Environmentally Resistant Flax Fiber-Reinforced Composites for Aircraft Applications: Aviation Stress Tests with Optical and Mechanical Analyses

IF 2.9 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES
Sarina Schulte, Hannes Schäfer, Christoph Vogel, Vineet Shah, Stephen Kroll, Andrea Siebert-Raths
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Abstract

Flax fiber-reinforced composites (FFRCs) must be resistant to environmental conditions to use them for external components in aviation. It was investigated how contact with typical aviation liquids, i.e. water, jet fuel and hydraulic oil, affects the optical and mechanical properties of twill fabric epoxy resin-based FFRCs. These influences were compared to the effect of UV weathering. Samples were exposed to these conditions for up to 28 days at RT. Uncoated samples with different fiber contents served as references and were compared with coated samples. A polyurethane/epoxy-based aircraft coating system and a partially biobased automotive interior coating as a more sustainable alternative were examined. The main damage for the uncoated samples was caused by UV weathering and water. UV light leads to photo-oxidation, causing material erosion. Water is absorbed by the hydrophilic flax fibers. Subsequent swelling leads to deformation and delamination. Thus, the damage was more severe for a higher fiber content. No effect could be demonstrated by immersion in jet fuel and hydraulic oil, as they are hardly absorbed by the fibers. Both coatings showed good protection against UV weathering and delayed water absorption. Nevertheless, mechanical damage was found for the FFRC covered with the fossil coating after 28 days of immersion in water. FFRC with an appropriate coating could therefore be suitable for use in aviation, but prolonged contact with water should be avoided. Protective measures should focus on preventing water uptake and UV irradiation, as these cause significantly more damage than jet fuel and hydraulic oil.

飞机用耐环境亚麻纤维增强复合材料:光学和机械分析的航空应力测试
亚麻纤维增强复合材料(ffrc)必须具有良好的耐环境条件才能用于航空外部部件。研究了环氧树脂基ffrc与典型航空液体(水、喷气燃料和液压油)的接触对斜纹织物光学性能和力学性能的影响。将这些影响与紫外线风化的影响进行了比较。样品在室温下暴露在这些条件下长达28天。具有不同纤维含量的未涂层样品作为参考,并与涂层样品进行比较。研究了聚氨酯/环氧基飞机涂层系统和部分生物基汽车内饰涂层作为更可持续的替代方案。对未包覆样品的破坏主要是由紫外线风化和水分造成的。紫外光导致光氧化,造成材料侵蚀。水被亲水性的亚麻纤维吸收。随后的膨胀导致变形和分层。因此,纤维含量越高,损伤越严重。浸泡在喷气燃料和液压油中没有效果,因为它们几乎不被纤维吸收。两种涂层均表现出良好的抗紫外线老化和延迟吸水性能。然而,在水中浸泡28天后,被化石涂层覆盖的FFRC发现了机械损伤。因此,涂有适当涂层的FFRC可适用于航空,但应避免长时间与水接触。防护措施应侧重于防止吸水和紫外线照射,因为它们造成的损害比喷气燃料和液压油严重得多。
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来源期刊
Applied Composite Materials
Applied Composite Materials 工程技术-材料科学:复合
CiteScore
4.20
自引率
4.30%
发文量
81
审稿时长
1.6 months
期刊介绍: Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes. Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.
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