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Global Stable Region Analysis to Nonlinear Axial Flow Compressor
Author(s): 
Pages: 1-4
Year: Issue:  1
Journal: Journal of Air Force Engineering University(Natural Science Edition)

Keyword:  航空压气机稳定域喘振旋转失速主动控制;
Abstract: 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.
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