DocumentCode :
358387
Title :
Helicopter drive system diagnostics through multivariate statistical process control
Author :
Mimnagh, Michael L. ; Hardman, William ; Sheaffer, Jonathan
Author_Institution :
Dept. of Machinery Silencing, Naval Surface Warfare Center, Philadelphia, PA, USA
Volume :
6
fYear :
2000
fDate :
2000
Firstpage :
381
Abstract :
The Naval Air Warfare Center has developed a Helicopter Integrated Diagnostic System (HIDS) which performs mechanical diagnostics on a helicopter´s drive system. Diagnostic indicators indicative of the mechanical health of the drive system components are derived from vibration data through a combination of statistical and signal processing methods. This paper discusses the application of a multivariate statistical process known as Hotelling´s T2 analyysis to HIDS diagnostic indicators. Multivariate analysis uses a composite function of multiple quality indicators to produce a single, trendable indicator that characterizes the state of the monitored process. A statistically valid method of creating and adjusting an alarm threshold for the resultant composite indicator is inherent in the method. When applied to mechanical diagnostic indicators from helicopter drive system seeded fault tests, the method produced timely and unambiguous fault identification with a reduced number of false alarms as compared to current diagnostic methods
Keywords :
aircraft testing; dynamic testing; fault diagnosis; helicopters; military aircraft; multivariable control systems; statistical process control; vibration measurement; HIDS diagnostic indicators; Helicopter Integrated Diagnostic System; Hotelling´s T2 analysis; Naval Air Warfare Center; alarm threshold; composite function; composite indicator; diagnostic indicators; false alarms; fault identification; helicopter drive; mechanical diagnostic indicators; mechanical diagnostics; mechanical health; multivariate statistical process; multivariate statistical process control; signal processing; vibration data; Aircraft propulsion; Control systems; Fault diagnosis; Helicopters; Intrusion detection; Machinery; Monitoring; Process control; Signal processing; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.877914
Filename :
877914
Link To Document :
بازگشت