DocumentCode :
3584335
Title :
The development and demonstration of a probabilistic diagnostic and prognostic system (ProDAPS) for gas turbines
Author :
Callan, Robert ; Larder, Brian
Author_Institution :
Electron. Syst., Smiths Aerosp., Eastleigh, UK
Volume :
6
fYear :
2002
fDate :
6/24/1905 12:00:00 AM
Firstpage :
432235
Abstract :
Smiths Aerospace, Electronic Systems, has been engaged by the US Air Force Research Laboratory (AFRL) on a dual-use science and technology program to develop a probabilistic diagnostic and prognostic system (ProDAPS) for engine health management. This paper introduces the components of ProDAPS and the rationale for the adopted approach, along with some preliminary results and future directions.
Keywords :
aerospace engines; condition monitoring; fault diagnosis; gas turbines; life cycle costing; safety systems; ProDAPS; Smiths Aerospace; US Air Force Research Laboratory; engine health management; gas turbine engines; life-cycle costs; operational capabilities; probabilistic diagnostic and prognostic system; safety; Aerospace electronics; Aerospace safety; Data mining; Engines; Laboratories; Monitoring; Technology management; Testing; Turbines; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1036150
Filename :
1036150
Link To Document :
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