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Fatigue strength of tungsten inert gas-repaired weld joints in airplane critical structures

机译:飞机关键结构中钨极惰性气体修复的焊接接头的疲劳强度

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摘要

In this work the effect of Gas Tungsten Arc Welding (GTAW) repairs on the axial fatigue strength of an AISI 4130 steel welded joint used in airframe critical to the flight-safety was investigated. Fatigue tests were performed at room temperature on 0.89 mm thick hot-rolled plates with constant amplitude and load ratio of R = 0.1, at 20 Hz frequency. Monotonic tensile tests, optical metallography and microhardness, residual stress and weld geometric factors measurements were also performed. The fatigue strength decreased with the number of GTAW repairs, and was related to microstructural and microhardness changes, as well as residual stress field and weld profile geometry factors, which gave origin to high stress concentration at the weld toe. (C) 2011 Elsevier B.V. All rights reserved.
机译:在这项工作中,研究了气体钨极电弧焊(GTAW)修复对飞机机身中对飞行安全至关重要的AISI 4130钢焊接头的轴向疲劳强度的影响。在室温下对0.89毫米厚的热轧板进行疲劳测试,该板具有恒定的振幅,并且负载比为R = 0.1,频率为20 Hz。还进行了单调拉伸试验,光学金相和显微硬度,残余应力和焊缝几何因子测量。疲劳强度随着GTAW修补次数的增加而降低,并且与显微组织和显微硬度的变化以及残余应力场和焊缝轮廓几何因子有关,这是导致焊趾处应力集中的原因。 (C)2011 Elsevier B.V.保留所有权利。

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