Al-Mg-Mn-Sc-Zr alloys with excellent weldability have emerged as ideal candidates for aerospace applications.Currently,the investigations on the corrosion behavior of alloys under tungsten inert gas(TIG)welding condit...Al-Mg-Mn-Sc-Zr alloys with excellent weldability have emerged as ideal candidates for aerospace applications.Currently,the investigations on the corrosion behavior of alloys under tungsten inert gas(TIG)welding conditions are insufficient.Here,the stress corrosion cracking(SCC)behavior of base metal(BM)and weld zone(WZ)of TIG welded Al-Mg-Mn-Sc-Zr alloys was investigated by using pre-cracked compact tensile samples immersed in 3.5%NaCl solution.The direct current potential drop(DCPD)method was used to record the crack propagation.The microstructure and fracture morphology of different regions of TIG welded joints were studied by SEM,EBSD and TEM,and the SCC crack propagation mechanism of BM and WZ was analyzed.The results demonstrated that the critical stress intensity factor for stress corrosion cracking(K_(ⅠSCC))of BM and WZ was 7.05 MPa·m_(1/2) and 11.79 MPa·m_(1/2),respectively.Then,the crack propagation rate of BM was faster than that of WZ,and BM was more susceptible to SCC than WZ.Additionally,the fracture mode of the BM mainly exhibited transgranular fracture,while the fracture mode of the WZ mainly exhibited intergranular and transgranular mixed fracture.Moreover,SCC crack propagation was attributed to the combined effect of anodic dissolution and hydrogen embrittlement.This study will provide experimental and theoretical basis for the wide application of TIG welded Al-Mg-Mn-Sc-Zr alloys in aerospace.展开更多
针对厚度为4 mm的2219-T87铝合金进行惰性气体钨极保护焊(Tungsten inert gas arcwelding,TIGAW)试验研究,分析焊缝的组织结构及力学性能。拉伸试验结果显示,接头试样平均屈服强度为母材的49.3%,平均抗拉强度为母材的67.8%,断后伸长率...针对厚度为4 mm的2219-T87铝合金进行惰性气体钨极保护焊(Tungsten inert gas arcwelding,TIGAW)试验研究,分析焊缝的组织结构及力学性能。拉伸试验结果显示,接头试样平均屈服强度为母材的49.3%,平均抗拉强度为母材的67.8%,断后伸长率为母材的18.5%。测试了焊接试样各区域的显微硬度,测试结果表明焊缝区域硬度高于其他部位,其中熔合线和热影响区之间的显微硬度最低,同时焊接试样的整体区域硬度均比母材低。对焊接试样进行腐蚀试验,发现接头焊缝区抗腐蚀能力明显强于母材。要提高2219铝合金焊接性能,需改进焊接工艺,减少熔合区以及热影响区的粗大晶粒的形成,解决CuAl2相的偏析等问题。展开更多
基金Project (2023GK1080) supported by the Major Special Projects of Hunan Province of China。
文摘Al-Mg-Mn-Sc-Zr alloys with excellent weldability have emerged as ideal candidates for aerospace applications.Currently,the investigations on the corrosion behavior of alloys under tungsten inert gas(TIG)welding conditions are insufficient.Here,the stress corrosion cracking(SCC)behavior of base metal(BM)and weld zone(WZ)of TIG welded Al-Mg-Mn-Sc-Zr alloys was investigated by using pre-cracked compact tensile samples immersed in 3.5%NaCl solution.The direct current potential drop(DCPD)method was used to record the crack propagation.The microstructure and fracture morphology of different regions of TIG welded joints were studied by SEM,EBSD and TEM,and the SCC crack propagation mechanism of BM and WZ was analyzed.The results demonstrated that the critical stress intensity factor for stress corrosion cracking(K_(ⅠSCC))of BM and WZ was 7.05 MPa·m_(1/2) and 11.79 MPa·m_(1/2),respectively.Then,the crack propagation rate of BM was faster than that of WZ,and BM was more susceptible to SCC than WZ.Additionally,the fracture mode of the BM mainly exhibited transgranular fracture,while the fracture mode of the WZ mainly exhibited intergranular and transgranular mixed fracture.Moreover,SCC crack propagation was attributed to the combined effect of anodic dissolution and hydrogen embrittlement.This study will provide experimental and theoretical basis for the wide application of TIG welded Al-Mg-Mn-Sc-Zr alloys in aerospace.
文摘针对厚度为4 mm的2219-T87铝合金进行惰性气体钨极保护焊(Tungsten inert gas arcwelding,TIGAW)试验研究,分析焊缝的组织结构及力学性能。拉伸试验结果显示,接头试样平均屈服强度为母材的49.3%,平均抗拉强度为母材的67.8%,断后伸长率为母材的18.5%。测试了焊接试样各区域的显微硬度,测试结果表明焊缝区域硬度高于其他部位,其中熔合线和热影响区之间的显微硬度最低,同时焊接试样的整体区域硬度均比母材低。对焊接试样进行腐蚀试验,发现接头焊缝区抗腐蚀能力明显强于母材。要提高2219铝合金焊接性能,需改进焊接工艺,减少熔合区以及热影响区的粗大晶粒的形成,解决CuAl2相的偏析等问题。
