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Fatigue strength of AL-6XN stainless steel weldments.

机译:AL-6XN不锈钢焊件的疲劳强度。

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摘要

This study presents an assessment of the fatigue strength limit state of large scale welded joints fabricated from nonmagnetic AL-6XN superaustenitic stainless steel. Three welded details were tested under constant amplitude loading, subjected to both compressive and tensile stresses. The experimental program included longitudinal fillet welds, transverse groove welds, and simulated bulkhead attachments. Fabrication was of shipyard quality using the GMAW weld process. Two Ni-based weld metals, IN625 and IN622, were used. A total of 66 large-scale I-beams were tested. Over 186 fatigue cracks were observed, resulting in 82 through flange thickness fatigue cracks used in the assessment of fatigue strength, in addition to many uncracked details related to the constant amplitude fatigue limit (CAFL).; Discontinuities associated with initiation of fatigue cracks were identified from the fracture surfaces and included: lack of fusion areas at the weld root of longitudinal fillet welds; internal lack of fusion planes, internal volumetric discontinuities, and micro-discontinuities at the reinforcement weld toe of transverse groove welds; and micro-discontinuities (tears or inclusions) at the bulkhead attachment weld toe in combination with regions of sharp weld toe reentry angle.; Fatigue strength was evaluated analytically using fracture mechanics concepts. Initial discontinuities and fatigue propagation behavior observed during the experimental program were used to assess the fatigue strength of longitudinal fillet welds and simulated bulkhead attachments. The analytical models attempt to estimate the lower bound finite life fatigue strength curves for the longitudinal fillet weld and bulkhead attachment details, as well as the CAFL. Based on the experimental and analytical results, the following design recommendations were made: (1) Use AASHTO Category B for standard double sided longitudinal fillet welds, with a CAFL of 100 MPa. (2) Use AASHTO Category C for transverse groove welds subjected to nondestructive evaluation to avoid large internal defects, with a CAFL of 83 MPa. (3) Use AASHTO Category E for 200 mm long bulkhead attachments, with a CAFL of 41 MPa. (4) Use AASHTO fatigue classification categories to develop preliminary fatigue resistance curves for details not yet tested with AL-6XN stainless steel.
机译:这项研究提出了由非磁性AL-6XN超奥氏体不锈钢制成的大规模焊接接头的疲劳强度极限状态的评估。在恒定振幅载荷下,对三个焊接零件进行了测试,使其承受压缩应力和拉伸应力。实验程序包括纵向角焊缝,横向坡口焊缝和模拟舱壁附件。使用GMAW焊接工艺可以达到造船厂的质量。使用了两种Ni基焊接金属IN625和IN622。总共测试了66个大型工字梁。 ;观察到超过186个疲劳裂纹,除了用于与恒定振幅疲劳极限(CAFL)相关的许多完整细节之外,还产生了82个贯穿凸缘厚度的疲劳裂纹,用于评估疲劳强度。从断裂表面发现了与疲劳裂纹萌生有关的不连续性,包括:纵向角焊缝焊缝根部缺乏熔合区;内部缺乏熔合平面,内部体积不连续性以及横向槽焊缝的增强焊趾处的微观不连续性;舱壁附件焊趾处的微不连续性(眼泪或夹杂物)与锐利的焊趾折返角区域结合在一起;使用断裂力学概念对疲劳强度进行了分析评估。在实验程序中观察到的初始不连续性和疲劳传播行为用于评估纵向角焊缝和模拟舱壁附件的疲劳强度。分析模型试图估计纵向角焊缝和舱壁附件细节以及CAFL的下限有限寿命疲劳强度曲线。根据实验和分析结果,提出了以下设计建议:(1)将AASHTO B类用于标准双面纵向角焊缝,CAFL为100 MPa。 (2)将AASHTO C类用于经过无损评估的横向坡口焊缝,以避免较大的内部缺陷,CAFL为83 MPa。 (3)将AASHTO E类用于200 mm长的舱壁附件,CAFL为41 MPa。 (4)使用AASHTO疲劳分类类别为尚未使用AL-6XN不锈钢测试的细节建立初步的疲劳强度曲线。

著录项

  • 作者

    Metrovich, Brian.;

  • 作者单位

    Lehigh University.;

  • 授予单位 Lehigh University.;
  • 学科 Engineering Civil.; Applied Mechanics.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2004
  • 页码 224 p.
  • 总页数 224
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 建筑科学;应用力学;机械、仪表工业;
  • 关键词

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