Correlation between Drop Impact Energy and Residual Compressive Strength According to the Lamination of CFRP with EVA Sheets

被引:9
作者
Go, Sun-Ho [1 ]
Lee, Min-Sang [1 ]
Hong, Chang-Gi [2 ]
Kwac, Lee-Ku [3 ]
Kim, Hong-Gun [3 ]
机构
[1] Jeonju Univ, Grad Sch, Dept Mech Engn, Jeonju 55069, South Korea
[2] Jeonju Univ, Grad Sch, Dept Carbon Fus Engn, Jeonju 55069, South Korea
[3] Jeonju Univ, Dept Automot Engn, Jeonju 55069, South Korea
基金
新加坡国家研究基金会;
关键词
carbon-fiber-reinforced plastic; building materials; impact; ethylene vinyl acetate; DAMAGE; COMPOSITES;
D O I
10.3390/polym12010224
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
Carbon-fiber-reinforced plastic is an important building material; however, its application is limited because of its brittleness, leading to vulnerability under shock. Thus, the strength performance of carbon-fiber-reinforced plastics needs to be improved. Here, the drop impact test was conducted to analyze the impact energy and fracture characteristics of carbon-fiber-reinforced plastics and ethylene vinyl acetate sheets. The compression after impact test was performed to assess the residual compressive strength. The thermal energy generated was measured as change in temperature at the time of fracture to investigate the relationship between thermal and mechanical properties. The impact absorption efficiency of 100% was achieved when the carbon-fiber-reinforced plastics specimen was laminated with four or more sheets of ethylene vinyl acetate. The thermal energy generated during impact, the impact load, and the compression after impact test strength was reduced with the increasing number of laminated ethylene vinyl acetate layers. Our results showed that, by carefully selecting the optimal conditions of fabricating the carbon-fiber-reinforced plastic/ethylene vinyl acetate composites, carbon composite materials can be used for impact mitigation.
引用
收藏
页数:17
相关论文
共 19 条
[1]  
BYUN JONGIK, 2018, [Transactions of the Korean Hydrogen and New Energy Society, 한국수소및신에너지학회논문집], V29, P190
[2]  
서영욱, 2011, [Aerospace Engineering and Technology, 항공우주기술], V10, P183
[3]   Electrospun nanofibrous interleaves for improved low velocity impact resistance of glass fibre reinforced composite laminates [J].
Daelemans, Lode ;
Cohades, Amael ;
Meireman, Timo ;
Beckx, Jasper ;
Spronk, Siebe ;
Kersemans, Mathias ;
De Baere, Ives ;
Rahier, Hubert ;
Michaud, Veronique ;
Van Paepegem, Wim ;
De Clerck, Karen .
MATERIALS & DESIGN, 2018, 141 :170-184
[4]   IMPACT DAMAGE PREDICTION IN CARBON COMPOSITE STRUCTURES [J].
DAVIES, GAO ;
ZHANG, X .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1995, 16 (01) :149-170
[5]   Experimental determination of compressive residual strength of a carbon/epoxy laminate after a near-edge impact [J].
Falaschetti, M. P. ;
Scafe, M. ;
Troiani, E. ;
Agostinelli, V. ;
Sangiorgi, S. .
XXIII ITALIAN GROUP OF FRACTURE MEETING, IGFXXIII, 2015, 109 :171-180
[6]   The impact fracture behaviors of CFRP/EVA composites by drop-weight impact test [J].
Go, Sun-Ho ;
Kim, Hong-Gun ;
Shin, Hee-Jae ;
Lee, Min-Sang ;
Yoon, Hyun-Gyung ;
Kwac, Lee-Ku .
CARBON LETTERS, 2017, 21 (01) :23-32
[7]  
Han J.W., 2008, J KOREAN SOC SAFETY, V23, P24
[8]  
Joo HJ, 2002, POLYM-KOREA, V26, P270
[9]   Determination of Shock Absorption Performance and Shear Modulus of Rubbers by Drop Impact Test [J].
Kang, Dong-Hwan ;
Seo, Mu-Yeol ;
Gimm, Hakin ;
Kim, Tae-Won .
TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENGINEERS A, 2009, 33 (04) :321-328
[10]   Effects of alumina nanoparticles on dynamic impact responses of carbon fiber reinforced epoxy matrix nanocomposites [J].
Kaybal, Halil B. ;
Ulus, Hasan ;
Demir, Okan ;
Sahin, Omer S. ;
Avci, Ahmet .
ENGINEERING SCIENCE AND TECHNOLOGY-AN INTERNATIONAL JOURNAL-JESTECH, 2018, 21 (03) :399-407