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Effect of microstructures on notch fatigue properties in ultra-high strength steel sheet welded joint

机译:显微组织对超高强度钢板焊接接头缺口疲劳性能的影响

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The fatigue properties of different regions, namely, the weld metal (WM), the fusion line (FL) and the fine grain heat affected zone (FGHAZ), in welded joints with different surface notch root radii r = 0.1, 0.2 and 0.3 mm were investigated by using welded joints of 980 MPa grade ultra-high strength steel sheets with a thickness of 2.3 mm. The fatigue strength of the FGHAZ was higher than those of the WM and FL despite the lower hardness of the FGHAZ, while the effect of the microstructure became prominent at r >= 0.2 mm, where the stress concentration factor K-t <= 2.24. The strain gauge measurement and FE analysis imply that the effect of the microstructure arose only within 50 mu m from the surface of the notch. In addition, the critical distance approach was applied to evaluate the relationship between the effective stress range Delta sigma(eff) and the number of cycles to faliure N-f. As a result, the critical distance L of WM, FL and FGHAZ were 37.2, 59.7 and 26.7 mu m, respectively. The fracture surface and cross-secctional observation suggested that fatigue cracks of WM and FL initiated at twin or prior austenite grain boundaries, then propagated along martensite laths in the crystallographic propagation stage (Stage I). In contrast, the fatigue cracks of FGHAZ initiated inside ferrite grains, and then the fine grain boundaries and martensite-austenite of the FGHAZ blocked and branched the cracks. These results can explain the fatigue strength reversal phenomenon with respect to the hardness of the FGHAZ.
机译:在具有不同表面缺口根半径r = 0.1、0.2和0.3 mm的焊接接头中,不同区域的疲劳特性,即焊接金属(WM),熔合线(FL)和细晶粒热影响区(FGHAZ)通过使用厚度为2.3 mm的980 MPa级超高强度钢板的焊接接头进行了研究。尽管FGHAZ的硬度较低,但FGHAZ的疲劳强度仍比WM和FL的高,而在r> = 0.2 mm时,应力集中因子K-t <= 2.24时,微观结构的影响变得明显。应变仪的测量和有限元分析表明,微观结构的影响仅出现在缺口表面50微米以内。此外,采用临界距离方法评估了有效应力范围Delta sigma(eff)与破坏N-f的循环次数之间的关系。结果,WM,FL和FGHAZ的临界距离L分别为37.2、59.7和26.7μm。断裂表面和横断面观察表明,WM和FL的疲劳裂纹始于双相或先前的奥氏体晶界,然后在晶体学扩展阶段(第一阶段)沿马氏体板条扩展。相比之下,FGHAZ的疲劳裂纹在铁素体晶粒内部产生,然后FGHAZ的细晶界和马氏体-奥氏体阻塞并分支了裂纹。这些结果可以解释关于FGHAZ的硬度的疲劳强度反转现象。

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