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A comparative experiment for the analysis of microwave and thermal process induced strains of carbon fiber/bismaleimide composite materials

机译:微波和热过程引起的碳纤维/双马来酰亚胺复合材料应变分析的对比实验

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摘要

Carbon fiber reinforced bismaleimide composites provide many outstanding properties and are widely used in aerospace applications. However, cure-induced strains are present in virtually all composites that severely impact on the whole service lifecycle of composite components. This paper will demonstrate that the cure-induced strains can be drastically reduced in fiber/ bismaleimide composites using the microwave curing process. Nearly 95% reduction of cure-induced strains has been achieved compared with the conventional thermal heating process. The microwave manufacturing cycle for composites was only 36% of the thermal processing cycle. When using the microwave process, the spring-in angle of an L-shaped part was reduced by about 1.2°Compared by using thermal heating.
机译:碳纤维增强双马来酰亚胺复合材料具有许多出色的性能,并广泛用于航空航天应用。但是,几乎所有复合材料中都存在固化诱导的应变,这些应变会严重影响复合材料组件的整个使用寿命。本文将证明使用微波固化工艺可以大大降低纤维/双马来酰亚胺复合材料中的固化诱导应变。与传统的热加热工艺相比,已将固化引起的应变降低了近95%。复合材料的微波制造周期仅为热处理周期的36%。与微波加热相比,使用微波工艺时,L形零件的弹入角减小了约1.2°。

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