TY - GEN
T1 - Application of smart coating sensor in crack detection for aircraft
AU - Liu, Mabao
AU - Wang, Xianhui
AU - Liu, Qida
AU - Gao, Hong
PY - 2012
Y1 - 2012
N2 - A novel smart coating sensor, consisted of driving layer, sensing layer and protective layer, has been successfully developed, and it was utilized to detect crack initiation and growth in fatigue tests. The results show that the smart coating sensor can detect cracks above 300μm, corresponding to the increment of the sensing layer's resistance at the level of 0.05Ω. Subsequently, the development of SCS is of importance significance in the substitution of an existed inspection that requires substantial disassembly and surface preparation, and, thus, can find numerous applications in difficult-to-access locations on commercial and military aircrafts.
AB - A novel smart coating sensor, consisted of driving layer, sensing layer and protective layer, has been successfully developed, and it was utilized to detect crack initiation and growth in fatigue tests. The results show that the smart coating sensor can detect cracks above 300μm, corresponding to the increment of the sensing layer's resistance at the level of 0.05Ω. Subsequently, the development of SCS is of importance significance in the substitution of an existed inspection that requires substantial disassembly and surface preparation, and, thus, can find numerous applications in difficult-to-access locations on commercial and military aircrafts.
KW - Aircraft
KW - Crack
KW - Resistance
KW - Smart coating
UR - https://www.scopus.com/pages/publications/84863170911
U2 - 10.4028/www.scientific.net/AMM.152-154.554
DO - 10.4028/www.scientific.net/AMM.152-154.554
M3 - 会议稿件
AN - SCOPUS:84863170911
SN - 9783037853528
T3 - Applied Mechanics and Materials
SP - 554
EP - 559
BT - Mechanical Engineering and Materials
T2 - 2012 International Conference on Mechanical Engineering and Materials, ICMEM 2012
Y2 - 15 January 2012 through 16 January 2012
ER -