Super toughened immiscible polycarbonate/poly(L-lactide) blend achieved by simultaneous addition of compatibilizer and carbon nanotubes

Yong-hong Wang, Xian-ling Xu, Jian Dai, Jing-hui Yang, Ting Huang, Nan Zhang, Yong Wang*, Zuo-wan Zhou and Ji-hong Zhang
Key Laboratory of Advanced Technologies of Materials (Ministry of Education), School of Materials Science & Engineering, Southwest Jiaotong University, Chengdu, 610031, China. E-mail: yongwang1976@163.com; Tel: +86 28 87603042

Received 26th September 2014 , Accepted 22nd October 2014

First published on 24th October 2014


Abstract

Polycarbonate/poly(L-lactide) (PC/PLLA) blend exhibits great potential application in several fields, including package, toy, electronic element and automobile. However, the poor mechanical properties of the immiscible PC/PLLA blend restrict its application. In this work, a compatibilizer maleic anhydride grafted ethylene–octene copolymer (EOR-g-MAH) and functionalized carbon nanotubes (F-CNTs) were introduced into the immiscible PC/PLLA blend by simple melt-compounding processing. Mechanical property measurements showed that even at low environmental temperature (0 °C), the blend composites exhibited excellent fracture toughness, e.g. 40.9 ± 2.1 kJ m−2 at F-CNT content of 2 wt%. To better understand the toughening mechanism, the morphologies of the blend composites and the dispersion of F-CNTs and the rheological properties were systematically investigated. The results showed that with the combined effects of EOR-g-MAH and F-CNTs, the decreased PLLA particles were achieved. Most of F-CNTs selectively located in the PC matrix and some F-CNTs entered into PLLA particles. Specifically, at relatively high content (>2 wt%), F-CNTs formed percolated network structure. Then, the toughening mechanism was proposed on the basis of the morphology evolution, the formation of F-CNT network structure and the impact-fractured surface morphologies. This work demonstrated that even for the immiscible polymer blend, the super toughened blend composites could be achieved by the combined effects of compatibilizer and carbon nanotubes, and therefore it provides an alternative strategy for largely improving the fracture toughness of immiscible polymer blends.


1. Introduction

Polymer blending has proved to be one of the most efficient ways to prepare new high-performance materials. To date, only few dozens of blends are completely miscible at the molecular level, most blends are immiscible. The mechanical properties of immiscible blends are determined by many factors, including morphology, crystalline structure and interfacial interaction between components. Specifically, the appropriate interfacial interaction not only favors the dispersion of dispersed component but also favors the stress transfer between components under the load condition, which weakens the stress concentration phenomenon at the interface leading to the failure of the material. It is well known to all, that compatibilizer, which can be introduced as the third component or can be formed by in situ chemical reaction between components plays the role of reducing interfacial tension and improving interfacial interaction.1,2

Polycarbonate (PC) is a typical engineering plastic, which exhibits good processing ability and excellent physical properties, including high tensile ductility, strength, heat deformation temperature (HDT) and electrical insulation. To date, PC-based articles have been widely used in the fields of package, toy, electronic element and automobile. However, PC belongs to those engineering plastics, which exhibit high degree of dependence on petroleum resources. Therefore, developing a new material from renewable sources to replace or partially replace PC satisfies the requirement of sustainable development, and it has been a goal of high technological and environmental priority.

Poly(L-lactide) (PLLA) is a biocompatible and biodegradable polymer, which can be obtained from completely renewable sources such as core, wheat and rice; hence, it reduces the degree of dependence on petroleum sources. PLLA exhibits excellent tensile modulus and strength, and it has been an alternative for replacing traditional petroleum-based engineering plastic. Therefore, introducing PLLA into other engineering plastic to develop new material attracted considerable attention of researchers. Different blends, such as PLLA/polyamide (PA),3–5 PLLA/poly(ethylene terephthalate) (PET)6 and PLLA/poly(butylene terephthalate) (PBT),7 have been developed in the last ten years.

Blending PC and PLLA to develop a new material is very significant, because the addition of PLLA reduces the amount of PC in articles, which can weaken the dependence on the petroleum product. However, PC/PLLA blend is immiscible, and the blends usually exhibit deteriorated mechanical properties compared with pure PC and/or PLLA due to the poor interfacial interaction between PC and PLLA.8–11 A considerable amount of effort has been taken to improve the mechanical properties of the blends. For example, Lee, J. B. et al.12 introduced different compatibilizers into PC/PLLA blends and determined that the mechanical, morphological, rheological and degradation properties were greatly dependent upon the type of the compatibilizer. Kanzawa, T. et al.13 investigated the mechanical and morphological changes of the ternary PLLA/PC/poly(butylene adipate-co-terephthalate) blends through reactive processing. The results showed that the tensile strain and impact strength of the ternary blends were considerably enhanced. Phuong, V. T. et al.14 introduced tetrabutylammonium tetraphenylborate (TBATPB) and triacetin into PC/PLLA blends through extrusion processing. The results showed that PC/PLLA copolymer was formed during the short extrusion time, and then the compatibility between PC and PLLA was improved.

However, from the results reported in the literatures one can see that for the traditionally compatibilized PC/PLLA blends, the degree of improvement of mechanical property is still very small, especially for the fracture resistance, which usually determines the application of PC/PLLA articles under the impact load condition. Therefore, considerable work needs to be performed to seek other strategies to further improve the fracture resistance of PC/PLLA blends. Recently, introducing functionalized carbon nanotubes (F-CNTs) into an immiscible polymer blends has been proved as an efficient method to largely improve the fracture resistance of the blend.15–19 The toughening efficiency is dependent on the selective location of F-CNTs in the blend composites. If F-CNTs were selectively located at the interface, the toughening mechanism is related to the bridge effect of F-CNTs at the blend interface, which prevents the propagation of crack along the interface. As a consequence, largely enhanced tensile ductility can be achieved.15–17 If F-CNTs were selectively located in one component of the blend, the toughening mechanism is proposed to be related to the formation of F-CNT network structure, which facilitates the stress transfer between components under the load condition.18,19 In our previous work, F-CNTs were introduced into PC/PLLA (60/40, wt/wt) blend, which exhibited cocontinuous morphology.20 The results showed that the selective location of F-CNTs in PC component increased the phase size of PC component but decreased the phase size of PLLA component. Mechanical properties measurements showed that elongation at break and notched Izod impact strength were enhanced by adding a small amount of F-CNTs (0.5 wt%).

To further develop PC/PLLA material with high-performance, in the present work, we attempted to simultaneously introduce compatibilizer, i.e. maleic anhydride grafted ethylene–octene copolymer (EOR-g-MAH), and F-CNTs into PC/PLLA blend. Interestingly, the new PC/PLLA/EOR-g-MAH/F-CNT material exhibited considerably higher impact strength but without an apparent deterioration of modulus and tensile strength as compared with the binary PC/PLLA blend. Even at low environmental temperature (0 °C), the material also exhibited excellent impact strength. Namely, super toughened PC/PLLA blend composites were successfully achieved.

2. Experimental

2.1. Materials

PC (S-2001R, with a viscosity-average molecular weight (Mη) of 2.3 × 104 g mol−1, a melt flow rate (MFR) of 7.5–10.5 g/10 min (300 °C/1.2 kg) and a density of 1.2 g cm−3) was purchased from Mitsubishi Engineering-Plastics Corp. PLLA (2002D, with a D-isomer content of 4.3%, a weight-average molecular weight (Mw) of 2.53 × 105 g mol−1, the MFR of 4–8 g/10 min (190 °C/2.16 kg) and the density of 1.24 g cm−3) was purchased from NatureWorks®, USA. Functionalized carbon nanotubes (F-CNTs, containing 1.23 wt% carboxyl group) were obtained from Chengdu Institute of Organic Chemistry, Chinese Academy of Science (Chengdu, China). The outer diameters of F-CNTs were 20–30 nm, and the length of a single F-CNT was about 30 μm. Compatibilizer maleic anhydride grafted ethylene–octene copolymer (EOR-g-MAH) (KT-9, with MFR of 2.5 g/10 min (190 °C/2.16 kg)) was obtained from Shenyang Ketong Plastic Co., Ltd. The grafting ratio of MAH was 0.8 wt%.

2.2. Sample preparation

All the materials were first dried at 70 °C for 10 h. A master batch of PC/F-CNT containing 10 wt% F-CNTs was prepared using a twin-screw extruder SHJ-30 (Nanjing Ruiya, China). Then, the master batch was diluted by melt-blending with PC, EOR-g-MAH and PLLA to prepare the corresponding compositions. In this work, the weight ratio between PC and PLLA was maintained at 80[thin space (1/6-em)]:[thin space (1/6-em)]20, the content of EOR-g-MAH was maintained at 5 wt%, and the content of F-CNTs was varied from 0.5 to 5 wt%. The sample notation was defined as C8A2E5Fx, where x represents the content of F-CNTs. For example, C8A2E5F2 indicates that the content of F-CNTs was 2 wt%. The melt blending was carried out at a screw speed of 100 rpm and melt temperatures of 170–200–220–240–255–255–250 °C from hopper to die. After being granulated, the pellets were injection-molded using an injection-molding machine EM80-V (Chen Hsong Machinery, China) to obtain the standard specimen. The melt temperatures were set at 240–255–255–250 °C from hopper to nozzle, and a mould temperature of 25 °C was used. The injection speed was 6.3 g s−1 and the holding pressure was 35 MPa. For making a comparison, the binary PC/PLLA (80/20, C8A2) and the ternary PC/PLLA/EOR-g-MAH (80/20/5, C8A2E5) were also prepared by the completely same processing method.

2.3. Mechanical property measurement

Tensile properties were measured using a universal tensile machine AGS-J (SHIMADZU, China) according to ASTM D638. The dumbbell-shaped specimen had a width of 10 mm and a thickness of 4.2 mm. During the measurement, the gauge distance was set at 50 mm and a cross-head speed of 50 mm min−1 was used. For the notched Izod impact strength, it was measured using a rectangular sample with the width and thickness of 10 and 4.2 mm, respectively. The impact measurement was carried out at two different environmental temperatures, i.e. 23 and 0 °C. The measurement was conducted on a XC-22Z impact tester (Chengde, China) according to ASTM D 256-04. The notch depth was 2.0 mm and the residual width of the specimen was about 8.0 mm. For each sample, the average value of mechanical properties reported was derived from the data of more than 5 specimens.

2.4. Scanning electron microscopy (SEM)

SEM was used to characterize sample morphology. Whether for the cryogenically fractured surface, which was obtained in the liquid nitrogen or for the impact-fractured surface, which was obtained during the impact measurement, the fractured surface was coated with a thin layer of gold before SEM characterization. To further clarify the dispersion of EOR-g-MAH, the cryogenically fractured surface of the C8A2E5 sample was further treated using n-heptane at 50 °C for 4 h to remove EOR-g-MAH component. Then, the treated surface was carefully washed and coated before SEM characterization. The characterization was conducted on a FEI Inspect (FEI, the Netherlands), and an accelerating voltage of 5.0 kV was used.

2.5. Transmission electron microscopy (TEM)

TEM was further used to characterize the morphology, composition and the dispersion of F-CNTs in material. The characterization was conducted on a Tecnai G2 F20 (FEI, USA), and an operating voltage of 200 kV was used. An ultrathin section with a thickness of about 90 nm, which was cut using a cryo-diamond knife on a microtome EM UC6/F6 (LEICA, Germany), was used. Before TEM characterization, the samples containing EOR-g-MAH were stained with OsO4.

2.6. Rheological measurement

The rheological measurement was conducted on a stress-controlled rheometer AR 2000ex (TA Instruments, USA). The sample disk was first prepared by a compression-molding method, which was carried out at a melt temperature of 250 °C and pressure of 5 MPa. The sample had a thickness of 1.0 mm and a diameter of 20 mm. During the rheological measurement process, the frequency sweep from 0.01 to 100 Hz was performed at 250 °C under dry nitrogen atmosphere. For all the measurements, the samples were tested within the linear viscoelastic strain range, which could be estimated by an initial survey through a dynamic strain sweep experiment at strains ranging from 0.01% to 100%.

3. Results and discussion

3.1. Mechanical properties

Fig. 1 shows the typical engineering stress–strain curves of the PC/PLLA/EOR-g-MAH/F-CNT specimens and the corresponding tensile properties. For comparison, the results of the binary PC/PLLA and the ternary PC/PLLA/EOR-g-MAH specimens are also shown. It is worth noting that PC is a ductile polymer with apparent yielding and cold-drawing behaviors, whereas PLLA is a brittle polymer without yielding during the universal tensile process. From Fig. 1 one can see that the binary PC/PLLA (80/20) specimen exhibits the elongation at a break of 102.2 ± 1.9%. It has already been proved that the addition of a small amount of PLLA can slightly enhance the tensile ductility of PC, which can be attributed to the toughening effect of rigid PLLA particles on ductile PC matrix.9,14 In our previous work, 30 wt% PLLA was introduced into PC and the elongation at break was increased from 83.8% of pure PC to 119.6% of the PC/PLLA (70/30) specimen.9 Similar results were also reported by Phuong, V. T. et al.14 In their work, the PC/PLLA (70/30) specimen exhibited elongation at break of about 125 ± 3.3%, considerably higher compared to pure PC (84.4 ± 4.3%). In the present work, although the composition was different, the binary PC/PLLA specimen still exhibited the enhanced tensile ductility as compared with pure PC, which further proved the weak toughening effect of PLLA on PC. For the ternary PC/PLLA/EOR-g-MAH specimen, the elongation at break was increased up to 132.4 ± 0.7%. This proved that EOR-g-MAH is a compatibilizer of immiscible PC/PLLA blend, and it plays a role of improving the tensile ductility of the material.12 Although the presence of EOR-g-MAH induced the deterioration of tensile modulus, the addition of F-CNTs apparently enhanced the tensile modulus of specimen. Specifically, the tensile modulus of specimen gradually increased with increasing F-CNT content. However, from Fig. 1 one can also see that the addition of high content of F-CNT induces the dramatic deterioration of tensile ductility of specimen. For example, the elongation at break dramatically decreased from 132.4 ± 0.7% of the C8A2E5 specimen to 28.8 ± 3.9% of the C8A2E5F5 specimen. There are at least two possibilities, which take charge of the deterioration of the tensile ductility. One possibility is related to the formation of large F-CNT agglomerates, which act as the stress concentrator, which results in the failure of the sample during the tensile process. The other possibility is related to the formation of a dense F-CNT network structure in the material, which prevents the plastic flow of PC macromolecules along the tensile direction. The formation of F-CNT network structure will be proved in the next section by rheological measurement.
image file: c4ra11282b-f1.tif
Fig. 1 (a) Typical engineering stress–strain curves of specimens and (b) the corresponding tensile properties.

The impact strength of the sample was first measured at room temperature (23 °C). The C8A2 specimen exhibited impact strength of 12.9 ± 0.6 kJ m−2. Although the value was higher compared to pure PLLA (3.1 ± 0.1 kJ m−2), it was considerably smaller compared to pure PC sample (66.9 ± 2.7 kJ m−2). This proves the poor interfacial interaction between the components in the binary blend. The addition of a small amount of EOR-g-MAH, the impact strength of the ternary blend specimen was greatly enhanced to 73.5 ± 5.7 kJ m−2, which was nearly 6 times higher compared to the binary blend specimen. Further enhanced fracture resistance was achieved for the C8A2E5F0.5 specimen and the impact strength was increased up to 87.1 ± 3.0 kJ m−2. Furthermore, it is interesting to observe that the specimen did not completely fracture during the impact measurement. As shown in Fig. 2, nearly half of the specimen did not fracture. The similar phenomenon was also observed for other samples containing high content of F-CNTs. It is well known to all, that during the Charpy test, the breaking of the specimen is essential; otherwise the results of the Charpy test are meaningless. Therefore, to clearly understand the variation of the fracture resistance of specimen, the impact measurement was further carried out at low environmental temperature, i.e. 0 °C. In this condition, nearly all the specimens were completely fractured during the impact measurement.


image file: c4ra11282b-f2.tif
Fig. 2 (a) Optical image of impact-fractured C8A2E5F2 sample and (b) the corresponding SEM image of impact-fractured surface morphology obtained at low magnification.

As shown in Fig. 3, the C8A2 and C8A2E5 specimens exhibited the impact strength of 7.3 ± 0.6 and 27.5 ± 1.5 kJ m−2, respectively. However, it is worth noting that the toughening efficiency of EOR-g-MAH at low environmental temperature slightly decreased compared with that measured at room temperature. Here, the impact strength of the C8A2E5 was only about 4 times higher compared to the C8A2 specimen. Surprisingly, the impact strength of the PC/PLLA/EOR-g-MAH/F-CNT specimen gradually increased when increasing the content of F-CNTs until very high content of F-CNTs were present in the material. For example, the C8A2E5F0.5 specimen exhibited the impact strength of 31.6 ± 1.1 kJ m−2. For the C8A2E5F1 and C8A2E5F2 specimens, the impact strength increased up to 35.8 ± 0.9 and 40.9 ± 2.1 kJ m−2, respectively. Specifically, it is still observed that the C8A2E5F2 specimen was not completely fractured. In a word, with simultaneous addition of compatibilizer and carbon nanotubes, super toughened PC/PLLA blend composites were successfully achieved.


image file: c4ra11282b-f3.tif
Fig. 3 Notch Izod impact strength of samples as indicated in the graph. The measurement was carried out at low environmental temperature (0 °C).

Analyzing the impact-fractured surface morphology facilitates to further understand the fracture behavior of the specimen. Here, the fractured surfaces of representative specimens, which were obtained at 0 °C, were characterized using SEM. Fig. 4 shows the surface morphologies characterized at a relatively small magnification. It can be seen that although the specimen is not completely fractured, the impact-fractured surface in the fractured part of the C8A2 specimen was very smooth, which indicates that the fracture process occurred at relatively high speed. Obviously, the C8A2 specimen exhibited the typical brittle fracture mode. This agrees well with its low impact strength (7.3 ± 0.6 kJ m−2) as shown in Fig. 3. Different from the smooth surface of the C8A2 specimen, the C8A2E5 specimen exhibited coarse surface, indicating that the fracture resistance of the specimen was enhanced. Adding F-CNTs into the material further enhanced the roughness of the fractured surface. Specifically, one can see that a part of the sample was pulled out from the fractured surface. Such phenomenon became more apparent at relatively high F-CNT content. For the C8A2E5F2 specimen, even at low magnification, one can also see that the intense plastic deformation of specimen.


image file: c4ra11282b-f4.tif
Fig. 4 SEM images showing the impact-fractured surface morphologies of representative samples obtained at low magnification. (a) C8A2, (b) C8A2E5, (c) C8A2E5F0.5 and (d) C8A2E5F2.

More differences in surface morphologies of different specimens can be clearly seen from the SEM images obtained at high magnifications. Generally speaking, the fracture of a specimen during the impact process experiences two stages: crack initiation and crack propagation. Correspondingly, the fractured surface can be divided into crack initiation zone (Zone A as shown in Fig. 4a) and crack propagation zone (Zone B and C as shown in Fig. 4a, representing the early stage and later stage of crack propagation, respectively). Therefore, the surface morphologies in different zones were carefully characterized at high magnification. As shown in Fig. 5, for the C8A2 specimen (Fig. 5a), in all zones (Zones A–C), one can see that some PLLA particles were debonded from PC matrix, proving the weak interfacial interaction between PC and PLLA. For the C8A2E5 specimen (Fig. 5b), even in the crack initiation zone (Zone A), one can observe the plastic deformation of specimen. The plastic deformation became more apparent in the specimens containing F-CNTs (Fig. 5c and d). Specifically, in addition to the plastic deformation of PC matrix, the fibrillated PLLA component was also observed in the crack initiation zone of the C8A2E5F2 specimen (Zone A). In the later stage of crack propagation process (Zone C), it was difficult to differentiate PLLA component from PC matrix, and the specimen exhibited very intense plastic deformation. This indicates that the plastic deformation of PC matrix was companioned with the simultaneous plastic deformation of PLLA component. It is well known to all that PLLA is a typical brittle material and pure PLLA usually exhibits the brittle fracture mode without any plastic deformation. Generally speaking, the fibrillation of a material is greatly related to the intense plastic deformation occurred under the load condition.21 This indicates that in the present work, the plastic deformation of PLLA component was also activated with the combined effects of EOR-g-MAH and F-CNTs. The fibrillar PLLA observed during the impact measurement has also been reported elsewhere and it is believed that one of the main reasons for the largely enhanced fracture resistance.20,22 However, it is still not clear why the brittle PLLA component can be fibrillated or deformed. In the next section, we will explain the mechanism for the fibrillation of PLLA component.


image file: c4ra11282b-f5.tif
Fig. 5 SEM images showing the impact-fractured surface morphologies at different zones as shown in Fig. 4a. The images were taken at high magnification. (a) C8A2, (b) C8A2E5, (c) C8A2E5F0.5 and (d) C8A2E5F2.

3.2. Morphology

The mechanical properties of the blend composites are mainly related to their microstructure and morphology, including the crystalline structure of components, the dispersed particle morphology and the dispersion of fillers. In the present work, PC is an amorphous polymer and no crystallization occurs during the whole melt-processing procedures. PLLA is a typical semicrystalline polymer, however, it is still in the amorphous state through the traditional melt-processing because of which the crystallization ability of PLLA is very small and the relative high cooling rate prevents the crystallization of PLLA. Even with the presence of F-CNTs, which usually exhibit excellent nucleation effect for the crystallization of semicrystalline polymer, the crystallization of PLLA is still very difficult and no crystallization occurs during the whole melt-processing procedures.20 Therefore, the influence of crystalline structure change on the mechanical properties of the PC/PLLA/EOR-g-MAH/F-CNT can be ignored. Thus, the main attention was focused on the morphological change of the blend and the selective location of F-CNTs in the blend composites.

Here, the morphology of the blend composites and the dispersion of F-CNTs were characterized using SEM and TEM. Fig. 6 exhibits the SEM images of the samples. For the binary PC/PLLA blend (Fig. 6a), it exhibits the typical “two-phase structure” feature, proving the weak interfacial interaction between PC and PLLA. With the addition of EOR-g-MAH (Fig. 6b), although the blend still showed the “two-phase structure” feature, one can see that some EOR-g-MAH were located at the interface between PC and PLLA. The dispersion of EOR-g-MAH can be further proved by the image shown in Fig. 6f, in which only EOR-g-MAH was first removed by n-heptane and the black holes represent the EOR-g-MAH component. This indicates that the selectively located EOR-g-MAH can exhibit the bridge effect to strengthen the interaction between PC and PLLA. On the other hand, different from the smooth surface of the C8A2 sample, the cryogenically fractured surface of the C8A2E5 sample became rougher. For the PC/PLLA/EOR-g-MAH/F-CNT blend composites, although the C8A2E5F0.5 sample (Fig. 6c) exhibited similar morphology to that of the C8A2E5 sample, apparently decreased PLLA particles were observed in the sample containing high content of F-CNTs, especially in the C8A2E5F5 sample (Fig. 6e). The decrease of PLLA particle size can be attributed to the increase in the melt viscosity induced by high content of F-CNTs, which prevent the migration of dispersed PLLA particles and the steric hindrance effect of F-CNTs, which prevents the collision and aggregation of adjacent PLLA particles.23–25 The variation of viscosity of the samples can be seen in the following section.


image file: c4ra11282b-f6.tif
Fig. 6 (a–e) SEM images showing the cryogenically fractured surface morphologies of different samples and (f) morphology of the representative C8A2E5 sample when EOR-g-MAH was removed by n-heptane. (a) C8A2, (b) C8A2E5, (c) C8A2E5F0.5, (d) C8A2E5F2 and (e) C8A2E5F5.

Fig. 7 exhibits the TEM images of the representative samples. Because of the inherent electron density difference between PC and PLLA, the “two-phase structure” feature can also be clearly seen: PC component appears dark while PLLA component appears white in the image. Similar phenomenon in appearance has been reported elsewhere.14 EOR-g-MAH can also be differentiated because it can be stained by OsO4. Specifically, from Fig. 7c and d one can see that most of F-CNTs were selectively located in the PC matrix, and some of F-CNTs penetrated PLLA particles or a part of a single F-CNT entered into PLLA particles. Obviously, these F-CNTs can also exhibit the bridge effect to intensify the interaction between PC and PLLA, facilitating the stress transfer in the material and avoiding the stress concentration at the blend interface under the load condition.17 Furthermore, from Fig. 7d one can also see that some F-CNTs contact each other and form a network-like structure in the PC matrix. This also indicates that stress can transfer along the osculatory F-CNTs. In other word, the F-CNT network also avoids the presence of stress concentration in the PC matrix, which facilitates the improvement of the fracture resistance of the sample.


image file: c4ra11282b-f7.tif
Fig. 7 TEM images showing the morphologies of PLLA component and the dispersion of F-CNTs in different samples. (a) C8A2, (b) C8A2E5, (c) C8A2E5F0.5 and (d) C8A2E5F2.

3.3. Rheological properties

The formation of F-CNT network structure in the material can be further proved by rheological measurement, because rheological measurement provides not only a fundamental understanding of the nature of the processability and the structure–property relationship of the composites but also provides information about the dispersion and microstructure of nanofiller in the polymer melt. Fig. 8 exhibits the storage modulus (G′), loss modulus (G′′), Cole–Cole plots of Gversus G′′ and complex viscosity (η*). From Fig. 8a one can see that the presence of EOR-g-MAH induces a slight increase of G′ at low frequencies. Similar phenomena have been widely reported in literatures.26–29 To date, many researches have shown that the interfacial activity and micelle formation significantly influence the rheological behaviors of the compatibilized blends. For example, Entezam, M. et al.30 proved that micelle formation due to extra amounts of compatibilizer in a system with higher interfacial activity resulted in an increase of the elastic modulus. Specifically, they concluded that the solid type rheological behavior was attributed to the interconnectivity between dispersed phase domains through matrix polymer chains trapped by the compatibilizer shell. For the PC/PLLA/EOR-g-MAH/F-CNT blend composites, the presence of a small amount (0.5 wt%) of F-CNTs does not induce the apparent change of G′ at all frequencies. However, increasing the content of F-CNTs further induced a great increase of G′ at low frequencies. Specifically, at F-CNT content of 2 and 5 wt%, the storage modulus curve even presents a platform at low frequencies. This indicates that G′ remained invariant and the melt exhibited apparent solid-like response. However, it has been widely accepted that for the composites filled with nanofillers, the presence of the platform in the storage modulus curve at low frequency is related to the formation of a percolated nanofiller network structure in the melt.31–33 Therefore, from Fig. 8a one can believe that the percolated F-CNT network structure forms in the PC/PLLA/EOR-g-MAH/F-CNT blend composites with high content of F-CNTs. Similar variation trends were also observed for G′′ (Fig. 8b). Although the platform at low frequencies became inconspicuous, the increase of G′′ with increasing content of F-CNTs also proves an enhancement of molecular interactions, namely the molecular mobility becomes more difficult.
image file: c4ra11282b-f8.tif
Fig. 8 Rheological properties of different samples as indicated in the graphs. The inserted graph shows the comparison of viscosity between pure PC and PLLA. (a) Storage modulus, (b) loss modulus, (c) Cole–Cole plots of storage modulus versus loss modulus and (d) complex viscosity.

Fig. 8c shows the Cole–Cole plots of Gversus G′′. It can be seen that the C8A2 sample exhibited an approximate linear relationship between G′ and G′′. The presence of F-CNTs induced the deviation from the linear relationship, especially when a high content of F-CNTs were present in the melt. It has been reported elsewhere that the change in the slope of the Cole–Cole plots indicate a significant change in microstructure of the melt. When the Cole–Cole plots exhibit the deviation from the linear relationship between G′ and G′′, the nanofiller forms the percolated rheological network structure in the melt.34,35 Therefore, Fig. 8c also proves the formation of the percolated F-CNT network structure in the PC/PLLA/EOR-g-MAH/F-CNT blend composites with high content of F-CNTs.

The variation of η* with increasing content of F-CNTs is shown in Fig. 8d. For making a comparison, the viscosity of pure PC and PLLA is also shown in the inserted graph. From the inserted graph one can see that in all frequencies, the melt viscosity of pure PC was considerably higher compared to the pure PLLA and the viscosity ratio between PC and PLLA component was bigger than 10. Furthermore, it can be seen that either for the C8A2 sample or for the C8A2E5 sample, it exhibited the Newtonian plateau with nearly invariant η* at relatively low frequencies. However, the presence of F-CNTs induces an enhancement of η*, especially at low frequencies. The more the F-CNTs in the blend composites, the more apparent the enhancement of η* is. Obviously, the molecular mobility of the melt is significantly restricted by F-CNTs. Previous morphological characterization has shown that most of F-CNTs are present in the PC component. Therefore, it can be concluded that the viscosity ratio between PC and PLLA component in the blend composites is also increased. This is possibly the other reason for the decrease in PLLA particle size as shown in Fig. 6. In addition, it can be seen that F-CNTs induced the change of the melt from the Newtonian fluid to the non-Newtonian fluid, and the feature of shear thinning behavior became more apparent at high content of F-CNTs.

3.4. Further understanding about the toughening mechanism

To further understand the fracture behavior and toughening mechanism of the PC/PLLA/EOR-g-MAH/F-CNT blend composites, the plastic deformation behavior from a broken Izod sample was further characterized using TEM. The schematic representation showing the sampling method from a broken Izod sample (cross-section of a broken sample in a plane perpendicular to the fractured surface) and the corresponding TEM image are shown in Fig. 9. From Fig. 9b one can see that even underneath the fractured surface, the rigid PLLA particles were also deformed. Furthermore, besides the deformation of rigid PLLA particles, which was also observed from the impact-fractured surface morphologies as shown in Fig. 5, one can also see the orientation of F-CNTs in the similar direction to that of the deformed PLLA particles. It has been proved that the motion and orientation of nanofiller during the fracture process of the sample facilitate the energy dissipation, which results in the improvement of fracture toughness.36 Considering the relatively bigger modulus of PLLA as compared with the ductile PC matrix, it can be believed that the orientation of F-CNTs and the deformation of PLLA particles were mainly attributed to the plastic deformation of PC matrix under the load condition. Therefore, the toughening mechanism of the PC/PLLA/EOR-g-MAH/F-CNT blend composites is proposed as follows.
image file: c4ra11282b-f9.tif
Fig. 9 (a) Schematic representation showing the sampling method from a broken Izod sample and (b) the corresponding TEM image showing the plastic deformation behavior of sample below impact-fractured surface. The representative C8A2E5F2 sample was characterized.

To better understand the toughening mechanism, more visualized schematic representations are shown in Fig. 10. Fig. 10a represents the dispersion of PLLA particles and F-CNTs in the as-prepared sample. Previous TEM images (Fig. 7) have proven that at relatively high content, some of F-CNTs penetrate PLLA particles or a part of a single F-CNT enters into PLLA particles. Obviously, these F-CNTs can exhibit the bridge effect to intensify the interfacial adhesion between PC and PLLA. Under the load condition (Fig. 10b), the dispersed PLLA particles act as the stress concentrator. With the aid of F-CNTs, the local stress formed around PLLA particles can be easily transferred to PC matrix (as shown by arrows), especially when F-CNTs form the network structure. In this condition, the plastic deformation of PC matrix was promoted. With the increase of plastic deformation degree of PC matrix, the coiled F-CNTs agglomerates were disentangled and oriented along the deformation direction of PC matrix (Fig. 10c), leading to more energy dissipation. Simultaneously, under the hydrostatic stress of around PC matrix and inducing the effect of oriented F-CNTs, the deformation of rigid PLLA particles was also promoted. This also facilitates the energy absorption of the sample during the impact fracture process. Obviously, the more the F-CNTs in the blend composites, the denser the F-CNT network structure, and the more apparent the bride effect of F-CNTs is, and therefore the more energy dissipation during the impact process will be. However, it is worth noting that very high content of F-CNTs (5 wt%) result in the formation of large F-CNT agglomerates, on the one hand, which act as the stress concentrator under the load condition. On the other hand, too dense F-CNT network can deteriorate the plastic deformation of PC matrix by restricting the motion of PC chain segments. That is the reason why the C8A2E5F5 sample exhibited a deteriorated tensile ductility and impact fracture toughness as compared with the blend composites containing relatively smaller F-CNTs (≤2 wt%).


image file: c4ra11282b-f10.tif
Fig. 10 Schematic representation showing the plastic deformation of PLLA component and the orientation of F-CNTs during the impact process. (a) The dispersion of PLLA and F-CNTs in the as-prepared sample, (b) PLLA particles act as the stress concentrator, and stress transfer occurs through F-CNTs and (c) the deformation of PLLA particles and the orientation of F-CNTs under the load condition.

4. Conclusions

In summary, the PC/PLLA/EOR-g-MAH/F-CNT blend composites have been prepared by melt-compounding processing. The mechanical properties measurements showed that F-CNTs do not apparently change the tensile properties of the blend composites. However, largely enhanced impact strength was observed for the PC/PLLA/EOR-g-MAH/F-CNT blend composites even if the measurement was carried out at relatively low environmental temperature (0 °C) and the impact strength gradually increased with increasing the content of F-CNTs until very high content of F-CNTs were present in the blend composites, which induces the deterioration of their fracture resistance. In addition, the plastic deformation of PC matrix, the plastic deformation of rigid PLLA particles and the orientation of F-CNTs were also observed. With the combined effects of EOR-g-MAH and F-CNTs, the decreased PLLA particles were achieved. Most of F-CNTs were observed in the PC matrix and form a percolated network structure, which has been further proved by rheological measurement. It is proposed that the largely improved fracture toughness is mainly attributed to the compatibilizing effect of EOR-g-MAH, which significantly improves the interfacial interaction between PC and PLLA components, and the formation of F-CNT network structure and the bridge effect of F-CNTs penetrate PLLA particles, which not only facilitate the stress transfer in the material but also promote the orientation of F-CNTs and the plastic deformation of rigid PLLA particles, leading to more energy dissipation during the fracture process.

Conflict of interest

The authors declare no competing financial interests.

Acknowledgements

Authors express their sincere thanks to the National Natural Science Foundation of China (51473137 and 50973090).

References

  1. C. Koning, M. V. Duin, C. Pagnoulle and R. Jerome, Prog. Polym. Sci., 1998, 23, 707–757 CrossRef CAS.
  2. N. C. Liu and W. E. Baker, Adv. Polym. Technol., 1992, 11, 249–262 CrossRef CAS.
  3. R. Khankrua, S. Pivsa-Art, H. Hiroyuki and S. Suttiruengwong, Polym. Degrad. Stab., 2014, 108, 232–240 CrossRef CAS PubMed.
  4. G. Stoclet, R. Seguela and J. M. Lefebvre, Polymer, 2011, 52, 1417–1425 CrossRef CAS PubMed.
  5. R. Patel, D. A. Ruehle, J. R. Dorgan, P. Halley and D. Martin, Polym. Eng. Sci., 2014, 54, 1523–1532 CAS.
  6. F. P. La Mantia, L. Botta, M. Morreale and R. Scaffaro, Polym. Degrad. Stab., 2012, 97, 21–24 CAS.
  7. M. L. Di Lorenzo, P. Rubino and M. Cocca, J. Appl. Polym. Sci., 2014, 131, 40372 CrossRef.
  8. C. Liu, S. Lin, C. Zhou and W. Yu, Polymer, 2013, 54, 310–319 CrossRef CAS PubMed.
  9. Y. H. Wang, Y. Y. Shi, J. H. Yang, T. Huang, N. Zhang and Y. Wang, J. Appl. Polym. Sci., 2013, 127, 3333–3339 CrossRef CAS.
  10. A. M. Harris and E. C. Lee, J. Appl. Polym. Sci., 2013, 128, 2136–2144 CAS.
  11. Y. Wang, S. M. Chiao, T. F. Hung and S. Y. Yang, J. Appl. Polym. Sci., 2012, 125, E402–E412 CrossRef CAS.
  12. J. B. Lee, Y. K. Lee, G. D. Choi, S. W. Na, T. S. Park and W. N. Kim, Polym. Degrad. Stab., 2011, 96, 553–560 CrossRef CAS PubMed.
  13. T. Kanzawa and K. Tokumitsu, J. Appl. Polym. Sci., 2011, 121, 2908–2918 CrossRef CAS.
  14. V. T. Phuong, M. B. Coltelli, P. Cinelli, M. Cifelli, S. Verstichel and A. Lazzeri, Polymer, 2014, 55, 4498–4513 CrossRef CAS PubMed.
  15. F. M. Xiang, J. Wu, L. Liu, T. Huang, Y. Wang, C. Chen, Y. Peng, C. X. Jiang and Z. W. Zhou, Polym. Adv. Technol., 2011, 22, 2533–2542 CrossRef CAS.
  16. Y. Y. Shi, Y. L. Li, F. M. Xiang, T. Huang, C. Chen, Y. Peng and Y. Wang, Polym. Adv. Technol., 2012, 23, 783–790 CrossRef CAS.
  17. J. Chen, Y. Y. Shi, J. H. Yang, N. Zhang, T. Huang and Y. Wang, Polymer, 2013, 54, 464–471 CrossRef CAS PubMed.
  18. L. Liu, Y. Wang, Y. L. Li, J. Wu, Z. W. Zhou and C. X. Jiang, Polymer, 2009, 50, 3072–3078 CrossRef CAS PubMed.
  19. Y. Y. Shi, W. B. Zhang, J. H. Yang, T. Huang, N. Zhang, Y. Wang, G. P. Yuan and C. L. Zhang, RSC Adv., 2013, 3, 26271–26282 RSC.
  20. Y. H. Wang, Y. Y. Shi, J. Dai, J. H. Yang, T. Huang, N. Zhang, Y. Peng and Y. Wang, Polym. Int., 2013, 62, 957–965 CrossRef CAS.
  21. R. S. Hadal, A. Dasari, J. Rohrmann and R. D. K. Misra, Mater. Sci. Eng., A, 2004, 372, 296–315 CrossRef PubMed.
  22. S. D. Park, M. Todo, K. Arakawa and M. Koganemaru, Polymer, 2006, 47, 1357–1363 CrossRef CAS PubMed.
  23. D. F. Wu, D. Lin, J. Zhang, W. Zhou, M. Zhang, Y. Zhang, D. Wang and B. Lin, Macromol. Chem. Phys., 2011, 212, 613–626 CrossRef CAS.
  24. F. F. Tao, D. Auhl, A. C. Baudouin, F. J. Stadler and C. Bailly, Macromol. Chem. Phys., 2013, 214, 350–360 CrossRef CAS.
  25. A. C. Baudouin, D. Auhl, F. F. Tao, J. Devaux and C. Bailly, Polymer, 2011, 52, 149–156 CrossRef CAS PubMed.
  26. A. Ajji and L. A. Utracki, Polym. Eng. Sci., 1996, 36, 1574–1585 CAS.
  27. W. Gleinser, H. Braun, C. Friedrich and H. J. Cantow, Polymer, 1994, 35, 128–135 CrossRef CAS.
  28. M. Iza, M. Bousmina and R. Jerome, Rheol. Acta, 2001, 40, 10–22 CrossRef CAS.
  29. C. Sailer and U. A. Handge, Macromolecules, 2007, 40, 2019–2028 CrossRef CAS.
  30. M. Entezam, H. A. Khonakdar, A. A. Yousefi, S. H. Jafari, U. Wagenknecht, G. Heinrich and B. Kretzschmar, Macromol. Mater. Eng., 2012, 297, 312–328 CrossRef CAS.
  31. R. Krishnamoorti and E. P. Giannelis, Macromolecules, 1997, 30, 4097–4102 CrossRef CAS.
  32. P. Pötschke, T. D. Fornes and D. R. Paul, Polymer, 2002, 43, 3247–3255 CrossRef.
  33. Z. H. Xu, Y. H. Niu, L. Yang, W. Y. Xie, H. Li, Z. H. Gan and Z. G. Wang, Polymer, 2010, 51, 730–737 CrossRef CAS PubMed.
  34. R. A. Khare, A. R. Bhattacharyya, A. R. Kulkarni, M. Saroop and A. Biswas, J. Polym. Sci., Part B: Polym. Phys., 2008, 46, 2286–2295 CrossRef CAS.
  35. H. K. F. Cheng, N. G. Sahoo, Y. Z. Pan, S. H. Chan, J. H. Zhao and G. Chen, J. Polym. Sci., Part B: Polym. Phys., 2010, 48, 1203–1212 CrossRef CAS.
  36. T. H. Zhou, W. H. Ruan, M. Z. Rong, M. Q. Zhang and Y. L. Mai, Adv. Mater., 2007, 19, 2667–2671 CrossRef CAS.

This journal is © The Royal Society of Chemistry 2014
Click here to see how this site uses Cookies. View our privacy policy here.