WO2007093825A1 - Fischer-tropsch catalyst preparation - Google Patents
Fischer-tropsch catalyst preparation Download PDFInfo
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- WO2007093825A1 WO2007093825A1 PCT/GB2007/050058 GB2007050058W WO2007093825A1 WO 2007093825 A1 WO2007093825 A1 WO 2007093825A1 GB 2007050058 W GB2007050058 W GB 2007050058W WO 2007093825 A1 WO2007093825 A1 WO 2007093825A1
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- WIPO (PCT)
- Prior art keywords
- temperature
- reduction
- cobalt
- hours
- metal oxide
- Prior art date
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- 239000003054 catalyst Substances 0.000 title claims abstract description 37
- 238000002360 preparation method Methods 0.000 title description 2
- 230000009467 reduction Effects 0.000 claims abstract description 56
- 229910052751 metal Inorganic materials 0.000 claims abstract description 45
- 239000002184 metal Substances 0.000 claims abstract description 45
- 239000000919 ceramic Substances 0.000 claims abstract description 29
- 239000012298 atmosphere Substances 0.000 claims abstract description 25
- 239000001257 hydrogen Substances 0.000 claims abstract description 24
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 24
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 23
- 239000010941 cobalt Substances 0.000 claims abstract description 23
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910000428 cobalt oxide Inorganic materials 0.000 claims abstract description 19
- IVMYJDGYRUAWML-UHFFFAOYSA-N cobalt(ii) oxide Chemical compound [Co]=O IVMYJDGYRUAWML-UHFFFAOYSA-N 0.000 claims abstract description 19
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 16
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 11
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 claims abstract description 9
- 238000001354 calcination Methods 0.000 claims abstract description 9
- 150000002431 hydrogen Chemical class 0.000 claims abstract description 9
- 229910052707 ruthenium Inorganic materials 0.000 claims abstract description 9
- 238000001035 drying Methods 0.000 claims abstract description 7
- 238000000034 method Methods 0.000 claims description 30
- 229910044991 metal oxide Inorganic materials 0.000 claims description 25
- 150000004706 metal oxides Chemical class 0.000 claims description 25
- 239000007789 gas Substances 0.000 claims description 14
- 230000003647 oxidation Effects 0.000 claims description 11
- 238000007254 oxidation reaction Methods 0.000 claims description 11
- 238000011946 reduction process Methods 0.000 claims description 11
- 239000000758 substrate Substances 0.000 claims description 10
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 9
- 239000001301 oxygen Substances 0.000 claims description 9
- 229910052760 oxygen Inorganic materials 0.000 claims description 9
- 150000003839 salts Chemical class 0.000 claims description 8
- 230000003197 catalytic effect Effects 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 5
- 239000007800 oxidant agent Substances 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 5
- 238000011010 flushing procedure Methods 0.000 claims description 4
- 238000003786 synthesis reaction Methods 0.000 abstract description 5
- 150000001868 cobalt Chemical class 0.000 abstract description 4
- 150000003303 ruthenium Chemical class 0.000 abstract 1
- 238000006722 reduction reaction Methods 0.000 description 45
- 239000011888 foil Substances 0.000 description 25
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 24
- 238000002411 thermogravimetry Methods 0.000 description 13
- 239000011248 coating agent Substances 0.000 description 8
- 238000000576 coating method Methods 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 239000011148 porous material Substances 0.000 description 6
- 239000000243 solution Substances 0.000 description 6
- 239000006185 dispersion Substances 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000001464 adherent effect Effects 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- MRELNEQAGSRDBK-UHFFFAOYSA-N lanthanum(3+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[La+3].[La+3] MRELNEQAGSRDBK-UHFFFAOYSA-N 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 239000012266 salt solution Substances 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- VHUUQVKOLVNVRT-UHFFFAOYSA-N Ammonium hydroxide Chemical compound [NH4+].[OH-] VHUUQVKOLVNVRT-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910002651 NO3 Inorganic materials 0.000 description 1
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 150000004645 aluminates Chemical class 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-N ammonia Natural products N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- 230000003190 augmentative effect Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 150000001869 cobalt compounds Chemical class 0.000 description 1
- QGUAJWGNOXCYJF-UHFFFAOYSA-N cobalt dinitrate hexahydrate Chemical compound O.O.O.O.O.O.[Co+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O QGUAJWGNOXCYJF-UHFFFAOYSA-N 0.000 description 1
- UBEWDCMIDFGDOO-UHFFFAOYSA-N cobalt(II,III) oxide Inorganic materials [O-2].[O-2].[O-2].[O-2].[Co+2].[Co+3].[Co+3] UBEWDCMIDFGDOO-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005137 deposition process Methods 0.000 description 1
- -1 felt Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000000499 gel Substances 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000002459 porosimetry Methods 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000001757 thermogravimetry curve Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/16—Reducing
- B01J37/18—Reducing with gases containing free hydrogen
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J23/00—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00
- B01J23/70—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper
- B01J23/74—Iron group metals
- B01J23/75—Cobalt
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J23/00—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00
- B01J23/70—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper
- B01J23/89—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper combined with noble metals
- B01J23/8913—Cobalt and noble metals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/02—Impregnation, coating or precipitation
- B01J37/024—Multiple impregnation or coating
- B01J37/0242—Coating followed by impregnation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/12—Oxidising
- B01J37/14—Oxidising with gases containing free oxygen
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/30—Catalysts, in general, characterised by their form or physical properties characterised by their physical properties
- B01J35/391—Physical properties of the active metal ingredient
- B01J35/394—Metal dispersion value, e.g. percentage or fraction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/60—Catalysts, in general, characterised by their form or physical properties characterised by their surface properties or porosity
- B01J35/61—Surface area
- B01J35/613—10-100 m2/g
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/60—Catalysts, in general, characterised by their form or physical properties characterised by their surface properties or porosity
- B01J35/63—Pore volume
- B01J35/633—Pore volume less than 0.5 ml/g
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J35/00—Catalysts, in general, characterised by their form or physical properties
- B01J35/60—Catalysts, in general, characterised by their form or physical properties characterised by their surface properties or porosity
- B01J35/64—Pore diameter
- B01J35/647—2-50 nm
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/02—Impregnation, coating or precipitation
- B01J37/0201—Impregnation
- B01J37/0203—Impregnation the impregnation liquid containing organic compounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/02—Impregnation, coating or precipitation
- B01J37/0215—Coating
- B01J37/0225—Coating of metal substrates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J37/00—Processes, in general, for preparing catalysts; Processes, in general, for activation of catalysts
- B01J37/02—Impregnation, coating or precipitation
- B01J37/0215—Coating
- B01J37/0225—Coating of metal substrates
- B01J37/0226—Oxidation of the substrate, e.g. anodisation
Definitions
- This invention relates to a method of preparing a catalyst suitable for use in a Fischer-Tropsch reactor, and to a catalyst made by this method.
- a metal such as iron, cobalt or nickel
- the catalyst would typically be augmented by a promoter such as ruthenium, rhenium or platinum.
- ruthenium, rhenium or platinum These metals can be deposited onto a ceramic support by contacting the ceramic with a solution of a metal salt, calcining it to form an oxide, and then reducing it to metal .
- the activity of the catalyst has also been found to depend on how it is made, because this can affect the size and distribution of the metal crystallites.
- a method of preparing a Fischer-Tropsch catalyst comprising the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists primarily of cobalt; b) reducing the metal oxide to metal by heating in the presence of a reducing atmosphere including hydrogen, the heating process being such as to ramp up the temperature to a maximum temperature below 42O 0 C and above a TGA peak by no more than 30 K over a period of several hours, this temperature ramp being no more than l°C/min while reduction is occurring and including holding the temperature for at least an hour at a temperature above the start of the said TGA peak; c) subjecting the resulting metal to an oxidation process at an elevated temperature, by replacing the reducing atmosphere by an atmosphere containing an oxidising agent, and increasing the proportion of the oxidising agent gradually over a period of hours, to ensure formation of metal oxide,-
- the method comprises the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists of cobalt and less than 2% by weight of ruthenium; b) in the presence of a reducing atmosphere comprising hydrogen, raising the temperature gradually over a period of at least 2 hours to a temperature no more than 125 0 C to ensure the metal oxide is thoroughly dry, and then gradually ramping the temperature to a maximum temperature less than 42O 0 C which is between 20 and 30 K above a second cobalt oxide reduction TGA peak over a period of at least about 20 hours, this temperature ramp being no more than l°C/min while reduction is occurring and including holding the temperature for at least 3 hours at a holding temperature above the start of the second cobalt oxide reduction TGA peak, and then holding the temperature at the maximum temperature for at least 3 hours so the metal oxide undergoes full reduction,- c) while remaining at the
- the appropriate temperatures at which the temperature should be held during the reduction and oxidation steps are preferably determined by monitoring changes of weight during a thermogravimetric analysis (or thermal gravimetric analysis) (TGA) on a specimen of the ceramic support containing the same metal oxide, in a reducing atmosphere.
- TGA thermogravimetric analysis
- the reducing atmosphere in steps (b) and (d) contains no more than 10% hydrogen during the initial stages of reduction; and the concentration of hydrogen may be increased during the later stages of reduction.
- the concentration of hydrogen may be above 90% whilst the temperature is held at the maximum temperature.
- the pressure of the reducing atmosphere may be above atmospheric at least during the later stages of reduction, for example at 3 barg.
- the reducing atmosphere may be at atmospheric pressure and at no more than 10% hydrogen throughout the reduction process .
- the temperature ramp in the first reducing step (b) also includes holding the temperature at a temperature above that of the start of the first cobalt oxide reduction TGA peak.
- the temperature is preferably raised at no more than l°C/min, for example 0.5 or 0.2°C/min.
- the reducing atmosphere is preferably arranged to flow continuously over the substrate, preferably with a space velocity of at least 6000 /hr, more preferably about 8000 /hr.
- This has the benefit of preventing the development of hot-spots, and also removing water vapour (formed by the reduction process) , so suppressing the formation of aluminates and oxides and hydrothermal ageing of the support if the ceramic comprises alumina.
- the space velocity in this specification, is defined as the volume flow rate of the gases supplied to a chamber containing the ceramic support (measured at STP) , divided by the void volume of the chamber .
- the ceramic is in the form of a coating on a metal substrate.
- a metal substrate This ensures a well-defined thickness in which the active catalyst metal will be evenly distributed and dispersed.
- the active catalyst metal For example it might be a 100 ⁇ m thick coating on each surface of a metal foil.
- the foil provides mechanical support and also is a heat conductor.
- the metal substrate is a steel alloy that forms an adherent surface coating of aluminium oxide when heated, for example an aluminium-bearing ferritic steel such as iron with 15% chromium, 4% aluminium, and 0.3% yttrium (eg Fecralloy (TM)) .
- TM yttrium
- the substrate may be a wire mesh or a felt sheet, which may be flat, corrugated or pleated, but the preferred substrate is a thin metal foil for example of thickness less than 100 ⁇ m (prior to oxidation) .
- the preferred ceramic is alumina.
- a planar catalyst structure combining the catalyst metal (for example, cobalt) doped into a thin film ceramic support typically between 20 and 150 ⁇ m thick, coated on a thin metal foil, felt, foam or sintered structure typically between 50 and 150 ⁇ m thick
- a thin film ceramic support typically between 20 and 150 ⁇ m thick, coated on a thin metal foil, felt, foam or sintered structure typically between 50 and 150 ⁇ m thick
- the cobalt oxide reduction process is driven by the diffusion of hydrogen gas into the pores of the ceramic, and the counter-diffusion of the water vapour produced by the reduction reaction out of those pores.
- the use of a thin ceramic layer enhances the counter-diffusion process, resulting in lower local concentrations of water vapour and higher concentrations of hydrogen.
- the weight of the cobalt is preferably between 20% and 45% that of the ceramic in which it is distributed, which in the case of a thin alumina coating on a metal foil would be the weight of the alumina coating. Most preferably it is between 25% and 40%, for example 30%.
- the preferred promoter is ruthenium, and in this case its weight may be only a hundredth that of the catalyst metal .
- the promoter is preferably co- deposited with the catalyst metal, by mixing a small proportion of a salt of the promoter with the solution of the catalyst metal salt.
- step (a) the contacting, drying and calcining (step (a) ) is carried out on ceramic material in the form of a powder; the powder is then milled to a suitable particle size of say 10 or 20 ⁇ m (if necessary) , combined with a suitable binder, and coated onto a metal substrate prior to the subsequent reduction, oxidation and reduction steps.
- the reduction/oxidation/reduction process of the invention produces a highly active catalyst, for example having an activity up to 50% greater than that obtained with a single reduction step.
- Figure 1 shows graphically a temperature reduction profile obtained by thermogravimetric analysis, in a flow of a reducing atmosphere
- Figure 2 shows graphically a temperature reduction profile obtained in the same way as that of figure 1, on a different specimen.
- the following example is of a cobalt catalyst with a ruthenium promoter, in a porous gamma-alumina coating on a Fecralloy foil.
- the foil is corrugated, and is intended for use in a flow channel in a compact catalytic reactor for performing Fischer-Tropsch synthesis. The process is described in relation to one foil, but in practice you would usually make several foils at once.
- the weighed foil is heated to about 55O 0 C, and is repeatedly and lightly sprayed with the well -mixed alumina suspension, to form a coating about 120 ⁇ m thick on each side. It is then cooled down to room temperature again.
- the alumina is then dehydroxylated (calcined) by putting the coated foil in a furnace through which dry air is passed, and heated at l°C/min up to 100 0 C, held for 4 hours at this temperature, and then heated at the same rate up to 55O 0 C, and held for another 4 hours. It is then cooled back to room temperature. The alumina adheres tenaciously to the foil. At this point the coated foil can be weighed, to determine the mass and final thickness (about 80 ⁇ m) of alumina.
- a mixed salt solution is made by combining 212.6 g of cobalt nitrate hexahydrate with a 1.7 g of ruthenium
- the proportion of catalytic metal in the ceramic is preferably arranged to be between 28% and 45%.
- the addition of the mixed salt solution, drying, and calcining are repeated three times, so the expected amount of cobalt is about 30% of the weight of the alumina.
- the foils are installed in flow channels of a Fischer-Tropsch reactor at this stage, the subsequent steps being performed in the reactor, or the foils may be put in a stainless steel tube.
- thermogravimetric analysis Before reducing the cobalt oxide, a specimen of the alumina is removed at this stage, and is subjected (in the form of a powder) to a thermogravimetric analysis, heating it at for example 0.5°C/min up to 700 0 C in an atmosphere of argon with 5% hydrogen, while monitoring any changes of weight.
- thermogravimetric analysis heating it at for example 0.5°C/min up to 700 0 C in an atmosphere of argon with 5% hydrogen, while monitoring any changes of weight.
- the second significant thermal event, the peak marked B, corresponds to the reduction of CoO to Co metal; this is referred to as the second cobalt oxide reduction peak.
- the graph shows that this stage starts at about 21O 0 C and occurs most vigorously at about 35O 0 C, whereas in the example of figure 2 this second stage starts at about 26O 0 C and occurs most vigorously at about 37O 0 C. After completion of these reduction stages, there are no significant further thermal events.
- the shape of the graph that is to say the characteristic positions, magnitude and shapes of the reduction maxima A and B, is different for different proportions of cobalt and ruthenium on the alumina, and may also be affected by the pH of the alumina dispersion that was deposited, and by the method by which cobalt was impregnated into it (such as the solvent and the organic or inorganic cobalt salt used) .
- the graphs can be assumed to also be the same. It will be appreciated that the deposition process described above may be varied for example by using a solution of a different cobalt salt in a different solvent.
- the foil (or foils) are then reduced, with a supply of dry argon containing 5% hydrogen passing though the reactor channels (or the tube) flowing though at a space velocity of 8000 /hr.
- a supply of dry argon containing 5% hydrogen passing though the reactor channels (or the tube) flowing though at a space velocity of 8000 /hr.
- the temperature is ramped at 3°C/min to 8O 0 C, and held for an hour; the temperature is then increased at 3°C/min to 12O 0 C and held for an hour to ensure the foils are thoroughly dried (in case they may have picked up moisture from the atmosphere) .
- the temperature is then raised at 0.5°C/min to about 17O 0 C (this temperature is set at 10 K below the maximum of the TGA peak in this vicinity, which is the first cobalt oxide reduction peak) , the pressure (in this example) is increased to 3 barg, and the temperature is held for two hours.
- the temperature is then ramped at 0.2°C/min to 25O 0 C (this temperature being set above the start of the second cobalt oxide reduction peak) , and then held for 16 hours to allow slow initiation of the second reduction step.
- the temperature is then ramped at 0.2°C/min from 25O 0 C up to about 375 0 C (this maximum temperature being set at 25 K above the maximum of the second cobalt oxide reduction peak) , where it is held for 2 hours.
- the gas mixture is then replaced with pure hydrogen at the same pressure and the same space velocity as before, and the temperature held at this maximum temperature for at least a further 30 hours.
- the reduction process described above is by way of example only; the reduction process can be modified, for example holding the temperature at 25O 0 C for even longer, for example for 60 hours, and the temperature might be held for longer at the maximum temperature, for example for 46 hours, or each hold may be for a shorter period of only a few hours.
- the gas might contain less than 10% hydrogen, and the pressure may be held at or near atmospheric pressure, throughout the reduction process. Indeed the temperature holds at 25O 0 C and 375 0 C can be decreased to 4 hours each, with no change to the activity of the resulting catalyst.
- the catalyst-carrying foils are then subjected to a gradual oxidation procedure. While still at the maximum temperature in the reduction procedure (about 375 0 C) , the pressure is reduced to atmospheric and the reducing gases are flushed out with dry helium at a space velocity of 14,000 /hr for 10 minutes. Over a period of six hours, air is gradually introduced into the gas flow, while continuously checking the temperature of the foils,- if the temperature increases by more than 5 K then the proportion of air is reduced to the previous value. The time steps are as shown in the table.
- the foils are then subjected to a second reduction procedure, which is similar to the first reduction procedure.
- the temperature is lowered to the value of about 25O 0 C mentioned before, and the air is purged out using helium at a space velocity of 8000 /hr.
- the gas is then changed to dry argon with 5% hydrogen, at the same space velocity, and the temperature is held at 25O 0 C with this reducing atmosphere for 2 hours.
- the pressure is then raised to 3 barg, and the temperature is then ramped at 0.2°C/min from 25O 0 C up to about 375 0 C (the maximum temperature used previously) , where it is held for 2 hours.
- the gas mixture is then replaced with pure hydrogen at the same pressure and the same space velocity as before, and the temperature held at this maximum temperature for at least a further 30 hours.
- the gas may be less than 10% hydrogen, and the pressure be at or near atmospheric, throughout the reduction process.
- the use of this low hydrogen concentration during both the first and second reduction steps has been found to produce as active a catalyst as is produced using higher concentration and pressure. And (as with the first reduction step) the temperature need only be held at 375 0 C for 4 hours. 5. Quality Checks
- the resulting catalyst foils, or specimens of the ceramic removed from the surface are preferably then subjected to measurements of several different parameters, to ensure quality.
- the ceramic will have mesopores, of characteristic size in the range 2 nm to 20 nm, which provide the majority of sites for the dispersed catalyst metal .
- the pores are of size between 8 and 16 nm, more preferably between 12 and 14 nm.
- For Fischer-Tropsch synthesis it is also necessary for there to be larger mesopores and also macropores, that is to say pores of size at least 50 nm and above.
- the specific surface area of the catalyst-containing ceramic is preferably about 60-140 m 2 /g (as measured by the BET gas adsorption technique), for example 90 m 2 /g.
- the specific pore volume, as measured by mercury intrusion porosimetry, of the as-supplied particulate alumina is preferably in the range 0.35 to 0.59 cm 3 /g; while that of the catalyst-containing ceramic is in the range 0.20 to 0.30 cm 3 /g (as measured by the BET technique), for example 0.24 cm 3 /g.
- the dispersion of cobalt is desirably in the range between 0.06 and 0.15 (that is to say the proportion of cobalt metal atoms which are exposed at surfaces of or within the ceramic) .
- the extent of reduction of cobalt in the final material is between 90% and 100%.
- the hydrogen chemisorption is preferably between 100 and 300 micromoles/g of catalyst-containing ceramic.
- the method of the invention enables a highly active Fischer-Tropsch catalyst to be made, the catalyst comprising active catalytic metal in a ceramic support on a metal substrate.
- the metal substrate suppresses the development of hotspots during use of the catalyst so that the highly active catalyst does not overheat and deteriorate. If the maximum temperature for reduction goes more than about 25 K above the TGA peak, the dispersion becomes less and the activity decreases. If the maximum temperature for reduction is less than about 20 K above the TGA peak, the dispersion will be too high, and the catalyst will be too active and non- selective .
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Abstract
A catalyst for Fischer-Tropsch synthesis comprises cobalt catalyst metal on a ceramic support. It can be made by (a) contacting a ceramic support with a solution of a cobalt salt; (b) drying and then calcining, to form cobalt oxide; (c) in the presence of a reducing atmosphere comprising hydrogen, raising the temperature gradually to about 375°C, so the cobalt oxide undergoes reduction; (d) gradually oxidising cobalt back to cobalt oxide at an elevated temperature; and (e) again reducing the cobalt oxide to cobalt using hydrogen and the same reducing temperatures as previously. During the first reducing step the temperature is held at a value above the start of the second cobalt oxide reduction peak on a TGA trace. Ruthenium as a promoter can be deposited along with the cobalt, by combining a ruthenium salt with the solution of the cobalt salt.
Description
FISCHER-THOPSCH CATALy-JT PREPARATION
This invention relates to a method of preparing a catalyst suitable for use in a Fischer-Tropsch reactor, and to a catalyst made by this method.
The use of a metal such as iron, cobalt or nickel as a catalyst for a Fischer-Tropsch synthesis is well known. For this synthesis reaction the catalyst would typically be augmented by a promoter such as ruthenium, rhenium or platinum. These metals can be deposited onto a ceramic support by contacting the ceramic with a solution of a metal salt, calcining it to form an oxide, and then reducing it to metal . However the activity of the catalyst has also been found to depend on how it is made, because this can affect the size and distribution of the metal crystallites.
According to the present invention there is provided a method of preparing a Fischer-Tropsch catalyst comprising the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists primarily of cobalt; b) reducing the metal oxide to metal by heating in the presence of a reducing atmosphere including hydrogen, the heating process being such as to ramp up the temperature to a maximum temperature below 42O0C and above a TGA peak by no more than 30 K over a period of several hours, this temperature ramp being no more than l°C/min while reduction is occurring and including holding the temperature for at least an hour at a temperature above the start of the said TGA peak; c) subjecting the resulting metal to an oxidation process at an elevated temperature, by replacing the reducing atmosphere by an atmosphere containing an oxidising agent, and increasing the proportion of the oxidising
agent gradually over a period of hours, to ensure formation of metal oxide,- d) and then subjecting the resulting metal oxide to a reduction process at temperatures less than or up to substantially the said maximum temperature so the metal oxide is again reduced to metal .
More preferably, the method comprises the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists of cobalt and less than 2% by weight of ruthenium; b) in the presence of a reducing atmosphere comprising hydrogen, raising the temperature gradually over a period of at least 2 hours to a temperature no more than 1250C to ensure the metal oxide is thoroughly dry, and then gradually ramping the temperature to a maximum temperature less than 42O0C which is between 20 and 30 K above a second cobalt oxide reduction TGA peak over a period of at least about 20 hours, this temperature ramp being no more than l°C/min while reduction is occurring and including holding the temperature for at least 3 hours at a holding temperature above the start of the second cobalt oxide reduction TGA peak, and then holding the temperature at the maximum temperature for at least 3 hours so the metal oxide undergoes full reduction,- c) while remaining at the maximum temperature, flushing out the reducing atmosphere and introducing a gas containing oxygen, increasing the proportion of oxygen gradually over a period of at least 3 hours, and then holding the proportion of oxygen for a period of at least 6 hours, to ensure formation of the metal oxide,- d) then flushing out the oxygen-containing gas, lowering the temperature to the holding temperature, introducing a reducing atmosphere, and gradually ramping the temperature up to the maximum temperature, and then holding the temperature at that value for at least 3 hours so the metal oxide again undergoes reduction.
The appropriate temperatures at which the temperature should be held during the reduction and oxidation steps are preferably determined by monitoring changes of weight during a thermogravimetric analysis (or thermal gravimetric analysis) (TGA) on a specimen of the ceramic support containing the same metal oxide, in a reducing atmosphere.
Preferably the reducing atmosphere in steps (b) and (d) contains no more than 10% hydrogen during the initial stages of reduction; and the concentration of hydrogen may be increased during the later stages of reduction. The concentration of hydrogen may be above 90% whilst the temperature is held at the maximum temperature. The pressure of the reducing atmosphere may be above atmospheric at least during the later stages of reduction, for example at 3 barg. Alternatively the reducing atmosphere may be at atmospheric pressure and at no more than 10% hydrogen throughout the reduction process .
Preferably the temperature ramp in the first reducing step (b) also includes holding the temperature at a temperature above that of the start of the first cobalt oxide reduction TGA peak.
During the reduction process the temperature is preferably raised at no more than l°C/min, for example 0.5 or 0.2°C/min.
The reducing atmosphere is preferably arranged to flow continuously over the substrate, preferably with a space velocity of at least 6000 /hr, more preferably about 8000 /hr. This has the benefit of preventing the development of hot-spots, and also removing water vapour (formed by the reduction process) , so suppressing the formation of aluminates and oxides and hydrothermal ageing of the support if the ceramic comprises alumina.
The space velocity, in this specification, is defined as the volume flow rate of the gases supplied to a chamber containing the ceramic support (measured at STP) , divided by the void volume of the chamber .
Preferably the ceramic is in the form of a coating on a metal substrate. This ensures a well-defined thickness in which the active catalyst metal will be evenly distributed and dispersed. For example it might be a 100 μm thick coating on each surface of a metal foil. The foil provides mechanical support and also is a heat conductor. Preferably the metal substrate is a steel alloy that forms an adherent surface coating of aluminium oxide when heated, for example an aluminium-bearing ferritic steel such as iron with 15% chromium, 4% aluminium, and 0.3% yttrium (eg Fecralloy (TM)) . When this metal is heated in air it forms an adherent oxide coating of alumina, which protects the alloy against further oxidation and against corrosion. The substrate may be a wire mesh or a felt sheet, which may be flat, corrugated or pleated, but the preferred substrate is a thin metal foil for example of thickness less than 100 μm (prior to oxidation) . The preferred ceramic is alumina.
Use of a planar catalyst structure combining the catalyst metal (for example, cobalt) doped into a thin film ceramic support (typically between 20 and 150 μm thick, coated on a thin metal foil, felt, foam or sintered structure typically between 50 and 150μm thick) leads to a number of benefits. During the reduction phases it is critical to minimise the partial pressure of water vapour, to avoid the formation of undesired cobalt compounds that are resistant to reduction to metal; the formation of such compounds is promoted by high water vapour partial pressure and by high local temperatures. The cobalt oxide reduction process is driven by the diffusion of hydrogen gas into the pores of the ceramic, and the counter-diffusion of the water vapour produced by
the reduction reaction out of those pores. The use of a thin ceramic layer enhances the counter-diffusion process, resulting in lower local concentrations of water vapour and higher concentrations of hydrogen.
An additional benefit arises from the fact that the metal substrate combined with the thin layer of ceramic support enhances the heat transfer to and from the sites at which reduction or oxidation are occurring, so that substantially isothermal conditions can be maintained within the ceramic support during all the steps of the process. This leads to a more uniform distribution of cobalt crystallites within the catalyst, and it also allows a shorter process time than would be necessary with a more conventional pellet or spherical geometry. Thus this planar geometry provides a particularly effective heat and mass transfer environment for the chemical reactions, so that higher temperature ramp rates can be employed than with a conventional catalyst geometry, and that lower reductant and oxidant gas pressures and concentrations can be employed, because the diffusion path lengths are shorter.
The weight of the cobalt is preferably between 20% and 45% that of the ceramic in which it is distributed, which in the case of a thin alumina coating on a metal foil would be the weight of the alumina coating. Most preferably it is between 25% and 40%, for example 30%. There should also be a promoter combined with the catalyst metal, and this is required in a much smaller proportion, typically no more than a tenth the amount of the catalyst metal . The preferred promoter is ruthenium, and in this case its weight may be only a hundredth that of the catalyst metal . The promoter is preferably co- deposited with the catalyst metal, by mixing a small proportion of a salt of the promoter with the solution of the catalyst metal salt. Consequently the promoter is subjected to calcination and then reduction along with the catalyst metal .
In one option the contacting, drying and calcining (step (a) ) is carried out on ceramic material in the form of a powder; the powder is then milled to a suitable particle size of say 10 or 20 μm (if necessary) , combined with a suitable binder, and coated onto a metal substrate prior to the subsequent reduction, oxidation and reduction steps.
The reduction/oxidation/reduction process of the invention produces a highly active catalyst, for example having an activity up to 50% greater than that obtained with a single reduction step.
The invention will now be further and more particularly described, by way of example only, and with reference to the accompanying drawings, in which:
Figure 1 shows graphically a temperature reduction profile obtained by thermogravimetric analysis, in a flow of a reducing atmosphere; and
Figure 2 shows graphically a temperature reduction profile obtained in the same way as that of figure 1, on a different specimen.
The following example is of a cobalt catalyst with a ruthenium promoter, in a porous gamma-alumina coating on a Fecralloy foil. The foil is corrugated, and is intended for use in a flow channel in a compact catalytic reactor for performing Fischer-Tropsch synthesis. The process is described in relation to one foil, but in practice you would usually make several foils at once.
1. Production of Ceramic Layer Containing Cobalt Oxide
The annealed and shaped foil is heated to 95O0C in air to ensure it has an oxide surface. It is then cooled back to room temperature, cleaned with water, and then degreased for example with acetone. An alumina suspension is made by blending 25 g dispersible alumina (e.g. Dispal 18N4-80 (TM)) with 700 g water to form a sol in a Silverson mixer with a high shear head; a small amount of 10% aqueous ammonia is added to raise the pH to between 8.5 and 9.0, at which pH it gels, becomes white and forms a smooth viscous paste,- then 270 g of gamma- alumina particles (of average size 30 μm) (e.g. Catal (TM) 601 FC), surface area 140 m2/g, containing about 3% lanthana) are added, mixed and well sheared. The weighed foil is heated to about 55O0C, and is repeatedly and lightly sprayed with the well -mixed alumina suspension, to form a coating about 120 μm thick on each side. It is then cooled down to room temperature again.
The alumina is then dehydroxylated (calcined) by putting the coated foil in a furnace through which dry air is passed, and heated at l°C/min up to 1000C, held for 4 hours at this temperature, and then heated at the same rate up to 55O0C, and held for another 4 hours. It is then cooled back to room temperature. The alumina adheres tenaciously to the foil. At this point the coated foil can be weighed, to determine the mass and final thickness (about 80 μm) of alumina.
A mixed salt solution is made by combining 212.6 g of cobalt nitrate hexahydrate with a 1.7 g of ruthenium
(III) 2, 4-pentanedionate (equivalent to a Co: Ru ratio of 100:1), and making up to 750 ml with acetone. Using a microlitre syringe, 25 microlitres of the solution is added dropwise to each 0.01 g of alumina, ensuring that it spreads evenly. On reduction this will provide about 10% (weight) cobalt.
The foil is then dried at 8O0C in a forced air oven for up to about 4 hours, until it appears dry on the surface. It is then placed in a tube furnace, through which heated dry air is passed at a space velocity of about 3000 /hr, and dried and calcined. This is achieved by raising the temperature of the air and furnace at l°C/min to 12O0C and holding the temperature at that for 16 hours,- and then raising the temperature at the same rate to 25O0C, and holding it for 6 hours. This ensures that the salts break down, to give the oxides. It is then allowed to cool. Introduction of only a small proportion of cobalt at any one time, and use of a solvent with a comparatively low surface tension, ensures that cobalt particles with a narrow size distribution are deposited within the pores of the alumina.
The proportion of catalytic metal in the ceramic is preferably arranged to be between 28% and 45%. In this example, the addition of the mixed salt solution, drying, and calcining are repeated three times, so the expected amount of cobalt is about 30% of the weight of the alumina. Preferably the foils are installed in flow channels of a Fischer-Tropsch reactor at this stage, the subsequent steps being performed in the reactor, or the foils may be put in a stainless steel tube.
Before reducing the cobalt oxide, a specimen of the alumina is removed at this stage, and is subjected (in the form of a powder) to a thermogravimetric analysis, heating it at for example 0.5°C/min up to 7000C in an atmosphere of argon with 5% hydrogen, while monitoring any changes of weight. Referring to the figures, there are shown resulting differential thermogravimetric graphs as observed with two different specimens. The graphs show the percentage change of mass for every degree rise in temperature (i.e. the rate of change of mass, as a percentage of the total mass, plotted against temperature) , and provides detailed information as to the temperatures at which the two major stages in the
reduction occur. In each case there is a small peak P, which is understood to correspond to removal of hydroxyl groups and residual nitrate, this being observed at a temperature in the range 160-1800C. There are then two successive larger thermal peaks: the first thermal event, the peak marked A, is believed to correspond to the reduction of Co3O4 to CoO; this is referred to as the first cobalt oxide reduction peak. In the example of figure 1 the graph shows that this stage starts at about 16O0C, and occurs most vigorously at about 1820C, whereas in the example of figure 2 this stage starts at about 18O0C and occurs most vigorously at about 2000C. The second significant thermal event, the peak marked B, corresponds to the reduction of CoO to Co metal; this is referred to as the second cobalt oxide reduction peak. In the example of figure 1 the graph shows that this stage starts at about 21O0C and occurs most vigorously at about 35O0C, whereas in the example of figure 2 this second stage starts at about 26O0C and occurs most vigorously at about 37O0C. After completion of these reduction stages, there are no significant further thermal events.
It will be appreciated that this test need only be carried out if the position and extent of the reduction events are not already known. The shape of the graph, that is to say the characteristic positions, magnitude and shapes of the reduction maxima A and B, is different for different proportions of cobalt and ruthenium on the alumina, and may also be affected by the pH of the alumina dispersion that was deposited, and by the method by which cobalt was impregnated into it (such as the solvent and the organic or inorganic cobalt salt used) . For different foils produced from the same batch of alumina dispersion, and with the same proportions of cobalt and ruthenium deposited in the same way, the graphs can be assumed to also be the same. It will be appreciated that the deposition process described above
may be varied for example by using a solution of a different cobalt salt in a different solvent.
2. First Reduction Procedure
The foil (or foils) are then reduced, with a supply of dry argon containing 5% hydrogen passing though the reactor channels (or the tube) flowing though at a space velocity of 8000 /hr. Starting at ambient temperature the temperature is ramped at 3°C/min to 8O0C, and held for an hour; the temperature is then increased at 3°C/min to 12O0C and held for an hour to ensure the foils are thoroughly dried (in case they may have picked up moisture from the atmosphere) .
In the following explanation it will be assumed that the ceramic has the TGA profile shown in figure 1.
The temperature is then raised at 0.5°C/min to about 17O0C (this temperature is set at 10 K below the maximum of the TGA peak in this vicinity, which is the first cobalt oxide reduction peak) , the pressure (in this example) is increased to 3 barg, and the temperature is held for two hours. The temperature is then ramped at 0.2°C/min to 25O0C (this temperature being set above the start of the second cobalt oxide reduction peak) , and then held for 16 hours to allow slow initiation of the second reduction step. The temperature is then ramped at 0.2°C/min from 25O0C up to about 3750C (this maximum temperature being set at 25 K above the maximum of the second cobalt oxide reduction peak) , where it is held for 2 hours. The gas mixture is then replaced with pure hydrogen at the same pressure and the same space velocity as before, and the temperature held at this maximum temperature for at least a further 30 hours.
It will be appreciated that the reduction process described above is by way of example only; the reduction process can be modified, for example holding the
temperature at 25O0C for even longer, for example for 60 hours, and the temperature might be held for longer at the maximum temperature, for example for 46 hours, or each hold may be for a shorter period of only a few hours. And the gas might contain less than 10% hydrogen, and the pressure may be held at or near atmospheric pressure, throughout the reduction process. Indeed the temperature holds at 25O0C and 3750C can be decreased to 4 hours each, with no change to the activity of the resulting catalyst.
3. Oxidation Procedure
The catalyst-carrying foils are then subjected to a gradual oxidation procedure. While still at the maximum temperature in the reduction procedure (about 3750C) , the pressure is reduced to atmospheric and the reducing gases are flushed out with dry helium at a space velocity of 14,000 /hr for 10 minutes. Over a period of six hours, air is gradually introduced into the gas flow, while continuously checking the temperature of the foils,- if the temperature increases by more than 5 K then the proportion of air is reduced to the previous value. The time steps are as shown in the table.
Table
Space velocity Proportion of Dry Air Hold for
14 000 /hr 0.25% 5 min
14 000 /hr 0.60% 10 min
14 000 /hr 0.85% 10 min
14 000 /hr 1.36% 10 min
14 000 /hr 2.10% 20 min
12 850 /hr 2.35% 10 min
12 850 /hr 3.0% 10 min
13 160 /hr 4.6% 20 min
12 050 /hr 8.0% 10 min
13 050 /hr 14.8% 10 min
11 600 /hr 16.7% 10 min
10 150 /hr 19.0% 10 min
8 700 /hr 22.2% 10 min
7 250 /hr 26.7% 20 min
8 200 /hr 35.3% 30 min 9 150 /hr 42.1% 10 min
6 300 /hr 61.5% 10 min
5 100 /hr 76.2% 10 min
3 900 /hr 100% 8 hr
4. Second Reduction Procedure
The foils are then subjected to a second reduction procedure, which is similar to the first reduction procedure. The temperature is lowered to the value of about 25O0C mentioned before, and the air is purged out using helium at a space velocity of 8000 /hr. The gas is then changed to dry argon with 5% hydrogen, at the same space velocity, and the temperature is held at 25O0C with this reducing atmosphere for 2 hours. The pressure is then raised to 3 barg, and the temperature is then ramped at 0.2°C/min from 25O0C up to about 3750C (the maximum temperature used previously) , where it is held for 2 hours. The gas mixture is then replaced with pure hydrogen at the same pressure and the same space velocity as before, and the temperature held at this maximum temperature for at least a further 30 hours.
In a modification the gas may be less than 10% hydrogen, and the pressure be at or near atmospheric, throughout the reduction process. The use of this low hydrogen concentration during both the first and second reduction steps has been found to produce as active a catalyst as is produced using higher concentration and pressure. And (as with the first reduction step) the temperature need only be held at 3750C for 4 hours.
5. Quality Checks
The resulting catalyst foils, or specimens of the ceramic removed from the surface, are preferably then subjected to measurements of several different parameters, to ensure quality. The ceramic will have mesopores, of characteristic size in the range 2 nm to 20 nm, which provide the majority of sites for the dispersed catalyst metal . Preferably the pores are of size between 8 and 16 nm, more preferably between 12 and 14 nm. For Fischer-Tropsch synthesis it is also necessary for there to be larger mesopores and also macropores, that is to say pores of size at least 50 nm and above. The specific surface area of the catalyst-containing ceramic is preferably about 60-140 m2/g (as measured by the BET gas adsorption technique), for example 90 m2/g. The specific pore volume, as measured by mercury intrusion porosimetry, of the as-supplied particulate alumina is preferably in the range 0.35 to 0.59 cm3/g; while that of the catalyst-containing ceramic is in the range 0.20 to 0.30 cm3/g (as measured by the BET technique), for example 0.24 cm3/g.
The dispersion of cobalt is desirably in the range between 0.06 and 0.15 (that is to say the proportion of cobalt metal atoms which are exposed at surfaces of or within the ceramic) . The extent of reduction of cobalt in the final material is between 90% and 100%. And the hydrogen chemisorption is preferably between 100 and 300 micromoles/g of catalyst-containing ceramic.
The method of the invention enables a highly active Fischer-Tropsch catalyst to be made, the catalyst comprising active catalytic metal in a ceramic support on a metal substrate. The metal substrate suppresses the development of hotspots during use of the catalyst so that the highly active catalyst does not overheat and deteriorate. If the maximum temperature for reduction goes more than about 25 K above the TGA peak, the
dispersion becomes less and the activity decreases. If the maximum temperature for reduction is less than about 20 K above the TGA peak, the dispersion will be too high, and the catalyst will be too active and non- selective .
Claims
1. A method of preparing a Fischer-Tropsch catalyst comprising the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists primarily of cobalt; b) reducing the metal oxide to metal by heating in the presence of a reducing atmosphere including hydrogen, the heating process being such as to ramp up the temperature gradually to a maximum temperature below 42O0C and above a TGA peak by no more than 30 K over a period of several hours, this temperature ramp being no more than l°C/min while reduction is a occurring and including holding the temperature for at least an hour at a temperature above the start of the said TGA peak; c) subjecting the resulting metal to an oxidation process at an elevated temperature, by replacing the reducing atmosphere by an atmosphere containing an oxidising agent, and increasing the proportion of the oxidising agent gradually over a period of hours, to ensure formation of metal oxide,- d) and then subjecting the resulting metal oxide to a reduction process at temperatures less than or up to substantially the said maximum temperature so the metal oxide is again reduced to metal .
2. A method of preparing a Fischer-Tropsch catalyst comprising the steps of: a) contacting a ceramic support with a solution of a salt of catalytic metal, drying and then calcining, to form the metal oxide, wherein the metal of the resulting metal oxide consists of cobalt and less than 2% by weight of ruthenium; b) in the presence of a reducing atmosphere comprising hydrogen, raising the temperature gradually over a period of at least 2 hours to a temperature no more than 1250C to ensure the metal oxide is thoroughly dry, and then gradually ramping the temperature to a maximum temperature less than 42O0C which is between 20 and 30 K above a second cobalt oxide reduction TGA peak over a period of at least about 20 hours, this temperature ramp being no more than l°C/min while reduction is occurring and including holding the temperature for at least 3 hours at a holding temperature above the start of the second cobalt oxide reduction TGA peak, and then holding the temperature at the maximum temperature for at least 3 hours so the metal oxide undergoes full reduction; c) while remaining at the maximum temperature, flushing out the reducing atmosphere and introducing a gas containing oxygen, increasing the proportion of oxygen gradually over a period of at least 3 hours, and then holding the proportion of oxygen for a period of at least 6 hours, to ensure formation of the metal oxide,- d) then flushing out the oxygen-containing gas, lowering the temperature to the holding temperature, introducing a reducing atmosphere, and gradually ramping the temperature up to the maximum temperature, and then holding the temperature at that value for at least 3 hours so the metal oxide again undergoes reduction.
3. A method as claimed in claim 1 or claim 2 wherein throughout steps (b) and (d) the reducing atmosphere contains no more than 10% hydrogen.
4. A method as claimed in claim 1 or claim 2 wherein in steps (b) and (d) the reducing atmosphere contains no more than 10% hydrogen during the initial stages of reduction; and the method involves increasing the concentration of hydrogen during the later stages of reduction.
5. A method as claimed in claim 4 wherein the concentration of hydrogen is above 90% whilst the temperature is at the maximum temperature.
6. A method as claimed in any one of the preceding claims wherein the temperature ramp in the first reducing step (b) also includes holding the temperature at a temperature above that of the start of the first cobalt oxide reduction TGA peak.
7. A method as claimed in any one of the preceding claims wherein in both the reduction steps the reducing atmosphere is arranged to flow continuously over the substrate, with a space velocity of at least 6000 /hr, more preferably about 8000 /hr.
8. A method as claimed in any one of the preceding claims wherein the oxidation step uses air as a source of oxygen .
9. A catalyst made by a method as claimed in any one of the preceding claims.
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WO2011027104A1 (en) * | 2009-09-01 | 2011-03-10 | Gtl.F1 Ag | Fischer-tropsch catalysts |
WO2011089440A1 (en) * | 2010-01-25 | 2011-07-28 | Compactgtl Plc | Catalytic reactor treatment process |
US8952076B2 (en) | 2004-01-28 | 2015-02-10 | Statoil Asa | Fischer-Tropsch catalysts |
US9242229B2 (en) | 2010-08-09 | 2016-01-26 | Gtl.F1 Ag | Fischer-tropsch catalysts |
US10040054B2 (en) | 2009-11-18 | 2018-08-07 | Gtl.Fi Ag | Fischer-Tropsch synthesis |
US10351779B2 (en) * | 2015-03-31 | 2019-07-16 | Johnson Matthey Public Limited Company | Catalyst precursor, method of preparation and use thereof |
CN114929382A (en) * | 2020-01-10 | 2022-08-19 | 英国石油有限公司 | Process for producing a fischer-tropsch synthesis catalyst and fischer-tropsch start-up process |
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EP0253924A1 (en) * | 1981-10-13 | 1988-01-27 | Shell Internationale Researchmaatschappij B.V. | Synthesis gas conversion using ROR-activated catalyst |
US4729981A (en) * | 1981-10-13 | 1988-03-08 | Shell Internationale Research Maatschappij B.V. | ROR-activated catalyst for synthesis gas conversion |
WO2005011864A1 (en) * | 2003-08-01 | 2005-02-10 | Gtl Microsystems Ag | Alumina-coated metal structure and catalyst structure |
-
2006
- 2006-02-14 GB GBGB0602922.7A patent/GB0602922D0/en not_active Ceased
-
2007
- 2007-02-13 WO PCT/GB2007/050058 patent/WO2007093825A1/en active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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EP0253924A1 (en) * | 1981-10-13 | 1988-01-27 | Shell Internationale Researchmaatschappij B.V. | Synthesis gas conversion using ROR-activated catalyst |
US4729981A (en) * | 1981-10-13 | 1988-03-08 | Shell Internationale Research Maatschappij B.V. | ROR-activated catalyst for synthesis gas conversion |
WO2005011864A1 (en) * | 2003-08-01 | 2005-02-10 | Gtl Microsystems Ag | Alumina-coated metal structure and catalyst structure |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
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US8952076B2 (en) | 2004-01-28 | 2015-02-10 | Statoil Asa | Fischer-Tropsch catalysts |
WO2011027104A1 (en) * | 2009-09-01 | 2011-03-10 | Gtl.F1 Ag | Fischer-tropsch catalysts |
US8969231B2 (en) | 2009-09-01 | 2015-03-03 | Gtl.Fi Ag | Fischer-Tropsch catalysts |
EA022062B1 (en) * | 2009-09-01 | 2015-10-30 | Гтл.Ф1 Аг | Fischer-tropsch catalysts |
US10040054B2 (en) | 2009-11-18 | 2018-08-07 | Gtl.Fi Ag | Fischer-Tropsch synthesis |
WO2011089440A1 (en) * | 2010-01-25 | 2011-07-28 | Compactgtl Plc | Catalytic reactor treatment process |
CN102712849A (en) * | 2010-01-25 | 2012-10-03 | 康帕克特Gtl有限公司 | Catalytic reactor treatment process |
US20120302433A1 (en) * | 2010-01-25 | 2012-11-29 | Compactgtl Plc | Catalytic Reactor Treatment Process |
JP2013517923A (en) * | 2010-01-25 | 2013-05-20 | コンパクトジーティーエル パブリック リミテッド カンパニー | Catalytic reactor treatment method |
US9242229B2 (en) | 2010-08-09 | 2016-01-26 | Gtl.F1 Ag | Fischer-tropsch catalysts |
US10351779B2 (en) * | 2015-03-31 | 2019-07-16 | Johnson Matthey Public Limited Company | Catalyst precursor, method of preparation and use thereof |
CN114929382A (en) * | 2020-01-10 | 2022-08-19 | 英国石油有限公司 | Process for producing a fischer-tropsch synthesis catalyst and fischer-tropsch start-up process |
Also Published As
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GB0602922D0 (en) | 2006-03-22 |
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