Creep-Fatigue Life Prediction for Aeroengine’s High Temperature Component

Yi Rui Xia; Jing Tao Dai; Zhong Yun Sun

doi:10.4028/www.scientific.net/AMM.670-671.1083

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 670-671Creep-Fatigue Life Prediction for Aeroengine’s...

Creep-Fatigue Life Prediction for Aeroengine’s High Temperature Component

Abstract:

In this paper, the key technique involved in life prediction of aeroengine’s high temperature component for creep and fatigue/creep interaction, namely, the life prediction methods for high temperature component are discussed systematically. The essential thinking、features and development direction of the theories are commented in detail. All the results obtained are valuable to engineering applications.

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Periodical:

Applied Mechanics and Materials (Volumes 670-671)

Pages:

1083-1086

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.670-671.1083

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Online since:

October 2014

Authors:

Yi Rui Xia*, Jing Tao Dai, Zhong Yun Sun

Keywords:

Aeroengine, Creep, Fatigue, High Temperature Component, Life Prediction

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* - Corresponding Author

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