节点文献

端壁造型在叶轮机械中的应用与发展

Application and Development of End-wall Profiling in Turbomachinery

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 卢家玲楚武利朱俊强刘志伟

【Author】 LU Jia-ling,CHU Wu-li,LIU Zhi-wei(College of Power and Energy Source,Northwest China Polytechnic University,Xi’an,China,Post Code: 710072),ZHU Jun-qiang(Engineering Thermophysics Research Institute,Chinese Academy of Sciences,Beijing,China,Post Code: 100190)

【机构】 西北工业大学动力与能源学院中国科学院工程热物理研究所

【摘要】 对一项新的设计技术—端壁造型技术的发展历史进行了回顾。端壁造型技术可以降低端壁区二次流损失,其提高效率的作用已经在涡轮中得到了广泛的验证,相关结论可以直接被工程采用。端壁造型技术在压气机中的研究虽晚于其在涡轮中的研究,但最新研究表明:端壁造型在改变跨音压气机激波结构,改善压气机稳定工作裕度,以及降低静叶角区分离等领域能够发挥一定作用。端壁造型技术反应了人们利用复杂型面来提高叶轮机械性能的研究趋势,值得研究者在未来开展更深入的研究。

【Abstract】 Reviewed was the evolution of a new design technology-end-wall profiling technology,which can reduce secondary flow losses in the zones around end-walls.The technology may enhance the thermal efficiency of a turbine,and has been widely verified with relevant conclusions being adopted directly in engineering projects.Although the research for applying the above technology in compressors is somehow delayed in comparison with that in turbines,the latest research findings show that the technology has played a definite role in such efforts as changing the shock wave structure of a transonic compressor,improving its stable operating margin and reducing the separation of flows in the corners of stationary blades.The technology in question reflects the research tendency of utilizing complex profiles to enhance turbomachine performance,and merits further study and investigation in the future by researchers.

【关键词】 端壁造型叶轮机械涡轮压气机
【Key words】 end-wall modelingturbomachineryturbinecompressor
【基金】 国家自然基金资助项目(50506026);航空基金资助项目(2007ZB53021)
  • 【文献出处】 热能动力工程 ,Journal of Engineering for Thermal Energy and Power , 编辑部邮箱 ,2009年06期
  • 【分类号】TK474.8
  • 【被引频次】15
  • 【下载频次】382
节点文献中: 

本文链接的文献网络图示:

本文的引文网络