Yi Gong , Rui Zhou , Xiangli Li , Shizhao Wang , Miao Li , Sheng Liu
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引用次数: 0
Abstract
Carbon fiber reinforced polymer (CFRP) plays an increasingly important role in aerospace industry. However, CFRP is susceptible to external impacts damage during service. The evaluation of residual mechanical properties is essential to ensure the safety of damaged components. Existing studies usually focus on qualitative analyses, which is difficult to accurately predict the mechanical properties. In this study, we develop a multi-task prediction model based on multi-modal damage features for evaluating both absorbed energy and residual compressive properties of post-impact CFRP laminates. Specifically, the multi-modal features, obtained by adaptive fusion of surface morphology and dent features, are used to improve the learning ability of global and local damage. The regression module is optimized by an attention mechanism (the squeeze-and-excitation networks) to enhance the weight of key feature channels. Additionally, independent regression modules are designed to reduce interference between prediction tasks. The results show that the improved model achieves high fitting accuracy ( = 96.62 %) and low prediction error (less than 5.76 %), which realizes precise prediction of the residual compressive properties. This study provides a novel approach for properties assessment of damaged CFRP structures.
期刊介绍:
Composites Science and Technology publishes refereed original articles on the fundamental and applied science of engineering composites. The focus of this journal is on polymeric matrix composites with reinforcements/fillers ranging from nano- to macro-scale. CSTE encourages manuscripts reporting unique, innovative contributions to the physics, chemistry, materials science and applied mechanics aspects of advanced composites.
Besides traditional fiber reinforced composites, novel composites with significant potential for engineering applications are encouraged.