DocumentCode :
1887927
Title :
Wireless corrosion monitoring for evaluation of aircraft structural health
Author :
Demo, Jeff ; Friedersdorf, Fritz ; Andrews, Conrad ; Putic, Mateja
Author_Institution :
Luna Innovations Inc., Charlottesville, VA, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
10
Abstract :
The military spends billions of dollars annually on inspection, identification, and repair of damage resulting from aircraft corrosion. The currently available methods for identifying aircraft corrosion damage involve expensive, labor intensive scheduled inspections, resulting in longer periods in depot, and reduction in aircraft availability. In order to increase aircraft safety, availability, and operational efficiency, an on-platform monitoring system capable of fusing data streams from an array of environmental and corrosivity sensors is needed to provide inspection-free indicators of the existence of corrosion as well as the level of corrosive severity in difficult to access aircraft locations. This paper will discuss the design, test, and validation of such a system utilizing a wireless, ultra-low power network of sensors.1 2
Keywords :
aerospace safety; condition monitoring; corrosion; design engineering; inspection; maintenance engineering; military aircraft; structural engineering; wireless sensor networks; aircraft availability; aircraft corrosion; aircraft safety; aircraft structural health; corrosive severity; corrosivity sensor array; damage identification; damage inspection; damage repair; data stream fusing; environmental sensor array; labor intensive-scheduled inspection; on-platform monitoring system; operational efficiency; system design; system test; system validation; wireless corrosion monitoring; wireless ultralow-power sensor network; Aircraft; Corrosion; Humidity; ISO standards; Temperature measurement; Temperature sensors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187362
Filename :
6187362
Link To Document :
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