期刊文献+

43″汽轮机叶片材料热变形行为及制坯工艺参数优化 被引量:2

Thermal Deformation Behavior of 43" Turbine Blade Material and Forging Parameters Optimization
下载PDF
导出
摘要 针对制造高质量叶片锻件的材料热变形问题,采用热模拟试验及数据回归拟合的方法建立了某43"汽轮机叶片材料的高温流变应力方程.采用所建立的方程,使用软件DEFORM3D对叶片锻造过程进行了数值模拟和正交试验分析.应力方程计算结果表明,所用材料在高温压缩下的流变应力符合双曲正弦函数关系.试验分析结果表明,凸台直径对叶片锻造质量的影响最为显著,叶根过渡处圆角与摆料位置的影响其次,叶冠过渡处圆角的影响最小,据此对锻造工艺参数进行了优化.生产实践表明:采用优化后的参数可降低载荷,使尺寸公差保持在3mm之内,从而提高了产品质量,减小了材料成本,降低了锻造次数,提高了材料利用率和生产效率,这对叶片材料及模锻件的国产化具有重要意义. In order to solve the problem of thermal deformation in high-quality blade forging, a high temperature constitutive equation for a 43" turbine blade material was established by thermal simulation experiments and data regression. Using the established equation, the forging process was analyzed by orthogonal test and numerical simulation software DEFOEM-3D. The calculation results show that the elevated temperature flow stress of the material accords with hyperbolic sine function. The analysis results show that the effects of the boss diameter, the fillet near blade root, the distance between the center line of blank and mold, and the fillet near blade shroud on the forging quality is successively from large to small. The practical production shows that the forging process using the optimized parameters can not only lower the load, hold the tolerance within 3 mm, and reduce forging times, but also save material and increase the economic efficien- cy of the enterprise. This study may benefit the nationalization of the blade materials and die forgings.
出处 《西安交通大学学报》 EI CAS CSCD 北大核心 2011年第1期94-98,126,共6页 Journal of Xi'an Jiaotong University
关键词 叶片材料 锻造 流变应力方程 参数优化 blade material forging constitutive equation parameter optimization
  • 相关文献

参考文献6

  • 1张志文著..叶片锻造[M].西安:西安交通大学出版社,1987:252.
  • 2LU X, BALENDRA R. Temperature-related errors on aerofoil section of turbine blade[J]. Journal of Materials Processing Technology, 2001,115(2) : 240-244. 被引量:1
  • 3刘郁丽..叶片精锻成形规律的三维有限元分析[D].西北工业大学,2001:
  • 4CHENG Lti, ZHANG Liwen, MU Zhengjun, et al. 3D FEM simulation of the multi-stage forging process of a gas turbine compressor blade[J]. Journal of Mate- rials Processing Technology, 2008, 198 (1/2/3) : 463- 470. 被引量:1
  • 5LIN Y C, CHEN M S, ZHONG J. Effect of temperature and strain rate on the compressive deformation behavior of 42CrMo steel[J]. Journal of Material Processing Technology, 2008, 205(1/2/3):308-315. 被引量:1
  • 6BARIANI P F, BRUSCHI S, NEGRO T D. Integrating physical and numerical simulation techniques to design the hot forging process of stainless steel turbine blades[J]. Machine Tools & Manufacture, 2004, 44 (9) :945-951. 被引量:1

同被引文献16

引证文献2

二级引证文献7

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