EP0784100B1 - Iron-cobalt alloy, manufacturing process for strips made from iron-cobalt alloy and product obtained - Google Patents
Iron-cobalt alloy, manufacturing process for strips made from iron-cobalt alloy and product obtained Download PDFInfo
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- EP0784100B1 EP0784100B1 EP97400024A EP97400024A EP0784100B1 EP 0784100 B1 EP0784100 B1 EP 0784100B1 EP 97400024 A EP97400024 A EP 97400024A EP 97400024 A EP97400024 A EP 97400024A EP 0784100 B1 EP0784100 B1 EP 0784100B1
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- alloy
- strip
- iron
- heat treatment
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- 229910000531 Co alloy Inorganic materials 0.000 title claims abstract description 10
- QVYYOKWPCQYKEY-UHFFFAOYSA-N [Fe].[Co] Chemical compound [Fe].[Co] QVYYOKWPCQYKEY-UHFFFAOYSA-N 0.000 title claims abstract description 10
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 9
- 239000012535 impurity Substances 0.000 claims abstract description 11
- 229910045601 alloy Inorganic materials 0.000 claims description 41
- 239000000956 alloy Substances 0.000 claims description 41
- 238000010438 heat treatment Methods 0.000 claims description 22
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 17
- 229910052710 silicon Inorganic materials 0.000 claims description 14
- 239000010703 silicon Substances 0.000 claims description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 10
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- 239000000126 substance Substances 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 229910052757 nitrogen Inorganic materials 0.000 claims description 6
- 229910052760 oxygen Inorganic materials 0.000 claims description 6
- 229910052698 phosphorus Inorganic materials 0.000 claims description 6
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 5
- 229910052732 germanium Inorganic materials 0.000 claims description 5
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 229910052717 sulfur Inorganic materials 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 239000011651 chromium Substances 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 239000011733 molybdenum Substances 0.000 claims description 4
- 239000001301 oxygen Substances 0.000 claims description 4
- 239000011574 phosphorus Substances 0.000 claims description 4
- 239000002893 slag Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- VTHJTEIRLNZDEV-UHFFFAOYSA-L magnesium dihydroxide Chemical compound [OH-].[OH-].[Mg+2] VTHJTEIRLNZDEV-UHFFFAOYSA-L 0.000 claims description 3
- 239000000347 magnesium hydroxide Substances 0.000 claims description 3
- 235000012254 magnesium hydroxide Nutrition 0.000 claims description 3
- CRGZYKWWYNQGEC-UHFFFAOYSA-N magnesium;methanolate Chemical compound [Mg+2].[O-]C.[O-]C CRGZYKWWYNQGEC-UHFFFAOYSA-N 0.000 claims description 3
- 238000007711 solidification Methods 0.000 claims description 3
- 230000008023 solidification Effects 0.000 claims description 3
- 239000002966 varnish Substances 0.000 claims description 3
- 238000005272 metallurgy Methods 0.000 claims description 2
- 238000003723 Smelting Methods 0.000 claims 3
- 238000000034 method Methods 0.000 claims 3
- 239000013067 intermediate product Substances 0.000 claims 2
- 239000005864 Sulphur Substances 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 10
- 229910052782 aluminium Inorganic materials 0.000 description 10
- 239000010941 cobalt Substances 0.000 description 9
- 229910017052 cobalt Inorganic materials 0.000 description 9
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 9
- 239000011265 semifinished product Substances 0.000 description 5
- 239000004411 aluminium Substances 0.000 description 4
- 230000002349 favourable effect Effects 0.000 description 4
- 230000005415 magnetization Effects 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 238000000137 annealing Methods 0.000 description 3
- 238000005097 cold rolling Methods 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 239000011593 sulfur Substances 0.000 description 3
- 229910017061 Fe Co Inorganic materials 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 229910052500 inorganic mineral Inorganic materials 0.000 description 2
- 239000011707 mineral Substances 0.000 description 2
- 235000010755 mineral Nutrition 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- LDFJQWGCLSAONS-UHFFFAOYSA-N [Si][Co][Fe] Chemical compound [Si][Co][Fe] LDFJQWGCLSAONS-UHFFFAOYSA-N 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 239000004205 dimethyl polysiloxane Substances 0.000 description 1
- 238000004870 electrical engineering Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
Definitions
- the present invention relates to an Iron-Cobalt alloy for the manufacture of magnetic circuits for electrotechnical machines.
- electrotechnical machines such as electric motors, transformers or relays have built-in magnetic circuits of stacks of parts cut from alloy strips, the magnetic properties are suitable. These properties should be all the more better than machines with high specific energy, which is the case, for example, for machines on board vehicles such as planes or high speed trains. Indeed, for these applications it is necessary to minimize the weight of the equipment, which involves an increase in specific energy, i.e. power per unit massive.
- the magnetic circuits of machines with high specific energy are often made of Iron-Cobalt alloy whose chemical composition includes, by weight, about 50% cobalt and 2% vanadium, the balance being iron and impurities.
- Iron-Cobalt alloy whose chemical composition includes, by weight, about 50% cobalt and 2% vanadium, the balance being iron and impurities.
- these alloys have several disadvantages because that they all have an ⁇ / ⁇ phase transformation which limits very notably the possibilities of action on the magnetic properties by heat treatment.
- these alloys generally have a resistivity electric too weak and are too expensive.
- the object of the present invention is to remedy these drawbacks by proposing an alloy of the Iron-Cobalt type having magnetic properties close to those of known alloys, but with a higher cobalt content low, so as to be less expensive than existing alloys, and which can be cold rolled.
- the impurities resulting from the preparation can be, in particular, elements such as chromium, titanium, germanium, vanadium and molybdenum, and elements like carbon, oxygen, nitrogen, sulfur and phosphorus.
- the chemical composition checks one or more more than one of the following relationships: 10% ⁇ Co ⁇ 35%, Si ⁇ 2.5% or Al ⁇ 1.5% or Si + Al ⁇ 1.5%.
- the coating with an insulating layer can be obtained by covering the strip, or, after the heat treatment, of at least one layer of varnish mineral or organic, i.e., before the heat treatment, at least one layer of magnesium methylate.
- the coating with an insulating layer can be obtained by applying to the band a milk of magnesia, before the heat treatment.
- the invention relates to a strip of an alloy according to the invention, coated with at least one electrically insulating layer, preferably having a cubic texture (100) [001] or a texture (110) [001], as well as its use for manufacturing a magnetic circuit of a machine electrical engineering.
- the inventors have found in a new way that by adding aluminum to an Iron-Cobalt alloy possibly containing silicon, we significantly increased the resistivity of the alloy without dropping too much the saturation magnetization, and, that by choosing the content of this element taking into account the possible silicon content, we could remove the ⁇ / ⁇ phase transformation while obtaining a material sufficiently ductile to be suitable for cold rolling.
- This provides a strip whose magnetic properties can be improved by a heat treatment and by obtaining a favorable texture.
- the impurities resulting from processing are, in particular, elements such as chromium, titanium, germanium, vanadium and molybdenum which can be tolerated provided the sum of their contents remains less than 0.5%.
- Impurities are also elements such as carbon, oxygen, nitrogen, sulfur and phosphorus whose contents must be as low as possible and preferably such that: C ⁇ 0.03%, O ⁇ 0.005 %, N ⁇ 0.003%, S ⁇ 0.003%, P ⁇ 0.003%.
- the alloy can be produced using vacuum oven or arc furnace followed by a vacuum bag treatment then cast as a semi-finished product.
- the alloy can be remelted under vacuum or under electroconductive slag.
- the alloy is cast in the form of a reflow electrode which is remelted under vacuum or under electroconductive slag to obtain the semi-finished product.
- the semi-finished product is placed still hot in a reheating oven to be brought to rolling temperature, then hot rolled to obtain a hot strip of thickness between approximately 1 mm and approximately 6 mm.
- the hot strip is then pickled and, if necessary, stretched by heating between 200 ° C and 600 ° C and finally, cold rolled (or warm when the strip is stretched) in several passes with, possibly annealing intermediate between 700 ° C and 1100 ° C, to obtain a cold strip generally between 0.05 mm and 0.5 mm thick.
- the succession of cold rolling and annealing intermediaries to obtain a cubic texture (100) [001] or a texture (110) [001] very favorable for obtaining good magnetic properties.
- intermediate annealing should preferably be made under an atmosphere of pure and dry hydrogen.
- the cold strip is then subjected to a heat treatment by heating and maintaining temperature between 850 ° C and 1200 ° C for a time between 1 hour and 10 hours and coated with at least one insulating layer electrically.
- the heat treatment which is done under atmosphere pure and dry hydrogen makes it possible to enlarge the grain which improves the magnetic properties.
- At least one electrically insulating layer may consist of a mineral or organic varnish deposited after heat treatment, or magnesium methylate deposited before heat treatment.
- At least one electrically insulating layer can be obtained by applying to the strip, before the heat treatment, a milk of magnesia. During the heat treatment, the silicon located on the surface of the tape reacts with magnesia to form an insulating glass.
- the strips thus obtained can be cut to obtain parts which, after stacking, form magnetic circuits for transformers, electric motors, relays or any other electrotechnical machine.
- alloys C to D were manufactured (chemical composition by weight in%): alloy Fe Co Yes Al VS NOT O S VS ball 15 - 1.54 0.016 0.0008 0.001 0.0005 D ball 15 - 2.4 0.027 0.0005 0.001 0.0005 E ball 15 - 3.1 0.011 0.0005 0.001 0.0005 F ball 15 0.98 1.55 0.011 0.0012 0.0013 0.0005
- alloys were produced in a vacuum oven, hot rolled then cold rolled to obtain strips of 0.2 mm thick. The strips were subjected to a heat treatment under hydrogen.
- the heat treatment conditions and the magnetic characteristics obtained were: alloy ⁇ ° C t (hours) ⁇ ( ⁇ . ⁇ .cm) B to 600Oe (G) Hc (Oe) VS 900 4 35 22100 0.5 VS 1050 4 35 22100 0.53 D 900 4 38 21200 0.53 D 1150 4 38 21200 0.4 E 900 4 40 21000 0.43 E 1150 4 40 21000 0.4 F 900 4 39.5 21500 0.4 F 1000 4 39.5 21500 0.32
- alloys according to the invention After heat treatment at 900 ° C and 1000 ° C, their characteristics were: alloy ⁇ ° C t (hours) ⁇ ( ⁇ . ⁇ .cm) B to 600Oe (G) Hc (Oe) AT 900 4 30 22500 0.58 AT 1000 4 30 22500 0.71 It can be seen that the alloys according to the invention have a higher resistivity, a lower coercive field and a magnetization comparable to that of alloy A.
- the iron-cobalt alloys according to the prior art contain more than 15% of cobalt and the characteristics of the bands in these alloys are typically: Co% ⁇ ( ⁇ . ⁇ .cm) B to 600 Oe (G) Hc (Oe) 50 40 22500 1 25 22 22500 1.5
- the alloys according to the invention have a resistivity comparable electric power, a significantly weaker coercive field and a fairly close magnetization despite a very appreciably higher cobalt content low. These results show some of the advantages of the alloy according to the invention.
Abstract
Description
La présente invention concerne un alliage Fer-Cobalt pour la fabrication de circuits magnétiques pour machines électrotechniques.The present invention relates to an Iron-Cobalt alloy for the manufacture of magnetic circuits for electrotechnical machines.
les machines électrotechniques telles que les moteurs électriques, les transformateurs ou les relais comportent des circuits magnétiques constitués d'empilages de pièces découpées dans des bandes en alliage dont les propriétés magnétiques sont adaptées. Ces propriétés doivent être d'autant meilleures que les machines sont à forte énergie spécifique, ce qui est le cas, par exemple, pour les machines embarquées sur des véhicules tels que des avions ou des trains à grande vitesse. En effet, pour ces applications il est nécessaire de réduire au maximum le poids des équipements, ce qui passe par une augmentation de l'énergie spécifique, c'est à dire de la puissance par unité de masse.electrotechnical machines such as electric motors, transformers or relays have built-in magnetic circuits of stacks of parts cut from alloy strips, the magnetic properties are suitable. These properties should be all the more better than machines with high specific energy, which is the case, for example, for machines on board vehicles such as planes or high speed trains. Indeed, for these applications it is necessary to minimize the weight of the equipment, which involves an increase in specific energy, i.e. power per unit massive.
Les circuits magnétiques des machines à forte énergie spécifique sont souvent fabriqués en alliage Fer-Cobalt dont la composition chimique comprend, en poids, environ 50 % de cobalt et 2% de vanadium, le reste étant du fer et des impuretés. Mais ces alliages ont plusieurs inconvénients parce qu'ils présentent tous une transformation de phase α / γ qui limite très notablement les possibilités d'action sur les propriétés magnétiques par traitement thermique. De plus, ces alliages ont, en général, une résistivité électrique trop faible et sont trop coûteux.The magnetic circuits of machines with high specific energy are often made of Iron-Cobalt alloy whose chemical composition includes, by weight, about 50% cobalt and 2% vanadium, the balance being iron and impurities. But these alloys have several disadvantages because that they all have an α / γ phase transformation which limits very notably the possibilities of action on the magnetic properties by heat treatment. In addition, these alloys generally have a resistivity electric too weak and are too expensive.
Il a été proposé, notamment dans DE - C - 705 516 d'utiliser des alliages fer-cobalt-silicium contenant de 2 % à 18 % de cobalt et de 1 % à 6 % de silicium. Cependant, ces alliages n'apportent pas une solution satisfaisante au problème énoncé ci-dessus. En effet, pour obtenir des propriétés magnétiques satisfaisantes, il est nécessaire que l'alliage contienne plus de 3 % de silicium, il devient alors très fragile et ne peut plus être laminé à froid dans des conditions satisfaisantes, on ne peut donc plus obtenir les faibles épaisseurs souhaitables pour réduire les pertes par courants de Foucault dans les circuits magnétiques.It has been proposed, in particular in DE - C - 705 516 to use alloys iron-cobalt-silicon containing from 2% to 18% of cobalt and from 1% to 6% of silicon. However, these alloys do not provide a satisfactory solution to the problem stated above. Indeed, to obtain magnetic properties satisfactory, it is necessary that the alloy contains more than 3% of silicon, it then becomes very fragile and can no longer be cold rolled in satisfactory conditions, we can no longer obtain the small thicknesses desirable to reduce eddy current losses in circuits magnetic.
Le but de la présente invention est de remédier à ces inconvénients en proposant un alliage du type Fer-Cobalt ayant des propriétés magnétiques proches de celles des alliages connus, mais avec une teneur en cobalt plus faible, de façon à être moins coûteux que les alliages existants, et pouvant être laminé à froid.The object of the present invention is to remedy these drawbacks by proposing an alloy of the Iron-Cobalt type having magnetic properties close to those of known alloys, but with a higher cobalt content low, so as to be less expensive than existing alloys, and which can be cold rolled.
A cet effet, l'invention a pour objet un alliage Fer-Cobalt dont la
composition chimique comprend en poids:
Les impuretés résultant de l'élaboration peuvent être, notamment, des éléments tels que le chrome, le titane, le germanium, le vanadium et le molybdène, et des éléments tels que le carbone, l'oxygène, l'azote, le soufre et le phosphore.The impurities resulting from the preparation can be, in particular, elements such as chromium, titanium, germanium, vanadium and molybdenum, and elements like carbon, oxygen, nitrogen, sulfur and phosphorus.
De préférence, les impuretés résultant de l'élaboration que sont le
carbone, l'oxygène, l'azote, le soufre et le phosphore, ont des teneurs
inférieures aux valeurs suivantes:
De préférence également, la composition chimique vérifie une ou plusieurs des relations suivantes: 10 % ≤ Co ≤ 35 %, Si ≥ 2,5 % ou Al ≥ 1,5 % ou Si + Al ≥ 1,5%.Preferably also, the chemical composition checks one or more more than one of the following relationships: 10% ≤ Co ≤ 35%, Si ≥ 2.5% or Al ≥ 1.5% or Si + Al ≥ 1.5%.
L'invention concerne également un procédé de fabrication d'une bande en un alliage conforme à l'invention selon lequel:
- on élabore l'alliage soit sous vide soit au four à arc suivi d'une opération de métallurgie en poche et, éventuellement, après une première solidification, on le refond sous vide ou sous laitier électroconducteur pour obtenir un demi produit,
- on lamine à chaud le demi-produit pour obtenir une bande à chaud dont l'épaisseur est comprise entre 1 et 6 mm,
- on décape la bande à chaud et on la lamine après l'avoir éventuellement réchauffée entre 200°C et 600°C pour obtenir une bande à froid d'épaisseur comprise entre 0,05 mm et 0,5 mm,
- on effectue un traitement thermique entre 850 °C et 1200 °C pendant 1 à 10 heures et un revêtement par une couche électriquement isolante.
- the alloy is produced either under vacuum or in an arc furnace followed by a ladle metallurgy operation and, possibly, after a first solidification, it is remelted under vacuum or under electroconductive slag to obtain a semi-finished product,
- the semi-finished product is hot rolled to obtain a hot strip whose thickness is between 1 and 6 mm,
- the strip is stripped hot and it is laminated after having optionally reheated it between 200 ° C and 600 ° C to obtain a cold strip of thickness between 0.05 mm and 0.5 mm,
- heat treatment is carried out between 850 ° C and 1200 ° C for 1 to 10 hours and coating with an electrically insulating layer.
Le revêtement par une couche isolante peut être obtenu en recouvrant la bande, soit, après le traitement thermique, d'au moins une couche de vernis minéral ou organique, soit, avant le traitement thermique, d'au moins une couche de méthylate de magnésium.The coating with an insulating layer can be obtained by covering the strip, or, after the heat treatment, of at least one layer of varnish mineral or organic, i.e., before the heat treatment, at least one layer of magnesium methylate.
Lorsque la teneur en silicium de l'alliage est supérieure à 2 %, le revêtement par une couche isolante peut être obtenu en appliquant sur la bande un lait de magnésie, avant le traitement thermique.When the silicon content of the alloy is greater than 2%, the coating with an insulating layer can be obtained by applying to the band a milk of magnesia, before the heat treatment.
L'invention concerne, enfin, une bande en un alliage selon l'invention, revêtue d'au moins une couche électriquement isolante, ayant de préférence une texture cubique (100) [001] ou une texture (110) [001], ainsi que son utilisation pour la fabrication d'un circuit magnétique d'une machine électrotechnique.Finally, the invention relates to a strip of an alloy according to the invention, coated with at least one electrically insulating layer, preferably having a cubic texture (100) [001] or a texture (110) [001], as well as its use for manufacturing a magnetic circuit of a machine electrical engineering.
L'invention va maintenant être décrite de façon plus précise, mais non limitative.The invention will now be described in more detail, but not limiting.
Les inventeurs ont constaté de façon nouvelle qu'en ajoutant de l'aluminium à un alliage Fer-Cobalt contenant éventuellement du silicium, on augmentait sensiblement la résistivité de l'alliage sans trop baisser l'aimantation à saturation, et, qu'en choisissant convenablement la teneur en cet élément en tenant compte de l'éventuelle teneur en silicium, on pouvait faire disparaítre la transformation de phase α/γ tout en obtenant un matériau suffisamment ductile pour être apte au laminage à froid. Cela permet d'obtenir une bande dont les propriétés magnétiques peuvent être améliorées par un traitement thermique et par l'obtention d'une texture favorable.The inventors have found in a new way that by adding aluminum to an Iron-Cobalt alloy possibly containing silicon, we significantly increased the resistivity of the alloy without dropping too much the saturation magnetization, and, that by choosing the content of this element taking into account the possible silicon content, we could remove the α / γ phase transformation while obtaining a material sufficiently ductile to be suitable for cold rolling. This provides a strip whose magnetic properties can be improved by a heat treatment and by obtaining a favorable texture.
Outre le fer et les impuretés résultant de l'élaboration, la composition chimique de l'alliage selon l'invention comprend en poids:
- de 5% à 40% et de préférence de 10% à 35% de cobalt qui est le seul élément connu améliorant l'aimantation à saturation du fer; le cobalt étant un élément très coûteux sa teneur est ajustée, pour chaque application particulière, à la teneur juste nécessaire pour obtenir les caractéristiques magnétiques souhaitées pour l'application;
- de 0,2 % à 5 % d'aluminium et de 0% à 5% de silicium pour réduire l'étendue du domaine d'existence de la phase γ ; l'aluminium présente l'avantage supplémentaire d'augmenter la résistivité électrique et de ne pas détériorer la ductilité à froid ; le silicium qui réduit également le domaine d'existence de la phase γ, présente cependant l'inconvénient de rendre difficile les opérations de laminage à froid ; de préférence, soit la teneur en aluminium est supérieure ou égale à 1,5%, soit la teneur en silicium est supérieure ou égale à 2,5%, soit la somme des teneurs en silicium et aluminium est supérieure ou égale à 1,5%, car au delà de ces valeurs, la phase γ n'existe plus, ce qui permet des traitements thermiques à haute température pour faire grossir le grain et développer une texture favorable, et ainsi, améliorer les propriétés magnétiques;
- from 5% to 40% and preferably from 10% to 35% of cobalt which is the only known element improving the saturation magnetization of iron; cobalt being a very expensive element, its content is adjusted, for each particular application, to the content just necessary to obtain the magnetic characteristics desired for the application;
- from 0.2% to 5% of aluminum and from 0% to 5% of silicon to reduce the extent of the domain of existence of the γ phase; aluminum has the additional advantage of increasing the electrical resistivity and of not deteriorating the ductility when cold; silicon which also reduces the domain of existence of the γ phase, however has the drawback of making cold rolling operations difficult; preferably, either the aluminum content is greater than or equal to 1.5%, or the silicon content is greater than or equal to 2.5%, or the sum of the silicon and aluminum contents is greater than or equal to 1.5 %, because beyond these values, the γ phase no longer exists, which allows heat treatments at high temperature to make the grain coarser and develop a favorable texture, and thus, improve the magnetic properties;
Les impuretés résultant de l'élaboration sont, notamment, des éléments tels que le chrome, le titane, le germanium, le vanadium et le molybdène qui peuvent être tolérées à condition que la somme de leurs teneurs reste inférieure à 0,5%. Les impuretés sont également des éléments tels que le carbone, l'oxygène, l'azote, le soufre et le phosphore dont les teneurs doivent être le plus faible possible et, de préférence, telles que :C ≤ 0,03 %, O ≤ 0,005 %, N ≤ 0,003 %, S ≤ 0,003 %, P ≤ 0,003 %.The impurities resulting from processing are, in particular, elements such as chromium, titanium, germanium, vanadium and molybdenum which can be tolerated provided the sum of their contents remains less than 0.5%. Impurities are also elements such as carbon, oxygen, nitrogen, sulfur and phosphorus whose contents must be as low as possible and preferably such that: C ≤ 0.03%, O ≤ 0.005 %, N ≤ 0.003%, S ≤ 0.003%, P ≤ 0.003%.
Afin d'obtenir un niveau de pureté suffisant, l'alliage peut être élaboré au four sous vide ou au four à arc suivi d'un traitement en poche sous vide puis coulé sous forme d'un demi produit. Avantageusement, l'alliage peut être refondu sous vide ou sous laitier électroconducteur. Dans ce cas, après l'élaboration sous vide ou après l'opération de traitement en poche sous vide, l'alliage est coulé sous forme d'une électrode de refusion qui est refondue sous vide ou sous laitier éléctroconducteur pour obtenir le demi produit.In order to obtain a sufficient level of purity, the alloy can be produced using vacuum oven or arc furnace followed by a vacuum bag treatment then cast as a semi-finished product. Advantageously, the alloy can be remelted under vacuum or under electroconductive slag. In this case, after preparation under vacuum or after the vacuum bag processing operation, the alloy is cast in the form of a reflow electrode which is remelted under vacuum or under electroconductive slag to obtain the semi-finished product.
Le demi produit est enfourné encore chaud dans un four de réchauffage pour être porté à la température de laminage, puis laminé à chaud pour obtenir une bande à chaud d'épaisseur comprise entre environ 1 mm et environ 6 mm. La bande à chaud est alors décapée puis, éventuellement, dégourdie par chauffage entre 200°C et 600°C et enfin, laminée à froid (ou à tiède lorsque la bande est dégourdie) en plusieurs passes avec, éventuellement des recuits intermédiaires entre 700°C et 1100°C, pour obtenir une bande à froid d'épaisseur comprise, en général, entre 0,05 mm et 0,5 mm.The semi-finished product is placed still hot in a reheating oven to be brought to rolling temperature, then hot rolled to obtain a hot strip of thickness between approximately 1 mm and approximately 6 mm. The hot strip is then pickled and, if necessary, stretched by heating between 200 ° C and 600 ° C and finally, cold rolled (or warm when the strip is stretched) in several passes with, possibly annealing intermediate between 700 ° C and 1100 ° C, to obtain a cold strip generally between 0.05 mm and 0.5 mm thick.
Dans certains cas, la succession de laminages à froid et de recuits intermédiaires permet d'obtenir une texture cubique (100) [001] ou une texture (110) [001] très favorables à l'obtention de bonnes propriétés magnétiques. Afin d'éviter l'oxydation de l'aluminium ou de silicium, les recuits intermédiaires doivent, de préférence, être faits sous atmosphère d'hydrogène pur et sec.In some cases, the succession of cold rolling and annealing intermediaries to obtain a cubic texture (100) [001] or a texture (110) [001] very favorable for obtaining good magnetic properties. In order to avoid oxidation of aluminum or silicon, intermediate annealing should preferably be made under an atmosphere of pure and dry hydrogen.
La bande à froid est ensuite soumise à un traitement thermique par chauffage et maintien en température entre 850°C et 1200°C pendant un temps compris entre 1 heure et 10 heures et revêtue d'au moins une couche isolante électriquement. Le traitement thermique qui est fait sous atmosphère d'hydrogène pur et sec permet de faire grossir le grain ce qui améliore les propriétés magnétiques.The cold strip is then subjected to a heat treatment by heating and maintaining temperature between 850 ° C and 1200 ° C for a time between 1 hour and 10 hours and coated with at least one insulating layer electrically. The heat treatment which is done under atmosphere pure and dry hydrogen makes it possible to enlarge the grain which improves the magnetic properties.
Au moins une couche électriquement isolante peut être constituée d'un vernis minéral ou organique déposé après le traitement thermique, ou de méthylate de magnésium déposé avant le traitement thermique. At least one electrically insulating layer may consist of a mineral or organic varnish deposited after heat treatment, or magnesium methylate deposited before heat treatment.
Lorsque la teneur en silicium de l'alliage est suffisante, c'est à dire supérieure à 2%, au moins une couche électriquement isolante peut être obtenue en appliquant sur la bande, avant le traitement thermique, un lait de magnésie. Pendant le traitement thermique, le silicium situé en surface de la bande réagit avec la magnésie pour former un verre isolant.When the silicon content of the alloy is sufficient, i.e. greater than 2%, at least one electrically insulating layer can be obtained by applying to the strip, before the heat treatment, a milk of magnesia. During the heat treatment, the silicon located on the surface of the tape reacts with magnesia to form an insulating glass.
Les bandes ainsi obtenues peuvent être découpées pour obtenir des pièces qui, après empilage, forment des circuits magnétiques pour des transformateurs, des moteurs électriques, des relais ou pour tout autre machine électrotechnique.The strips thus obtained can be cut to obtain parts which, after stacking, form magnetic circuits for transformers, electric motors, relays or any other electrotechnical machine.
Ces bandes ont un champ coercitif faible (Hc < 0,55 Oe ; 1 Oe = 79,577 A/m) et une résistivité électrique élevée (ρ > 33 µ.Ω.cm), ce qui les rend particulièrement aptes à la fabrication de circuits magnétiques pour des machines électrotechniques à forte énergie spécifique destinées notamment à équiper des véhicules tels que des trains à grande vitesse ou des aéronefs.These bands have a weak coercive field (Hc <0.55 Oe; 1 Oe = 79.577 A / m) and a high electrical resistivity (ρ> 33 µ.Ω.cm), which makes them particularly suitable for the manufacture of magnetic circuits for high specific energy electrotechnical machines intended in particular for equip vehicles such as high-speed trains or aircraft.
A titre d'exemple on a fabriqué les alliages C à D (composition chimique
en poids en %):
Tous ces alliages ont été élaborés au four sous vide, laminé à chaud
puis à froid pour obtenir des bandes de 0,2 mm d'épaisseur. Les bandes ont
été soumises à un traitement thermique sous hydrogène. Les conditions de
traitement thermique et les caractéristiques magnétiques obtenues étaient:
A titre de comparaison, on a fabriqué une bandes en alliage Fer-Cobalt
selon l'art antérieur (repéré A) dont la composition chimique était :
Après traitement thermique à 900 °C et 1000 °C, leurs caractéristiques
étaient :
En général, les alliages fer-cobalt selon l'art antérieur contiennent plus
de 15 % de cobalt et les caractéristiques des bandes en ces alliages sont
typiquement :
On constate que les alliages selon l'invention ont une résistivité électrique comparable, un champ coercitif sensiblement plus faible et une aimantation assez voisine malgré une teneur en cobalt très sensiblement plus faible. Ces résultats montrent certains des avantages de l'alliage selon l'invention.It is found that the alloys according to the invention have a resistivity comparable electric power, a significantly weaker coercive field and a fairly close magnetization despite a very appreciably higher cobalt content low. These results show some of the advantages of the alloy according to the invention.
Claims (13)
- Iron-cobalt alloy, characterized in that its chemical composition comprises, by weight:5% ≤ Co ≤ 40%0% ≤ Si ≤ 5%0.2% ≤ Al ≤ 5%0.5% ≤ Si + Al ≤ 5%
- Alloy according to Claim 1, characterized in that the carbon, oxygen, nitrogen, sulphur and phosphorus impurities resulting from smelting have contents less than the following values:C ≤ 0.03%O ≤ 0.005%N ≤ 0.003%S ≤ 0.003%P ≤ 0.003%.
- Alloy according to Claim 1 or Claim 2, characterized in that the chromium, titanium, germanium, vanadium and molybdenum impurities resulting from smelting have contents whose sum is less than 0.5%.
- Alloy according to any one of Claims 1 to 3, characterized in that:
10% ≤ Co ≤ 35% - Alloy according to any one of Claims 1 to 4, characterized in that:
Si ≥ 2.5% - Alloy according to any one of Claims 1 to 4, characterized in that:
Al ≥ 1.5% - Alloy according to any one of Claims 1 to 4, characterized in that:
Si + Al ≥ 1.5% - Process for manufacturing a strip made of an alloy according to any one of Claims 1 to 5, characterized in that:the alloy is smelted either under vacuum or in an arc furnace followed by an in-ladle metallurgy operation and, optionally, after a first solidification, the alloy is remelted under vacuum or under an electrically conductive slag, in order to obtain an intermediate product;the intermediate product is hot-rolled in order to obtain a hot-rolled strip whose thickness is between 1 and 6 mm;the hot-rolled strip is pickled, optionally reheated between 200°C and 600°C and rolled in order to obtain a cold-rolled strip having a thickness of between 0.05 mm and 0.5 mm;a heat treatment between 850°C and 1200°C for 1 to 10 hours is carried out and a coating, with an insulating layer, is applied.
- Process according to Claim 8, characterized in that the coating with an insulating layer is obtained by covering the strip either, after the heat treatment, with at least one layer of inorganic or organic varnish, or, before the heat treatment, with at least one layer of magnesium methoxide.
- Process according to Claim 8, characterized in that, when the silicon content of the alloy is greater than 2%, the coating with an insulating layer is obtained by applying a milk of magnesia to the strip before the heat treatment.
- Strip made of an alloy according to any one of Claims 1 to 7.
- Strip according to Claim 11, characterized in that it has a (100)[001] cubic texture or a (110) [001] texture.
- Strip according to Claim 11 or Claim 12, characterized in that it is coated with at least one electrically insulating layer.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9600232A FR2743572B1 (en) | 1996-01-11 | 1996-01-11 | IRON-COBALT ALLOY, METHOD FOR MANUFACTURING A STRIP OF IRON-COBALT ALLOY AND STRIP OBTAINED |
FR9600232 | 1996-01-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0784100A1 EP0784100A1 (en) | 1997-07-16 |
EP0784100B1 true EP0784100B1 (en) | 2001-03-28 |
Family
ID=9488022
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97400024A Expired - Lifetime EP0784100B1 (en) | 1996-01-11 | 1997-01-08 | Iron-cobalt alloy, manufacturing process for strips made from iron-cobalt alloy and product obtained |
Country Status (6)
Country | Link |
---|---|
US (1) | US5919319A (en) |
EP (1) | EP0784100B1 (en) |
JP (1) | JPH09195010A (en) |
AT (1) | ATE200112T1 (en) |
DE (1) | DE69704381T2 (en) |
FR (1) | FR2743572B1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
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US6855240B2 (en) * | 2000-08-09 | 2005-02-15 | Hitachi Global Storage Technologies Netherlands B.V. | CoFe alloy film and process of making same |
US20080035245A1 (en) * | 2006-08-09 | 2008-02-14 | Luana Emiliana Iorio | Soft magnetic material and systems therewith |
US20100201469A1 (en) * | 2006-08-09 | 2010-08-12 | General Electric Company | Soft magnetic material and systems therewith |
KR101376507B1 (en) | 2012-02-22 | 2014-03-21 | 포항공과대학교 산학협력단 | METHOD OF MANUFACTURING Fe-Co BASED ALLOY SHEET WITH TEXTURE STRUCTURE AND SOFT MAGNETIC STEEL SHEET MANUFACTURED BY THE SAME |
CN105209188B (en) * | 2013-06-07 | 2017-10-13 | Vdm金属有限公司 | The method for preparing metal foil |
JP6388925B2 (en) | 2013-06-07 | 2018-09-12 | ファオデーエム メタルズ ゲゼルシャフト ミット ベシュレンクテル ハフツングVDM Metals GmbH | Metal foil manufacturing method |
DE102014213794A1 (en) | 2014-07-16 | 2016-01-21 | Robert Bosch Gmbh | Soft magnetic alloy composition and method for producing such |
US10454352B1 (en) | 2016-05-02 | 2019-10-22 | Williams International Co., L.L.C. | Method of producing a laminated magnetic core |
EP3957757B1 (en) * | 2020-08-18 | 2023-03-01 | Vacuumschmelze GmbH & Co. KG | Method of producing a cofe alloy strip and a cofe alloy lamination |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE705516C (en) * | 1933-10-13 | 1941-05-02 | Fried Krupp Akt Ges | Manufacture of dynamo and transformer sheets and similar magnetically stressed objects |
US4059462A (en) * | 1974-12-26 | 1977-11-22 | The Foundation: The Research Institute Of Electric And Magnetic Alloys | Niobium-iron rectangular hysteresis magnetic alloy |
JP2615543B2 (en) * | 1985-05-04 | 1997-05-28 | 大同特殊鋼株式会社 | Soft magnetic material |
JPH0689366B2 (en) * | 1986-05-01 | 1994-11-09 | 株式会社神戸製鋼所 | Magnetic powder for electromagnetic clutch |
JPS63233507A (en) * | 1987-03-20 | 1988-09-29 | Kobe Steel Ltd | Magnetic powder for electromagnetic clutch |
JPH0715121B2 (en) * | 1988-08-20 | 1995-02-22 | 川崎製鉄株式会社 | Fe-Co alloy fine powder for injection molding and Fe-Co sintered magnetic material |
JPH04259355A (en) * | 1991-02-14 | 1992-09-14 | Hitachi Metal Precision Ltd | Fe-co series magnetic alloy for casting high in toughness, specific resistance and saturation magnetic flux density |
JPH0633199A (en) * | 1992-07-16 | 1994-02-08 | Hitachi Metal Precision Ltd | Yoke core for printer head |
US5425912A (en) * | 1994-07-07 | 1995-06-20 | Inco Alloys International, Inc. | Low expansion superalloy with improved toughness |
-
1996
- 1996-01-11 FR FR9600232A patent/FR2743572B1/en not_active Expired - Fee Related
-
1997
- 1997-01-08 AT AT97400024T patent/ATE200112T1/en not_active IP Right Cessation
- 1997-01-08 DE DE69704381T patent/DE69704381T2/en not_active Expired - Fee Related
- 1997-01-08 EP EP97400024A patent/EP0784100B1/en not_active Expired - Lifetime
- 1997-01-10 JP JP9014518A patent/JPH09195010A/en not_active Withdrawn
- 1997-01-13 US US08/782,948 patent/US5919319A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE69704381T2 (en) | 2001-10-11 |
FR2743572A1 (en) | 1997-07-18 |
DE69704381D1 (en) | 2001-05-03 |
JPH09195010A (en) | 1997-07-29 |
ATE200112T1 (en) | 2001-04-15 |
EP0784100A1 (en) | 1997-07-16 |
FR2743572B1 (en) | 1998-02-13 |
US5919319A (en) | 1999-07-06 |
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