网站首页期刊简介编委会过刊目录投稿指南广告合作征订与发行联系我们English
TC4钛合金中空叶片扩散连接-超塑成形技术
英文标题:DB-SPF technology of hollow blade for TC4 titanium alloy
作者:王国峰 赵相禹 孙超 杨默 
单位:哈尔滨工业大学 
关键词: 
分类号:
出版年,卷(期):页码:2015,40(4):48-53
摘要:

采用扩散连接-超塑成形技术成形中空叶片在发动机减重方面具有重要的意义,本文进行了中空叶片的扩散连接-超塑成形实验,成形出质量较好的中空叶片,确定了最优的实验参数。分析了叶片芯板的壁厚分布以及上下面板与芯板的连接情况,并线扫描分析了扩散连接的接头。结果表明,随着扩散连接保温时间的延长,扩散连接接头的效果较好;通过多次试验得出,在成形温度T=920 ℃、内部气压P=2 MPa、成形时间t=2 h的条件下,进行超塑成形,成形所得的中空叶片表面质量良好,扩散连接接头较好,芯板的厚度变化较均匀。

It is of great importance to form hollow blade by DB-SPF technology in reducing weight of the engine. The DB-SPF tests of hollow blade were carried out, the good quality hollow blades were obtained, and the optimum experimental parameters were determined. The thickness distribution of core plate and the connection of the panels and core plate were analyzed, and the diffusion bonding joint was analyzed by line scanning analysis. The results show that effects of the diffusion bonding joint are better with the increase of holding time during diffusion bonding. By multiple experiments, it is obtained that the quality of hollow blade and the diffusion bonding joints are good, and thickness of the core board is uniform when temperature is 920 ℃,internal pressure is 2 MPa and the forming time is 2 h. 
 

基金项目:
国家自然科学基金资助项目(51275129);长江学者和创新团队发展计划资助(IRT1229)
作者简介:
王国峰(1973-),男,博士,教授,博士生导师
参考文献:

[1]Kaibyshev O A, Safiullin R V, Lutfullin R Y, et al. Advanced superplastic forming and diffusion bonding of titanium alloy[J].Materials Science and Technology, 2006, 22(3): 343-348.


[2]Maehara Y, Komizo Y, Langdon T G. Principles of superplastic diffusion bonding[J]. Materials Science and Technology, 1988, 4(8): 669-674.


[3]Jiang S S, Zhang K F. Study on controlling thermal expansion coefficient of ZrO2B-TiO2 ceramic die for superplastic blow-forming high accuracy Ti-6Al-4V component[J]. Materials and Design, 2009, 30: 3904-3097.


[4]Fan X G, Yang H, Gao P F, et al. Dependence of microstructure morphology on processing in subtransus isothermal local loading forming of TA15 titanium alloy [J]. Materials Science and Engineering A, 2012,546: 46-52.


[5]Feng X U, Zhao Y, Ning W. Application of the titanium alloy in civil aviation[J]. Baosteel Technical Research, 2011, 5(4):25-35.


[6]Wu G Q, Huang Z. Superplastic forming/diffusion bonding of laser surface melted TiAl intermetallic alloy[J]. Scripta Materialia, 2001, 45(8): 895-899.


 [7]Zhang K F, Wang G F, Wu D Z, et al. Research on the controlling of the thickness distribution in superplastic forming[J]. Journal of Materials Processing Technology, 2004, 151: 54-57.


[8]Xun Y W, Tan M J. Applications of superplastic forming and diffusion bonding to hollow engine blades[J]. Journal of Materials Processing Technology, 2000, 99(1): 80-85.


[9]Yang H, Fan X G, Sun Z C, et al. Recent developments in plastic forming technology of titanium alloys[J]. Science China Technological Sciences, 2011, 54(2): 490-501.


[10]Abdoos H, Khorsand H, Shahani A R. Fatigue behavior of diffusion bonded powder metallurgy steel with heterogeneous microstructure[J]. Materials & Design, 2009, 30(4): 1026-1031.


[11]Schuh C, Dunand D C. Whisker alignment of Ti-6Al-4V/TiB composites during deformation bytransformation superplasticity[J]. International Journal of Plasticity, 2001, 17(3): 317-340.


[12 ]Bing Z, Zhiqiang L, Hongliang H, et al. Three dimensional FEM simulation of titanium hollow blade forming process[J]. Rare Metal Materials and Engineering, 2010, 39(6): 963-968.

 

服务与反馈:
本网站尚未开通全文下载服务】【加入收藏
《锻压技术》编辑部版权所有

中国机械工业联合会主管  中国机械总院集团北京机电研究所有限公司 中国机械工程学会主办
联系地址:北京市海淀区学清路18号 邮编:100083
电话:+86-010-82415085 传真:+86-010-62920652
E-mail: fst@263.net(稿件) dyjsjournal@163.com(广告)
京ICP备07007000号-9