TY - CONF
T1 - Optical stress sensing alumina nanocomposite coatings for aerospace structures
AU - Freihofer, Gregory
AU - Gupta, Ankur
AU - Van Newkirk, Amy
AU - Seal, Sudipta
AU - Raghavan, Seetha
N1 - Funding Information:
The authors would like to thank the staff at Boeing’s Research and Technology group for providing the OHT samples. ELANTAS PDG is acknowledged for their assistance with material processing. Dr. Axel Schülzgen, CREOL at UCF is acknowledged for supplying Fiber Bragg grating fibers. Scientists at the Center for Nanoscale Materials (CNM) at Argonne National Laboratory (ANL) who assisted with SEM imaging. Use of the Center for Nanoscale Materials was supported by the U. S. Department of Energy, Office of Science, Office of Basic Energy Sciences, under Contract No. DE-AC02-06CH11357. This material is based upon work supported by the National Science Foundation under Grant No. CMMI 1130837.
PY - 2014
Y1 - 2014
N2 - Alpha alumina (α-Al2O3) nanocomposites have a multi-functional stress sensing ability via their photoluminescence (PL) spectral peak shifts defined by Piezospectroscopic (PS) relationships. This has prompted the development of α-Al2O3 nanocomposite coatings to enable real-time stress measurements and damage assessment of structures with the potential for unparalleled spatial resolution and sensitivity. Here, two types of stress-sensing coatings were evaluated, including an atmospheric plasma spray (APS) coating on metallic substrates and an epoxy nanocomposite coating on a composite substrate. The stress sensitivity of the APS coating, represented by the slope of the peak shifts against stress or PS coefficient, varied inversely with the thickness of the substrates between 3.2 and 1.7 cm-1=GPa. These values decreased by more than 50% after tensile cycling for all substrate thicknesses due to microstructural damage in the APS coating indicating the need for repeatability and durability studies. The epoxy nanocomposite coating successfully captured the stress gradients associated with an open hole tension (OHT) composite substrate revealing damage initiation at 77% of failure load, earlier than visual appearance of a surface crack (93%). The findings validate the successful development of quantitative and multiscale spatial resolution stress-sensing coatings, capable of detecting subsurface damage of composite structures, that will take structural testing and integrity monitoring to the next level.
AB - Alpha alumina (α-Al2O3) nanocomposites have a multi-functional stress sensing ability via their photoluminescence (PL) spectral peak shifts defined by Piezospectroscopic (PS) relationships. This has prompted the development of α-Al2O3 nanocomposite coatings to enable real-time stress measurements and damage assessment of structures with the potential for unparalleled spatial resolution and sensitivity. Here, two types of stress-sensing coatings were evaluated, including an atmospheric plasma spray (APS) coating on metallic substrates and an epoxy nanocomposite coating on a composite substrate. The stress sensitivity of the APS coating, represented by the slope of the peak shifts against stress or PS coefficient, varied inversely with the thickness of the substrates between 3.2 and 1.7 cm-1=GPa. These values decreased by more than 50% after tensile cycling for all substrate thicknesses due to microstructural damage in the APS coating indicating the need for repeatability and durability studies. The epoxy nanocomposite coating successfully captured the stress gradients associated with an open hole tension (OHT) composite substrate revealing damage initiation at 77% of failure load, earlier than visual appearance of a surface crack (93%). The findings validate the successful development of quantitative and multiscale spatial resolution stress-sensing coatings, capable of detecting subsurface damage of composite structures, that will take structural testing and integrity monitoring to the next level.
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U2 - 10.2514/6.2014-0159
DO - 10.2514/6.2014-0159
M3 - Paper
AN - SCOPUS:84894492976
T2 - 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference - SciTech Forum and Exposition 2014
Y2 - 13 January 2014 through 17 January 2014
ER -