Hybrid sequential fault estimation for multi-mode diagnosis of gas turbine engines

被引:27
作者
Hanachi, Houman [1 ,2 ]
Liu, Jie [1 ,3 ]
Kim, Il Yong [2 ]
Mechefske, Chris K. [2 ]
机构
[1] Chongqing Technol & Business Univ, Natl Res Base, Intelligent Mfg Serv, Chongqing 400067, Peoples R China
[2] Queens Univ, Dept Mech & Mat Engn, Kingston, ON K7L 3N6, Canada
[3] Carleton Univ, Dept Mech & Aerosp Engn, Ottawa, ON K1S 5B6, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Fault estimation; Real-time diagnosis; Multi-mode diagnosis; Measurement noise; ANFIS; IDENTIFICATION; ALGORITHM; SYSTEM;
D O I
10.1016/j.ymssp.2018.05.054
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Health condition monitoring of Gas Turbine Engine (GTE) components is key for predictive maintenance planning. The task is challenging, as the gas-path components are mostly inaccessible for direct measurements, while at the same time hidden incipient faults must be diagnosed using the available measurements. The presence of multiple faults with similar symptoms adds to the complexity of the diagnostic process. In previous research work, a data-driven multi-mode fault parameter estimation scheme was introduced for real-time multimode diagnosis of GTEs under diverse operating conditions and fault scenarios. In this work, a hybrid diagnostic framework is developed that fuses the results from a measurement-based fault parameter estimation strategy together with a fault propagation model. The hybrid framework uses a novel particle filter (PF) structure with redundant measurements that facilitates updating the particle weights while reducing the dimensionality of the measurement likelihood. Applying the developed framework on GTE gas-path data with four different gradually worsening faults, the results show the diagnostic accuracy increases up to ten times, compared to the previously developed fault parameter estimation scheme. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:255 / 268
页数:14
相关论文
共 51 条
[1]  
[Anonymous], 2017, ENV CANADA
[2]   Turbofan Engine Health Assessment From Flight Data [J].
Aretakis, N. ;
Roumeliotis, I. ;
Alexiou, A. ;
Romesis, C. ;
Mathioudakis, K. .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (04)
[3]   A tutorial on particle filters for online nonlinear/non-Gaussian Bayesian tracking [J].
Arulampalam, MS ;
Maskell, S ;
Gordon, N ;
Clapp, T .
IEEE TRANSACTIONS ON SIGNAL PROCESSING, 2002, 50 (02) :174-188
[4]   Artificial intelligence for the diagnostics of gas turbines - Part II: Neuro-fuzzy approach [J].
Bettocchi, R. ;
Pinelli, M. ;
Spina, P. R. ;
Venturini, M. .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2007, 129 (03) :720-729
[5]   Coupling principal component analysis and Kalman filtering algorithms for on-line aircraft engine diagnostics [J].
Borguet, S. ;
Leonard, O. .
CONTROL ENGINEERING PRACTICE, 2009, 17 (04) :494-502
[6]   PERFORMANCE DETERIORATION IN INDUSTRIAL GAS-TURBINES [J].
DIAKUNCHAK, IS .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1992, 114 (02) :161-168
[7]   Pattern recognition in multivariate time series - A case study applied to fault detection in a gas turbine [J].
Fontes, Cristiano Hora ;
Pereira, Otacilio .
ENGINEERING APPLICATIONS OF ARTIFICIAL INTELLIGENCE, 2016, 49 :10-18
[8]  
Ganguli R., 2004, P ASME TURB 2004 C 2, P499
[9]  
Ganguli R., 2004, ASME TURBO EXPO
[10]  
Ghiocel D., 2001, CRITICAL MODELING IS