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Influence of cutting parameters on thrust force, drilling torque and delamination during drilling of carbon fibre reinforced composites

机译:切削参数对碳纤维增强复合材料钻孔过程中推力,钻孔扭矩和分层的影响

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摘要

Composite materials have become valuable construction materials in aerospace, defense and in recent years in automotive industry. The advantage of composite materials over conventional materials stems largely from their higher specific strength, stiffness and fatigue characteristics. Composite components are joined by mechanical fasteners, accurate, precise high quality holes need to be drilled to ensure proper and durable assemblies. Drilling of composite materials causes several damages, such us: delamination, fibre-pull out, edge chipping, uncut fibers and others. Delamination is a major problem associated with drilling fiber reinforced composite materials. It causes poor assembly tolerance, reduces structural integrity of material and the potential for long term performance deterioration. The thrust force has been cited as main cause of delamination. In this paper the objective was to establish correlation between cutting parameters and thrust force, drilling torque and delamination. Drilling tests were carried out on carbon epoxy composite material using three different drills, HSS-Co twist drill, Multi Constructional twist drill and "Brad & Spur" drill. The data have been processed by the "DesignExpert" software package which generated the mathematical models.
机译:复合材料已成为航空航天,国防和汽车工业中近年来有价值的建筑材料。与常规材料相比,复合材料的优势主要是由于它们具有更高的比强度,刚度和疲劳特性。复合组件通过机械紧固件连接在一起,需要钻出准确,精确的高质量孔,以确保正确且耐用的组装。复合材料的钻孔会造成多种损坏,例如:分层,纤维拉出,边缘碎裂,未切割的纤维等。分层是与钻孔纤维增强复合材料相关的主要问题。这会导致不良的装配公差,降低材料的结构完整性,并可能导致长期性能下降。推力被认为是分层的主要原因。本文的目的是建立切削参数与推力,钻削扭矩和分层之间的相关性。使用三种不同的钻头,HSS-Co麻花钻,Multi Constructional麻花钻和“ Brad&Spur”钻对碳环氧复合材料进行了钻孔测试。数据已由“ DesignExpert”软件包处理,该软件包生成了数学模型。

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