中国航空学报(英文版)
中國航空學報(英文版)
중국항공학보(영문판)
CHINESE JOURNAL OF AERONAUTICS
2014年
5期
1288-1300
,共13页
Iosipescu shear tests%Nanocomposites%Optimum nanofiller weight percentage%Scanning electron microscopic%Tension tests%Ultrasonic
Epocast 50-A1/946 epoxy was primarily developed for joining and repairing of compos-ite aircraft structural components. The objective of the present work is to modify the Epocast epoxy resin by different nanofillers infusion. The used nanofillers include multi-walled carbon nanotubes (MWCNTs), SiC and Al2O3 nanoparticles. The nanofillers with different weight percentages are ultrasonically dispersed in the epoxy resin. The sonication time and amplitude for MWCNTs are reduced compared to Al2O3 and SiC nanoparticles to avoid the damage of MWCNTs during son-ication processes. The fabricated neat epoxy and twelve nanocomposite panels were characterized via standard tension and in-plane shear tests. The experimental results show that the nanocompos-ites materials with 0.5wt% MWCNTs, 1.5wt% SiC and 1.5wt% Al2O3 nanoparticles have the highest improvement in the tensile properties compared to the other nanofiller loading percentages. The improvements in the shear properties of these nanocomposite materials were respectively equal to 5.5%, 4.9%, and 6.3%for shear strengths, and 10.3%, 16.0%, and 8.1%for shear moduli. The optimum nanofiller loading percentages will be used in the following papers concerning their effect on the bonded joints/repairs of carbon fiber reinforced composites.