Layered clustering multi-fault diagnosis for hydraulic piston pump

Abstract Efficient diagnosis is very important for improving reliability and performance of aircraft hydraulic piston pump, and it is one of the key technologies in prognostic and health management system. In practice, due to harsh working environment and heavy working loads, multiple faults of an aircraft hydraulic pump may occur simultaneously after long time operations. However, most existing diagnosis methods can only distinguish pump faults that occur individually. Therefore, new method needs to be developed to realize effective diagnosis of simultaneous multiple faults on aircraft hydraulic pump. In this paper, a new method based on the layered clustering algorithm is proposed to diagnose multiple faults of an aircraft hydraulic pump that occur simultaneously. The intensive failure mechanism analyses of the five main types of faults are carried out, and based on these analyses the optimal combination and layout of diagnostic sensors is attained. The three layered diagnosis reasoning engine is designed according to the faults' risk priority number and the characteristics of different fault feature extraction methods. The most serious failures are first distinguished with the individual signal processing. To the desultory faults, i.e., swash plate eccentricity and incremental clearance increases between piston and slipper, the clustering diagnosis algorithm based on the statistical average relative power difference (ARPD) is proposed. By effectively enhancing the fault features of these two faults, the ARPDs calculated from vibration signals are employed to complete the hypothesis testing. The ARPDs of the different faults follow different probability distributions. Compared with the classical fast Fourier transform-based spectrum diagnosis method, the experimental results demonstrate that the proposed algorithm can diagnose the multiple faults, which occur synchronously, with higher precision and reliability.

[1]  David He,et al.  A segmental hidden semi-Markov model (HSMM)-based diagnostics and prognostics framework and methodology , 2007 .

[3]  Atsushi Yamaguchi Tribology of Hydraulic Pumps , 1997 .

[4]  Andrew K. S. Jardine,et al.  Optimizing a mine haul truck wheel motors’ condition monitoring program Use of proportional hazards modeling , 2001 .

[5]  Liu Hongmei,et al.  Fault diagnosis based on wavelet package and Elman neural network for a hydraulic pump , 2007 .

[6]  Zhen Zhao,et al.  Intermittent chaos and sliding window symbol sequence statistics-based early fault diagnosis for hydraulic pump on hydraulic tube tester , 2009 .

[7]  Qin Zhang,et al.  A Wavelet Packet and Residual Analysis Based Method for Hydraulic Pump Health Diagnosis , 2006 .

[8]  Patrick S. K. Chua,et al.  Fault degradation assessment of water hydraulic motor by impulse vibration signal with Wavelet Packet Analysis and Kolmogorov–Smirnov Test , 2008 .

[9]  Qin Zhang,et al.  WAVELET--BASED PRESSURE ANALYSIS FOR HYDRAULIC PUMP HEALTH DIAGNOSIS , 2003 .

[10]  Andrew Hess,et al.  PHM and Corrosion Control on the Joint Strike Fighter , 2007 .

[11]  Lin Tingqi,et al.  Fault diagnosis of airplane hydraulic pump , 2002, Proceedings of the 4th World Congress on Intelligent Control and Automation (Cat. No.02EX527).

[12]  Peng Chen,et al.  Intelligent Method for Condition Diagnosis of Pump System Using Discrete Wavelet Transform, Rough Sets and Neural Network , 2007, 2007 Second International Conference on Bio-Inspired Computing: Theories and Applications.

[13]  Matti Pietola,et al.  Usefulness of high-resolution thermography in fault diagnosis of fluid power components and systems , 1996, Defense, Security, and Sensing.

[14]  Martin B. Treuhaft,et al.  Wear Measurement of a Large Hydraulic Fluid Power Pump Using Radioactive Tracer Wear Technology , 2003 .

[15]  William Scheuren,et al.  Joint Strike Fighter Prognostics and Health Management , 1998 .

[16]  M. Glade,et al.  Life cycle cost impact of using prognostic health management (PHM) for helicopter avionics , 2007, Microelectron. Reliab..

[17]  N. Scott Clements,et al.  Prognostics and Health Management as Design Variable in Air-Vehicle Conceptual Design , 2006 .

[18]  Xiaomin Zhao,et al.  Vibration-Based Fault Diagnosis of Slurry Pumps Using the Neighborhood Rough Set Model , 2009 .

[19]  Wright-Patterson Afb,et al.  Distributed, Integrated PHM and Control via Smart Engine Accessories for Future Modern Aircraft , 2010 .