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
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