EP0100287A1 - Amorphous or microcrystalline alloys based on aluminium - Google Patents
Amorphous or microcrystalline alloys based on aluminium Download PDFInfo
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- EP0100287A1 EP0100287A1 EP83420113A EP83420113A EP0100287A1 EP 0100287 A1 EP0100287 A1 EP 0100287A1 EP 83420113 A EP83420113 A EP 83420113A EP 83420113 A EP83420113 A EP 83420113A EP 0100287 A1 EP0100287 A1 EP 0100287A1
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- Prior art keywords
- alloys
- amorphous
- essentially amorphous
- microcrystallized
- alloy
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 35
- 239000000956 alloy Substances 0.000 title claims abstract description 35
- 229910052782 aluminium Inorganic materials 0.000 title description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title 1
- 239000004411 aluminium Substances 0.000 title 1
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 6
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 6
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- 229910052751 metal Inorganic materials 0.000 claims abstract description 5
- 239000002184 metal Substances 0.000 claims abstract description 5
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 4
- 229910052802 copper Inorganic materials 0.000 claims abstract description 4
- 239000012535 impurity Substances 0.000 claims abstract description 4
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 4
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 4
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 4
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 3
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 3
- 150000002739 metals Chemical class 0.000 claims description 4
- 238000005266 casting Methods 0.000 claims 2
- 229910052727 yttrium Inorganic materials 0.000 claims 1
- 239000000203 mixture Substances 0.000 abstract description 3
- 229910052750 molybdenum Inorganic materials 0.000 abstract description 3
- 229910052721 tungsten Inorganic materials 0.000 abstract description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 229910000808 amorphous metal alloy Inorganic materials 0.000 description 4
- 238000002425 crystallisation Methods 0.000 description 4
- 230000008025 crystallization Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000001493 electron microscopy Methods 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 235000019589 hardness Nutrition 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052763 palladium Inorganic materials 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910018459 Al—Ge Inorganic materials 0.000 description 1
- 229910018507 Al—Ni Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 229910052733 gallium Inorganic materials 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C45/00—Amorphous alloys
- C22C45/08—Amorphous alloys with aluminium as the major constituent
Definitions
- the invention relates to essentially amorphous or microcrystalline Al-based alloys.
- alloys in the amorphous state obtained by rapid cooling at a speed generally greater than 10 5 ° C / sec from a disordered state (liquid or vapor).
- Particularly known are the alloys of type T i X j in which T represents one or more transition metals (in particular iron) and X one or more metalloides (or not) such as B, P, Si, C, Al with i ⁇ 50 at%.
- T represents one or more transition metals (in particular iron)
- X one or more metalloides (or not)
- B, P, Si, C, Al with i ⁇ 50 at% In these alloys, Al intervenes as a minor element whose content in general of the order of 10 at%, does not exceed 35 at%.
- amorphous alloys have been developed by A. INOUE et al (Journal of Mat. Science, 16, 1981, p. 1895) but relate to the systems (Fe, Co, Ni) -Al-B which may contain up to 60 at. Al and in general from 15 to 45-50 at. % B.
- the invention therefore relates to alloys based on boron-free Al, which can be obtained in an essentially amorphous or microcrystalline state, by cooling at speeds of the order of 10 to 10 6 K / sec, which 'It is possible to obtain industrially, from a liquid or gaseous state.
- essentially amorphous alloy is meant a state in which the atoms have no order at long distance, characterized by broad X-ray diffraction spectra and diffusa in the absence of lines characteristic of the crystallized state; the corresponding electron microscopy examinations show that more than 80% by volume of the alloy is amorphous.
- microcrystalline state means an alloy in which 20% of the volume or more is in the crystallized state and the average size of the crystallites of which is less than 1000 nm, preferably less than 100 nm (1000 A). This average dimension is evaluated from the width at mid-height of the line of the dense planes of the alloy, or by electron microscopy (in black field). In this state, the diffraction lines at small angles ( ⁇ ⁇ '22 °) have disappeared.
- Microcrystalline alloys are generally obtained either directly from the liquid state, or by crystallization heat treatment above the starting crystallization temperature Tc of the amorphous alloy (this was determined below by enthal analysis - differential spike with a heating rate of 10 ° C / min.).
- the alloys according to the invention have the following chemical composition defined by the formula: in which: M representing one or more metals from the group Mn, Ni, Cu, Zr, Ti, V, Cr, Fe, Co with M 'representing the Mo and / or the W with X representing one or more elements of the group Ca, Li, Mg, Ge, Si, Zn with Y representing the inevitable processing impurities such as 0, N, C, H, He, Ga, etc., the overall content of which does not exceed 3 atom%, in particular for the lightest elements, but which are required to preferably below 1 at. %.
- the content of additives is limited above due to metallurgical considerations (melting temperature, viscosity, surface tension, oxidability, etc.), but also economic (price, availability). Mo and W are limited to 15% because they significantly increase the density and the melting point of the alloy.
- Essentially amorphous or microcrystalline alloys have been obtained with alloys containing between 6 and 25% at Cu with a value of 15 ⁇ b ⁇ 40 at%, the impurities being kept below 1 at%.
- compositions include individually, or in combination, from 0.5 to 5 at% Mo, 0.5 to 9 at% Si, 5 to 25 at% V and 7 to 25 at% Ni.
- Figure 1a represents the diagram of the amorphous alloy ,
- Figure 1b being an enlarged part of the diagram of Figure 1a.
- FIG. 1c represents the diffraction diagram of the corresponding crystallized alloy.
- Figure 2 shows the evolution of the hardness of this amorphous alloy according to the invention as a function of time, when maintained at 150 ° C.
- the alloy Al 80 Cu 10 Ni 8 Mo 2 obtained above and which has a crystallization temperature Tc 156 ° C and a density of 3.7 g / cm 3 , a ratio of the electrical resistance to the state amorphous with respect to the resistance in the crystallized state at 300 ° K of 7, was subjected to maintenance at 150 ° C;
- FIG. 2 gives the evolution of the Vickers micro-hardness under 10 g, during this test: it reaches 500 HV approx. after 10 h.
- the Al 72 Cu 15 V 10 Mo 1 Si 2 alloy prepared as in Example 1 has a crystallization temperature of 360 ° C. and a density of 3.6 g / cm 3 . Its micro-hardness reaches 750 HV after 1/2 hour at 400 ° C and 840.HV after 1/2 hour at 450 ° C.
- the very high hardnesses are favorable for obtaining powders of very high chemical homogeneity, by grinding.
- the alloys according to the invention can be obtained according to known techniques in the form of wires, strips, ribbons, sheets or powders in the amorphous state and / or in the microcrystallized state. They can be used either directly or as reinforcing elements of other materials or they can also be used for obtaining surface coatings improving for example the resistance to corrosion or wear.
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- Organic Chemistry (AREA)
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- Laminated Bodies (AREA)
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- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
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Abstract
Description
L'invention se rapporte aux alliages à base d'Al essentiellement amorphes ou microcristallins.The invention relates to essentially amorphous or microcrystalline Al-based alloys.
Il existe de nombreux alliages à l'état amorphe, obtenus par refroidissement rapide à une vitesse en général supérieure à 105°C/sec à partir d'un état désordonné (liquide ou vapeur). On connaît, en particulier, les alliages de type TiXj dans lesquels T représente un ou plusieurs métaux de transition (en particulier le fer) et X un ou plusieurs mé- talloides (ou non) tels que B, P, Si, C, Al avec i ≥ 50 at %. Dans ces alliages, l'Al intervient comme élément mineur dont la teneur en général de l'ordre de 10 at %, ne dépasse pas 35 at %.There are many alloys in the amorphous state, obtained by rapid cooling at a speed generally greater than 10 5 ° C / sec from a disordered state (liquid or vapor). Particularly known are the alloys of type T i X j in which T represents one or more transition metals (in particular iron) and X one or more metalloides (or not) such as B, P, Si, C, Al with i ≥ 50 at%. In these alloys, Al intervenes as a minor element whose content in general of the order of 10 at%, does not exceed 35 at%.
Pour les alliages à base d'Al (contenant plus de 50 % at Al), la littérature technique rapporte des tentatives d'obtention d'alliages amorphes qui ont été effectuées sur des alliages binaires contenant du Bi, du Cd, du Cu, du Ge, de l'In, du Mg, du Ni, du Pd, du Si, du Cr, de l'Ag ou du Zn, mais seuls quatre d'entre eux Al-Ge, Al-Pd, Al-Ni, Al-Cr se sont révélés très localement amorphes (régions visibles en microscopie électronique) et ce, pour de très grandes vitesses de refroidissement de l'ordre de 109 à 1010K/sec, très difficiles à atteindre industriellement - voir T.R. ANANTHARAMAN et al. -"Rapidiy Quenched Metals III" - volume 1-Editor B. Cantor, The Metals Society, Londres (1978) p. 126 et P.FURRER et WARLIMONT, Mat. Science and Eng., 28 (1977) p. 127.For alloys based on Al (containing more than 50% at Al), the technical literature reports attempts to obtain amorphous alloys which have been carried out on binary alloys containing Bi, Cd, Cu, Ge, In, Mg, Ni, Pd, Si, Cr, Ag or Zn, but only four of them Al-Ge, Al-Pd, Al-Ni, Al -Cr have proven to be very locally amorphous (regions visible in electron microscopy) and this, for very high cooling rates of the order of 10 9 to 10 10 K / sec, very difficult to achieve industrially - see TR ANANTHARAMAN et al . - "Rapidiy Quenched Metals III" - volume 1-Editor B. Cantor, The Metals Society, London (1978) p. 126 and P.FURRER and WARLIMONT, Mat. Science and Eng., 28 (1977) p. 127.
Pour les alliages ternaires, des alliages amorphes ont été élaborés par A. INOUE et al (Journal of Mat. Science, 16, 1981, p. 1895) mais sont relatifs aux systèmes (Fe, Co, Ni) -Al-B pouvant contenir jusqu'à 60 at. Al et en général de 15 à 45-50 at. % B.For ternary alloys, amorphous alloys have been developed by A. INOUE et al (Journal of Mat. Science, 16, 1981, p. 1895) but relate to the systems (Fe, Co, Ni) -Al-B which may contain up to 60 at. Al and in general from 15 to 45-50 at. % B.
L'invention concerne donc des alliages à base d'Al exempt de bore,que l'on peut obtenir à l'état essentiellement amorphe ou microcristallin, par refroidissement à des vitesses de l'ordre de 10 à 106 K/sec, qu'il est possible d'obtenir industriellement, à partir d'un état liquide ou gazeux.The invention therefore relates to alloys based on boron-free Al, which can be obtained in an essentially amorphous or microcrystalline state, by cooling at speeds of the order of 10 to 10 6 K / sec, which 'It is possible to obtain industrially, from a liquid or gaseous state.
Par alliage essentiellement amorphe, on entend un état dans lequel les atomes ne présentent aucun ordre à grande distance, caractérisé par des spectres de diffraction des rayons X larges et diffusa en l'absence de raies caractéristiques de l'état cristallisé; les examens en microscopie électronique correspondants montrent que plus de 80 % en volume de l'alliage est amorphe.By essentially amorphous alloy is meant a state in which the atoms have no order at long distance, characterized by broad X-ray diffraction spectra and diffusa in the absence of lines characteristic of the crystallized state; the corresponding electron microscopy examinations show that more than 80% by volume of the alloy is amorphous.
Par état microcristallin, on entend un alliage dans lequel 20 % du volume ou plus est à l'état cristallisa et dont la dimension moyenne des cristallites est inférieure à 1 000 nm, de préférence inférieure à 100 nm (1 000 A). Cette dimension moyenne est évaluée à partir de la largeur à mi-hauteur de la raie des plans denses de l'alliage, ou par microscopie électronique (en champ noir). Dans cet état, les raies de diffraction aux petits angles (θ <'22°) ont disparu.The term “microcrystalline state” means an alloy in which 20% of the volume or more is in the crystallized state and the average size of the crystallites of which is less than 1000 nm, preferably less than 100 nm (1000 A). This average dimension is evaluated from the width at mid-height of the line of the dense planes of the alloy, or by electron microscopy (in black field). In this state, the diffraction lines at small angles (θ <'22 °) have disappeared.
Les alliages microcristallins sont obtenus généralement soit directement à partir de l'état liquide, soit par traitement thermique de cristallisation au-dessus de la température de cristallisation commençante Tc de l'alliage amorphe (celle-ci a été déterminée ci-après par analyse enthal- pique différentielle avec une vitesse de chauffage de 10°C/min.).Microcrystalline alloys are generally obtained either directly from the liquid state, or by crystallization heat treatment above the starting crystallization temperature Tc of the amorphous alloy (this was determined below by enthal analysis - differential spike with a heating rate of 10 ° C / min.).
Les alliages selon l'invention possèdent la composition chimique suivante définie par la formule :
La teneur en éléments d'addition est limitée supérieurement en raison de considérations métallurgiques (température de fusion, viscosité, tension superficielle, oxydabilité, etc...), mais aussi économiques (prix, disponibilité). Le Mo et le W sont limités à 15 % car ils augmentent notablement la densité et le point de fusion de l'alliage.The content of additives is limited above due to metallurgical considerations (melting temperature, viscosity, surface tension, oxidability, etc.), but also economic (price, availability). Mo and W are limited to 15% because they significantly increase the density and the melting point of the alloy.
I1 a été constaté qu'il est plus facile d'obtenir un alliage essentiellement amorphe ou microcristallin si la teneur en Al est limitée supérieurement à 85 at %.It has been found that it is easier to obtain an essentially amorphous or microcrystalline alloy if the Al content is limited above 85 at%.
Des alliages essentiellement amorphes ou microcristallins ont été obtenus avec des alliages contenaht entre 6 et 25 % at de Cu avec une valeur de 15 ≤ b ≤ 40 at %, les impuretés étant maintenues inférieures à 1 at %.Essentially amorphous or microcrystalline alloys have been obtained with alloys containing between 6 and 25% at Cu with a value of 15 ≤ b ≤ 40 at%, the impurities being kept below 1 at%.
Des compositions préférentielles comprennent individuellement, ou en combinaison, de 0,5 à 5 at % Mo, 0,5 à 9 at % Si, 5 à 25 at % V et 7 à 25 at % Ni.Preferred compositions include individually, or in combination, from 0.5 to 5 at% Mo, 0.5 to 9 at% Si, 5 to 25 at% V and 7 to 25 at% Ni.
Les figures et exemples illustrent l'invention.The figures and examples illustrate the invention.
La figure 1 montre le diagramme des rayons X d'un alliage Al80Cu10Ni8 MO2, obtenu à l'aide de radiation monomochromatique du Co (λ = 0,17889nm) La figure 1a représente le diagramme de l'alliage amorphe, la figure 1b étant une partie agrandie du diagramme de la figure 1a.Figure 1 shows the X-ray diagram of an Al 80 Cu 10 Ni 8 MO 2 alloy, obtained using monomochromatic radiation of Co (λ = 0.17889nm) Figure 1a represents the diagram of the amorphous alloy , Figure 1b being an enlarged part of the diagram of Figure 1a.
La figure 1c représente le diagramme de diffraction de l'alliage cristallisé correspondant.FIG. 1c represents the diffraction diagram of the corresponding crystallized alloy.
La figure 2 représente l'évolution de la dureté de cet alliage amorphe conforme à l'invention en fonction du temps, lors d'un maintien à 150°C.Figure 2 shows the evolution of the hardness of this amorphous alloy according to the invention as a function of time, when maintained at 150 ° C.
Divers alliages ont été coulés sous hélium à 30 kPa (0,3 bar) à partir d'un bain liquide, maintenu dans un creuset en quartz, sur l'extérieur d'un tambour en acier doux de 25 cm de diamètre, tournant à 3 000 t/mn (V ≃ 40 m/sec) de manière à obtenir un ruban de 2 mm x 20 µm environ de section transversale.Various alloys were cast under helium at 30 kPa (0.3 bar) from of a liquid bath, held in a quartz crucible, on the outside of a 25 cm diameter mild steel drum, rotating at 3000 rpm (V ≃ 40 m / sec) so as to obtain a tape of approximately 2 mm x 20 µm cross section.
Les résultats de micro-dureté et/ou d'examen aux rayons X obtenus sur ceux-ci sont reportés au tableau I ci-après.The results of micro-hardness and / or X-ray examination obtained thereon are given in Table I below.
L'alliage Al80Cu10Ni8Mo2 obtenu ci-dessus et qui présente une température de cristallisation Tc = 156° C et une masse volumique de 3,7 g/cm3, un rapport de la résistance électrique à l'état amorphe par rapport à la résistance à l'état cristallisé à 300°K de 7, a été soumis à un maintien à 150° C; la figure 2 donne l'évolution de la micro-dureté Vickers sous 10 g, lors de cet essai : celle-ci atteint 500 HV env. au bout de 10 h.The alloy Al 80 Cu 10 Ni 8 Mo 2 obtained above and which has a crystallization temperature Tc = 156 ° C and a density of 3.7 g / cm 3 , a ratio of the electrical resistance to the state amorphous with respect to the resistance in the crystallized state at 300 ° K of 7, was subjected to maintenance at 150 ° C; FIG. 2 gives the evolution of the Vickers micro-hardness under 10 g, during this test: it reaches 500 HV approx. after 10 h.
L'alliage Al72Cu15V10Mo1Si2 préparé comme dans l'exemple 1 présente une température de cristallisation de 360° C et une masse volumique de 3,6 g/cm3. Sa micro-dureté atteint 750 HV après maintien de 1/2 h à 400°C et 840.HV après maintien de 1/2 h à 450° C.The Al 72 Cu 15 V 10 Mo 1 Si 2 alloy prepared as in Example 1 has a crystallization temperature of 360 ° C. and a density of 3.6 g / cm 3 . Its micro-hardness reaches 750 HV after 1/2 hour at 400 ° C and 840.HV after 1/2 hour at 450 ° C.
Les duretés très élevées sont favorables à l'obtention de poudres d'une très grande homogénéité chimique, par broyage.The very high hardnesses are favorable for obtaining powders of very high chemical homogeneity, by grinding.
Les alliages suivant l'invention peuvent être obtenus suivant des techniques connues sous forme de fils, bandes, rubans, feuilles ou poudres à l'état amorphe et/ou à l'état micro-cristallisé. Ils peuvent être utilisés soit directement, soit comme éléments de renforcement d'autres matériaux ou encore ils peuvent également être utilisés pour l'obtention de revêtements superficiels améliorant par exemple la résistance à la corrosion ou à l'usure.The alloys according to the invention can be obtained according to known techniques in the form of wires, strips, ribbons, sheets or powders in the amorphous state and / or in the microcrystallized state. They can be used either directly or as reinforcing elements of other materials or they can also be used for obtaining surface coatings improving for example the resistance to corrosion or wear.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT83420113T ATE23565T1 (en) | 1982-07-06 | 1983-07-04 | AMORPHOUS OR MICROCRYSTALLINE ALUMINUM-BASED ALLOYS. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8212404A FR2529909B1 (en) | 1982-07-06 | 1982-07-06 | AMORPHOUS OR MICROCRYSTALLINE ALLOYS BASED ON ALUMINUM |
FR8212404 | 1982-07-06 |
Publications (2)
Publication Number | Publication Date |
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EP0100287A1 true EP0100287A1 (en) | 1984-02-08 |
EP0100287B1 EP0100287B1 (en) | 1986-11-12 |
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Application Number | Title | Priority Date | Filing Date |
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EP83420113A Expired EP0100287B1 (en) | 1982-07-06 | 1983-07-04 | Amorphous or microcrystalline alloys based on aluminium |
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US (2) | US4595429A (en) |
EP (1) | EP0100287B1 (en) |
JP (1) | JPS5920442A (en) |
AT (1) | ATE23565T1 (en) |
CA (1) | CA1214665A (en) |
DE (1) | DE3367622D1 (en) |
DK (1) | DK163883C (en) |
FR (1) | FR2529909B1 (en) |
IL (1) | IL69123A (en) |
NO (1) | NO160862C (en) |
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FR2555610A1 (en) * | 1983-11-29 | 1985-05-31 | Cegedur | ALUMINUM ALLOYS HAVING HIGH HOT STABILITY |
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FR2577941A1 (en) * | 1985-02-27 | 1986-08-29 | Pechiney | AMORPHO ALLOY ALLOYS CONTAINING ESSENTIALLY NI AND / OR FE AND IS AND PROCESS FOR OBTAINING THE SAME |
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WO1988009825A1 (en) * | 1987-06-05 | 1988-12-15 | Allied-Signal Inc. | Rapidly solidified aluminum iron silicon vanadium alloys |
EP0303100A1 (en) * | 1987-08-12 | 1989-02-15 | Ykk Corporation | High strength, heat resistant aluminum alloys and method of preparing wrought article therefrom |
EP0317710A1 (en) * | 1987-11-10 | 1989-05-31 | Yoshida Kogyo K.K. | High strength, heat resistant aluminum alloys |
US4878967A (en) * | 1985-10-02 | 1989-11-07 | Allied-Signal Inc. | Rapidly solidified aluminum based, silicon containing alloys for elevated temperature applications |
FR2635117A1 (en) * | 1988-08-04 | 1990-02-09 | Centre Nat Rech Scient | COATING MATERIALS FOR ALUMINUM ALLOYS |
EP0354391A1 (en) * | 1988-07-22 | 1990-02-14 | Yoshida Kogyo K.K. | Corrosion-resistant and heatresistant aluminum-based alloy thin film and process for producing the same |
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EP0445684A1 (en) * | 1990-03-06 | 1991-09-11 | Ykk Corporation | High strength, heat resistant aluminum-based alloys |
EP0458029A1 (en) * | 1990-03-22 | 1991-11-27 | Ykk Corporation | Corrosion resistant aluminum-based alloy |
WO1992001078A1 (en) * | 1990-07-06 | 1992-01-23 | Allied-Signal Inc. | Aluminum iron silicon based, elevated temperature, aluminum alloys |
AU620155B2 (en) * | 1988-10-15 | 1992-02-13 | Koji Hashimoto | Amorphous aluminum alloys |
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- 1983-07-04 JP JP58121470A patent/JPS5920442A/en active Granted
- 1983-07-04 DE DE8383420113T patent/DE3367622D1/en not_active Expired
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Also Published As
Publication number | Publication date |
---|---|
DK163883C (en) | 1992-09-14 |
CA1214665A (en) | 1986-12-02 |
NO160862B (en) | 1989-02-27 |
JPH0116899B2 (en) | 1989-03-28 |
DK163883B (en) | 1992-04-13 |
EP0100287B1 (en) | 1986-11-12 |
NO832458L (en) | 1984-01-09 |
ATE23565T1 (en) | 1986-11-15 |
US4710246A (en) | 1987-12-01 |
NO160862C (en) | 1989-06-07 |
FR2529909A1 (en) | 1984-01-13 |
DK310083D0 (en) | 1983-07-05 |
DE3367622D1 (en) | 1987-01-02 |
IL69123A0 (en) | 1983-10-31 |
US4595429A (en) | 1986-06-17 |
JPS5920442A (en) | 1984-02-02 |
DK310083A (en) | 1984-01-07 |
IL69123A (en) | 1987-03-31 |
FR2529909B1 (en) | 1986-12-12 |
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