Application of Laboratory Diffraction Methods in Characterization of Elements Made By Additive SLM Methods – State of the Art

Q4 Engineering
Elżbieta Gadalińska, Łukasz Pawliszak, G. Moneta
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引用次数: 1

Abstract

Abstract The greatest challenge of widely developed incremental manufacturing methods today is to obtain, as a result of the manufacturing process, such components that will have acceptable strength properties from the point of view of a given application. These properties are indirectly determined by three key characteristics: the level of surface residual stress, the roughness of the component and its porosity. Currently, the efforts of many research groups are focused on the problem of optimizing the parameters of incremental manufacturing so as to achieve the appropriate level of compressive residual stress, the lowest possible porosity and the lowest possible roughness of parts obtained by 3D methods. It is now recognized that determining the level of these three parameters is potentially possible using experimental X-ray diffraction methods. The use of this type of radiation, admittedly, is only used to characterize the surface layer of elements, but its undoubted advantage is its easy availability and relatively low cost compared to experiments carried out using synchrotron or neutron radiation.
实验室衍射方法在添加剂SLM方法制备的元素表征中的应用——最新技术
目前广泛发展的增量制造方法面临的最大挑战是,作为制造过程的结果,从给定应用的角度来看,这些组件将具有可接受的强度特性。这些性能是由三个关键特征间接决定的:表面残余应力水平,部件的粗糙度及其孔隙率。目前,许多研究小组的努力都集中在优化增量制造的参数问题上,以便通过三维方法获得合适的压残余应力水平,尽可能低的孔隙率和尽可能低的粗糙度。现在人们认识到,用实验x射线衍射方法来确定这三个参数的水平是可能的。诚然,这种类型的辐射的使用仅用于表征元素的表层,但与使用同步加速器或中子辐射进行的实验相比,其无疑的优点是易于获得和相对较低的成本。
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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
自引率
0.00%
发文量
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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