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Inconel 718的激光束钻孔及其对在室温和高温下通过静态单轴拉伸试验测定的力学性能的影响。

Laser Beam Drilling of Inconel 718 and Its Effect on Mechanical Properties Determined by Static Uniaxial Tensile Testing at Room and Elevated Temperatures.

作者信息

Petrů Jana, Pagáč Marek, Grepl Martin

机构信息

Department of Machining, Assembly and Engineering Metrology, Faculty of Mechanical Engineering, VSB-Technical University of Ostrava, 708 00 Ostrava, Czech Republic.

Honeywell International s.r.o., 148 00 Prague, Czech Republic.

出版信息

Materials (Basel). 2021 Jun 3;14(11):3052. doi: 10.3390/ma14113052.

Abstract

Particularly in the aerospace industry and its applications, recast layers and microcracks in base materials are considered to be undesirable side effects of the laser beam machining process, and can have a significant influence on the resulting material behavior and its properties. The paper deals with the evaluation of the affected areas of the Inconel 718 nickel-base superalloy after its drilling by a laser beam. In addition, measurements and analyses of the mechanical properties were performed to investigate how these material properties were affected. It is supposed that the mechanical properties of the base material will be negatively affected by this accompanying machining process phenomenon. As a verification method of the final mechanical properties of the material, static uniaxial tension tests were performed on experimental flat shape samples made of the same material (Inconel 718) and three different thicknesses (0.5/1.0/1.6 mm) which best represented the practical needs of aerospace sheet metal applications. There was one hole that was drilled with an angle of under 70° in the middle of the sample length. Additionally, there were several sets of samples for each material thickness that were drilled by both conventional and nonconventional methods to emphasize the effect of the recast layer on the base material. In total, 192 samples were evaluated within the experiment. Moreover, different tensile testing temperatures (room as 23 °C and elevated as 550 °C) were determined for all the circumstances of the individual experiments to simulate real operation load material behavior. As a result, the dependencies between the amount of the recast layer and the length of the microcracks observed after the material was machined by laser beam, and the decrease in the mechanical properties of the base material, were determined.

摘要

特别是在航空航天工业及其应用中,基材中的重铸层和微裂纹被认为是激光束加工过程中不良的副作用,并且会对最终材料性能及其特性产生重大影响。本文探讨了因科镍合金718镍基高温合金在激光束钻孔后的受影响区域评估。此外,还进行了力学性能的测量和分析,以研究这些材料性能是如何受到影响的。据推测,这种伴随加工过程出现的现象会对基材的力学性能产生负面影响。作为材料最终力学性能的验证方法,对由相同材料(因科镍合金718)制成的、三种不同厚度(0.5/1.0/1.6毫米)且最能代表航空航天钣金应用实际需求的实验扁平形状样品进行了静态单轴拉伸试验。在样品长度中间有一个钻孔角度小于70°的孔。此外,对于每种材料厚度,都有几组样品采用传统方法和非传统方法进行钻孔,以强调重铸层对基材的影响。在该实验中总共评估了192个样品。此外,针对各个实验的所有情况确定了不同的拉伸试验温度(室温23°C和高温550°C),以模拟实际运行载荷下材料的行为。结果确定了激光束加工材料后观察到的重铸层数量与微裂纹长度之间的相关性,以及基材力学性能的下降情况。

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