Affiliation:
1. Universiti Teknologi Malaysia
Abstract
Blade fault is one of the most common faults in turbomachinery. In this article, a rotor system consists of multiple rows of blade was developed. The effectiveness of conventional FFT spectrum and wavelet analysis in the diagnosis of multi stage blade rubbing faults is examined at different stages, variety of blade fault conditions, and different blades rubbing severity. Blade fault caused impacts and the use of wavelets as analysis tool to detect the blade faults was studied. Results showed that, vibration spectrum can clearly depict the location and the stage of blade rubbing, while it is difficult to be identified in wavelet analysis. The limitations of wavelet analysis for multi stage blade fault diagnosis were identified. Some probable solutions to improve wavelet time-frequency representation in blade fault diagnosis were also presented.
Publisher
Trans Tech Publications, Ltd.
Reference14 articles.
1. Meher-Homji, C.B. (1995b). Blading Vibration and Failures in Gas Turbines: Part B, Compressor and Turbine Airfoil Distress. ASME paper no. 95- (1995) GT-419.
2. Abdelrhman, A.M., et al., A Review of Vibration Monitoring as a Diagnostic Tool for Turbine Blade Faults, Applied Mechanics and Materials, (2012). 229: pp.1459-1463.
3. M Salman LEONG, Field Experiences of Gas Turbines Vibrations -A Review and Case Studies, Journal of System Design and Dynamics, Vol. 2, No. 1 (2008), pp.24-35.
4. Simmons, H.R., a Non-Intrusive Method for Detecting HP Blade Resonance, ASME Paper, 1986, No. 86-JPGC-Pwr-36.
5. Simmons, H.R. (1987), Non-Intrusive Detection of Turbine Blade Resonance, Third EPRI Conference on Incipient Failure Detection in Power Plants, (1987) Philadelphia.
Cited by
8 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献