多级高速压气机喘振失稳的确定学习建模与预警OA
Deterministic learning and surge warning for a multistage high-speed compressor
高性能航空发动机压气机气动失稳预警和安全运行监测是航空发动机领域非常重要且极具挑战的难题.针对航空涡扇发动机核心部件——多级高速压气机喘振先兆特征微弱、机理复杂、难以预判等问题,本文以五级高速压气机试验台为研究对象,提出了一种基于单测点脉动压力数据的喘振建模与预警方法.首先,利用基于采样观测器的确定学习算法辨识喘振失稳的动力学模型,从而构造刻画压气机喘振特性的动态模式库;然后,基于模式库中的建模结果设计动态估计器,根据实时输入的单测点数据实现压气机喘振预警;最后,在五级高速压气机试验台上进行了不同转速下的离线和在线预警试验,初步实现了从原来喘振发生后毫秒级检测到喘振发生前秒级预警的技术突破.本文所提学习方法能够从多级高速压气机脉动压力数据中学习到喘振失稳更加本质、全面的动力学特征,具有良好的可解释性;在此基础上发展的预警方法仅利用单测点数据实现了喘振在线预警,有望为高性能航空发动机安全稳定运行提供实时监测方法,具有一定的工程应用价值.
Aerodynamic instability warning and safe operation monitoring of compressors are important and challeng-ing problems in high-performance aero-engine research.For issues such as weak characteristics,complex mechanisms,and the difficult-to-predict nature of multistage high-speed compressor surges,this paper presents a unified learning and warning method based on single-sensor data.Firstly,a sampled-data observer-based deterministic learning algorithm is used to identify the compressor dynamics,forming a pattern library that characterizes the dynamic information of surge evolution.Subsequently,this library is used to design dynamical estimators,which utilize real-time input from single-sensor data to achieve surge warning.Finally,offline and online warning experiments at different speeds are carried out on a five-stage high-speed compressor test rig.Preliminary experimental results show that based on the single-sensor data,the proposed method can achieve a technological breakthrough from millisecond-level detection after the surge occurs to second-level warning before the surge occurs.In summary,the proposed learning method can utilize compressor data of the multistage high-speed compressor to obtain the essential and comprehensive dynamic characteristics of the compressor surge,which has favorable interpretability.The warning method developed on this basis only uses single-sensor data to achieve online early detection of sudden surges.It is expected to provide a real-time monitoring method for the safe and stable operation of high-performance aero-engines,which has a certain application value.
胡竞涛;潘若痴;王聪;吴伟明;张志博;张付凯;朱泽键;韩帅;陈禹西;贾博博;刘世官
山东大学控制科学与工程学院,山东济南 250061中国航空发动机集团有限公司沈阳发动机研究所,辽宁沈阳 100080山东大学控制科学与工程学院,山东济南 250061山东大学控制科学与工程学院,山东济南 250061中国航空发动机集团有限公司沈阳发动机研究所,辽宁沈阳 100080山东大学控制科学与工程学院,山东济南 250061广东美的暖通设备有限公司楼宇科技事业部,广东佛山 528311山东大学控制科学与工程学院,山东济南 250061中国航空发动机集团有限公司沈阳发动机研究所,辽宁沈阳 100080中国航空发动机集团有限公司沈阳发动机研究所,辽宁沈阳 100080中国航空发动机集团有限公司沈阳发动机研究所,辽宁沈阳 100080
多级高速压气机气动失稳动态系统确定学习径向基函数网络
multistage high-speed compressoraerodynamic instabilitydynamical systemdeterministic learningradial basis function network
《控制理论与应用》 2026 (8)
1639-1648,10
中国博士后科学基金资助项目(2024M761803),国家资助博士后研究计划项目(GZC20231451),山东省博士后创新项目(SDCX-ZG-202400315),国家自然科学基金项目(62350083,62203262,62203263)资助.Supported by the China Postdoctoral Science Foundation(2024M761803),the Postdoctoral Fellowship Program of CPSF(GZC20231451),the Shan-dong Postdoctoral Science Foundation(SDCX-ZG-202400315)and the National Natural Science Foundation of China(62350083,62203262,62203263).
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