Creep life assessment method
WO2025243255A1PCT designated stage Publication Date: 2025-11-27PTT GLOBAL CHEMICAL PUBLIC COMPANY LIMITED +1
8 Cites -1 Cited by
Patent Information
- Application Number
- PCT/IB2025/055351
- Authority / Receiving Office
- WO · WO
- Patent Type
- Applications
- Current Assignee / Owner
- Priority Date
- 2024-05-24
- Filing Date
- 2025-05-23
- Publication Date
- 2025-11-27
Abstract
The present invention relates to a creep life assessment method having high precision and accuracy, especially for using in an inspection and assessment of the service life of material at high temperature including easy to apply with the conventional creep assessment. Moreover, said method intends to assess the actual creep life considering the creep life prediction from the model built from machine learning from the factor and operating condition data that affects the creep such as temperature, stress, including Larson-Miller parameter and Larson-Miller constant, which have been adjusted to consider the factor and operating condition, resulting in more precise and accurate creep life prediction. Said method also considers the creep life fraction assessment by considering the physical property of the material together with the accumulated creep condition simulation, so that the creep life fraction assessment of the material from model built from machine learning is more precise. Therefore, the actual creep life can be assessed.
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Citation Information
Patent Citations
A method for predicting the thermodynamic response and fatigue-creep damage of high-chromium steel.
CN108931448B
A creep fatigue life prediction method based on crystal plasticity
CN112364535B
Method and system for real-time prognosis analysis and usage based residual life assessment of turbine engine components and display
US20110137575A1
Aircraft engine systems and methods for operating same
US20140244133A1
Extension of model-based design to identify and analyze impact of reliability information on systems and components
US20160357895A1