中国电机工程学报2012，Vol.32Issue(32)：95-100,前插15,7.
某重型燃气轮机压气机顶切方法的数值模拟
Numerical Simulation Analysis of the Tip-cutting Method in a Compressor of a Heavy Duty Gas Turbine
摘要
Abstract
To fulfill the demands of one compressor redesign, the method of tip-cutting based on correcting location was proposed and deduced, which was named equal stream tube. Using this method, the redesign of inlet guide vane and the first two stages including five rows of cascade was carried out. Three dimensional numerical simulation was performed to verify the method feasibility. Furthermore the influence on the redesign compressor caused by tip-cutting was analyzed. The results indicate that this method can ensure quick and accurate tip-cutting according to various value of mass flow. The redesigned compressor can satisfy the mass flow requirement and keep the same pressure ratio as well as high aerodynamic performance, without any optimization. This method will not cause serious flow mismatch problem.关键词
重型燃气轮机/压气机/顶切/等流管法Key words
heavy duty gas turbine/ compressor/ tip-cutting/ equal stream tube分类
能源科技引用本文复制引用
蔡乐,杜鑫,王松涛,周逊..某重型燃气轮机压气机顶切方法的数值模拟[J].中国电机工程学报,2012,32(32):95-100,前插15,7.基金项目
国家高技术研究发展计划(863计划)(2008AA5A302). （863计划）
