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Laser Ablative Surface Treatment for Enhanced Bonding of Ti-6AI-4V Alloy

机译:激光烧蚀表面处理可增强Ti-6Al-4V合金的结合力

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Adhesive bonding offers many advantages over mechanical fastening, but requires certification before it can be incorporated in primary structures for commercial aviation without disbond-arrestment features or redundant load paths. Surface preparation is widely recognized as the key step to producing robust and predictable adhesive bonds. Surface preparation by laser ablation provides an alternative to the expensive, hazardous, polluting, and less precise practices used currently such as chemical-dip, manual abrasion and grit blast. This report documents preliminary testing of a surface preparation technique using laser ablation as a replacement for the chemical etch and abrasive processes currently applied to Ti-6Al-4V alloy adherends. Surface roughness and surface chemical composition were characterized using interference microscopy and X-ray photoelectron spectroscopy, respectively. A technique for fluorescence visualization was developed which allowed for quantitative failure mode analysis. Wedge crack extension testing in a hot, humid environment indicated the relative effectiveness of various surface treatments. Increasing ablation duty cycle reduced crack propagation and adhesive failure. Single lap shear testing showed an increase in strength and durability as laser ablation duty cycle and power were increased. Chemical analyses showed trends for surface chemical species, which correlated with improved bond strength and durability.
机译:粘接比机械紧固具有许多优势,但是要在没有防粘扣功能或多余的载荷路径的情况下将其结合到商用航空的主要结构中,就需要进行认证。表面处理被公认为是产生牢固且可预测的粘合剂粘结的关键步骤。通过激光烧蚀进行的表面处理为目前使用的昂贵,危险,污染和不太精确的操作提供了替代方法,例如化学浸涂,手动磨蚀和喷砂处理。该报告记录了使用激光烧蚀替代目前应用于Ti-6Al-4V合金被粘物的化学蚀刻和研磨工艺的表面制备技术的初步测试。使用干涉显微镜和X射线光电子能谱分别表征表面粗糙度和表面化学组成。开发了用于荧光可视化的技术,其允许定量失效模式分析。在炎热潮湿的环境中进行楔形裂纹扩展测试表明了各种表面处理的相对有效性。增大烧蚀占空比可减少裂纹扩展和粘合失败。单圈剪切试验表明,随着激光烧蚀占空比和功率的增加,强度和耐久性得到提高。化学分析显示了表面化学物质的趋势,这与提高的粘合强度和耐久性相关。

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