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Static, fatigue and impact behaviour of an autoclaved flax fibre reinforced composite for aerospace engineering
Composites Part B: Engineering ( IF 13.1 ) Pub Date : 2020-05-22 , DOI: 10.1016/j.compositesb.2020.108049
Tulio Hallak Panzera , Thomas Jeannin , Xavier Gabrion , Vincent Placet , Chrystel Remillat , Ian Farrow , Fabrizio Scarpa

This work describes the physical and mechanical characterization of unidirectional [0]12 and crossply [(0/90)3/0]S flax fibre reinforced composites fabricated in autoclave using a prepreg flax tape impregnated with fire retardant epoxy polymer. Tensile, bending and impact properties are evaluated along the longitudinal and transverse fibre directions. The tensile-tensile fatigue behaviour is characterised along the fibre direction. Physical and specific properties are also assessed to identify the potential characteristics of these bio-based composites for lightweight and secondary loadbearing applications. The robust manufacturing process described in this work, coupled with precision laser cutting, makes this type of composite a promising sustainable material for aircraft, transport and lightweight construction designs.



中文翻译:

航空航天工程用高压灭菌亚麻纤维增强复合材料的静态,疲劳和冲击性能

这项工作描述了单向[0] 12和交叉[[0/90)3 /0]小号亚麻纤维增强复合材料使用具有阻燃环氧聚合物浸渍的预浸料坯带亚麻制造在高压釜中。沿着纤维的纵向和横向评估拉伸,弯曲和冲击性能。沿纤维方向表征了拉伸-拉伸疲劳行为。还评估了物理和特定性能,以识别这些生物基复合材料在轻型和二次承重应用中的潜在特性。这项工作中描述的坚固的制造工艺,再加上精密的激光切割,使得这种复合材料成为飞机,运输和轻型结构设计的有前途的可持续材料。

更新日期:2020-05-22
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