用高穿透辐射研究激光粉末床熔合和选择性激光熔化部件

Q4 Engineering
Elżbieta Gadalińska, Łukasz Pawliszak, G. Moneta
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引用次数: 0

摘要

增量制造方法,即3D打印,近年来经历了显着的增长,无论是在现代技术的发展,致力于各种应用,以及在优化工艺本身的参数,以确保以这种方式生产的零件所需的机械和强度性能。目前,人们对使用高穿透性辐射寄予厚望,即同步加速器和/或中子辐射,用于定量识别3D打印产生的物体的特征参数。借助衍射方法,不仅可以获得用于优化3D打印过程的输入信息,还可以对现场打印过程进行监控。由于这些方法,有可能获得有关参数的信息,这些参数从应用这些获得的元素的角度来看是至关重要的,例如在打印过程中产生的应力本身以及打印后的残余应力。从抗拉强度、抗压强度和疲劳强度的角度来看,这个参数是至关重要的,它决定了将增量法生产的元件引入广泛工业应用的可能性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Laser Powder Bed Fusion and Selective Laser Melted Components Investigated with Highly Penetrating Radiation
Abstract Methods of incremental manufacturing, i.e. 3D printing, have been experiencing significant growth in recent years, both in terms of the development of modern technologies dedicated to various applications, and in terms of optimizing the parameters of the process itself so as to ensure the desired mechanical and strength properties of the parts produced in this way. High hopes are currently being pinned on the use of highly penetrating types of radiation, i.e. synchrotron and/or neutron radiation, for quantitative identification of parameters characterizing objects produced by means of 3D printing. Thanks to diffraction methodologies, it is feasible to obtain input information to optimize 3D printing procedures not only for finished prints but also to monitor in situ printing processes. Thanks to these methodologies, it is possible to obtain information on parameters that are critical from the perspective of application of such obtained elements as stresses generated during the printing procedure itself as well as residual stresses after printing. This parameter, from the point of view of tensile strength, compression strength as well as fatigue strength, is crucial and determines the possibility of introducing elements produced by incremental methods into widespread industrial use.
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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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