US3553010A - Carbon or graphite formed body - Google Patents
Carbon or graphite formed body Download PDFInfo
- Publication number
- US3553010A US3553010A US747129A US3553010DA US3553010A US 3553010 A US3553010 A US 3553010A US 747129 A US747129 A US 747129A US 3553010D A US3553010D A US 3553010DA US 3553010 A US3553010 A US 3553010A
- Authority
- US
- United States
- Prior art keywords
- layer
- carbon
- aluminum
- graphite
- comprised
- 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.)
- Expired - Lifetime
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title abstract description 40
- 229910052799 carbon Inorganic materials 0.000 title abstract description 21
- 229910002804 graphite Inorganic materials 0.000 title abstract description 18
- 239000010439 graphite Substances 0.000 title abstract description 18
- 239000010410 layer Substances 0.000 abstract description 54
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract description 20
- 229910052782 aluminium Inorganic materials 0.000 abstract description 18
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 14
- 239000011777 magnesium Substances 0.000 abstract description 12
- 229910052749 magnesium Inorganic materials 0.000 abstract description 12
- 229910052710 silicon Inorganic materials 0.000 abstract description 12
- 229910052742 iron Inorganic materials 0.000 abstract description 11
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 abstract description 10
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract description 10
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 abstract description 10
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 10
- 239000001301 oxygen Substances 0.000 abstract description 10
- 229910052760 oxygen Inorganic materials 0.000 abstract description 10
- 239000010703 silicon Substances 0.000 abstract description 10
- 239000011734 sodium Substances 0.000 abstract description 10
- 229910052708 sodium Inorganic materials 0.000 abstract description 10
- 239000010936 titanium Substances 0.000 abstract description 10
- 229910052719 titanium Inorganic materials 0.000 abstract description 10
- 229910052726 zirconium Inorganic materials 0.000 abstract description 10
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 abstract description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 abstract description 9
- 229910052796 boron Inorganic materials 0.000 abstract description 9
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract description 9
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 abstract description 8
- 230000003647 oxidation Effects 0.000 abstract description 8
- 238000007254 oxidation reaction Methods 0.000 abstract description 8
- 239000011574 phosphorus Substances 0.000 abstract description 8
- 229910052698 phosphorus Inorganic materials 0.000 abstract description 8
- 239000011241 protective layer Substances 0.000 abstract description 7
- 229910052791 calcium Inorganic materials 0.000 abstract description 6
- 239000011575 calcium Substances 0.000 abstract description 6
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 abstract description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 abstract description 5
- 229910017052 cobalt Inorganic materials 0.000 abstract description 5
- 239000010941 cobalt Substances 0.000 abstract description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 abstract description 5
- 229910052802 copper Inorganic materials 0.000 abstract description 5
- 239000010949 copper Substances 0.000 abstract description 5
- 239000011133 lead Substances 0.000 abstract description 5
- 239000011701 zinc Substances 0.000 abstract description 5
- 229910052725 zinc Inorganic materials 0.000 abstract description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 abstract description 4
- 239000011651 chromium Substances 0.000 abstract description 4
- 229910052804 chromium Inorganic materials 0.000 abstract description 4
- YUWBVKYVJWNVLE-UHFFFAOYSA-N [N].[P] Chemical compound [N].[P] YUWBVKYVJWNVLE-UHFFFAOYSA-N 0.000 abstract 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 230000008018 melting Effects 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 238000000576 coating method Methods 0.000 description 5
- 239000011247 coating layer Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 229910019142 PO4 Inorganic materials 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 239000010452 phosphate Substances 0.000 description 3
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- BTBUEUYNUDRHOZ-UHFFFAOYSA-N Borate Chemical compound [O-]B([O-])[O-] BTBUEUYNUDRHOZ-UHFFFAOYSA-N 0.000 description 2
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 2
- -1 SlilCOl'l Chemical compound 0.000 description 2
- 239000003513 alkali Substances 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910021350 transition metal silicide Inorganic materials 0.000 description 2
- 241000219793 Trifolium Species 0.000 description 1
- JCCZVLHHCNQSNM-UHFFFAOYSA-N [Na][Si] Chemical compound [Na][Si] JCCZVLHHCNQSNM-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000002585 base Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000006023 eutectic alloy Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000005923 long-lasting effect Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229940099990 ogen Drugs 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B7/00—Heating by electric discharge
- H05B7/02—Details
- H05B7/06—Electrodes
- H05B7/08—Electrodes non-consumable
- H05B7/085—Electrodes non-consumable mainly consisting of carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
- C04B41/90—Coating or impregnation for obtaining at least two superposed coatings having different compositions at least one coating being a metal
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/067—Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B7/00—Heating by electric discharge
- H05B7/02—Details
- H05B7/12—Arrangements for cooling, sealing or protecting electrodes
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2111/00—Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
- C04B2111/00474—Uses not provided for elsewhere in C04B2111/00
- C04B2111/0087—Uses not provided for elsewhere in C04B2111/00 for metallurgical applications
- C04B2111/00879—Non-ferrous metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
- Y10T428/24967—Absolute thicknesses specified
- Y10T428/24975—No layer or component greater than 5 mils thick
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Definitions
- the primary layer is comprised of 90 to 100%, 3,553,010
- This invention relates to a carbon or graphite formed particularly preferable to provide the primary layer with body, and m r p r y n rc el r ing a a layer thickness of 0.01 to 0.15 preferably p pg o protective layer which arrests oxidation, and which in- 0.1 rrrnm, and the comm a thickness 033i cludes a primary layer, applied. upon a carbon or graphite Winn, preferably ill to 0.3 mm.
- coated bodies are heated above approximately 550 C., of Sodium, magnesium, Calcium, 13 aluminum, titathe components of the double layer react with each othernium, Zirconium, manganese, iron, carbon, nit ogen p to form a low melting, eutectic alloy which closes the phorus and oxygen, separately or in combination.
- the pores formed by the flame injection
- cover layer is'comprised of 85 to 100%, preferably 93 that silicon which is dissolved mainly in aluminum, reacts to 99.5%, aluminum and 0 to 15%, pref bly 0.5 to 7%, with the carbon of the fundamental body forming silicon sodium, magnesium, boron, silicon, phosphorus, oxygen, carbide when the operational temperature of the procopper, zinc, lead, titanium, zirconium, chromium, mantected parts exceeds about 550 C. which leads to a tearg fi, irOXl, Cobalt and nickel, lfi y in flflfree and solid bond between the protective layer to the tion. carbon part. This bond is resistant to temperature changes.
- Carbon or graphite bodies provided with such coatings have shown a long lasting excellent stability with respect
- My invention relates to a carbon or graphite formed to oxidation, at approximately 1700 C., due to the aforebody, and more particularly an arc electrode having a described alloying effect.
- the protective effect of the double layer "eludes a primary layer, applied upon a carbon or graphite upon the body can be increased by an additional melting formed. body, and a metallic cover layer, comprised essenof the already applied coating. This melting is carried out tially of aluminum, over the primary layer.
- Carbon or graphite formed bodies are very widely used burner.
- the subsequent melting of the protective layers I in chemical and metallurgical arts because of their excelre ult in an elimination of the pores and in a chemical ⁇ X J lent mechanical and thermal qualities. Frequently, howanchoring, which leads to a considerable improvement of ,1 ,yever. the burning err, which occurs in these materials at the protection againstburning olf.
- the base layer may be a carbide layer, e.g. a a current supply and the are, are in a fluid or even in a silicon carbide layer, while the cover layer may either plastic state, so that no voltages whatsoever can be proconstitute a layer of an oxide mixture or a metal or siliduced in the coating layer through the dilferent expan- .cide layer. But even these layers do not yet afford an adesions of the coating layer and the fundamental body.
- tween 600 and 1200 (3., preferably 700 to i000" (3.,
- the Present invention, lhefefofa has 85 an j t rfform melting eutectics and to measure the current load such that the melting point of the eutectic is at least obtained on the electrode surface.
- EXAMPLE 1 A graphite electrode with a diameter of 450 mm. and a length of 2000 mm. is left to rotate at about 50 revolutions per minute, following the customary, accurately scaled turning oft", in a rotating lathe.
- Two tlame injection elec rodes arranged in sequence at a distance of 200 mm., uniformly coat the electrode surface (injection dis tance 100 mm.), first with an 0.05 mm. thick. primary layer of 98.5% silicon+0.8% Fe+0.5% Al+0.2% Ca and thereafter with an 0.15 mm. thick cover layer of 99% Al+0.7% Mg+0.3% Si.
- electrodes coated in this manner result in a graphite saving of 25 to 35% compared to untreated electrodes.
- EXAMPLE 2 A graphite crucible 200 mm. in diameter, 500 mm. high and with 20 mm. wall thickness is slowly rotated on a turntable, e.g. at 30 rpm. An approximately 0.1 mm. thick primary layer of 95% Si+3% Ti+1.5% Fe+0.5% Al is applied by means of a powder fiame injection pistol. The coating which is still approximately 70 C. is injection coated with a cover layer of 0.2 mm. thickness, comprised of 98.2% Al+1.5% Mg+0.3% Mn, by Using a wire flame injection pistol, The coated crucible is subsequently dipped briefly into a 20% sodium phospiate solution (pH 5) and thereafter dried. at 120 When employed to operate in a copper casting installation, the above-described crucibles achieve a life span which is 4 to 6 times longer than in untreated crucibles.
- Formed bodyof carbonor graphite having an oxidation arresting protective layer which encompasses a primary layer on the carbon or graphite formed body and a metallic cover layer on the primary layer, said primary layer being comprised of 90 to 100% silicon and 0 to 10% of sodium, magnesium, calcium, boron, aluminum, titanium, zirconium, manganese, iron, carbon, nitrogen, phosphorus and oxygen, separately or in combination, the cover layer being comprised of to 100% aluminum and 0 to 15% sodium, magnesium, boron, silicon, phosphorus, oxygen, copper, zinc, lead, titanium, zirconium, chromium, manganese, iron, cobalt and nickel, separately or in combination.
- the primary layer comprises to 98.9% silicon and 1.1 to 5.0% of a material selected from. sodium, magnesium, calcium, boron, aluminum, titanium, zirconium, manganese, iron, carbon, nitrogen, phosphorus, oxygen and mixtures thereof and the cover layer comprises 93 to 99.5% aluminum and 0.5 to 7% sodium, magnesium, boron, silicon, phosphorus, oxygen, copper, zinc, lead, titanium, zirconium, chromium, manganese, iron, cobalt and nickel and mixtures thereof.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- Structural Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Manufacturing & Machinery (AREA)
- Carbon And Carbon Compounds (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
THIS INVENTION RELATES TO A CARBON OR GRAPHITE FORMED BODY, AND MORE PARTICULARLY AN ARC ELECTRODE HAVING A PROTECTIVE LAYER WHICH ARRESTS OXIDATION, AND WHICH INCLUDES A PRIMARY LAYER, APPLIED UPON A CARBON OR GRAPHIC FORMED BODY, AND A METALLIC COVER LAYER COMPRISED ESSENTIALLY OF ALUMINUM OVER THE PRIMARY LAYER. THE PRIMARY LAYER IS COMPRISED OF 90 TO 100%, PREFERABLY 95 TO 98.9%, OF SILCON AND 0 TO 10%, PREFERABLY 1.1 TO 5.0%, OF SODIUM, MAGNESIUM, CALCIUM, BORON, ALUMINUM, TITANIUM, ZIRCONIUM, MANGANESE, IRON, CARBON, NITROGEN PHOSPHORUS AND OXYGEN, SEPARATELY OR IN COMBINATION. THE COVER LAYER IS COMPRISED OF 85 TO 100%, PREFERABLY 93 TO 99.5%, ALUMINUM AND 0 TO 15%, PREFERABLY 0.5 TO 7%, SODIUM, MAGNESIUM, BORON, SILICON, PHOSPHORUS, OXYGEN, COPPER, ZINC, LEAD, TITANIUM, ZIRCONIUM, CHROMIUM, MANGANESE, IRON, COBALT AND NICKEL, SEPARATELY OR IN COMBINATION.
Description
CARBGN R GRAPHZTE FORMED BODY ttrnar Rubisch, Meitingen, near Augsburg, Germany, assignor to Sigri Elel-rtrographit Gescllschatt mit beschranltter lilaftung, Mcitingen, near Augsburg, Gerfective protection against oxidation of the aforementioned formed body of graphite or carbon. According to the 428 408e XR 395539010 SR 12 assault; a g Patented ,.laln. 5, 1971 invention, the primary layer is comprised of 90 to 100%, 3,553,010
preferably 95 to 98.9%, of silicon and 0 to 10%, preferably 1.1 to 5%, of sodium, magnesium, calcium, boron. aluminum, titanium, zirconium, manganese, iron, carbon, nitrogen, phosphorus and oxygen, separately or in com- 5 an bmatron, and the cover layer of 85 to 100%, preferably ia l lirgssi iig l il sd ifiiz? 719 08. Ser. No. 747,129 93 to 99.5%, of aluminum and 0 to 15%, preferably 0.5 Claims priority, application Germany, July 26, 1967, to 7%, of sodium, magnesium, boron, SlilCOl'l, phosphorus,
1,571,055 oxygen, copper, zinc, lead, titanium, zirconium chro- B443 1/20 mium manganese, iron, cobalt and nickel, separately or in 3 CL 117-217 5 Claims combination. All percentages used in this application are by weight. 1 b ff 5 The a lication of such a double ayer may e e ecte ABSTRACT OF THE DISCLOSURE in a kn ii'n manner by means of flame injection. It is This invention relates to a carbon or graphite formed particularly preferable to provide the primary layer with body, and m r p r y n rc el r ing a a layer thickness of 0.01 to 0.15 preferably p pg o protective layer which arrests oxidation, and which in- 0.1 rrrnm, and the comm a thickness 033i cludes a primary layer, applied. upon a carbon or graphite Winn, preferably ill to 0.3 mm. formed body, and a metallic cover layer comprised essen- Wen such a proEE'tiVlfiYE-"r" is applied by flame injectial y of aluminum r the P y y The p y -2 tion, it is only mechanically bound to the carbon or layer is comprised of 90 to 100%, preferably 95 to graphite formed body. It was found that when the thus 9 9%, of silicon and 0 to 10%, preferably 1.1 to 5.0%, coated bodies are heated above approximately 550 C., of Sodium, magnesium, Calcium, 13 aluminum, titathe components of the double layer react with each othernium, Zirconium, manganese, iron, carbon, nit ogen p to form a low melting, eutectic alloy which closes the phorus and oxygen, separately or in combination. The pores formed by the flame injection. Finally, I also found cover layer is'comprised of 85 to 100%, preferably 93 that silicon which is dissolved mainly in aluminum, reacts to 99.5%, aluminum and 0 to 15%, pref bly 0.5 to 7%, with the carbon of the fundamental body forming silicon sodium, magnesium, boron, silicon, phosphorus, oxygen, carbide when the operational temperature of the procopper, zinc, lead, titanium, zirconium, chromium, mantected parts exceeds about 550 C. which leads to a tearg fi, irOXl, Cobalt and nickel, lfi y in flflfree and solid bond between the protective layer to the tion. carbon part. This bond is resistant to temperature changes. Carbon or graphite bodies provided with such coatings have shown a long lasting excellent stability with respect My invention relates to a carbon or graphite formed to oxidation, at approximately 1700 C., due to the aforebody, and more particularly an arc electrode having a described alloying effect. During a particularly strong protective layer which arrests oxidation, and which inoxidation attack, the protective effect of the double layer "eludes a primary layer, applied upon a carbon or graphite upon the body can be increased by an additional melting formed. body, and a metallic cover layer, comprised essenof the already applied coating. This melting is carried out tially of aluminum, over the primary layer. in a known manner by an argon are or a direct plasma Carbon or graphite formed bodies are very widely used burner. The subsequent melting of the protective layers I in chemical and metallurgical arts because of their excelre ult in an elimination of the pores and in a chemical \X J lent mechanical and thermal qualities. Frequently, howanchoring, which leads to a considerable improvement of ,1 ,yever. the burning err, which occurs in these materials at the protection againstburning olf.
? temperatures above 550 C. in an oxidizing atmosphere, A similar additional increase of the protective action ;z is disturbing 5 may be obtained by sealing the metallic double layer with y ,f, It is kn wn that burning Off of the carbon and graphite a coating of an aqueous solution of -10 to 30% alkali bodies can be reduced by impregnation with phosphate. borate and/or phosphate and/0r silicate. ll This, b reduces ihe burning Off y p r The effect of the cover layer is also heightened through I tures up to approximately 1100 C. the fact that during operation of the arc furnace, the l t It is further known to reduce the burning Off through current load of the electrodes is so measured that the the utilization of clover layers on carbon or graphite cover layer is heatedio above its melting point or soften- 1,; bodies. It is preferred to produce said cover layers of ing point. This counteracts an otherwise possible tear transition metal silicides. The effect of such layers comformation in the cover layer caused by a. dilference in the prised of transition metal silicides is limited, though, to thermal expansion coefficients of the fundamental material high temperatures within a range of 1200 to 1700 C. and the cover layer, thus preventing increased oxidation Furthermore, the application of said layers is possible which is feasible inand near the tears. only by means of expensive techniques. It is also known In this type of operation, the coating layers in the to apply double layer coatings upon carbon or graphite total region between the electrode holder which serves as bodies. The base layer may be a carbide layer, e.g. a a current supply and the are, are in a fluid or even in a silicon carbide layer, while the cover layer may either plastic state, so that no voltages whatsoever can be proconstitute a layer of an oxide mixture or a metal or siliduced in the coating layer through the dilferent expan- .cide layer. But even these layers do not yet afford an adesions of the coating layer and the fundamental body. quate protection, since it was not possible, heretofore, to Previously formed tears are automatically sealed by the adjust the expansion coefficients of the body to be proplastic or fluid coating layer. Therefore a breaking off of tected and the applied layer, to each other. in the aforethe applied protective layer is not possible. mentioned double layers, the melting point is so high that I found it particularly advantageous to produce, using tears which form cannot be recovered by thellow of the aforementioned preferred method of operation, coatthe layer. As a result, the layer is undercut by oxidation ings of components which in a temperature range beand breaks off. tween 600 and 1200 (3., preferably 700 to i000" (3., The Present invention, lhefefofa, has 85 an j t rfform melting eutectics and to measure the current load such that the melting point of the eutectic is at least obtained on the electrode surface.
The atoredescrihed invention will now be disclosed with some embodiment examples.
EXAMPLE 1' A graphite electrode with a diameter of 450 mm. and a length of 2000 mm. is left to rotate at about 50 revolutions per minute, following the customary, accurately scaled turning oft", in a rotating lathe. Two tlame injection elec rodes, arranged in sequence at a distance of 200 mm., uniformly coat the electrode surface (injection dis tance 100 mm.), first with an 0.05 mm. thick. primary layer of 98.5% silicon+0.8% Fe+0.5% Al+0.2% Ca and thereafter with an 0.15 mm. thick cover layer of 99% Al+0.7% Mg+0.3% Si.
When used in an arc furnace, electrodes coated in this manner result in a graphite saving of 25 to 35% compared to untreated electrodes.
EXAMPLE 2 A graphite crucible 200 mm. in diameter, 500 mm. high and with 20 mm. wall thickness is slowly rotated on a turntable, e.g. at 30 rpm. An approximately 0.1 mm. thick primary layer of 95% Si+3% Ti+1.5% Fe+0.5% Al is applied by means of a powder fiame injection pistol. The coating which is still approximately 70 C. is injection coated with a cover layer of 0.2 mm. thickness, comprised of 98.2% Al+1.5% Mg+0.3% Mn, by Using a wire flame injection pistol, The coated crucible is subsequently dipped briefly into a 20% sodium phospiate solution (pH 5) and thereafter dried. at 120 When employed to operate in a copper casting installation, the above-described crucibles achieve a life span which is 4 to 6 times longer than in untreated crucibles.
I claim:
1. Formed bodyof carbonor graphite having an oxidation arresting protective layer which encompasses a primary layer on the carbon or graphite formed body and a metallic cover layer on the primary layer, said primary layer being comprised of 90 to 100% silicon and 0 to 10% of sodium, magnesium, calcium, boron, aluminum, titanium, zirconium, manganese, iron, carbon, nitrogen, phosphorus and oxygen, separately or in combination, the cover layer being comprised of to 100% aluminum and 0 to 15% sodium, magnesium, boron, silicon, phosphorus, oxygen, copper, zinc, lead, titanium, zirconium, chromium, manganese, iron, cobalt and nickel, separately or in combination.
2. The body of claim 1 wherein the primary layer comprises to 98.9% silicon and 1.1 to 5.0% of a material selected from. sodium, magnesium, calcium, boron, aluminum, titanium, zirconium, manganese, iron, carbon, nitrogen, phosphorus, oxygen and mixtures thereof and the cover layer comprises 93 to 99.5% aluminum and 0.5 to 7% sodium, magnesium, boron, silicon, phosphorus, oxygen, copper, zinc, lead, titanium, zirconium, chromium, manganese, iron, cobalt and nickel and mixtures thereof.
3. The body of claim 1, wherein the primary. layer has a ltgglgnessmmgl tgfl 15 mrn and the cover layer has a thickness of 0.05150 M 4;"Fheh6dybf claim 1, wherein the primary layer has a thickness of 0.02 to 0.1 mm. and the cover layer has a thickness of 0.1 to 0.3 mm.
5. The body of claim 4, wherein a sealing layer consisting of alkali borate, phosphate, silicate or mixtures thereof is on the cover layer.
References Cited UNITED STATES PATENTS 2,295,379 9/1942 Beck et a1 117--223X 3,120,453 2/1964 Fitzer et a1. 117-217 3,348,929 10/1967 Valtschev et a1. 1172l7X 3,390,013 6/1968 Rubisch 117-221X 3,476,586 11/1969 Valtchev ct a1. 117-217X r ALFRED L. LEAVITT, Primary Examiner C. K. WEIFFENBACH, Assistant Examiner US. Cl. XJR-
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1615404A DE1615404C3 (en) | 1967-07-26 | 1967-07-26 | Arc furnace |
DE19671671065 DE1671065C3 (en) | 1967-07-26 | 1967-07-26 | Carbon or graphite moldings |
Publications (1)
Publication Number | Publication Date |
---|---|
US3553010A true US3553010A (en) | 1971-01-05 |
Family
ID=25753726
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US747129A Expired - Lifetime US3553010A (en) | 1967-07-26 | 1968-07-24 | Carbon or graphite formed body |
Country Status (5)
Country | Link |
---|---|
US (1) | US3553010A (en) |
AT (1) | AT285195B (en) |
FR (1) | FR1587074A (en) |
GB (1) | GB1166429A (en) |
SE (1) | SE329966B (en) |
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3770488A (en) * | 1971-04-06 | 1973-11-06 | Us Air Force | Metal impregnated graphite fibers and method of making same |
US3864164A (en) * | 1971-10-22 | 1975-02-04 | British Steel Corp | Method for depositing protective coatings on carbon articles |
US3881039A (en) * | 1971-01-22 | 1975-04-29 | Snam Progetti | Process for the treatment of amorphous carbon or graphite manufactured articles, for the purpose of improving their resistance to oxidation, solutions suitable for attaining such purpose and resulting product |
US3921023A (en) * | 1969-07-21 | 1975-11-18 | Dmz Lennin Bg1969072112705 | Method for joining carbon electrodes and product thereof |
FR2283874A1 (en) * | 1974-09-09 | 1976-04-02 | Secr Defence Brit | ANTI-OXIDATION COATING FOR CARBON PARTS |
US4000026A (en) * | 1973-03-12 | 1976-12-28 | Union Carbide Corporation | Method and cement for bonding carbon articles |
US4418097A (en) * | 1981-12-11 | 1983-11-29 | Martin Marietta Corporation | Coating for graphite electrodes |
US4487804A (en) * | 1982-08-02 | 1984-12-11 | Nalco Chemical Company | Coating to prevent the oxidation of electrodes during electric furnace steel making |
EP0146013A2 (en) * | 1983-11-30 | 1985-06-26 | Mitsumaru Chemical & Synthetic Industrial Co., Ltd. | Coating composition for preventing high temperature oxidation for electrodes |
EP0175136A1 (en) * | 1984-08-13 | 1986-03-26 | N P P Po Elektrotermia | Protecting coating for graphite electrodes |
US4617232A (en) * | 1982-04-15 | 1986-10-14 | Kennecott Corporation | Corrosion and wear resistant graphite material |
US4621017A (en) * | 1982-04-15 | 1986-11-04 | Kennecott Corporation | Corrosion and wear resistant graphite material and method of manufacture |
US4668579A (en) * | 1984-02-01 | 1987-05-26 | The United States Of America As Represented By The Secretary Of The Air Force | Interstitially protected oxidation resistant carbon-carbon composite |
US4716572A (en) * | 1984-12-19 | 1987-12-29 | Sigri Gmbh | Method for coating carbon and graphite bodies |
US4716078A (en) * | 1983-08-08 | 1987-12-29 | Kao Corporation | Substrate for a magnetic disc and method manufacturing same |
US4772514A (en) * | 1985-12-24 | 1988-09-20 | Ceskoslovenska Akademie Ved | Protective layer for carbonaceous materials and method of applying the same |
US4824733A (en) * | 1986-04-25 | 1989-04-25 | Canadian Patents And Development Limited/Societe | Anti-oxidant barrier for carbon based material |
US5695883A (en) * | 1991-09-17 | 1997-12-09 | Tocalo Co., Ltd. | Carbon member having a metal spray coating |
US6555173B1 (en) | 2000-11-08 | 2003-04-29 | Honeywell International Inc. | Carbon barrier controlled metal infiltration layer for enhanced oxidation protection |
WO2005113844A1 (en) * | 2004-05-14 | 2005-12-01 | Sgl Carbon Ag | Gas impervious electrodes for carbothermic reduction furnace |
US20060115243A1 (en) * | 2002-12-23 | 2006-06-01 | Jae-In Jeong | Resistance-heated boat and manufacturing method thereof |
US20090129762A1 (en) * | 2005-07-01 | 2009-05-21 | Ulrich Goetz | Initial Wetting Auxiliary Material for a Vaporiser Body |
US8923360B2 (en) | 2010-07-01 | 2014-12-30 | Graftech International Holdings Inc. | Graphite electrodes |
WO2022187638A1 (en) * | 2021-03-05 | 2022-09-09 | Ecolab Usa Inc. | Coatings for electrodes in electric arc furnaces |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US4567103A (en) * | 1983-07-28 | 1986-01-28 | Union Carbide Corporation | Carbonaceous articles having oxidation prohibitive coatings thereon |
CN112371087B (en) * | 2020-11-10 | 2021-09-21 | 昆明理工大学 | Preparation method and application of activated carbon fiber-based adsorbent for removing hydrogen sulfide, phosphine, arsine and ammonia gas |
-
1968
- 1968-07-24 US US747129A patent/US3553010A/en not_active Expired - Lifetime
- 1968-07-25 SE SE10145/68A patent/SE329966B/xx unknown
- 1968-07-26 GB GB35916/68A patent/GB1166429A/en not_active Expired
- 1968-07-26 AT AT732568A patent/AT285195B/en not_active IP Right Cessation
- 1968-07-26 FR FR1587074D patent/FR1587074A/fr not_active Expired
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3921023A (en) * | 1969-07-21 | 1975-11-18 | Dmz Lennin Bg1969072112705 | Method for joining carbon electrodes and product thereof |
US3881039A (en) * | 1971-01-22 | 1975-04-29 | Snam Progetti | Process for the treatment of amorphous carbon or graphite manufactured articles, for the purpose of improving their resistance to oxidation, solutions suitable for attaining such purpose and resulting product |
US3770488A (en) * | 1971-04-06 | 1973-11-06 | Us Air Force | Metal impregnated graphite fibers and method of making same |
US3864164A (en) * | 1971-10-22 | 1975-02-04 | British Steel Corp | Method for depositing protective coatings on carbon articles |
US4000026A (en) * | 1973-03-12 | 1976-12-28 | Union Carbide Corporation | Method and cement for bonding carbon articles |
FR2283874A1 (en) * | 1974-09-09 | 1976-04-02 | Secr Defence Brit | ANTI-OXIDATION COATING FOR CARBON PARTS |
US4418097A (en) * | 1981-12-11 | 1983-11-29 | Martin Marietta Corporation | Coating for graphite electrodes |
US4621017A (en) * | 1982-04-15 | 1986-11-04 | Kennecott Corporation | Corrosion and wear resistant graphite material and method of manufacture |
US4617232A (en) * | 1982-04-15 | 1986-10-14 | Kennecott Corporation | Corrosion and wear resistant graphite material |
US4487804A (en) * | 1982-08-02 | 1984-12-11 | Nalco Chemical Company | Coating to prevent the oxidation of electrodes during electric furnace steel making |
US4716078A (en) * | 1983-08-08 | 1987-12-29 | Kao Corporation | Substrate for a magnetic disc and method manufacturing same |
EP0146013A2 (en) * | 1983-11-30 | 1985-06-26 | Mitsumaru Chemical & Synthetic Industrial Co., Ltd. | Coating composition for preventing high temperature oxidation for electrodes |
EP0146013A3 (en) * | 1983-11-30 | 1985-08-07 | Mitsumaru Chemical & Synthetic Industrial Co., Ltd. | Coating composition for preventing high temperature oxidation for electrodes |
US4668579A (en) * | 1984-02-01 | 1987-05-26 | The United States Of America As Represented By The Secretary Of The Air Force | Interstitially protected oxidation resistant carbon-carbon composite |
EP0175136A1 (en) * | 1984-08-13 | 1986-03-26 | N P P Po Elektrotermia | Protecting coating for graphite electrodes |
US4750187A (en) * | 1984-08-13 | 1988-06-07 | N P P Po Elektrotermia | Graphitic electrode with protective coating |
US4716572A (en) * | 1984-12-19 | 1987-12-29 | Sigri Gmbh | Method for coating carbon and graphite bodies |
US4772514A (en) * | 1985-12-24 | 1988-09-20 | Ceskoslovenska Akademie Ved | Protective layer for carbonaceous materials and method of applying the same |
US4824733A (en) * | 1986-04-25 | 1989-04-25 | Canadian Patents And Development Limited/Societe | Anti-oxidant barrier for carbon based material |
US5695883A (en) * | 1991-09-17 | 1997-12-09 | Tocalo Co., Ltd. | Carbon member having a metal spray coating |
US6555173B1 (en) | 2000-11-08 | 2003-04-29 | Honeywell International Inc. | Carbon barrier controlled metal infiltration layer for enhanced oxidation protection |
US20060115243A1 (en) * | 2002-12-23 | 2006-06-01 | Jae-In Jeong | Resistance-heated boat and manufacturing method thereof |
WO2005113844A1 (en) * | 2004-05-14 | 2005-12-01 | Sgl Carbon Ag | Gas impervious electrodes for carbothermic reduction furnace |
US20090129762A1 (en) * | 2005-07-01 | 2009-05-21 | Ulrich Goetz | Initial Wetting Auxiliary Material for a Vaporiser Body |
US8923360B2 (en) | 2010-07-01 | 2014-12-30 | Graftech International Holdings Inc. | Graphite electrodes |
US9253827B2 (en) | 2010-07-01 | 2016-02-02 | Graftech International Holdings, Inc. | Graphite electrodes |
US9497804B2 (en) | 2010-07-01 | 2016-11-15 | Graftech International Holdings Inc. | Graphite electrode |
WO2022187638A1 (en) * | 2021-03-05 | 2022-09-09 | Ecolab Usa Inc. | Coatings for electrodes in electric arc furnaces |
Also Published As
Publication number | Publication date |
---|---|
SE329966B (en) | 1970-10-26 |
FR1587074A (en) | 1970-03-13 |
AT285195B (en) | 1970-10-12 |
GB1166429A (en) | 1969-10-08 |
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