Ali Nabipour Chakoli*a,
Jinmei Heb,
Maryam Amirian Chayjanc,
Yudong Huang*b and
Baode Zhangd
aNuclear Safety and Radiological Protection Research Dep., NSTRI, P. O. Box: 14395-836, Tehran, Iran. E-mail: a_nssabipour@yahoo.com
bSchool of Chemical Engineering and Technology, State Key Laboratory of Urban Water Resource and Environment, Harbin Institute of Technology, Harbin 150001, China. E-mail: ydhuang.hit1@yahoo.com.cn; Fax: +86-451-8622-1048; Tel: +86-451-8641-4806
cTeachers University, Ferdosi Center, Baghestan, Karaj, Iran
dSchool of Mechanical Engineering, Liaoning Shihua University, Fushun, 113001, China
First published on 11th June 2015
Radiation sterilization processes by high energy radiation are successfully utilized for modification and sterilization of sensitive biodegradable and biocompatible polymer composites. The effect of γ-irradiation on mechanical and thermal properties of poly (L-lactide) (PLLA) biodegradable polymer reinforced with PLLA grafted from multiwalled carbon nanotubes (MWCNT-g-PLLA)s was characterized. For this purpose, the PLLA chains covalently grafted from the sidewall of aminated MWCNTs. Then, the MWCNT-g-PLLAs/PLLA composite films are prepared by solution casting using chloroform as solvent. The prepared composites were γ-irradiated and characterized by differential scanning calorimeter (DSC), SEM and tensile test instruments. It is found that the γ-irradiation increases the tensile modulus and tensile strength, while decreases the elongation at break. The melting point of composites decreases by irradiation, while the melting enthalpy increases. Additionally, It is found that if the γ-irradiation of composites increases to higher than 50 kGy, the rigidity and brittleness of composites, that have more concentrations of functionalized MWCNTs, increase gradually.
Since high energy electromagnetic and particle radiation exhibit properties of controlled penetration and intensities, which are especially suitable for synthesis and modification of polymeric biomaterials without the need of usually toxic additives, the interest for performing radiation techniques in biotechnology and biomedicine is growing rapidly.16
Irradiation creates free radicals which will often chemically react in various ways, sometimes at slow reaction rates. The free radicals can recombine forming the cross-links. Another influence which may not be as subtle is oxidation during irradiation.
The possible radical that can be formed during γ-irradiation of PLLA is presented in Scheme 1, according to the literatures.16,17 The scheme shows that it is possible to create two radicals for each monomer of PLLA chains by γ-irradiation. Hence it is predictable that the irradiation of MWCNT-g-PLLAs/PLLA, creates some radicals not only on bulk PLLA chains but also on the grafted polymer chains on the sidewall of MWCNT-g-PLLAs. Due to the created radicals in composites, the covalent bonds can be created between grafted polymer chains and matrix polymer chains. As a result of the radiation effect, the polymers are subject in varying extents to degradation and cross-linking reactions. Parameters such as morphology, chemical structure of the polymer, dose and irradiation media determine whether cross-linking or chain scission is the dominating effect of the irradiation.
Scheme 1 The possible radical formation in PLLA polymer chains under the γ-irradiation.16,17 |
In this research, the PLLA chains were grafted on the surface of aminated MWCNTs. Then, the neat PLLA was reinforced using functionalized MWCNTs. The prepared composites were irradiated using 60Co irradiator. To investigate the effect of irradiation on the morphology of composites, the SEM has been carried out. The physical and mechanical properties of irradiated composites were characterized using DSC and tensile test device.
The L-lactide oligomer (LA) (Xiaogan Esun New Material Co, China) is used as received. The stannous octanoate (St(Oct)2) (Shanghai chemical reagent company, China) is used as a catalyst for LA polymerization. The chloroform, ethanol, methanol, toluene were purchased from Kermel of China as analytic reagent.
The differential scanning calorimetery (DSC) was carried out with a Perkin-Elmer Diamond DSC. The samples (10 ± 0.5 mg) were placed in aluminium crucibles. An empty aluminium crucible was used as reference. Samples were heated from −30 °C to 200 °C at flow of nitrogen. Heating rate of 20 °C min−1 was used and continuous recordings of the heat flow and sample temperature were taken. To enhance the accuracy of characterization test results, each sample considered as average of at least three specimens.
The tensile behaviour of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs are carried out according to the ASTM D638 standard method. The tensile tests are performed using a microcontroller electronic tension meter (model WDW3100) machine at a crosshead speed of 2.5 mm min−1 at room temperature. The value of tensile modulus, yield strength, ultimate strength, and elongation at break of each sample are the average of at least three specimens per sample.
Fig. 1 The SEM micrographs of MWCNT-g-PLACLs (a), the fracture surface refer to neat PLLA (b) and the fracture surface for composites: (1 wt%)MWCNT-g-PLLAs/PLLA (c) and (3 wt%)MWCNT-g-PLLAs/PLLA (d). |
Fig. 1(b) presents the fracture surface of neat PLLA after tensile test. It can be seen that the fracture surface of neat PLLA, due to the crystallinity of PLLA, is not very smooth. The breaking points are near to the crystalline phases of samples. Fig. 1(c) and (d) presents the fracture surface of (1 wt%)MWCNT-g-PLLAs/PLLA and (3 wt%)MWCNT-g-PLLAs/PLLA (d) composites, respectively, after tensile test at room temperature. At the fracture surface of the (1 wt%)MWCNT-g-PLLAs/PLLA, there is some wide tips that which maybe caused during elongation at fracture points. Additionally, there are many fine tips that can be attributed to the pulled out and fractured MWCNT-g-PLLAs under the tensile test.
At the fracture surface of the (3 wt%)MWCNT-g-PLLAs/PLLA composite, the MWCNT-g-PLLAs are well dispersed throughout the polymer matrix. The adhesion effect between MWCNTs and PLLA matrix is greatly improved because most of the MWCNT-g-PLLAs on the fracture surface are pulled out and then some of them broken. Therefore, the functionalization of MWCNTs effectively improves the dispersion and interfacial bonding in MWCNTs reinforced PLLA polymer composite.
During dispersion of small fillers in a low viscosity medium, diffusion processes and filler–filler and filler–matrix interactions play an increasingly important role as the diameter drops below one micrometer. Both of the size and specific surface area of MWCNT-g-PLLAs significantly influences the dispersion process. These regions are distinctly different from the bulk polymer and can represent a substantial volume fraction of the matrix for nanoparticles with surface areas of the order of hundreds of m2 g−1. The actual inter phase volume depends on the dispersion and distribution of the MWCNT-g-PLLAs particles, as well as their surface area.
The surface morphology of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs after 50 kGy γ-irradiation are indicated in Fig. 2. The SEM micrograph shows that the 50 kGy γ-irradiation slightly changes the surface morphology of composites. As can be seen, some defects were created on the surface of neat PLLA and its composites.
Fig. 2 The SEM micrographs of neat PLLA (a) and its composites with various concentrations of MWCNT-g-PLLAs, 1 wt% (b) and 3 wt% (c) after 50 kGy γ-irradiation. |
The surface morphology of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs after 100 kGy γ-irradiation are presented in Fig. 3. It can be seen that the density of surface defects after 100 kGy γ-irradiation is significantly higher than that of 50 kGy γ-irradiated composites.
Fig. 3 The SEM micrographs of neat PLLA (a) and its composites with various concentrations of MWCNT-g-PLLAs, 1 wt% (b) and 3 wt% (c) after 100 kGy γ-irradiation. |
It can be seen that the created defects in the lower concentration of amorphous phase in (3 wt%)MWCNT-g-PLLAs/PLLA composites, after 100 kGy γ-irradiation is higher than that of neat PLLA. The crystalline phase of composites and the spherulites, due to their rigidity, has higher strength in comparison with amorphous phase during the γ-irradiation.
It can be seen that the melting point of neat PLLA decreases after γ-irradiation. The result indicates that the chain scissoring is occurred during γ-irradiation. Hence, the melting point of PLLA decreases due to molecular chain scissoring. As can be seen, the melting enthalpy of irradiated neat PLLA is slightly higher than that of primary neat PLLA. It reveals that the crystallinity of neat PLLA slightly increases during γ-irradiation. It may due to the cross-linking effect of γ-irradiation on PLLA molecular chains and creation of smaller lamellaes with shorter polymer chains that made of scissoring effect of γ-irradiation on PLLA.
Fig. 4 shows the DSC curves of neat PLLA and its composites with 1 wt% and 3 wt% of MWCNT-g-PLLAs after 50 kGy γ-irradiation.
Fig. 4 The DSC curves of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs after 50 kGy γ-irradiation under the air atmosphere at room temperature. |
The detailed information of Fig. 3 such as melting point and melting enthalpy of neat PLLA and MWCNT-g-PLLAs/PLLA after 50 kGy γ-irradiation are illuminated in Table 1. The results show that after γ-irradiation, the crystallinity of composites are higher than that of neat PLLA. The increment in crystallinity of irradiated MWCNT-g-PLLAs composites decreases with increasing the concentrations of MWCNTs-g-PLLAs. It is due to decreasing the mobility of polymer chains with increment the concentrations of MWCNT-g-PLLAs. Before irradiation, the crystallinity of MWCNT-g-PLLAs is increases with increasing the concentrations of MWCNT-g-PLLAs. Hence, the mobility of broken PLLA chains during γ-irradiation decreases.
Filler contents (wt%) | Melting point (°C) | Melting enthalpy (J g−1) |
---|---|---|
0 | 173.2 | 47.3 |
1 | 179.4 | 42.5 |
3 | 177.5 | 41.2 |
Fig. 5 shows the DSC curves of neat PLLA and its composites with 1 wt% and 3 wt% of MWCNT-g-PLLAs after 100 kGy γ-irradiation. The melting point and melting enthalpy of neat PLLA and its composites after 100 kGy γ-irradiation under the air atmosphere at room temperature are illuminated in Table 2. The results indicate that before and after γ-irradiation, the crystallinity of composites are higher than that of neat PLLA. The crystallinity of irradiated MWCNT-g-PLLAs composites decreases with increasing the concentrations of MWCNTs-g-PLLAs. It is due to decreasing the mobility of broken PLLA chains with increment in concentrations of MWCNT-g-PLLAs.
Fig. 5 The DSC curves of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs after 100 kGy γ-irradiation under the air atmosphere at room temperature. |
Filler contents (wt%) | Melting point (°C) | Melting enthalpy (J g−1) |
---|---|---|
0 | 153.5 | 52.3 |
1 | 160.3 | 50.7 |
3 | 155.9 | 48.9 |
Before irradiation, the crystallinity of composites is increases with increasing the concentration of MWCNT-g-PLLAs. Hence, the mobility of broken PLLA chains during γ-irradiation decreases. The broken PLLA chains under γ-irradiation create small lamellaes. Increment in concentration of small lamellaes in composites decreases the melting point of composites. The results show that the melting enthalpy of composites decreases with increasing the concentrations of MWCNT-g-PLLAs in composites. Less movement of polymer chains that made of scissoring effect under the γ-irradiation in composites in comparison with the neat PLLA, occurs due to the MWCNT-g-PLLAs, that decreases the creation of new lamellaes after γ-irradiation.
MWCNT-g-PLLAs | Tensile modulus (MPa) | Yield strength (MPa) | Ultimate strength (MPa) | Elongation (%) |
---|---|---|---|---|
0 (primary PLLA) | 4.1 | 32.3 | 37.8 | 158 |
0 (irradiated PLLA) | 3.6 | 29.5 | 30.1 | 40.55 |
0 | 3.6 | 29.5 | 30.1 | 40.55 |
1 | 4.86 | 33.2 | 35.8 | 16.4 |
3 | 5.5 | 38.7 | 40.5 | 13.9 |
The results show that after 50 kGy γ-irradiation of neat PLLA, the tensile modulus and yield strength increases, while, the elongation at break decreases 74%. In addition, the 100 kGy γ-irradiated neat PLLA, is too brittle to do tensile analysis. As can be seen, the γ-irradiation decreases the mechanical performance of neat PLLA. It means that the γ-irradiation for neat PLLA is not useful to enhance the performance of neat PLLA. It must be considered that for sterilization of devices that made of PLLA, the γ dose must be less than 50 kGy.
The stress–strain curves of neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs, after 50 kGy γ-irradiation at room temperature are presented in Fig. 7.
Fig. 7 The tensile test results of 50 kGy γ-irradiated neat PLLA and its composites with various concentrations of MWCNT-g-PLLAs at room temperature. |
The summary of tensile test results are indicated in Table 3. Due to the decreasing in mobility of broken PLLA chains with increment the concentrations of MWCNT-g-PLLAs, the elongation at break of neat PLLA decreases. Before irradiation, the crystallinity of composites is increases with increasing the concentration of MWCNT-g-PLLAs. Hence, the mobility of broken PLLA chains during γ-irradiation decreases. The broken PLLA chains under γ-irradiation create small lamellaes. The ratio of crystalline phase in composites increases with increasing the concentrations of MWCNT-g-PLLAs in composites. Due to lower concentration of amorphous phase in (3 wt%)MWCNT-g-PLLAs/PLLA, the elongation at break decreases. In addition, the shorter PLLA chains occur low elongation at break under the tensile test. It can be seen that the γ-irradiation slightly increases the tensile strength of neat PLLA and its composites, while, decreases the elongation at break gradually. Rapid decreasing in mechanical properties occurs when higher irradiation doses (100 kGy) is imposed.
Decreasing in mechanical properties is considered to be correlated to degradation (chain scission) of neat PLLA under the γ-irradiation. Nevertheless, after γ-irradiation at 100 kGy, the pure PLLA film is clear and colorless, but it lost its mechanical strength. Hence, the 100 kGy irradiated samples are brittle and useless for tensile test and related analysis.
Footnote |
† Electronic supplementary information (ESI) available. See DOI: 10.1039/c5ra08319b |
This journal is © The Royal Society of Chemistry 2015 |