航天制造技术
航天製造技術
항천제조기술
HANGTIAN ZHIXAO JI SHU
2013年
3期
5-7,21
,共4页
朱瑞灿%王伟荣%王国庆%王炜%徐雯
硃瑞燦%王偉榮%王國慶%王煒%徐雯
주서찬%왕위영%왕국경%왕위%서문
Ti-22Al-25Nb合金%电子束焊接%热处理%显微组织%力学性能
Ti-22Al-25Nb閤金%電子束銲接%熱處理%顯微組織%力學性能
Ti-22Al-25Nb합금%전자속한접%열처리%현미조직%역학성능
Ti-22Al-25Nb alloy%electron beam welding%heat treatment%microstructure%mechical properties
使用金相显微镜(OM)、扫描电镜(SEM)、透射电镜(TEM)和X射线衍射谱仪(XRD),研究了不同温度热处理后 Ti-22Al-25Nb 合金电子束焊接接头显微组织,对接头拉伸性能及断口分析后认为,经过850℃保温2h空冷的热处理可以有效地改善接头的室温和高温拉伸性能。
使用金相顯微鏡(OM)、掃描電鏡(SEM)、透射電鏡(TEM)和X射線衍射譜儀(XRD),研究瞭不同溫度熱處理後 Ti-22Al-25Nb 閤金電子束銲接接頭顯微組織,對接頭拉伸性能及斷口分析後認為,經過850℃保溫2h空冷的熱處理可以有效地改善接頭的室溫和高溫拉伸性能。
사용금상현미경(OM)、소묘전경(SEM)、투사전경(TEM)화X사선연사보의(XRD),연구료불동온도열처리후 Ti-22Al-25Nb 합금전자속한접접두현미조직,대접두랍신성능급단구분석후인위,경과850℃보온2h공랭적열처리가이유효지개선접두적실온화고온랍신성능。
The post-weld heat treatment (PWHT) parameters of 800℃, 850℃and 900℃were carried out. Aimed at the electron beam welding joints of Ti-22Al-25Nb alloy before and after the heat treatment, the tensile tests on room temperature and 650℃were carried out. The microstructure, mechical properties of Ti-22Al-25Nb (at%) alloys welded joints were investigated by using the equipments optical microscopy (OM), scanning electron microscopy (SEM) and X-ray diffraction (XRD). The result shows that the mechanics performance of the joints with PWHT of 850℃holding two hours followed cooling in air would get better.