航空学报 > 1997, Vol. 18 Issue (2): 207-209

轴流压缩系统动态失速的简化模型

胡骏   

  1. 南京航空航天大学动力工程系, 南京, 210016
  • 收稿日期:1996-04-15 修回日期:1996-09-16 出版日期:1997-04-25 发布日期:1997-04-25

NEW SIMPLIFIED MODEL OF POST STALL TRANSIENTS IN AXIAL COMPRESSION SYSTEMS

Hu Jun   

  1. Power Engineering Department, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016
  • Received:1996-04-15 Revised:1996-09-16 Online:1997-04-25 Published:1997-04-25

摘要:

在原Moore-Greitzer模型的基础上,发展了一个描述轴流压缩系统动态失速过程的一阶非线性模型。该模型耦合了旋转失速和喘振,并考虑了旋转扰动波中高阶谐波分量的影响,可用于详细分析旋转失速/喘振的动态特性、由失速状态退出的恢复特性,及系统参数的影响等。

关键词: 压缩系统, 旋转失速, 喘振, 恢复特性

Abstract:

Based on the theory developed by Moore and Greitzer, a new simplifying approximation, which takes into account the influence of higher harmonics of rotating waves, is proposed to get a simplified model of post stall transients in axial compression systems. This model consists of a set of three simultaneous nonlinear first order partial differential equations.It is shown that the further investigations of post stall behavior for different response modes of instabilities (rotating stall and/or surge), recoverability from rotating stall or surge, and the effect of compression system parameters on them can be carried out by this model.

Key words: compression system, rotating stall, surge, recover ability

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