聚丙烯复合材料增强铝蜂窝芯的力学和摩擦学性能

Panneerselvam K
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摘要

新型聚合物基复合材料的开发不断增加,以满足工业需求。本文采用铝蜂窝芯结构增强聚丙烯,研制了一种新型复合材料,并对其力学性能和摩擦学性能进行了表征。对聚丙烯增强铝蜂窝芯的拉伸强度、弯曲强度、冲击强度和硬度等力学性能进行了研究,结果表明,与纯聚丙烯增强铝蜂窝芯相比,其力学性能有明显改善。采用双体磨料磨损试验对铝蜂窝芯结构增强聚丙烯复合材料进行了摩擦学表征。在干接触条件下,采用销盘式磨损试验机进行磨粒磨损试验。设计过程参数考虑法向载荷、滑动速度、滑动距离和砂纸粒度,响应参数考虑摩擦系数和比磨损率。本研究采用L9正交阵列设计实验。最小摩擦系数的最佳工艺参数组合为:30 N法向载荷、1.046 m/秒滑动速度、450 m滑动距离和320粒磨砂纸;30 N载荷、1.569 m/秒滑动速度、450 m滑动距离和400粒磨砂纸,通过方差分析得到最小比磨损率。摩擦系数受法向载荷、磨粒大小的影响较大。比磨损率受滑动距离、正常载荷的显著影响。磨损表面的光学显微镜分析表明,铝蜂窝芯与聚丙烯之间存在良好的粘结性和磨粒性磨损机制
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Mechanical and Tribological Behavior of Aluminum Honeycomb Core Reinforced with Polypropylene Composite
Development of new Polymeric Matrix Composite are continuously increasing to meet out the industrial needs. In this paper new composite was developed by Aluminum Honeycomb Core structure was reinforced Polypropylene and it was characterized for mechanical and tribological properties. The characterization of mechanical properties like tensile strength, flexural strength, Impact strength and hardness of Aluminium honeycomb core reinforced with Polypropylene has been investigated over pure Polypropylene shows remarkable improvement in mechanical properties. Also in the Tribological characterization was done by using two-body abrasive wear test for the Aluminum Honeycomb Core structure reinforced Polypropylene composite. Abrasive wear experiments were conducted using a pin-on-disc wear tester under dry contact condition. Normal load, sliding velocity, sliding distance and abrasive paper grit size are considered as the design processes parameters and Coefficient Of Friction& Specific Wear Rate are considered as the responses. The design of experiments are based on L9 Orthogonal array used for this study. The optimum combination of process parameters for minimum Coefficient Of Friction are 30 N normal load, 1.046 m/sec sliding velocity, 450 m sliding distance and 320 grit size of abrasive paper and 30 N load, 1.569 m/sec sliding velocity, 450 m sliding distance and 400 grit size of abrasive gives minimum specific wear rate was obtained by using Analysis of Variance. Coefficient of friction is significantly influenced by the normal load, grit size. Specific wear rate is significantly influenced by sliding distance, normal load. Optical microscopy of worn surfaces revealed that wear mechanism is adhesive and abrasive, and there was a good bonding between Aluminium honeycomb core and Polypropylene
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