EP0102892A1 - Process for manufacturing high purity metals and alloys - Google Patents
Process for manufacturing high purity metals and alloys Download PDFInfo
- Publication number
- EP0102892A1 EP0102892A1 EP83401671A EP83401671A EP0102892A1 EP 0102892 A1 EP0102892 A1 EP 0102892A1 EP 83401671 A EP83401671 A EP 83401671A EP 83401671 A EP83401671 A EP 83401671A EP 0102892 A1 EP0102892 A1 EP 0102892A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- metal
- metallic
- alloy
- chromium
- inclusions
- 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.)
- Granted
Links
- 239000002184 metal Substances 0.000 title claims abstract description 51
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 48
- 238000000034 method Methods 0.000 title claims abstract description 33
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 18
- 150000002739 metals Chemical class 0.000 title claims abstract description 14
- 229910045601 alloy Inorganic materials 0.000 title claims description 11
- 239000000956 alloy Substances 0.000 title claims description 11
- 230000008569 process Effects 0.000 title abstract description 11
- 239000011651 chromium Substances 0.000 claims abstract description 44
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 39
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 35
- 229910001092 metal group alloy Inorganic materials 0.000 claims abstract description 23
- 230000001603 reducing effect Effects 0.000 claims abstract description 19
- 239000003638 chemical reducing agent Substances 0.000 claims abstract description 14
- 239000010953 base metal Substances 0.000 claims abstract description 8
- 238000000859 sublimation Methods 0.000 claims abstract description 5
- 230000008022 sublimation Effects 0.000 claims abstract description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 32
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 32
- 238000000227 grinding Methods 0.000 claims description 21
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 17
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 claims description 13
- 238000007133 aluminothermic reaction Methods 0.000 claims description 13
- 238000006243 chemical reaction Methods 0.000 claims description 13
- 229910000423 chromium oxide Inorganic materials 0.000 claims description 13
- KMUONIBRACKNSN-UHFFFAOYSA-N potassium dichromate Chemical compound [K+].[K+].[O-][Cr](=O)(=O)O[Cr]([O-])(=O)=O KMUONIBRACKNSN-UHFFFAOYSA-N 0.000 claims description 10
- 230000007547 defect Effects 0.000 claims description 9
- 239000011230 binding agent Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 8
- 238000010408 sweeping Methods 0.000 claims description 7
- 229910044991 metal oxide Inorganic materials 0.000 claims description 6
- 150000004706 metal oxides Chemical class 0.000 claims description 6
- 239000006229 carbon black Substances 0.000 claims description 5
- 239000007789 gas Substances 0.000 claims description 5
- 230000003647 oxidation Effects 0.000 claims description 5
- 238000007254 oxidation reaction Methods 0.000 claims description 5
- 239000001257 hydrogen Substances 0.000 claims description 4
- 229910052739 hydrogen Inorganic materials 0.000 claims description 4
- 230000001590 oxidative effect Effects 0.000 claims description 4
- 238000000926 separation method Methods 0.000 claims description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 3
- 239000000654 additive Substances 0.000 claims description 3
- 230000007935 neutral effect Effects 0.000 claims description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- 229910001021 Ferroalloy Inorganic materials 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- 230000000996 additive effect Effects 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 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 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000010955 niobium Substances 0.000 claims description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 2
- 238000002360 preparation method Methods 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000010937 tungsten Substances 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 2
- 229910002065 alloy metal Inorganic materials 0.000 claims 1
- 229910001038 basic metal oxide Inorganic materials 0.000 claims 1
- 239000003795 chemical substances by application Substances 0.000 abstract description 3
- 238000005275 alloying Methods 0.000 abstract description 2
- 238000003801 milling Methods 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 18
- 229910052760 oxygen Inorganic materials 0.000 description 18
- 239000001301 oxygen Substances 0.000 description 18
- 239000000047 product Substances 0.000 description 17
- 230000009467 reduction Effects 0.000 description 12
- 229920001342 Bakelite® Polymers 0.000 description 8
- 239000004637 bakelite Substances 0.000 description 8
- HYBBIBNJHNGZAN-UHFFFAOYSA-N furfural Chemical compound O=CC1=CC=CO1 HYBBIBNJHNGZAN-UHFFFAOYSA-N 0.000 description 6
- 229910000601 superalloy Inorganic materials 0.000 description 6
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 5
- 239000003570 air Substances 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 3
- QDOXWKRWXJOMAK-UHFFFAOYSA-N chromium(III) oxide Inorganic materials O=[Cr]O[Cr]=O QDOXWKRWXJOMAK-UHFFFAOYSA-N 0.000 description 3
- 238000005868 electrolysis reaction Methods 0.000 description 3
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 3
- 229910052753 mercury Inorganic materials 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 239000008188 pellet Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 239000002893 slag Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 238000005054 agglomeration Methods 0.000 description 2
- 230000002776 aggregation Effects 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 150000002894 organic compounds Chemical class 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000007873 sieving Methods 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- 229910001309 Ferromolybdenum Inorganic materials 0.000 description 1
- 229910000519 Ferrosilicon Inorganic materials 0.000 description 1
- 229910001145 Ferrotungsten Inorganic materials 0.000 description 1
- 229910000628 Ferrovanadium Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 239000010431 corundum Substances 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- PNXOJQQRXBVKEX-UHFFFAOYSA-N iron vanadium Chemical compound [V].[Fe] PNXOJQQRXBVKEX-UHFFFAOYSA-N 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052752 metalloid Inorganic materials 0.000 description 1
- 150000002738 metalloids Chemical class 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- XVOFZWCCFLVFRR-UHFFFAOYSA-N oxochromium Chemical compound [Cr]=O XVOFZWCCFLVFRR-UHFFFAOYSA-N 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 229910000753 refractory alloy Inorganic materials 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000006228 supernatant Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B1/00—Preliminary treatment of ores or scrap
- C22B1/14—Agglomerating; Briquetting; Binding; Granulating
- C22B1/24—Binding; Briquetting ; Granulating
- C22B1/242—Binding; Briquetting ; Granulating with binders
- C22B1/244—Binding; Briquetting ; Granulating with binders organic
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B1/00—Preliminary treatment of ores or scrap
- C22B1/14—Agglomerating; Briquetting; Binding; Granulating
- C22B1/24—Binding; Briquetting ; Granulating
- C22B1/2406—Binding; Briquetting ; Granulating pelletizing
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B1/00—Preliminary treatment of ores or scrap
- C22B1/14—Agglomerating; Briquetting; Binding; Granulating
- C22B1/24—Binding; Briquetting ; Granulating
- C22B1/242—Binding; Briquetting ; Granulating with binders
- C22B1/244—Binding; Briquetting ; Granulating with binders organic
- C22B1/245—Binding; Briquetting ; Granulating with binders organic with carbonaceous material for the production of coked agglomerates
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B34/00—Obtaining refractory metals
- C22B34/30—Obtaining chromium, molybdenum or tungsten
- C22B34/32—Obtaining chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B5/00—General methods of reducing to metals
- C22B5/02—Dry methods smelting of sulfides or formation of mattes
- C22B5/04—Dry methods smelting of sulfides or formation of mattes by aluminium, other metals or silicon
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S75/00—Specialized metallurgical processes, compositions for use therein, consolidated metal powder compositions, and loose metal particulate mixtures
- Y10S75/959—Thermit-type reaction of solid materials only to yield molten metal
Definitions
- the present invention relates to a method for manufacturing metals or metal alloys of high purity, in particular metallic chromium.
- the superalloys concerned require extremely careful and sophisticated processing from very high quality raw materials, both in chemical purity and in regularity. This is in particular the case for pure metallic chromium which is used as an alloying element providing the superalloys with resistance to hot oxidation.
- the electrolytic technique makes it possible to obtain a metallic chromium of very good chemical purity which however contains too many gases which are very harmful for superalloys, in particular oxygen, hydrogen and nitrogen.
- a reduction degassing is then carried out under vacuum, so that the content of chromium oxygen falls from 2000 to 5000 ppm for the raw electrolysis product to 300 - 500 ppm for the metallic chromium obtained after treatment.
- This treatment also makes it possible to appreciably lower the hydrogen and nitrogen contents as well as the contents in certain volatile metals such as lead or in certain. metalloids like sulfur.
- the aluminothermic technique consists of reducing chemically pure chromium oxide (99.5 to 99.7% Cr203) at very high temperature, ie above 2000 ° C, using powdered aluminum. Even if by a suitable choice of the raw materials used and by an evolved and very careful reaction technology we manage to obtain very satisfactory chemical purities on the whole and in some cases better than by electrolysis, the igneous elaboration used inevitably leads to the presence in the pure metallic chromium obtained, returned to ambient temperature, of non-metallic oxidized inclusions of alumina and chromium oxide.
- the oxygen content which is the consequence thereof and which varies inversely with the content of residual reducing agent in metallic chromium, in this case the aluminum content, is then prohibitive for the noblest aeronautical uses which, moreover, cannot tolerate very low residual aluminum contents.
- the process of the invention makes it possible to manufacture different metals, in particular chromium, and different alloys, with high purity.
- the process of the invention is based essentially on a primary production of a metal or of a metal alloy preferably containing non-metallic inclusions oxidized from the base metal, easily reducible, which is then ground and agglomerated before being subjected to a vacuum reducing treatment.
- the primary production of the metal or of the metal bond is preferably obtained by an unbalanced aluminothermic reaction allowing the content of difficultly reducible aluminous inclusions to be reduced to a minimum, but this preparation can also be obtained by other techniques, for example by silicothermal , by reduction in an electric oven, etc., provided that the characteristics of the non-metallic inclusions make it possible to reproduce the subsequent stages of grinding and reducing treatment under vacuum.
- the metals or metal alloys which can be obtained with high purity by the process of the invention are those likely to include reducible non-metallic inclusions which can be practically eliminated at the end of the grinding and reduction steps under vacuum, such as the own oxides of the base metal.
- the metals which can be produced with the process of the invention mention may in particular be made of chromium, titanium, vanadium, molybdenum, manganese, niobium and tungsten.
- the alloys envisaged in the context of the invention are alloys comprising at least one of the preceding metals, and / or boron, these alloys also comprising ferro-alloys in general.
- step a) comprises an aluminothermic reaction between at least one metal oxide and divided aluminum, the reaction being unbalanced by an aluminum defect relative to the usual amount, for producing a metal or a metal alloy containing reducible non-metallic inclusions consisting mainly of inclusions of the base metal oxide, the occurrence of inclusions of alumina Ai 2 0 3 being minimized.
- This defect in aluminum which can represent from 0.5 to 8%, preferably from 2 to 5%, by weight of the usual amount, is essential in order to minimize the inclusions of alumina which are the most difficult to reduce.
- the preferred metal for carrying out the process of the invention is chromium.
- the metallic chromium will advantageously be prepared by an unbalanced aluminothermic reaction, of the type indicated above, between chromium oxide, optionally an additive such as potassium dichromate, and divided aluminum.
- chromium oxide optionally an additive such as potassium dichromate
- additives of this kind is well known in the field of aluminothermy to provide additional oxygen and to heat the aluminothermic reaction.
- the grinding step (b) is advantageously carried out using an impact mill, for example a hammer mill.
- the grinding of the metal or of the metal alloy is a so-called "purifying" grinding.
- This purification associated with grinding is not compulsory, but of course preferred, because it allows a first physical separation of the non-metallic inclusions before the reducing treatment of step (c).
- non-metallic inclusions released during the purifying grinding seem to be preferably the inclusions of base metal oxide, for example the inclusions of Cr 2 0 3 in the caa of the production of metallic chromium.
- the purifying grinding is advantageously supplemented by elimination by sieving or any other selective separation of the finest particles from the ground product in which almost all of the non-metallic inclusions released by the grinding are found concentrated.
- the ground product thus obtained, from which part of the non-metallic inclusions will have been eliminated, is then agglomerated with an agglomerant and a reducing agent to form balls.
- the binder will advantageously consist of an organic compound or a mixture of organic compounds capable of leaving, during the heating of step (c), a carbon skeleton which completes the reducing action of the reducing agent.
- the binder can be constituted by a mixture of bakelite and furfuraldehyde and the reducing agent will advantageously be constituted by carbon black.
- the balls are shaped in a conventional compacting press and then baked at a set temperature, for example between 200 and 230 ° C to avoid any oxidation of the metal or metals constituting the balls, while obtaining satisfactory cohesion.
- the reducing treatment is carried out in a vacuum oven and is optionally supplemented by sweeping using a non-oxidizing or reducing gas which is not soluble in the metal or the alloy.
- the metal product obtained after reduction treatment under vacuum is cooled in a neutral atmosphere and can then be used in the manufacture of metal parts.
- Chromium oxide (Cr 2 O 3 ), potassium dichromate (Cr 2 O 7 K 2 ) and divided aluminum are introduced into an aluminothermic crucible, lined with a refractory material. and potassium dichromate are advantageously commercial products having a particle size between 0 and 15 ⁇ , while the divided aluminum consists of grains less than 1 mm.
- Chromium oxide and potassium dichromate are present in the proportions of the classic aluminothermic reaction, while aluminum is present with a defect compared to the proportion of the classic aluminothermic reaction. As indicated above, this defect in aluminum can represent from 0.5 to 8%, preferably from 2 to 5% by weight of the usual amount.
- the three constituents are mixed thoroughly and the reaction is initiated in the crucible as appropriate.
- the reaction temperature quickly reaches a value of about 2200 ° C., and at the end of the reaction, the metal is collected at the bottom of the crucible, and a supernatant slag.
- the analysis of the metallic chromium obtained shows that by deliberately choosing to remain below the usual proportions, with the consequence of not achieving the optimum extracting yield, the residual aluminum content in the metallic chromium drops to very low levels below 0.01% (100 ppm). This analysis also shows that the content of non-metallic inclusions rises very quickly to reach high levels of 0.40 to 0.80%, or even more, but that these non-metallic inclusions are almost entirely composed of chromium oxide. not reduced (Cr 2 0 3 ) with very little Al 2 O 3 .
- non-metallic alumina Al 2 O 3 present in normal solidified pure metallic chromium do not consist of reaction slag (chromium corundum, i.e. aluminous slag from reduction by aluminum) poorly decanted and having been trapped during the passage of the metal from the liquid state to the solid state.
- reaction slag chromium corundum, i.e. aluminous slag from reduction by aluminum
- it is a secondary alumina formed either at the time of solidification, or even in the metal in the solid state slightly below the temperature of the solidus, therefore at a still very high temperature where the diffusion phenomena and the reactivity of the components is still very high.
- This secondary alumina would in fact result from the reaction, the equilibrium conditions having shifted with the drop in temperature where the state is by nature out of equilibrium, between chromium oxide or oxygen dissolved in chromium metal and excess residual aluminum also present in chromium metal.
- the residual aluminum is in an amount large enough to be able to reduce all of the chromium oxide or dissolved oxygen and there is even an unused excess in chromium.
- the non-metallic inclusions which remain trapped in the solid metal are then almost entirely formed of alumina A1 2 0 3 .
- the operation is carried out, in accordance with the process of the invention, with an aluminum defect with respect to the previous usual quantity, the residual aluminum present is in insufficient quantity to be able to reduce all of the chromium oxide or of the dissolved oxygen.
- All or almost all aluminum present is oxidized by the oxygen present (phase equilibrium in slow cooling) and the excess of chromium oxide or unreduced dissolved oxygen precipitates in the form of non-metallic inclusions Cr 2 0 3 .
- step a) The unbalanced aluminothermic reaction of step a) obviously gives a slightly less good yield than in conventional aluminothermic processes.
- the elemental chromium is nevertheless reduced and the final product obtained is a metallic chromium of high purity, identical to normal aluminothermic metallic chromium of good quality, except that it contains a very high oxygen content ( 2000 to 3000 ppm or more), but in the almost exclusive form of non-metallic Cr 2 O 3 inclusions (0.40 to 0.80% or more) with the presence of very few aluminous inclusions A1 2 0 3 (100 to 400 ppm corresponding to 50 to 200 ppm of oxygen bound to aluminum).
- Metallic chromium is therefore obtained with non-metallic inclusions mainly constituted by Cr 2 O 3 inclusions which are easy to remove and secondarily by alumina inclusions, which are more difficult to remove, but in small quantities.
- the metallic chromium from step a) is ground in an impact mill advantageously constituted by a high energy mill of the hammer type (mobile hammers / counter hammers) until a fine powder is obtained which passes entirely through a sieve with 200 ⁇ mesh opening.
- the high impact energy of the grinder causes the grains to burst, which releases, at least in large part, the non-metallic inclusions Al 2 0 3 and Cr 2 0 3 contained in the metal, the inclusions Cr 2 0 3 appearing preferentially released. .
- the grinding is a purifying grinding which produces ventilation, that is to say a certain flow of purge air.
- This ventilation can be produced directly by the crusher itself or indirectly by an additional device, such as a blower.
- This sweeping air makes it possible to ventilate the product during grinding, which on the one hand prevents the product from overheating, and therefore possibly its oxidation and nitriding by ambient air, and on the other hand causes the most fractions. fine and lighter in the sweeping air stream, that is to say preferably the non-metallic inclusions released, the density of which is lower.
- the air flow can be adjusted voluntarily to accentuate, if desired, the purifying effect.
- this purifying effect can be supplemented by elimination by sieving or any other selective separation of the finest particles from the ground product in which almost all of the non-metallic inclusions released by grinding are found concentrated.
- the purified chromium powder thus obtained is then intimately mixed with a reducing agent and a binder.
- a reducing agent and a binder are advantageously constituted by a mixture of bakelite and furfuraldehyde.
- Furfuraldehyde aims to facilitate agglomeration when cold, the bakelite dissolved in the furfuraldehyde forming cold glue, as well as the subsequent polymerization of the hot bakelite.
- other thermosetting agglomerants and other solvents can be used.
- the reducer for its part, is advantageously constituted by carbon black which complements the carbon of the bakelite.
- the respective amounts of these products are variable but are generally adjusted, with a slight excess, to the residual oxygen content of the ground product.
- the reducing / binder mixture may consist of 0.1% bakelite, 0.3% of furfuraldehyde and 0.05 to 0.2% of carbon black, these percentages being based on the weight of the crushed product.
- the mixture obtained is shaped into balls or pellets by means of a conventional compacting press, such as a ball press with tangential wheels or a tableting press. After agglomeration, the mixture is baked at the appropriate temperature (200 to 230 ° C approximately) to remove the volatile furfuraldehyde and polymerize the bakelite which forms a binder and gives resistance to the balls or pellets.
- a conventional compacting press such as a ball press with tangential wheels or a tableting press.
- oven temperature must be limited to the minimum necessary in order to avoid any oxidation of the product.
- the balls or pellets obtained in the previous step are then subjected to a reducing treatment under vacuum at 1100 ° -1400 ° C under high vacuum of the order of 10 -4 mm of mercury.
- the bakelite decomposes at around 600 ° C, leaving a carbon skeleton which is added to the carbon black introduced as a reducing agent in the mixture.
- this carbon reacts on the oxygen of the Cr203 remaining in the product but practically not on the oxygen of the alumina Al 2 O 3 because to reduce the alumina it would be necessary to operate at a higher temperature. high and reach deeper voids.
- the vacuum is reduced in the treatment oven to 10 mm of mercury by sweeping controlled by a non-oxidizing or reducing gas, such as hydrogen, which has the particularity of being practically not soluble in solid chromium.
- a non-oxidizing or reducing gas such as hydrogen
- a product containing at most 300 to 400 ppm of total oxygen in the form of 200 to 300 ppm of alumina approximately containing 100 to 150 ppm of oxygen and about 500 ppm maximum of unreduced chromium oxide containing about 150 ppm of oxygen. It is therefore a chromium of high purity which makes it possible to develop superalloys which can be used in particular in the manufacture of the noble parts of aeronautical turbo-engines.
- step a the use of a conventional starting product without imbalance in step a) would necessarily lead, insofar as it is desired to lower the oxygen content to the required level of about 300 ppm, treatment allowing the reduction of Al 2 O 3 by carbon which, in addition to the preceding drawbacks, would bring a rise in the residual aluminum content of the finished product to levels not acceptable by the users preparing the superalloys.
- step a) can be carried out other than by aluminothermy, for example by silicothermal or else by reduction in an electric furnace, to obtain a metal or alloy comprising oxidized non-metallic inclusions of the base metal.
- ferro-chromium or chromium metal by reduction with silicon metal or silico-chromium, as well as the manufacture of ferro-tungsten or ferro-molybdenum, by way of non-limiting examples. by reduction with one; high-grade ferro-silicon or metal silicon.
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Abstract
Description
La présente invention concerne un procédé de fabrication de métaux ou d'alliages métalliques de pureté élevée, en particulier de chrome métallique.The present invention relates to a method for manufacturing metals or metal alloys of high purity, in particular metallic chromium.
Les industries modernes exigent de plus en plus de métaux et d'alliages métalliquesde pureté élevée pour la fabrication de pièces mécaniques.Modern industries increasingly demand high purity metals and metal alloys for the manufacture of mechanical parts.
C'est le cas notamment des parties nobles des turbo-moteurs aéronautiques qui requièrent des alliages super-réfractaires, appelés "super-alliages" de très haute qualité, car il s'agit des pièces les plus fortement sollicitées, tant au point de vue thermique que mécanique. De telles pièces comprennent des ailettes fixes et mobiles de _turbines, des disques de turbines, des chambres de combustion, des tuyères, etc.This is the case in particular for the noble parts of aeronautical turbo-engines which require super-refractory alloys, called "super-alloys" of very high quality, because they are the most heavily stressed parts, both from the point of view thermal than mechanical. Such parts include stationary and movable fins of turbines, turbine disks, combustion chambers, nozzles, etc.
Afin d'obtenir des caractéristiques satisfaisantes, les super-alliages concernés exigent des élaborations extrêmement soignées et sophistiquées à partir de matières premières de très haute qualité, tant en pureté chimique qu'en régularité. C'est en particulier le cas pour le chrome métallique pur qui est utilisé comme élément d'alliage apportant aux super-alliages la résistance à l'oxydation à chaud.In order to obtain satisfactory characteristics, the superalloys concerned require extremely careful and sophisticated processing from very high quality raw materials, both in chemical purity and in regularity. This is in particular the case for pure metallic chromium which is used as an alloying element providing the superalloys with resistance to hot oxidation.
Il existe à l'heure actuelle deux techniques d'élaboration du chrome métallique pur, à savoir la technique électrolytique et la technique alumino-thermique.There are currently two techniques for producing pure metallic chromium, namely the electrolytic technique and the alumino-thermal technique.
La technique électrolytique permet d'obtenir un chrome métallique de très bonne pureté chimique qui contient cependant trop de gaz très nocifs pour les super-alliages, en particulier de l'oxygène, de l'hydrogène et de l'azote.The electrolytic technique makes it possible to obtain a metallic chromium of very good chemical purity which however contains too many gases which are very harmful for superalloys, in particular oxygen, hydrogen and nitrogen.
Pour améliorer la qualité du chrome métallique obtenu par électrolyse, on procède ensuite à un dégazage réducteur sous vide, si bien que la teneur en oxygène du chrome tombe de 2000 à 5000 ppm pour le produit brut d'électrolyse à 300 - 500 ppm pour le chrome métallique obtenu après traitement. Ce traitement permet également d'abaisser sensiblement les teneurs en hydrogène et en azote ainsi que les teneurs en certains métaux volatils comme le plomb ou en certains . métalloïdes comme le soufre.To improve the quality of the metallic chromium obtained by electrolysis, a reduction degassing is then carried out under vacuum, so that the content of chromium oxygen falls from 2000 to 5000 ppm for the raw electrolysis product to 300 - 500 ppm for the metallic chromium obtained after treatment. This treatment also makes it possible to appreciably lower the hydrogen and nitrogen contents as well as the contents in certain volatile metals such as lead or in certain. metalloids like sulfur.
C'est généralement ce chrome électrolytique dégazé sous vide qui, en raison de sa pureté élevée et de sa faible teneur en oxygène, est préféré pour la production des pièces nobles de turbomachines aéronautiques.It is generally this electrolytic chromium degassed under vacuum which, because of its high purity and its low oxygen content, is preferred for the production of noble parts of aeronautical turbomachines.
La technique aluminothermique consiste à réduire à très haute température, à savoir à plus de 2000°C, de l'oxyde de chrome chimiquement pur (99,5 à 99,7 % de Cr203) par de l'aluminium en poudre. Même si par un choix convenable des matières premières utilisées et par une technologie de réaction évoluée et très soignée on parvient à obtenir des puretés chimiques très satisfaisantes dans l'ensemble et dans certains cas meilleures que par électrolyse, l'élaboration ignée utilisée conduit inévitablement à la présence dans le chrome métallique pur obtenu, revenu à la température ambiante, d'inclusions non métalliques oxydées d'alumine et d'oxyde de chrome. La teneur en oxygène qui en est la conséquence et qui varie en fonction inverse de la teneur en réducteur résiduel dans le chrome métallique, en l'occurence la teneur en aluminium, est alors prohibitive pour les usages aéronautiques les plus nobles qui par ailleurs ne peuvent tolérer que des teneurs en aluminium résiduel très basses.The aluminothermic technique consists of reducing chemically pure chromium oxide (99.5 to 99.7% Cr203) at very high temperature, ie above 2000 ° C, using powdered aluminum. Even if by a suitable choice of the raw materials used and by an evolved and very careful reaction technology we manage to obtain very satisfactory chemical purities on the whole and in some cases better than by electrolysis, the igneous elaboration used inevitably leads to the presence in the pure metallic chromium obtained, returned to ambient temperature, of non-metallic oxidized inclusions of alumina and chromium oxide. The oxygen content which is the consequence thereof and which varies inversely with the content of residual reducing agent in metallic chromium, in this case the aluminum content, is then prohibitive for the noblest aeronautical uses which, moreover, cannot tolerate very low residual aluminum contents.
Le procédé de l'invention permet de fabriquer différents métaux, notamment du chrome, et différents alliages,avec une pureté élevée.The process of the invention makes it possible to manufacture different metals, in particular chromium, and different alloys, with high purity.
Le procédé de l'invention est fondé essentiellement sur une élaboration primaire d'un métal ou d'un alliage métallique contenant préférentiellement des inclusions non métalliques oxydées du métal de base, facilement réductibles, qui est ensuite broyé et aggloméré avant d'être soumis à un traitement réducteur sous vide.The process of the invention is based essentially on a primary production of a metal or of a metal alloy preferably containing non-metallic inclusions oxidized from the base metal, easily reducible, which is then ground and agglomerated before being subjected to a vacuum reducing treatment.
L'élaboration primaire du métal ou de laLliage métallique est de préférence obtenue par une réaction aluminothermique déséquilibrée permettant d'abaisser au minimum la teneur en inclusions alumineuses difficilement réductibles, mais cette élaboration peut être également obtenue par d'autres techniques, par exemple par silicothermie, par réduction au four électrique, etc., à condition que les caractéristiques des inclusions non métalliques permettent de reproduire les étapes ultérieures de broyage et de traitement réducteur sous vide.The primary production of the metal or of the metal bond is preferably obtained by an unbalanced aluminothermic reaction allowing the content of difficultly reducible aluminous inclusions to be reduced to a minimum, but this preparation can also be obtained by other techniques, for example by silicothermal , by reduction in an electric oven, etc., provided that the characteristics of the non-metallic inclusions make it possible to reproduce the subsequent stages of grinding and reducing treatment under vacuum.
Selon la caractéristique essentielle du procédé de l'invention, celui-ci comporte les étapes qui consistent à :
- a) élaborer un métal ou un alliage métallique dont les inclusions non métalliques sont préférentiellement des oxydes du métal de base facilement réductibles,
- b) broyer le métal ou l'alliage métallique ainsi obtenu et agglomérer le métal ou l'alliage métallique broyé avec un agglomérant et un agent réducteur pour former des boulets, et
- c) soumettre les boulets à un traitement réducteur sous vide dans des conditbns réglées de pression et de température pour que l'agent réducteur réagisse sur les inclusions non métalliques réductibles et qu'il n'y ait pas de sublimation substantielle du métal ou des métaux d'alliage, le cas échéant.
- a) developing a metal or a metal alloy whose non-metallic inclusions are preferably easily reducible base metal oxides,
- b) grinding the metal or the metal alloy thus obtained and agglomerating the ground metal or metal alloy with a binder and a reducing agent to form balls, and
- c) subjecting the balls to a reducing treatment under vacuum under controlled conditions of pressure and temperature so that the reducing agent reacts on the reducible non-metallic inclusions and that there is no substantial sublimation of the metal or of the metals alloy, if applicable.
Comme indiqué précédemment, les métaux ou les alliages métalliques pouvant être obtenus avec une pureté élevée grâce au procédé de l'invention sont ceux susceptibles de comprendre des inclusions non métalliques réductibles pouvant être pratiquement éliminées à l'issue des étapes de broyage et de réduction sous vide, tels que les propres oxydes du métal de base.As indicated above, the metals or metal alloys which can be obtained with high purity by the process of the invention are those likely to include reducible non-metallic inclusions which can be practically eliminated at the end of the grinding and reduction steps under vacuum, such as the own oxides of the base metal.
Parmi les métaux pouvant être fabriqués avec le procédé de l'invention, on peut citer notamment le chrome, le titane, le vanadium, le molybdène, le manganèse, le niobium et le tungstène. De même, les alliages envisagés dans le cadre de l'invention sont des alliages comprenant l'un au moins des métaux précédents, et/ou le bore, ces alliages comprenant aussi les ferro-alliages en général.Among the metals which can be produced with the process of the invention, mention may in particular be made of chromium, titanium, vanadium, molybdenum, manganese, niobium and tungsten. Likewise, the alloys envisaged in the context of the invention are alloys comprising at least one of the preceding metals, and / or boron, these alloys also comprising ferro-alloys in general.
Conformément au mode de réalisation préféré de l'invention, l'étape a) comprend une réaction aluminothermique entre au moins un oxyde métallique et de l'aluminium divisé, la réaction étant déséquilibrée par un défaut en aluminium par rapport à la quantité usuelle, pour produire un métal ou un alliage métallique contenant des inclusions non métalliques réductibles constituées principalement par des inclusions de l'oxyde métallique de base, l'apparition d'inclusions d'alumine Ai203 étant réduite au minimum.In accordance with the preferred embodiment of the invention, step a) comprises an aluminothermic reaction between at least one metal oxide and divided aluminum, the reaction being unbalanced by an aluminum defect relative to the usual amount, for producing a metal or a metal alloy containing reducible non-metallic inclusions consisting mainly of inclusions of the base metal oxide, the occurrence of inclusions of alumina Ai 2 0 3 being minimized.
Ce défaut en aluminium qui peut représenter de 0,5 à 8 %, de préférence de 2 à 5 %, en poids de la quantité usuelle est indispensable pour abaisser au minimum les inclusions d'alumine qui sont les plus difficilement réductibles.This defect in aluminum, which can represent from 0.5 to 8%, preferably from 2 to 5%, by weight of the usual amount, is essential in order to minimize the inclusions of alumina which are the most difficult to reduce.
Cette réaction aluminothermique déséquilibrée par un défaut volontaire et important d'aluminium par rapport à la quantité usuelle va tout à fait à l'encontre des procédés aluminothermiques habituels où l'on utilise toujours des quantités d'aluminium plus élevées et plus proches de la stoechiométrie de la réaction, de manière à obtenir le rendement maximal, pour lequel on obtient un produit dont les inclusions non métalliques sont constituées en majeure partie par des inclusions d'alumine difficilement réductibles.This aluminothermic reaction unbalanced by a voluntary and significant defect in aluminum compared to the usual quantity goes completely against the usual aluminothermic processes where one always uses higher quantities of aluminum and closer to stoichiometry of the reaction, so to obtain the maximum yield, for which a product is obtained whose non-metallic inclusions consist for the most part of inclusions of alumina which are difficult to reduce.
Comme indiqué précédemment, le métal préféré pour la mise en oeuvre du procédé de l'invention est le chrome.As indicated previously, the preferred metal for carrying out the process of the invention is chromium.
Le chrome métallique sera avantageusement préparé par une réaction aluminothermique déséquilibrée, du type indiqué précédemment, entre de l'oxyde de chrome éventuellement un additif tel que du bichromate de potassium, et de l'aluminium divisé. L'utilisation d'additifs de ce genre est bien connue dans le domaine de l'aluminothermie pour apporter de l'oxygène supplémentaire et réchauffer la réaction aluminothermique.The metallic chromium will advantageously be prepared by an unbalanced aluminothermic reaction, of the type indicated above, between chromium oxide, optionally an additive such as potassium dichromate, and divided aluminum. The use of additives of this kind is well known in the field of aluminothermy to provide additional oxygen and to heat the aluminothermic reaction.
L'étape (b) de broyage est avantageusement effectuée au moyen d'un broyeur à choc , par exemple d'un broyeur à marteaux.The grinding step (b) is advantageously carried out using an impact mill, for example a hammer mill.
Dans le mode de réalisation préféré de l'invention, le broyage du métal ou de l'alliage métallique est un broyage dit "épurant".qui permet de produire un certain débit d'air de balayage pour entraîner en partie les inclusions non métalliques libérées lors du broyage. Cette épuration associée au broyage n'est pas obligatoire, mais bien entendu préférée, car elle permet une première séparation physique des inclusions non métalliques avant le traitement réducteur de l'étape (c). Il faut cependant noter que les inclusions non métalliques libérees lors du broyage épurant semblent être préférentiellement les inclusions d'oxyde de métal de base, par exemple les inclusions de Cr203 dans le caa de la fabrication de chrome métallique.In the preferred embodiment of the invention, the grinding of the metal or of the metal alloy is a so-called "purifying" grinding. Which makes it possible to produce a certain flow of sweeping air to partially entrain the released non-metallic inclusions. during grinding. This purification associated with grinding is not compulsory, but of course preferred, because it allows a first physical separation of the non-metallic inclusions before the reducing treatment of step (c). However, it should be noted that non-metallic inclusions released during the purifying grinding seem to be preferably the inclusions of base metal oxide, for example the inclusions of Cr 2 0 3 in the caa of the production of metallic chromium.
Le broyage épurant est avantageusement complété par l'élimination par tamisage ou touteautre séparation sélective des particules les plus fines du produit broyé où se retrouvent concentréesla quasi totalité des inclusions non métalliques libérées par le broyage.The purifying grinding is advantageously supplemented by elimination by sieving or any other selective separation of the finest particles from the ground product in which almost all of the non-metallic inclusions released by the grinding are found concentrated.
Le produit broyé ainsi obtenu, dont une partie des inclusions non métalliques aura été éliminée,est ensuite aggloméré avec un agglomérant et un agent réducteur pour former des.boulets. L'agglomérant sera avantageusement constitué par un composé organique ou un mélange de composés organiques susceptibles de laisser, lors du chauffage de l'étape (c), un squelette carboné venant compléter l'action réductrice de l'agent réducteur. Ainsi, l'agglomérant pourra être constitué par un mélange de bakélite et de furfuraldéhyde et l'agent réducteur sera avantageusement constitué par du noir de carbone.The ground product thus obtained, from which part of the non-metallic inclusions will have been eliminated, is then agglomerated with an agglomerant and a reducing agent to form balls. The binder will advantageously consist of an organic compound or a mixture of organic compounds capable of leaving, during the heating of step (c), a carbon skeleton which completes the reducing action of the reducing agent. Thus, the binder can be constituted by a mixture of bakelite and furfuraldehyde and the reducing agent will advantageously be constituted by carbon black.
Lors de l'étape(b), les boulets sont mis en forme dans une presse à compacter classique puis étuvés à température réglée, par exemple entre 200 et 230°C pour éviter toute oxydation du métal ou des métaux constituant les boulets, tout en obtenant une cohésion satisfaisante.During step (b), the balls are shaped in a conventional compacting press and then baked at a set temperature, for example between 200 and 230 ° C to avoid any oxidation of the metal or metals constituting the balls, while obtaining satisfactory cohesion.
Conformément au mode de réalisation préféré de l'invention, le traitement réducteur est effectué dans un four à vide et est complété éventuellement par un balayage au moyen d'un gaz non oxydant ou réducteur non soluble dans le métal ou l'alliage.In accordance with the preferred embodiment of the invention, the reducing treatment is carried out in a vacuum oven and is optionally supplemented by sweeping using a non-oxidizing or reducing gas which is not soluble in the metal or the alloy.
Le produit métallique obtenu après traitement réducteur sous vide est-refroidi en atmosphère neutre et peut être ensuite être utilisé dans la fabrication de pièces métalliques.The metal product obtained after reduction treatment under vacuum is cooled in a neutral atmosphere and can then be used in the manufacture of metal parts.
D'autres caractéristiques et avantages de l'invention résulteront de la description détaillée qui suit et qui se réfère à la fabrication de chrome métallique de pureté élevée par une réaction aluminothermique déséquilibrée. Cette description ne constitue qu'un exemple non limitatif et ne saurait en aucun cas limiter la portée de l'invention.Other characteristics and advantages of the invention will emerge from the detailed description which follows and which refers to the production of metallic chromium of high purity by an unbalanced aluminothermic reaction. This description is only a non-limiting example and cannot in any way limit the scope of the invention.
On introduit dans un creuset aluminothermique, garni d'une matière réfractaire, de l'oxyde de chrome (Cr2O3) du bichromate de potassium (Cr2O7K2) et de l'aluminium divisé.L'oxyde de chrome et le bichromate de potassium sont avantageusement des produits du commerce ayant une granulométrie comprise entre O et 15 µ, tandis que l'aluminium divisé est constitué par des grains inférieurs à 1 mm.Chromium oxide (Cr 2 O 3 ), potassium dichromate (Cr 2 O 7 K 2 ) and divided aluminum are introduced into an aluminothermic crucible, lined with a refractory material. and potassium dichromate are advantageously commercial products having a particle size between 0 and 15 μ, while the divided aluminum consists of grains less than 1 mm.
L'oxyde de chrome et le bichromate de potassium sont présents dans les proportions de la réaction aluminothermique classique, tandis que l'aluminium est présent avec un défaut par rapport à la proportion de la réaction aluminothermique classique. Comme indiqué plus haut, ce défaut d'aluminium peut représenter de 0,5 à 8 %, de préférence de 2 à 5 % en poids de la quantité usuelle.Chromium oxide and potassium dichromate are present in the proportions of the classic aluminothermic reaction, while aluminum is present with a defect compared to the proportion of the classic aluminothermic reaction. As indicated above, this defect in aluminum can represent from 0.5 to 8%, preferably from 2 to 5% by weight of the usual amount.
Les trois constituants sont mélangés soigneusement puis la réaction est initiée dans le creuset de façon appropriée. La température de la réaction atteint rapidement une valeur d'environ 2200°C, et à l'issue de la réaction, on recueille le métal au fond du creuset, et un laitier surnageant.The three constituents are mixed thoroughly and the reaction is initiated in the crucible as appropriate. The reaction temperature quickly reaches a value of about 2200 ° C., and at the end of the reaction, the metal is collected at the bottom of the crucible, and a supernatant slag.
L'analyse du chrome métallique obtenu montre qu'en choisissant délibérémment de rester en deça des proportions usuelles, avec pour conséquence de ne pas atteindre le rendement extractif optimal, la teneur en aluminium résiduel dans le chrome métallique descend à des niveaux très bas inférieurs à 0,01 % (100 ppm). Cette analyse montre également que la teneur en inclusions non métalliques monte très vite pour atteindre des taux élevés de 0,40 à 0,80 %, voire même plus, mais que ces inclusions non métalliques sont en quasi-totalité composées d'oxyde de chrome non réduit (Cr203) avec très peu d'Al2O3.The analysis of the metallic chromium obtained shows that by deliberately choosing to remain below the usual proportions, with the consequence of not achieving the optimum extracting yield, the residual aluminum content in the metallic chromium drops to very low levels below 0.01% (100 ppm). This analysis also shows that the content of non-metallic inclusions rises very quickly to reach high levels of 0.40 to 0.80%, or even more, but that these non-metallic inclusions are almost entirely composed of chromium oxide. not reduced (Cr 2 0 3 ) with very little Al 2 O 3 .
Cette manière de procéder contraste nettement avec la manière classique où l'on recherche toujours, pour des raisons économiques, le rendement maximal en utilisant des quantités d'aluminium plus élevées, tout en restant compatible avec la teneur en aluminium résiduel maximum admissible. Ainsi,si l'on conduit une réaction aluminothermique classique entre de l'oxyde de chrome et de l'aluminium en quantité habituelle, on obtient pour une teneur en aluminium résiduel dans le chrome métallique de 0,1 % maximum (teneur maximum usuellement admise pour les usages aéronautiques) des teneurs en inclusions de 1500 à 2500 ppm en quasi-totalité ou tout au moins en majeure partie, sous forme d'alumine Al2O3.This way of proceeding contrasts sharply with the conventional way where one always seeks, for economic reasons, the maximum yield by using higher amounts of aluminum, while remaining compatible with the maximum admissible residual aluminum content. Thus, if a conventional aluminothermic reaction is carried out between chromium oxide and aluminum in the usual amount, one obtains for a residual aluminum content in metallic chromium of 0.1% maximum (maximum content usually accepted for aeronautical uses) of contents of inclusions from 1500 to 2500 ppm in almost all or at least for the most part, in the form of alumina Al 2 O 3 .
Sans vouloir limiter l'invention à une théorie particulière, on peut cependant tenter d'expliquer le mécanisme du phénomène observé. Contrairement à une opinion admise auparavant, les inclusionsWithout wishing to limit the invention to a particular theory, we can however attempt to explain the mechanism of the phenomenon observed. Contrary to a previously accepted opinion, inclusions
. non métalliques d'alumine Al2O3 présentes dans le chrome métallique pur solidifié normal, ne sont pas constituées par du laitier de réaction (corindon de chrome, c'est-à-dire laitier alumineux de la réduction par l'aluminium) mal décanté et s'étant trouvé piégé lors du passage du métal de l'état liquide à l'état solide. Il s'agit au contraire d'une alumine secondaire formée soit au moment de la solidification, soit même dans le métal à l'état solide peu en dessous de la température du solidus, donc à une température encore très élevée où les phénomènes de diffusion et la réactivité des composants est encore très grande. Cette alumine secondaire serait en fait issue de la réaction, les conditions d'équilibre s'étant déplacées avec la baisse de la température où l'état étant par nature hors d'équilibre, entre de l'oxyde de chrome ou de l'oxygène dissous dans le chrome métal et l'aluminium résiduel excédentaire lui aussi présent dans le chrome métal.. non-metallic alumina Al 2 O 3 present in normal solidified pure metallic chromium, do not consist of reaction slag (chromium corundum, i.e. aluminous slag from reduction by aluminum) poorly decanted and having been trapped during the passage of the metal from the liquid state to the solid state. On the contrary, it is a secondary alumina formed either at the time of solidification, or even in the metal in the solid state slightly below the temperature of the solidus, therefore at a still very high temperature where the diffusion phenomena and the reactivity of the components is still very high. This secondary alumina would in fact result from the reaction, the equilibrium conditions having shifted with the drop in temperature where the state is by nature out of equilibrium, between chromium oxide or oxygen dissolved in chromium metal and excess residual aluminum also present in chromium metal.
Ainsi, dans les réactions aluminothermiques classiques, où les quantités d'aluminium sont plus importantes et se rapprochent de la quantité stoechiométrique de la réaction, l'aluminium résiduel est en quantité suffisamment importante pour pouvoir réduire la totalité de l'oxyde de chrome ou de l'oxygène dissous et il en reste même un excès non utilisé dans le chrome. Les inclusions non métalliques qui restent emprisonnées dans le métal solide sont alors en quasi totalité formées d'alumine A1203.Thus, in conventional aluminothermic reactions, where the amounts of aluminum are greater and approach the stoichiometric amount of the reaction, the residual aluminum is in an amount large enough to be able to reduce all of the chromium oxide or dissolved oxygen and there is even an unused excess in chromium. The non-metallic inclusions which remain trapped in the solid metal are then almost entirely formed of alumina A1 2 0 3 .
Si au contraire on opère, conformément au procédé de l'invention, avec un défaut en aluminium par rapport à la quantité usuelle précédente, l'aluminium résiduel présent est en quantité insuffisante pour pouvoir réduire la totalité de l'oxyde de chrome ou de l'oxygène dissous. Tout ou presque tout l'aluminium présent est oxydé par l'oxygène présent (équilibre de phasesen refroidissement lent) et l'excès d'oxyde de chrome ou d'oxygène dissous non réduit précipite sous forme d'inclusions non métalliques Cr203. Il y a alors d'autant moins d'inclusions alumineuses A1203 et d'autant plus de Cr2O3 que la réduction a été conduite avec un défaut d'aluminium de plus en plus marqué (réaction déséquilibrée par défaut).If, on the contrary, the operation is carried out, in accordance with the process of the invention, with an aluminum defect with respect to the previous usual quantity, the residual aluminum present is in insufficient quantity to be able to reduce all of the chromium oxide or of the dissolved oxygen. All or almost all aluminum present is oxidized by the oxygen present (phase equilibrium in slow cooling) and the excess of chromium oxide or unreduced dissolved oxygen precipitates in the form of non-metallic inclusions Cr 2 0 3 . There are then all the less aluminous inclusions A1 2 0 3 and all the more Cr 2 O 3 as the reduction has been carried out with an increasingly marked aluminum defect (unbalanced reaction by default).
La réaction aluminothermique déséquilibrée de l'étape a) donne bien évidemment un rendement un peu moins bon que dans les procédés aluminothermiques classiques .The unbalanced aluminothermic reaction of step a) obviously gives a slightly less good yield than in conventional aluminothermic processes.
Avec le procédé de l'invention, le chrome élémentaire se trouve néanmoins réduit et le produit final obtenu est un chrome métallique de pureté élevée, identique au chrome métallique aluminothermique normal de bonne qualité, sauf qu'il contient une très forte teneur en oxygène (2000 à 3000 ppm ou davantage), mais sous forme quasi exclusive d'inclusions non métalliques Cr2O3 (0,40 à 0,80 % ou davantage) avec présence de très peu d'inclusions alumineuses A1203 (100 à 400 ppm correspondant à 50 à 200 ppm d'oxygène lié à de l'aluminium).With the process of the invention, the elemental chromium is nevertheless reduced and the final product obtained is a metallic chromium of high purity, identical to normal aluminothermic metallic chromium of good quality, except that it contains a very high oxygen content ( 2000 to 3000 ppm or more), but in the almost exclusive form of non-metallic Cr 2 O 3 inclusions (0.40 to 0.80% or more) with the presence of very few aluminous inclusions A1 2 0 3 (100 to 400 ppm corresponding to 50 to 200 ppm of oxygen bound to aluminum).
On obtient par conséquent un chrome métallique avec des inclusions non métalliques constituées principalement par des inclusions de Cr2O3 faciles à éliminer et secondairement par des inclusions d'alumine, plus difficiles à éliminer, mais en faible quantité.Metallic chromium is therefore obtained with non-metallic inclusions mainly constituted by Cr 2 O 3 inclusions which are easy to remove and secondarily by alumina inclusions, which are more difficult to remove, but in small quantities.
Le chrome métallique provenant de l'étape a) est broyé dans un broyeur à choc constitué avantageusement par un broyeur à haute énergie du type à marteaux (marteaux mobiles/contre marteaux fixes) jusqu'à obtention d'une poudre fine passant entièrement à travers un tamis de 200 µ d'ouverture de maille. La haute énergie d'impact du broyeur provoque l'éclatement des grains qui libère, au moins en bonne partie, les inclusions non métalliques Al203 et Cr203 contenues dans le métal, les inclusions Cr203 semblant préférentiellement libérées.The metallic chromium from step a) is ground in an impact mill advantageously constituted by a high energy mill of the hammer type (mobile hammers / counter hammers) until a fine powder is obtained which passes entirely through a sieve with 200 µ mesh opening. The high impact energy of the grinder causes the grains to burst, which releases, at least in large part, the non-metallic inclusions Al 2 0 3 and Cr 2 0 3 contained in the metal, the inclusions Cr 2 0 3 appearing preferentially released. .
Dans le présent exemple, le broyage est un broyage épurant qui produit une ventilation, c'est-à-dire un certain débit d'air de balayage. Cette ventilation peut être produite directement par le broyeur lui-même ou indirectement par un dispositif annexe, tel une soufflerie. Cet air de balayage permet de ventiler le produit en cours de broyage ce qui d'une part évite l'échauffement du produit, et donc éventuellement son oxydation et sa nitruration par l'air ambiant, et d'autre part entraîne les fractions les plus fines et les plus légères dans le courant d'air de balayage, c'est-à-dire de préférence les inclusions non métalliques libérées, dont la densité est moindre.In the present example, the grinding is a purifying grinding which produces ventilation, that is to say a certain flow of purge air. This ventilation can be produced directly by the crusher itself or indirectly by an additional device, such as a blower. This sweeping air makes it possible to ventilate the product during grinding, which on the one hand prevents the product from overheating, and therefore possibly its oxidation and nitriding by ambient air, and on the other hand causes the most fractions. fine and lighter in the sweeping air stream, that is to say preferably the non-metallic inclusions released, the density of which is lower.
Le débit d'air peut être réglé volontairement pour accentuer, si on le désire, l'effet épurateur. De même, cet effet épurateur peut être complété par l'élimination par tamisage ou tout autre séparation sélective des particules les plus fines du produit broyé où se retrouvent concentrées la quasi totalité des inclusions non métalliques libérées par le broyage.The air flow can be adjusted voluntarily to accentuate, if desired, the purifying effect. Likewise, this purifying effect can be supplemented by elimination by sieving or any other selective separation of the finest particles from the ground product in which almost all of the non-metallic inclusions released by grinding are found concentrated.
La poudre de chrome épurée ainsi obtenue est ensuite mélangée intimement avec un réducteur et un agglomérant. Ce dernier est avantageusement constitué par un mélange de bakélite et de furfuraldéhyde. Le furfuraldéhyde a pour but de faciliter l'agglomération à froid, la bakélite dissoute dans le furfuraldéhyde formant colle à froid, ainsi que la polymérisation ultérieure de la bakélite à chaud. Bien entendu, on peut utiliser d'autres agglomérants thermodurcissables et d'autres solvants.The purified chromium powder thus obtained is then intimately mixed with a reducing agent and a binder. The latter is advantageously constituted by a mixture of bakelite and furfuraldehyde. Furfuraldehyde aims to facilitate agglomeration when cold, the bakelite dissolved in the furfuraldehyde forming cold glue, as well as the subsequent polymerization of the hot bakelite. Of course, other thermosetting agglomerants and other solvents can be used.
Le réducteur, quant à lui, est avantageusement constitué par du noir de carbone venant en complément du carbone de la bakélite. Les quantités respectives de ces produits sont variables mais sont globalement ajustées, avec un léger excès, à la teneur résiduelle en oxygène du produit broyé. A titre d'exemple, le mélange réducteur/agglomérant peut être constitué de 0,1 % de bakélite, 0,3 % de furfuraldéhyde et de 0,05 à 0,2 % de noir de carbone,ces pourcentages étant rapportés au poids du produit broyé.The reducer, for its part, is advantageously constituted by carbon black which complements the carbon of the bakelite. The respective amounts of these products are variable but are generally adjusted, with a slight excess, to the residual oxygen content of the ground product. For example, the reducing / binder mixture may consist of 0.1% bakelite, 0.3% of furfuraldehyde and 0.05 to 0.2% of carbon black, these percentages being based on the weight of the crushed product.
Le mélange obtenu est mis en forme de boulets ou de pastilles au moyen d'une presse à compacter classique, telle qu'une presse à bouleter à roues tangentes ou une presse à pastiller. Après aggloméra- _tion, le mélange est étuvé à la température adéquate (200 à 230°C environ)pour éliminer le furfuraldéhyde volatil et polymériser la bakélite qui forme liant et donne de la tenue aux boulets ou aux pastilles.The mixture obtained is shaped into balls or pellets by means of a conventional compacting press, such as a ball press with tangential wheels or a tableting press. After agglomeration, the mixture is baked at the appropriate temperature (200 to 230 ° C approximately) to remove the volatile furfuraldehyde and polymerize the bakelite which forms a binder and gives resistance to the balls or pellets.
Il faut cependant remarquer que la température d'étuvage doit être limitée au minimum mécessaire afin d'éviter toute oxydation du produit.It should however be noted that the oven temperature must be limited to the minimum necessary in order to avoid any oxidation of the product.
Les boulets ou pastilles obtenus à l'étape précédente sont alors soumis à un traitement réducteur sous vide à 1100°-1400°C sous vide poussé de l'ordre de 10-4 mm de mercure.The balls or pellets obtained in the previous step are then subjected to a reducing treatment under vacuum at 1100 ° -1400 ° C under high vacuum of the order of 10 -4 mm of mercury.
Au début du cycle de chauffage sous vide, la bakélite se décompose vers 600°C en laissant un squelette carboné qui s'ajoute au noir de carbone introduit comme réducteur dans le mélange. Une fois arrivé à la température de traitement, ce carbone réagit sur l'oxygène du Cr203 restant dans le produit mais pratiquement pas sur l'oxygène de l'alumine Al2O3 car pour réduire l'alumine il faudrait opérer à une température plus élevée et atteindre des vides plus poussés.At the start of the vacuum heating cycle, the bakelite decomposes at around 600 ° C, leaving a carbon skeleton which is added to the carbon black introduced as a reducing agent in the mixture. Once arrived at the processing temperature, this carbon reacts on the oxygen of the Cr203 remaining in the product but practically not on the oxygen of the alumina Al 2 O 3 because to reduce the alumina it would be necessary to operate at a higher temperature. high and reach deeper voids.
A cet égard, il convient de noter que, déjà à des températures de 1200 à 1300°C sous des vides de 10-4 mm de mercure, le chrome se sublime et une partie non négligeable se vaporise. Ceci explique qu'il n'est économiquement pas possible de pousser plus loin la réduction de l'alumine résiduelle et justifie l'élaboration "déséquilibrée" de l'étape a) afin de limiter l'alumine résiduelle à sonplus strict minimum.In this regard, it should be noted that, already at temperatures of 1200 to 1300 ° C under voids of 10-4 mm of mercury, the chromium sublimes and a non-negligible part vaporizes. This explains why it is not economically possible to push further the reduction of residual alumina and justifies the "unbalanced" development of step a) in order to limit the residual alumina to its strictest minimum.
On ramène le vide dans le four de traitement à 10 mm de mercure par balayage contrôlé par un gaz non oxydant ou réducteur, tel que l'hydrogène, qui a pour particularité de n'être pratiquement pas soluble dans le chrome solide.The vacuum is reduced in the treatment oven to 10 mm of mercury by sweeping controlled by a non-oxidizing or reducing gas, such as hydrogen, which has the particularity of being practically not soluble in solid chromium.
Du fait des vides relativement faibles et des températures relativement basses imposées par la sublimation du chrome, le traitement peut demander plusieurs heures pour atteindre une réaction quasiment complète.Due to the relatively low voids and relatively low temperatures imposed by chromium sublimation, processing can take several hours to achieve an almost complete reaction.
Une fois la réaction terminée et après refroidissement en atmosphère neutre, on obtient un produit contenant au plus 300 à 400 ppm d'oxygène total sous forme de 200 à 300 ppm d'alumine environ contenant 100 à 150 ppm d'oxygène et environ 500 ppm an maximum d'oxyde de chrome non réduit contenant environ 150 ppm d'oxygène. Il s'agit par conséquent d'un chrome de pureté élevée qui permet d'élaborer des super- alliages utilisables en particulier dans la fabrication des parties nobles des turbo-moteurs aéronautiques.Once the reaction is complete and after cooling in a neutral atmosphere, a product is obtained containing at most 300 to 400 ppm of total oxygen in the form of 200 to 300 ppm of alumina approximately containing 100 to 150 ppm of oxygen and about 500 ppm maximum of unreduced chromium oxide containing about 150 ppm of oxygen. It is therefore a chromium of high purity which makes it possible to develop superalloys which can be used in particular in the manufacture of the noble parts of aeronautical turbo-engines.
Il faut observer que l'utilisation d'un produit de départ classique sans déséquilibre au niveau de l'étape a)conduirait obligatoirement, dans la mesure où l'on désire abaisser la teneur en oxygène au niveau requis de 300 ppm environ, à un traitement permettant la réduction d'Al2O3 par le carbone qui, outre les inconvénients précédents, amènerait une remontée de la teneur en aluminium résiduel du produit fini à des niveaux non acceptables par les utilisateurs élaborant les super-alliages.It should be noted that the use of a conventional starting product without imbalance in step a) would necessarily lead, insofar as it is desired to lower the oxygen content to the required level of about 300 ppm, treatment allowing the reduction of Al 2 O 3 by carbon which, in addition to the preceding drawbacks, would bring a rise in the residual aluminum content of the finished product to levels not acceptable by the users preparing the superalloys.
Bien entendu, l'invention n'est.pas limitée au mode de réalisation préféré décrit ci-dessus et on peut envisager d'autres variantes de réalisation sans sortir du cadre de l'invention. Ainsi,l'étape a) peut être conduite autrement que par aluminothermie, par exemple par silicothermie ou bien par réduction au four électrique, pour obtenir un métal ou alliage comprenant des inclusions non métalliques oxydées du métal de base.Of course, the invention is not limited to the preferred embodiment described above and one can envisage other alternative embodiments without departing from the scope of the invention. Thus, step a) can be carried out other than by aluminothermy, for example by silicothermal or else by reduction in an electric furnace, to obtain a metal or alloy comprising oxidized non-metallic inclusions of the base metal.
Pour la silicothermie on peut citer, à titre d'exemples non limitatifs, la fabrication de ferro-chrome ou de chrome métal par réduction avec du silicium métal ou du silico-chrome, ainsi que la fabrication de ferro- tungstène ou de ferro-molybdène par réduction avec un ; ferro-silicium à haute teneur ou du silicium métal.By way of non-limiting examples, the manufacture of ferro-chromium or chromium metal by reduction with silicon metal or silico-chromium, as well as the manufacture of ferro-tungsten or ferro-molybdenum, by way of non-limiting examples. by reduction with one; high-grade ferro-silicon or metal silicon.
Pour la réduction au four électrique, on peut citer, à titre d'exemple non limitatif, la fabrication de ferro-vanadium au four électrique, suivie d'une alumino-thermie.For reduction in an electric oven, mention may be made, by way of nonlimiting example, of the manufacture of ferro-vanadium in an electric oven, followed by an alumino-thermy.
Claims (15)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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AT83401671T ATE24205T1 (en) | 1982-08-20 | 1983-08-17 | PROCESSES FOR THE PRODUCTION OF HIGH PURITY METALS AND ALLOYS. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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FR8214386A FR2531978B1 (en) | 1982-08-20 | 1982-08-20 | PROCESS FOR THE MANUFACTURE OF HIGH PURITY METALS OR ALLOYS |
FR8214386 | 1982-08-20 |
Publications (2)
Publication Number | Publication Date |
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EP0102892A1 true EP0102892A1 (en) | 1984-03-14 |
EP0102892B1 EP0102892B1 (en) | 1986-12-10 |
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Family Applications (1)
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EP83401671A Expired EP0102892B1 (en) | 1982-08-20 | 1983-08-17 | Process for manufacturing high purity metals and alloys |
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US (1) | US4504310B1 (en) |
EP (1) | EP0102892B1 (en) |
JP (1) | JPS5956540A (en) |
AT (1) | ATE24205T1 (en) |
DE (1) | DE3368288D1 (en) |
FR (1) | FR2531978B1 (en) |
ZA (1) | ZA835957B (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2608478A1 (en) * | 1986-12-22 | 1988-06-24 | Delachaux Sa | PROCESS FOR PRODUCING CHROME-ALUMINUM BALLS FOR ADDING CHROMIUM IN FUSION ALUMINUM BATHS |
EP0426375A1 (en) * | 1989-11-01 | 1991-05-08 | JAPAN METALS & CHEMICALS CO., LTD. | Method for producing high-purity metallic chromium |
GB2255349A (en) * | 1991-04-15 | 1992-11-04 | Tosoh Corp | Process for producing chromium metal |
EP0582006A1 (en) * | 1992-08-03 | 1994-02-09 | JAPAN METALS & CHEMICALS CO., LTD. | Method for producing high-purity metallic chromium |
FR2835000A1 (en) * | 2002-01-21 | 2003-07-25 | Delachaux Sa | PROCESS FOR MANUFACTURING METAL ELEMENTS USING A CRUCIBLE |
FR2834999A1 (en) * | 2002-01-21 | 2003-07-25 | Delachaux Sa | PROCESS FOR MANUFACTURING HIGH PURITY METAL ELEMENTS |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4610720A (en) * | 1984-05-16 | 1986-09-09 | The United States Of America As Represented By The Department Of Energy | Method for preparing high purity vanadium |
JPS63195233A (en) * | 1987-02-10 | 1988-08-12 | Tosoh Corp | Deoxidizing method for trace amount of oxygen |
JPS63199832A (en) * | 1987-02-13 | 1988-08-18 | Tosoh Corp | Manufacture of high-purity metallic chromium |
JPS63199833A (en) * | 1987-02-13 | 1988-08-18 | Tosoh Corp | Manufacture of high-purity metallic chromium |
JPS63282217A (en) * | 1987-05-13 | 1988-11-18 | Japan Metals & Chem Co Ltd | Manufacture of high-purity metal chromium |
US5013357A (en) * | 1989-10-26 | 1991-05-07 | Westinghouse Electric Corp. | Direct production of niobium titanium alloy during niobium reduction |
US5866067A (en) * | 1997-03-24 | 1999-02-02 | Sony Corporation And Materials Research Corporation | High purity chromium metal by casting with controlled oxygen content |
EP1102651B1 (en) * | 1998-08-06 | 2004-10-06 | Eramet Marietta Inc. | Purification process for chromium |
JP3338701B2 (en) * | 2000-03-07 | 2002-10-28 | 日本鋼管株式会社 | Method for producing chromium-containing metal |
CN1311943C (en) * | 2002-06-13 | 2007-04-25 | 财团法人生产技术研究奖励会 | Method for producing metal powder and formed product of raw material for metal |
US8840833B1 (en) * | 2010-11-30 | 2014-09-23 | Bloom Energy Corporation | Iron coated chromium powder and SOFC IC made therefrom |
CN114790518A (en) * | 2022-05-05 | 2022-07-26 | 兰州理工大学 | Preparation method of metal vanadium |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1019752A (en) * | 1949-06-24 | 1953-01-26 | Electric Furnace Prod Co | Process of reduction of chromic oxides by carbon |
US4148628A (en) * | 1977-02-18 | 1979-04-10 | Toyo Soda Manufacturing Co., Ltd. | Process of producing metallic chromium |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2332415A (en) * | 1940-08-15 | 1943-10-19 | Marvin J Udy | Chromium recovery |
US2839379A (en) * | 1955-08-19 | 1958-06-17 | Union Carbide Corp | Metal aggregate |
JPS537369A (en) * | 1976-07-09 | 1978-01-23 | Seiko Instr & Electronics Ltd | Electronic watch |
JPS5372718A (en) * | 1976-12-10 | 1978-06-28 | Showa Denko Kk | Manufacture of ferrochromium |
-
1982
- 1982-08-20 FR FR8214386A patent/FR2531978B1/en not_active Expired
-
1983
- 1983-08-05 US US90/002180A patent/US4504310B1/en not_active Expired - Lifetime
- 1983-08-12 ZA ZA835957A patent/ZA835957B/en unknown
- 1983-08-17 EP EP83401671A patent/EP0102892B1/en not_active Expired
- 1983-08-17 DE DE8383401671T patent/DE3368288D1/en not_active Expired
- 1983-08-17 AT AT83401671T patent/ATE24205T1/en not_active IP Right Cessation
- 1983-08-19 JP JP58152367A patent/JPS5956540A/en active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1019752A (en) * | 1949-06-24 | 1953-01-26 | Electric Furnace Prod Co | Process of reduction of chromic oxides by carbon |
US4148628A (en) * | 1977-02-18 | 1979-04-10 | Toyo Soda Manufacturing Co., Ltd. | Process of producing metallic chromium |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2608478A1 (en) * | 1986-12-22 | 1988-06-24 | Delachaux Sa | PROCESS FOR PRODUCING CHROME-ALUMINUM BALLS FOR ADDING CHROMIUM IN FUSION ALUMINUM BATHS |
EP0275774A2 (en) * | 1986-12-22 | 1988-07-27 | Delachaux S.A. | Process for preparing chromium-aluminium agglomerates for adding chromium to a melt of aluminium |
EP0275774A3 (en) * | 1986-12-22 | 1988-08-03 | Delachaux S.A. | Process for preparing chromium-aluminium agglomerates for adding chromium to a melt of aluminium |
EP0426375A1 (en) * | 1989-11-01 | 1991-05-08 | JAPAN METALS & CHEMICALS CO., LTD. | Method for producing high-purity metallic chromium |
GB2255349A (en) * | 1991-04-15 | 1992-11-04 | Tosoh Corp | Process for producing chromium metal |
EP0582006A1 (en) * | 1992-08-03 | 1994-02-09 | JAPAN METALS & CHEMICALS CO., LTD. | Method for producing high-purity metallic chromium |
FR2835000A1 (en) * | 2002-01-21 | 2003-07-25 | Delachaux Sa | PROCESS FOR MANUFACTURING METAL ELEMENTS USING A CRUCIBLE |
FR2834999A1 (en) * | 2002-01-21 | 2003-07-25 | Delachaux Sa | PROCESS FOR MANUFACTURING HIGH PURITY METAL ELEMENTS |
WO2003062480A1 (en) * | 2002-01-21 | 2003-07-31 | Delachaux S.A. | Reductive method for production of metallic elements such as chrome using a crucible with a perforated wall |
WO2003062479A1 (en) * | 2002-01-21 | 2003-07-31 | Delachaux S.A. | Method for production of metallic elements of high purity such as chromes |
US7361205B2 (en) | 2002-01-21 | 2008-04-22 | Delachaux S.A. | Method for production of metallic elements of high purity such as chromes |
CN100383267C (en) * | 2002-01-21 | 2008-04-23 | 登莱秀公司 | Reductive method for production of metallic elements such as chrome using a crucible with a perforated wall |
US7513930B2 (en) | 2002-01-21 | 2009-04-07 | Delachaux S.A. | Reductive method for production of metallic elements such as chrome using a crucible with a perforated wall |
Also Published As
Publication number | Publication date |
---|---|
FR2531978A1 (en) | 1984-02-24 |
FR2531978B1 (en) | 1985-07-12 |
US4504310B1 (en) | 1994-03-15 |
ZA835957B (en) | 1984-04-25 |
ATE24205T1 (en) | 1986-12-15 |
JPS5956540A (en) | 1984-04-02 |
US4504310A (en) | 1985-03-12 |
DE3368288D1 (en) | 1987-01-22 |
JPH0261531B2 (en) | 1990-12-20 |
EP0102892B1 (en) | 1986-12-10 |
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