首页> 外文会议>SAMPE Long Beach Conference and Exhibition >A LASER INTERFERENCE-BASED SURFACE TREATMENT OF ALUMINUM AND CARBON FIBER POLYMER COMPOSITES FOR ENHANCED BONDING
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A LASER INTERFERENCE-BASED SURFACE TREATMENT OF ALUMINUM AND CARBON FIBER POLYMER COMPOSITES FOR ENHANCED BONDING

机译:基于激光干涉的铝和碳纤维聚合物复合材料的表面处理,用于增强粘接

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Due to its increased use in the automotive and aerospace industries, joining of Carbon Fiber-reinforced Polymer matrix Composites (CFPC) to metals demands enhanced surface preparation and control of surface morphology prior to joining. In this study, surfaces of both composite and aluminum were prepared for joining using a new laser based technique, in which the laser interference power profile was created by splitting the beam and guiding those beams to the sample surface by overlapping each other with defined angles to each other. Results are presented for the overlap shear testing of single-lap joints made with Al 5182 and CFPC specimens whose surfaces prepared by (a) surface abrasion and solvent cleaning; and (b) laser-interference structured surfaces by rastering with a 4 mm laser beam at approximately 3.5 W power. CFPC specimens of T700S carbon fiber, Prepreg - T70 epoxy, 4 or 5 ply thick, 0/90° plaques were used. Adhesive DP810 was used to bond Al and CFPC. The bondline was 0.25mm and the bond length was consistent among all joints produced. First, the effect of the laser speed on the joint performance was evaluated by laser-interference structure Al and CFPC surfaces with a beam angle of 3° and laser beam speeds of 3, 5, and 10 mm/s. For this sensitivity study, 3 joint specimens were used per each joint type. Based on the results for minimum, maximum, and mean values for the shear lap strength and maximum load for all the 9 joint types, two joint types were selected for further evaluations. Six additional joint specimens were prepared for these two joint types in order to obtain better statistics and the shear test data was presented for the range, mean, and standard deviation. The results for the single-lap shear tests obtained for six joint specimens, indicate that the shear lap strength, maximum load, and displacement at maximum load for those joints made with laser-interference structured surfaces were increased by approximately 14.8%, 16%, and 100%, respectively over those measured for the baseline joints. It was also found that joints made with laser-structured surfaces can absorb approximately 150% more energy than the baseline joints.
机译:由于其在汽车和航空航天行业的使用增加,碳纤维增强聚合物基质复合材料(CFPC)与金属的连接需要增强的表面制剂和加入前表面形态的控制。在该研究中,制备复合材料和铝的表面来使用新的激光基础技术来加入,其中通过将光束分割并通过用定义的角度重叠地将这些光束引导到样本表面来产生激光干涉功率曲线。彼此。提出了用Al 5182和CFPC样本制成的单圈接头的重叠剪切测试,其表面由(a)表面磨损和溶剂清洁制备; (b)激光干涉结构表面,通过在大约3.5W的电力下用4mm激光束光栅。使用T700S碳纤维的CFPC样品,预浸料 - T70环氧树脂,4或5倍厚,0/90°PLaques。粘合剂DP810用于键合Al和CFPC。粘合线为0.25mm,键长在所有产生的关节中一致。首先,激光干涉结构AL和CFPC表面的激光干扰结构AL和CFPC表面评估激光速度对关节性能的影响,光束角度为3°和3,5和10mm / s的激光束速度。对于这种敏感性研究,每个关节型使用3个关节标本。基于剪切圈强度和所有9个关节类型的最大负荷的最小,最大和平均值的结果,选择了两种关节类型以进一步评估。为这两个关节类型制备六种另外的关节标本,以获得更好的统计,并且剪切测试数据被呈现为范围,平均值和标准偏差。获得六个关节标本的单圈剪切试验的结果表明,使用激光干扰结构表面制成的那些接头的剪切圈强度,最大载荷和位移量增加了约14.8%,16%,和100%分别在测量基线关节的那些。还发现,使用激光结构表面制造的接头可以比基线接头吸收大约150%的能量。

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