DocumentCode :
2006489
Title :
A study of aircraft landing gear testing system on PHM
Author :
Zhou, Yang ; Yunxia, Chen ; Rui, Kang
Author_Institution :
Sch. Of Reliability & Syst. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2011
fDate :
24-25 May 2011
Firstpage :
1
Lastpage :
4
Abstract :
According to statistics, landing gears play the major role in the failure of aircrafts. However there are no specifically testing systems currently in use. To solve this problem, this paper presented a landing gear testing system based on PHM technology, designed a framework of both hardware and software of this system. A precise reference can be given to the experimenters by the system embodied the idea of PHM. An example proving the feasibility of the system is given at the end of this paper.
Keywords :
aircraft maintenance; aircraft testing; instrument landing systems; PHM; aircraft landing gear testing system; Accelerometers; Aerospace safety; Fatigue; Monitoring; Prognostics and health management; Radiation detectors; Stress; PHM; landing gear testing system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Prognostics and System Health Management Conference (PHM-Shenzhen), 2011
Conference_Location :
Shenzhen
Print_ISBN :
978-1-4244-7951-1
Electronic_ISBN :
978-1-4244-7949-8
Type :
conf
DOI :
10.1109/PHM.2011.5939549
Filename :
5939549
Link To Document :
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