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Marine Composites Based on Low Styrene Content Resins. Influence of Lamination Procedure and Peel Plies on Interlaminar Resistance

机译:基于低苯乙烯含量树脂的船用复合材料。层压程序和剥离层对层间电阻的影响

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Delays between lamination of structures and secondary bonding arc common in boatbuilding. This paper presents results from an experimental study of the influence of manufacturing procedure on the bond strength of unidirectional glass fibre reinforced polyester composites. Continuously laminated panels are taken as the reference and compared with panels overlaminated after delays of one week with and without peel ply protection. A standard polyester and low styrene DCPD formulation were tested. ILSS testing is shown not to be sensitive to the procedure but crack propagation tests show very large differences in mode I fracture energy. A small drop in fracture energy is measured for a delay of one week between lamination of the first and second halves of the specimen without peel ply. When a nylon peel ply is applied and removed just before overlamination of the second half very large drops in propagation energy, around 75 percent, are noted for both materials. Surface abrasion after peel ply removal enables fracture energy to be recovered for the standard polyester and to a lesser extent for the low styrcne DCPD composite.
机译:在造船中,结构的层压和二次粘结之间的延迟很常见。本文介绍了有关制造工艺对单向玻璃纤维增​​强聚酯复合材料粘结强度影响的实验研究结果。以连续层压的面板为参考,并与延迟了一个星期的层压面板进行了比较,无论有无剥离层保护,延迟了一周。测试了标准聚酯和低苯乙烯DCPD配方。已显示ILSS测试对该程序不敏感,但裂纹扩展测试显示出I型断裂能的很大差异。在没有剥离层的情况下,在样品的第一半部分和第二半部分的层压之间的一个星期的延迟时间内测量到断裂能的小幅下降。当在下半部覆膜之前施加并去除尼龙剥离层时,两种材料均会出现非常大的传播能量下降(约75%)。去除剥离层后的表面磨损使得标准聚酯可以回收断裂能,而低苯乙烯DCPD复合材料的回收能较小。

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