利用计算机模拟减少热塑性复合材料加工中的红外加热循环时间

G.J. Sweeney, P.F. Monaghan, M.T. Brogan, S.F. Cassidy
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引用次数: 28

摘要

本文讨论了在热塑性复合材料的加工过程中如何提高红外加热循环的速度。加热过程的一个限制是,在开始成形之前,材料的所有部分必须在推荐的加工温度范围内。采用数学模型对连续碳纤维增强聚醚醚酮(APC-2)平板固结板加热过程中的瞬态温度分布进行了预测。该模型包括(i)自然对流,(ii)中波和长波辐射以及(iii)通过材料的一维传导。利用红外试验台对该模型进行了实验验证。改变以下工艺参数以获得最佳工艺条件:(i)加热器功率;(ii)加热器与复合材料的距离;(iii)复合材料厚度;(iv)与复合材料表面积相比,加热器面积过大的程度;(v)单面或双面加热。结果表明,当加热器与复合材料的距离从100 mm减小到50mm时,复合材料的稳态温度提高了88%,而当加热器功率密度从25.6 kWm2增加到47.3 kWm2时,复合材料的稳态温度仅提高了17%。使用单面加热,实验结果表明,向上加热器比向下加热器在面板表面产生更均匀的温度分布。模型结果显示,0.5 ~ 9.5 mm厚度的复合板加热时间为1 R。
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Reduction of infra-red heating cycle time in processing of thermoplastic composites using computer modelling

This paper deals with increasing the speed of the infra-red (IR) heating cycle in the processing of thermoplastic composites. A constraint on the heating process is that all parts of the material must be within the recommended processing temperature range before forming can start. A mathematical model is used to predict the transient temperature distribution through the thickness of flat consolidated panels of continuous carbon fibre-reinforced poly(ether ether ketone) (APC-2) during heating. The model includes (i) natural convection, (ii) medium and long wave radiation and (iii) one-dimensional conduction through the material. Experimental validation of the model is conducted using an IR test rig. The following process parameters were varied to obtain optimum process conditions: (i) heater power: (ii) heater-to-composite distance: (iii) composite thickness; (iv) degree of oversizing of heater area compared with surface area of composite: and (v) one- or two-sided heating. Results presented show that reduction of the heater-to-composite distance from 100 to 50mm increases the steady-state temperature of the composite by 88%, whereas almost doubling the heater power density from 25.6 to 47.3 kWm2 - increases the composite temperature by only 17%. Using one-sided heating, experimental results show that upward-facing heaters produce a more even temperature distribution across a panel surface than downward-facing heaters. Model results showing 1 R heating times for composite panels of thickness 0.5 to 9.5 mm are also presented.

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