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Journal of Materials Engineering and Performance

Published in:

15-10-2019

Fatigue Failure Analysis and Life Prediction of Aeroengine Compressor Components

Authors: Yajun Chen, Xuntao Zhang, Fusheng Wang, Xiaoxiao Song, Ailun Wang, Haipeng Song

Published in: Journal of Materials Engineering and Performance | Issue 10/2019

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Abstract

In order to study the fatigue properties and fatigue life prediction model of aeroengine compressor components made of Ni-based superalloy GH4169 under simplified service condition, creep–fatigue test and fatigue test under different stresses at 650 °C were performed. The morphology of fatigue damage was analyzed. A modified Bannantine life prediction model which considers fatigue damage as the foundation and creep–fatigue damage factor as the correction was suggested and explained the different failure contributions between fatigue damage and creep damage, which leads to less logarithmic relative error compared with common method. The finite element analyses of compressor’s mechanical properties were conducted by the software ABAQUS to find failure position, and mechanical parameters of failure location were obtained by statistical analysis. The results indicated that the fatigue life of compressor components was predicted by optimized model, which exhibited a good agreement with the experiment data, which has important reference value for the engineering application of aeroengine compressors.

previous article Very High-Cycle Fatigue Properties and Residual Stress Relaxation of Micro-shot-Peened EA4T Axle Steel

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Title: Fatigue Failure Analysis and Life Prediction of Aeroengine Compressor Components
Authors: Yajun Chen
Xuntao Zhang
Fusheng Wang
Xiaoxiao Song
Ailun Wang
Haipeng Song
Publication date: 15-10-2019
Publisher: Springer US
Published in: Journal of Materials Engineering and Performance / Issue 10/2019
Print ISSN: 1059-9495
Electronic ISSN: 1544-1024
DOI: https://doi.org/10.1007/s11665-019-04370-y

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