for transient processes at the critical points of turbine disks is established, enabling the rapid evaluation of the transient temperature and thermal stress at these points under complex loading histories. Secondly, a performance degradation model is established based on real engine test data, explicitly describing the general trend of performance degradation characteristics with respect to the cycle number and engine power. Finally, a time-varying load spectrum for turbine disks is compiled, considering both short-term transient processes and long-term performance degradation. The life of turbine disks at the fir-tree slot root and disk bore is assessed using the Manson–Coffin equation, Wilshire equation, and linear damage accumulation rule. The results indicate that neglecting transient processes leads to conservative life assessment results while neglecting performance degradation leads to dangerous life assessment results. Compared with traditional methods, the time-varying load spectrum significantly improves the accuracy and scientific nature of turbine disk life assessment.https://www.mdpi.com/2226-4310/12/5/423time-varying load spectrumaero-engine turbine disklife assessmenttransient processperformance degradation
spellingShingle Shunyu Yao
Xuming Niu
Zhigang Sun
Yingdong Song
A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
Aerospace
time-varying load spectrum
aero-engine turbine disk
life assessment
transient process
performance degradation
title A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
title_full A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
title_fullStr A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
title_full_unstemmed A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
title_short A Method for the Life Assessment of Aero-Engine Turbine Disks Based on a Time-Varying Load Spectrum
title_sort method for the life assessment of aero engine turbine disks based on a time varying load spectrum
topic time-varying load spectrum
aero-engine turbine disk
life assessment
transient process
performance degradation
url https://www.mdpi.com/2226-4310/12/5/423
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