期刊文献+

镍基单晶合金TLP焊接件破坏特性研究 被引量:1

Fracture characterization of the TLP welding specimen of a single crystal superalloy DD3
下载PDF
导出
摘要 为研究镍基单晶合金的高温焊接性能,通过三点弯曲试验和扫描电镜对单晶体焊接件和单晶体试件在高温下的破坏机理进行了研究,并从晶体滑移理论出发,采用有限元方法对两种不同试样在相同载荷下的M ises应力分布和最大分切应力进行了数值分析.研究结果表明:对于采用TLP焊接连接的单晶焊接件,试样的破坏形式主要表现为脆性断裂,试样的抗弯强度明显低于单晶体试样;对于焊接连接的单晶体结构,由于焊缝处材料性质的差异,在焊缝附近出现明显的应力不连续性,对晶体界面附近的最大分切应力产生明显影响,引起界面附近分切应力分布梯度的显著增加,使试样的破坏特性发生改变,引起试样的脆性破坏,降低了试样的抗弯曲强度. In order to study the welding characteristics of single crystal nism of the TLP welding specimen of single crystal superalloy DD3 and superalloy DD3, the fracture mechaoriginal DD3 specimen is studied with the three -point bending tests and SEM. Based on the single crystallographic theory, the distributing of the Mises stress and the maximum of resolved shear stress is analyzed by the FEM. The results showed that the welding specimen of single crystal superalloy DD3 changed more brittle than the original DD3 specimen and therefore the welding specimen had nearly half of the bending strength of original DD3 alloy. The numerical results of the Mises stress and the maximum of resolved shear stress proved that the w portant role in the models. Because of the material difference, the stress distribution elding line played an imchanged near the welding region, and the resolved shear stress concentrated very evidently near the welding line. Consequently, the brittleness of the single crystal welding specimen increased, the bending strength reduced.
出处 《材料科学与工艺》 EI CAS CSCD 北大核心 2006年第2期124-126,130,共4页 Materials Science and Technology
基金 国家自然科学基金资助项目(10472094) 航空科学基金资助项目(03B53003) 西北工业大学青年教师创新基金 研究生创业种子基金资助项目
关键词 单晶 焊缝 分切应力 三点弯曲试样 扫描电镜 single crystal welding line resolved shear stress three-point bending test SEM
  • 相关文献

参考文献7

二级参考文献51

  • 1杜随更.Lyl2--T2摩擦焊接头中次生摩擦面形成机制的研究[J].西北工业大学学报,1993,:63-68.
  • 2陈荣章 李嘉荣 崔正山 等.铸造高温合金篇:中国航空材料手册(第2版:第2卷)[M].北京:中国标准出版社出版,2002.752-754.
  • 3NESSLER C G. Joining technique for fabrication of high-temperature superalloy blades [R]. AFML-TR-71-237 (AD-743107).
  • 4GIAMEI A F, SALKELD R W, HAYERS C W. Energy efficient engine high-pressures turbine single crystal vane and blade fabrication technology report [R] . NASA-CR-165400.
  • 5岳珠峰,Theor Appl Fract Mech,1996年,25卷,127页
  • 6岳珠峰,Theor Appl Fract Mech,1996年,24卷,139页
  • 7岳珠峰,Metall Mater Trans A,1995年,26卷,1815页
  • 8岳珠峰,航空学报,1993年,3期,23页
  • 9Goulette M J. In: Kissinger R D, Deye D J, Anton D L,Getel A D, Nathal M V, Pollock T M, Woodford D A eds,Superalloys 1996, Pennsylvania: TMS, 1996:3
  • 10Tin S, Pollock T M, King W T. In: Pollock T M, Kissinger R D, Bowman R R, Green K A, Mclean M, Olson S,Schirra J J eds, Superalloys 2000, Pennsylvania: TMS,2000:201

共引文献40

同被引文献6

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部