...
首页> 外文期刊>Composites >A hysteresis energy dissipation based model for multiple loading damage in continuous fiber-reinforced ceramic-matrix composites
【24h】

A hysteresis energy dissipation based model for multiple loading damage in continuous fiber-reinforced ceramic-matrix composites

机译:基于磁滞能量耗散的连续纤维增强陶瓷基复合材料多次载荷损伤模型

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

In this paper, a hysteresis energy dissipation based damage model for fiber-reinforced ceramic-matrix composites (CMCs) subjected to multiple loading stress levels is developed. Considering the combination effects of multiple loading sequences and multiple fatigue damage mechanisms, i.e., matrix cracking, fiber/matrix interface de-bonding and interface wear, the evolution of the fiber/matrix interface debonding and sliding, fatigue hysteresis loops, fatigue hysteresis dissipated energy and fatigue hysteresis modulus changing with increasing applied cycles are analyzed. The effects of fiber volume fraction, matrix crack spacing, fatigue peak stress and fatigue stress range on the damage development inside of CMCs are discussed. The difference of the fiber/matrix interface shear stress existed between the interface wear region and new interface debonded region affects the fiber/matrix interface debonded length and loading carrying ability of intact and broken fibers. The damage evolution for C/SiC and SiC/SiC composites subjected to multiple fatigue loading sequences are predicted using the hysteresis energy dissipation damage model. Under multiple loading stress, the fatigue hysteresis dissipated energy increases when high peak stress and stress range increases due to the increase of fiber/matrix interface sliding range. However, when the low peak stress increases, the evolution of fatigue hysteresis dissipated energy depends on the interface debonding and sliding state.
机译:本文建立了一种基于磁滞能量耗散的纤维增强陶瓷基复合材料(CMC)承受多种载荷应力水平的损伤模型。考虑到多种加载顺序和多种疲劳破坏机制的组合效应,即基体开裂,纤维/基体界面剥离和界面磨损,纤维/基体界面剥离和滑动的演变,疲劳磁滞回线,疲劳磁滞耗散能量分析了疲劳滞后模量随应用循环次数的增加而变化的情况。讨论了纤维体积分数,基体裂纹间距,疲劳峰值应力和疲劳应力范围对CMC内部损伤发展的影响。界面磨损区域与新界面剥离区域之间存在的纤维/基质界面剪切应力的差异影响了纤维/基质界面的剥离长度和完整和断裂纤维的承载能力。使用磁滞能量耗散损伤模型预测了经受多个疲劳载荷序列的C / SiC和SiC / SiC复合材料的损伤演化。在多重加载应力下,由于纤维/基体界面滑动范围的增大,当高峰值应力和应力范围增大时,疲劳滞后耗散的能量也会增加。然而,当低峰值应力增加时,疲劳滞后耗散能量的演变取决于界面剥离和滑动状态。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号