系统仿真学报 ›› 2018, Vol. 30 ›› Issue (2): 551-559.doi: 10.16182/j.issn1004731x.joss.201802023

• 仿真应用工程 • 上一篇    下一篇

基于熵的航空发动机压气机失速与喘振仿真

皮骏, 邱永超, 胡智伟, 武威   

  1. 中国民航大学 通用航空学院,天津 300300
  • 收稿日期:2015-12-30 出版日期:2018-02-08 发布日期:2019-01-02
  • 作者简介:皮骏(1973-), 男, 湖南, 博士, 副教授, 研究方向为流体机械, 航空发动机; 邱永超(1990-), 男, 河南, 研究生, 研究方向为流体机械。
  • 基金资助:
    中央高校基本科研业务费中国民航大学专项(3122013H001)

Simulation of Surge and Stall for Aero Engine Compressor Based on Entropy

Pi Jun, Qiu Yongchao, Hu Zhiwei, Wu Wei   

  1. General Aviation College, Civil Aviation University of China, Tianjin 300300, China
  • Received:2015-12-30 Online:2018-02-08 Published:2019-01-02

摘要: 采用NASA Rotor37模型并用CFX仿真软件模拟压气机从稳定工作状态到失速与喘振的非稳定工作状态的转变过程,用热力学熵和样本熵的相关理论对这一过程进行分析研究。以实现为压气机失速与喘振的故障诊断提供依据。通过分析,发现平均比熵值和等熵效率这两个热力学熵参数的变化情况在发生失速时出现异常;由机匣处静压序列信号计算所得的样本熵值在近失速点附近达到最小值。这些结果可为压气机失速与喘振的故障诊断提供重要依据。

关键词: 压气机, 热力学熵, 样本熵, 失速, 喘振, 故障诊断

Abstract: The mature model NASA Rotor37 is used to simulate the transition of the compressor’s operation from the steady state to the non-steady state of stall and surge using the simulation software CFX. The transition is analyzed and researched based on the theory of thermodynamics entropy and sample entropy to provide a basis for the fault diagnosis of stall and surge. The two thermodynamic entropy parameters of average specific entropy value and the isentropic efficiency are found by the analysis changing abnormally in the event of stall. The values of the sample entropy obtained by calculation using the static pressure sequence signal at the receiver reach the minimum near the operation point of stall. The goal of providing an important basis for the fault diagnosis of the compressor stall and surge is achieved.

Key words: compressor, thermodynamic entropy, sample entropy, stall, surge, fault diagnosis

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