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