Green chemical incorporation of silicon into polyoxoanions of molybdenum: characterization, thermal kinetics study and their photocatalytic water splitting activity

Bessy D'Cruza, Jadu Samuel*a and Leena Georgeb
aDepartment of Chemistry, Mar Ivanios College, Thiruvananthapuram 695015, India. E-mail: jadu_samuel@yahoo.co.in; Fax: +91 471 2530023; Tel: +91 471 2114206
bCatalysis and Inorganic Chemistry Division, National Chemical Laboratory, Pune 411008, India

Received 14th October 2014 , Accepted 13th November 2014

First published on 13th November 2014


Abstract

Cetylpyridinium silicomolybdate (CSM) nanorods were successfully synthesized by applying green chemistry principles using sodium molybdate and a structure directing cationic surfactant, cetyl pyridinium chloride (CPC) at room temperature. The composition and morphology of the nanorods were established by Fourier transform infrared spectroscopy (FT-IR), scanning electron microscopy (SEM), transmission electron microscopy (TEM), thermogravimetric analysis (TG) and inductively coupled plasma atomic emission spectroscopic (ICP-AES) techniques. The thermal decomposition kinetics of CSM nanorods were investigated by a non-isothermal thermogravimetric analyzer at various heating rates. The thermal decomposition of CSM occurred in two stages. The activation energies of the first and second stages of thermal decomposition for all heating rates have been estimated using the iso-conventional methods of Flynn–Wall–Ozawa (FWO) and Kissinger–Akahira–Sunose (KAS) and the results are found to be in good agreement with each other. The invariant kinetic parameter (IKP) method and master plot method were also used to evaluate the kinetic parameters and mechanism for the thermal decomposition of CSM. The photocatalytic water oxidation mechanism using the CSM catalyst in the presence of platinum (Pt) co-catalyst enhances the H2 evolution and was found to be 1.946 mmol g−1 h−1.


Introduction

Interest in polyoxometalates (POMs) is increasing worldwide in contemporary solid-state chemistry due to their enormous variety of structures and electronic versatility.1,2 The diversity of structures as well as the high number of elements that can make up the structure of a POM allows for a wide range of applications in fields such as catalysis, medicine, biology, material science and more recently in nanotechnology.3,4 Polyoxomolybdate species (many of these are mixed-valence types) show an extreme variety of complicated structures and therefore great significance in structural details. In recent years, a variety of very large polyoxomolybdates have been synthesized and structurally characterized, for example the wheel-shaped anions of the type {Mo154}, {Mo176}5,6 as well as the corresponding derivative {Mo248},7 the spherical icosahedral capsule {Mo132},8 and the hedgehog-shaped {Mo368} type cluster species.9,10 In terms of forming direct POM polymers linked by Mo–O–Mo units, it has been observed that in the synthesis of wheel and sphere-shaped nano sized molybdenum-oxide based clusters even under one-pot conditions, extensive linking via these types of units can occur. This means that the clusters primarily formed by self-assembly can become further linked in the same phase.11 An example is that the paramagnetic Keplerate “necklaces” synthesized by a novel room temperature solid state reaction were characterized in the solid state as metal–oxide-based nano particles which is formed from controlled linking of {(MoVI)–MoVI}12Fe30 type Keplerate balls connected by inter-ball Mo–O–Mo bonds.

Due to their acidic and redox properties, POMs can act in synergy with various compounds, yielding new attractive catalytic systems.2,3,12 However, their high solubility in water and polar solvents, low surface area and relatively low thermal stability precludes them as stable supports for heterogenization. Because of this, the preparation of POM-based materials is an active field of research and positively charged surfactants can replace the counter-ions of POMs, resulting in surfactant encapsulated clusters (SECs) with a core–shell structure and a well-defined composition.13–16 This surface modification for POMs improves their stability in air and enhances their solubility in nonpolar solvents such as chloroform, toluene, and benzene. Moreover, synthetic parameters such as concentration of the reactants, pH of the reaction medium, organic template and temperature seem to influence the formation of a solid, its crystal structure as well as morphology including nanostructural features.17,18 Recent research has shown that nanostructured vanadium and molybdenum oxides could be prepared by employing soft chemistry routes in the presence of long chain amines and surfactants.19–21

However, a great deal of research has focused on the synthesis and characterization of POMs, while there have been few studies on the fundamental thermodynamic.22,23 As far as we know, the thermodynamic properties of POMs, such as apparent activation energy (E), pre-exponential factor (A) and reaction mechanism functions of thermal decomposition process are important properties that reflect the structures and stabilities of compounds but were rarely reported. Currently non-isothermal decomposition data from TG is analyzed by two methods: model-fitting (Differential, Freeman–Carroll, Coats–Redfern) and model-free (Kissinger, Flynn–Wall–Ozawa (FWO), Kissinger–Akahira–Sunose (KAS)) methods.24–29 Model-fitting methods consist in fitting different models to the data so that a model is chosen when it gives the best statistical fit as the model from which the kinetic parameters are calculated. Model-free (isoconversional) methods require several kinetic curves to perform the analysis and the calculations from several curves at different heating rates are performed on the same value of conversion, which allows to calculate the activation energy for each conversion point.

Historically, model-fitting methods were widely used for solid-state reaction because of their ability to directly determine the kinetic triplet (activation energy, frequency factor and reaction model) from a single TG measurement. It is well established that force-fitting non-isothermal data to different reaction models results in a widely varying Arrhenius parameters.30 The kinetic analysis based on isoconversional method is frequently referred to as model-free because it is possible to obtain the apparent activation energy (E) as the function of conversion degree (α) and these methods are considered as the mostly reliable ones. According to the recommendations of International Confederation for Thermal Analysis and Calorimetry (ICTAC) Kinetics Committee,31 multi heating rate programs are recommended for computation of reliable kinetic parameters, while the methods that use a single heating program should be avoided.

Here, it is a report on a simple, cost-effective and environmentally benign synthesis of the water insoluble polyoxomolybdate containing silicon hetero atom from aqueous solutions at room temperature by applying the principles of green chemistry resulted in nanorods and its characterization by FT-IR, SEM, TEM, EDAX and ICP-AES techniques. The present work also aims to understand the thermal decomposition kinetics of resulting material using non-isothermal multi-heating thermogravimetric (TG) data in terms of model-fitting and model-free isoconversional methods as recommended by ICTAC Kinetics Committee. In this article, we have also tried to explore the photocatalytic water splitting activity of CSM catalyst.

Materials and methods

Synthesis of CSM nanorods

All chemicals are of reagent grade and were used without any further purification. In the present work, sodium molybdate as molybdenum source, CPC as structure directing template and double-distilled water as the medium of reactions were used. The synthesis of CSM was carried out by preparing two different solutions. Sodium silicate (0.5 mL) was slowly added to the aqueous solution of Na2MoO4·2H2O (0.02 mol) with constant stirring and heated to boiling (solution I). Required amount of the surfactant was dissolved in 1 M solution of HCl with vigorous stirring (solution II). Solution I was slowly added to solution II at room temperature with vigorous stirring by keeping the mass ratio as CPC/Na2MoO4·2H2O = 0.33, a yellow green precipitate was formed at pH 5, which was adjusted to pH 4 by adding HCl. The above mixture was then stirred continuously for 24 h.32,33 The precipitate is then washed continuously with double-distilled water and then with absolute alcohol thoroughly to remove the excess of surfactant. The formed precipitate was then dried below 50 °C.

Photocatalytic reaction

A 70 mL quartz cell was used for performing the water splitting activity. The CSM catalyst (0.025 g) was dispersed in 80 v/v% water and 20 v/v% methanol by means of a magnetic stirrer. To the reaction mixture about 2 μL of chloroplatinic acid solution was added as a co-catalyst and methanol as sacrificial reagent. The visible light source was 400 W high pressure mercury lamp and the reaction was carried out for 4 h. The amount of H2 evolved was determined using Agilent Technologies 7890A gas chromatography (GC) system and the evolving gas mixture was taken in a gas tight syringe and injected into the GC.

Kinetic methods

Iso-conversional methods. It is well known that the iso-conversional method easily gives an estimate of activation energy regardless of the reaction mechanism. Two kinds of iso-conversional methods are applied in this article.

FWO method is an integral method which is based on the measurement of the adequate temperature to certain values of the conversion α, for experiments effectuated to different rates of heating.34 The equation corresponding to this method is:

 
image file: c4ra12331j-t1.tif(1)
where g(α) is integral reaction model, α is extent of conversion, E is activation energy, A is pre-exponential factor, T is Kelvin temperature, β is heating rate and R is gas constant.

The KAS method35 is another integral isoconversional method and is based on the equation:

 
image file: c4ra12331j-t2.tif(2)

The relations given by eqn (1) and (2) involve all three members of kinetic triplet. From these relations the apparent activation energy can be evaluated using the linear representation of ln[thin space (1/6-em)]β, ln(β/T2) vs. 1/T with a given value of the conversion.

Model fitting methods. These methods obtain the kinetic parameters with a single heating rate. In this work, the method that has been employed is the integral Coats–Redfern (C–R) method.36
 
image file: c4ra12331j-t3.tif(3)

Algebraic expressions for g(α) for the most frequently used mechanisms (see Table S1 in ESI). For each theoretical kinetic model, g(α), and at each heating rate, from the slope and the intercept of plots ln[g(α)/T2] versus 1/T, the parameters ln[thin space (1/6-em)]A and E can be evaluated. For a given model and heating rate, the linear plot of the left hand side versus 1/T permitted the determination of E and A from the slope and the intercept, respectively.

Invariant kinetic parameters (IKP) method. Furthermore, the ‘true’ kinetic model can be obtained using the Invariant kinetic parameters (IKP) method37–39 and is based on the study of the compensation effect. If the compensation effect between ln[thin space (1/6-em)]A and E (obtained from CR method) exists, then by plotting ln[thin space (1/6-em)]A versus E straight lines should be obtained for each heating rate, according to
 
ln[thin space (1/6-em)]A = α* + β*E (4)

The lines of the plot should intercept in a point that corresponds to the ‘true’ values of E and ln[thin space (1/6-em)]A for the ‘true’ kinetic model, which were called by Lesnikovich and Levchik37–39 the invariant kinetic parameters, Einv and Ainv. Due to the fact that certain variations of the experimental conditions determine regions of intersections, the intersection is only approximate. Therefore, in order to eliminate the influence of experimental conditions on the determinations of Einv and Ainv they were determined from the slope and intercept of the so called super correlation relation.

 
αv* = ln[thin space (1/6-em)]Ainvβv*Einv (5)

The slopes and intercepts of the plot give the compensation parameters. The straight line, αv* and βv*, allows us to determine the IKP (Einv and Ainv) from the slope and intercept.

It has been reported that the values of the invariant conversion function are proportional to their true values.40,41 Therefore, the IKP method aims to determine the invariant parameters independent of the kinetic model; comparing the invariant parameters to those obtained using other methods also allows us to determine which kinetic model is better for describing the process.

Integral master plot method. Integral master-plot method42–44 was used for the determination of the reaction model for the thermal decomposition of solids. Essentially the master plot method is based on the comparison of theoretical master plot, which are obtained for a wide range of ideal kinetic models, with the experimental master plot. The integral function of conversion in the solid state nonisothermal decomposition reactions is expressed as
 
image file: c4ra12331j-t4.tif(6)
where u = E/RT. The temperature integral, image file: c4ra12331j-t5.tif has no analytical solution and can be expressed by an approximation. An approximate formula45 of p(u) with high accuracy is used
 
p(u) = eu/[u(1.00198882u + 1.87391198)] (7)

From the integral kinetic equation the following equation can be obtained using a reference point at α = 0.5 and according to eqn (6), one gets

 
image file: c4ra12331j-t6.tif(8)
where u0.5 = E/RT0.5. The following equation is obtained by dividing eqn (6) by eqn (8)
 
image file: c4ra12331j-t7.tif(9)

Plotting g(α)/g(0.5) against α corresponds to the theoretical master plots of various kinetic functions (ESI, Table S1). Using the predetermined value of E from isoconversional method, along with the temperature measured as a function of α, p(u) can be calculated according to the eqn (7). Then the experimental master plots of p(u)/p(u0.5) against α can be obtained. Comparing the experimental master plots with theoretical ones, can conclude the kinetic model.

Results and discussion

Spectrochemical analysis

FT-IR spectrum technique provides information related to the maintenance of the Keggin structure after salt preparation. In the Keggin structure, the four types of oxygen provide four characteristic bands in the spectrum in the range 1100–550 cm−1, called the fingerprint region.3 The exact position of these bands depends upon the degree of hydration and the type of counter ion present. In the present study Fig. 1 shows the FT-IR spectra of CSM which yielded four characteristic peaks related to a Keggin structure: ν(Mo–Oc–Mo) = 789 cm−1, related to asymmetric stretching of molybdenum with edge oxygens in Mo–O–Mo; ν(Mo–Ob–Mo) = 864 cm−1, attributed to the asymmetric stretching of corner oxygens in Mo–O–Mo; ν(Mo[double bond, length as m-dash]Od) = 949 cm−1, indicative of the asymmetric stretching of the terminal oxygen; and ν(Si–Oa) = 890 cm−1, assigned to asymmetric stretching of oxygens with a central silicon atom.46 In addition to these bands, there is also a band related to N–H extending vibrations of CPC moiety stretching observed at 1382, 1474, and 1484 cm−1. Two absorption bands of 2926 and 2850 cm−1 corresponded to aliphatic C–H vibrations of CPC. Thus the FT-IR analysis confirms the presence only of the specific bands of the Keggin unit in the synthesized CSM.
image file: c4ra12331j-f1.tif
Fig. 1 FT-IR spectrum of CSM nanorods.

Fig. 2(a) and (b) shows the typical SEM and TEM images of the synthesized product. The particles were found to be nanorods of diameter ∼150–160 nm and length ∼0.5–1 μm.


image file: c4ra12331j-f2.tif
Fig. 2 (a) SEM (b) TEM (c) EDAX images of CSM nanorods.

EDAX analysis (Fig. 2(c)) as well as ICP-AES analysis showed the presence of Mo, Si and O in the nanorods. ICP-AES analysis indicated the ratio of Si[thin space (1/6-em)]:[thin space (1/6-em)]Mo is 1[thin space (1/6-em)]:[thin space (1/6-em)]12. XRD pattern (Fig. 3) of the synthesized nanomaterial shows that the particles are below crystalline dimension and hence amorphous in nature.


image file: c4ra12331j-f3.tif
Fig. 3 XRD pattern of CSM nanorods.

Thermogravimetric analysis

The TG-DTG curves of CSM nanorods at four heating rates 10, 15, 20 and 25 °C min−1 in the temperature range of 35–700 °C are shown in Fig. 4(a) and (b) and it seems that TG curve exhibits mass losses in two stages. For 10 °C min−1, the first stage of decomposition takes place in the temperature range of 42 °C to 334 °C with a mass loss of 13.6% and is due to the loss of 1.5 cetyl pyridinium group. The corresponding DTG peak is seen at 322.08 °C. The second stage of decomposition takes place in the temperature range of 334 °C to 698 °C with a mass loss of 31.8% and it is due to the loss of 3.5 cetyl pyridinium group, 1.5 water molecules and the collapse of Keggin-type structure. The final decomposition product is the mixture of MoO3 and Si2O5. This is accompanied by DTG peak at 368.8 °C. There is a good agreement between the expected and observed mass losses for the loss of cetyl pyridinium cation and silicomolybdic anions.23 As seen in Fig. 4(b), the DTG peaks were shifted to higher temperature with increase in heating rate. DTG peak of first stage observed at 322.08 °C for heating rate 10 °C min−1 was shifted to 323.97 °C, 335.11 °C and 340.78 °C for 15, 20 and 25 °C min−1, respectively. Similarly the DTG peak of second stage observed at 368.8 °C for heating rate 10 °C min−1 was also displaced to 387.5 °C, 391.29 °C and 393.17 °C for 15, 20 and 25 °C min−1, respectively. On the basis of TGA and EDAX, composition of the CSM nanorods was found to be around (C21H38N)5H3 [SiMo12O40xH20 (x < 1).
image file: c4ra12331j-f4.tif
Fig. 4 (a) Thermal degradation (TG) and (b) derivative mass loss (DTG) curves at the different heating rates (β = 10, 15, 20 and 25 °C min−1) for the thermal decomposition of CSM nanorods.

Kinetic analysis

Isoconversional methods. The results obtained from thermogravimetric analysis were elaborated according to model-free methods to calculate the kinetic parameters. In order to apply different kinetic methods on the thermal decomposition process of CSM, the dependence of fraction decomposed (α) on temperature (T) at different heating rates for stages I and II are plotted (Fig. 5). It is seen that all αT curves have the same shapes. The sigmoid-shaped curves are shifted to higher temperatures with an increase of heating rates as reported earlier.47
image file: c4ra12331j-f5.tif
Fig. 5 Plot of fraction reacted (α), versus temperature (T) for stages I and II at four different heating rates using TG data.

The FWO plots of ln[thin space (1/6-em)]β versus 1/T for different values of conversion are shown in Fig. 6. KAS plots (ln(β/T2) versus 1/T) also give same pattern of curves and hence these are not included in the present paper. The apparent activation energies and frequency factors were obtained from the slope and intercept of regression lines and are given in Table 1. The calculated correlation coefficients, r, were higher for all cases. From Table 1, we can observe that values of E obtained by FWO method are in the ranges of 143.95–179.21 and 144.52–158.38 kJ mol−1 for the first and second decomposition stages, respectively. And values of E obtained by KAS method are about 141.69–178.38 and 141.42–155.36 kJ mol−1, respectively. The averages of E for two stages from FWO and KAS methods are 163.78 and 150.89, 162.33 and 147.80 kJ mol−1, which are noted that the calculated values of the activation energy in the FWO method very well agree with KAS method.


image file: c4ra12331j-f6.tif
Fig. 6 FWO plot for stages I and II in nitrogen atmosphere for the non-isothermal decomposition of CSM using TG data. obtained by FWO and KAS methods for stages I and II.
Table 1 Kinetic parameters for stages I and II for the non-isothermal decomposition of CSM by FWO and KAS methods
Degree of conversion (α) FWO KAS
Stage I Stage II Stage I Stage II
E kJ−1 mol−1 ln[thin space (1/6-em)]A/S−1 E kJ−1 mol−1 ln[thin space (1/6-em)]A/S−1 E kJ−1 mol−1 ln[thin space (1/6-em)]A/S−1 E kJ−1 mol−1 ln[thin space (1/6-em)]A/S−1
0.1 143.95 ± 0.69 28.24 ± 1.17 144.52 ± 0.93 25.47 ± 1.45 141.69 ± 0.69 27.65 ± 1.18 141.42 ± 0.93 24.73 ± 1.45
0.2 151.82 ± 1.35 30.03 ± 2.28 145.78 ± 1.35 25.98 ± 2.10 149.89 ± 1.35 29.54 ± 2.29 142.66 ± 1.36 25.23 ± 2.11
0.3 155.15 ± 1.67 30.77 ± 2.80 146.43 ± 1.30 26.19 ± 2.01 153.34 ± 1.59 30.31 ± 2.67 143.26 ± 1.24 25.44 ± 1.92
0.4 162.23 ± 1.42 32.22 ± 2.38 149.03 ± 1.07 26.71 ± 1.64 160.74 ± 1.43 31.85 ± 2.39 145.93 ± 1.07 25.98 ± 1.64
0.5 166.14 ± 1.51 33.01 ± 2.51 150.07 ± 0.92 26.91 ± 1.41 164.81 ± 1.5 32.68 ± 2.52 146.95 ± 0.92 26.17 ± 1.40
0.6 167.45 ± 1.47 33.27 ± 2.44 152.26 ± 0.83 27.27 ± 1.25 166.15 ± 1.43 32.95 ± 2.36 149.16 ± 0.64 26.56 ± 1.32
0.7 173.25 ± 1.49 34.44 ± 2.45 154.94 ± 0.89 27.73 ± 1.33 172.19 ± 1.73 34.18 ± 2.84 151.91 ± 0.76 27.04 ± 1.13
0.8 174.80 ± 1.73 34.74 ± 2.83 156.58 ± 1.02 28.01 ± 1.51 173.79 ± 1.60 34.48 ± 2.62 153.55 ± 1.02 27.33 ± 1.51
0.9 179.21 ± 1.59 35.65 ± 2.61 158.38 ± 0.99 28.34 ± 1.47 178.38 ± 1.42 35.44 ± 2.35 155.36 ± 1.00 27.67 ± 1.47
Average 163.78 ± 1.44 32.49 ± 2.39 150.89 ± 1.03 26.96 ± 1.57 162.33 ± 1.42 32.12 ± 2.35 147.80 ± 0.99 26.24 ± 1.55


Fig. S1 in ESI shows the dependence of the activation energy (E) on the degree of conversion (α). Because the values of activation energy worked out for both stages by the KAS and FWO methods were very close, we chose the average values of two as the value of activation energy used in the master-plot method.

Model fitting methods. The sets of ln[thin space (1/6-em)]A and E for stages I and II can be calculated at different heating rates for various kinetic functions (see ESI, Table S1) by using eqn (3) and are given in Table 2. For a given model and heating rate, the linear plot of the left hand side of eqn (3) versus 1/T permitted the determination of E and A from the slope and the intercept, respectively. It can be observed that a wide variety of results depend on the applied mechanism. If the collected E values shown in Table 2 are compared with those determined previously using the isoconversional methods, the function that yields a better fit to the experimental results corresponds to Avrami mechanism, A2 for stage I and A3/2 for stage II.
Table 2 Integral parameters determined by using CR Method for stages I and II for the thermal decomposition of CSM nanorods
Heating rate
Kinetic model β = 10 °C min−1 β = 15 °C min−1 β = 20 °C min−1 β = 25 °C min−1
E kJ−1 mol−1 ln[thin space (1/6-em)]A/s−1 r E kJ−1 mol−1 ln[thin space (1/6-em)]A/s−1 r E kJ−1 mol−1 ln[thin space (1/6-em)]A/s−1 r E kJ−1 mol−1 ln[thin space (1/6-em)]A/s−1 r
Stage I
P2 112.4 ± 9.1 14.6 ± 4.3 0.9776 120.7 ± 11.5 16.4 ± 5.3 0.9697 127.5 ± 11.1 17.8 ± 5.5 0.9745 130.2 ± 11.8 18.5 ± 5.9 0.9723
P3 71.7 ± 6.1 5.9 ± 3.2 0.9756 77.2 ± 7.7 7.4 ± 4.2 0.9671 81.6 ± 7.4 8.4 ± 4.1 0.9724 83.5 ± 7.9 8.9 ± 4.7 0.9700
P4 51.3 ± 4.6 1.6 ± 2.6 0.9732 55.4 ± 5.8 2.7 ± 3.5 0.9642 58.7 ± 5.6 3.6 ± 3.7 0.9700 60.1 ± 5.9 4 ± 4.1 0.9675
A2 160.5 ± 4.4 24.8 ± 2.6 0.9974 172.8 ± 7.2 27.5 ± 4.0 0.9939 181.9 ± 5.9 29.2 ± 3.8 0.9963 186.0 ± 6.8 30.1 ± 4.4 0.9953
A3 103.7 ± 2.9 12.9 ± 1.9 0.9972 111.9 ± 4.8 14.9 ± 3.1 0.9935 117.9 ± 4.0 16.1 ± 3.0 0.9961 120.6 ± 4.6 16.8 ± 3.5 0.9950
A4 75.3 ± 2.2 6.9 ± 1.4 0.9970 81.5 ± 3.6 8.4 ± 2.6 0.9931 85.9 ± 3.0 9.5 ± 2.6 0.9958 87.9 ± 3.4 10 ± 3.0 0.9947
A3/2 217.2 ± 5.9 36.6 ± 3.2 0.9974 233.8 ± 9.6 39.9 ± 4.8 0.9941 245.9 ± 7.9 42.2 ± 4.5 0.9964 251.4 ± 9.1 43.2 ± 5.1 0.9954
R1 234.7 ± 18.3 39.7 ± 6.8 0.9795 251.4 ± 23.0 43.0 ± 8.3 0.972 264.9 ± 22.2 45.5 ± 8.4 0.9763 270.6 ± 23.7 46.5 ± 8.9 0.9743
R2 278.0 ± 13.8 48.1 ± 5.6 0.9914 298.4 ± 19.0 52.1 ± 7.4 0.9861 314 ± 17.5 54.9 ± 7.2 0.9893 320.9 ± 19.1 56.2 ± 7.8 0.9878
[thin space (1/6-em)]
Stage II
A2 117.5 ± 0.0 13.6 ± 2.4 0.9876 117.2 ± 7.7 13.6 ± 4.0 0.9853 117.2 ± 7.3 13.6 ± 4.2 0.9868 125.2 ± 7.3 15.2 ± 4.4 0.9882
A3 74.8 ± 0.0 5.3 ± 3.3 0.9863 74.5 ± 5.1 5.4 ± 3.2 0.9838 74.5 ± 4.9 5.5 ± 3.1 0.9854 79.8 ± 4.9 6.7 ± 3.5 0.9871
A4 53.4 ± 0.0 1.0 ± 3.8 0.9849 53.1 ± 3.9 1.2 ± 2.6 0.9821 53.1 ± 3.6 1.4 ± 2.8 0.9838 57.1 ± 3.7 2.3 ± 3.1 0.9858
A3/2 160.3 ± 0.0 21.7 ± 1.6 0.9882 159.9 ± 10.2 21.7 ± 4.8 0.9859 159.9 ± 9.7 21.6 ± 4.9 0.9874 170.7 ± 9.8 23.6 ± 5.1 0.9887
R1 171.1 ± 19.8 23.3 ± 6.9 0.9561 170.5 ± 20.4 23.2 ± 7.4 0.9531 170.8 ± 20.0 23.1 ± 7.5 0.9553 182.3 ± 20.8 25.2 ± 7.8 0.9573
R2 204.7 ± 0.0 29.2 ± 0.6 0.9754 204.2 ± 18.3 28.9 ± 6.9 0.9729 204.3 ± 17.7 28.9 ± 7.0 0.9748 217.9 ± 18.3 31.3 ± 7.3 0.9763
R3 217.6 ± 0.0 31.3 ± 0.3 0.9806 216.9 ± 17.3 31.1 ± 6.6 0.9783 217.2 ± 16.6 30.9 ± 6.7 0.9799 231.6 ± 17.1 33.5 ± 7.0 0.9814
F3/2 224.3 ± 0.0 32.3 ± 1.1 0.9829 223.7 ± 12.9 32.1 ± 5.5 0.9806 223.9 ± 11.8 31.9 ± 5.5 0.9822 238.7 ± 11.4 34.5 ± 5.6 0.9836


IKP method. Other method using the calculation of kinetic parameters is IKP. The application of the IKP method is based on the study of the compensation effect. If a compensation effect is observed, a linear relation defined by eqn (4) for each heating rate, β is obtained. It is shown by plotting ln[thin space (1/6-em)]A versus E that a compensation effect is observed for each heating rate (Fig. 7) for the first and second stages of thermal decomposition. The slopes and intercepts of the plot give the compensation parameters α* and β* for both the stages and the values are presented in Table 3.
image file: c4ra12331j-f7.tif
Fig. 7 IKP plots obtained from the CR method at different heating rates (β = 10, 15, 20 and 25 °C min−1) for stages I and II for the thermal decomposition of CSM nanorods.
Table 3 Values of integral compensation parameters calculated from data in Table 2 for stages I and II for the thermal decomposition of CSM nanorods
Heating rate/°C min−1 Stage I Stage II
α*/min−1 β*/mol kJ−1 r α*/min−1 β*/mol kJ−1 r
10 0.2060 ± 0.0016 8.642 ± 0.256 0.9998 0.1831 ± 0.0023 8.322 ± 0.425 0.9994
15 0.2039 ± 0.0015 8.181 ± 0.256 0.9998 0.1809 ± 0.0026 7.945 ± 0.425 0.9994
20 0.2016 ± 0.0014 7.858 ± 0.256 0.9998 0.1788 ± 0.0026 7.682 ± 0.425 0.9994
25 0.2004 ± 0.0014 7.624 ± 0.256 0.9998 0.1775 ± 0.0024 7.400 ± 0.425 0.9994


A plot α* versus β* is actually a straight line proving the existence of a super correlation relation, whose parameters allow evaluation of the invariant activation parameters (Fig. 8) for stages I and II. The obtained values of Einv and ln[thin space (1/6-em)]Ainv are 176.60 kJ mol−1 and 27.77 s−1 for the stage I and 160.2 kJ mol−1 and 21.01 s−1 for the stage II are in agreement with the values of E and ln[thin space (1/6-em)]A estimated for models A2 and A3/2 for stages I and II respectively, presented in Table 2.


image file: c4ra12331j-f8.tif
Fig. 8 Supercorrelation relationship for stages I and II for the thermal decomposition of CSM nanorods.
Integral master plot method. The reaction model for the thermal decomposition of CSM was confirmed by integral master-plot method. Using the predetermined value of E from isoconversional method, along with the temperature measured as a function of α, p(u) can be calculated according to the eqn (7). Then the experimental master plots of p(u)/p(u0.5) against α under various heating rates for the first and second stages of thermal decomposition of CSM can be drawn. Both of the theoretical master plots of various kinetic functions and experimental master plots are shown in Fig. 9. The comparisons of the experimental and theoretical master curves show that the kinetic process of the thermal decomposition of CSM agree with the A2 master curve for the first stage of decomposition and A3/2 master curve for the second stage of decomposition. In the literature A2 and A3/2 models are known as Avrami–Erofeev mechanism which describes the decomposition through nucleation and nuclei growth. These observations are in agreement with the mechanism obtained by CR method in the previous section.
image file: c4ra12331j-f9.tif
Fig. 9 Theoretical (lines) integral master plots of g(α)/g(0.5) versus α and the experimental master curves (symbols) for stages I and II for the thermal decomposition of CSM nanorods.

Photocatalytic activity of CSM

There are various challenging methods employed for solar energy conversion. Among them, the most attractive one was the photocatalytic decomposition of water into hydrogen and oxygen which is known to be a clean renewable source. Many of the photocatalysts were UV active, thus wasting the abundance of visible light irradiance in sunlight falling on earth's surface. Photocatalytic reactions on semiconductors are initiated by the absorption of photons with energy equal to, or greater than, the semiconductor band gap.

The presence of surface active sites on the photocatalyst is also an important parameter for the production of hydrogen. In the absence of surface active sites the photogenerated conduction band electrons can recombine with valence bond holes very quickly and release energy in the form of unproductive heat or photons. This is because the photo-excited electron and hole possess an electrostatic attraction between each other. Availability of surface active sites for the redox reactions by the photogenerated electrons and holes minimize the chances of recombination processes. The photocatalytic decomposition of water before recombination process can be achieved by introducing photocatalytic active sites in the nanostructured particles. This can be achieved by loading them with noble metals as co-catalysts like Pt, Au, Pd, Rh, Ni, Cu and Ag which are very effective for the enhancement of photocatalytic decomposition of water.48–53 These activities greatly reduce the possibility of electron–hole recombination, resulting in efficient separation and stronger photocatalytic reactions in the CSM photocatalyst. The rate of photocatalytic hydrogen production can be further increased by sacrificial reagents like methanol, ethanol and also organic compounds, organics derived from renewable sources like biomass which may be profitably employed as hole scavengers. But, the mechanisms of the role of cocatalysts, sacrificial agents and photocatalytic water splitting have been under debate with many researchers. Kudo et al.54 first studied the photocatalytic properties of many Ta-based catalysts, among them La-doped NiO/NaTaO3 showed high efficiency. Zou et al. carried out direct water splitting on In–Ni–Ta oxides under visible light irradiation. The photocatalytic water splitting activity was found to be 3.3 times higher for doped TiO2 than the bare TiO2.

In present work, the CSM acts as catalyst in the presence of platinum co-catalyst. In the absence of platinum cocatalyst, CSM does not display any photocatalytic water splitting activity due to its large band gap in the UV region. There are reports suggesting that the band gap issue can be minimized with proper cocatalysts which serve as the reaction sites and catalyze the reactions. The role of Pt as co-catalyst is to reduce the band gap of CSM catalyst so that visible light can be harvested by the catalyst to act as an electron donor for H2 evolution through the splitting of water.

The detrimental effect of Pt co-catalyst on the CSM catalyst is an interesting observation. The presence of Pt has definitely enhanced the H2 evolution and was found to be 1.946 mmol g−1 h−1.

Conclusions

Synthesis under suitable conditions based on the requirements of green chemistry using cetylpyridinium chloride as template led to the formation of cetylpyridinium silicomolybdate nanorods. Non-isothermal thermogravimetric measurements at various heating rates enable calculation of kinetic parameters characterizing the decomposition process. The average values of activation energy of the thermal decomposition of cetylpyridinium silicomolybdate nanorods obtained by Flynn–Wall–Ozawa and Kissinger–Akahira–Sunose methods were found to be 163.1 and 140.4 kJ mol−1 for the first and second stages, respectively, over the range of α = 0.1–0.9. For the first and second stages of decomposition, the invariant activation energy obtained by the invariant kinetic parameter method was in good agreement with the average value obtained by integral isoconversional methods in the conversion range of 0.10 to 0.90. The master plot method revealed that the first stage of thermal decomposition takes place through Avrami–Erofeev A2 mechanism, g(α) = [−ln(1 − α)]1/2 while the second stage of decomposition occurs through Avrami–Erofeev (A3/2) mechanism, g(α) = [−ln(1 − α)]2/3. In the present work, we have shown that the photocatalytic water splitting activity of cetylpyridinium silicomolybdate in the presence of platinum co-catalyst enhances the H2 evolution.

Conflicts of interest

The authors declare no competing financial interest.

Acknowledgements

Bessy D'Cruz thanks the University of Kerala for the award of research fellowship and financial support. The authors are grateful to NIIST at Thiruvananthapuram, Government Arts College at, University College at Thiruvananthapuram and SAIF at Cochin for lending the analytical facilities.

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Footnote

Electronic supplementary information (ESI) available: One figure showing dependence of activation energy E with conversion α obtained by FWO and KAS methods for stages I and II and one table giving the expressions for reaction models have been made available as ESI available. See DOI: 10.1039/c4ra12331j

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