Composite cure simulation scheme fully integrating internal strain measurement

被引:37
作者
Minakuchi, Shu [1 ]
Niwa, Shoma [1 ]
Takagaki, Kazunori [1 ]
Takeda, Nobuo [1 ]
机构
[1] Univ Tokyo, Grad Sch Frontier Sci, Dept Adv Energy, 5-1-5 Kashiwanoha, Kashiwa, Chiba 2778561, Japan
关键词
Cure behavior; Residual/internal stress; Process simulation; Process monitoring; RESIDUAL-STRESSES; DEFORMATION; SHRINKAGE; FAILURE;
D O I
10.1016/j.compositesa.2016.01.001
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study proposes a new approach to determine key material parameters for stress/strain calculation of curing composite laminates and validate the simulation. Specifically, fiber Bragg grating (FBG) strain sensors are embedded in a composite laminate and the two key parameters for simulation, composite shrinkage strain and stiffness change during curing, are simultaneously determined from in-situ measurements by the embedded sensors. Furthermore, the simulation is validated using internal strain change during curing. This paper begins by presenting an overview of the proposed simulation scheme and by comparing it with previous approaches to highlight its advantages. Material parameter determination using a shear-lag effect at the edge of the embedded sensors is then described and the practical procedure to obtain the key parameters is demonstrated using a carbon/epoxy laminate. Finally, cure simulation is conducted for validation. Further extension to more general cases including thermoplastic composites is also discussed. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:53 / 63
页数:11
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