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MULTI-SCALE MODELING OF DAMAGE AND DELAMINATIONS FAILURE IN CERAMIC MATRIX COMPOSITES

机译:陶瓷基复合材料损伤和分层破坏的多尺度建模

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摘要

Ceramic Matrix Composite (CMC) materials are high-temperature material of particular interest to aircraft engine manufacturers as they have the potential to provide better thermal efficiency at a lower weight compared to conventional metallic materials. As these materials are being inserted into service it is essential to understand their damage and failure mechanisms to ensure designs with sufficient margins as well as their long-term durability. High-fidelity analytical and computational models of CMC failure processes can enable robust design of CMC components. This talk will focus on multi-scale modeling of elastic behavior as well as ply-damage and delamination fracture in CMCs developed over many years under several AFRL funded programs. The effects of defects as well as issues in scaling the behavior from coupon-scale to component-scale will be discussed via analysis of test coupons and representative sub-elements.
机译:陶瓷基复合材料(CMC)材料是飞机发动机制造商特别感兴趣的高温材料,因为与传统的金属材料相比,它们有可能在更轻的重量下提供更好的热效率。在将这些材料投入使用时,必须了解它们的损坏和失效机理,以确保设计具有足够的余量以及长期的耐用性。 CMC故障过程的高保真分析和计算模型可以实现CMC组件的稳健设计。这次演讲的重点是在多个AFRL资助的计划下多年开发的CMC的弹性行为以及层板破坏和分层断裂的多尺度建模。缺陷的影响以及将行为从试样规模缩放到组件规模的问题将通过测试试样和代表性子元素的讨论进行讨论。

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