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Experimental Study of Surge and Rotating Stall Occurring in High-speed Multistage Axial Compressor

机译:高速多级轴流压气机喘振和失速的实验研究

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The analysis of signals of surges and rotating stalls occurring and processing is essential to reveal the characteristics of instability phenomena,to develop detecting methodology and active control technique,to assure the rig and compressor safety.A high-speed 7-stage compressor was tested on a rig,with 10 channels of casing static pressures and a channel of outlet total pressure.It illustrates by the case with the rotating speed 16,400RPM.Firstly,to detect the stall precursors,the spectrum analysis and the short-time-Fourier-transform(STFT)are employed.It shows the precursors are formed about 3.5s before the surge point in each stage individually.Then,the correlation functions are calculated to analysis the relationship between casing static pressures.Results show that the rotating stalls of the 1-3 stages have phase differences,while the 4-7 stages do not.Finally,the time-domain waveforms analysis instruct that the stagnation cell of surge is firstly formed between the 3rd and the 4th stator rows,and then moves downwards.The surge is companied with the rotating stalls.The front 3 stages are in the cycles of the stall-surge-recover-stall in the whole surge process.
机译:分析喘振和旋转失速的信号以及处理过程对于揭示不稳定现象的特征,开发检测方法和主动控制技术,确保钻机和压缩机安全至关重要。对高速7级压缩机进行了测试钻机具有10个套管静压通道和1个出口总压通道。以转速为16,400RPM的情况为例进行说明。首先,检测失速前兆,频谱分析和短时傅立叶变换采用(STFT)方法,显示前驱体在每个阶段的激增点之前约3.5s形成,然后计算相关函数以分析套管静压力之间的关系。结果表明1-旋转失速3个阶段具有相位差,而4-7个阶段没有相位差。最后,时域波形分析表明,电涌的停滞单元首先在3和4之间形成。定子行,然后向下移动。喘振与旋转失速同时发生。前三个阶段处于整个喘振过程的失速-喘振-恢复-失速的循环中。

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