Experimental and Numerical Stress State Assesment in Refill Friction Stir Spot Welding Joints

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2021-12-01 DOI:10.2478/fas-2021-0006
Elżbieta Gadalińska, A. Kubit, T. Trzepieciński, G. Moneta
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引用次数: 2

Abstract

Abstract Refill Friction Stir Spot Welding (RFSSW) is a technology used for joining solid materials that was developed in Germany in 2002 by GKSS-GmbH as a variant of the conventional friction stir spot welding (FSSW) [1]. In the RFSSW technology, the welding tool consists of a fixed outer part and rotating inner parts, which are called a pin and a sleeve. The tool for RFSSW is designed to plasticize the material of the parts to be joined by means of a rotary movement. The design of the tool allows independent vertical movement of both elements of the welding tool. This allows obtaining spot welds without creating holes that could weaken the structure. The main advantage of RFSSW is the potential for replacing the technologies that add weight to the structure or create discontinuities, such as joining with screws or rivets. Thus, RFSSW has great potential in the automotive, shipbuilding and aviation industries. Furthermore, the technology can be used to join different materials that could not be connected using other joining methods. The main objective of this work is to understand the physical and mechanical aspects of the RFSSW method – including the residual stress state inside the weld and around the joint. The results of the investigations can help to determine optimal parameters that could increase the strength and fatigue performance of the joint and to prove the significant advantage of RFSSW connections over other types of joints. The work assumes the correlation of two mutually complementary investigation methods: numerical analyses and experimental studies carried out with diffraction methods. The comparison between numerical and experimental results makes potentially possible the determination of degree of fatigue degradation of the material by observing the macroscopic stress state and the broadening of the diffraction peak width (FWHM), which is an indicator of the existence of micro-stress related to the dislocation density and grain size.
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再填充搅拌摩擦点焊接头应力状态的实验与数值评估
摘要重新填充搅拌摩擦点焊(RFSSW)是2002年由德国GKSS-GmbH公司开发的一种用于连接固体材料的技术,是传统搅拌摩擦点焊(FSSW)[1]的变体。在RFSSW技术中,焊接工具由固定的外部部件和旋转的内部部件组成,称为销和套。RFSSW的工具被设计为通过旋转运动使要连接的部件的材料塑化。该工具的设计允许焊接工具的两个元件独立垂直运动。这样可以获得点焊,而不会产生可能削弱结构的孔。RFSSW的主要优点是可以取代增加结构重量或造成不连续性的技术,例如用螺钉或铆钉连接。因此,RFSSW在汽车、造船和航空工业中具有巨大的潜力。此外,该技术可用于连接其他连接方法无法连接的不同材料。这项工作的主要目的是了解RFSSW方法的物理和机械方面-包括焊缝内部和接头周围的残余应力状态。研究结果可以帮助确定可以提高连接强度和疲劳性能的最佳参数,并证明RFSSW连接比其他类型的连接具有显著优势。这项工作假定了两种相互补充的调查方法的相关性:数值分析和用衍射方法进行的实验研究。通过数值与实验结果的比较,可以通过观察宏观应力状态和衍射峰宽度(FWHM)的增宽来确定材料的疲劳退化程度,FWHM是与位错密度和晶粒尺寸有关的微应力存在的标志。
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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%
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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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