Development of a Novel Technique to Address Compressor fouling in a Turbo-shaft Engine

被引:0
|
作者
Kumar, S. Saji [1 ]
Muthu, S. Esakki [2 ]
Dileep, S. [2 ]
Mishra, R. K. [3 ]
机构
[1] Hindustan Aeronaut Ltd, Engine Div, Bangalore 560093, Karnataka, India
[2] Hindustan Aeronaut Ltd, Aero Engine R&D Ctr, Bangalore 560093, Karnataka, India
[3] DRDO, CEMILAC, Reg Ctr Mil Airworthiness Engines, Bangalore 560093, Karnataka, India
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Compressor washing is commonly used in gas turbine engines to retrieve engine power. Severity of fouling should be known to decide on mounted or uninstalled washing and also to optimize the time and money. The present study aims to develop a system for predicting and scheduling the washing process. One 1 MW turbo shaft engine has been taken as the model for this study. The deviations in performance parameters have been quantified based on test data over a period. Deterioration of engine health parameters namely efficiency and flow capability of compressor, gas generator turbine and power turbine are considered for analysis. Sensitivity analysis and ranking of the measurements were done using a correlative technique suggested by Stamatis. The interdependency and observability of the measurements were checked. The fault signatures of selected measurement set on component degradations were isolated and estimation charts were formed to predict the optimum time intervals for compressor washing. The study forms a base platform to apply techniques like artificial neural networks for the accurate forecasting of optimum cleaning intervals for turbo shaft engines.
引用
收藏
页数:10
相关论文
共 46 条
  • [21] Failure analysis on central drive bevel gear of turbo-shaft engine with complex excitation
    Chen X.
    Ma Y.
    Wang Y.
    Hong J.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (06): : 1222 - 1227
  • [22] Research on backup hydromechanical control plan of the turbo-shaft engine's control system
    Liao, Guang-Huang
    Huang, Jin-Quan
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2015, 30 (11): : 2713 - 2720
  • [23] Design and simulation of a control scheme for turbo-shaft engine in helicopter autorotation training process
    Yan, C.-K., 1744, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [24] Analysis of factors influencing the exhaust gas electrostatic monitoring signals of a turbo-shaft engine
    Sun, Jianzhong
    Zuo, Hongfu
    Zhan, Zhijuan
    Liu, Pengpeng
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2012, 33 (03): : 412 - 420
  • [25] Robust disturbance rejection control design for integrated helicopter system/turbo-shaft engine
    Zhang, Haibo
    Sun, Liguo
    Sun, Jianguo
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (05): : 883 - 892
  • [26] Turbo-shaft engine adaptive neural network control based on nonlinear state space equation
    Ziyu GU
    Qiuhong LI
    Shuwei PANG
    Wenxiang ZHOU
    Jichang WU
    Chenyang ZHANG
    Chinese Journal of Aeronautics, 2024, 37 (04) : 493 - 507
  • [27] Gaussian weighted sum clustering method of adaptive hybrid diagnostic model for turbo-shaft engine
    She, Yun-Feng
    Huang, Jin-Quan
    Lu, Feng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (05): : 1178 - 1184
  • [28] An adaptive turbo-shaft engine modeling method based on PS and MRR-LSSVR algorithms
    Wang Jiankang
    Zhang Haibo
    Yan Changkai
    Duan Shujing
    Huang Xianghua
    Chinese Journal of Aeronautics , 2013, (01) : 94 - 103
  • [29] Turbo-shaft engine adaptive neural network control based on nonlinear state space equation
    Gu, Ziyu
    Li, Qiuhong
    Pang, Shuwei
    Zhou, Wenxiang
    Wu, Jichang
    Zhang, Chenyang
    CHINESE JOURNAL OF AERONAUTICS, 2024, 37 (04) : 493 - 507
  • [30] A New Turbo-shaft Engine Control Law during Variable Rotor Speed Transient Process
    Hua, Wei
    Miao, Lizhen
    Zhang, Haibo
    Huang, Jinquan
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2015, 32 (04) : 325 - 340