航空制造技术
航空製造技術
항공제조기술
Aeronautical Manufacturing Technology
2015年
17期
82-85
,共4页
TA15钛合金%电子束焊接接头%纯钛夹层%强韧性匹配
TA15鈦閤金%電子束銲接接頭%純鈦夾層%彊韌性匹配
TA15태합금%전자속한접접두%순태협층%강인성필배
TA15 titanium alloy%Electron beam welded joint%Pure titanium interlayer%Matching strength and toughness
为了进一步优化TA15钛合金电子束焊接接头的强韧性匹配,研究了添加纯钛夹层对焊接接头力学性能的影响。利用扫描电镜对焊接接头显微组织进行了表征,对添加不同纯钛夹层条件下焊接接头的硬度、拉伸性能、冲击韧性、断裂韧性进行对比分析。研究结果表明:添加纯钛夹层对焊缝显微组织形态无明显影响;焊缝熔合区中部硬度存在低谷,而硬度在热影响区则出现峰值。
為瞭進一步優化TA15鈦閤金電子束銲接接頭的彊韌性匹配,研究瞭添加純鈦夾層對銲接接頭力學性能的影響。利用掃描電鏡對銲接接頭顯微組織進行瞭錶徵,對添加不同純鈦夾層條件下銲接接頭的硬度、拉伸性能、遲擊韌性、斷裂韌性進行對比分析。研究結果錶明:添加純鈦夾層對銲縫顯微組織形態無明顯影響;銲縫鎔閤區中部硬度存在低穀,而硬度在熱影響區則齣現峰值。
위료진일보우화TA15태합금전자속한접접두적강인성필배,연구료첨가순태협층대한접접두역학성능적영향。이용소묘전경대한접접두현미조직진행료표정,대첨가불동순태협층조건하한접접두적경도、랍신성능、충격인성、단렬인성진행대비분석。연구결과표명:첨가순태협층대한봉현미조직형태무명현영향;한봉용합구중부경도존재저곡,이경도재열영향구칙출현봉치。
In order to further optimize the strength and toughness of the electron beam welding (EBW) joints of TA15 titanium alloy,the effect of pure titanium interlayer on mechanical properties of EBW joint is studied. Scanning electron microscope (SEM) is used to characterizethe microstructure of the EBW joints.Hard-ness, tensile properties, impact toughness, fracture tough-ness of welded joint with different pure titanium interlay-ers are compared and analyzed.The results show that the addition of pure titanium interlayer has no obvious effect on the microstructure morphology of the joint. The hard-ness of fusion zone is relatively lower, and the hardness of the heat affected zone appearspeak.