DocumentCode :
3144833
Title :
An Integrated PHM Approach for Gas Turbine Engines
Author :
Patnaik, Alok R. ; Narasimhan, V. ; Nayak, Amiya ; Patnaik, Prakash C.
Author_Institution :
Tecsis Corp., Ottawa, Ont.
fYear :
2006
fDate :
38838
Firstpage :
2476
Lastpage :
2479
Abstract :
The prognosis & health management (PHM) of aerospace components is a very complex system. A complete PHM system involves sensors, signal processing, condition monitoring, health assessment, physical reasoning and decision-making. Such an integrated approach to prognostics involves physics-based modelling, experience-based modelling and modelling based on the statistical properties of the components by using neural network and fuzzy logic techniques. In this paper, we give an overview of the PHM system currently being developed
Keywords :
aerospace components; aerospace computing; aerospace industry; condition monitoring; fuzzy logic; gas turbines; neural nets; statistics; aerospace components; aerospace industry; condition monitoring; decision-making; experience-based modelling; fuzzy logic technique; gas turbine engines; health assessment; neural network; physical reasoning; physics-based modelling; prognosis-health management; sensors; signal processing; statistical properties; Aerospace components; Condition monitoring; Decision making; Engines; Fuzzy logic; Neural networks; Prognostics and health management; Sensor systems; Signal processing; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Computer Engineering, 2006. CCECE '06. Canadian Conference on
Conference_Location :
Ottawa, Ont.
Print_ISBN :
1-4244-0038-4
Electronic_ISBN :
1-4244-0038-4
Type :
conf
DOI :
10.1109/CCECE.2006.277288
Filename :
4055072
Link To Document :
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