不同试样尺寸的选择性激光熔融铬镍铁合金718的微观结构和力学性能

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2020-11-07 DOI:10.2478/fas-2020-0002
Bartosz Madejski, Maciej Malicki, Sławomir Czarnewicz, K. Gruber
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引用次数: 2

摘要

摘要选择性激光熔化(SLM)属于增材制造技术的一类,这些技术在航空航天工业中的应用越来越多。本研究介绍了选择性激光熔化铬镍铁合金718的微观结构和力学性能的测试结果。测试是针对不同几何形状(厚度、形状)的样品进行的。研究表明,试样的尺寸和印刷方向对微观结构和力学性能的影响。在微观结构研究中,使用了光学显微镜和扫描电子显微镜。微观结构研究包括晶粒尺寸和碳化物含量的测量。为了估计孔隙度,使用了计算机断层扫描。拉伸试验在室温下进行。结果表明,不同尺寸试样的力学性能和微观结构性能存在差异。
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Microstructural And Mechanical Properties Of Selective Laser Melted Inconel 718 For Different Specimen Sizes
Abstract Selective laser melting (SLM) falls into the category of additive manufacturing technologies that are being increasingly used in the aerospace industry. This study presents the results of the examination of the microstructure and mechanical properties of selective laser melted Inconel 718. The tests were carried out for samples of different geometry (thickness, shape). The investigation showed the effect of the specimen’s size and the printing direction on the microstructure and mechanical properties. In the microstructural investigation, light and scanning electron microscopes were used. The microstructure investigation included measurements of the grain size and the carbides’ content. In order to estimate porosity computer tomography was used. Tensile tests were carried out at room temperature. The results showed differences in mechanical and microstructural properties of different size specimens.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
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0.00%
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0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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