期刊文献+

新型高负荷氦气压气机的三维级性能研究 被引量:1

A performance study on the three-dimensional stage of a new high-loaded helium compressor
下载PDF
导出
摘要 按照传统空气设计规律设计的氦气压气机存在级数较多的问题.为了提高氦气压气机的级压比以减少级数,采用适合于氦气压气机的新型基元级速度三角形理论进行高负荷氦气压气机的三维级气动设计,应用CFD软件对其三维级流场进行数值模拟,同时进行了与常规设计准则的对比研究.研究结果表明,高负荷基元级沿径积叠成三维级是可行的;相同条件下,高负荷设计三维级方案设计点的级压比达到1.138 8,级压比是常规设计的2倍多,且效率还能维持高达89.86%的较高水平. According to the design rules of conventional air compressors,the number of stages necessary for the helium compressor is excessive.In order to increase the pressure ratio and thereby decrease the number of stages,an aerodynamic design for the three-dimensional stage of a high-loaded helium compressor was investigated by adopting the theory of new elementary stage velocity triangle.The three-dimensional stage flow field was numerically simulated with the computational fluid dynamics(CFD) software and a comparison study on its conventional design criteria was also presented.The results show that the high-loaded elementary stage radial stacking to three-dimensional stage is feasible.Under the same condition,the stage pressure ratio of a design point of the high-loaded three-dimensional stage design is 1.1388,which is more than twice that of the conventional design while still maintaining high efficiency(up to 89.86%).
出处 《哈尔滨工程大学学报》 EI CAS CSCD 北大核心 2012年第4期464-469,共6页 Journal of Harbin Engineering University
基金 国家973计划基金资助项目(2007CB210105)
关键词 高负荷氦气压气机 新型基元级 三维级 气动设计 数值模拟 high-loaded helium compressor new elementary stage three-dimensional stage aerodynamic design numerical simulation
  • 相关文献

参考文献10

  • 1吴宗鑫,张作义著..先进核能系统和高温气冷堆[M].北京:清华大学出版社,2004:294.
  • 2陈夷华,王捷,张作义.高温气冷堆联合循环技术潜力研究[J].核动力工程,2001,22(5):475-480. 被引量:7
  • 3BRYCE J D, CHERRETY M A, LYES P A. Three-dimen- sional flow in a highly loaded single-stage transonic fan [ J ]. ASME Journal of Turbomachinery, 1995,117 ( 1 ) :22-28. 被引量:1
  • 4EMMERSON P R. Three-dimensional flow calculations of the stator in a highly loaded transonic fan [ J ]. ASME Journal of Turbomachinery, 1998, 120(1): 141-147. 被引量:1
  • 5CALVERT W J, EMMERSON P R, MOORE J M. Design,test and analysis of a high-pressure-ratio transonic fan [ C ]// ASME Conference Proceedings. Atlanta. USA. 2003:417-427. 被引量:1
  • 6MATFHIAS B, LEONHARD F. Effects of riblets on the loss behavior of a highly loaded compressor cascade [ C ]//ASME Conference Proceedings. Amsterdam, The Nether- lands, 2002: 743-750. 被引量:1
  • 7DOUGLAS J W, LI S M, SONG B, et al. Effects of free stream turbulence on the losses of a highly loaded compres- sor stator blade [ C ]//ASME Conference Proceedings. At- lanta, USA,2003 : 521-530. 被引量:1
  • 8LOTHAR H, MICHAEL P. Unsteady boundary layer devel- opment due to wake passing effects on a highly loaded linear compressor cascade [ J ]. ASME Journal of Turbomachinery, 2004, 126(4) :493-500. 被引量:1
  • 9米哈依洛夫.封闭循环气体涡轮装置[M].曹孝瑾,马同泽,译.北京:科学出版社,1964:39-57. 被引量:1
  • 10LONG Yanli, XU Limin, XIE Chunling, et al. Simulation for a new cascade of helium compressor with enhanced pressure ratio [ C ]//ASME Conference Proceedings. Ber- lin, Germany, 2008:405-414. 被引量:1

二级参考文献1

  • 1焦树建,整体煤气化燃气.蒸汽联合循环,1996年 被引量:1

共引文献6

同被引文献3

引证文献1

二级引证文献3

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部