基于功率谱互相关的旋转失速预测算法OA
Rotating stall identification algorithm based on power spectrum cross-correlation
失速和喘振是发动机经常遇到的2种气动失稳现象,失速表现为低能量气团沿周向的旋转运动,喘振表现为轴向气流压力大幅度波动,发动机一旦发生气动失稳不能及时退出,可能导致发动机性能急剧恶化,甚至损坏发动机.当前零部件试车台采用的防喘系统是基于时域频域特征向量进行辨识判定,存在响应时间长、对失速不敏感的问题.随着发动机主动控制技术发展,需要更加精确地实时监测失稳初始扰动波信号,对失速辨识算法的快速响应提出了更高要求.提出了一种基于功率谱互相关的失速辨识算法,通过计算2个传感器通道之间的相关系数,在发动机进入旋转失速状态后及时发出警报,有效提前了失速预警时间,为发动机主动控制提供技术基础.
Stall and surge represent two prevalent forms of aerodynamic instability in engine.Stall is characterized by the circumferential propagation of rotating stall cells,while surge manifests as large-amplitude axial oscillations in pres-sure and mass flow.Failure to promptly mitigate such instabilities once initiated can lead to a rapid degradation in en-gine performance and,in severe cases,catastrophic mechanical damage.Current stall/surge detection or prevention systems deployed on component test facilities typically rely on feature vectors extracted from time-and frequency-domain signal analyses for instability detection.However,these conventional approaches often exhibit limited respon-siveness and insufficient sensitivity to incipient stall events.In light of recent advances in active engine control method-ologies,there is a growing need for high-fidelity,real-time monitoring of the initial perturbation waves associated with aerodynamic instability.This demand necessitates stall detection algorithms with enhanced speed and accuracy in identifying the onset of instability.To address this challenge,this paper presents a stall identification algorithm based on cross-correlation of power spectral densities.By computing the correlation coefficient between signals acquired from two spatially separated sensor channels,the proposed method enables timely detection of stall or surge inception and triggers an early warning.The algorithm effectively advances the lead time for stall prediction,thereby establishing a critical technical foundation for the implementation of active instability control strategies in engine.
张耕;肖丽君;钟明;宿丕强;赖小皇
中国航发四川燃气涡轮研究院,绵阳 621000中国航发四川燃气涡轮研究院,绵阳 621000中国航发四川燃气涡轮研究院,绵阳 621000中国航发四川燃气涡轮研究院,绵阳 621000中国航发四川燃气涡轮研究院,绵阳 621000
航空航天
航空发动机旋转失速喘振相关系数功率谱密度
aero-enginerotational stallsurgecorrelation coefficientpower spectral density
《航空学报》 2026 (15)
123-131,9
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