DocumentCode
2273889
Title
Predicting the remaining life of propulsion system bearings
Author
Marble, Sean ; Morton, Brogan P.
Author_Institution
Sentient Corp., Idaho Falls, ID
fYear
0
fDate
0-0 0
Abstract
Diagnostic technologies for rolling element bearings are relatively well developed, but accurate prediction of remaining life once an incipient fault has been detected is considerably more difficult. This paper describes a comprehensive experimental study of bearing spall progression and a physics-based model being developed for bearing prognostics. The model computes the spall growth trajectory and time to failure based on operating conditions, and uses diagnostic feedback to self-adjust and reduce prediction uncertainty. The predictions compare very well to fault progression tests on both subscale bearings and full-scale turbine engine bearings. The experimental data has demonstrated that spall propagation is better behaved than once thought and can be predicted with high confidence. For turbine engine core thrust bearings with a typical mission mix, the prognostic window (first detection to failure) is on the order of 100 flight hours, which provides ample opportunity to plan future missions and maintenance activities with considerable safety margin. Since the model is physics-based, it is readily adaptable to most bearing applications, and a reduced order version has also been developed which is efficient enough to run on-board with little or no loss in accuracy
Keywords
aerospace engines; aerospace propulsion; fault diagnosis; machine bearings; remaining life assessment; bearing prognostics; bearing spall progression; diagnostic feedback; fault progression; incipient fault; physics-based model; prediction uncertainty; propulsion system bearings; reduced order model; remaining life prediction; rolling element bearings; spall growth trajectory; spall propagation; spall time to failure; thrust bearings; turbine engine bearings; Engines; Fault detection; Feedback; Predictive models; Propulsion; Rolling bearings; Testing; Trajectory; Turbines; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2006 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-9545-X
Type
conf
DOI
10.1109/AERO.2006.1656121
Filename
1656121
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