航空钢与奥氏体不锈钢自熔PCGTA焊接件的抗拉强度和冲击韧性表征

M. Arivarasu, K. D. Ramkumar, N. Arivazhagan
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引用次数: 5

摘要

本文报道了脉冲电流气体钨弧焊AISI 4340和AISI 304L的冶金性能和力学性能。本文采用光学显微镜和扫描电镜技术详细研究了焊接件的组织-性能关系。显微组织研究证实,AISI 4340在焊接区和热影响区形成马氏体,室温下硬度和强度较高。拉伸研究推断,在环境和高温条件下(600◦C),破坏分别发生在母材和焊缝区域。焊接接头在常温和高温下的平均抗拉强度分别为708 MPa、308 MPa。夏比v型缺口研究表明,由于焊缝处存在马氏体组织,焊缝的平均冲击能为6.2 J。研究结果证明使用自脉冲电流气体钨极电弧焊,消除了填充丝的需要,这是连接这些不同金属组合的经济有效的焊接技术。航空用钢,奥氏体不锈钢,脉冲电流,显微组织,力学特性
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Characterization of tensile strength and impact toughness of autogenous PCGTA weldments of aeronautical steel and austenitic stainless steel
This research article reports the metallurgical and mechanical properties of pulsed current gas tungsten arc welded AISI 4340 and AISI 304L by autogenous technique. This article investigates the detailed structure-property relationship of the weldments using optical and scanning electron microscopy techniques. Microstructure studies corroborated the formation of martensite at the weld zone and heat affected zone of AISI 4340, which contributed to higher hardness and strength at room temperature. Tensile studies inferred that the failure occurred at the parent metal and in the weld region when operated at ambient and high-temperature conditions (600◦C), respectively. The average tensile strength of the welded joint was found to be 708 MPa, 308 MPa in the ambient temperature and elevated temperature, respectively. Charpy V-notch studies revealed that the average impact energy of the weldments was found to be 6.2 J, due to the presence of martensitic structure at the weld. The outcomes of the study attested the use of autogenouspulsed current gas tungsten arc welding, eliminating the need for filler wire, which is cost effective welding technique for joining these dissimilar metal combinations. K e y w o r d s: aeronautical steel, austenitic stainless steel, pulsed current, microstructure, mechanical characterization
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