Fracture surface analysis on nano-SiO2/epoxy composite

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Abstract

Fracture surface morphologies of nano-SiO2/epoxy composite with different weight percentage of SiO2 are investigated using scanning electron microscopy. Two types of curing agent, dimethylbenzanthracene (DMBA) and methyltetrahydrophthalic anhydride (MeTHPA), are individually used for preparing the composites. It is found that the fracture surface morphology of the composite cured by DMBA shows as radial striations, which suggests a rapid brittle fracture mode, while the fracture surface morphology of the composite cured by MeTHPA shows as regularly spaced ‘rib’ markings, which indicates a stick–slip motion during the fracture process. Furthermore, the uniaxial tensile behavior under constant loading rate and ambient temperature are investigated. It is shown that the elastic modulus of the composite cured by DMBA firstly increases, and then decreases with the mass fraction of nano-SiO2 particles, but the elongation of the composite cured by MeTHPA is reversed with increasing fraction of nano-SiO2 particles. For nano-SiO2/epoxy composite cured with MeTHPA that possesses a suitable fraction of nano-SiO2, an excellent synthetic mechanical property on elastic modulus and elongation is obtained.

Introduction

Due to their increasing engineering applications, epoxy resin and epoxy based composites have been extensively studied in recent years [1], [2], [3], [4], [5]. The fracture surface morphology analysis is of an important aspect for study on fracture patterns and their corresponding fracture mechanism. There are different fracture surface morphologies corresponding to different deformation and fracture mechanism. For the poly(methyl methacrylate) (PMMA) enduring loads, the craze fracture at crack tip commonly occurs at the middle of craze fibril under a slow crack propagation velocity, the crack propagates along the midrib of craze fibril, consequently, the fracture surface shows as a smooth mirror [6], and a little amount of energy is needed to produce new crack surfaces. In the loading process, the crack propagation velocity increases, and a series of regularly spaced ‘rib’ markings that are perpendicular to the direction of fracture propagation emerge on the fracture surface [7], [8]. The transition between the fracture surface morphology of smooth mirror and that of ‘rib’ marking occurs abruptly [9]. The characteristic morphology showing as conic-shaped patterns is investigated on the fracture surfaces of polymers with low crack propagation velocity [8], [10], [11], [12], while some irregular ‘mackerel’ or ‘patch’ are observed on the fracture surfaces of polymers under high crack propagation velocities [9]. In this paper, the tensile fracture surfaces of nano-SiO2/epoxy composite with different SiO2 contents are observed using scanning electron microscopy (SEM). Two different curing agents, dimethylbenzanthrancene (DMBA) and methyltetrahydrophthalic anhydride (MeTHPA), are individually used in the preparation of the composites. The uniaxial tensile behavior under constant loading rate and ambient temperature are investigated to bring more powerful understanding of the effects of curing agent and weight percentage of nano-SiO2 particles on the fracture surface patterns and some mechanical properties of the composites.

Section snippets

Fracture surface analysis

The epoxy resin used in this research is CYD-128 produced by Yueyang Chemical Industry. The nano-SiO2 particles with different mass fractions are selected to blend with epoxy resin to prepare nano-SiO2/epoxy composites. The composites are cured by either DMBA or MeTHPA.

Fig. 1 shows SEM images of the fracture surface of net epoxy resin cured by DMBA. The specimen breaks in a brittle manner. Radial striations are observed on the fracture surface, the intersection of the striations indicates the

Uniaxial tensile test

The tensile rupture tests were carried out on a CSS-44020 Universal Electronic Test Machine with capacity of 20 kN at room temperature and a crosshead speed of 2 mm/min. Fig. 4 shows the stress–stretch relations of the two nano-SiO2/epoxy composites cured by different curing agents. It is shown that regardless of the mass fraction of SiO2 and the used curing agent, the elastic moduli of the nano-SiO2/epoxy composites are greater than those of the net epoxy resins. However, the modulus does not

Conclusions

  • (i)

    The fracture pattern of nano-SiO2/epoxy composite cured with DMBA reveals a rapid brittle fracture, the fracture surface shows as radial striations; while nano-SiO2/epoxy composite cured with MeTHPA fractures in a stick–slip manner, and the fracture surface morphology appears as regularly spaced ‘rib’ markings.

  • (ii)

    Regardless of the weight fraction of SiO2 and the used curing agent, the elastic moduli of the nano-SiO2/epoxy composites are greater than those of the net epoxy resins, but the

Acknowledgements

This work was supported by the Hunan Provincial Natural Science Foundation of China (no. 05JJ30014), the Scientific Research Fund of Hunan Province Education Department of China (no. 05C100) and the Doctoral Scientific Research Fund of Xiangtan University (no. 04QDZ29).

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