中国电机工程学报2011，Vol.31Issue(26)：1-8,8.
F级中低热值燃料燃气轮机透平部分气动方案优化设计与分析
Aerodynamic Optimization Design and Analysis on the Turbine Part of F Class Gas Turbine Under Middle and Low Heat Value Fuel
摘要
Abstract
The turbine of heavy duty gas turbine was studied by one-dimensional and quasi three-dimensional method, including mode design and optimization. The quasi three-dimensional calculation was based on the result of the one-dimensional optimization, and the quasi three-dimensional result was optimized. The result shows that the efficiency increases 0.8% by the one-dimensional optimization, and the outlet flow angle is close to 90 degree. There is transonic flow in the flow path of the second and third stator. In the quasi three-dimensional calculation, the cool air mix loss takes an important part in the total loss, due to the large quantity of cool air in the first stage. The secondary loss is a great factor to impact the loss distribution along blade height. The loss is decreased by the quasi three-dimensional optimization, especially in the third stator. The purpose of this study, refer to the general F-class turbine aerodynamic design experience, to discuss gas turbine design on how to choose one dimensional, quasi three-dimensional parameters, so as to provide cascade reference to the engineering design.关键词
燃气轮机/气动设计/一维/准三维/中低热值Key words
gas turbine/aerodynamic design/one-dimensional/quasi three-dimensional/middle and low heatfuel value分类
能源科技引用本文复制引用
刘勋,周逊,温风波,王松涛,王仲奇..F级中低热值燃料燃气轮机透平部分气动方案优化设计与分析[J].中国电机工程学报,2011,31(26):1-8,8.基金项目
国家高技术研究发展计划（863计划)（2008AA5A302). （）
