DocumentCode
3442096
Title
Notice of Retraction
Prognostic theory and key techniques of aircraft hydraulic system
Author
Kang Wang ; Shaoping Wang ; Zhaomin He ; Lei Han
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear
2013
fDate
15-18 July 2013
Firstpage
1702
Lastpage
1706
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The target of this paper is to develop a novel analysis, design and evaluation theory for aircraft hydraulic prognostic and health management system. The main points in this project are to explore failure generation and growth mechanism, and to discover the value of fault feature contributing to system health. A novel aircraft hydraulic system residual life prediction combining field fight data together with infield life evaluation is proposed firstly in this project. Furthermore, this project attempts to solve the difficulties in failure development mechanism, multivariable-fused failure prognostic, and field data dynamically iterated residual life prediction. The research results of this project will serve China large aircraft development plan, and guide aircraft hydraulic system residual life evaluation in future.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The target of this paper is to develop a novel analysis, design and evaluation theory for aircraft hydraulic prognostic and health management system. The main points in this project are to explore failure generation and growth mechanism, and to discover the value of fault feature contributing to system health. A novel aircraft hydraulic system residual life prediction combining field fight data together with infield life evaluation is proposed firstly in this project. Furthermore, this project attempts to solve the difficulties in failure development mechanism, multivariable-fused failure prognostic, and field data dynamically iterated residual life prediction. The research results of this project will serve China large aircraft development plan, and guide aircraft hydraulic system residual life evaluation in future.
Keywords
aircraft; condition monitoring; failure analysis; fault diagnosis; hydraulic systems; iterative methods; China aircraft development plan; aircraft hydraulic system; dynamic iterated residual life prediction; evaluation theory; failure development mechanism; failure generation; fault feature; field fight data; growth mechanism; infield life evaluation; multivariable-fused failure prognostic; prognostic theory; prognostic-health management system; Aircraft; Feature extraction; Hydraulic systems; Maintenance engineering; Prognostics and health management; Vibrations; data driven; failure physic; health evaluation; integrated prognostics; residual life;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4799-1014-4
Type
conf
DOI
10.1109/QR2MSE.2013.6625904
Filename
6625904
Link To Document