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Development of 3D Angle-Interlock Woven Preforms for Composites

机译:用于复合材料的3D角互锁编织预成型坯的开发

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摘要

The advent of three dimensional (3D) reinforcements has been mainly to overcome the issue of delamination and improve upon the damage tolerance properties by introducing fibres in the thickness direction for advanced composite applications. 3D preforms can be developed using various techniques. Angle-interlock weaving is one of them. This paper details about the efforts being put at CSIR-NAL for developing angle-interlock woven preforms. Four types of angle-interlock structures viz., layer-to-layer and through thickness (both with and without stuffer yarns) were developed using 6K, 400 Tex TC-33 grade Carbon tows on a custom designed handloom. The preforms without stuffer yarns had 4 layers of warp and were of 1.5± 0.2 mm thick. Preforms with stuffer yarns had 6 layers of warp (including 2 stuffer yarn layers) and were of 2.3±0.1 mm thick. Thermoset composites were prepared from these preforms using EPOLAM 2063 (an epoxy based resin system) by RTM process. The fibre weight fraction for these composites ranged from 0.53 to 0.58 and they were subjected to mechanical tests such as tensile, flexural and interlaminar shear strength. Test results showed improved response (in the warp direction) with respect to shear properties while the tensile and flexural properties were equivalent to that of the plain woven composites.
机译:三维(3D)增强材料的出现主要是为了克服分层问题,并通过在厚度方向上引入纤维来改善复合材料的应用,从而提高了其抗损伤性能。可以使用各种技术来开发3D瓶坯。角度互锁编织就是其中之一。本文详细介绍了CSIR-NAL为开发角度互锁编织预成型件而付出的努力。在定制设计的手摇织机上使用6K,400 Tex TC-33级碳纤维束开发了四种类型的角度互锁结构,即层与层以及贯穿厚度(带和不带填充纱)。没有填充纱的预成型件具有4层经纱,厚度为1.5±0.2 mm。带有填充纱的预成型件具有6个经纱层(包括2个填充纱层),厚度为2.3±0.1 mm。使用EPOLAM 2063(基于环氧树脂的树脂系统),通过RTM工艺从这些预成型坯中制备热固性复合材料。这些复合材料的纤维重量分数在0.53至0.58的范围内,并经过了机械测试,如拉伸,弯曲和层间剪切强度。测试结果表明,在剪切性能方面的响应有所改善(在经向),而拉伸和弯曲性能则与平纹复合材料相当。

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