航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2010年
1期
41-46
,共6页
赵衍华%刘景铎%张丽娜%孙忠绍%王国庆
趙衍華%劉景鐸%張麗娜%孫忠紹%王國慶
조연화%류경탁%장려나%손충소%왕국경
摩擦塞补焊%2014铝合金%接头组织%力学性能%微观硬度
摩抆塞補銲%2014鋁閤金%接頭組織%力學性能%微觀硬度
마찰새보한%2014려합금%접두조직%역학성능%미관경도
friction plug welding%2014 Al alloy%joint microstructures%mechanical property%micro-hardness
采用拉锻式摩擦塞补焊方法对4mm厚的2014铝合金搅拌摩擦焊接头缺陷进行了补焊,焊后对塞补焊接头的微观组织和拉伸性能进行了分析.研究结果表明,摩擦塞补焊接头分为焊缝区、热影响区和母材区三部分,焊缝由细小的等轴再结晶组织构成.选择合适的焊接参数和接头结构,塞补焊接头的抗拉强度可以达到330MPa以上, 达到或超过搅拌摩擦焊接头强度.塞补焊接头微观硬度分析表明,塞补焊后接头焊缝区硬度较高,但整体硬度变化不大.
採用拉鍛式摩抆塞補銲方法對4mm厚的2014鋁閤金攪拌摩抆銲接頭缺陷進行瞭補銲,銲後對塞補銲接頭的微觀組織和拉伸性能進行瞭分析.研究結果錶明,摩抆塞補銲接頭分為銲縫區、熱影響區和母材區三部分,銲縫由細小的等軸再結晶組織構成.選擇閤適的銲接參數和接頭結構,塞補銲接頭的抗拉彊度可以達到330MPa以上, 達到或超過攪拌摩抆銲接頭彊度.塞補銲接頭微觀硬度分析錶明,塞補銲後接頭銲縫區硬度較高,但整體硬度變化不大.
채용랍단식마찰새보한방법대4mm후적2014려합금교반마찰한접두결함진행료보한,한후대새보한접두적미관조직화랍신성능진행료분석.연구결과표명,마찰새보한접두분위한봉구、열영향구화모재구삼부분,한봉유세소적등축재결정조직구성.선택합괄적한접삼수화접두결구,새보한접두적항랍강도가이체도330MPa이상, 체도혹초과교반마찰한접두강도.새보한접두미관경도분석표명,새보한후접두한봉구경도교고,단정체경도변화불대.
Friction plug welding of 2014 Al alloy FSW joints in 4 mm thickness have been successfully completed. The metallurgy experiment demonstrates that the FPW joint microstructures could be divided into three different regions: welding line zone, HAZ and base metal zone. The dynamic recrystallization occurs in the welding line zone, which consist of refined, equiaxed grains. Mechanical property measurements demonstrate that the peak tensile strength of the joint can reach more than 330MPa, reach or exceed the joint strength of the FSW welding joint when the suited parameters were used. The microhardness analysis shows that the hardness of the welding line zone is higher than the other zones, but the changes of the FPW joint microhardness is not very acutely.