Metal structure fatigue crack propagation life prediction method based on material R curve
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- AIR FORCE UNIV PLA
- Publication Date
- 2012-11-14
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to a fatigue crack growth life prediction method for metal structures, in particular to a metal structure fatigue crack growth life prediction model based on material R curves. Background technique
[0002] Typical major equipment in machinery, transportation and energy industries have been in service for many years. Reliable prediction of the life of cracked components is an important way to effectively improve the service performance of equipment and control the occurrence of failure accidents, because premature decommissioning means huge waste and economic loss, continued operation requires a reasonable life forecast to ensure safety. Metal materials are widely used in aviation equipment as the main load-bearing parts of the structure. This is particularly evident in the various types of main combat aircraft currently in service in my country. Even as the most advanced fighter F-22 in the world, the amount of composite materia...