Bhaskar Jyoti Saikia and
Swapan Kumar Dolui*
Tezpur University, Chemical Sciences, India. E-mail: swapandolui@gmail.com
First published on 19th October 2015
An azide–alkyne cycloaddition based self-healing system was designed by a semiencapsulation method. Multiwall carbon nanotubes were functionalized with poly(t-butyl acrylate) containing azide end functionality using atom transfer radical polymerization. Subsequently the alkyne counterpart was encapsulated in urea formaldehyde microcapsules and embedded in an epoxy matrix. The healing click reaction was triggered by an embedded copper catalyst. Whenever a damaging event occurs in the epoxy matrix, the liquid cross linker in the presence of catalyst will dissolve the implanted catalyst from the matrix initiating the crosslinking reaction between azide and alkyne and thus healing the cracks. The effects of temperature and healing duration on healing efficiency are investigated. Once healed, the self-healing system recovers as much as 65% of its original fracture toughness.
Preparation of multifunctional and well-defined macromolecules requires a smart selection of controlled polymerization (CRP) technique in combination with appropriate coupling reactions. ATRP is the most versatile CRP method owing to its exceptional properties like preparation of polymer with predetermined molecular weight, narrow polydispersity index, predetermined chain end functionality and tunable architecture.18–20 Click chemistry is a powerful coupling approach which in combination with ATRP can be used for generation of polymers having almost all of the desired properties.21–25
Click chemistry has been extensively used as a crosslinking reaction while designing self-healing polymers providing high healing efficiency. Among these reactions the Huisgen 1,3-dipolar cycloaddition reaction of organic azides and alkynes also known as CuAAC has gained considerable attention as they are very robust, simple, insensitive and can be used as a polymerization reaction for synthesis of long linear polymers.26–29
Recently, a number of metal chelating systems based on 1,2,3-triazoles and various 1,2,3-triazole containing ligands synthesized by CuAAC has been employed successfully for designing self-healing systems.30–33 However, most of the systems are gels, lacking mechanical and thermal stability for structural applications and requires the presence of suitable metal ions. In this report, we have designed an efficient self-healing system based on direct CuAAC via semi encapsulation approach which has the flexibility of choosing any matrix and enjoy reinforcement by MWCNT. The main strategy for a semi capsulation method is that a matrix is prepared with either inherent or implanted azide (or alkyne) functionality with embedded copper catalyst (preferably CuBr(PPh3)3) and microcapsules containing the compliment functionality alkyne (or azide). As soon as the damaging event occurs the liquid cross linker in presence of catalyst embedded in the matrix will initiate the crosslinking reaction between azide and alkyne and thus healing the cracks. For this purpose, we have first functionalized multiwall carbon nanotube (MWCNT) with ATRP initiator then functionalized with poly(t-butyl acrylate). The bromine end group was subsequently converted to azide and used as multifunctional azide which acts both as crosslinker and provides reinforcement. Urea–formaldehyde microcapsules containing tripropargylpentaerythritol was synthesized via in situ condensation method. Finally azide functionalized MWCNT, tripropargylpentaerythritol containing microcapsules and CuBr(PPh3)3 were embedded into an epoxy matrix to obtain the self-healing composites.
:
1 yielding 3.9 g of pale yellow viscous liquid.
The attachment of ATRP initiator to MWCNT was confirmed by observing the FTIR spectrum of MWCNT–Br with the absorption peaks at 664 cm−1 corresponding to C–Br stretching frequency (Fig. 1). The tertiary center so generated on the surface of MWCNT was used for grafting of t-butyl acrylate using same catalyst system. 1H NMR spectra of the MWCNT–t-BA in CDCl3 shows the presence of characteristic peaks at δ = 4.52 ppm (
CH–Br), 1.92–2.56 ppm (–CH2CH(COOC(CH3)3)–Br), 1.61–1.83 ppm (
CHCOO(CH3)3) ppm, 1.48 ppm (–CH2–), and 1.39 ppm (–C(CH3)3) confirming successful formation of t-BA brushes on MWCNT with bromine end group intact. The broader signals in the spectrum of MWCNT–t-BA may be due to local field effects due to MWCNT itself, or slow tumbling of the large polymer brush in solution36 (Fig. 2).
Finally the bromine end group of MWCNT–t-BA was converted to azide by treatment with NaN3. It is seen that in the FTIR spectra of the azide modified polymer new absorption peaks appears at 2037 cm−1 corresponding to the –N3 stretching confirming successful conversion of bromide to azide. Presence of C–O stretching frequency in MWCNT–t-BA and MWCNT–t-BA–N3 at 1249 cm−1 further confirms the presence of –COO(CH3)3. However other characteristic absorption peaks are not distinguishable due to highly absorbing media of MWCNTs. To confirm that MWCNT–t-BA was only formed due to EiBr covalently anchored on the MWCNT surfaces, a control experiment was also done using pristine MWCNTs to replace MWCNT–Br in the t-BA grafting system. After 36 h, the collected MWCNTs were subjected to TGA measurement which reveals no major weight loss. These results demonstrates that EiBr was successfully attached onto MWCNT surfaces and have the ability to serve as initiating sites for surface-initiating ATRP.
Fig. 3 represents the TGA thermogram of pristine MWCNT, MWCNT–Br and MWCNT–t-BA. It is seen that pristine MWCNT shows only 4% degradation while MWCNT–Br undergoes 24% degradation till 600 °C. The degradation of MWCNT–Br starts at 157 °C which originates from the degradation of ethyl isobutyrate and bromide covalently attached to MWCNT. The TGA curve of MWCNT–t-BA shows a multi-step weight loss. Degradation starts at 230 °C and nearly half of the total degradation occur at that temperature. There is also some weight loss at 260 and 420 °C which contribute the remaining half of the total degradation. The degradation pattern corresponds to degradation of poly(t-butyl acrylate) which indicates successful grafting of t-BA from MWCNT–Br surface.
The healing liquid for microcapsules tripropargylpentaerythritol was synthesized by simple nucleophilic substitution reaction of pentaerythritol with propargyl bromide. The structure was established by 1H NMR spectroscopy with characteristic chemical shift values at δ = 4.09 ppm (–CH2–O), 3.63 ppm (–CH2–OH), 3.40 ppm (–OH), 2.41 (
C–H) (Fig. 4).
The urea formaldehyde microcapsules containing tripropargylpentaerythritol were prepared via in situ condensation method. The controlling parameters were used following literature procedure reported by Zhang Ting et al.37 Initially the encapsulation process was monitored by an optical microscope. Fig. 5(a) shows the optical microscope image of prepared microcapsules. Almost all the microcapsules were found to be of spherical shape. In the optical microscopy study of the microcapsules we found the appearance of diffraction rings which is in accordance with the theory of optics indicating successful incorporation of healing liquid inside.38 Optical microscope image of the glass slides compressed microcapsules in Fig. 5(b) clearly shows the bleeding of the healent out of the capsules. To further confirm the encapsulation of the healing liquid inside the microcapsules 10-styrylanthracene was mixed with tripropargylpentaerythritol before encapsulation and was observed with fluorescent optical microscope. Green bright fluorescent microcapsules in Fig. 5(c) and corresponding broken microcapsule in Fig. 5(d) confirms the successful incorporation of the healent inside UF shells.
The size distribution histogram of the prepared microcapsules is shown in the Fig. 6 Microcapsule size was found to be in a wide range 25–90 μm. It may be due to the fact that the fluid flow around the propeller is turbulent, in the region of flow away from the propeller, many larger microeddies exist, and in the vicinity of the propeller blades, many smaller microeddies exist, which result in a wider distribution of capsule size. In our case the mean diameter of the prepared microcapsules is found to be ∼45 μm which is quite satisfactory for the use in self-healing of material.
Surface morphology and size of the microcapsules were determined by SEM micrograph. Fig. 7 shows the SEM micrograph of microcapsules. It is clear from the micrograph that surface of microcapsules are rough which may be due to presence of UF nanoparticles protruding from the surface. The protuberant nanoparticle enhances the surface area of microcapsules offering better surface adhesion. The microcapsules were found to be spherical with average diameter of about 50 μm. Thickness of shell wall of microcapsules mainly depends on the manufacturing parameter which in turn determines the mechanical property of the microcapsules. Fig. 7(c) shows the wall thickness of a cracked microcapsule and Fig. 7(d) shows the SEM image of a microcapsule in a cross-section of prepared composite. In our study the wall thickness of the synthesized microcapsules were found to be 1.1 μm. The microcapsules are clearly visible in the matrix (Fig. 6(f)) which indicates that embedded microcapsules still maintain their integrity and are well adhered to the matrix without undergoing any damage during processing conditions. The inner surface of the microcapsule formed was found to be smooth and compact which allows easy flow of healing agent into the crack. SEM micrograph shows uniform dispersion of MWCNT–N3 in epoxy resin with few small remaining aggregates which are smeared out and well penetrated by the epoxy resin matrix (Fig. 7(e)).
Fig. 8(a) represents the FTIR spectra of the core material tripropargylpentaerythritol. The characteristic peaks includes 1715 cm−1, 2118 cm−1, 3286 cm−1 and 3450 cm−1 corresponding to
C
O, –C
C–, H–C
and –OH respectively. Fig. 8(b) represents characteristic absorption bands appear due to empty UF polymeric shells. The absorption peak appeared at 3381 cm−1 peak denotes –NH and –OH stretching. The stretching frequency at 1531 cm−1 corresponds to the N–H banding, 1374 cm−1 corresponding to C–H bending and a 1025 cm−1 stretching frequency was noted for –CO–NH. Fig. 8(c) represents the FTIR spectra for the tripropargylpentaerythritol loaded UF microcapsules which contains all the characteristic absorption peaks for both the core and shell materials confirming successful encapsulation.
Core content of the microcapsules were determined by solvent extraction. For this purpose some pre-weighted microcapsules were grinded in a mortar to crush it completely. It was then collected and washed with acetone several times to remove any core material. Finally the crushed microcapsules were collected and dried to constant weight. If the initial weight of the microcapsules is Wi and weight of the residual shell wall is Wf then % core content of the microcapsules (CW) can be given by:
Following this procedure the core content of the microcapsules was found to be 78%.
Thermal stability of microcapsules plays an important role in their applications as self-healing composite. Fig. 9 shows the TGA thermogram of core material, poly urea formaldehyde prepolymer and corresponding microcapsules. In the degradation pattern of UF-prepolymer, the weight loss below 200 °C is attributed to the gasification of small molecules such as water, formaldehyde and low molecular weight polymer. Major weight loss observed between 200 and 375 °C is attributed to the pyrolysis of the UF resin. Thermal degradation pattern of tripropargylpentaerythritol exhibits two step degradation patterns. First major weight loss occurs between 150 and 250 °C and second one occurs at 270–500 °C temperature range. Any weight loss below these temperatures is due to evaporation of water. As for the microcapsules, the weight loss below 150 °C is again attributed to the evaporation of adsorbed water and free formaldehyde. The degradation pattern almost resembles the degradation pattern of the core content of the microcapsules. The thermal stability of the microcapsules are slightly higher than the core material owing to the protection of the shield of the urea–formaldehyde wall. However thermogravimetric study resolves that the microcapsules are stable upto 150 °C only i.e. the thermostability of the microcapsules is considerably lower than the shell material which can be attributed to the lower thermal stability of the core material.
Tensile strength of neat cross-linked epoxy resins and that containing MWCNT–Br, catalyst and microcapsules were measured in accordance with ASTM-D3039 to access the inclusion of the ingredients. Zwik Roll (10KN) universal testing machine was used at a crosshead speed of 10 mm min−1 in room temperature. Three samples were tested in each case.
Fig. 10 shows the stress–strain curves of the tested samples of neat epoxy, epoxy loaded with MWCNT–t-BA–N3 and epoxy loaded with microcapsule, MWCNT–t-BA–N3 and catalyst. It was found that ultimate tensile strength and Young's modulus of the epoxy decreases on addition of functionalized MWCNT while flexibility increases substantially. This occurs due to inhomogeneous distribution of MWCNT and slippage of graphite layers of MWCNT. After incorporation of all the ingredients the ultimate tensile strength and Young's modulus increases substantially compared to the neat epoxy while elasticity decreases. It is due to the fact that shell material of the microcapsules i.e. urea–formaldehyde resin, is compatible with epoxy and considerably strong interfacial interaction occurs during curing. Although at high concentration of MWCNT homogenous dispersion is not possible which tend to decrease the tensile strength but at the same time the microcapsule hard walls are able to withstand some load transferred by the interface.
![]() | ||
| Fig. 10 Stress–strain curve for (a) epoxy + MWCNT, (b) epoxy + MWCNT + microcapsules, (c) neat epoxy (here MWCNT represents MWCNT–t-BA). | ||
Single-edge notched bending (SENB) test was performed to measure plane-strain fracture toughness and hence to evaluate self-healing ability of the prepared composites. In accordance with ASTM standard D5045-99, prior to testing a notch was precasted and then sharpened by tapping a fresh razor blade into the material. Three samples were tested in each condition. A loading rate of 10 mm min−1 was applied for the test. The original specimens were tested to failure, giving the fracture toughness, K0IC. It was then clamped together and heated in an oven at preset temperature allowing the healing process to occur. The healed specimens were then retested to yield the fracture toughness, K′IC. Accordingly, the healing efficiency of the prepared epoxy was calculated by using the formula:
| η = K′IC/K0IC × 100% |
A schematic representation of the self-healing process is presented in Scheme 2. Azide alkyne cycloaddition between the MWCNT–N3 in the epoxy matrix and tripropargylpentaerythritol from microcapsules in presence of CuBr(PPh3)3, as catalyst constitutes the healing mechanism. It can be visualized from the SEM micrograph of the composites that rough exterior shell wall of the microcapsules leads to formation of a three-part interphase consisting of thin continuous interior shell wall of the microcapsules, the rough exterior shell wall of the microcapsules and the continuous epoxy matrix. The epoxy matrix is well penetrated through the rough outside wall of the microcapsules promoting high possibility of capsule fracture, and hence increasing probability of healing agent delivery.
Fig. 11 shows the SEM image of a crack created by a sharp razor blade before and after healing (for 120 h at 100 °C). It is very clear from the figure that a successful healing of the crack was occurred.
![]() | ||
| Fig. 11 SEM micrograph showing a razor blade pre-notched composite before (a) and after (b) healing. | ||
Primarily crack healing efficiency of the prepared epoxy composite was evaluated for the sample cured up to 100 °C. Fig. 12 shows the fracture toughness of the virgin and cures epoxy resins and variation of healing efficiency with time at constant temperature of 100 °C. A maximum healing efficiency of 60.2% was obtained upon heating the samples to 120 h at this temperature. The healing efficiency shows an exponential increase with time which is due to the fact that more and more healent flow to the crack plane with time. From the fracture toughness measurement it was also found that virgin specimen is less brittle in nature compared to the healed specimen. It may be due to the deformation that occurs during the fracture testing of the virgin specimen which breaks some the microcapsules in the bulk leaching out the crosslinker which undergoes similar reaction as that of healing reaction. This will increase the crosslinking density and hence the brittleness.
![]() | ||
| Fig. 12 Flexural strength of prepared composites before and after healing at various times (a) and variation of healing efficiency with time at constant temperature of 100 °C (b). | ||
Fig. 13 shows the variation of healing efficiency with temperature. All the samples were allowed to heal at various temperatures for a constant amount of time (120 h). It is seen that healing efficiency increases with increasing temperature with two remarkable brakes in the curve. Below 60 °C healing efficiency was very low which increases stripy above this temperature. The healing efficiency between 60 and 130 °C shows almost constant behavior. Above this temperature healing efficiency rises again and reaches a maximum of 65%. This is due to the fact that above 60 °C the catalyst CuBr(PPh3)3 drives the azide–alkyne cycloaddition reaction increasing its efficiency. Again above 130 °C along with copper catalyzed reaction copper free azide alkyne cycloaddition reaction starts to occur which adds to the former to make the healing process more efficient. However further heating above 140 °C is irrelevant as microcapsules are not stable above this temperature as indicated by TGA thermogram. Although the azide alkyne cycloaddition can occur even at room temperature the application of high temperature fastens the healing process not only because of the increasing reaction rate but due to softening the composites bringing the two parts closer. High temperature also helps to solubilize the catalyst and poly(t-butyl acrylate)–N3 in the liquid crosslinker medium which plays an key role in the healing process.
To evaluate self-healing performance of our system a controlled experiment was performed without the inclusion of microcapsules in the epoxy matrix while enclosing both MWCNT–t-BA–N3 and CuBr(PPh3)3. Samples were broken to failure, clamped together and then heated at 140 °C for 120 h. However this control experiment showed no healing effects confirming that healing process originates solely due to azide alkyne cycloaddition reaction.
| This journal is © The Royal Society of Chemistry 2015 |