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首页> 外文期刊>The International Journal of Advanced Manufacturing Technology >Investigating the recast layer formed during the laser trepan drilling of Inconel 718 using the Taguchi method
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Investigating the recast layer formed during the laser trepan drilling of Inconel 718 using the Taguchi method

机译:使用Taguchi方法研究在Inconel 718的激光Trepan钻孔期间形成的重铸层

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This paper presents an investigation into the recast layer formed during the laser trepan drilling of Inconel 718 by aNd:YAG laser. Laser drilling has evolved into the method of choice for the drilling of cooling holes in aerospace components. However, holes drilled with this particular technique are liable to display a variety of defects, including spattering, tapering, microcracks, and a recast layer. In order to meet the standards specified by the original engine manufacturer, this paper investigates the effects of the various laser drilling parameters on the recast layer thickness in the trepan drilling mode. A total of eight laser drilling parameters are considered in a series of experiments arranged using a Taguchi L18 orthogonal array. Taguchi analytical techniques are employed to establish the optimum set of parameters which yields a minimum recast layer thickness. The results indicate that the assist gas pressure, the peak power, and the focal position exert the greatest influence on the recast layer thickness. Having performed a confirmation experiment based on the initial Taguchi design experiments, the recast layer thickness is reduced further by adjusting the values of the assist gas pressure and the trepanning speed.
机译:本文介绍了对用Ndd:YAG激光对Inconel 718进行的激光冲孔钻削过程中形成的重铸层的研究。激光钻孔已经发展成为在航空航天部件上钻孔的首选方法。但是,用这种特殊技术钻出的孔容易出现各种缺陷,包括飞溅,逐渐变细,微裂纹和重铸层。为了满足原始发动机制造商指定的标准,本文研究了在trepan钻孔模式下各种激光钻孔参数对重铸层厚度的影响。在使用Taguchi L18正交阵列排列的一系列实验中,总共考虑了八个激光钻孔参数。 Taguchi分析技术用于建立最佳参数集,从而产生最小的重铸层厚度。结果表明,辅助气体压力,峰值功率和焦点位置对重铸层的厚度影响最大。根据最初的Taguchi设计实验进行了确认实验后,通过调整辅助气体压力和击穿速度的值可以进一步减小重铸层的厚度。

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