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Vacuum-Assisted Resin Infusion Molding (VARIM) Processing for Thick-Section Composite Laminates in Wind Turbine Blades

机译:用于风力涡轮机叶片的厚截面复合层压板的真空辅助树脂输液模塑(VARIM)加工

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In this paper a comprehensive investigation of exothermal reaction and curing kinetics is conducted on thick glass-fiber reinforced thermoset composite laminates up to 80 plies (3.6 inches after cure) in thickness. The composite material selected for the study is a polyester-matrix-based, E-glass fabric reinforced composite system of various laminate thicknesses. Composite laminate panels of 8-inch by 8-inch in size have been infused in a setup representative of large-part VARIM processing. Through-thickness exothermic temperature, ion viscosity, degree of cure and their evolutions in the composite during processing are obtained by direct measurements of embedded thermocouples and dielectric sensors. Through-thickness curing index profiles at different time instances are determined from the DEA data and related to the instantaneous degree of cure to illustrate the curing extent and its variations in the thickness direction of the thick composite. Dimensional stability of the thick laminate composite is determined in real time during the infusion and curing processes. The important issue of the laminate-thickness effect on through-thickness gradients and their evolutions of exothermic reaction temperature and curing kinetics are addressed. Comparisons are made with a series of experiments on composite laminate panels with several different numbers of plies.
机译:本文在厚度为80层(固化后3.6英寸)的厚玻璃纤维增​​强热固性复合层压板上进行了对放热反应和固化动力学的综合调查。选择用于研究的复合材料是一种基于聚酯 - 基质的电子玻璃织物增强复合体系的各种层压厚度。在大零件瓦米处理的设置中,尺寸为8英寸8英寸×8英寸的复合层压板。通过直接测量嵌入式热电偶和介电传感器,通过直接测量加工过程中的通过厚度放热温度,离子粘度,固化程度及其在复合材料中的演进。不同时间实例的贯穿厚度固化指数分布由DEA数据确定并与固化瞬时程度相关,以说明厚复合材料的厚度方向的固化程度及其变化。在输注和固化过程中实时确定厚层压复合材料的尺寸稳定性。解决了层压厚度效应的重要问题及其对放热反应温度和固化动力学的演变。通过一系列关于具有多种不同数量不同的复合层压板的一系列实验进行比较。

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