复合材料V型构件的固化变形预测及其工装型面设计
发布时间：2019-07-18 07:35
【摘要】：利用固化动力学模型对20mm厚度和3mm厚度的ZT7H/5429碳纤维复合材料层合板进行了固化模拟,在固化过程中,20mm厚度平板出现了温度峰值,中心温度与表面温度差不超过6℃,3mm平板温度分布均匀,温度历程与热压罐工艺温度基本一致。利用简化的温度场和等效热膨胀系数对60°和90°拐角的V型基准试件进行了固化变形模拟,并进行了V型基准试件的固化试验。60°和90°拐角试件的固化回弹角的模拟值分别为1.58°和1.18°,试验测得的回弹角的平均值分别为1.59°和1.11°。对V型复合材料蒙皮构件进行了固化变形模拟,并得到了补偿过的工装型面,在该工装上成型的试件与设计形状基本一致。
[Abstract]:The curing simulation of ZT7H/5429 carbon fiber composite laminates with 20mm thickness and 3mm thickness was carried out by using curing kinetics model. During the curing process, the temperature peak value of 20mm thickness plate appeared, the difference between central temperature and surface temperature was not more than 6 鈩，
本文编号：2515733
[Abstract]:The curing simulation of ZT7H/5429 carbon fiber composite laminates with 20mm thickness and 3mm thickness was carried out by using curing kinetics model. During the curing process, the temperature peak value of 20mm thickness plate appeared, the difference between central temperature and surface temperature was not more than 6 鈩，
本文编号：2515733
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