首页 | 本学科首页   官方微博 | 高级检索  
     检索      

涡轴发动机涡轮部件改型气动分析
引用本文:李文,张新敬,张华良,张冬阳,谭春青.涡轴发动机涡轮部件改型气动分析[J].推进技术,2010,31(3):314-319.
作者姓名:李文  张新敬  张华良  张冬阳  谭春青
作者单位:1. 中科院工程热物理研究所,北京,100190;中科院研究生院,北京,100190
2. 中科院工程热物理研究所,北京,100190
摘    要:首先对涡轴发动机涡轮部件的变工况特性进行了数值研究,计算结果与实验测量吻合良好。在此基础上,引入拓扑分析手段,对有、无中间承力支板的涡轮内部流场进行了详细分析。结果表明:支板对效率、流量等总体性能参数影响不大。最后对涡轮进行了改型优化,去掉支板,缩小尺寸并由动力涡轮静叶栅作为承力框架。计算表明:通过适当的气动优化,无支板的涡轮气动性能可以进一步提高。

关 键 词:涡轮轴发动机  涡轮  涡轮叶片  气动构型  气动设计

Aerodynamic investigation on retrofit for turbine of a turbo-shaft engine
LI Wen,ZHANG Xin-jing,ZHANG Hua-liang,ZHANG Dong-yang and TAN Chun-qing.Aerodynamic investigation on retrofit for turbine of a turbo-shaft engine[J].Journal of Propulsion Technology,2010,31(3):314-319.
Authors:LI Wen  ZHANG Xin-jing  ZHANG Hua-liang  ZHANG Dong-yang and TAN Chun-qing
Institution:1(1.Inst.of Engineering Thermophysics,Academia Sinica,Beijing 100190,China;2.Graduate School of the Chinese Academy of Sciences,Beijing 100190,China)
Abstract:Numerical investigation on the turbine performance of a turbo-shaft engine is carried out under various working conditions.It shows that the numerical results agree well with the experimental measured data.To study the effects of the guide vanes,limiting streamline and topology of the internal flow fields are analyzed based on the numerical results.It is found that the overall performance of the turbine including efficiency and flow rate varies little by comparing with that in absence of the guide vanes.Optimization is then conducted finally by replacing the guide vanes with the free power turbine stator blades and optimizing the meridional flow path.The results reveal that,after optimization,the performance is improved with less weight and higher power output.
Keywords:Turbo shaft engine  Turbine  Turbine blade  Aerodynamic configuration  Aerodynamic stalling
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号