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Publishing Language: Chinese

Life design method of high-temperature equipment based on dual-scale damage theory

Kaishang LI, Haoqi FAN, Runzi WANG, Xiancheng ZHANG( ), Shantung TU
School of Mechanical and Power Engineering, East China University of Science and Technology, Shanghai 200237
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Abstract

The contradiction between the long-term safe operation of high-temperature structures and harsh service environment is becoming increasingly prominent. Creep-fatigue interaction damage has become increasingly prominent, leading to high failure rates of high-temperature components. In addition, the urgent demand for deep peak shaving in power generation units under carbon neutrality targets means that the critical high-temperature components face a lack of accurate life assessment methods. Traditional life design approaches based on single-scale or single-parameter are insufficient to simultaneously account for multi-axial stress effects and microstructural evolution in high-temperature structures, especially for the structures with inhomogeneous microstructures. In this paper, dual-scale modeling approach based on macro-continuum mechanics and micro-crystal plasticity is systematically introduced. Taking hole structure as an example, a life prediction method based on the dual-scale damage theory is presented. To facilitate the engineering application of the dual-scale theoretical framework, a creep-fatigue life prediction software considering surface strengthening effects is developed, enabling rapid damage assessment and life prediction for surface strengthening structures.

CLC number: V231.95;O346 Document code: A Article ID: 1000-6893(2025)05-531706-25

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
LI K, FAN H, WANG R, et al. Life design method of high-temperature equipment based on dual-scale damage theory. Acta Aeronautica et Astronautica Sinica, 2025, 46(5). https://doi.org/10.7527/S1000-6893.2025.31706

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Received: 24 December 2024
Revised: 17 January 2025
Accepted: 19 February 2025
Published: 11 March 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica