摘要
Based on analytic and feature modeling methods, a parametric design method for three-dimensional internally cooling turbine blade model with ribs and bleed was developed. Blade profiles were defined by five-order polynomial expression. The cooling passage profiles were defined by the thickness of wall according to the blade profiles. A FORTRAN program was written with the intent to provide rapid and robust geometry generation of realistic turbine blades. The ribs, rabbet and margin pale were designed by means of CAD with feature modeling method. As an example, a tri-cavities internal cooling turbine blade was successfully established using this method.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 637-640+656 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 28 |
| 期 | 6 |
| 出版状态 | 已出版 - 12月 2007 |
学术指纹
探究 'Parametric design for cooling turbine blades based on analytic and feature modeling' 的科研主题。它们共同构成独一无二的学术指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver