Tandecka Katarzyna, Kacalak Wojciech, Szafraniec Filip, Wieczorowski Michał, Mathia Thomas G
Department of Engineering and Informatics Systems, Faculty of Mechanical Engineering and Energy, Koszalin University of Technology, 75-620 Koszalin, Poland.
Faculty of Mechanical Engineering, Institute of Applied Mechanics, Poznan University of Technology, 3 Piotrowo St., 60-965 Poznan, Poland.
Materials (Basel). 2024 May 18;17(10):2430. doi: 10.3390/ma17102430.
This study investigates the surface topography of microfinishing abrasive films and their machining capability on the Nimonic 80A superalloy, a high-performance nickel-based alloy commonly used in aerospace and gas turbine engine applications. Surface analysis was conducted on three abrasive films with nominal grain sizes of 30, 15, and 9 μm, exploring wear patterns, contact frequency, and distribution. To assess the distribution of grain apexes, Voronoi cells were employed. Results revealed distinct wear mechanisms, including torn abrasive grains and cracked bond surfaces, highlighting the importance of efficient chip removal mechanisms in microfinishing processes. Larger grain sizes exhibited fewer contacts with the workpiece but provided more storage space for machining products, while smaller grain sizes facilitated smoother surface finishes. The research demonstrated the effectiveness of microfinishing abrasive films in reducing surface irregularities. Additionally, surface analysis of worn abrasive tools provided insights into wear mechanisms and chip formation, with the segmentation of microchips contributing to efficient chip removal. These findings underscore the significance of selecting appropriate abrasive films and implementing effective chip removal mechanisms to optimize microfinishing processes and improve surface finishing quality in advanced material machining applications. It is worth emphasizing that no prior research has investigated the microfinishing of components crafted from Nimonic 80A utilizing abrasive films, rendering this study truly unique in its contribution to the field.
本研究调查了微精整磨料薄膜的表面形貌及其对Nimonic 80A高温合金的加工能力,Nimonic 80A是一种常用于航空航天和燃气轮机发动机应用的高性能镍基合金。对三种标称粒度分别为30、15和9μm的磨料薄膜进行了表面分析,探究了磨损模式、接触频率和分布情况。为了评估晶粒顶点的分布,采用了Voronoi单元。结果揭示了不同的磨损机制,包括磨粒撕裂和粘结表面开裂,突出了微精整过程中高效切屑去除机制的重要性。较大的粒度与工件的接触较少,但为加工产物提供了更多的存储空间,而较小的粒度有助于获得更光滑的表面光洁度。该研究证明了微精整磨料薄膜在减少表面不规则性方面的有效性。此外,对磨损磨具的表面分析为磨损机制和切屑形成提供了见解,微切屑的分割有助于高效切屑去除。这些发现强调了选择合适的磨料薄膜和实施有效的切屑去除机制对于优化微精整过程以及提高先进材料加工应用中的表面光洁度质量的重要性。值得强调的是,此前没有研究调查过利用磨料薄膜对由Nimonic 80A制成的部件进行微精整,因此本研究在该领域的贡献具有独特性。