DocumentCode :
3516491
Title :
Leakage Fault Detection Method for Axial-Piston Variable Displacement Pumps
Author :
Palazzolo, Jerome J. ; Scheunemann, Larry D. ; Hartin, John R.
Author_Institution :
Sentient Corp., Williston, VT
fYear :
2008
fDate :
1-8 March 2008
Firstpage :
1
Lastpage :
8
Abstract :
To address the lack of health monitoring for gas turbine engine accessory components, Sentient developed a promising fault estimation algorithm for axial-piston variable displacement pumps. The key to this success was the development of a physics-based nonlinear model of the system that includes three common types of fluid leakage faults. The modeling effort and simulation results provided the thorough knowledge needed to extract features from the system responses to detect the occurrence of faults. The nominal pump and the pump with a single piston replaced by three different machined pistons were tested to emulate varying stages of piston wear. The experiments demonstrated that the model was able to capture the dynamic behavior of the actual system. By considering several time and frequency domain metrics, a fault estimation method was developed that correctly identified the presence and severity of leakage faults, while using a fraction of the memory and computational resources of other model-based methods.
Keywords :
aerospace engines; aerospace instrumentation; condition monitoring; fault diagnosis; gas turbines; pistons; pumps; wear; axial-piston variable displacement pumps; fault estimation algorithm; fluid leakage faults; gas turbine engine; health monitoring; leakage fault detection method; physics-based nonlinear model; piston wear; Engines; Fault detection; Feature extraction; Frequency domain analysis; Frequency estimation; Monitoring; Pistons; Pumps; Testing; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2008 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-1487-1
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2008.4526609
Filename :
4526609
Link To Document :
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