期刊文献+

多级轴流式压气机平均模型级特性获取方法 被引量:2

An Average Stage Characteristics Generation Method of Multistage Axial Flow Compressors
下载PDF
导出
摘要 针对压气机的级特性计算问题,提出轴流式压气机平均模型级特性的概念,并对经典的相似定律进行改进,使相似工况下各级进出口运动相似条件得到满足.在保证高转速工作区压气机特性计算误差最小化的前提下,采用最优化方法辨识平均模型级特性,结合相似模化的修正方法外推得到模型级完整特性图,进而采用逐级计算的方法重构出压气机完整特性图.新方法改进了传统外推方法,计及到空气密度变化差异和压气机转速对压气机特性的影响,充分利用已有的压气机特性数据并能够在特性线外推中更好地体现压气机自身特性. Concepts of average model stage characteristics of axial flow compressors were proposed. With modified scaling method, the new generation technique of average model stage characteristics can satisfy the analogy criterion perfectly. To minimize the error between the calculated characteristic and the test characteristic of the axial flow compressor at high rotational speeds, the average model stages performance characteristics are identified with optimization method. The total compressor performance characteristic maps are synthesized with the modified scaling method and the average model stage characteristics. The proposed technique improves the conventional scaling method so as to take into account the effect of air density change different and the rotational speed of the compressor, and it can make good use of available data which can reflect the own performance characteristics of the compressor.
出处 《上海交通大学学报》 EI CAS CSCD 北大核心 2007年第12期1954-1958,共5页 Journal of Shanghai Jiaotong University
基金 国家自然科学基金资助项目(5997022)
关键词 热力系统 特性图 相似模化 轴流式压气机 thermodynamic system characteristic maps scaling method axial flow compressors
  • 相关文献

参考文献9

  • 1Agrawal R K, Yunis M. A generalized mathematical model to estimate gas turbine starting characteristics [J]. Journal of Engineering of Power, 1982, 104(1): 194-201. 被引量:1
  • 2Changduk K, Seonhee K, Jayoung K. Component map generation of a gas turbine using genetic algorithms [J]. Journal of Engineering for Gas Turbines and Power, 2006, 128(1): 92-96. 被引量:1
  • 3Kong C, Ki J, Kang M. A new scaling method for component maps of gas turbine using system identification [J]. Journal of Engineering for Gas Turbines and Power, 2003, 125(1): 979-985. 被引量:1
  • 4Song T W, Kim T S, Kim J H. Performance prediction of axial flow compressors using stage characteristics and simultaneous calculation of interstage parameters [J]. Journal of Power and Energy, 2001, 215(1) : 89-98. 被引量:1
  • 5Kim J H, Kim T S, Song T W. Comparative analysis of off-design performance characteristics of single and two-shaft industrial gas turbines [J]. Journal of Engineering for Gas Turbines and Power, 2003, 125 (1): 954-960. 被引量:1
  • 6Kim J H, Song T W, Kim T S. Model development and simulation of transient behavior heavy duty gas turbines [J]. Journal of Engineering for Gas Turbines and Power, 2001, 123(1): 589-594. 被引量:1
  • 7Kim J H, Song T W, Kim T S. Dynamic simulation of full start-up procedure of heavy duty gas turbines [J]. Journal of Engineering for Gas Turbines and Power, 2002, 124(1): 510-516. 被引量:1
  • 8Muir D E, Saravanamuttoo H I H, Marshall D J. Health monitoring of Variable geometry gas turbines for the Canadian navy [J]. Journal of Engitleering for Gas Turbines and Power, 1989, 111(1):244-250. 被引量:1
  • 9Howell A R, Bonham R P. Overall and stage characteristics of axial flow compressors [J]. Journal of Mechanical Engineering, 1950, 163(1): 235-248, 被引量:1

同被引文献18

引证文献2

二级引证文献5

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