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首页> 外文期刊>International Journal of Machine Tools & Manufacture: Design, research and application >Effect of beam angle on HAZ, recast and oxide layer characteristics in laser drilling of TBC nickel superalloys
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Effect of beam angle on HAZ, recast and oxide layer characteristics in laser drilling of TBC nickel superalloys

机译:束角对TBC镍超合金激光钻孔中热影响区,重铸和氧化层特性的影响

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摘要

Industrial applications of laser drilling include the production of cooling holes at acute angles in certain parts of the aero-engine components. These parts are often covered with ceramic thermal barrier coatings (TBC) to protect them from reaching excessive temperatures in hot engine environments. Acute angle TBC drilling brings three major simultaneous complications to the process. These are: (i) multi-layer drilling, (ii) non-symmetrical geometry and melt ejection, and (iii) increased depth of drilling. In a previous investigation by the authors, delamination of TBC was found as a main problem of angled drilling and mechanisms involved were studied. In the present study, implications of these difficulties on the hole quality is investigated through a comparative study of vertical and acute angle drilled holes. Characteristics of recast layer, heat-affected zone (HAZ), oxide layer and TBC delamination are investigated. Variation of these metallurgical characteristics with the depth of the hole is evaluated. Results for vertical and inclined holes are compared. The extent of HAZ, recast layer and oxide layer is seen to vary significantly with location and is found increasing with decreasing drilling angle to surface. Numerical simulation of pulsed laser heating of TBC Nimonic 263 was carried out for acute angle drilling with assist gas considerations. Results from the simulation suggested that the total heat transfer rate is higher on the leading edge side than the trailing edge of the heated region. Experimentally observed larger HAZ on leading edge side and larger recast layer on trailing edge side are explained by the analysis of heat flow characteristics obtained with the model.
机译:激光钻孔的工业应用包括在航空发动机部件的某些部分中以锐角生产冷却孔。这些零件通常覆盖有陶瓷热障涂层(TBC),以防止它们在高温的发动机环境中达到过高的温度。锐角TBC钻孔同时带来三个主要的复杂过程。它们是:(i)多层钻孔,(ii)非对称几何形状和熔体喷射,以及(iii)钻孔深度增加。在作者先前的调查中,TBC的分层被发现是成角度钻孔的主要问题,并研究了所涉及的机理。在本研究中,通过对垂直孔和锐角孔的比较研究来研究这些困难对孔质量的影响。研究了重铸层,热影响区(HAZ),氧化层和TBC分层的特性。评估这些冶金特性随孔深的变化。比较垂直孔和倾斜孔的结果。热影响区,重铸层和氧化层的范围随位置的变化而显着变化,并且随着对地面钻孔角度的减小而增加。考虑到辅助气体,对锐角钻孔进行了TBC Nimonic 263脉冲激光加热的数值模拟。模拟的结果表明,加热区域的前缘侧的总传热率高于后缘。通过对模型获得的热流特性进行分析,可以解释实验观察到的前缘较大的热影响区和后缘较大的重铸层。

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