蒸汽透平高压级扭叶片的气动优化设计  

Aerodynamics Optimization for Twist Blade in HP Steam Turbine Stages

作　　者：朱晓峰[1] 袁新[1] 

机构地区：[1]清华大学热科学与动力工程教育部重点实验室,北京100084

出　　处：《热力透平》2009年第4期217-220,268,共5页Thermal Turbine

基　　金：国家自然科学基金资助项目(50676043);国家重点基础研究发展计划(2007CB210108)

摘　　要：提出了一种实现截面局部扭转、控制喉部面积的扭叶片参数化造型方法。用控制喉部面积替代流量约束,对某蒸汽透平高压级动叶进行了气动优化设计;另一方面以流量差异和气动效率为目标函数,采用非支配排序遗传算法(NSGA-II)进行了多目标并行优化设计。两种方法的结果吻合较好。结果表明,本文的优化方法是有效的,扭积叠造型有助于提高蒸汽透平高压级的气动效率。In the present paper, a parametric modeling method for twist blade is established, which can partially rotate a blade section and control the blade＇s throat. The rotor blade of a HP steam turbine stage is optimized by using an idea of controlling its throat instead of mass flow constraint. The rotor blade is also optimized by a multi-objective method named Non-dominated Sorting Genetic Algorithm II （NSGA-II）, which minimizes mass flow difference and maximizes efficiency simultaneously. The results of the two optimizations are well conformed, indicating that the optimization methods are valid and twist blade is useful to enhance HP steam stages＇ efficiency.

关 键 词：气动优化设计 蒸汽透平 高压级 扭叶片 NURBS 

分 类 号：TK263.3[动力工程及工程热物理—动力机械及工程]