DocumentCode :
3584388
Title :
PROMIS - A generic PHM methodology applied to aircraft subsystems
Author :
Smeulers, J.P.M. ; Zeelen, R. ; Bos, A.
Author_Institution :
TPD, TNO, Delft, Netherlands
Volume :
6
fYear :
2002
fDate :
6/24/1905 12:00:00 AM
Firstpage :
457802
Abstract :
This paper describes the basic concepts of the PROMIS methodology for system´s Prognostic Health Management (PHM). The key elements of the PROMIS methodology are: (i) system health is monitored by continuously measuring so-called Condition Parameters (CPs), representing the physical condition of critical system components, (ii) CPs are derived using model-based estimation processes so that the existing set of sensors is exploited as much as possible, and (iii) the remaining lifetime of components is calculated using aging models and the expected system load.
Keywords :
ageing; aircraft testing; condition monitoring; PROMIS; aging model; aircraft subsystem; component lifetime; condition parameters; prognostic health management; system health monitoring; Aging; Aircraft; Condition monitoring; Costs; Filters; Life testing; Logistics; Prognostics and health management; Sensor systems; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1036156
Filename :
1036156
Link To Document :
بازگشت