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Influence of Layup and Curing on the Surface Accuracy in the Manufacturing of Carbon Fiber Reinforced Polymer (CFRP) Composite Space Mirrors

机译:叠加和固化对碳纤维增强聚合物(CFRP)复合空间镜制造表面精度的影响

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摘要

Carbon fiber reinforced polymer, CFRP, composite materials have been used to fabricate space mirror. Usually the composite space mirror can completely replicate the high-precision surface of mould by replication process, but the actual surface accuracy of replicated space mirror is always reduced, still needed further study. We emphatically studied the error caused by layup and curing on the surface accuracy of space mirror through comparative experiments and analyses, the layup and curing influence factors include curing temperature, cooling rate of curing, method of prepreg lay-up, and area weight of fiber. Focusing on the four factors, we analyzed the error influence rule and put forward corresponding control measures to improve the surface figure of space mirror. For comparative analysis, six CFRP composite mirrors were fabricated and surface profile of mirrors were measured. Four guiding control measures were described here. Curing process of composite space mirror is our next focus.
机译:碳纤维增强聚合物,CFRP,复合材料已用于制造空间镜。通常,复合空间镜可以通过复制过程完全复制模具的高精度表面,但是复制空间镜的实际精度总是减少,仍然需要进一步研究。我们通过比较实验和分析,重点研究了上铺上和固化的误差和固化空间镜的表面精度,叠加和固化影响因素包括固化温度,固化冷却速率,预浸料铺设的方法,以及纤维的面积重量。 。专注于四个因素,我们分析了误差影响规则并提出了相应的控制措施来改善太空镜的表面图。对于比较分析,制造了六个CFRP复合镜,测量了镜子的表面轮廓。这里描述了四种指导控制措施。复合空间镜的固化过程是我们的下一个焦点。

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