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在涂覆有陶瓷热障涂层的镍基高温合金中使用皮秒超短脉冲激光进行深孔冲击钻削。

Percussion Drilling of Deep Holes Using Picosecond Ultrashort Pulse Laser in Ni-Based Superalloy Coated with Ceramic Thermal Barrier Coatings.

作者信息

Liu Haodong, Zhao Wanqin, Wang Lingzhi, Shen Xiaowei, Wang Ning, Wang Xu

机构信息

School of Materials Engineering, Shanghai University of Engineering Science, Shanghai 201620, China.

State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an 710049, China.

出版信息

Materials (Basel). 2020 Aug 13;13(16):3570. doi: 10.3390/ma13163570.

Abstract

Ni-based superalloy with ceramic thermal barrier coatings (TBCs) is a composite material, which can be used in special environments with high temperature and high pressure such as aeroengine blade. In order to improve the cooling effect of the aeroengine, it is necessary to perform multi-size and large-area holes processing on the surface of blades. As a non-contact processing method with fast processing speed, good processing quality and almost no deformation, laser processing has been one of the important processing methods for film cooling hole processing of aeroengine blades. Percussion drilling is presented using picosecond ultrashort pulse laser in order to explore processing of deep holes in Ni-based superalloy, ceramic TBCs, and ceramic TBCs/substrate multilayer material. The effects of pulses, threshold and wavelength on hole diameter have been discussed, and the experiment on the deep hole ablation with 1064 nm wavelength has been performed. By analyzing the hole size and morphological characteristics of multiple processing parameters, the variation of hole cylindricity is obtained. A high-quality hole, without spatters around the periphery of hole entrance and without recast layer on the side-wall surface, in Ni-based superalloy coated with ceramic TBCs has been drilled. This research has potential applications to blade film cooling holes.

摘要

带有陶瓷热障涂层(TBCs)的镍基高温合金是一种复合材料,可用于航空发动机叶片等高温高压特殊环境。为提高航空发动机的冷却效果,有必要在叶片表面进行多尺寸、大面积的打孔加工。激光加工作为一种加工速度快、加工质量好且几乎无变形的非接触加工方法,一直是航空发动机叶片气膜冷却孔加工的重要加工方法之一。为探索镍基高温合金、陶瓷热障涂层以及陶瓷热障涂层/基体多层材料中深孔的加工,采用皮秒超短脉冲激光进行了冲击钻孔。讨论了脉冲、阈值和波长对孔径的影响,并进行了波长为1064nm的深孔烧蚀实验。通过分析多种加工参数下的孔尺寸和形貌特征,得到了孔圆柱度的变化情况。在涂覆陶瓷热障涂层的镍基高温合金上钻出了高质量的孔,孔入口周边无飞溅物,侧壁表面无重铸层。该研究在叶片气膜冷却孔方面具有潜在应用价值。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/89d6/7475972/02c41593ebfc/materials-13-03570-g001.jpg

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