An investigation on the influence of catalyst composition, calcination and reduction temperatures on Ni/MgO catalyst for dry reforming of methane
In the present paper, the following issues regarding the dry reforming of methane, over Ni/MgO catalyst prepared by microemulsion synthesis were investigated: (i) the effect of nickel content (20, 40 and 80 wt%) in the Ni/MgO catalyst (ii) the effect of calcination temperatures (450 °C, 600 °C and 8...
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Veröffentlicht in: | RSC advances 2016-01, Vol.6 (94), p.9163-91616 |
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Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | In the present paper, the following issues regarding the dry reforming of methane, over Ni/MgO catalyst prepared by microemulsion synthesis were investigated: (i) the effect of nickel content (20, 40 and 80 wt%) in the Ni/MgO catalyst (ii) the effect of calcination temperatures (450 °C, 600 °C and 800 °C) on the solid solution formation between NiO and MgO (iii) the effect of reduction temperatures (550 °C and 800 °C) on the catalytic activity and stability of the catalyst at a very high space velocity of the reactants (CH
4
/CO
2
= 1, GHSV = 1.68 × 10
5
ml h
−1
g
−1
). Under optimum conditions, the Ni/MgO catalyst having higher Ni content (80%), calcined at higher temperature (800 °C) and reduced at lower temperature (550 °C) exhibited better catalytic activity and stability. This was attributed to the presence of higher Ni
o
active sites, formation of a strong NiO-MgO solid solution and also the catalyst was less prone to sintering at a lower reduction temperature. Furthermore, BET analysis of the Ni/MgO catalysts indicates a decrease in surface area from 153.22 to 54.01 m
2
g
−1
, as the Ni content was increased from 20% to 80%, respectively. Furthermore, fresh and spent catalysts were characterized by BET, XRD, TPR-H
2
, CO
2
-TPD, FESEM and TEM.
Catalytic activity of Ni/MgO catalyst investigated at different Ni content (20, 40 and 80 wt%), calcination (450, 600 and 800 °C) and reduction temperatures (550 and 800 °C) for dry reforming reaction at very high space velocity. |
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ISSN: | 2046-2069 2046-2069 |
DOI: | 10.1039/c6ra15256b |