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轴流压气机旋转失速建模与检测:基于确定学习理论与高阶Moore-Greitzer模型的研究

王聪 文彬鹤 司文杰 彭滔 袁成志 陈填锐 林文愉 王勇 侯安平

王聪, 文彬鹤, 司文杰, 彭滔, 袁成志, 陈填锐, 林文愉, 王勇, 侯安平. 轴流压气机旋转失速建模与检测:基于确定学习理论与高阶Moore-Greitzer模型的研究. 自动化学报, 2014, 40(7): 1265-1277. doi: 10.3724/SP.J.1004.2014.01265
引用本文: 王聪, 文彬鹤, 司文杰, 彭滔, 袁成志, 陈填锐, 林文愉, 王勇, 侯安平. 轴流压气机旋转失速建模与检测:基于确定学习理论与高阶Moore-Greitzer模型的研究. 自动化学报, 2014, 40(7): 1265-1277. doi: 10.3724/SP.J.1004.2014.01265
WANG Cong, WEN Bin-He, SI Wen-Jie, PENG Tao, YUAN Cheng-Zhi, CHEN Tian-Rui, LIN Wen-Yu, WANG Yong, HOU An-Ping. Modeling and Detection of Rotating Stall in Axial Flow Compressors:Part I——Investigation on High-order M-G Models via Deterministic Learning. ACTA AUTOMATICA SINICA, 2014, 40(7): 1265-1277. doi: 10.3724/SP.J.1004.2014.01265
Citation: WANG Cong, WEN Bin-He, SI Wen-Jie, PENG Tao, YUAN Cheng-Zhi, CHEN Tian-Rui, LIN Wen-Yu, WANG Yong, HOU An-Ping. Modeling and Detection of Rotating Stall in Axial Flow Compressors:Part I——Investigation on High-order M-G Models via Deterministic Learning. ACTA AUTOMATICA SINICA, 2014, 40(7): 1265-1277. doi: 10.3724/SP.J.1004.2014.01265

轴流压气机旋转失速建模与检测:基于确定学习理论与高阶Moore-Greitzer模型的研究

doi: 10.3724/SP.J.1004.2014.01265
基金项目: 

国家杰出青年科学基金(61225014),国家自然科学基金重点项目(60934001),国家自然科学基金(61304084),重庆理工大学科研启动基金(2013ZD01)资助

详细信息
    作者简介:

    文彬鹤 中航工业航空动力系统研究所系统工程师. 主要研究方向为航空发动机全权限数字电子控制研究,确定学习理论,动态模式识别.E-mail:bhwen5516521@126.com

Modeling and Detection of Rotating Stall in Axial Flow Compressors:Part I——Investigation on High-order M-G Models via Deterministic Learning

Funds: 

Supported by National Science Fund for Distinguished Young Scholars (61225014), State Key Program of National Natural Science Foundation of China (60934001), National Natural Science Foundation of China (61304084), and Startup Fund of Chongqing University of Technology (2013ZD01)

  • 摘要: 喘振和旋转失速是轴流压气机研究领域中重要而困难的问题. 本文基于确定学习理论及动态模式识别方法提出一个旋转失速初始扰动 近似准确建模和快速检测的方法. 首先,基于高阶Moore-Greitzer模型(Mansoux模型),利用确定学习理论提出一个对旋转失速初始扰动的内在系统动态的近似准确建模方法;其次,基于以上近似准确建模,利用 动态模式识别方法提出一个对旋转失速初始扰动的快速检测方法. 基于MIT的Mansoux-C2模型仿真研究验证了 所提方法的有效性. 最后,在北京航空航天大学航空发动机重点实验室的低速轴流压气机试验台上开展了试验研究. 通过对低速轴流压气机试验台参数进行测量,得到基于北航低速轴流压气机试验台的Mansoux模型. 通过对基于北航试验台Mansoux模型进行仿真研究,验证了所提方法的有效性.
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出版历程
  • 收稿日期:  2013-06-19
  • 修回日期:  2014-01-27
  • 刊出日期:  2014-07-20

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