DocumentCode :
1769318
Title :
Intelligent diagnosis for aero-engine wear condition based on immune theory
Author :
Anxiang Ma ; Yanjun Li ; Yuyuan Cao ; Gang An ; Zhenyu Wang
Author_Institution :
Coll. of Civil Aviation, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2014
fDate :
24-27 Aug. 2014
Firstpage :
678
Lastpage :
682
Abstract :
Based on the traditional oil monitoring technology and combined with the artificial immune system´s advantages, such as adaptive characteristic, learning and memory characteristic and recognition characteristics, an intelligent diagnosis method for aero-engine wear condition is proposed. The method uses negative selection principle of artificial immune theory to build detectors, and then uses fault samples to train and evolve mature detectors. So the typical information of aeroengine wear conditions is stored in the detectors. Wear failure of the system can be found through the activated detectors. The results of sample data analysis demonstrate that the method has strong ability to recognize aero-engine wear faults.
Keywords :
aerospace computing; aerospace engines; artificial immune systems; failure (mechanical); fault diagnosis; learning (artificial intelligence); mechanical engineering computing; wear; activated detectors; adaptive characteristic; aero-engine wear condition; aero-engine wear fault recognition; artificial immune system; immune theory; intelligent diagnosis; learning characteristic; memory characteristic; negative selection principle; oil monitoring technology; recognition characteristics; sample data analysis; wear failure; Artificial intelligence; Detectors; Fatigue; Fault diagnosis; Gears; Immune system; Indexes; aero-engine; artificial immune theory; fault diagnosis; oil analysis; wear;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Prognostics and System Health Management Conference (PHM-2014 Hunan), 2014
Conference_Location :
Zhangiiaijie
Print_ISBN :
978-1-4799-7957-8
Type :
conf
DOI :
10.1109/PHM.2014.6988259
Filename :
6988259
Link To Document :
بازگشت