DocumentCode :
2250317
Title :
A data fusion based approach for evaluation of material loss in corroded aluminum panels
Author :
De, S. ; Gupta, K. ; Stanley, R.J. ; Steffes, G. ; Palmer, D. ; Zoughi, R.
Author_Institution :
Dept. of Electr. & Comput. Eng., Missouri Univ. of Sci. & Technol., Rolla, MO, USA
fYear :
2009
fDate :
4-7 Oct. 2009
Firstpage :
1
Lastpage :
6
Abstract :
Nondestructive Testing (NDT) is used to detect hidden corrosion in ageing aircraft structures. Use of any single NDT modality provides an incomplete picture of the corrosion environment. Data fusion techniques can be used for improved visualization and automated detection of hidden corrosion in multilayered structures. This work investigates a data fusion based technique using ultrasound measurements from corroded aircraft samples for estimating material loss. Experimental results are presented and suggestions for future work are made for evaluating residual structural integrity of the panels for a damage tolerance approach to corrosion mitigation.
Keywords :
aerospace components; aerospace materials; ageing; aircraft testing; aluminium; corrosion; multilayers; sensor fusion; structural panels; ultrasonic materials testing; Al; NDT; ageing aircraft structures; automated detection; corroded aluminum panels; damage tolerance approach; data fusion techniques; hidden corrosion; material loss; multilayered structures; nondestructive testing; residual structural integrity; Aerospace materials; Aging; Aircraft; Aluminum; Corrosion; Data visualization; Loss measurement; Nondestructive testing; Ultrasonic imaging; Ultrasonic variables measurement; Corrosion; PACS: 81.70.-q; Structural Analysis; data fusion; nondestructive evaluation; ultrasound;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Transportation Systems, 2009. ITSC '09. 12th International IEEE Conference on
Conference_Location :
St. Louis, MO
Print_ISBN :
978-1-4244-5519-5
Electronic_ISBN :
978-1-4244-5520-1
Type :
conf
DOI :
10.1109/ITSC.2009.5309830
Filename :
5309830
Link To Document :
بازگشت