Audrey
Scholz
,
Russell L.
Lewis
,
Michael A.
Bachan
,
Amanda L.
Stewart
and
Rafael L.
Quirino
*
Chemistry Department, Georgia Southern University, USA. E-mail: rquirino@georgiasouthern.edu
First published on 2nd May 2017
Collagen from three different sources has been added to a tung oil-based thermosetting resin in order to enhance its mechanical properties for possible applications in the biomedical field as materials directly derived from biological molecules. The thermosets prepared in this work are made using tung oil, divinylbenzene (DVB), n-butyl methacrylate (BMA), tert-butyl peroxide (TBPO), asolectin, and collagen types I and III. Composites containing up to 5.0 wt% of collagen have been successfully prepared and characterized by dielectric analysis (DEA), thermogravimetric analysis (TGA), and differential scanning calorimetry (DSC). The structure of the collagen samples used in this work was investigated through circular dichroism (CD) spectroscopy. Dynamic mechanical analysis (DMA) was used to assess composites' mechanical properties and revealed an improvement in the storage modulus at room temperature with increasing amounts of collagen, reaching an impressive increase of ∼100% for composites containing 5.0 wt% of collagen extracted from beef tendons in comparison to the unreinforced resin. The results indicate that collagen exhibits a reinforcing behavior similar to that obtained with nanostructured materials, such as carbon nanotubes for instance, therefore working as an effective reinforcement for the preparation of biocomposites.
In most of the aforementioned examples, however, there is an inherent incompatibility between the hydrophobic resin and a hydrophilic reinforcement, which prevents maximization of the reinforcing effect imparted by the reinforcing materials used. Asolectin, a mixture of phospholipids naturally formed and obtained from soybeans, has been successfully used as a bio-based reactive surfactant in the emulsion polymerization of tung oil,22 and as a bio-based compatibilizer in tung oil-based/cellulose composites.13 Asolectin contains both saturated and unsaturated phospholipids,23 which allow it to react with hydrophobic olefins, such as tung oil, and interact with hydrophilic groups, such as those present in collagen. Collagen is a fibrous and linear, triple helical protein24,25 that can be found in the majority of organic tissues, such as skin, tendons, and bones.25,26 It has been used in the medical field for tissue engineering,25 but so far, its use in the synthesis of bio-based composites has been scarcely reported, mainly as a reinforcement for castor oil-containing polyurethanes.27 It is believed that collagen's polar segments are stronger or more prevalent than its hydrophobic segments, making the addition of a compatibilizer necessary in order to maximize its reinforcing effect in a tung oil resin.
In this study, a collagen-reinforced biocomposite from tung oil was prepared using free radical initiation and thermal polymerization, leading to a polyolefinic tung oil-based matrix with properties and structure very different from those of the castor oil-containing polyurethanes reported in the literature,27 with a completely different chemistry involved, hence the relevance of this work in the arena of vegetable oil-based materials. The structure of collagen extracted from beef tendon was compared against purified type I collagen and a commercial mixture of types I and III collagen by circular dichroism (CD) spectroscopy. Cure time was determined through dielectric analysis (DEA). The thermal and mechanical properties of the composites were assessed by means of thermogravimetric analysis (TGA), differential scanning calorimetry (DSC), and dynamic mechanical analysis (DMA), showing impressive improvement in storage modulus upon addition of collagen. The primary goal of the work presented is to establish and study a bio-based composite system that shows promise for use in the biomedical field as an implant material. A full mechanical characterization of the tung oil/collagen composites prepared is beyond the originally intended scope of this manuscript. The discussion revolves around a description of this new composite system by providing its thermo-mechanical properties, including traditional characterization methods, such as dynamic mechanical analysis, TGA, and DSC.
DEA was run using an Epsilon DEA 230/1 cure monitor (Netzsch Instruments North America LLC, Burlington, MA) with frequencies ranging from 0.3 Hz to 10000.0 Hz to show the resin's cure behavior in the presence of collagen. A flexible probe was submersed in the resin for the duration of the cure schedule. The sample was heated in a convection oven for a total of 24 hours at temperatures ranging from 100 °C to 140 °C. The permittivity and loss factor of the composite were measured as a function of time. The results presented in the text correspond to a plot of ion viscosity (Ohm cm) versus time. The sample size was approximately 10 g.
Raman spectra and optical microscopy images were acquired with a DXR Raman Microscope (Thermo Fisher Scientific, Waltham, MA, USA) equipped with a digital camera. A total of 32 scans were collected per sample at an exposure time of 1 s for each scan. Laser power was set to 7.0 mW, and a 50 μm slit aperture was used.
FTIR spectra were collected using a Thermo Nicolet Avatar 370-FTIR spectrometer (Thermo Scientific, Waltham, MA) with an attenuated total reflectance (ATR) accessory. The spectra were obtained in the 400–4000 cm−1 spectral region, with 64 scans, and 4 cm−1 resolution.
Thermal stability was assessed using a Q50 TGA instrument (TA Instruments, New Castle, DE). Samples were heated from room temperature to 600 °C at a rate of 20 °C min−1 while the weight of the sample was measured under an air atmosphere as a function of time. All TGA experiments were carried out in triplicate to ensure consistency of the results reported. A Q20 DSC instrument (TA Instruments, New Castle, DE) was used under a N2 atmosphere with samples of approximately 10 mg being heated from −20 °C to 200 °C at a rate of 10 °C min−1.
The presence of collagen in the beef tendon extracts was confirmed through CD spectroscopy using a Jasco J-815 CD Spectrometer with an auto peltier 6 cell changer operated under nitrogen gas. All samples were prepared in 0.1 M acetic acid in 0.02 M Na2HPO4. The samples were kept at a constant temperature of 5 °C throughout the experiment. All collagen samples were also evaluated with respect to their fraction folded as the temperature increased from 0 °C to 100 °C to show denaturation patterns. These experiments were duplicated showing a maximum deviation of 1 °C between any two measurements for the same type of collagen investigated.
DMA experiments were performed on a Q800 instrument (TA Instruments, New Castle, DE) under tension mode. A multi-frequency strain method was used with an amplitude of 14.0 μm and a frequency of 1 Hz. The composite samples were cut into specimens of 10.00 mm × 4.00 mm × 2.20 mm (length, width, thickness) to examine their dynamic mechanical behavior between −60 °C and 150 °C. Storage modulus (MPa) and tan delta were measured as a function of temperature (°C) under a heating rate of 3 °C min−1. The DMA data reported corresponds to the average of 3–7 measurements per sample and includes the corresponding standard deviation.
SEM images were obtained in a JSM-760F Field Emission Scanning Electron Microscope (JEOL, Peabody, MA), using an accelerating voltage of 1.0 kV, lower detector scanning mode (LEI), and an emission current of approximately 81 μA.
In order to avoid formation of bubbles and cracks in the composites upon cure, two new cure schedules were attempted, as described in Table 1. On cure schedule II, the introduction of an additional step at 120 °C for 4 hours and 30 minutes was meant to slow the polymerization rate and limit crack and bubble formation, as previously observed in similar systems.22 For practical reasons, it was desirable that the overall cure process lasted for no longer than 8 hours. The times at 120 °C and 140 °C were arbitrarily broken down into 4 h 30 min and 3 h 30 min, respectively, to allow for a longer time for the first step. Implementation of cure schedule II failed to produce good composites at 5 wt% and 10 wt% collagen loadings due to extensive bubble formation. A third cure sequence consisting of a 24 hour, multi-step temperature profile (cure schedule III, Table 1) was then implemented, producing composites with no imperfections at 0 wt%, 0.5 wt%, 1 wt%, 2 wt%, and 5 wt% collagen loadings. Because the radical formation rate for di-t-butyl peroxide peaks at 110–140 °C, it was decided that the times of those steps should be maximized and evenly spaced, while the initial step at 100 °C (when the polymerization process isn't occurring at an appreciable rate) and at 140 °C (when most of the polymerization has already completed) received lower times. Cure schedule III was employed in all following samples described in this manuscript.
Cure schedule | 100 °C | 110 °C | 120 °C | 130 °C | 140 °C |
---|---|---|---|---|---|
I | — | — | — | — | 15 h |
II | — | — | 4 h 30 min | — | 3 h 30 min |
III | 2 h | 6 h | 6 h | 6 h | 4 h |
The polymer obtained by the bulk free radical co-polymerization of tung oil, BMA, DVB, and asolectin is a crosslinked thermoset and therefore doesn't exhibit a defined molecular weight as typical thermoplastics. Maldi-Tof has been previously employed to show evidence of the free radical polymerization reaction of a partially cured binary mixture of tung oil and asolectin heated under emulsion polymerization conditions.22 In this work, however, the bulk polymerization of the system leads to high crosslink densities, making the products insoluble. Several unsuccessful attempts have been made to date to obtain Maldi-Tof evidence for the bulk free radical polymerization reaction of the resin investigated in this work. In an effort to estimate the extent of monomer conversion, Soxhlet extraction experiments have been performed on the final cured resin and in composites prepared with 5.0 wt% of collagen I + III mixture and collagen from beef tendons. The results revealed that only 5.2 wt% of extractables were recovered after the polymerization of the resin, indicating an overall 96.8% monomer conversion. When the polymerization was carried out in the presence of 5.0 wt% of collagen, a higher amount of extractables was recovered (8.1 wt% for collagen from beef tendons and 9.1 wt% for type I + III collagen). These results confirm significant polymerization of the initial monomer mixture, with monomer conversions consistently higher than 90% for all samples reported in this manuscript.
The cure of a composite containing 1.0 wt% of collagen under schedule III was monitored through DEA (Fig. 1) in order to track the polymerization of the resin in the presence of collagen. The DEA results presented in Fig. 1 match the expected behavior for the cure of thermosetting resins. Indeed, the initial drop in ion viscosity (0–1 h, Fig. 1) corresponds to initial heating of the resin before the free radical initiator (TBPO) is significantly cleaved to trigger polymerization at an appreciable rate. In that stage, the increase in temperature from room temperature to 100 °C imparts greater mobility of all molecules in the system, resulting in a greater permittivity, which translates into lower ion viscosity.
Fig. 1 Dielectric analysis results for the cure of a composite containing 1.0 wt% of collagen I + III mixture following cure schedule III. |
After approximately 3 h (Fig. 1), the temperature reaches 110 °C (Table 1), and the resin experiences significant polymerization. As polymerization progresses, increases in polymer chain length and crosslink density result in lower chain mobility, resulting in a continuous increase of ion viscosity until approximately 20 h (Fig. 1). The change in polymerization rate upon each temperature change in that stage, according to cure schedule III (Table 1), can be appreciated by clear changes in the slope of the ion viscosity curve in Fig. 1 (∼8 h, 14 h, 20 h). After 20 h, when the temperature reaches 140 °C, the resin attains cure completion and, after a slight drop in ion viscosity (20–21 h, Fig. 1), no further changes are observed, indicating completion of the cure process after 21 h. The completion of the cure process can also be verified by Raman and FTIR spectroscopies (Fig. 2 and 3, respectively).
Fig. 2 Raman spectra of (a) tung oil and (b) resin containing 40 wt% of tung oil, 30 wt% of BMA, 20 wt% of DVB, and 10 wt% of asolectin, subjected to cure schedule III. |
On Fig. 2, a comparison of the Raman spectrum of tung oil (Fig. 2a) with that of the optimized resin subjected to cure schedule III (Fig. 2b) clearly shows that after the cure, the peak corresponding to CC vibrations at approximately 1650 cm−1 can't be detected, suggesting that the vast majority of the carbon–carbon double bonds in the system react fully during the cure process. A similar situation is observed when comparing the FTIR spectrum of tung oil and that of the optimized resin subjected to cure schedule III (Fig. 3). Indeed after cure, the fully polymerized resin doesn't exhibit the characteristic peak of C(sp2)–H vibrations at 3011 cm−1. All other major peaks in tung oil are also present in the resin, as can be clearly seen in Fig. 3.
The evolution of bubbles during the cure of collagen composites can be associated to the presence of about 10 wt% of water in the collagen I + III mixture, confirmed through TGA (Fig. S1, ESI†). Despite drying the collagen I + III mixture prior to its incorporation in composites, its ability to quickly adsorb moisture present in the air significantly limits the possibility of preparing composites with collagen loadings higher than 10 wt% in a practical manner.
Upon a comparison of the thermal degradation profiles of composites reinforced with different loadings of collagen (Fig. 5), an overall trend of increase in thermal stability can be seen for increasing collagen load. The initial degradation of the unreinforced resin and the composite reinforced with 1.0 wt% collagen I + III mixture coincide until approximately 320 °C. After that temperature, the unreinforced resin exhibits a significantly faster degradation rate. The composite reinforced with 5.0 wt% of collagen I + III mixture exhibits a markedly higher stability than the other two samples in Fig. 5, with an onset degradation temperature of ∼350 °C. This trend confirms that the interaction between collagen and resin results in an increased thermal stability of the composite when compared to the individual components.
Fig. 5 TGA curve for composites containing (a) 0.0 wt%, (b) 1.0 wt%, and (c) 5.0 wt% of collagen I + III mixture. |
When comparing the DSC curves of the unreinforced tung oil-based resin, the collagen I + III mixture, and a composite containing 5 wt% collagen I + III mixture (Fig. 6), no visible peaks are detected for the resin and for the composite (Fig. 6b and c), indicating cure completion for both materials when subjected to cure schedule III. The DSC curve of the collagen I + III mixture reveals a broad peak centered at 110 °C and compatible with loss of water from the collagen mixture sample (Fig. S1, ESI† and Fig. 6a).
As shown in Fig. S2 (ESI†), the three different kinds of collagen used in this work had a similar DSC profile with characteristic peaks for loss of water centered at 105–110 °C. The collagen extracted from beef tendons exhibit several peaks overlapping with the broad loss of water centered at 110 °C (Fig. S2C, ESI†). In order to confirm the reversibility of these peaks, a heat–cool–heat DSC experiment was carried-out (Fig. S3, ESI†).
Upon initial heating, the collagen extracted from beef tendons exhibits the already discussed DSC profile with the evident loss of water predominating over narrower overlapping peaks, possibly related to collagen conformation changes. On Fig. S3 (ESI†), no peaks are detected during either the cooling of the sample, or the second heating cycle, suggesting that the loss of water during the experiment and any accompanying changes are irreversible. It is worth mentioning, however, that dry samples, upon exposure to ambient conditions, re-adsorb moisture quickly, making it impractical to prepare composites in the absence of water.
As observed in Fig. S4b (ESI†), collagen type I has the signature curve expected from the dominant triple helix structure of collagen with a maximum at approximately 222 nm and a minimum at approximately 200 nm. The collagen extracted from beef tendons (Fig. S4a, ESI†) does not show a maximum at 222 nm, indicating lack of a triple helix structure. Likewise, the collagen I + III mixture also lack the triple helix characteristic signals in the CD spectrum. A detailed study of the loss of the triple helix during collagen extraction/purification will be carried-out in the near future.
Based on the results shown in Fig. S4 (ESI†), at 5 °C, the triple helix structure of collagen type I would ensure a better mechanical performance than the other two collagen samples investigated. However, since the cure of the composites requires heating up to 140 °C over 24 hours, it is necessary to evaluate the thermal denaturation behavior of the different types of collagen employed (Fig. 7). Fig. 7 presents a graph of the collagen fraction folded (determined from the intensity of the triple helix peak in the CD spectrum) as a function of the temperature. From the results presented, the temperatures traditionally referred to as melting points (Tm) can be determined. At 0.5 fraction folded, the corresponding Tm is 42 °C for the collagen extracted from beef tendons, 39 °C for collagen type I, and 47 °C for the collagen I + III mixture. This suggests that the collagen I + III mixture is slightly more thermally stable than the other two collagen samples. Nevertheless, it is evident from Fig. 7c that the collagen I + III mixture does not exhibit the typical sigmoidal curve expected for the thermal denaturation graph of a regular helical protein. This indicates that either the combination of two types of collagen or a side effect of the preparation method of the mixture impacted its final structure.
Fig. 7 Sigmoidal fit over original CD data for the thermal denaturation of (a) collagen extracted from beef tendons, (b) type I collagen, and (c) collagen I + III mixture. |
Entry | Source | Collagen load (wt%) | T g (°C) | E′ at 25 °C (MPa) | E′ at Tg + 50 °C (MPa) |
---|---|---|---|---|---|
a The resin yielded prematurely at 70 °C. b http://https://www.plasticsintl.com/datasheets/HDPE.pdf. c http://https://www.marleypipesystems.co.za/images/pdfdownloads/productbrochures/hdpe-physical-properties.pdf. d Material melts at 126 °C. | |||||
1 | — | — | 29 ± 2 | 122.2 ± 12.4 | —a |
2 | Beef tendon | 0.5 | 27 ± 3 | 120.7 ± 3.7 | 37.4 ± 2.4 |
3 | Beef tendon | 1 | 27 ± 3 | 143.0 ± 19.5 | 40.0 ± 1.3 |
4 | Beef tendon | 5 | 31 ± 3 | 247.6 ± 6.3 | 50.4 ± 3.4 |
5 | Type I | 0.5 | 35 ± 2 | 98.9 ± 1.3 | 19.8 ± 8.9 |
6 | Type I | 1 | 36 ± 3 | 132.8 ± 17.5 | 26.0 ± 2.9 |
7 | Type I | 5 | 30 ± 3 | 104.1 ± 12.2 | 28.8 ± 3.8 |
8 | Types I + III | 0.5 | 36 ± 3 | 129.0 ± 17.0 | 23.0 ± 3.7 |
9 | Types I + III | 1 | 37 ± 1 | 131.0 ± 15.0 | 27.0 ± 6.4 |
10 | Types I + III | 5 | 35 ± 4 | 152.5 ± 3.3 | 37.0 ± 5.7 |
11 | HDPE | — | 67b | 1150.0c | —d |
The similarity in tan Delta behavior between the unreinforced resin and a composite reinforced with 5.0 wt% of collagen extracted from beef tendons can be further evaluated in Fig. 8. As will be discussed later in the text, the lack of a premature break of the composite shows that the addition of collagen extracted from beef tendons increases the mechanical properties of the resin.
A more significant increase of the Tg (up to 8 °C) is noticed when the resin is reinforced with type I collagen or collagen I + III mixture (Table 2, entries 5–10), indicating that the flow of resin segments is more significantly impacted by these collagen samples. It is interesting to note that these trends do not necessarily imply a stronger interaction between resin and reinforcement for type I collagen and collagen I + III mixture as one would expect. Indeed, little change in Tg is noticed with changes in collagen loading, suggesting that collagen is simply dispersed amongst the resin. The only deviation observed occurs for the sample reinforced with 5.0 wt% of type I collagen, which exhibits a Tg very similar to that of the unreinforced resin. Furthermore, the reverse trend is observed when comparing the results for storage moduli, with collagen extracted from beef tendons resulting in overall higher values than composites prepared with type I collagen or collagen I + III mixture (Table 2). The only exception to that trend occurs with the composite reinforced with 0.5 wt% of collagen I + III mixture, which exhibits a slightly higher storage modulus at 25 °C than the equivalent composite prepared with collagen extracted from beef tendons. Such deviation from the predominant trend could be related to the low reinforcement load used.
According to the results for storage modulus at 25 °C in Table 2, the reinforcing effect of adding collagen to the resin can only be observed at higher collagen loadings. The only composite that exhibits an improvement of the storage modulus at 25 °C at a 0.5 wt% load, in comparison to the pure resin, is the one prepared with collagen I + III mixture (Table 2, entry 8). Likewise, with the exception of the sample reinforced with 1.0 wt%, all composites prepared with type I collagen exhibited a decrease in E′ at 25 °C in comparison to the unreinforced resin. Regardless of the collagen type used, an increase in storage modulus at 25 °C is clearly observed with increasing collagen loading (Table 2), with an impressive ∼100% improvement for the sample reinforced with 5.0 wt% of collagen extracted from beef tendons in comparison to the unreinforced resin (Table 2, entry 4). Along the same lines, an increase from 129.0 MPa to 152.5 MPa in E′ at 25 °C is observed for the composite prepared with collagen I + III mixture as the collagen load increases from 0.5 wt% to 5.0 wt%, also resulting in an increase in E′ at Tg + 50 °C from 23.0 MPa to 37.0 MPa.
The oscillations in storage modulus at 25 °C pointed out for composites prepared with lower collagen loadings and with type I collagen can be the result of these values being taken at a temperature immediately preceding the Tg of the resin, affecting E′ and deviating from the expected trend. Indeed, the standard deviations calculated for E′ at 25 °C are overall significantly higher than those for E′ at Tg + 50 °C. When E′ is measured at a temperature 50 °C higher than Tg, a more consistent trend is observed, with a clear improvement in E′ for all reinforced samples with respect to the unreinforced resin, and increasing E′ with collagen loading for all types of collagen investigated (Table 2).
As can be seen in Table 2, entry 11, the bio-based composites prepared in this work exhibit inferior properties than HDPE, one of the most widely used material for knee-cap replacements. It is worth noting, however, that a diverse range of properties are desirable for materials used for implants in the biomedical field due to the variety of soft and hard tissues that may need replacement. For example, the properties required for cartilage are very different than those desired for knee-caps. One advantage of the system investigated in this work is the potential tuning of properties by changing the concentration of specific resin components, as explored previously.15
The predominant trends in storage modulus can be fully appreciated for composites containing 5.0 wt% collagen in Fig. 9. The sample prepared with collagen extracted from beef tendons exhibits higher E′ than all other samples up until approximately 90 °C, when the sample prepared with collagen I + III mixture surpasses it briefly before yielding prematurely at ∼120 °C (Fig. 9). When comparing E′ for the unreinforced resin and the composite containing type I collagen, no significant differences are clearly observed, with the exception of the premature yielding of the unreinforced resin at ∼70 °C. The premature yielding of these samples is an indication of their brittleness. Such samples exhibit a shorter temperature range of operation that limits their applicability. It is worth noting that all composites reach the rubbery plateau at approximately 100 °C. Based on the results presented in this report, the purification method employed for the extraction of collagen from beef tendons results in a collagen sample with superior properties than the collagen I + III mixture, which is, in turn, superior than the commercially sourced collagen type I used in this study.
Footnote |
† Electronic supplementary information (ESI) available. See DOI: 10.1039/c7qm00112f |
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