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Development and evaluation of a novel integrated anti-icing/de-icing technology for carbon fibre composite aerostructures using an electro-conductive textile

机译:碳纤维复合材料航空结构新型导电防冰除冰技术的开发和评估

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摘要

The preliminary evaluation is described of a new electro-thermal anti-icing/de-icing device for carbon fibre composite aerostructures. The heating element is an electro-conductive carbon-based textile (ECT) by Gorix. Electrical shorting between the structural carbon fibres and the ECT was mitigated by incorporating an insulating layer formed of glass fibre plies or a polymer film. A laboratory-based anti-icing and de-icing test program demonstrated that the film-insulated devices yielded better performance than the glssass fibre insulated ones. The heating capability after impact damage was maintained as long as the ECT fabric was not breached to the extent of causing electrical shorting. A modified structural scarf repair was shown to restore the heating capacity of a damaged specimen.
机译:对碳纤维复合材料航空结构的新型电热除冰/除冰装置进行了初步评估。加热元件是Gorix生产的导电碳基纺织品(ECT)。通过引入由玻璃纤维帘布层或聚合物膜形成的绝缘层,可以减轻结构碳纤维与ECT之间的电短路。基于实验室的防冰和除冰测试程序表明,与玻璃纤维绝缘的设备相比,薄膜绝缘的设备具有更好的性能。只要不破坏ECT织物达到引起电短路的程度,冲击破坏后的加热能力就得以维持。研究表明,经过改进的结构性围巾修复可以恢复受损样品的加热能力。

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