摘要
以某型发动机逼喘试验中的脉动压力为研究对象,运用短时傅立叶变换的信号处理方法将高采样率的数据转化到时频域,呈现某型发动机在试飞过程中发生气动不稳定现象时的瀑布图,分析压气机在发生喘振和失速时脉动压力出现的不同的现象,得出对压气机气动不稳定性有指示作用的脉动压力频率,在飞行中,监测这些频率处的脉动压力波动情况,对于压气机气动稳定性的实时判断是非常有意义的。
In this paper, the pulsating pressure in the test of a type of engine flight platform is studied. Short-time Fourier transform(STFT) signal processing method is used to transform high-sampling data into time-frequency domain. The waterfall diagram shows the aerodynamic instability of a certain type of engine during the test flight. The different phenomena of pulsating pressure during surge and stall of the compressor are analyzed, thus the pulsating pressure frequency which can indicate the aerodynamic instability of compressor is obtained. In the flight process, monitoring pulsating pressure fluctuations at these frequencies is very meaningful to judge the aerodynamic stability of compressor in real time.
引文
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