CLC number: TH49
On-line Access: 2019-01-04
Received: 2018-03-09
Revision Accepted: 2018-08-13
Crosschecked: 2018-11-10
Cited: 0
Clicked: 4415
Bin-bin Liao, Dong-liang Wang, Li-yong Jia, Jin-yang Zheng, Chao-hua Gu. Continuum damage modeling and progressive failure analysis of a Type III composite vessel by considering the effect of autofrettage[J]. Journal of Zhejiang University Science A,in press.Frontiers of Information Technology & Electronic Engineering,in press.https://doi.org/10.1631/jzus.A1800152 @article{title="Continuum damage modeling and progressive failure analysis of a Type III composite vessel by considering the effect of autofrettage", %0 Journal Article TY - JOUR
考虑自增强影响的III型复合材料气瓶连续损伤模拟及渐进失效分析创新点:1. 建立针对三维气瓶的Hashin失效准则和指数型损伤演化的渐进失效模型,并通过ABAQUS-UMAT隐式有限元方法确定气瓶最佳自紧压力; 2. 通过渐进失效分析,揭示自紧后的气瓶纤维和基体损伤的损伤演化规律,并阐明自紧对气瓶渐进失效的影响. 方法:1. 基于连续损伤力学,建立三维Hashin失效准则和指数型损伤演化的渐进失效理论模型; 2. 通过ABAUQS-UMAT二次开发用户子程序实现渐进失效理论模型,并开展气瓶渐进失效计算; 3. 通过平板拉伸算例以及与气瓶试验数据对比,验证模型的准确性. 结论:1. 基体损伤首先出现在螺旋层,而纤维损伤首先出现在环向层. 2. 除了自紧后的泄压阶段和自紧后重新加压至压力值等于自紧压力的升压阶段,有无自紧的气瓶损伤演化规律基本一致; 而在上述泄压和升压阶段,基体损伤保持不变,说明经过自紧后的气瓶在工作压力下存在基体损伤. 3. 当内压压力低于自紧压力时,自紧工艺才会影响气瓶应力分布; 且随着压力的升高,基体损伤不变,内衬应力减少,纤维应力增加; 此外,经过自紧的气瓶在工作压力下最大环向和轴向内衬应力减少且出现在筒体部分的两端. 关键词组: Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article
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