A method for predicting crack opening displacement of fiber-reinforced ceramic matrix composites considering fiber breakage
Through a prediction method that considers fiber breakage, the crack opening displacement of fiber reinforced ceramic matrix composites is predicted by using load bearing criteria, interface debonding criteria, shear hysteresis model and slip mechanism, which solves the problem that the impact of fiber breakage in the prior art is not considered, and improves the accuracy of prediction and the reliability of the material.
Patent Information
- Application Number
- CN202111465594.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2021-12-03
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2041-12-03
AI Technical Summary
The prior art has not yet established a method for predicting crack opening displacement of fiber reinforced ceramic matrix composite materials that consider the influence of fiber fracture, which makes it difficult to ensure the reliability and safety of materials when used in aircraft and aircraft engine structures.
A method for predicting the crack opening displacement of fiber-reinforced ceramic matrix composite material that considers fiber fragmentation is provided. Through the overall load bearing criteria, fracture mechanical interface debonding criteria, shear hysteresis model and fiber relative matrix slip mechanism, the fiber axial stress distribution, matrix axial stress distribution, fiber axial displacement and matrix axial displacement are determined at the crack plane, and finally predict the axial relative displacement of fiber and matrix at the crack plane.
The accuracy of crack opening displacement prediction of fiber-reinforced ceramic matrix composite materials is improved, and the impact of fiber breakage factors on the crack opening displacement of material is considered, which enhances the reliability and safety of the material in high temperature and high stress environments.