DocumentCode :
2470210
Title :
Research of prognostics and health management for Aircraft Propulsion System
Author :
Xu, Menglin ; Han, Minghong
Author_Institution :
Sch. of Reliability & Syst. Eng., Beihang Univ., Beijing, China
fYear :
2012
fDate :
23-25 May 2012
Firstpage :
1
Lastpage :
4
Abstract :
Aircraft Propulsion System is a complex system which needs to be detected to make sure the safety of flying and maintain in time. The prognostics and health management (PHM) of aircraft propulsion system is the core of the PHM of whole aircraft. Because of it is considered that the ground surveillance technology is more important than the online PHM, this paper introduces the connotation, functionalities and architecture of prognostics and health management. The function requirement and allocation of the prognostics and health management of aircraft propulsion system is considered to design PHM, in the terms of architecture and functionalities. The integrated prognostics is described and designed. An inference engine is proposed. The designing and the function of integrated diagnosis of Prognostics and Health Management for Aircraft Propulsion System are achieved. And it has great value for engineering applications.
Keywords :
aerospace propulsion; aerospace safety; aircraft; condition monitoring; failure analysis; fault diagnosis; inference mechanisms; mechanical engineering computing; PHM allocation; PHM architecture; PHM connotation; aircraft propulsion system; complex system; flying safety; function requirement; ground surveillance technology; inference engine; integrated prognostics; prognostic and health management; Aircraft Propulsion System; function requirement; integrated diagnosis; prognostics and health management;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Prognostics and System Health Management (PHM), 2012 IEEE Conference on
Conference_Location :
Beijing
ISSN :
2166-563X
Print_ISBN :
978-1-4577-1909-7
Electronic_ISBN :
2166-563X
Type :
conf
DOI :
10.1109/PHM.2012.6228891
Filename :
6228891
Link To Document :
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