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Finite element analysis of localised impact loading on short glass fibrereinforced polyamide engine oil pan subjected to low velocity impact from flying projectiles

机译:局部冲击荷载发动机油平板局部冲击载荷的有限元分析经受飞行射弹的低速冲击的影响

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This paper investigates low velocity impact involving a glass fibre-reinforced polyamide engine oil pan as part of a complete new development of thermoplastic components. The assessment of the impact resistance has driven the need to employ LS DYNA for finite element modelling in order to virtually benchmark and predict the strength and fracture behaviour of stressed plastic parts. In order to develop a reliable predictive capability and to validate simulations, complete components were manufactured by injection moulding techniques for the experimental samples. Low velocity impact investigations were carried out using a gas gun and a falling weight tester in order to simulate impact events to which the oil pan is subjected whilst in operational service. This was intended to point out damage tolerance and failure mechanisms likely to occur in the structure. The study results show the significant contribution of the design in terms of shock absorption. Specific oil pan design with protective ribbing combined with a superior material considerably improves the impact resistance. The paper provides results and discussions on experimental and finite element analysis investigations before concluding with some remarks.
机译:本文研究了玻璃纤维增​​强聚酰胺发动机油底壳的低速局面,作为热塑性成分的全新开发的一部分。抗冲击性的评估推动了需要使用LS Dyna进行有限元建模,以便几乎基于基准和预测应激塑料部件的强度和断裂行为。为了开发可靠的预测性和验证模拟,通过用于实验样品的注塑技术来制造完整的组分。使用气枪和下降的重量测试仪进行低速冲击研究,以模拟在运营服务中进行油底盘的影响事件。这旨在指出可能在结构中发生的损坏容差和失效机制。研究结果表明了设计在减震方面的显着贡献。具有保护性罗纹的特定油底壳设计与优质材料相结合,显着提高了抗冲击性。本文提供了关于实验和有限元分析调查的结果和讨论,在结束时结束了一些评论。

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