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作 者:付鹏飞[1] 胡芳友[1] 崔爱永[1] 赵培仲[1] 卢长亮[1] 胡滨[1]
机构地区:[1]海军航空工程学院航空宇航科学与技术,山东青岛266041
出 处:《中国表面工程》2011年第6期87-91,共5页China Surface Engineering
摘 要:为修复飞机TC2钛合金结构裂纹,应用YAG激光器进行了TC2钛合金的焊接实验。利用扫描电镜(SEM)和电子显微硬度仪分析了工艺参数对焊缝形貌和焊缝截面显微硬度的影响。结果表明:随着电流的升高,焊缝的熔宽逐渐增加,焊缝截面形貌由钉型向X型转变;随着焊接速度的增大,焊缝的熔宽呈减小趋势。采用电流150A、脉宽10ms、频率4Hz、焊接速度2.0mm/s的工艺参数可获得宏观质量良好的焊缝。焊缝熔合区可能为针状马氏体α′交织成的网篮组织;热影响区为75μm左右的环形带,其组织可能是由等轴的α相和针状马氏体组成,靠近熔合线部分较之远离熔合线的区域针状马氏体数量更多且更加密集,靠近熔合线区域有逐渐减弱的再结晶,再结晶尺寸明显大于基材;焊缝截面的显微硬度呈明显的阶梯状分布,基材的硬度在310~350HV0.5之间,熔合区的硬度在500~600HV0.5之间,熔合区硬度相对于基材提高了60%左右。In order to repair the cracked structure of aero TC2 alloy, the welding experiment of TC2 alloy was carried out by YAG:laser. The effect of process parameters on welding seam was investigated. The microstructure of welding seam was observed by SEM. The microhardness of the cross-sections of welding seam was measured. The results show that the weld width increases with the increasing of electric current. At the same time, the microstructure of welding seam changes from T to X type. The increase of welding rate reduces the weld width. According to the test data, a good quality of welding seam can be obtained by the electric current of 150 A, pulse width of 10 ms, frequency of 4 Hz and the welding rate of 2.0 mm/s. The fusion zone is attributed to basketweave microstructure consisted of needle type martensire a'. The heat affected zone is a circumferential band with the dimension of 75μm, which is consisted of needle type martensite and equiaxed α phases. There is more and denser needle type martensite in the region near the fusion line than that away the fusion line. The trend of recrystallization become weak gradually close to the fusion line. The recrystal grain size is obviously greater than that in the base material. Microhardness along the cross-sections is distributed like a ladder. The microhardness of the base material is from a10 to 35o HV05. And the microhardness of fusion zone is en- hanced by 60% to 500~600 HV0.5.
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