Influence of Matrix Polarity on the Properties of Ethylene Vinyl Acetate–Carbon Nanofiller Nanocomposites
© to the authors 2009
Received: 8 December 2008
Accepted: 5 March 2009
Published: 21 March 2009
A series of ethylene vinyl acetate (EVA) nanocomposites using four kinds of EVA with 40, 50, 60, and 70 wt% vinyl acetate (VA) contents and three different carbon-based nanofillers—expanded graphite (EG), multi-walled carbon nanotube (MWCNT), and carbon nanofiber (CNF) have been prepared via solution blending. The influence of the matrix polarity and the nature of nanofillers on the morphology and properties of EVA nanocomposites have been investigated. It is observed that the sample with lowest vinyl acetate content exhibits highest mechanical properties. However, the enhancement in mechanical properties with the incorporation of various nanofillers is the highest for EVA with high VA content. This trend has been followed in both dynamic mechanical properties and thermal conductivity of the nanocomposites. EVA copolymer undergoes a transition from partial to complete amorphousness between 40 and 50 wt% VA content, and this changes the dispersion of the nanofillers. The high VA-containing polymers show more affinity toward fillers due to the large free volume available and allow easy dispersion of nanofillers in the amorphous rubbery phase, as confirmed from the morphological studies. The thermal stability of the nanocomposites is also influenced by the type of nanofiller.
Ethylene vinyl acetate (EVA) is one of the important organic polymers, extensively used for electrical insulation, cable jacketing and repair, component encapsulation and water proofing, corrosion protection, and packaging of components. However, bulk EVA does not often fulfill the requirements in terms of its thermal stability and mechanical properties in some specific areas. Studies have been reported on the effect of electron beam irradiation on the mechanical properties and thermal stability of the EVA elastomer [1, 2]. Also, in order to improve various properties, nanoparticles are added as fillers. Various research investigations have been reported on the properties of nanoclay-filled EVA nanocomposites [3–5]. Costache et al.  have worked on the thermal degradation behavior of EVA–clay nanocomposites. Studies have been reported on the linear viscoelastic behavior of EVA-layered silicate nanocomposites [7, 8]. Effect of vinyl acetate (VA) content on the mechanical and thermal properties of EVA/MgAl-layered double hydroxide nanocomposites has been studied by various groups [9, 10]. Several studies have focussed on the influence of VA content on the dispersion of clay platelets, addition of external compatibilizers [11, 12], or the nature of the clay organo-modifier . Preparation and characterization of natural rubber (NR)/EVA blend–clay nanocomposites have also been reported in the literature . Silica nanoparticles prepared through the sol–gel mechanism by hydrolysis of tetraethoxysilane (TEOS) are found to improve the gas barrier properties of EVA–silica nanocomposites membranes .
EVA is a random copolymer consisting of ethylene and vinyl acetate as repeating units. VA content has two fundamental effects that influence the properties of EVA copolymers. The first effect is to disrupt the crystalline regions formed by the polyethylene segments of the copolymer. The second overriding effect of VA content results from the polar nature of the acetoxy side chain. The EVA shows various properties by varying the VA content. The properties of EVA depend on the crystallinity of the EVA [15–18], which can be controlled by the VA content.
Elastomers are proved to be very compatible matrices for carbon-based fillers. Several applications of rubbers might benefit from the incorporation of carbon nanofillers to form rubber-based nanocomposites. Studies have been carried out on the effect of carbon-based nanofillers on various properties of EVA thermoplastic elastomers having low VA content (25–32%), by melt mixing techniques [19–22]. From our laboratory, we have reported preliminary studies on the effect of various carbon-based nanofillers on the properties of elastomeric grade EVA [23–25]. However, there is no study carried out so far on the effect of VA content on the properties of these nanocomposites. Lee and Kim  describe the process of manufacturing nanocomposite material, which involves adding CNTs to improve EVA’s physical characteristics such as radiation resistance and thermal properties. Effect of MWCNT on the fire retardant and electromagnetic interference shielding properties of EVA has been investigated by various groups [22, 26]. Effect of VA content on the properties of MWCNT-filled thermoplastic elastomeric EVA nanocomposites has also been reported in the literature .
This study aims at evaluating the effect of the VA content in elastomeric grade EVA copolymers, on the dispersion states of three different carbon nanofillers: expanded graphite (EG), multiwalled carbon nanotubes (MWCNTs), and carbon nanofibers (CNFs) and also on the morphological, mechanical, dynamic mechanical, and thermal properties of the resulting nanocomposites. The effect of polarity of the EVA matrix on the extent of dispersion and distribution of the carbon-based nanofillers has been investigated by solution blending of 4 wt% of these three fillers with four EVA matrices containing 40, 50, 60, and 70% VA units. These studies have not been reported in the literature.
Four commercial ethylene vinyl acetate copolymer grades were supplied by Bayer (now Lanxess), Germany. The expanded graphite was procured from Asbury Graphite Mills Inc, NJ, USA. MWCNT was provided by Helix Material Solutions, TX, USA. CNF (as grown grade PR-24 AG, Pyrograf-III™) was obtained from Applied Sciences Inc., OH, USA. The dicumyl peroxide (DCP, 99% pure), cross-linker for the rubber, was obtained from Hercules India. Triallyl cyanurate (TAC), the co-crosslinker was procured from Fluka A G, Germany. Tetrahydrofuran (THF) of LR grade, used as the solvent for EVA was obtained from MERCK (India) Ltd., Mumbai, India.
Preparation of Nanocomposites
The nanocomposites were synthesized by using a solution-mixing technique. EVA (5 g per batch) was dissolved in 50 mL of THF to make 10% solution of the rubber using a mechanical stirrer. DCP (0.05 g) as the curing agent and 0.05 g of TAC as the co-agent were added to the rubber solution. The solution was thoroughly stirred using a mechanical stirrer. The nanofiller dispersed in THF was first sonicated for 15 min and subsequently added to the rubber solution while stirring at room temperature (27 °C). The final solution was cast over teflon trays and kept for air drying followed by vacuum drying at 50 °C, till there was practically no weight variation. The dried films were molded in a hot press at a pressure of 5 MPa at 150 °C for an optimum cure time of 25 min, determined from a Monsanto oscillating disc rheometer (ODR, 100S).
Sample designations for various nanocomposites
Virgin EVA elastomer with 40% VA content
Virgin EVA elastomer with 50% VA content
Virgin EVA elastomer with 60% VA content
Virgin EVA elastomer with 70% VA content
EVA filled with 4 wt% of EG
EVA filled with 4 wt% of MWCNT
EVA filled with 4 wt% of CNF
The microscopy was performed using a JEOL JEM-2010 (Japan), Transmission Electron Microscope (TEM) operating at an accelerating voltage of 200 kV. The composite samples were cut by ultra-cryomicrotomy using a Leica Ultracut UCT. Freshly sharpened glass knives with cutting edge of 45° were used to get the cryosections of 50–70 nm thickness. Since these samples were elastomeric in nature, the temperature during ultra-cryomicrotomy was kept at −50 °C (which was well below the glass transition temperature of EVA). The cryosections were collected individually on sucrose solution and directly supported on a copper grid of 300-mesh size.
Mechanical Property Analysis
The mechanical properties of the nanocomposites were evaluated by a universal testing machine (UTM, Zwick 1445) on dumbbell specimens, punched out from the cast films using an ASTM Die C. All the tests were carried out as per ASTM D 412-99 method at 25 ± 2 °C at a crosshead speed of 500 mm/min. The average values of three tests for tensile strength, tensile modulus, and elongation at break are reported for each sample.
where, Vr is volume fraction of rubber in the swollen gel, D the de-swollen weight of the composites, F the fraction insoluble, T the initial weight of the sample, and A0 the amount of solvent imbibed. ρr is the density of the rubber, while ρs is density of the swelling solvent.
Differential Scanning Calorimetry (DSC)
DSC of various samples was carried out by using a Q-100 DSC, of TA instruments, USA. The test was carried out in the temperature range −100 to +100 °C, with samples of 5 mg weight and the rate of heating/cooling was fixed at 10 °C/min in nitrogen.
Dynamic Mechanical Thermal Analysis (DMTA)
Dynamic mechanical thermal characteristics of the composite films (0.4–0.6 mm thick) were evaluated by using a DMTA IV (Rheometric Scientific) under tension mode. All the data were analyzed using RSI Orchestrator application software on an ACER computer attached to the machine. The temperature sweep measurements were made from −35 to 20 °C. The experiments were carried out at a frequency of 1 Hz at a heating rate of 2 °C/min. The storage modulus (E′) and the loss tangent (tan δ) data were recorded for all the samples under identical conditions.
whereW is the power in watts (here 4 W),K is the thermal conductivity,t the thickness of sample,A the area of the sample, and dT the temperature difference between the two plates.
Thermal Degradation Studies
Thermal stability of the composites was investigated by thermogravimetric analysis (TGA) by using a Perkin Elmer TGA instrument [Model: Pyris Diamond TG/DTA] from ambient to 800 °C at a programed heating rate of 20 °C/min in nitrogen. A sample weight of approximately 10 mg was taken for all the measurements. The weight loss against temperature was recorded. Differential thermogravimetric analysis (DTG) of the composites was represented in terms of the first derivative plots of the TGA curves. The data points denote the weight loss/time against temperature at the specified heating rate.
Results and Discussion
Tensile properties of EVA grades and their nanocomposites at 4 wt% filler loading
Tensile strength (MPa)
Elongation at break (%)
Modulus at 100% elongation (MPa)
8.36 ± 0.19
495 ± 15
1.31 ± 0.12
5.35 ± 0.12
440 ± 10
0.74 ± 0.11
5.24 ± 0.20
430 ± 10
0.57 ± 0.05
5.04 ± 0.17
410 ± 14
0.48 ± 0.07
9.32 ± 0.18
525 ± 12
2.39 ± 0.15
7.21 ± 0.14
435 ± 16
1.94 ± 0.08
7.51 ± 0.10
420 ± 10
2.05 ± 0.06
7.98 ± 0.15
410 ± 15
2.29 ± 0.12
8.95 ± 0.18
470 ± 15
2.56 ± 0.13
6.60 ± 0.12
370 ± 15
2.40 ± 0.09
6.68 ± 0.18
370 ± 16
2.42 ± 0.10
6.75 ± 0.20
375 ± 15
2.46 ± 0.10
11.10 ± 0.21
565 ± 20
3.13 ± 0.14
11.34 ± 0.12
400 ± 15
3.38 ± 0.11
11.45 ± 0.15
375 ± 13
3.65 ± 0.10
12.30 ± 0.16
380 ± 15
4.13 ± 0.15
The addition of expanded graphite and MWCNTs has significant reinforcing effect, the maximum improvement in tensile strength and modulus being shown by the high vinyl acetate grades of EVA50to EVA70and exhibits least increment for EVA40. This may be because of the easy dispersion of nanofillers in the rubbery phase and hence the high vinyl acetate grades disperse the fillers well. Addition of 4 wt% of EG enhances the tensile strength of EVA40by 11.5%, whereas MWCNT and CNF increase it by 7 and 32.8%, respectively. On the other hand, the increments are 58, 14, and 150%, respectively, in EVA70. The EVA40consists of more plastic (crystalline) phase and hence the nanofillers find it more difficult to disperse and hence form relatively more agglomerations, whereas in high vinyl acetate grades, the amount of free volume is more and hence the fillers can disperse relatively easily.
From the plots, it is clear that the reinforcing factor of EG and CNF increases in direct proportion with the VA content. The reinforcing effect of MWCNTs is lower. This might have resulted from relatively poor dispersion of MWCNT as compared to the other two fillers. It is to be noted that increment is more prominent in the partially amorphous to fully amorphous transition region which occurs beyond 50% VA content.
Solvent Swelling Analysis
Rubber volume fraction of EVA grades and their nanocomposites at 4 wt% filler
Volume fraction of rubber (Vr)
Differential Scanning Calorimetry
DSC studies of all the EVA copolymers and their nanocomposites have been carried out. On loading the nanofillers, there is marginal change in the enthalpy of melting (ΔHm) values with no change in the melting peak temperature. The percentage crystallinity of all the samples lies in the range 0.3–0.4%, thus confirming that all the nanocomposites are basically amorphous materials. It has been reported earlier that loading of carbon nanotubes reduces the crystallinity of EVA having 27% VA content (much lower than those used in the present investigation) due to the reduction in the orientation of polymer chains as a result of polymer–filler interaction . However, there is no such indication from the DSC traces for these amorphous polymers, as the ΔHm values are very low.
Dynamic Mechanical Thermal Analysis
DMTA data of EVA grades and their nanocomposites at 4 wt% filler loading
Storage modulus LogE’ (Pa) at
tan δ at
As expected, various nanocomposites exhibit much higher storage modulus than pure EVA grades, especially at low temperatures, given the reinforcing effect of nanofillers on the matrix. In addition, the presence of the fillers also enables the matrix to sustain high-modulus value at high temperatures. Also, various nanocomposites show a reduction in tan δ peak height as compared to those of respective neat elastomers. This is due to the restriction in polymer chain movements employed by the filler–polymer interactions.
The thermal conductivity of various nanocomposite samples has been analyzed in this section (Table 5 and Fig. 8). There is no significant difference among the thermal conductivity values of different EVA grades. Addition of 4 wt% of expanded graphite increases the thermal conductivity several folds over the neat elastomers. Increments are more prominent in the high VA-containing grades. Due to their inherent superior thermal conductivity, MWCNTs provide highest enhancement in thermal conductivity in various matrices. The thermal conductivity enhancement of polymer nanocomposites depends to a large extent on the thermal conductivity of nanoscale fillers and their structural properties . Even though CNF has higher aspect ratio, its intrinsic thermal conductivity is about 2000 W/mK which is much lower than that of MWCNT which is 3000 W/mK . In spite of the higher polymer–filler interaction revealed by Vr values, CNF-based composites register lower thermal conductivity values because of the above reason. Interfacial bonding between filler and polymer plays a vital role on the thermal conductivity of the resulting nanocomposites following earlier references . In the present case, however, the MWCNT shows a relatively poorer dispersion and also the swelling resistance is lower than that of CNF-based composites. It seems that there are many factors, including the thermal conductivity of the filler, important in determining the thermal conductivity of the composites.
Thermal conductivity data of various EVA nanocomposites at 4 wt% filler loading.
Thermal conductivity (W/mK)
Thermal degradation data of various EVA nanocomposites at 4 wt% filler loading
Maximum rate of degradation (%/°C)
Reinforcing effect of expanded graphite, multiwalled carbon nanotube, and carbon nanofiber on various elastomeric grades of EVA have been investigated and the effect of vinyl acetate content on various composite properties has been analyzed. The enhancements in mechanical, dynamic mechanical, and thermal properties indicate that the more elastomeric (VA content) the matrix is, the more easily the nanofillers get dispersed due to higher free volume. This effect is more prominent where the polymer achieves complete amorphousness which occurs between 40 and 50% VA content. Further increments in VA content did not bring about significant improvements in filler dispersion as evident from the TEM photographs. This effect is reflected in the enhancement in properties with the addition of nanofillers, though EVA40exhibits highest mechanical properties as compared to the higher VA-containing grades. This trend has been followed in both dynamic mechanical properties and thermal conductivity of the nanocomposites. The thermal degradation of the nanocomposites shows more dependence on the type of nanofiller rather than the VA content of EVA. Among the three nanofillers, expanded graphite provides maximum thermal stability.
The authors acknowledge the financial assistance provided by DRDO, New Delhi, India.
- Datta SK, Bhowmick AK, Chaki TK, Majali AB, Despande RS: Polymer (Guildf). 1996, 37: 45. COI number [1:CAS:528:DyaK28XhsVGisA%3D%3D] 10.1016/0032-3861(96)81598-9View ArticleGoogle Scholar
- Datta SK, Bhowmick AK, Mukunda PG, Chaki TK: Polym. Degrad. Stab.. 1995, 50: 75. 10.1016/0141-3910(95)00125-6View ArticleGoogle Scholar
- Pramanik M, Srivastava SK, Samantaray BK, Bhowmick AK: J. Appl. Polym. Sci.. 2003, 87: 2216. COI number [1:CAS:528:DC%2BD3sXhtFKnsbY%3D] 10.1002/app.11475View ArticleGoogle Scholar
- Pramanik M, Srivastava SK, Samantaray BK, Bhowmick AK: J. Polym. Sci. B Polym. Phys.. 2002, 40: 2065. COI number [1:CAS:528:DC%2BD38XmslChsL4%3D] 10.1002/polb.10266View ArticleGoogle Scholar
- Srivastava SK, Pramanik M, Acharya H: J. Polym. Sci. B Polym. Phys.. 2006, 44: 471. COI number [1:CAS:528:DC%2BD28XotFWqsA%3D%3D] 10.1002/polb.20702View ArticleGoogle Scholar
- Costache MC, Jiang DD, Wilkie CA: Polymer (Guildf). 2005, 46: 6947. COI number [1:CAS:528:DC%2BD2MXns1Sntbc%3D] 10.1016/j.polymer.2005.05.084View ArticleGoogle Scholar
- Prasad R, Gupta RK, Cser F, Bhattacharya SN: J. Appl. Polym. Sci.. 2006, 101: 2127. COI number [1:CAS:528:DC%2BD28XmvV2ku78%3D] 10.1002/app.22331View ArticleGoogle Scholar
- La Mantia FP, Dintcheva NT: Polym. Test.. 2006, 25: 701. 10.1016/j.polymertesting.2006.03.003View ArticleGoogle Scholar
- Zhang W, Chen D, Zhao Q, Fang Y: Polymer (Guildf). 2003, 44: 7953. COI number [1:CAS:528:DC%2BD3sXpt1KlsLc%3D] 10.1016/j.polymer.2003.10.046View ArticleGoogle Scholar
- Kuila T, Acharya H, Srivastava SK, Bhowmick AK: J. Appl. Polym. Sci.. 2008, 108: 1329. COI number [1:CAS:528:DC%2BD1cXisFymurc%3D] 10.1002/app.27834View ArticleGoogle Scholar
- Suh IS, Ryu SH, Bae JH, Chang YW: J. Appl. Polym. Sci.. 2004, 94: 1057. COI number [1:CAS:528:DC%2BD2cXot12lsrg%3D] 10.1002/app.20962View ArticleGoogle Scholar
- Jeon CH, Ryu SH, Chang YW: Polym. Int.. 2003, 52: 153. COI number [1:CAS:528:DC%2BD3sXhtlCgt70%3D] 10.1002/pi.1066View ArticleGoogle Scholar
- Sharif J, Yunus WMZW, Dahlan KH, Ahmad MH: J. Appl. Polym. Sci.. 2006, 100: 353. COI number [1:CAS:528:DC%2BD28XitVOlsL0%3D] 10.1002/app.23121View ArticleGoogle Scholar
- Sadeghi M, Khanbabaei G, Dehaghani AHS, Sadeghi M, Aravand MA, Akbarzade M, Khatti S: J. Membr. Sci.. 2008, 322: 423. COI number [1:CAS:528:DC%2BD1cXptlemt7k%3D] 10.1016/j.memsci.2008.05.077View ArticleGoogle Scholar
- Brogly M, Nardin M, Schultz J: J. Appl. Polym. Sci.. 1997, 64: 1903. COI number [1:CAS:528:DyaK2sXivVyhurY%3D] 10.1002/(SICI)1097-4628(19970606)64:10<1903::AID-APP4>3.0.CO;2-MView ArticleGoogle Scholar
- Arsac A, Carrot C, Guillet J: J. Appl. Polym. Sci.. 1999, 74: 2625. COI number [1:CAS:528:DyaK1MXmslKhsL8%3D] 10.1002/(SICI)1097-4628(19991209)74:11<2625::AID-APP9>3.0.CO;2-GView ArticleGoogle Scholar
- Bistac S, Kunemann P, Schultz J: Polymer (Guildf). 1998, 39: 4875. COI number [1:CAS:528:DyaK1cXltVens7s%3D] 10.1016/S0032-3861(97)10328-7View ArticleGoogle Scholar
- Gospodinova N, Zlatkov T, Terlemezyan L: Polymer (Guildf). 1998, 39: 2583. COI number [1:CAS:528:DyaK1cXisVOntLc%3D] 10.1016/S0032-3861(97)00558-2View ArticleGoogle Scholar
- Peeterbroeck S, Lepoittevin B, Pollet E, Benali S, Broekaert C, Alexandre MD, Viville PB, Lazzaroni R, Dubois P: Polym. Eng. Sci.. 2006, 46: 1022. COI number [1:CAS:528:DC%2BD28XnvFyksbg%3D] 10.1002/pen.20560View ArticleGoogle Scholar
- Peeterbroeck S, Alexandre M, Nagy JB, Pirlot C, Fonseca A, Moreau N, Philippin G, Delhalle J, Mekhalif Z, Sporken R, Beyer G, Dubois P: Compos. Sci. Technol.. 2004, 64: 2317. COI number [1:CAS:528:DC%2BD2cXnsVGhsrw%3D] 10.1016/j.compscitech.2004.01.020View ArticleGoogle Scholar
- Lee K-Y, Kim K-Y: Polym. Degrad. Stab.. 2008, 93: 1290. COI number [1:CAS:528:DC%2BD1cXnt1Oqs74%3D] 10.1016/j.polymdegradstab.2008.04.007View ArticleGoogle Scholar
- Peeterbroeck S, Laoutid F, Swoboda B, Lopez-Cuesta J-M, Moreau N, Nagy JB, Alexandre M, Dubois P: Macromol. Rapid Commun.. 2007, 28: 260. COI number [1:CAS:528:DC%2BD2sXisVyitb0%3D] 10.1002/marc.200600614View ArticleGoogle Scholar
- George JJ, Sengupta R, Bhowmick AK: J. Nanosci. Nanotechnol.. 2008, 8: 1913. COI number [1:CAS:528:DC%2BD1cXmslWku7k%3D] 10.1166/jnn.2008.024View ArticleGoogle Scholar
- George JJ, Bhowmick AK: J. Mater. Sci.. 2008, 43: 702. ; COI number [1:CAS:528:DC%2BD2sXhsVaqurvM]; Bibcode number [2008JMatS..43..702G] 10.1007/s10853-007-2193-6View ArticleGoogle Scholar
- George JJ, Bhowmick AK: Nanoscale Res. Lett.. 2008, 3: 508. ; COI number [1:CAS:528:DC%2BD1cXhsVyhtrjF]; Bibcode number [2008NRL.....3..508G] 10.1007/s11671-008-9188-3View ArticleGoogle Scholar
- Das NC, Maiti S: J. Mater. Sci.. 2008, 43: 1920. ; COI number [1:CAS:528:DC%2BD1cXhslemu7Y%3D]; Bibcode number [2008JMatS..43.1920D] 10.1007/s10853-008-2458-8View ArticleGoogle Scholar
- Peeterbroeck S, Breugelmans L, Alexandre M, Nagy JB, Viville P, Lazzaroni R, Dubois P: Compos. Sci. Technol.. 2007, 67: 1659. COI number [1:CAS:528:DC%2BD2sXjtVaqt7k%3D] 10.1016/j.compscitech.2006.07.001View ArticleGoogle Scholar
- Sadhu S, Bhowmick AK: J. Polym. Sci. B Polym. Phys.. 2004, 42: 1573. COI number [1:CAS:528:DC%2BD2cXjsV2hsrc%3D] 10.1002/polb.20036View ArticleGoogle Scholar
- Henderson AM: IEEE Electr. Insul. Mag.. 1993, 9: 30. 10.1109/57.249923View ArticleGoogle Scholar
- Miltner HE, Peeterbroeck S, Viville P, Dubois P, Vanmele B: J. Polym. Sci. B Polym. Phys.. 2007, 45: 1291. COI number [1:CAS:528:DC%2BD2sXlsV2mt7w%3D] 10.1002/polb.21193View ArticleGoogle Scholar
- Yang Y, Gupta MC, Zalameda JN, Winfree WP: Micro & Nano Lett. 2008,3(2):35. COI number [1:CAS:528:DC%2BD1cXhtFemsbrE] 10.1049/mnl:20070073View ArticleGoogle Scholar
- Al-Saleh MH, Sundararaj U: Carbon. 2009, 47: 2. COI number [1:CAS:528:DC%2BD1cXhsVChsbfN] 10.1016/j.carbon.2008.09.039View ArticleGoogle Scholar
- Huxtable ST, Cahill DG, Shenogin S, Xue L, OZisik R, Barone P, Usrey M, Strano MS, Siddons G, Shim M, Keblinski P: Nat. Mater.. 2003, 2: 731. ; COI number [1:CAS:528:DC%2BD3sXosFWrtLY%3D]; Bibcode number [2003NatMa...2..731H] 10.1038/nmat996View ArticleGoogle Scholar