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非线性航空压气机系统全局稳定域
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V23

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陕西省自然科学基金资助项目(2007014)


Global Stable Region Analysis to Nonlinear Axial Flow Compressor
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    摘要:

    从理论上定性分析了非线性航空压气机系统的局部稳定性和全局稳定域,提出了以β、γ为参数的系统稳定性判据,获得了系统的全局稳定域。基于航空压气机系统的MG模型,应用非线性动力学理论,首先对系统有限远奇点进行定性分析,提出了在β、γ不同匹配条件下的稳定条件,且用数值仿真加以验证,即当γ=1.2,ψc0=1.5,β=0.67时为中心;当γ=1.4,ψc0=1.75,β=1时为焦点;当γ=1.2,ψc0=2.2,β=2时为结点。其次对系统无穷远奇点进行定性分析,划分了非线性航空压气机系统的全局稳定域。进一步分析了稳定性条件及全局稳定域与此系统喘振和旋转失速的关系。

    Abstract:

    Global stable region and stability of nonlinear axial compressor system are theoretically qualitatively analyzed in this paper, Criterion of stability of the system are presented by parameters . Based on the MG model of the nonlinear axial flow compressor systems and by applying the nonlinear dynamical theory, qualitative dynamical characters are analyzed for the limited singular point firstly. The stable conditions are achieved on the basis of the various matching of parameters . Simulation results prove that when [WTBX]γ=1.2,ψc0=1.5,β=0.67[WTBZ] singular point is center point; when γ=1.4,ψc0=1.75,β=1singular point is focus;when γ=1.2,ψc0=2.2,β=2singular point is node. Secondly, qualitative dynamical characters are analyzed for the unlimited singular point, the global stable region can be divided by the nonlinear axial flow compressor systems. In addition, the relation are researched between the stable conditions,global stable region and rotating stalls as well as surge. It has academic significance on achieving reliable active control of the nonlinear axial flow compressor and understanding the relations between the system's behaviors and the parameters.

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姚宏,邓涛,张广军.非线性航空压气机系统全局稳定域[J].空军工程大学学报,2009,(1):1-4

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  • 在线发布日期: 2015-11-24
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