oxidizing elements is considered as negative, and the reducing elements as positive, similar to the oxidation number concept familiar to chemists. Accordingly, the elemental valency of C, Sn, In, and H is +4, +2, +3, and +1, respectively, and oxidizing valency of oxygen is taken as -2. The valency of nitrogen is considered to be zero. Based on this concept, the oxidizing valency of aluminum nitrate and the reducing valency of urea are In(NO3)3 = -15; [In = +3, 3N = 0, 9O= (9 x -2) = -18], CH4N2O = +6; [C = +4, 4H = (4 x +1) = +4, 2N = 0, O = (1 x -2) = -2]. Sn(NO3)2 = -8 [Sn = +4, 3N = 0, 6O = (6 x -2) = -12] 9 (In(NO3)3) + 1 (Sn(NO3)2) + 6n = 0 [ n = 23.833 g] for the ratio In2O3 : SnO2 = (90:10) 8.5 (In(NO3)3) + 1.5 (Sn(NO3)2) + 6n = 0 [ n = 23.25 g] for the ratio In2O3 : SnO2 = (85:15) 8 (In(NO3)3) + 2 (Sn(NO3)2) + 6n = 0 [ n = 22.67 g] for the ratio In2O3 : SnO2 = (80:20) 5 (In(NO3)3) + 5 (Sn(NO3)2) + 6n = 0 [ n = 19.17 g] for the ratio In2O3 : SnO2 = (50:50) 10 (In(NO3)3) + 6n = 0 [ n = 25 g] for In2O3 10 (Sn(NO3)2) + 6n = 0 [ n = 13.333 g] for SnO2 Accordingly, for the complete combustion of indium nitrate: urea mixture, the molar ratio becomes 15/6 = 2.5. Like that for the complete combustion of tin nitrate: urea mixture, the molar ratio becomes 8/6 = 1.333. 2.6.1 Preparation of In2O3 In a typical synthesis, an aqueous solution containing ions of In2O3 was prepared by dissolving typical amount of high purity analytical grade chemicals i.e., 27 indium metal ingots (99%, Aldrich, India supplied from Merck Chemical Company), distilled water (~ 100 ml) and nitric acid (99% Merck, India) in a glass beaker. Urea (99%, Merck, India) and 25% NH3 (0.91 g cm-3) was then added to the solution containing In ions. Amount of urea was calculated based on total valence of the oxidizing and reducing agents for maximum release of energy during combustion. Oxidant/fuel ratio of the system was adjusted by adding nitric acid and ammonium hydroxide; and the ratio was kept at unity. The resulting translucent solution was heated on a hot plate (at about 100 ºC) until it turned into a viscous solution. The solution boils upon heating and undergoes dehydration accompanied by foam. The foam then ignites by itself due to persistent heating giving a voluminous and fluffy product of combustion. The combustion product was subsequently characterized as single phase nanopowders of In2O3. Yellow ashes obtained after combustion were then collected for structural characterization and other morphological studies. The system was homogeneous during the whole process and no precipitation was observed. The entire processing steps are illustrated in Fig. (2.3) 14In(NO3)3.3H2O + 3NH2CONH2 ⎯ ⎯→7In2O3 + 48NO2 + 3CO2 + 48H2O (2.3) 2.6.2 Preparation of SnO2 In a typical synthesis, an aqueous solution containing ions of SnO2 was prepared by dissolving typical amount of high purity the analytical grade chemicals i.e., tin metal ingots (99%, Aldrich, India supplied from Merck Chemical Company), distilled water (~ 100 ml) and nitric acid (99% Merck, India) in a glass beaker. Urea (99%, Merck, India) and 25% NH3 (0.91 g cm-3) was then added to the solution containing Sn ions. Amount of urea was calculated based on total valence of the oxidizing and reducing agents for maximum release of energy during combustion. 28 Oxidant/fuel ratio of the system was adjusted by adding nitric acid and ammonium hydroxide; and the ratio was kept at unity. The resulting translucent solution was heated on a hot plate (at about 100 ºC) until it turned into a viscous solution. The solution boils upon heating and undergoes dehydration accompanied by foam. The foam then ignites by itself due to persistent heating giving a voluminous and fluffy product of combustion. The combustion product was subsequently characterized as single phase nanopowders of SnO2. White ashes obtained after combustion were then collected for structural characterization and other morphological studies. The system was homogeneous during the whole process and no precipitation was observed. According to the principle of propellant chemistry [22], for a stoichiometric combustion reaction between a fuel and an oxidizer, the ratio of the net oxidizing valency of the metal nitrate to the net reducing valency of the fuel should be unity. The total oxidizing valency of Sn(NO3)2.3H2O works out to be -15. Urea (N2H4CO) was taken as a fuel, which contains one carboxylic and four hydroxyl group for coordinating the metal ions, which facilitate the formation of a viscous gel [23]. The total reducing valency of urea works out to be +6. Hence, in order to have the stoichiometric combustion reaction, one mole of tin nitrate needs 15/6 (or 2.5) mol of urea. This ratio of oxidant: fuel (1:2.5) gives a satisfactory viscous gel to initiate combustion. Since oxidant-fuel composition was optimum, sluggish decomposition was not possible and therefore the reaction not leftover carbonaceous material in the as-prepared powder. These observations are in good agreement with those reported in the literature [24]. The further fuel-rich ratios were not suitable due to a sluggish and incomplete combustion. 3Sn(NO3)2.2H2O + 4NH2CONH2 ⎯ ⎯→3SnO2 + 7N2 + 4CO2 +14H2O (2.4) 29 2.6.3 Preparation of ITO with different proportions An aqueous solution containing ions of indium nitrate and tin nitrate in the ratio of 95:05, 90:10, 85:15, 80:20 and 50:50 and amount of doping was prepared by dissolving stoichiometric amount of high purity In(NO3)3.3H2O (99%, Merck, India) and Sn(NO3)2.2H2O (99%, Merck, India) in 100ml distilled water in a glass beaker. Urea (99%, Merck, India) was then added to the solution containing In(NO3)3.3H2O and Sn(NO3)2.2H2O ions. Amount of urea was calculated based on total valence of the oxidizing and reducing agents for maximum release of energy during combustion [25]. In the preparation of nanoparticles of other ceramic oxides using combustion process polyvinyl alcohol and urea were used as the complexing agent and fuel, respectively. In these cases, usual calcinations of the combustion product were essential to get a single phase nano material. In the present combustion method, urea was used as the complexing agent instead of polyvinyl alcohol and urea was replaced with ammonia. Using this complexing agent and oxidant fuel system, it was possible to get a single phase ITO nanoparticles in single-step combustion without the usual calcinations for prolonged duration at high temperature. Amount of Urea = Valency of metal ions × m.w. of urea × req. wt. 3 × m.w. of Compound (2.5) Oxidant/fuel ratio of the system was adjusted by adding nitric acid and ammonium hydroxide; and the ratio was kept at unity. At such a condition, maximum energy is released. The solution containing the precursor mixture was heated using a hot plate at ~250°C in a ventilated fume hood. The solution boils upon heating and undergoes dehydration accompanied by foam. The foam then ignites by itself due to persistent heating giving a voluminous and fluffy product from combustion. The system was homogeneous during the whole process and no precipitation was observed. The combustion product was subsequently characterized as single phase 30 nanocrystals of ITO in the ratio of 95:05, 90:10, 85:15, 80:20 and 50:50. The schematic diagram of experimental technique is shown in Fig. 2.3. 2.7 Conclusion This chapter presents the various powder preparation techniques. The combustion synthesis method has been elaborately discussed with the principles of combustion process and the steps involved in the preparation of monophase oxide powders. Preparation of In2O3, SnO2 and ITO powders under the optimized conditions is presented. 31 References [1] H.Gleiter, Progr. Mater. 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Res., 16 (2001) 1982. 32 Fig. 2.1 Two basic approaches to nanomaterials fabrication: top-down (from left to right) and bottom-up (from right to left) Fig. 2.2 Comparison of the “top-down” and “bottom-up” approach to nanomaterials synthesis Clear Solution of Indium Clear Solution of Tin 95:05, 90:10, 85:15, 80:20 and 50:50 Indium & Tin Nitrate Solution Dehydration stage Combustion (Ignition) above 300ºC As prepared powder Calcination at different high temperatures Compounds Fig. 2.3 Flow chart for the preparation of ITO
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