Low velocity impact response of fibre metal laminates based on aramid fibre reinforced polypropylene

被引：43

作者：

Carrillo, J. G. ^{[1
]}

Gonzalez-Canche, N. G. ^{[1
]}

Flores-Johnson, E. A. ^{[2
]}

Cortes, P. ^{[3
]}

机构：

[1] Ctr Invest Cient Yucatan, Unidad Mat, Calle 43,130, Merida 97205, Yucatan, Mexico

[2] Ctr Invest Cient Yucatan, CONACYT, Unidad Mat, Calle 43,130, Merida 97205, Yucatan, Mexico

[3] Youngstown State Univ, Civil Environm & Chem Engn Dept, One Univ Plaza, Youngstown, OH 44555 USA

来源：

COMPOSITE STRUCTURES | 2019年 / 220卷

关键词：

Fibre metal laminate; Low velocity impact; Thermoplastic composite; Aluminium; MECHANICAL-PROPERTIES; AZ31B-H24; MAGNESIUM; ALUMINUM; BEHAVIOR; DAMAGE; PERFORMANCE; RESISTANCE;

D O I：

10.1016/j.compstruct.2019.04.018

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

In this work, the low velocity impact behaviour of thermoplastic fibre metal laminates (FMLs) made of aramid fibre reinforced polypropylene and aluminium alloy Al 5052-H32 is presented. The impact behaviour of these FMLs and their constituent materials was determined using a drop-weight impact tower. Force-time curves were used to obtain the absorbed energy for each tested material at different impact energies. The results showed that the FML configuration based on a 3/4 layering arrangement (3 layers of aluminium and 4 layers of composite) exhibited the highest specific absorbed energy for the first damage and perforation threshold when compared to the other laminates and constituent materials here studied. Optical analysis showed that the plastic deformation and the tearing of the aluminium layers, as well as fibre breakage and delamination were the main impact energy-absorption mechanisms. These findings warrant further research to fully understand the low velocity impact behaviour of these thermoplastic FMLs for engineering applications.

引用

页码：708 / 716

页数：9

共 43 条

[1] The impact resistance of polypropylene-based fibre-metal laminates [J].

Abdullah, M. R. ;

Cantwell, W. J. .

COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (11-12) :1682-1693

[2]

[Anonymous], 2001, FIBRE METAL LAMINATE

[3] Investigation of fatigue crack growth rate in CARALL, ARALL and GLARE [J].

Asghar, W. ;

Nasir, M. A. ;

Qayyum, F. ;

Shah, M. ;

Azeem, M. ;

Nauman, S. ;

Khushnood, S. .

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2017, 40 (07) :1086-1100

[4] Fiber metal laminates: An advanced material for future aircraft [J].

Asundi, A ;

Choi, AYN .

JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 1997, 63 (1-3) :384-394

[5] An experimental investigation on the impact response of fiberglass/aluminum composites [J].

Atas, Cesim .

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2007, 26 (14) :1479-1491

[6] An experimental and numerical investigation on the low velocity impact response of thermoplastic hybrid composites [J].

Bandaru, Aswani Kumar ;

Patel, Shivdayal ;

Ahmad, Suhail ;

Bhatnagar, Naresh .

JOURNAL OF COMPOSITE MATERIALS, 2018, 52 (07) :877-889

[7] Impact damage growth in carbon fibre aluminium laminates [J].

Bienias, Jaroslaw ;

Jakubczak, Patryk .

COMPOSITE STRUCTURES, 2017, 172 :147-154

[8] Ballistic performance of thermoplastic composite laminates made from aramid woven fabric and polypropylene matrix [J].

Carrillo, J. G. ;

Gamboa, R. A. ;

Flores-Johnson, E. A. ;

Gonzalez-Chi, P. I. .

POLYMER TESTING, 2012, 31 (04) :512-519

[9] Mechanical properties of a novel fiber-metal laminate based on a polypropylene composite [J].

Carrillo, J. G. ;

Cantwell, W. J. .

MECHANICS OF MATERIALS, 2009, 41 (07) :828-838

[10] Low velocity impact response of fibre-metal laminates - A review [J].

Chai, Gin Boay ;

Manikandan, Periyasamy .

COMPOSITE STRUCTURES, 2014, 107 :363-381

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