WO2011060064A2 - Composite material useful in electrolytic aluminum production cells - Google Patents

Composite material useful in electrolytic aluminum production cells Download PDF

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Publication number
WO2011060064A2
WO2011060064A2 PCT/US2010/056222 US2010056222W WO2011060064A2 WO 2011060064 A2 WO2011060064 A2 WO 2011060064A2 US 2010056222 W US2010056222 W US 2010056222W WO 2011060064 A2 WO2011060064 A2 WO 2011060064A2
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Prior art keywords
liner plate
composite liner
weight percent
plate
aluminum production
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PCT/US2010/056222
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WO2011060064A3 (en
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Russell Lee Yeckley
Robinson Lattimer
Sean Erin Landwehr
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Kennametal Inc
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Kennametal Inc
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Priority to DE112010004393T priority Critical patent/DE112010004393T5/en
Priority to BR112012011070A priority patent/BR112012011070A2/en
Priority to RU2012124075/02A priority patent/RU2012124075A/en
Priority to GB1210445.1A priority patent/GB2490052A/en
Publication of WO2011060064A2 publication Critical patent/WO2011060064A2/en
Publication of WO2011060064A3 publication Critical patent/WO2011060064A3/en
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Definitions

  • the present invention relates to composite .materials for use in electrolytic aluminum production cells, and more particularly relates to the use of composites comprising titanium diboride and boron nitride in the walls of aluminum production cells.
  • the .materials used in electrolytic aluminum production cells must be thermally stable at high temperatures on. the order of L000°C, and must be capable of withstanding extremely harsh conditions such as exposure to molten cryolite, molten aluminum, and oxygen at elevated temperatures. Although various types of materials have been used to Sine the walls of electrolytic aluminum production cells, a need still, exists for improved materials capable of withstanding such harsh conditions.
  • the present invention provides composite materials comprising titanium diboride and boron nitride that are used to Sine electrolytic aluminum production cells.
  • the composite materials may be used to line the side walls and'br bottom wall of the cell.
  • the ratio of titanium diboride to boron nitride may be controlled in order to provide the desired, level of electrical conduc tivity depending upon the partic ular region of the eel ! in. which the liner plate is installed.
  • the titanium diboride/boron nitride composite materials exhibit desirable aluminum wetting behavior, and are capable of withstanding exposure to molten cryolite, molten aluminum and oxygen at elevated temperatures during operation of the electrolytic aluminum production cells.
  • An aspect of the present invention is to provide a composite liner plate of an electrolytic aluminum production cell, the composite liner plate comprising TiBj and BR
  • Another aspect of the present invention is to provide a method of making a composite Silver plate for an electrolytic aluminum production cell.
  • the method comprises mixing Ti.B;> powder and BN powder, and consolidating the mixture of TiB? and BN to form the composite liner plate.
  • a further aspect of the present invention is to provide an aluminum production cell comprising a bottom wall and a side wall for containing molten cryolyte, wherein at least one of the bottom wall and side wall comprise a composite liner plate comprising TiBa and BR
  • Fig.1 is a partially schematic side sectional view of an electrolytic aluminum production ceil including walls made of a titanium, diboride/boron nitride composite material in accordance with, an embodiment of the present invention.
  • Figs. 2-4 are photomicrographs of titanium diboride/boron nitride composite materials having different ratios of TiB 2 to BN in accordance with embodiments of the present invention.
  • Fig. I schematically illustrates an electroiytic aluminum production ceil 10 including a bottom wall 12 and side walls 14.
  • An anode 18 extends into the cell 10
  • the anode 18 may be a carbonaceous consumable anode, or may be a stable Inert anode.
  • the cell 10 contains molten cryolite 20 comprising alumina in a fluoride salt bath, and current is generated between the anode 18 and the cathode bottom wail .12 of the cell.
  • the alumina in the molten cryolite 20 is converted to aluminum 22, which settles on the bottom wall 12 of the cell.
  • the cell 10 is typically open to the atmosphere, and at least the upper portions of the side wails 14 and 16 are exposed to oxygen in the surrounding air.
  • Bach of the bottom wall 12, and side walls 14 and 16, must be thermally stable at the elevated temperatures experienced during the elec troiytic process, and must he capable of withstanding exposure to molten cryolite, molten aluminum, and oxygen at such elevated temperatures, in addition, the bottom wall 12, and side walls 14 and 16, must have satisfactory aluminum wetting characteristics and controlled levels of electrical conductivity.
  • the bottom wall 12 and/or side walls 14 and 16 of the cell 10 may be made of a composite material comprising titanium dibori.de and boron nitride.
  • the titanium diboride typically comprises from about 50 to about 99 weight percent of the composite, preferably from about 70 to about 98 weight percent of the composite.
  • the boron, nitride typically comprises from about 1 to about 50 weight percent of the composite, preferably from about 2 to about 30 weight percent of the composite.
  • the titanium dibori.de content may range between 75 and 95 percent
  • the boron nitride content may range between about 5 and 25 weight percent where good aluminum wetting behavior and resistance to molten cryolite are required.
  • the titanium, diboride phase of the composite material typically forms a continuous
  • the boron nitride phase may be either continuous or discontinuous, depending upon the relative amount of boron nitride that is present in the material
  • the bottom wall 12, and side walls 14 and 16, of the cell 10 may he fabricated in the form of plates that are installed in the interior side wails of the cell.
  • the plates may have any suitable thickness.
  • the ratio of titanium diboride to boron nitride in the composite material may be controlled in order to provide the desired amount, of electrical conductivity, depending upon the particular location in the ceil.
  • the boron nitride content may be relatively low in sections where higher electrical conductivity is required, in. such high-conductivity regions, the boron nitride content may range from about 1 to about 10 weight percent, typically from about 3 to about 8 weight percent. As a particular example, the boron, nitride content may be about 5 weight percent in such regions.
  • the boron nitride content of the composite material may be increased to 10 or 20 weight percent, or higher.
  • the boron nitride content may be at least 25 weight percent and up to 50 weight percent or more in such electrical insulating regions.
  • a liner plate of the composite material may comprise a graded composition in. which the ratio of titanium diboride to boron nitride is varied throughout the plate.
  • the upper portion of the plate that is exposed to cryolite and oxygen may have a different ratio of titanium diboride to boron nitride than, the lower portion of such a side wall liner plate thai; is positioned adjacent to the bottom wall of the cell.
  • the TiB 2 :BH ratio along the height of a side wall liner plate the ratio may be adjusted through the thickness of the plate.
  • the surface of the plate tha t is exposed to the molten cryolite and aluminum in the cell may have a different .ratio of titanium diboride to boron nitride than the interior region of the liner plate.
  • the present composite materials may be made by any suitable method such as hoi pressing a mixture of the titanium diboride and boron nitride powders.
  • Hie titanium diboride powder typically has an average particle size range of from about 1 to about 50 microns, for example, from about 2 to about 10 microns.
  • the boron nitride powder typically has an average particle size range of from about 1 to about 50 microns, for example, from about 2 to about 10 microns.
  • the powders may be mixed, in the desired ratio by any suitable mixing method such as dry blending or ball milling.
  • the .resultant powder mixture may be hot pressed at pressures typically ranging from about 20 to about 50 MPa and temperatures typically ranging from about 1 ,800 to about 2,200oC.
  • the resultant hot pressed powders have high densities, typically above 95 percent, for example, above 98 or 99 percent,
  • Composite TiB 2 -BN plates were made from TiB 2 powders having the specifications set forth in Table 1 below, and BN powders having specifications set forth in Tables 2 and 3 below.
  • the blended powders were loaded into a graphite die for hot pressing.
  • the hot pressing schedule was as follows, with the maximum temperature being 1 , 900°C for 15 and 25% BN, and 2>.100*C for 5% BN: pull vacuum to ⁇ 10O mtorr; apply 7 MPa of pressure to the compact and heat at 10C/min to l.,650C while under vacuum; hold for .1 hr under vacuum while maintaining 7 MPa of pressure; after hold backfill with Ar and.

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Abstract

Composite materials comprising titanium diboride and boron nitride that are used to line electrolytic aluminum production cells (10) are disclosed. The composite materials may be used to line the side walls (14, 16) and/or bottom wall (12) of the cell (10). The ratio of titanium diboride to boron nitride may be controlled in order to provide the desired level of electrical conductivity depending upon the particular region of the cell (10) in which the liner plate (12, 14, 16) is installed. The titanium diboride/boron nitride composite materials exhibit desirable aluminum wetting behavior, and are capable of withstanding exposure to molten cryolite (20), molten aluminum (22) and oxygen at elevated temperatures during operation of the electrolytic aluminum production cells (10).

Description

COMPOSITE MATERIAL USEFUL IN ELECTROLYTIC
ALUMINUM PRODUCTION CELLS
[0001] The present invention relates to composite .materials for use in electrolytic aluminum production cells, and more particularly relates to the use of composites comprising titanium diboride and boron nitride in the walls of aluminum production cells.
BACKGROUND INFORMATION
[0002] The .materials used in electrolytic aluminum production cells must be thermally stable at high temperatures on. the order of L000°C, and must be capable of withstanding extremely harsh conditions such as exposure to molten cryolite, molten aluminum, and oxygen at elevated temperatures. Although various types of materials have been used to Sine the walls of electrolytic aluminum production cells, a need still, exists for improved materials capable of withstanding such harsh conditions.
SUMMARY OF THE INVENTION
[0003] The present invention provides composite materials comprising titanium diboride and boron nitride that are used to Sine electrolytic aluminum production cells. The composite materials may be used to line the side walls and'br bottom wall of the cell. The ratio of titanium diboride to boron nitride may be controlled in order to provide the desired, level of electrical conduc tivity depending upon the partic ular region of the eel ! in. which the liner plate is installed. The titanium diboride/boron nitride composite materials exhibit desirable aluminum wetting behavior, and are capable of withstanding exposure to molten cryolite, molten aluminum and oxygen at elevated temperatures during operation of the electrolytic aluminum production cells.
[0004] An aspect of the present invention is to provide a composite liner plate of an electrolytic aluminum production cell, the composite liner plate comprising TiBj and BR
[0005] Another aspect of the present invention is to provide a method of making a composite Silver plate for an electrolytic aluminum production cell. The method comprises mixing Ti.B;> powder and BN powder, and consolidating the mixture of TiB? and BN to form the composite liner plate. [0006] A further aspect of the present invention is to provide an aluminum production cell comprising a bottom wall and a side wall for containing molten cryolyte, wherein at least one of the bottom wall and side wall comprise a composite liner plate comprising TiBa and BR
[00(1? j These and other aspects of the present invention will be .more apparent from the following description.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Fig.1 is a partially schematic side sectional view of an electrolytic aluminum production ceil including walls made of a titanium, diboride/boron nitride composite material in accordance with, an embodiment of the present invention.
[0009] Figs. 2-4 are photomicrographs of titanium diboride/boron nitride composite materials having different ratios of TiB2 to BN in accordance with embodiments of the present invention.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENT
[0010] Fig. I schematically illustrates an electroiytic aluminum production ceil 10 including a bottom wall 12 and side walls 14. 16, An anode 18 extends into the cell 10, The anode 18 may be a carbonaceous consumable anode, or may be a stable Inert anode. During the electrolytic aluminum production process, the cell 10 contains molten cryolite 20 comprising alumina in a fluoride salt bath, and current is generated between the anode 18 and the cathode bottom wail .12 of the cell. During the electrolytic reduction process, the alumina in the molten cryolite 20 is converted to aluminum 22, which settles on the bottom wall 12 of the cell. The cell 10 is typically open to the atmosphere, and at least the upper portions of the side wails 14 and 16 are exposed to oxygen in the surrounding air. Bach of the bottom wall 12, and side walls 14 and 16, must be thermally stable at the elevated temperatures experienced during the elec troiytic process, and must he capable of withstanding exposure to molten cryolite, molten aluminum, and oxygen at such elevated temperatures, in addition, the bottom wall 12, and side walls 14 and 16, must have satisfactory aluminum wetting characteristics and controlled levels of electrical conductivity.
[0011] In accordance with the present invention, the bottom wall 12 and/or side walls 14 and 16 of the cell 10 may be made of a composite material comprising titanium dibori.de and boron nitride. The titanium diboride typically comprises from about 50 to about 99 weight percent of the composite, preferably from about 70 to about 98 weight percent of the composite. The boron, nitride typically comprises from about 1 to about 50 weight percent of the composite, preferably from about 2 to about 30 weight percent of the composite. In an embodiment of the invention, the titanium dibori.de content may range between 75 and 95 percent, and the boron nitride content may range between about 5 and 25 weight percent where good aluminum wetting behavior and resistance to molten cryolite are required. The titanium, diboride phase of the composite material typically forms a continuous
interconnected skeleton in the material, while the boron nitride phase may be either continuous or discontinuous, depending upon the relative amount of boron nitride that is present in the material
[0012] The bottom wall 12, and side walls 14 and 16, of the cell 10 may he fabricated in the form of plates that are installed in the interior side wails of the cell. The plates may have any suitable thickness.
[0013] In accordance with an embodiment of the present invention, the ratio of titanium diboride to boron nitride in the composite material may be controlled in order to provide the desired amount, of electrical conductivity, depending upon the particular location in the ceil. For example, the boron nitride content may be relatively low in sections where higher electrical conductivity is required, in. such high-conductivity regions, the boron nitride content may range from about 1 to about 10 weight percent, typically from about 3 to about 8 weight percent. As a particular example, the boron, nitride content may be about 5 weight percent in such regions. In regions where lower electrical conductivity or higher electrical insulating characteristics are required, the boron nitride content of the composite material may be increased to 10 or 20 weight percent, or higher. For example, the boron nitride content .may be at least 25 weight percent and up to 50 weight percent or more in such electrical insulating regions.
[0014] in accordance with an embodiment of the present invention, a liner plate of the composite material may comprise a graded composition in. which the ratio of titanium diboride to boron nitride is varied throughout the plate. For example, for a side wall liner plate, the upper portion of the plate that is exposed to cryolite and oxygen may have a different ratio of titanium diboride to boron nitride than, the lower portion of such a side wall liner plate thai; is positioned adjacent to the bottom wall of the cell. In addition, to adjusting the TiB2:BH ratio along the height of a side wall liner plate, the ratio may be adjusted through the thickness of the plate. For example, the surface of the plate tha t is exposed to the molten cryolite and aluminum in the cell may have a different .ratio of titanium diboride to boron nitride than the interior region of the liner plate.
[0015] The present composite materials may be made by any suitable method such as hoi pressing a mixture of the titanium diboride and boron nitride powders. Hie titanium diboride powder typically has an average particle size range of from about 1 to about 50 microns, for example, from about 2 to about 10 microns. The boron nitride powder typically has an average particle size range of from about 1 to about 50 microns, for example, from about 2 to about 10 microns. The powders may be mixed, in the desired ratio by any suitable mixing method such as dry blending or ball milling. The .resultant powder mixture may be hot pressed at pressures typically ranging from about 20 to about 50 MPa and temperatures typically ranging from about 1 ,800 to about 2,200ºC. The resultant hot pressed powders have high densities, typically above 95 percent, for example, above 98 or 99 percent,
[001.6] Composite TiB2-BN plates were made from TiB2 powders having the specifications set forth in Table 1 below, and BN powders having specifications set forth in Tables 2 and 3 below.
Figure imgf000006_0001
Figure imgf000007_0001
[0017] Three different TiBs:BN weight ratios were mixed with a dry powder blending process. The ratios employed were 95% TtB2-5% BN, 85% TiB215% BR and 75% TiB2- 25% BN. Both the first and second grades of BN were employed to make six different compositions. Fhe different ratios and compositions allow tailoring of wettability by molten A! as well as electrical conductivity in the Hall-HerouIt process.
[0018] The blended powders were loaded into a graphite die for hot pressing. The hot pressing schedule was as follows, with the maximum temperature being 1 , 900°C for 15 and 25% BN, and 2>.100*C for 5% BN: pull vacuum to <10O mtorr; apply 7 MPa of pressure to the compact and heat at 10C/min to l.,650C while under vacuum; hold for .1 hr under vacuum while maintaining 7 MPa of pressure; after hold backfill with Ar and. heat at 5C/min to maximum temperature while maintaining 7 M Pa of pressure; once maximum temperature is reached hold for 10 min with 7 MPa load; after the hold apply load slowly over 10 mm to the maximum pressure of 30 MPa; hold at maximum tempera tare and 30 MPa until ram travel slops; once rani travel stops allow the furnace to cool but. maintain 30 MPa of pressure until 1 ,300°C is reached; and once i >300°C is reached release pressure and allow to cool to room temperature,
[0019] After the materials were hot pressed, their density was measured, Vickers hardness was measured on polished cross-sections of the material and Young's modulus was deierrnitied with a time-of-.tltght calculation using an ultrasonic transducer. Because of the anisotropic nature ofBN, Young's modulus was measured both in the directions parallel to hot pressing and perpendicular to hot pressing. The properties of the six different compositions are shown in Table 4,
Figure imgf000008_0001
[0020] Upon examining the microstructures it was found that there was no diseernable difference between the first BN and second BN compositions for each amount of BN. Additionally, no obvious mtcrostructural anisotropy was observed, despite the Young's modulus measurements that suggest otherwise. Microstructures of the 95% TiB¾ 85% TiB2, and 75% TtBj samples at high and low magnification are shown in Figs. 2, 3 and 4, respectively, in each .micrograph, the lighter gray phase is TiB2 while the darker gray phase is the BN,
[0021 ] Whereas particular embodiments of this invention have been described above for purposes of illustration, it will be evident to those skilled in the art that numerous variations of the details of the present invention may be made without departing from the invention as defined in the appended claims.

Claims

CLAIMS:
1. A composite liner plate (12, 14, 16) of an electrolytic aluminum production ceil (10), the composite liner plate (12, 14, 16) comprising Tii¾ and BN.
2. The composite liner plate (12, 14, 16) of Claim 1 , wherein the Til¾ comprises from about 50 to about 99 weight percent of the composite liner plate (12, 14, 16), and the BN comprises irom about 1 to about 50 weight percent of the composite li ner plate (.12, 14, 16).
3. The composite liner plate ( 12, 14, 1.6) of Claim 1 , wherein the T1B2 comprises irom about 70 to about 98 weight percent of the composite liner plate ( 12, 14, 16), and the BN comprises from about 2 to about 30 weight percent of the composite liner plate (12, 14, 16),
4. The composite liner plate (12, 14, 16) of Claim I , wherein the TiB? comprises from about 75 to about 95 weight percent of the composite liner plate (12, 14, 16). and the BN comprises, from, about 5 to about 25 weight percent of the composite liner plate ( 12, 34, 16).
5. The composite liner plate (12, 14, 16) of Claim 1, wherein the relative amounts ofTtBj and BN are varied at different locations in the plate ( 12, 14, 16).
6. The composite liner plate (12, 14, 16) of Claim 5, wherein the ratio of TiBj to BN is varied at different locations in a plane of the plate (12, 14, 16).
7. The composite liner plate (1.2, 14, 1.6) of Claim 5, wherein the ratio of Ti¾ to BN is varied through a thickness of the plate (12, 1.4, 16).
8. The composite liner plate (12. .14, 16) of Claim Ϊ , wherein the TiBj has an average particle size of from about 1 to about 50 microns, and the BN has an average particle size of from about 1 to about 50 microns.
9. A. method of making a composite liner plate (12, 14, 16) for an electrolytic aluminum production cell ( 10) the method comprising:
mixing TiB2 powder and BN powder; and.
consolidating the mixture of TiB2 and BN to form the composite liner plate (12, 14, .16).
10. The method of Claim 9, further comprising washing the BN powder.
1 1 . The method of Claim .10, wherein the BN powder is washed before mixing with the TiB2 powder.
12. The method of Claim 9, wherein the mixture of TiB ? and BN is consolidated by hot pressing.
13, An aluramum production cell (10) comprising a bottom wall and a side wall ( 14, 16) for containing molten cryolyle (20), wherein at least one of the bottom wall (12) and side wall (14, 16) comprise a composite liner plate comprising Ti B2 and BN.
14. The aluminum production cell (10) of Claim 13, wherein the TiB2 comprises from about 50 to about 99 weight percent of the composite liner plate, and the BN comprises from about 1 to aboist 50 weight percent of the composite liner plate.
1.5. The aluminum production cell (10) of Claim 13, wherein the !¾ comprises irom about 70 to about 98 weight percent of the composite liner plate, and the BN comprises from about 2 to about 30 weight percent of the composite liner plate,
16. The aluminum production cell (TO) of Claim 1.3, wherein the ΤίΒτ comprises from about 75 to about 95 weight percent of the composite liner plate, and the BN comprises from about 5 to about 25 weight percent of the composite liner plate.
17. The aluminum production cell (10) of Claim 13, wherein the relative amounts of TiB? and BN are varied at different locations in the plate.
18. The aluminum production cell ( 10) of Claim 17, wherein the ratio of TiBi to BN is varied at different locations in a plane of the plate.
1.9. The aluminum production cell. (10) of Claim 17, wherein the ratio of TiB2 to BN is varied through a thickness of the plate.
20. The aluminum production cell ( 10) of Claim 13, wherein the TiB> has an average particle size of from about I to about 50 microns, and the BN has an average particle size of from about 1 to about 50 microns.
PCT/US2010/056222 2009-11-13 2010-11-10 Composite material useful in electrolytic aluminum production cells Ceased WO2011060064A2 (en)

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DE112010004393T DE112010004393T5 (en) 2009-11-13 2010-11-10 Composite material useful in aluminum production electrolysis cells
BR112012011070A BR112012011070A2 (en) 2009-11-13 2010-11-10 composite lining board, same production method and aluminum production cell.
RU2012124075/02A RU2012124075A (en) 2009-11-13 2010-11-10 COMPOSITE MATERIAL APPLICABLE IN ELECTROLYTIC BATHS FOR THE PRODUCTION OF ALUMINUM
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US8501050B2 (en) 2011-09-28 2013-08-06 Kennametal Inc. Titanium diboride-silicon carbide composites useful in electrolytic aluminum production cells and methods for producing the same
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Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4071420A (en) * 1975-12-31 1978-01-31 Aluminum Company Of America Electrolytic production of metal
US4097567A (en) * 1976-08-25 1978-06-27 Aluminum Company Of America Titanium diboride shapes
US4297180A (en) * 1976-08-25 1981-10-27 Aluminum Company Of America Electrolytic production of metal
US4338177A (en) * 1978-09-22 1982-07-06 Metallurgical, Inc. Electrolytic cell for the production of aluminum
US4353885A (en) * 1979-02-12 1982-10-12 Ppg Industries, Inc. Titanium diboride article and method for preparing same
US4224128A (en) * 1979-08-17 1980-09-23 Ppg Industries, Inc. Cathode assembly for electrolytic aluminum reduction cell
US4275026A (en) * 1979-11-02 1981-06-23 Ppg Industries, Inc. Method for preparing titanium diboride shapes
CH643885A5 (en) * 1980-05-14 1984-06-29 Alusuisse ELECTRODE ARRANGEMENT OF A MELTFLOW ELECTROLYSIS CELL FOR PRODUCING ALUMINUM.
AU543106B2 (en) * 1980-05-23 1985-04-04 Swiss Aluminium Ltd. Cathod for aluminium production
US4349427A (en) * 1980-06-23 1982-09-14 Kaiser Aluminum & Chemical Corporation Aluminum reduction cell electrode
US4399008A (en) * 1980-11-10 1983-08-16 Aluminum Company Of America Composition for inert electrodes
US4478693A (en) * 1980-11-10 1984-10-23 Aluminum Company Of America Inert electrode compositions
US4374761A (en) * 1980-11-10 1983-02-22 Aluminum Company Of America Inert electrode formulations
US4560448A (en) * 1982-05-10 1985-12-24 Eltech Systems Corporation Aluminum wettable materials for aluminum production
US4544469A (en) * 1982-07-22 1985-10-01 Commonwealth Aluminum Corporation Aluminum cell having aluminum wettable cathode surface
US4514355A (en) * 1982-12-22 1985-04-30 Union Carbide Corporation Process for improving the high temperature flexural strength of titanium diboride-boron nitride
US4599320A (en) * 1982-12-30 1986-07-08 Alcan International Limited Refractory lining material for electrolytic reduction cell for aluminum production and method of making the same
US4534835A (en) * 1982-12-30 1985-08-13 Corning Glass Works Electrolytic Al production with reaction sintered multiphase ceramic
US4664760A (en) * 1983-04-26 1987-05-12 Aluminum Company Of America Electrolytic cell and method of electrolysis using supported electrodes
US4582553A (en) * 1984-02-03 1986-04-15 Commonwealth Aluminum Corporation Process for manufacture of refractory hard metal containing plates for aluminum cell cathodes
US5158655A (en) * 1989-01-09 1992-10-27 Townsend Douglas W Coating of cathode substrate during aluminum smelting in drained cathode cells
US5227045A (en) * 1989-01-09 1993-07-13 Townsend Douglas W Supersaturation coating of cathode substrate
US5028301A (en) * 1989-01-09 1991-07-02 Townsend Douglas W Supersaturation plating of aluminum wettable cathode coatings during aluminum smelting in drained cathode cells
US4929328A (en) * 1989-03-07 1990-05-29 Martin Marietta Energy Systems, Inc. Titanium diboride ceramic fiber composites for Hall-Heroult cells
US4983340A (en) * 1989-12-28 1991-01-08 Union Carbide Coatings Service Technology Corporation Method for forming a high density metal boride composite
US5217583A (en) * 1991-01-30 1993-06-08 University Of Cincinnati Composite electrode for electrochemical processing and method for using the same in an electrolytic process for producing metallic aluminum
US5100845A (en) * 1991-03-13 1992-03-31 Union Carbide Coatings Service Technology Corporation Process for producing titanium diboride and boron nitride powders
US5310476A (en) * 1992-04-01 1994-05-10 Moltech Invent S.A. Application of refractory protective coatings, particularly on the surface of electrolytic cell components
FR2830856B1 (en) * 2001-10-15 2004-07-30 Pechiney Aluminium COATING PRECURSOR AND METHOD FOR COATING A SUBSTRATE WITH A REFRACTORY LAYER
FR2893329B1 (en) * 2005-11-14 2008-05-16 Aluminium Pechiney Soc Par Act ELECTROLYSIS TANK WITH THERMAL EXCHANGER.

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