Empirical formula blade generation system

The invention discloses an empirical formula blade generation system, which is characterized in that subsonic and transonic turbine stages are designed, and values of design variables used in a parameterization system are calculated by correlation equations; the design variables need to be modified...

Full description

Saved in:
Bibliographic Details
Main Authors HAN CHUANG, DUAN PENGHAO
Format Patent
LanguageChinese
English
Published 12.04.2022
Subjects
CALCULATING
COMPUTING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
PHYSICS
Online AccessGet full text

Cover

More Information
Summary:The invention discloses an empirical formula blade generation system, which is characterized in that subsonic and transonic turbine stages are designed, and values of design variables used in a parameterization system are calculated by correlation equations; the design variables need to be modified through iteration; then generating geometric shapes and blocks of the stator and the rotor by a parameterization system; automatically forming a grid through an ICEM CFD script by using geometric figures and blocks; the performance of the turbine stage is evaluated through a CFD solver; a calculation result is analyzed, and a future improvement direction is found; and the final blade design is obtained through multiple rounds of repeated training and residual iteration. Finally, high efficiency subsonic and transonic turbine stages are produced. 本发明公开了一种经验公式叶片生成系统，设计亚音速和跨音速涡轮级，参数化系统中使用的设计变量的值由相关方程计算；需要迭代来修改设计变量；然后由参数化系统生成静子和转子的几何形状和块；通过使用几何图形和块，在经ICEM CFD脚本自动形成网格；之后通过CFD求解器评估涡轮级的性能；对计算结果进行分析，并寻找未来改进的方向；通过多轮反复训练和残差迭
Bibliography:Application Number: CN202111649451