Mechanical Behavior of Nanostructured MaterialsView this Special Issue
Research Article | Open Access
Yu Liu, Cheng-Bing Qu, Qing-Ping Feng, Hong-Mei Xiao, Shao-Yun Fu, "Enhancement in Mode II Interlaminar Fracture Toughness at Cryogenic Temperature of Glass Fiber/Epoxy Composites through Matrix Modification by Carbon Nanotubes and n-Butyl Glycidyl Ether", Journal of Nanomaterials, vol. 2015, Article ID 812061, 6 pages, 2015. https://doi.org/10.1155/2015/812061
Enhancement in Mode II Interlaminar Fracture Toughness at Cryogenic Temperature of Glass Fiber/Epoxy Composites through Matrix Modification by Carbon Nanotubes and n-Butyl Glycidyl Ether
A typical diglycidyl ether of bisphenol-F (DGEBF)/diethyl toluene diamine (DETD) epoxy system modified by multiwalled carbon nanotubes (MWCNTs) and a reactive aliphatic diluent named n-butyl glycidyl ether (BGE) was used as the matrix for glass fiber composites. The glass fiber (GF) reinforced composites based on the unmodified and modified epoxy matrices were prepared by the hand lay-up hot-press process. Mode II interlaminar fracture toughness at both room temperature (RT) and cryogenic temperature (77 K) of the GF reinforced epoxy composites was investigated to examine the effect of the matrix modification. The result showed that the introduction of MWCNTs and BGE at their previously reported optimal contents led to the remarkable enhancement in mode II interlaminar fracture toughness of the composites. Namely, the 22.9% enhancement at RT and the 31.4% enhancement at 77 K were observed for mode II interlaminar fracture toughness of the fiber composite based on the optimally modified epoxy matrix by MWCNTs and BGE compared to the unmodified case.
It is well known that matrices play a very important role in load transfer and crack resistance and hence significantly affect the mechanical properties of fiber reinforced composites. Epoxy resins are most popular matrices for fiber reinforced composites. Due to their shortages such as high brittleness, they are often modified by toughening agents. In our previous work , a reactive aliphatic diluent, namely, n-butyl glycidyl ether (BGE), was displayed to be a proper toughening agent for modifying epoxy resins. On the other hand, carbon nanotubes (CNTs) have exhibited excellent mechanical properties and also demonstrated a great potential as toughening agents for modifying epoxy resins [2–6].
Delamination of the composite laminates would take place when shear and peeling stress concentrations were high. And the fracture toughness under shear loading (i.e., mode II interlaminar fracture toughness) is a critical property to evaluate the potential crack growth resistance . Therefore, mode II interlaminar fracture toughness () is an important parameter for design of composites in practical applications. Shindo et al.  investigated of glass fiber reinforced epoxy composites at cryogenic temperature. However, there is no report yet about mode II interlaminar fracture of fiber reinforced composites based on modified epoxy resins especially by both stiff modifier like CNTs and soft modifier such as BGE.
In our previous work , it has been demonstrated that the 0.5 wt% content of multiwalled CNTs was the optimal amount for modifying the epoxy resins since a higher CNT content would lead to CNT aggregates and thus deteriorated the epoxy performance. On the other hand, reactive BGE has also been displayed to have an effective role in modifying epoxy resins at the optimal content of 10 wt% . At these optimal contents, the glass fiber reinforced composites based on modified epoxy resins have shown great enhancements in tensile properties  and interlaminar shear strength at RT .
In this work, the diglycidyl ether of bisphenol F (DGEBF)/diethyl toluene diamine (DETD) epoxy system modified by multiwalled CNTs and BGE was prepared according to our previous works [1, 8–10] as the matrix. The glass fiber reinforced composites based on the unmodified and modified matrices were fabricated by the hand lay-up hot press process. Mode II interlaminar fracture toughness () at RT and 77 K of the glass fiber reinforced composites based on the unmodified and modified epoxy resins was investigated to examine the effect of matrix modification by multiwalled carbon nanotubes (MWCNTs) and BGE. The significant enhancement in mode II interlaminar fracture toughness at both RT and 77 K of the glass fiber reinforced composite was observed by the modification of the epoxy at the optimal contents of MWCNTs and BGE.
Woven E-glass fibers (GF) were purchased from Feihangtongda Co., Ltd., China. The average diameter of single GF was about 11 μm. The epoxy resin used in this work was diglycidyl ether of bisphenol-F (DGEBF, D.E.R.354, Dow Chemical Co., USA) with the epoxide weight equivalence in the range of 167–174. The curing agent was diethyl toluene diamine (DETD, Kunshan Chemical Material Co., Ltd., China), which is a mixture of the two DETD isomers (74–80 wt.% 2,4-isomer and 18–24 wt.% 2,6-isomer). n-Butyl glycidyl ether (BGE, Changshu Jiafa Chemistry Co., Ltd., China) was used as a soft modifier for epoxy resin. Multiwalled carbon nanotubes (MWCNTs) made by CVD (purity >95 wt.%, Chengdu Organic Chemicals Co., Ltd., China) were employed as a stiff modifier for epoxy resins. The diameters of the nanotubes were in the range of 30–50 nm and the length was between 10 and 20 μm . The chemical structures of DGEBF, DETD, and BGE have been given in our previous work .
2.2. Preparation of Composites
The preparation of the glass fiber reinforced epoxy composite has been given in detail in our previous works  and is briefly described here. First, the modified epoxy matrix was prepared by mixing epoxy resins and other additives at 50°C. The pure epoxy system was also employed as the matrix for the purpose of comparison. Formulations of unmodified and modified epoxy resins as matrices are shown in Table 1. Second, glass fiber clothes were impregnated with these epoxy resins. Twenty impregnated prepregs were stacked via the hand lay-up method and glass fiber reinforced composites based on the unmodified and modified matrices were fabricated by the hot-press process via the curing press machine (QLB 40T) under 5 MPa. Temperature and pressure profiles for manufacturing composites are shown in Figure 1. In order to induce the initial cracks between the middle layers, thin release films were partially placed during fabrication. Finally, the composites were cured at 130°C for 10 h. The resulting glass fiber reinforced composites have a fiber volume content of about 56% . The specimens for the mechanical tests were cut from the composite plates. The dimensions of the samples for measurement of are shown Figure 2.
In the end notched flexure (ENF) test, the critical energy release rate is determined by :where and are the initial crack length and the crack length at the critical load, respectively. indicates the compliance within initial elastic deformation without crack growth and indicates the compliance at the critical load. is the critical load which can be determined by the maximum load or 5% offset load according to the load-displacement curve. and 2L represent the width and the span length of the specimen, respectively. All the tests were performed using an Instron 5882 universal machine with 5 kN load cell. The crosshead rate was 2 mm/min at both RT and 77 K. The cryogenic temperature condition was achieved by immersing the specimens completely in a liquid nitrogen filled cryostat to ensure the uniform temperature of 77 K . At least five specimens were tested for each composition.
The fracture surfaces of the composites were evaluated by scanning electron microscopy (SEM, Hitachi S-4300) at an accelerating voltage of 10 kV. All specimens were coated with a thin layer of gold to eliminate charging effects.
3. Results and Discussion
3.1. Mode II Interlaminate Fracture Toughness
Typical ENF load-displacement curves at room temperature (RT) and liquid nitrogen temperature (77 K) for the composites are shown in Figures 3 and 4, respectively. At RT, the applied load shows nonlinearity at a relatively low load about 300 N. After attaining the maximum value, the load decreases gradually to the failure. In contrast, at 77 K, the applied load shows a linear relationship with the displacement and unstable crack growth occurs when the maximum value is reached. Moreover, the maximum load at 77 K is much higher than that at RT. In addition, it should be noted that the maximum load for the composite based on the modified epoxy matrix is higher than that based on the pure epoxy matrix at both RT and 77 K.
The results for the interlaminate fracture toughness at RT and 77 K are shown in Figures 5 and 6, respectively. It can be easily noticed that of the composites based on the modified matrix is higher than that of the composite based on the unmodified epoxy matrix at both RT and 77 K. Moreover, at 77 K is much higher than that at RT for the same composite. When the temperature decreased from RT to 77 K, the chemical bond of the epoxy matrix would shrink and the binding forces between matrix and fiber could become stronger . The higher mechanical performance at 77 K compared to RT might be attributed to the stronger binding forces at 77 K compared to RT.
The data for the interlaminar fracture toughness at RT and 77 K for the composites based on unmodified and modified epoxy matrices are given in Table 1. At RT, of Samples B and C are 4.3% and 13.6% higher compared to Sample A, respectively. In particular, the incorporation of both MWCNTs and BGE (Sample D) results in 22.9% improvement in compared to Sample A. On the other hand, at 77 K, of Samples B and C are improved by 11.7% and 22.8% compared to Sample A, respectively. Moreover, the value of Sample D is enhanced by 31.4% compared to Sample A. Consequently, it can be seen that the simultaneous incorporation of MWCNTs and BGE into the epoxy resin leads to the maximum enhancements in . In addition, the enhancement in at 77 K was higher than that at RT, this was likely because the chemical bond and molecules of the epoxy matrix would shrink and the binding forces between molecules would become stronger when the temperature decreased from RT to 77 K .
3.2. Microstructure of the Composites
The SEM images are presented in Figure 7 for the fracture surfaces of the ENF specimens. It is revealed that at RT, GF of the composite samples with modified matrices have a rougher surface than those of Sample A. The fracture surface observation coincides with the results for of samples. This indicates that the incorporation of MWCNTs and BGE into the conventional GFRP composites based on the pure epoxy matrix creates an increased fracture surface due to crack deflection , which will lead to the enhancement in the interlaminar fracture toughness. Sample D with the simultaneous introduction of MWCNTs and BGE into the epoxy resin shows the noticeable effect on the improvement of interlaminar fracture toughness.
At 77 K, the decrease in temperature makes the epoxy more brittle and reduces its strain to failure. The hackle mark features are shown in Figure 7. These hackle patterns are likely caused by secondary cracks . The hackle patterns are more obvious at 77 K than at RT. The increased fracture surface of the hackle pattern morphology means more surface energy dissipation and therefore an increase of the interlaminar fracture toughness compared to the RT case. The hackle pattern formation also helps to reduce the stress (or strain) concentration at the tip of the principal crack . Therefore, it is reasonable to observe that the simultaneous introduction of MWCNTs and BGE into the epoxy matrix has brought about the significant enhancement in mode II interlaminar fracture toughness.
In this work, glass fiber reinforced composites have been prepared by the hand lay-up hot press process based on unmodified and modified epoxy matrices by introducing MWCNTs and BGE into a pure epoxy resin in modifying the epoxy resins. Mode II interlaminar fracture toughness () of the glass fiber reinforced composites has been investigated at both room temperature (RT) and cryogenic temperature (77 K) to examine the effect of the matrix modification. It has been clearly demonstrated that the epoxy modification by both MWCNTs and BGE can lead to great enhancements in at both RT and 77 K.
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
This work was financially supported by the National Natural Science Foundation of China (nos. 51373187 and 11372312) and the Beijing Municipal Natural Science Foundation (no. 2122055).
- Z. K. Chen, G. Yang, J. P. Yang, S. Y. Fu, L. Ye, and Y. G. Huang, “Simultaneously increasing cryogenic strength, ductility and impact resistance of epoxy resins modified by n-butyl glycidyl ether,” Polymer, vol. 50, no. 5, pp. 1316–1323, 2009.
- S. Wang, Z. Liang, T. Liu, B. Wang, and C. Zhang, “Effective amino-functionalization of carbon nanotubes for reinforcing epoxy polymer composites,” Nanotechnology, vol. 17, no. 6, pp. 1551–1557, 2006.
- P. Guo, X. Chen, X. Gao, H. Song, and H. Shen, “Fabrication and mechanical properties of well-dispersed multiwalled carbon nanotubes/epoxy composites,” Composites Science and Technology, vol. 67, no. 15-16, pp. 3331–3337, 2007.
- L. Guadagno, L. Vertuccio, A. Sorrentino et al., “Mechanical and barrier properties of epoxy resin filled with multi-walled carbon nanotubes,” Carbon, vol. 47, no. 10, pp. 2419–2430, 2009.
- Q. F. Cheng, J. P. Wang, J. J. Wen et al., “Carbon nanotube/epoxy composites fabricated by resin transfer molding,” Carbon, vol. 48, no. 1, pp. 260–266, 2010.
- Y. Breton, G. Désarmot, J. P. Salvetat et al., “Mechanical properties of multiwall carbon nanotubes/epoxy composites: influence of network morphology,” Carbon, vol. 42, no. 5-6, pp. 1027–1030, 2004.
- Y. Shindo, F. Narita, and T. Sato, “Analysis of mode II interlaminar fracture and damage behavior in end notched flexure testing of GFRP woven laminates at cryogenic temperatures,” Acta Mechanica, vol. 187, pp. 231–240, 2006.
- Z.-K. Chen, J.-P. Yang, Q.-Q. Ni, S.-Y. Fu, and Y.-G. Huang, “Reinforcement of epoxy resins with multi-walled carbon nanotubes for enhancing cryogenic mechanical properties,” Polymer, vol. 50, no. 19, pp. 4753–4759, 2009.
- Y. Liu, H. M. Xiao, Q. P. Feng, and S. Y. Fu, “Synergistic effect of carbon nanotubes and n-butyl glycidyl ether on matrix modification for improvement of tensile performance of glass fiber/epoxy composites,” Composites A, vol. 62, pp. 39–44, 2014.
- Y. Liu, J.-P. Yang, H.-M. Xiao et al., “Role of matrix modification on interlaminar shear strength of glass fibre/epoxy composites,” Composites B: Engineering, vol. 43, no. 1, pp. 95–98, 2012.
- W.-X. Wang, M. Nakata, Y. Takao, and T. Matsubara, “Experimental investigation on test methods for mode II interlaminar fracture testing of carbon fiber reinforced composites,” Composites A: Applied Science and Manufacturing, vol. 40, no. 9, pp. 1447–1455, 2009.
- J. P. Yang, G. Yang, G. Xu, and S. Y. Fu, “Cryogenic mechanical behaviors of MMT/epoxy nanocomposites,” Composites Science and Technology, vol. 67, no. 14, pp. 2934–2940, 2007.
- T. Yokozeki, Y. Iwahori, M. Ishibashi et al., “Fracture toughness improvement of CFRP laminates by dispersion of cup-stacked carbon nanotubes,” Composites Science and Technology, vol. 69, no. 14, pp. 2268–2273, 2009.
- H. Lau and R. E. Rowlands, “Fracture morphology of composites tested at RT and 77K,” Advances in Cryogenic Engineering, vol. 36, pp. 913–919, 1990.
- Y. Shindo, D. Shinohe, S. Kumagai, and K. Horiguchi, “Analysis and testing of mixed-mode interlaminar fracture behavior of glass-cloth/epoxy laminates at cryogenic temperatures,” Journal of Engineering Materials and Technology, Transactions of the ASME, vol. 127, no. 4, pp. 468–475, 2005.
Copyright © 2015 Yu Liu et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.