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高压级涡轮的气动优化设计改型
引用本文:韩志双,唐洪飞. 高压级涡轮的气动优化设计改型[J]. 机械工程师, 2010, 0(2): 114-115
作者姓名:韩志双  唐洪飞
作者单位:1. 哈尔滨汽轮机厂有限责任公司,哈尔滨,150040
2. 哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
摘    要:蒸汽轮机高压级涡轮多为低展弦比直叶型设计,此类涡轮的二次流损失占整个流动损失的比重较大,现在的设计技术能够较好地设计出优秀的S1面叶型,但较难把握全三维的二次流损失。文中通过对单级某高压级涡轮导叶的优化设计改型,得到了较好的控制二次流损失的全三维直叶型。结果表明:最优全三维直叶型不是最优S1面叶型,二次流损失在流动中比重较大,设计中不容忽视;采用优化设计的方法,能够非常有效地提供最优直叶型,缩短设计周期。

关 键 词:高压涡轮  低展弦比  直叶型  数值模拟  高性能

Optimized Aerodynamics Design of High-pressure Turbine
HAN Zhi-Shuang,TANG Hong-Fei. Optimized Aerodynamics Design of High-pressure Turbine[J]. Mechanical Engineer, 2010, 0(2): 114-115
Authors:HAN Zhi-Shuang  TANG Hong-Fei
Affiliation:1.Harbin Turbine Company Limited/a>;Harbin 150040/a>;China/a>;2.School of Energy Science and Engineering/a>;Harbin Institute of Technology/a>;Harbin 150001/a>;China
Abstract:High-pressure steam turbine usually was low-aspect ratio and straight, the secondary flow loss of such type turbine accounted for a larger proportion of the total flow loss, the S1 section profile is able to designed better with the current design technology, but more difficult to grasp the full three-dimensional secondary flow loss. In this paper, a single-stage high -pressure stage of a turbine guide vane optimal design modifications, has been better control of secondary flow loss of the entire three -dim...
Keywords:high-pressure turbine  low aspect-ratio  straight blade profile  numerical simulation  high-performance  
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