DocumentCode
1769235
Title
Design on the health and usage monitoring system
Author
Yong Shen ; Xingwang Li ; Xiumei Zhai ; Huiyun Wang ; Yifei He
Author_Institution
Key Lab. of Aviation Technol. for Fault Diagnosis & Health Manage. Res., Avic Shanghai Aero Meas.-controlling Res. Inst., Shanghai, China
fYear
2014
fDate
24-27 Aug. 2014
Firstpage
465
Lastpage
468
Abstract
For the mechanical parts of helicopter easily damaged and often inducing accident, the key system to ensure flight safety of helicopter and achieve the on-condition maintenance is HUMS. In the paper the key technologies of HUMS are researched including position optimizing of the sensors, flight safety monitoring and diagnosing technology, the method of setting threshold, and it is dissertated in detail about the main function assemblies and realization methods of this system. The application in helicopter showed that this system could improve the flight security, prevent air accident, and enhance the maintenance capability.
Keywords
accident prevention; aerospace safety; condition monitoring; helicopters; maintenance engineering; air accident prevention; flight safety diagnosing technology; flight safety monitoring; health monitoring system; helicopter; mechanical parts; on-condition maintenance; usage monitoring system; Helicopters; Maintenance engineering; Monitoring; Rotors; Safety; Sensors; Vibrations; HUMS; fault diagnosis; helicopter;
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.2014.6988216
Filename
6988216
Link To Document