AU8829682A - Composite of tib2-graphite - Google Patents
Composite of tib2-graphiteInfo
- Publication number
- AU8829682A AU8829682A AU88296/82A AU8829682A AU8829682A AU 8829682 A AU8829682 A AU 8829682A AU 88296/82 A AU88296/82 A AU 88296/82A AU 8829682 A AU8829682 A AU 8829682A AU 8829682 A AU8829682 A AU 8829682A
- Authority
- AU
- Australia
- Prior art keywords
- article
- tib
- temperature
- dispersion
- forming
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000002131 composite material Substances 0.000 title claims description 33
- 229910002804 graphite Inorganic materials 0.000 title claims description 17
- 239000010439 graphite Substances 0.000 title claims description 17
- 229910033181 TiB2 Inorganic materials 0.000 claims description 57
- 238000000034 method Methods 0.000 claims description 53
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 claims description 49
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 claims description 44
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 42
- 229910052799 carbon Inorganic materials 0.000 claims description 40
- 239000006185 dispersion Substances 0.000 claims description 39
- 238000006243 chemical reaction Methods 0.000 claims description 31
- 239000000203 mixture Substances 0.000 claims description 31
- 238000010438 heat treatment Methods 0.000 claims description 30
- 239000000571 coke Substances 0.000 claims description 27
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical group O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 24
- 239000011230 binding agent Substances 0.000 claims description 23
- 239000002245 particle Substances 0.000 claims description 22
- 239000011301 petroleum pitch Substances 0.000 claims description 22
- 239000011295 pitch Substances 0.000 claims description 22
- 239000006229 carbon black Substances 0.000 claims description 20
- 230000000630 rising effect Effects 0.000 claims description 19
- 239000000376 reactant Substances 0.000 claims description 17
- 229910052782 aluminium Inorganic materials 0.000 claims description 16
- 238000005470 impregnation Methods 0.000 claims description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 14
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 claims description 14
- 150000001639 boron compounds Chemical class 0.000 claims description 14
- 239000007788 liquid Substances 0.000 claims description 14
- 239000011294 coal tar pitch Substances 0.000 claims description 12
- 239000007787 solid Substances 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 238000002156 mixing Methods 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 10
- 238000001816 cooling Methods 0.000 claims description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 6
- 238000007493 shaping process Methods 0.000 claims description 6
- 235000013312 flour Nutrition 0.000 claims description 5
- 238000000465 moulding Methods 0.000 claims description 5
- 238000010000 carbonizing Methods 0.000 claims description 4
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical compound [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 claims description 3
- 239000002008 calcined petroleum coke Substances 0.000 claims description 3
- 238000001035 drying Methods 0.000 claims description 3
- 238000001125 extrusion Methods 0.000 claims description 3
- 229920001971 elastomer Polymers 0.000 claims description 2
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 230000009850 completed effect Effects 0.000 claims 2
- 238000011065 in-situ storage Methods 0.000 claims 2
- 229910004844 Na2B4O7.10H2O Inorganic materials 0.000 claims 1
- 239000012300 argon atmosphere Substances 0.000 claims 1
- 238000005087 graphitization Methods 0.000 claims 1
- 238000000227 grinding Methods 0.000 claims 1
- 239000011440 grout Substances 0.000 claims 1
- PEYVWSJAZONVQK-UHFFFAOYSA-N hydroperoxy(oxo)borane Chemical compound OOB=O PEYVWSJAZONVQK-UHFFFAOYSA-N 0.000 claims 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 claims 1
- 210000004027 cell Anatomy 0.000 description 17
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 10
- 229910052580 B4C Inorganic materials 0.000 description 9
- 239000000463 material Substances 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910003481 amorphous carbon Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 229910001610 cryolite Inorganic materials 0.000 description 3
- 239000003792 electrolyte Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000002006 petroleum coke Substances 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 229910021538 borax Inorganic materials 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 239000011329 calcined coke Substances 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 239000007795 chemical reaction product Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005868 electrolysis reaction Methods 0.000 description 2
- -1 however Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000005011 phenolic resin Substances 0.000 description 2
- 229920001568 phenolic resin Polymers 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000004328 sodium tetraborate Substances 0.000 description 2
- 235000010339 sodium tetraborate Nutrition 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- 238000009736 wetting Methods 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 229920001732 Lignosulfonate Polymers 0.000 description 1
- 229910004835 Na2B4O7 Inorganic materials 0.000 description 1
- KKCBUQHMOMHUOY-UHFFFAOYSA-N Na2O Inorganic materials [O-2].[Na+].[Na+] KKCBUQHMOMHUOY-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- RQMIWLMVTCKXAQ-UHFFFAOYSA-N [AlH3].[C] Chemical compound [AlH3].[C] RQMIWLMVTCKXAQ-UHFFFAOYSA-N 0.000 description 1
- RHZUVFJBSILHOK-UHFFFAOYSA-N anthracen-1-ylmethanolate Chemical compound C1=CC=C2C=C3C(C[O-])=CC=CC3=CC2=C1 RHZUVFJBSILHOK-UHFFFAOYSA-N 0.000 description 1
- 239000003830 anthracite Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011305 binder pitch Substances 0.000 description 1
- 239000004327 boric acid Substances 0.000 description 1
- 150000001642 boronic acid derivatives Chemical class 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000003575 carbonaceous material Substances 0.000 description 1
- 239000011336 carbonized pitch Substances 0.000 description 1
- 210000002421 cell wall Anatomy 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- UQGFMSUEHSUPRD-UHFFFAOYSA-N disodium;3,7-dioxido-2,4,6,8,9-pentaoxa-1,3,5,7-tetraborabicyclo[3.3.1]nonane Chemical compound [Na+].[Na+].O1B([O-])OB2OB([O-])OB1O2 UQGFMSUEHSUPRD-UHFFFAOYSA-N 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 238000010952 in-situ formation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 229920005610 lignin Polymers 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000011331 needle coke Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000005580 one pot reaction Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000013618 particulate matter Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 239000006253 pitch coke Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 239000003039 volatile agent Substances 0.000 description 1
Landscapes
- Ceramic Products (AREA)
Description
Description
COMPOSITE OF TiB2-GRAPHITE
BACKGROUND OF THE INVENTION
Aluminum metal has been produced for 90 years in the Hall cell by electrolysis of alumina in a molten cryolite salt electrolyte bath operating at temperatures in the range of 900º-1000ºC. The reactivity of the molten cryolite, the need for excellent electrical conductivity, and cost considerations have limited the choice of materials for the electrodes and cell walls to the various allotropic forms of carbon.
Typically the Hall cell is a shallow vessel, with the floor forming the cathode, the side walls being a rammed coke-pitch mixture, and the anode being a block suspended in the bath at an anode-cathode separation of a few centimeters. The anode is typically formed from a pitch-calcined petroleum coke blend, prebaked to form a monolithic block of amorphous carbon. The cathode is typically formed from a pre-baked, pitch-calcined anthracite or coke blend, with cast-in-place iron over steel bar electrical conductors in grooves in the bottom side of the cathode. During operation of the Hall cell, only about 25% of the electricity consumed is used for the acnual reduction of alumina to aluminum, with approximately 40% of the current consumed by the voltage drop caused by the resistance of the bath. The ancde-cathode spacing is usually about 4-5 cm., and attempts to lower this distance result in an electrical discharge from the cathode to the anode through
aluminum droplets suspended in the bath.
The molten aluminum is present as a pad in the cell, but is not a quiescent pool due to the factors of preferential wetting of the carbon cathode surface by the cryolite melt in relation to the molten aluminum, causing the aluminum to form droplets, and the erratic movements of the molten aluzd-num from the strong electromagnetic forces generated by the high current density.
The wetting of a solid surface in contact with two immiscible liquids is a function of the surface free energy of the three surfaces, in which the carbon cathode is a low energy surface and consequently is not readily wet by the liquid aluminum. The angle of a droplet of aluminum at the cryolite-aluminum-carbon junction is governed by the relationship
where α12, α13, and α23 are the surface free energies at the aluminum carbon, cryolite-carbon, and cryolite-aluminuιa boundaries, respectively.
If the cathode were a high energy surface, such as would occur if it were a ceramic instead of carbon, it would have a higher contact angle and better wettability with the liquid aluminum. This in turn would tend to smooth out the surface of the liquid aluminum pool and lessen the possibility of interelectrode discharge allowing the anode-cathode distance to be lowered and the thermodynamic efficiency of the cell improved, by decreasing the voltage drop through the bath. Typically, amorphous carbon is a low energy surface, but also is quite durable, lasting for several years duration as a cathode, and relatively inexpensive. However, a cathode or a cathode component such as a TiB2 stud which has better wettability and would permit closer anode-cathode spacing could improve the thermodynamic efficiency and be very cost-effective.
Several workers in the field have developed refractory high free energy material cathodes. U.S. 2,915,442, Lewis, December 1, 1959, claims a process for production of aluminum using a cathode consisting of the bcrides, carbides, and nitrides of Ti, Zr, V, Ta, Nb, and Hf. U.S. 3,028,324, Ransley, April 3, 1962, claims a method of producing aluminum using a mixture of TiC and TiB2 as the cathode. U.S.
3,151,053, Lewis, September 29, 1964, claims a Hall cell cathode conducting element consisting of one of the carbides and borides of Ti, Zr, Ta and Nb. U.S. 3,156,639, Kibby, November 10, 1964, claims a cathode for a Hall cell with a cap of refractory hard metal and dis closes TiB2 as the material of construction. U.S. 3,314,876, Ransley, April 18, 1967, discloses the use of TiB2 for use in Hall cell electrodes. The raw materials must be of high purity particularly in regard to oxygen content, Col. 1, line 73-Col. 2, line 29; Col. 4, lines 39-50, Col. 8, lines 1-24. U.S. 3,400,061, Lewis, September 3, 1968 discloses a cathode comprising a refractory hard metal and carbon, which may be formed in a one-step reaction during calcination. U.S. 4,071,420, Foster, January 31, 1978, discloses a cell for the electrolysis of a metal component in a molten electrolyte using a cathode with refractory hard metal TiB2 tubular elements protruding into the electrolyte. S.N. 043,242, Kaplan et al. (Def. Pub.), filed Xay 29, 1979, discloses Hall cell bottoms of TiB2. Canada 922,384, March 6, 1973, discloses in situ formation of TiB2 during manufacture of arc furnace electrodes. Belgian 882,992, PPG Ind., October 27, 1980, discloses TiB2 cathode plates.
Our co-pending applications, S.N. 186,181 and S.N. 186,182, filed September 11, 1980, disclose related subject matter.
SUMMARY OF THE INVENTION
Titanium Diboride, TiB2 has been proposed for use as a cathodic element in Hall cells, giving an improved performance oyer the amorphous carbon and semi-graphite cathodes presently used. it had previously been known that Titanium Diboride (TiB2) was useful as a cathode component in the electrolytic production of aluminum, when retrofitted in the Hall cell as a replacement for the carbon or semi-graphite form. The electrical efficiency of the cell was improved due to better conductivity, due mainly to a closer anodecathode spacing; and the corrosion resistance was improyed, probably due to increased hardness, chemical inertness and lower solubility as compared to the carbon and graphite fonts.
The principal deterrent to the use of TiB as a Hall cell cathode or cathode component has been the sensitivity to thermal shock and the great material cost, approximately $25/lb., as
compared to the traditional carbonaceous compositions, which cost about $0.60/lb. Also, if the anode-cathode distance could be lowered, the % sayings in electricity would be as follows:
A-C distance % savings
3.8 cm. std.
1.9 cm. 20%
1.3 cm. 27%
1.0 cm. 30%
We have invented an improved process for producing a TiB2-carbon composite which shows excellent performance as a cathode or cathode component in Hall aluminum cells. The method is markedly more economical, and also produces an unexpectedly improved cathode when its performance is compared to the traditional carbonaceous material. The method involyes the use of a titania (TiO2) -graphite composite structure as a starting material. TiO2 is dispersed in the mixture of coke particles and flour, then wetted and dispersed in a carbonizable liquid binder to form a plastic mass. The binder is preferably a coal tar pitch, however, petroleum pitches, phenolic resins, lignin sulfonate, and other carbonizable binders may also be used. The coke particles most useful are selected size ranges of calcined delayed petroleum coke, made by heating a heavy hydrocarbon fraction to about 500º-510ºC and holding the material in a coker drum for about 18 hours, while taking the gas oils vaporizing off to a combination tower for separation and recycling. The solid coke re-sidue remaining is removed, xihen calcined at approximately 1200º-1300ºC to form the calcined coke useful in Hall cell electrodes or electrode components, and for conversion to graphite. Regular coke is isotropic, with a coefficient of thermal expansion (CTE) characteristic of from 10 to 30 x 10-7 cm/cm/ºC, over the range of 0º to 50ºC, relatively uniform on all 3 geometric axes in physical properties, while an acicular or needle coke will generally be anisotropic having a CTE characteristic which is variant on the axes and less than 10 x 10-7 cm/cm/ºC on the principal axis. Coke flour may also be included, using a particle size range with about 50% passing a 79 mesh/cm (200 mesh per in.) screen. The filler carbon in the original formed article may also be obtained from other common sources, such as pitch coke, charcoal and
metallurgical cokes from coal, with a mean particle diameter of about 3 mm being preferable, ana a high surface area/wt. ratio.
The plastic mass is then molded or extruded to form the desired shape and baked on a cycle rising to 700º-1100ºC oyer a period of 1 to 10 days to carbonize the binder, forming a solid C-TiO2 composite.
The baked carbon-TiO2 composite shape produced is a structure containing TiO2 and particulate carbon firmly bound in the matrix of carbonized pitch. The structure is highly porous due to the inherent porosity of the coke, incomplete packing, and the volatilization of about 30-40% of the initial weight of the pitch, and is specially formulated for high porosity.
The baked composite shape is then impregnated in a pressure vessel under alternate cycles of vacuum and about 7 x 103 Pa (100 PSI) pressure with a boron compound alor.e or with a dispersion of B2O3 and carbon black or other micronized carbon in H2O. Either B2O3 or H3BO3 may be used as B2O3 is hydrolyzec to H3BO3 in H2O by the reaction:
B2O3 + 3 H2O - 2 H3BO3 After impregnation with the dispersion, the article is then dried slowly to 100ºC to minimize loss of the solid impregnants while vaporizing the water. Multiple impregnations, each followed by a drying cycle, may be necessary.
Alternately, the article may be impregnated with molten B2O3 or boric acid or with a oarbcn black dispersion in a molten boron compound. A further modificaticn of the above procedure consists of mixing stoichiometric amounts of TiO2, carbon black and B2O3, heating the mixture to melt the B2O3, dispersing the TiO2 and carbon in the molten B2O3, cooling, allowing the paste to harden to a solid, milling the solid to a powder, dispersing the powder in a binder, then using this dispersion as an impregnant. The boron compound ana carbon black may be dispersed in a molten pitch or other carbonizable binder such as a petroleum pitch with a 110º- 120°C softening point, and the resulting dispersion used as an impregnant. Each impregnating cycle will nomally require a bake to the 700º-1100ºC
range, carbonizing the binder.
The process may also be used by mixing boron carbide (B4C) with coke particles and binder in the initial mix, baking, then impregnating the resulting baked piece with a TiO2-carbon black dispersion in a carbonizable binder.
The unique aspect of the process provides a method whereby TiB2 is formed during subsequent heat treatment to a temperature above 2000ºC, while the carbon is being made graphitic. The carbon black or similar finely divided carbon acts as the reductant to minimize consumption of the article matrix during the reaction of TiO2 and B2O3 to form TiB2.
TiO2 + 5 C + B2O → TiB2 + 5 CO ↑
> 1200°C Initial mixing, shaping by molding or extrusion of TiO2, coke, and binder pitch follow the standard practice of the carbon and graphite industry. The article is heat treated at 600º to 1100ºC to carbonize the binder, cooled and is then impregnated as described in a heated pressure vessel at temperatures from 100º-500ºC and pressures from 2-15 x 103 Pa (50-200 PSI).
After drying, the article is heated to the reaction temperature for the formation of TiB2, in the range of 1200º-1800ºC. The reaction starts to take place at about 800ºC but is quite slow below 1200ºC and reaches a high reaction rate at about 1750ºC. The heat treatment may be done in stages, with re-impregnation and reheating cycles to build up the desired concentration of TiB2. Due to the loss of the carbon black ana possibly a portion of the binder and coke as CO during the TiB2 forming reaction, the article may develop excess porosity and consequently have low strength and be poor in other physical properties. This can be remedied by additional impregnation with a carbonizable binder, preferably a petroleum pitch with a softening point in the 110º-123 range, although lignin sulfoπate, phenolic resins and other pitches may be used, under about
7 x 103 Pa (100 PSI) at about 200°-250ºC in a heated pressure vessel.
After impregnation, the article is again heated to the 600º to 1100ºC range over a period of 2 to 10 days to carbonize the pitch, sealing the surface and strengthening the article.
The last step in the process will generally include heating the
article to 2000ºC or higher, converting the carbon to the graphitic form. Generally the temperature range preferred is about 2400º- 2500ºC, although for particular processes any point in the 2000º- 3000º range may be used.
Example 1
A cathode shape is made by mixing coke particles with a mean diameter of 3 mm, coal tar pitch having a softening point of approximately 110º-120ºC and TiO2 in a high-shear heated mixer. The mix is heated to approximately 175 ºand the coke and TiO2 are well dispersed in the molten pitch. The cathodic element is molded at about 14 x 106
Pa (2000 PSI) pressure, then baked on a cycle rising to 720º in six days. After removal from the oven the shape is placed in an autoclave and impregnated with a dispersion of a rubber reinforcing grade of carbon black and B2O3 in H2O, then removed and dried slowly to vaporize the H2O without loss of B2O3. The piece is next heated to 1500ºC, at which temperature the TiO2 and B2O3 react, releasing CO. These gas-producing steps are carried out slowly in order to avoid fissuring due to too rapid gas evolution.
The piece is then re-impregnated, using a petroleum pitch with a softening point of from 110º-120ºC, baked to carbonize the pitch on a six day cycle, the temperature rising to 720ºC, which fills the porosity left by theTiB2 forming reaction, then graphitized by heating to 2400ºC.
Example 2
A mixture is prepared haying the following composition: B2O3 38 wt. %
Carbon black 29 wt. % TiO2 33 wt. %
100 wt. % The solids above are mixed in a sigma type mixer, then heated to the melting point of B2O3 or slightly higher, which may vary considerably with the purity. Pure B2O3 has a melting point of 450ºC but the commercially available grades usually melt at around 275° or slightly higher. The carbon and TiO2 are thoroughly dispersed in the molten B2O3, then the mixture is dumped and allowed to cool and harden. The
solid is ground to a fine particle size dispersion passing a 24 mesh/cm screen (60 mesh/in), then used to form an electrode mix of the following composition:
Above mix 100 parts by wt. Coal tar pitch, S.P. 110°-120°C 32 parts by wt.
This is mixed in a sigma type mixer heated to about 175ºC, dispersing the carbon black and reactive mixture in the melted pitch. After partial cooling, an article is molded, cooled, then baked to 720° over a six day period, carbonizing the binder. It is then heated to about 2000ºC, driving the TiB2 forming reaction to completion while graphitizing the carbon residue. The body thus formed is a very porous semi-graphite-TiB2 composite. The composite is impregnated with petroleum pitch having a 110º-120º softening point under alternate cycles of vacuum and pressure at about 240ºC, and re-baked on the above slow carbonizing cycle to 720º. The impregnation and baking steps are repeated, then the article is re-graphitized at 2300ºC, to form a strong graphite-TiB2 composite with about 60% TiB2 content by wt.
Example 3
A conventional carbon body, which has a high pore volume and is well suited for impregnation, is made from the following composition, by wt. :
Calcined coke particles, maximum particle size 60
12 mm, mean particle size 5 to 10 mm Coke flour, 50% passing 79 mesh/cm screen 40 Coal tar pitch, softening point 110°-120º 25
The mix is blended, shaped and baked as in Example 1. The article is then impregnated under cycles cf vacuum and pressure above the melting point of B2O3 with the mix prepared in Example 2, heated slowly to a TiB forming temperature above 1200ºC, preferably 1750 , held at that temperature for one to four hours, cooled and impregnated with the same petroleum pitch under alternate cycles of vacuum and pressure as above, re-baked as above, and heat treated to a temperature of 2100º or higher.
Example 4
A cathode shape is formed from pitch, coke, and TiO2 and baked as in Example 1. It is then impregnated with a dispersion of carbon black in molten B2O3 at 7 x 103 Pa (100 PSI). After impregnation, it is heated to 1500 for one hour to form TiB2, then cooled, impregnated with petroleum pitch under cycles of vacuum and 7 x 103 Pa at 250°C, re-baked for six days, the temperature reaching 720ºC, then graphitized by heating to 2300°C.
Example 5 A mixture is prepared having the following composition:
% by wt.
B4C 8
Coke particles (3 mm diam.) 36
Carbon black 36 Pitch (S.P. 110°). 20
100
The B4C, coke, and carbon black are mixed in a heated sigma mixer at about 170ºC, the pitch added and the mixture wetted by the molten pitch to form a plastic dispersion. A cathodic element for a Hall cell is formed by molding the dispersion trader about 1.4 x 107 Pa (2000 PSI) and baked on a cycle rising to about 800ºC in six days. After cooling to ambient temperature, the element is impregnated with a dispersion of 30% TiO2 by wt. (ceramic pigment grade) in petroleum pitch (S.P. 110º- 120°C) at 240°C under alternate cycles of vacuum and 6.9 x 105 Pa (100 PSI) pressure. The impregnation and bake steps are repeated to fully impregnate the element. It is next heated slowly to about 1750ºC, at which temperature TiB2 is formed and CO given off, and held at that temperature until the reaction is complete. To further strengthen the element and increase its density, it is re-impregnated with petroleum pitch, rebaked, then heated to about 2400ºC to convert the carbon matrix and particulate matter to a graphitic form.
EXAMPLE 6
Blends of the following dry ingredients are mixed in parts by wt. :
A B C D TiO2 10 50 80 60
Regular Petroleum coke particles (calcined) (mean diam. 3 mm) 90 50 50 40 Coal tar pitch
(S.P. 110°-120°C) 26 28 38 20
Theoretical % TiB2 in composite1 2 8% 57% 79% 77% 1Assuming a 75-80% coke yield from the pitch during the bake cycle from ambient to 700º-1100ºC. 2Assuming complete conversion of TiO2 to TiB2.
TheTiO2 and coke are charged into a sigma type mixer heated to about 160°-175°C and thoroughly blended while being heated. When the dry blend has reached about 160ºC, the pitch is added, melted, and the solid ingredients wetted by the molten pitch. After thorough mixing, the plastic mass is cooled and molded to the desired shape of the article.
The article is baked on a slowly rising temperature cycle, reaching 720°C in a period of 6 days, and removed from the furnace and cooled. After re-heating to about 500°C, the article, at that temperature or higher, is impregnated with moltenB2O3 , under 6.9 x 105 Pa pressure to a final pickup of sufficient boron-containing material to form the surface layer of TiB on further heat treatment.
On further heating the reaction B2O3 + TiO2 + 5 C → TiB2 + 5 CO starts to take place at about 800°C, becomes quite apparent at about 1200°C, and reaches a high reaction rate around 1750ºC. Impregnation can be repeated with re-baking to build the desired quantity of TiB2 in the composite. The article can be heated to 2200ºC or higher to graphitize the carbon, forming the final composite article of graphite-TiB2, with the surface particularly rich in TiB2.
EXAMPLE 7
The TiO2-C composites of Example 6 are prepared and impregnated with molten H3BO3 instead of B2O3, and further treated as in the Example.
EXAMPLE 8
The TiO2-C composites of Example 6 are prepared and impregnated with a water solution of B2O3. B2O3 is hydrated to H3BO3 in water and thus the two are interchangeable. The article is impregnated under 1.7-6.9 x 105 Pa of pressure, dried at about 100ºC, heat treated @ 1200º-2000ºC and the process repeated to build up the desired amount of B compound in the structure of the article. Heat drives the reaction of TiO2 and H3BO3, forming TiB by the overall reaction: TiO2 + 2 H3BO3 + 5 C → TiB2 + 3 H2O + 5 CO. The article may be re-impregnated and re-baked to produce the TiB2-carbon composite, but if aTiB2 -graphite composite is the desired end product, the article is further heated to 2200ºC or higher, which temperature will convert the amorphous C to semigraphite or graphite.
After heating to 1200ºC or higher, at which temperature TiB2 begins to form, some porosity will be present at the surface due to the loss of CO or CO2 formed by the overall reactions involved: TiO2 + 2 H3BO3 + 5 C → TiB2 + 3 H2O + 5 CO 2 C + 2HBO3 → B2O3 + H2O + 2 CO TiO2 + B2O3 + 5 C → TiB2 + 5 CO 2 TiO2 + Na2B4O7 . 10 H2O + 10 C → 2 TiB2 + Na2O + 10H2O + 10 CO.
A re-impregnation under alternate cycles of vacuum and pressure step with pitch or a dispersion of TiO2 or boron compound or with a mixture of both of the reactants (TiO2 and a boron cogιpound) dispersed in a liquid carbonizable binder or impregnant may be used to seal this remaining porosity and densify the article. The. preferred impregnant is a petroleum pitch having a melting point in the 100º-120ºC range used at about 165°-250°C. After impregnation, the article is baked to
700º-1100ºC, and is re-heated to 2200°c or higher to graphitize the carbon residue, and form TiB2.
EXAMPLE 9
B4C (10 g) is dispersed with calcined delayed petroleum coke particles (90 g) having a mean diameter of 3 mm in a sigma mixer and heated to about 170ºC, coal tar pitch (25 g) with a softening point of 110ºC is added, and melted, and a plastic dispersion is formed. A cathodic element is molded under about 1.4 x 107 Pa (2000 PSI), baked on a cycle with the temperature rising to 800ºC in six days. After baking, the element is cooled, then impregnated with a dispersion of TiO in petroleum pitch (30% by wt.) at 240°C with 6.9 x 105 Pa (100 PSI). The impregnation step is repeated with alternate vacuum and pressure cycles. After impregnation, the element is heated to 720ºC over a six day period, then cooled. The impregnation-bake cycle is repeated several times to build up the requiredTiO2 concentration firmly bound in the carbon matrix in the pore volume of the element. After baking, the element is further heated to 1750ºC, which converts the reactants to TiB2. The reaction produces CO as shown, and to seal porosity resulting from the loss of C from the matrix, the element is impregnated with petroleum pitch and baked as above to seal the porosity and strengthen the structure. Alternately, the element may be re-impregnated with the TiO2 dispersion, baked, and re-heated as above. After heating to 1750ºC, to form TiB2, the element is further heated to 2250ºC to convert the carbon matrix to graphite. The final cathodic element has TiB2 concentrated primarily on or near the surface.
The process disclosed uses the reactions forming TiB2 from TiO2, and B4C, B2O3, or other boron compounds to form a TiB2-graphite composite. The process may also be used to form other such composite structures from reactants forming refractory materials. In this instance the reactions are as follows:
TiO2 +B2O3 + 5 C → TiB2 + 5 CO. The reaction above probably proceeds through the formation of
B4C as an intermediate
2 B2O3 + 7 C → B4C + 6 CO
2 TiO2 + B4C + 3 C → 2 TiB2 + 4 CO.
The process is in general the generalized reaction taking place at temperatures in the range of 800º-3000ºC of:
MO + B2O3 + C → MB + CO (where M is a metal) or MO + B4C + C → MB + CO or MO + N + C → MN + CO (where N is a non-metal)
EXAMPLE 10 The article of Example 6, after baking, is impregnated with a dispersion of B4C in petroleum pitch with a softening point of 110º- 120ºC, at 240ºC under several cycles of vacuum and pressure of 6.9 x 105 Pa (100 PSI). After impregnation, the article is re-baked as above, then further heated to 1750ºC to drive the TiB2-forming reaction to completion, re-impregnated with petroleum pitch and re-baked, then heated to 2250ºC to form the graphite-TiB2 composite.
As may be seen, from the above, the process is useful for the formation of a large number of composite structures containing the end product of a reaction occurring at high temperatures in the presence of carbon, whether it enters the reaction or not.
We have found that the use of the approximate stoichiometric equivalents is preferable, e.g., TiO2 (80 g) + B2O3 (70 g) + C (excess) → TiB2 (70 g) + 5 CO ↑. The reaction Ti + 2 B → TiB2 will also occur under these conditions, but is economically unattractive due to the high cost of the elemental reactants. The reaction with borax occurs but is unattractive due to the volume of volatiles produced.
The reaction may occur with a number of boron compounds including borax and borates, however B2O3 and H3BO3 are the most economical and available compounds.
Claims (36)
1. A process for manufacturing a carbon-TiB2 composite article comprising blending coke, a first carbonizable binder and a first TiB2 forming reactant to form a dispersion, shaping said article, baking said article to carbonize said binder, impregnating said article under alternate cycles of vacuum and pressure at least once with a second TiB2-forming reactant in liquid form, and heating said article to aTiB2 -forming temperature to form said carbon-TiB2 composite article.
2. The process of Claims 1, 22, or 23 wherein the coke is a regular calcined petroleum coke having a mean particle diameter of approximately 3 mm.
3. The process of Claims 1, 22, or 23 wherein the binder is a molten coal tar pitch having a softening point from 100º to 120ºC, used at a temperature of approximately 160º to 175º.
4. The process of Claim 1 wherein the first TiB2-forming reactant is TiO2 and the second TiB2-forming reactant comprises a boron compound selected from the group consisting of B4C, B2O3 , H3BO3 and Na2B407 .10H2O.
5. The process of Claim 1 wherein the second TiB2-forming reactant is a boron compound selected from the group consisting of
B4C and B2O3, dispersed in a liquid selected from the group consisting of molten petroleum pitch and phenolic condensates.
6. The process of Claim 1 wherein the second TiB2-forming reactant is molten B2O3, used at about 500ºC.
7. The process of Claim 1 wherein the second TiB2-forming reactant is B2O3 , HBO3, or Na2B4O7 .10H2O in water solution.
The process of Claims 1 or 15 wherein the article is baked on a temnppeerraature cycle rising to 700º to 1100°C over a period of 1 to 10 days.
9. The process of Claims 1 or 15 wherein the article is impregnated with the second TiB2-forming reactant under alternate cycles of vacuum and a pressure of from 1.7 x 105 to 6.9 x 105 Pa (25 to 100 psi).
10. The process of Claims 1 or 15 wherein the article after impregnation is baked on a cycle with the temperature rising to 700º to 1100ºC over a period of 1 to 10 days, then further heated to a TiB2- forming temperature of at least 1200ºC.
11. The process of Claims 1 or 15 wherein after heating to the TiB2-forming temperature the article is further heated to a temperature of at least 2200°C.
12. The process of Claims 1 or 15 wherein the article after heating to the TiB2-forming temperature is cooled, then re-impregnated at least once under alternate cycles of vacuum and pressure with the second TiB2-forming reactant in liquid form, re-baked on a cycle rising to 700° to 1100ºC over a period of 1 to 10 days, and re-heated to the TiB2-forming temperature of at least 1200ºC.
13. The process cf Claims 1, 15, 30, or 35 wherein the article after heating to the TiB2-forming temperature is impregnated with petroleum pitch under alternate cycles of yacuum and pressure at about
240ºC and 6.9 x 105 Pa, re-baked on a cycle rising to 700º to 1100ºC5 over a period of 1 to 10 days, ana heated to at least 2200ºC.
14. The process of Claims 1 or 15 wherein the article is re- impregnated with a dispersion of both the first and second TiB2-forming reactants in petroleum pitch under alternate cycles of vacuum and pressure of 1.7 to 6.9 x 105 Pa at about 240°C, baked on a cycle rising to 700º to 1100ºC over a period of 1 to 10 days, heated to at least 2200ºC to form a TiB2-graphite composite.
15. The process of Claim 1 wherein the first TiB2-forming reactant is a boron compound and the second TiB2-forming reactant is TiO2.
16. The process of Claims 1 or 15 wherein the article is shaped by molding at a pressure of about 1.4 x 107 Pa.
17. The process of Claims 1 or 15 wherein the article is shaped by extrusion.
18. A process of manufacturing a cathodic element for a Hall aluminum cell comprising dispersing a firstTiB2-forming reactant selected from the grout consisting of B4C, H3BO3, and B2O3 and coke particles in molten coal tar pitch binder to form a plastic mass, shaping said mass to form said cathodic element, baking said element on a rising temperature cycle reaching 700º to 1100ºC over a period of 1 to 10 days, removing said element from said furnace, impregnating said element under a pressure of about 6.9 x 105 Pa with TiO2 dispersed in molten petroleum pitch, re-baking said element to 700º to 1100ºC over a period of 1 to 10 days, heating said element to 1750ºC to form a carbon- TiB2 composite, re-inpregnating said element with said petroleum pitch at about 240°C under about 6.9 x 105 Pa pressure, re-baking said element to 700° to 1100ºC over 1 to 10 days, and heating said element to 2250ºC in an argon atmosphere to form a graphite-TiB2 composite cathodic element.
19. A process of manufacturing a cathodic TiB2-graphite element for a Hall aluminum cell comprising dispersing TiO2 and coke particles in molten coal tar pitch to form a plastic mass, forming said element by molding or extrusion, baking said element on a rising temperature cycle over a period of 1 to 10 days, the temperature reaching from
700º to 1100ºC, cooling said element, impregnating said element under alternate cycles of vacuum and a pressure of from 1.7 to 6.9 x 105 Pa with a boron compound selected from the group consisting of molten B2O3, at approximately 500ºC, molten H3BO3 at approximately 500ºC, B2O3 in water solution, H3BO3 in water solution, and B4C dispersed in molten petroleum pitch, drying said element at a temperature of approximately 100ºC if a water solution was used when impregnating said element, re-baking said element on a 1 to 10 day cycle, rising to 700º to 1100ºC, heating said element to approximately 1750ºC, cooling, and re-impregnating said element with said molten petroleum pitch, baking said element over a 1 to 10 day cycle, rising to 700º to 1100ºC, and heating to approximately 2250ºC to form said TiB2-graphite element.
20. A product made by the process of Claims 1, 15, 18 or 19.
21. A method of operating an electrolytic aluminum reduction cell using as a cathode component the product made by the process of
Claims 1, 15, 18 or 19.
22. In a process for the production of a TiB2-graphite composite article by an in situ reaction, of carbon, a boron compound and TiO2, the improvement comprising the use. of carbon black as a source of carbon for said in situ reaction.
23. A process for the production of a composite TiB2-graphitic carbon article comprising the steps of:
1) Mixing TiO2, coke, and a liquid carbonizable binder to form a first plastic dispersion; 2) Shaping said dispersion to form an article;
3) Baking said article to carbonize said binder on a cycle from 1 to 10 days rising to a final temperature from 600º to 1100°C; 4) Dispersing carbon black in liquid B2O3 to form a second dispersion; 5) Impregnating said baked article with said second dispersion under a pressure from
2 to 15 x 103 Pa at a temperature from
100º to 500ºC;
6) Heating the impregnated, baked article to at least 1200ºC to a Tι3 forming temperature and maintaining that temperature until the TiB2 forming reaction is substantially completed;
7) Heating the article from 6) to at least
2100ºC to form saidTiB2-graphitic carbon comoosite article.
24. The process of Claims 22, 23, 30, 32, or 35 wherein the carbon used is a rubber reinforcing grade of carbon black.
25. The process of Claims 23 or 35 wherein after the article is heated to the TiB2 forming temperature, it is cooled, then impregnated under from 2 to 15 x 103 Pa pressure at from 200º to 250ºC witn a petroleum pitch having a softening point from 110º to 120ºC, tnen naked on a cycle with the temperature rising to 600º to 1100ºC over 2 to 10 days before graphitization at 2300ºC .
26. The process of Claims 23 or 35 wherein the article is impregnated with the second dispersion and baked a plurality of times, dried, then heated to a TiB2 forming temperature.
27. The process of Claim 23 wherein the second dispersion is a dispersion of carbon black in molten B2O3.
28. The process of Claim 23 wherein the second dispersion is a dispersion of carbon black and B2O3 in H2O, the article then being heated to about 100ºC to vaporize the H2O.
29. The process of Claim 26 wherein after heating to a boride forming temperature the article is re-impregnated with the second dispersion under alternate cycles of vacuum and pressure of from 2 to 15 x 103 Pa at 200º to 250ºC, rebaked on a cycle of 2 to 10 days, the temperature rising to 700º to 1100ºC, then graphitized at a temperature of 2300°C.
30. A process for the production of a composite TiB2-graphite article comprising the steps of:
1) Mixing B2O3, particulate carbon, and TiO2 to form a mixture; 2) Heating said mixture to the melting point of said B2O3;
3) Dispersing said carbon and said TiO2 in said B2O3 to form a plastic mixture;
4) Dumping said mixture, allowing it to harden to a solid;
5) Grinding said solid to particles passing a 24 mesh/cm (60 mesh/in) screen;
6) Mixing said particles with solid coal tar pitch, having a softening point of about 110° to 120°C;
7) Heating the mixture so formed to about 175ºC to melt said pitch;
8) Dispersing said particles in said molten pitch to form a dispersion; 9) Cooling said dispersion;
10) Molding an article from said dispersion;
11) Baking said article up to a temperature of about 700º to 1100ºC oyer a period of one ten days;
12) Heating said article to at least 2000ºC; and
13) Cooling said article.
31. The process of Claim 30 wherein 38 parts B2O3, 29 parts carbon black, and 33 parts TiO2 by wt. are mixed in step 1.
32. The process of Claim 30 wherein 100 parts by wt. of the particles formed in step 5 are mixed with 32 parts by wt. of coal tar pitch.
33. The process of Claim 30 wherein the particulate carbon com prises a mixture of calcined petroleum coke particles and carbon black.
34. A process for the production of a composite TiB2-graphite comprising forming a porous carbon article from relatively coarse coke particles having a maximum diameter of about 12 mm, coke flour, and coal tar pitch by melting said pitch and dispersing said particles and said flour in said pitch, shaping an article from the first dispersion thus formed, baking said article on a carbonizing cycle to carbonize said pitch, dispersing carbon black andTiO2 in a liquid boron compound, to form a second dispersion, impregnating said article with said second dispersion, heating said article to a TiB2 forming temperature above 1200ºC, cooling said article, impregnating said article with petroleum pitch, re-baking said article to 700º to 1100ºC over a period of one to ten days, and heating said article to at least 2100ºC to form aTiB2 -graphitic carbon composite article.
35. A process for the production of a composite TiB2-graphitic carbon article comprising the steps of:
1) Mixing a boron compound, coke, carbon, and a first liquid carbonizable binder to form a first plastic dispersion;
2) Shaping said dispersion to form said article;
3) Baking said article to carbonize said binder on a cycle of from 1 to 10 days rising to a final temperature from 600º to 1100°C;
4) Cooling said article to ambient temperature;
5) Dispersing TiO2 in a second liquid car bonizable binder to form a second dispersion;
6) Impregnating said article with said second dispersion under alternate cycles of vacuum and a pressure of frcm 2 to 15 x 103 Pa at a temperature from 100º to 500ºC;
7) Heating said article to at least 1200ºC to a TiB2 forming temperature and maintaining that temperature until the TiB2 forming reaction is substantially com pleted; and
8) Further heating said article to at least 2100ºC to form said TiB2 -graphitic carbon composite.
36. The process or Claim 35 wherein the boron compound is B4C.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US287,124 | 1981-07-27 | ||
US06/287,129 US4465581A (en) | 1981-07-27 | 1981-07-27 | Composite of TiB2 -graphite |
US287,129 | 1981-07-27 | ||
US06/287,124 US4439382A (en) | 1981-07-27 | 1981-07-27 | Titanium diboride-graphite composites |
PCT/US1982/001003 WO1983000347A1 (en) | 1981-07-27 | 1982-07-22 | COMPOSITE OF TiB2-GRAPHITE |
Publications (1)
Publication Number | Publication Date |
---|---|
AU8829682A true AU8829682A (en) | 1983-03-17 |
Family
ID=27374151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU88296/82A Abandoned AU8829682A (en) | 1981-07-27 | 1982-07-22 | Composite of tib2-graphite |
Country Status (1)
Country | Link |
---|---|
AU (1) | AU8829682A (en) |
-
1982
- 1982-07-22 AU AU88296/82A patent/AU8829682A/en not_active Abandoned
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