Baljinder K. Kandola*,
Latha Krishnan,
Dario Deli†
,
Piyanuch Luangtriratana and
John R. Ebdon
Fire Materials Group, Institute for Materials Research and Innovation (IMRI), University of Bolton, Deane Road, Bolton, BL3 5AB, UK. E-mail: b.kandola@bolton.ac.uk
First published on 2nd April 2015
A novel phenolic novolac resin bearing methacrylate functional groups has been synthesized by reaction of the novolac with methacryloyl chloride. This resin has been mixed with styrene and cured (crosslinked) free-radically under the relatively low temperature conditions used to cure unsaturated polyester/styrene mixtures, i.e. there is no need to employ the high temperatures and pressures that are required to cure conventional phenolic resins. Homogeneous cured blends of the methacrylated novolac with unsaturated polyester and styrene have been prepared also. The cured methacrylated novolac, and its blends with unsaturated polyester, are rigid materials with good mechanical strength, and have glass transition temperatures, thermal stabilities and flame retardancies superior to those of cured unsaturated polyester alone.
While different types of phenolic resins are available, classical resole and novolac types dominate the resin market. Phenol–formaldehyde (P/F) molar ratio and catalyst type (acid/alkali) used to synthesize a resin determines the resole/novolac resin type.6 Resins produced with P/F < 1 and alkaline catalyst are referred to as resoles. Resoles contain reactive methylol or dimethylene–ether linkages and can be cured by applying heat. Novolacs on the other hand are synthesized using P/F > 1 under acidic conditions and consist of phenol rings connected solely by methylene bridges. Novolac resins are thermally cured by addition of a methylene crosslinker such as hexamethylenetetramine.7,8 Resoles, being liquids, are easy to handle, hence are preferred for fibre-reinforced composites. Novolacs on the other hand are stable, thermoplastic, solid resins, and are preferred for moulding materials or as a component of other systems such as of epoxies. However, both resin types, on curing, produce highly cross-linked thermally stable networks, which on exposure to high heat or fire char so producing relatively low levels of combustible volatiles; hence their flammabilities are lower than those of epoxies and unsaturated polyester resins.
In our on-going research at Bolton we are exploring blending different phenolic resins with unsaturated polyester resin to reduce the flammability of the latter while maintaining its physical and mechanical properties for potential use in marine composites.4,9–12 We have adopted this approach to improving the fire retardance and also the mechanical properties of cured UP resins, rather than use perhaps more obvious strategies, such as adding a non-combustible inorganic filler, in order to preserve the low viscosity of the uncured resin, which is necessary if composite laminates are to be prepared from these resins by pressurized resin infusion, a method commonly used for the preparation of composite laminate components in the marine industry. While resin blending is well-established for thermosetting resins with compatible cure chemistries, such as epoxy and phenolic resins,13 it is challenging for incompatible systems such as UP and phenolics, owing to the inherent physical incompatibility of relatively hydrophobic UP resins with relatively hydrophilic formaldehyde-based resins, and also to the fact that the former cure by a low-temperature (typically 40–80 °C) free-radical chain reaction whereas the latter cure via a high temperature (ca. 150 °C) polycondensation, often with an acid catalyst.9,10,14,15 We have done extensive work on resole phenolic–UP blends4,9–12 and overcame these problems by compatibilizing resoles using different approaches: (i) the use of a common solvent (ethanol), (ii) using an external compatibilizer (epoxy functionalised phenolic resin) and (iii) chemical functionalization of at least one of the components of the blend (use of an allyl functionalized phenolic resin). These compatibilized, co-cured, resin blends are significantly more flame retardant than unmodified UPs, burn with lower evolution of heat and the formation of more char, have physical and mechanical properties that are superior to those of unmodified UPs, and can satisfactorily be used to make glass-reinforced composite panel.4,10–12 Of the modified resoles, that bearing allyl groups (a commercial Methylon resin) was found to be the most satisfactory in forming homogeneous blends with UP owing to the chemical incorporation of at least some of the allyl groups into the free-radically crosslinked network structure. However, allyl-functional resoles are designed primarily to be used as high temperature self-curing surface coating materials and, in our formulations, a high temperature post-curing process is still required to give dimensionally stable materials (i.e. to condense residual methylol groups in the resole and to complete polymerization of the allyl groups).4,10
In this paper we report the chemical modification of a PH novolac, i.e. a phenolic resin with no free methylol groups, with methacryloyl chloride to introduce methacrylate groups. These groups too were expected to aid miscibility of the PH resin with UP/styrene but to be more reactive in free-radical reactions than allyl groups and so permit the PH novolac to be free-radically cured with styrene and in blends with UP/styrene under conditions similar to those used for UP/styrene alone, i.e. room temperature for 24 h and post curing at 80 °C for 6 h.
Surprisingly there seems to have been relatively little work before to modify phenolic resins so as to enable them to take part in free-radical polymerization reactions, although acrylate and methacrylate functional epoxy novolacs, made by ring-opening reactions of epoxy groups in the novolac with acrylic or methacrylic acid, have been known for 50 years16 and are used extensively today in photocurable surface coatings and inks.17 Also there are reports of phenolics modified so as to contain vinyl benzyl and maleimide groups, also capable of being free radically polymerized.18,19
Catalyst M, Scott-Bader: a free-radical catalyst for UP curing consisting of methyl ethyl ketone peroxide dissolved in methyl ethyl ketone.
Accelerator G, Scott Bader: 1% by weight cobalt(II) octoate dissolved in styrene.
Durez 31459, Sumitomo Bakelite Europe N.V.: a phenolic novolac resin (Nov), MW = 2500.
Triethylamine (TEA), styrene and di-methyl aniline (DMA), TCI Europe.
Methacryloyl chloride (MC) and anhydrous tetrahydrofuran (THF), Aldrich.
The recovered TEA·HCl was washed with THF (3 × 20 ml) and dried in a vacuum oven for 24 hours at 80 °C. The dried TEA·HCl was weighed in order to determine the yield and thus indirectly the extent of methacrylation. One ml of the organic solution containing the M-Nov was evaporated in an oven at 100 °C for 24 h in order to calculate the solid content and provide a true measure of yield. THF was then evaporated off under vacuum from the remaining solution of M-Nov at a temperature below 60 °C. Styrene (26 g) was added to the mixture, which was stirred at high shear and cooled to RT.
Yields: 76.6 g of TEA·HCl, corresponding to 98% conversion of novolac to methacrylated novolac (77.9 g being the theoretical amount of TEA·HCl produced for 100% methacrylation of phenolic groups in the novolac); 80.9 g of M-Nov, corresponding to 99% methacrylation. The characterization of the resin by IR and NMR spectroscopy both before and after methacrylation is discussed later.
ROOH + Co2+ → RO˙ + HO− + Co3+ |
Di methyl-aniline also catalyses the decomposition of MEK peroxide.
Resin blends were prepared by mixing 70:
30 and 50
:
50% w/w UP/M-Nov for 10 min in a 100 ml beaker using a high-speed, overhead, electric stirrer fitted with a four-component blade (IKA RW16 at 900 rpm). Catalyst M (2% by weight w.r.t. resin blend) was then added to the resin mixtures and stirring continued for a further 10 min. The resulting mixtures were transferred to moulds and cured in the same way as for the pure resins. The appropriateness of the curing regimes outlined above was established by differential scanning calorimetric (DSC) studies of curing, the results of which are given in a later section.
Proton NMR spectra were recorded on solutions of Nov and M-Nov in acetone on a Bruker Avance 400 spectrometer at the University of Manchester. Solid-state C13 NMR spectra of cured samples of M-Nov, UP and UP/M-Nov blends were recorded on a Bruker Avance III HD spectrometer courtesy of the EPSRC-funded, University of Durham solid-state NMR service.
Differential scanning calorimetry (DSC) was used to monitor the curing of resin samples (2–10 mg) at a heating rate of 5 °C min−1 over the temperature range 30–350 °C using a TA Instruments Q2000 differential scanning calorimeter.
Dynamic mechanical thermal analysis (DMTA) was carried out on a TA Instruments Q800 DMA machine using a single cantilever clamp and multi-frequency-strain set-up (0.1% strain and 1 Hz frequency). The specimens were heated at 10 °C min−1 within the temperature range 30–350 °C. Values of tanδ and storage modulus were recorded.
Scanning electron microscopy (SEM) was performed on small samples of cured, cast resins previously fractured in simple bending experiments, and the fracture surfaces then gold coated using a Polaron Range SC7620 Sputter Coater with 60 s plasma exposure. The coated fracture surfaces were examined using an Hitachi S-3400N variable pressure scanning electron microscope.
A cone calorimeter (Fire Testing Technology Ltd) was used to assess flammability parameters for cured resins according to ISO 5660 standard with the exception of sample size. Circular samples of cured resins measuring 5.5 cm dia. with a nominal thickness of 3 mm, were fire tested in the horizontal mode with an ignition source at an applied heat flux of 50 kW m−2. Before testing, the bottom surface and the edges of the samples were wrapped with aluminium foil to ensure that only the top surface would be directly exposed to the heat source. A minimum of three tests were performed for each formulation. Previously in our laboratories, a comparative study of the cone calorimetric behaviour of round and standard square (10 cm × 10 cm) samples was undertaken in order to understand the effect of geometry on flammability properties of polymeric materials.20 Circular specimens with a four-fold reduction in area gave similar results for the peak heat release rates (PHRR), total heat release (THR) and effective heat of combustion (EHC). Smoke, CO and CO2 production results were found to be different from those measured for the larger specimens since these parameters are independent of exposed specimen surface area. However, in this work, these data were used for comparison purposes only with respect to control specimens, hence there was no need for adjustments.
The ATR spectrum of M-Nov provides clear evidence for the presence of methacrylate groups with characteristic peaks at 1730 cm−1 (CO stretch) and 1635 cm−1 (C
C stretch).23,24 In addition, the disappearance of the hydroxyl peak at 3310 cm−1 in the spectrum of M-Nov indicates the complete reaction of phenolic OH with methacryloyl chloride.
The DSC trace of uncured M-Nov, containing 32% by weight of styrene as the crosslinking monomer, plus Catalyst M, Accelerator G and dimethyl aniline as the initiator system, exhibits a curing exotherm similar to that of UP/styrene (Fig. 6(a)), as do those of the UP/M-Nov/styrene blends (Fig. 6(b)). This suggests that M-Nov/styrene cures in a manner analogous to UP/styrene, and that UP/M-Nov blends co-cure in a similar, single process. Reruns of the (now cured) samples on the DSC (also shown in Fig. 6(a) and (b)) give essentially flat traces, showing that curing is complete after the first programmed temperature run. The exotherm onset and peak temperatures, Tonset and Tpeak, and the areas under the exotherms (i.e. enthalpies of curing) for UP/styrene, M-Nov/styrene and the blends with styrene are listed in Table 1; the figures in parentheses are enthalpies of curing for blends calculated using eqn (1), assuming that these will be the mass averages of the values for the pure blend components. The enthalpy of curing for M-Nov/styrene is 222 J g−1 i.e. lower than that for UP/styrene (282 J g−1),10 similarly Tpeak for the M-Nov/styrene is 13 °C lower than that for UP/styrene; this latter feature may be a consequence of the expected greater reactivity in free-radical polymerization of the pendent, methacrylate, double bonds of M-Nov compared with the in-chain, olefinic, double bonds of the maleate units of UP. The data in Table 1 indicate that it is appropriate to cure M-Nov and blends of M-Nov with UP under conditions similar to those established for UP alone, i.e. 24 h at RT plus 6 h at 80 °C.10
Pblend = (PUP × mUP) + (PM-Nov × mM-Nov) | (1) |
Sample | DSC | DMTA | |||
---|---|---|---|---|---|
Tonset/°C | Tpeak/°C | Enthalpy of cure/J g−1 | Storage modulus at RT/MPa | Tg/°C | |
a Note: the enthalpies in parentheses are mass-average values calculated from those of the components using eqn (1). | |||||
M-Nov | 49 | 67 | 222 | 2130 | 182 |
UP | 30 | 82 | 282 | 2657 | 92 |
UP/M-Nov:80/20 | 35 | 60 | 271 (270) | 2860 | 116 |
UP/M-Nov:70/30 | 36 | 55 | 262 (264) | 3250 | 123 |
UP/M-Nov:60/40 | 36 | 60 | 266 (258) | 3011 | 125 |
UP/M-Nov:50/50 | 44 | 59 | 258 (252) | 2591 | 126 |
The blends also show single tanδ vs. T maxima indicating single Tg values and hence good miscibility. This implies that the resin blends behave as single homogeneous materials (effectively terpolymers) and that M-Nov can be co-cured to form a single continuous network with UP and styrene. As expected, the Tg values of the blends are between those of the individual resins (92 °C for UP and 182 °C for M-Nov), and increase as the amount of M-Nov in the blend is increased. However, the Tgs of the 70/30, 60/40 and 50/50 blends of UP/M-Nov are unexpectedly similar and not in accordance with the Fox equation, from which we would expect the Tg of a blend to be clearly dependent upon the weight fractions of the components.28 This may be due to differences in crosslink density and/or to slight compositional heterogeneity, as discussed below.
The overall compositions of these network blends will be the same as the compositions of the mixtures from which they have been made, given that polymerization and crosslinking is taken to maximum conversion. However, the compositions will undoubtedly drift during the polymerization and crosslinking process owing to expected differences in the reactivity ratios of the component species. Reactivity ratios of M-Nov and UP with each other and with other monomers are not known, but if we take diethylmaleate (DEM) to be a model for the polymerizable groups in UP and methyl methacrylate (MMA) to be a model for M-Nov, then the relevant reactivity ratio pairs have been reported to be: MMA/DEM = 354/0;29 MMA/styrene = 0.50/0.54;30 styrene/DEM = 6.592/0.001.31 From these pairs we can see that we would expect M-Nov to be reacted into the network much more readily than UP, giving a partial product richer in M-Nov at the outset of the polymerization and crosslinking process. This could lead to microscale heterogeneity within the fully crosslinked network but, if so, this heterogeneity is clearly not sufficient to cause significant phase separation and hence the observation of more than one Tg.
Also obtainable from the DMTA data are the storage moduli of the cured resins and resin blends; these are shown as a function of T in Fig. 7(b), with values at RT (25 °C) listed in Table 1. The variation of the storage modulus with temperature is mainly used to assess the likely retention of mechanical strength at high temperature. A material displaying a relatively slow decrease in modulus with increasing temperature will perform better at higher temperatures than one in which the modulus declines sharply.
In these respects, it can be seen from Table 1 and Fig. 7(b) that cured M-Nov has a modulus lower than that of cured UP at RT (indicating that it is a softer material than cured UP at this temperature) but retains this modulus more effectively at higher temperatures than does UP. Particularly noteworthy are the performances of the cured 80/20, 70/30 and 60/40 UP/M-Nov blends, all of which show superior storage moduli over the whole temperature range compared with that of cured UP, and indeed higher moduli than that of cured M-Nov. The reason for this latter feature is not clear but may, like the trend in Tgs, be a reflection of different extents of curing of the various resins.
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Fig. 8 SEM photomicrographs of fractured surfaces of cured M-Nov, UP and 70/30 and 50/50 UP/M-Nov blends. |
Sample | LOI/vol% O2 | ΔLOI (increase over that of UP) |
---|---|---|
a Note: the LOI values in italics are calculated mass-average values using eqn (1). | ||
M-Nov | 21.3 ± 0.1 | 3.4 |
UP | 17.9 ± 0.1 | 0 |
UP/M-Nov:80/20 | 19.0 ± 0.1 (18.6) | 1.1 |
UP/M-Nov:70/30 | 19.1 ± 0.2 (18.9) | 1.2 |
UP/M-Nov:60/40 | 19.5 ± 0.1 (19.3) | 1.6 |
UP/M-Nov:50/50 | 19.7 ± 0.1 (19.6) | 1.8 |
Sample | TTI/s | FO/s | PHRR/kW m−2 | THR/MJ m−2 | TSR/m2 m−2 | CY/% | FPI/kW−1 m2 s | FIGRA/kW m−2 s−1 |
---|---|---|---|---|---|---|---|---|
a Notes: (1) the probable errors for the cone parameters are: TTI ± 2; PHRR ± 33; THR ± 2.1; TSR ± 133 and CY ± 1.3. (2) FPI = TTI/PHRR; FIGRA = PHRR/TPHRR. (3) The negative numbers in parentheses are the percentage reductions in values with respect to those for UP. | ||||||||
M-Nov | 41 | 202 | 801 (−29) | 61 (−27) | 3512 (−27) | 19.7 | 0.051 | 8.09 |
UP | 38 | 178 | 1130 | 83 | 4813 | 1.9 | 0.034 | 10.09 |
UP/M-Nov:80/20 | 39 | 178 | 988 (−13) | 70 (−16) | 4103 (−15) | 5.7 | 0.039 | 10.74 |
UP/M-Nov:70/30 | 39 | 181 | 932 (−18) | 68 (−18) | 3909 (−19) | 7.6 | 0.042 | 9.23 |
UP/M-Nov:60/40 | 38 | 183 | 892 (−21) | 66 (−21) | 3815 (−21) | 9.7 | 0.043 | 9.39 |
UP/M-Nov:50/50 | 39 | 187 | 840 (−26) | 64 (−23) | 3623 (−25) | 12.4 | 0.046 | 8.66 |
The PHRR, THR, TSR and CY values for the UP/M-Nov 80/20, 70/30, 60/40 and 50/50 blends all lie between those of the pure components, as expected. However, the relationships between PHRR, THR, TSR and blend composition are not linear ones, with the incorporation of even small relatively amounts of M-Nov in UP having a disproportionately advantageous effect on these parameters. A possible reason for this feature is presented and discussed in a later section.
It is interesting to compare the cone calorimetric parameters for the UP/M-Nov blends with those recorded previously for blends of UP with Methylon (an allyl-functional resole that was found to co-cure to a limited extent with UP/styrene) of similar composition.4 For UP/Methylon:50/50, for example, PHRR was 800 kW m−2, THR was 61 MJ m−2, TSR was 3170 m2 m−2 and char yield was 14% w/w; for UP/M-Nov:50/50, the corresponding data are 840 kW m−2, 64 MJ m−2, 3623 m2 m−2 and 12.4% w/w, i.e. very similar to the results for the UP/allyl-resole blend. There is a similar close correspondence too for the data for the two 50/50 blends. Thus, from the point of view of their flame retardance, UP/M-Nov blends perform as well as UP/Methylon blends. This is particularly encouraging given that, prior to curing, extra styrene was added to the UP/M-Nov blends to give an overall concentration of styrene in the blended resin of about 35% w/w, whereas for the UP/Methylon blends, no extra styrene is added over that which is already present in the UP. So, for example, the UP/Methylon:50/50 blend contains only about 18% w/w styrene (a particularly flammable component).
The UP/M-Nov blends are also ranked with two other fire parameters, FPI and FIGRA, listed in Table 3. The fire performance index, FPI, is derived from TTI/PHRR. The fire growth rate, FIGRA is maximum quotient of HRR(t)/TPHRR, which often equals to PHRR/TPHRR in a cone calorimeter. From the point of view of flame retardancy, materials with higher FPI are preferred over materials with lower FPI because of the greater fire risks associated with the latter. From Table 3, it can be seen that the FPI values of UP/M-Nov blends increase with increasing M-Nov content, indicating that UP/M-Nov blends pose a lower fire risk than UP.
FIGRA is associated with the burning propensity of a material. From Table 3 it can be seen also that the FIGRA values of UP/M-Nov blends are lower than that of UP, indicating slower fire growth in the blends once ignition has occurred.
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Fig. 9 TGA traces in nitrogen (a1) and air (a2), DTG traces in nitrogen (b1) and air (b2), and DTA traces in nitrogen (c1) and air (c2) for cured M-Nov, UP and UP/M-Nov blends. |
Sample | Temp. range/°C | Mass loss/% | DTG max/°C | DTA peak max/°C | Residue at 525 °C/% |
---|---|---|---|---|---|
M-Nov | RT–246 | 0.9 | 431 | 152 (exo) | 28.7 |
246–567 | 72.3 | 432 (endo) | |||
UP | RT–183 | 0.9 | 383 | 2.5 | |
183–462 | 94.8 | 369 (endo) | |||
UP/M-Nov:80/20 | RT–206 | 0.7 | 403 | 174 (exo) | 7.9 |
206–503 | 90.8 | 386 (endo) | |||
UP/M-Nov:70/30 | RT–213 | 0.8 | 406 | 174 (exo) | 10.2 |
213–516 | 88.8 | 380 (endo) | |||
UP/M-Nov:60/40 | RT–223 | 0.7 | 411 | 174 (exo) | 12.9 |
223–516 | 86.7 | 380 (endo) | |||
UP/M-Nov:50/50 | RT–231 | 1.1 | 414 | 173 (exo) | 13.7 |
231–537 | 85.6 | 371 (endo) |
Sample | Temp. range/°C | Mass loss/% | DTG max/°C | DTA peak max/°C | Residue at 525 °C/% |
---|---|---|---|---|---|
a Note: s = small shoulder peak. | |||||
M-Nov | RT–295 | 2.7 | 35.3 | ||
295–489 | 55.7 | 422 | 427 (endo) | ||
489–601 | 41.2 | 563 | 561 (exo) | ||
UP | RT–183 | 0.9 | 2.8 | ||
183–435 | 93.1 | 373 | 352 (endo):404 (exo) | ||
435–566 | 5.6 | 532 | 533 (exo) | ||
UP/M-Nov:80/20 | RT–206 | 1.4 | 355 (endo) | 9.5 | |
206–459 | 84.5 | 381 | 425 (exo) | ||
459–599 | 14.1 | 540 | 538 (exo) | ||
UP/M-Nov:70/30 | RT–251 | 2.1 | 377 (endo) | 14.8 | |
251–472 | 78.3 | 371, 411 (s) | 397 (exo), 441 (s, exo) | ||
472–593 | 19.2 | 522 | 553 (exo) | ||
UP/M-Nov:60/40 | RT–251 | 2.3 | 368 (endo) | 15.2 | |
251–475 | 75.3 | 370, 404 (S) | 391 (s, exo), 423 (exo) | ||
475–596 | 22.1 | 548 | 545 (exo) | ||
UP/M-Nov:50/50 | RT–251 | 2.4 | 348 (endo) | 19.1 | |
251–477 | 70.7 | 372, 413 (S) | 392 (exo) | ||
477–594 | 26.7 | 543 | 541 (exo) |
It can be seen from Fig. 9(a1) and (b1), and Table 4 that cured M-Nov exhibits a single stage mass loss under nitrogen between 246 °C and 567 °C, with peak rate (DTG max) at 431 °C, leaving a residual mass of 28.7% at 525 °C. Associated with this mass loss is an endothermic DTA peak at 432 °C arising from the volatilization of the degradation products. The small exothermic DTA peak at 152 °C probably arises from some slight further curing of M-Nov during the DTA run. This overall behaviour of M-Nov is similar to that of UP, but cured M-Nov is significantly more thermally stable than cured UP, which degrades almost completely in a single stage between 183 and 462 °C, leaving a residue of only 2.5%. The cured UP/M-Nov blends also show single stage mass loss over temperature ranges intermediate between those observed for cured M-Nov and cured UP e.g. 90.8% mass loss between 206 and 503 °C for UP/M-Nov:80/20 and 85.6% mass loss between 231 and 537 °C for UP/M-Nov:50/50. We take this pattern of behaviour to indicate further the homogeneous nature of the blends, i.e. they behave as single polymeric materials with uniform chemical composition throughout. This behaviour is in marked contrast to that which we previously observed for cured blends of UP with some commercial phenolic resoles; these thermally decomposed in two or more stages indicating significant domains of pure UP and pure phenolic in phase-separated structures.4 The small mass losses that can be seen for the various samples between RT and the onset of the major degradation process (e.g. 0.9% for M-Nov and 1.1% for UP/M-Nov:50/50) almost certainly arise from the volatilization of small amounts of solvent, residual monomer and other low molar mass fragments in the materials.
When thermal degradation of the samples is carried out in air, two major regions of mass loss are seen for all the samples (see Fig. 9(a2), (b2) and (c2) and Table 5). The first region in each case (e.g. between 295 and 489 °C for M-Nov and between 251 and 477 °C for UP/M-Nov:50/50) corresponds to thermal and thermo-oxidative degradation of the original polymer, whilst the second (e.g. between 489 and 601 °C for M-Nov, and between 477 and 594 °C for UP/M-Nov:50/50) corresponds to the thermo-oxidative degradation of the otherwise thermally stable residue formed during the first degradation process (what can be termed a char oxidation stage). Both these regions of mass loss in all but pure M-Nov are accompanied by significant exothermic DTA peaks (Fig. 9(c2)), characteristic of exothermic oxidation processes (e.g. at 392 and 541 °C for UP/M-Nov:50/50, 397 and 553 °C for UP/M-Nov:70/30, and 404 and 533 °C for UP). These exotherms overwhelm the endothermic peaks that would be expected from volatilization of degradation products. Only in M-Nov is a single exotherm seen, probably indicating the greater oxidative stability of M-Nov and the products of its thermal decomposition compared with those of UP, leading to the exothermic peak corresponding to oxidation matching in size the endothermic peak corresponding to volatilization of degradation products.
Comparison of the residual masses for the various samples under nitrogen and air at 525 °C is also informative. Whereas in UP the residual mass at 525 °C in air is only marginally greater than in nitrogen (2.8% vs. 2.5%), for M-Nov the difference is much more marked (35.3% in air and 28.7% in nitrogen). The residual mass differences in air and nitrogen for the blends are intermediate between those of UP and M-Nov. This too is an indication of the greater thermo-oxidative stability of M-Nov compared with UP in that the residue remaining after the major stage of thermal decomposition initially gains mass through oxidation (replacement of H by O) before finally oxidatively degrading above 525 °C; in all samples, no mass remains in air above 600 °C.
In order to see whether or not blends of M-Nov and UP are more or less thermally and thermo-oxidatively stable than might be expected on the basis of their compositions and the behaviours of pure M-Nov and UP, mass-averaged mass loss curves have been calculated for the blends using eqn (1). The differences between experimental mass losses and calculated mass losses for all blends are plotted against T in Fig. 10(a) and (b).
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Fig. 10 Mass differences between experimental and calculated mass loss curves vs. T for all UP/M-Nov blends in (a) air and (b) nitrogen. |
From Fig. 10(a) and (b), it can be seen that in both nitrogen and air, the blends are more stable (lose less mass) than expected on the basis of eqn (1) between about 180 and 530 °C. This indicates that the resins are truly co-cured and have formed a co-continuous network structure in which the sequences of phenolic units have a thermally protective effect on the interwoven polyester sequences. Moreover, this increase in thermal and thermo-oxidative stability over that which might reasonably have been expected, i.e. lower than expected amounts of volatiles released, especially if flammable, is consistent with the increased flame retardancy of the blends (i.e. reduced PHRR and THR) beyond that which would be expected on the basis of their compositions, as seen in the data presented in Table 3, and discussed above. The release of volatiles from degrading M-Nov, UP and UP/M-Nov blends has been studied in more detail by FTIR evolved gas analysis, and the results of this are discussed in the next section.
The IR spectra were recorded at temperatures between room temperature and 900 °C on gases being evolved from cured M-Nov, UP and a UP/M-Nov:70/30 blend. In Fig. 11, the absorbances of the IR bands arising from the gaseous degradation products of interest are plotted as a function of temperature for pure cured M-Nov, UP and UP/M-Nov blends. From these plots, total amounts of gases evolved (in arbitrary units) over the whole degradation temperature range can be determined by measuring the areas under the absorbance vs. T curves; these date are given in Table 6.
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Fig. 11 Absorbances of the IR bands characteristic of the various gaseous volatile pyrolysis products for M-Nov, UP and UP/M-Nov blends as a function of temperature. |
Sample | Gas evolved (FTIR peak area × 10−2) | |||||||
---|---|---|---|---|---|---|---|---|
Gas | CO2 | Phenol | Phth. anhyd. | Styrene | Methane | Arom. rings | Arom. CH | Ali. CH |
IR cm−1 | 2360 | 3647 | 1866 | 700 | 3016 | 1600 | 3025 | 2925 |
a Note: the numbers in italics are mass-average amounts of gases expected from the blends, again calculated using eqn (1). | ||||||||
M-Nov | 2.28 | 0.37 | 0.00 | 0.71 | 0.58 | 0.48 | 0.75 | 1.03 |
UP | 1.91 | 0.00 | 2.68 | 2.53 | 0.00 | 0.39 | 1.11 | 1.49 |
UP/M-Nov:80/20 | 1.58 | 0.07 | 1.52 | 1.88 | 0.12 | 0.31 | 0.86 | 0.89 |
(1.98) | (0.07) | (2.14) | (2.17) | (0.12) | (0.41) | (1.04) | (1.40) | |
UP/M-Nov:70/30 | 1.66 | 0.10 | 1.39 | 1.85 | 0.21 | 0.36 | 0.86 | 0.88 |
(2.02) | (0.11) | (1.88) | (1.98) | (0.17) | (0.42) | (1.00) | (1.35) | |
UP/M-Nov:60/40 | 1.71 | 0.12 | 1.26 | 1.59 | 0.27 | 0.42 | 0.86 | 0.84 |
(2.06) | (0.15) | (1.61) | (1.80) | (0.23) | (0.43) | (0.97) | (1.30) | |
UP/M-Nov:50/50 | 1.67 | 0.12 | 1.06 | 1.22 | 0.29 | 0.45 | 0.72 | 0.63 |
(2.10) | (0.19) | (1.34) | (1.62) | (0.29) | (0.44) | (0.93) | (1.26) |
It can be seen from Table 6 that the amounts of the various gaseous products evolved from the UP/M-Nov blends are intermediate between those of UP and M-Nov, as expected. However, calculation of amounts of gases that might be expected from the blends based on blend composition and using eqn (1) to calculate expected mass losses (i.e. eqn (1)) gives some values significantly different from those measured. In particular, yields of CO2 (evolved by both components), phthalic anhydride (only from UP), styrene (from both components) and total aliphatic species (from both components) are all lower than might be expected over the range of blend compositions studied. This is further evidence that the blends pyrolyse slightly less readily than might be expected and that this is possibly owing to some protection of the polyester sequences by the co-cured phenolic sequences, especially given that phthalic anhydride is only evolved by UP, whereas the yields of phenol and methane, which are evolved only from the UP, are not much different from the calculated values.
Footnote |
† Present address: Romer Labs UK Ltd, The Heath Business & Technical Park, Runcorn, WA7 4QX, UK. |
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