DocumentCode
3516524
Title
Use of Paris Law for Prediction of Component Remaining Life
Author
Bechhoefer, Eric ; Bernhard, Andreaus ; He, David
Author_Institution
Goodrich SIS, Vergennes, VT
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
9
Abstract
Vibration based health and usage monitoring systems (HUMS) are providing good information as to the current state of a component, (e.g. health), but other than simple trending, are not robust enough to yield an estimated of the remaining useful life (RUL). There are three fundamental problems that need to be address to accurately estimate RUL. First, health index data is noisy. Even with filtering, the HI can be difficult to trend. Second - a damage model is required address component degradation. Finally, a relationship between physical damage and measured health/condition needs to be established.
Keywords
aircraft instrumentation; aircraft maintenance; aircraft testing; condition monitoring; vibrations; Paris law; address component degradation; component remaining life; health index data; remaining useful life; vibration based health-and-usage monitoring systems; Aircraft propulsion; Filtering; Gears; Helium; Industrial engineering; Logistics; Monitoring; Shafts; Testing; Vibration measurement;
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.2008.4526611
Filename
4526611
Link To Document