首页> 外文期刊>Composite Structures >Experimental studies on a two-step technique to reduce delamination damage during milling of large diameter holes in CFRP/Al stack
【24h】

Experimental studies on a two-step technique to reduce delamination damage during milling of large diameter holes in CFRP/Al stack

机译:减少CFRP / Al叠层中大直径孔铣削过程中分层损坏的两步法实验研究

获取原文
获取原文并翻译 | 示例
           

摘要

Non-conventional hole-making machining processes are being adopted to manufacture holes in the difficult to cut materials like carbon fiber reinforced polymer (CFRP) composites. Of the many non-conventional processes, helical milling remains the most favorable and the best alternative to conventional drilling. It possesses several advantages including low cutting forces, reduced tool wear and improved hole quality. The use of composites in conjunction with metals is very common in aerospace industry and the most common configurations are CFRP/Al and CFRP/Ti-6Al-4V. In this work, a two step process for helical milling in CFRP/Al stack is proposed and experimented then the results are compared with that of conventional drilling. In the first step, milling is done on the CFRP/Al stack starting on the composite part then the workpiece is flipped so that in the second step milling starts on the metal part. Results show that helical milling reduces axial forces by about 35% compared to that of conventional drilling. The forces involved in the second step were found to be about 25% less than that of the first step in the helical milling process. Reduction in forces consequently leads to less damage as scanning electron microscope (SEM) images of the machined holes show.
机译:正在采用非常规的制孔加工工艺在难切削的材料(如碳纤维增强聚合物(CFRP)复合材料)中制造孔。在许多非常规过程中,螺旋铣削仍然是常规钻孔的最有利和最佳替代方法。它具有几个优点,包括低切削力,减少刀具磨损和改善孔质量。复合材料与金属结合使用在航空航天工业中非常普遍,最常见的配置是CFRP / Al和CFRP / Ti-6Al-4V。在这项工作中,提出了在CFRP / Al堆中进行螺旋铣削的两步过程,并进行了实验,然后将结果与常规钻孔进行了比较。第一步,从复合零件开始在CFRP / Al叠层上进行铣削,然后翻转工件,以便在第二步中在金属零件上开始铣削。结果表明,与常规钻孔相比,螺旋铣削可将轴向力降低约35%。在螺旋铣削过程中,发现第二步所涉及的力比第一步低约25%。因此,如加工孔的扫描电子显微镜(SEM)图像所示,力的减小导致较小的损坏。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号