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HomeKey Engineering MaterialsKey Engineering Materials Vol. 891Fatigue Life of Ni-Based Single Crystal...

Fatigue Life of Ni-Based Single Crystal Super-Alloy Specimen with Single Hole

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Abstract:

A method of predicting the fatigue life under multiaxis loads based on the Paris law and EIFS was proposed. And the fatigue life under different loading stress and stress ratio were investigated. The results show that when the loading stress increased from 450~800 MPa, the fatigue life decreased from 6762379 to 10056, as well as when the stress ratio increased from 0.1~1, the fatigue life increased from 6762379 to 14932368. It was validated by test eventually. And the fatigue life model presented here agrees well with test results. It is significant to the prediction of turbine of Ni-based single crystal super-alloy material with filming hole.

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Periodical:

Key Engineering Materials (Volume 891)

Pages:

10-16

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.891.10

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Online since:

July 2021

Authors:

Xiang Zhen Xue*, Zhi Xun Wen, Wen Xian Li

Keywords:

Crack Propagation, Equivalent Initial Fatigue Size, Fatigue Life, Multi-Axis Loads, Stress Intensity Factor

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© 2021 Trans Tech Publications Ltd. All Rights Reserved

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