The Estimation Algorithm for Component Health Parameter of Turbofan Engine

被引:0
|
作者
Pan, Wang [1 ]
Nong, Cheng [1 ,2 ]
Qing, Li [1 ]
机构
[1] Tsinghua Univ, Beijing 10084, Peoples R China
[2] Flight Automat Control Res Inst, Sci & Technol Aircraft Control Lab, Xian 710065, Peoples R China
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For the measurements selection in the component health parameter estimation of turbofan engine, the paper proposes an optimization method. It gives a combination of measurement parameters selection through the health parameters correlation analysis and the condition number of coefficient matrix analysis. The linear estimation method of components health parameters is presented on the basis of measurement selection. At the same time, in order to solve the on-line real-time evaluation of health parameters in engineering, the paper augments the health parameters into state equation. The Kalman filter algorithm can still estimate the health parameters accurately using the chosen measurement parameters. It proves the correctness and effectiveness of the optimization method.
引用
收藏
页码:75 / 80
页数:6
相关论文
共 50 条
  • [41] Turbofan engine transient modeling based on inter-component volume method
    Tang, S.-J., 2013, Beijing University of Aeronautics and Astronautics (BUAA) (28):
  • [42] Automatic Filtering-Based Modification and Updating of Component Characteristics for Turbofan Engine
    Jin P.
    Lu F.
    Huang J.-Q.
    Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (12): : 2664 - 2672
  • [43] Prescribed performance control for nonlinear parameter-varying systems with an application to turbofan engine
    Zhu, Pingfang
    Yu, Lianchen
    Zeng, Jianping
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2023, 360 (12): : 7722 - 7738
  • [44] Health estimation of fan based on belief-rule-base expert system in turbofan engine gas-path
    Yin, Xiaojing
    Wang, Zhanli
    Zhang, Bangcheng
    Zhou, Zhijie
    Gao, Zhi
    ADVANCES IN MECHANICAL ENGINEERING, 2017, 9 (03)
  • [45] A simple model for the estimation of turbofan engine performance in all airborne phases of flight
    Poll, D. I. A.
    Schumann, U.
    AERONAUTICAL JOURNAL, 2024,
  • [46] LOW PRESSURE SYSTEM COMPONENT ADVANCEMENTS AND ITS INFLUENCE ON FUTURE TURBOFAN ENGINE EMISSIONS
    Gronstedt, Tomas
    Au, Dax
    Kyprianidis, Konstantinos
    Ogaji, Stephen
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 4, 2009, : 505 - 516
  • [47] Prognostic and Health Management of an Aircraft Turbofan Engine Using Machine Learning
    Thakkar, Unnati
    Chaoui, Hicham
    2023 IEEE VEHICLE POWER AND PROPULSION CONFERENCE, VPPC, 2023,
  • [48] Thermodynamic analysis of turbofan engine
    Yadav, R.
    Jugseniya, Chandrakant B.
    Pashilkar, Abhay A.
    PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 1, 2005, : 55 - 62
  • [49] A simple model for the estimation of turbofan engine performance in all airborne phases of flight
    Poll, D.I.A.
    Schumann, U.
    Aeronautical Journal, 2024,
  • [50] Assembled method for estimation of turbofan engine high pressure turbine inlet temperature
    Zhao Y.
    Li B.-W.
    Song H.-Q.
    Sun T.
    1600, Beijing University of Aeronautics and Astronautics (BUAA) (31): : 3026 - 3033