Electropolishing Procedure Dedicated to In-Depth Stress Measurements with X-Ray Diffractometry

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2016-06-01 DOI:10.1515/fas-2016-0004
Elżbieta Gadalińska, Wojciech Wronicz
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引用次数: 2

Abstract

Abstract Electropolishing is the sole reliable method of removing the outer layer of the specimen without changing its stress state. This feature of the electropolishing procedure allows researchers to investigate the in-depth stress distribution. Developing of the method in a diffraction laboratory is crucial because there is no universal theory for the electropolishing procedure allowing the removal of the layers of different thickness. This is due to the multiplicity of different factors affecting the electropolishing results. A factor of vital importance from the point of view of indepth stress measurements is the thickness of the electropolishing layer. Hence the importance of the procedures for the electropolishing of a layer of a precisely defined thickness. This work deals with the problem of the selection of the parameters in the electropolishing process for two types of materials: stainless steel and aluminium alloy. The tests of mutual correlation of current intensity, voltage applied and time of the procedure and its results are presented in the paper.
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电抛光程序专用于x射线衍射法的深度应力测量
电抛光是去除试样外层而不改变其应力状态的唯一可靠方法。电抛光过程的这一特点使研究人员能够深入研究应力分布。在衍射实验室中开发这种方法是至关重要的,因为目前还没有通用的理论用于电抛光过程,允许去除不同厚度的层。这是由于影响电抛光结果的不同因素的多样性。从深度应力测量的角度来看,一个至关重要的因素是电抛光层的厚度。因此,精确定义厚度的层的电抛光程序的重要性。本文研究了不锈钢和铝合金两种材料电抛光工艺参数的选择问题。本文介绍了电流强度、施加电压和操作时间的相互关系试验及其结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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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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