EP0356287A1 - Cladding materials for metal alloys and for metals - Google Patents

Cladding materials for metal alloys and for metals Download PDF

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Publication number
EP0356287A1
EP0356287A1 EP89402187A EP89402187A EP0356287A1 EP 0356287 A1 EP0356287 A1 EP 0356287A1 EP 89402187 A EP89402187 A EP 89402187A EP 89402187 A EP89402187 A EP 89402187A EP 0356287 A1 EP0356287 A1 EP 0356287A1
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Prior art keywords
coating
materials
phase
substrate according
substrate
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German (de)
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EP0356287B1 (en
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Jean-Marie Dubois
Pierre Weinland
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Centre National de la Recherche Scientifique CNRS
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Centre National de la Recherche Scientifique CNRS
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/08Amorphous alloys with aluminium as the major constituent

Definitions

  • the present invention relates to coating materials for metallic substrates, the substrates coated with these materials and the applications of these coated substrates.
  • Copper cooking utensils are also known, which traditionally have an internal coating of tin. This coating, although particularly suitable for food contact, has the disadvantage of being rapidly deteriorated due to its ductility.
  • European patent 100287 describes a family of amorphous or microcrystalline alloys having improved hardness, usable as reinforcing elements of other materials or for obtaining surface coatings improving the resistance to corrosion or wear.
  • a large number of the alloys described in this patent have a major drawback since, during their use, they are subjected to a temperature above 200 ° C. Indeed, they are not stable at temperature, and during a heat treatment, in particular the treatment to which they are subjected during deposition on a substrate, they change their structure: return to the microcrystalline state when it acts of essentially amorphous alloys, grain magnification for essentially microcrystalline alloys which initially have a grain size less than one micron. This change in crystalline or morphological structure induces a change in the physical characteristics of the material which essentially affects its density. This results in the appearance of micro-cracks, hence a brittleness, which adversely affects the mechanical stability deposits.
  • the object of the present invention is to provide a coating material which makes it possible to retain the good properties of certain metallic substrates commonly used while eliminating the disadvantages which they present on the surface.
  • the materials constituting these coatings have an improved hardness, a lower coefficient of friction, good stability at temperatures above 300 ° C. necessary in particular for cooking utensils.
  • quasi-crystalline phase is meant a phase or a metallic compound whose study by radiation diffraction reveals the existence of rotation symmetries normally incompatible with translation symmetry, that is to say the existence of axes of order 5, 8, 10 or 12.
  • phases or compounds mention may be made of the icosahedral quasicrystalline phases which are solid metal phases which diffract the electrons like a simple crystal, but which have a group of symmetry m35 with respect to a point which is incompatible with network translations. (Cf. D. Shechtman, I. Blech, D. Gratian, JW Cahn, Metallic Phase with Long-Range Orientational Order and No Translational Symmetry, Physical Review Letters, Vol. 53, No.
  • decagonal quasi-crystalline phases which are solid metallic phases which diffract the electrons like a simple crystal, but which have a group of symmetry 10 / m or 10 / mmm with respect to a point, a long order distance and one-dimensional translational symmetry.
  • Cf. L. Bendersky Quasicrystal with One Dimensional Translational Symmetry and a Tenfold Rotation Axis, Physical Review Letters, Vol. 55, N ° 14, 1985 page 1461-1463).
  • the stable quasi-crystalline phases of the coating materials according to the invention grow in a similar fashion to the usual crystals. They therefore behave as defined compounds and have transformation points located at higher temperatures than those of the eutectics of common binary aluminum alloys, Al / Al2Cu (547 ° C), Al / Si (577 ° C) , Al / Al3Fe (655 ° C), for example. This results in a stability which exists beyond or up to the vicinity of these eutectic points.
  • the materials according to the invention are obtained by conventional methods.
  • Coating materials according to the invention are particularly useful for commercial aluminum alloys, and in particular for so-called “food” alloys or so-called “foundry” alloys and for copper.
  • the material according to the invention is deposited on the substrate by spraying droplets of the material.
  • a powder torch can be used, such as the "Thermospray gun type 5P" sold by Metco Inc.
  • the material according to the invention in mass form is ground and sieved to obtain a powder whose grains have a dimension between approximately 0.02 mm and 0.2 mm, preferably less than 0.074 mm.
  • the material according to the invention will be deposited by a product in the vapor phase, for example by sputtering, or by using a plasma torch supplied with powder as indicated above.
  • - shot blasting for example using steel microbeads having a diameter of 0.5 to 1 mm.
  • - polishing for example using metallography paper, provided that the closed porosity of the coating is negligible.
  • a supersonic jet torch can be used which accelerates the powder of material according to the invention at speeds between Mach 6 and Mach 14.
  • the coatings obtained were characterized by their thickness (E.), their open porosity rate (PO), their adhesion index (IE), their coefficient of friction (CF), their hardness (D.) and their rate of quasi-crystalline phase (QC).
  • the open porosity (P.O.) rate was estimated from scanning microscopy images obtained using a SEM 505 scanning microscope from Philips.
  • adhesion indexes were assigned after fracture during a resilience test as follows: - index A when there is no visible detachment at the substrate / deposition interface; grip is considered perfect. - index B when at most 3 cracks are visible at the substrate / deposition interface, in optical metallography, with a magnification of 50. - index E when a detachment is visible at the substrate / deposition interface.
  • the coefficient of friction C.F. was evaluated during a scratch resistance test by a Vickers diamond indenter.
  • the hardness (Hv30) was determined using the WOLPERT durometer V-Testor 2, under load of 30 grams.
  • the existence of quasi-crystalline phases is confirmed by X-ray diffraction.
  • the thermal stability of the materials according to the invention was studied by differential scanning calorimetry using a SETARAM calorimeter.
  • a raw casting material obtained in the previous example was ground in a carbide steel roller mill.
  • the resulting powder was sieved and the fraction having a diameter of less than 0.074 mm was retained.
  • the hydrogen flow rate was 47 l / min and the oxygen flow rate was 28 l / min.
  • the part was maintained under an atmosphere of N2 at 5% of H2.
  • the substrate temperature remained below 200 ° C for the duration of the projection.
  • the coatings were polished with 1200 grit metallography paper.
  • the characteristics of the coatings R1 to R7 obtained from the materials M1 to M5 are collated in Table 2 below. TABLE 2 Rev. Mast. E. ( ⁇ m) PO IA CF D. (Hv30) QC (% by mass) R1 M1 30 ⁇ 10 10% B 0.5 560 > 90% R2 M1 50 ⁇ 10 35% AT 0.5 410 > 90% R3 M1 50 ⁇ 10 40% AT 0.5 370 > 90% R4 M2 40 ⁇ 10 30 % AT 500 > 80% R5 M3 40 ⁇ 10 30 % AT 480 > 80% R6 M4 50 ⁇ 10 40% B 510 > 60% R7 M5 30 ⁇ 10 30 % AT 0.55 510 > 60%
  • the residual phases are too small in proportion to be identified.
  • the residual phase contains a mixture of Al2Cu, Al7Cu2Fe, Al6Fe, Al and Si.
  • the residual phase contains a mixture of Al2Cu and Al3V.
  • the quasicrystalline structure of the materials of the invention induces great thermal stability of the coatings obtained.
  • the temperature Tx determined is that of the substrate, taking into account the small relative thickness of the coating.
  • the coating has a stability at least equal to that of the support.
  • the quasi-crystalline phase of the material according to the invention does not undergo any transformation: neither grain enlargement, nor change in grain structure and the possible amorphous phase is transformed into phase crystalline.
  • the coating will therefore be thermally stable whatever the process for obtaining the material according to the invention.
  • the proportion of quasi-crystalline phase corresponds to the ratio of the area of the peaks attributed to the quasi-crystalline phase to the total area visible peaks.
  • the slope of the curve gives a coefficient of friction of 1.6 for the substrate alone and 0.5 for R3.
  • the slope is modified: the indentor having crossed the coating layer, penetrated into the substrate and the slope of the curve from this point is equivalent to that from the curve in fig. 7.
  • the total length of a stripe corresponds to the 60 N plotted on the abscissa on the curve in fig. 8.
  • the indentor crosses the coating only on the final third of the scratch. From the point where the indentor has passed through the coating, a white border characteristic of the substrate material displaced by the indentor is formed on the image. The coating is damaged, but not torn off by plates.
  • Fig. 11 represents the scanning microscopy image of the coating R1 (the white portion of the horizontal line at the bottom of the image represents 1 mm) and Fig. 12 that of the coating R2 (the white portion of the horizontal line at the bottom 0.1 mm).
  • the area A occupied by the deposited particles P.O. 1- (A / S) was measured on a reference surface of area S of such an image.
  • Example 3 The materials of Example 3, crude casting, were deposited on a substrate identical to that of Example 2, using the method of Example 2. The coated substrates obtained were characterized and the results are collated in Table 5.
  • Table 5 Rev. Mast. E. ( ⁇ m) PO IA CF D. (Hv30) QC (% in vol) R8 M6 45 ⁇ 10 40% E 380 0% R9 M7 40 ⁇ 10 E 0.95 400 0% R10 M8 40 ⁇ 10 E 370 ⁇ 20%
  • the coating R8 essentially consists of a mixture of Al2Cu (t-lines), cubic aluminum with centered faces (line A) and of indeterminate amorphous or poorly crystallized compound ( lines a).
  • the I lines of the icosahedral phase and the D lines of the decagonal phase do not exist.
  • the coating R9 comprises, in addition to the low proportion of quasi-crystalline phase, a mixture of Al2Cu and Al3V.
  • Example 2 Five substrates were prepared by brushing with a wire brush and / or by sandblasting. Then, a powder of the material M1, obtained according to the method of Example 2, was applied to each of the substrates with a supersonic jet. The powder was thus accelerated in a high pressure nitrogen jet, up to a speed of Mach 10; it melted by passing through a reducing flame and it was deposited on the substrates to give the coated substrates R11 to R15.
  • FIGS. 13a, 13b, 13c, 13d and 13 e represent the Hv30 microduretures obtained respectively with the coated substrates R11, R12, R13, R14 and R15.
  • the microhardness was measured on the edge of the coated substrates, along a straight line perpendicular to the surface of the substrate. It should be noted that certain coated substrates have a surface hardness which exceeds 500 kg / mm2.
  • the alloys M9 and M10 of Example 1 were prepared and reduced to powder according to the method of Example 2. These alloys were applied to a AU5GT substrate according to the procedure of Example 3.
  • the coated substrates obtained R16 and R17 were used to evaluate the resistance to oxidation of coatings and therefore their performance when used in the field of food cooking. To this end, the coated substrates were first mechanically polished to obtain an optical polish, then subjected to air in treatments isotherms at 300 ° C and 400 ° C with a duration of 30 hours and 144 hours. By comparison, an uncoated substrate plate and an 18/8 stainless steel plate were subjected to the same treatments.
  • the optical micrographs of the test pieces obtained, without polishing after the heat treatment, show that the quasicrystalline deposits M9 and M10 show no visible degradation of their surface, while the substrate AU5GT and the stainless steel show a very marked deterioration in their area. This deterioration is due to the formation of oxides as shown in FIGS. 14 and 15.
  • the surface condition of the quasicrystalline deposits M9 and M10 being practically unchanged, the properties which result directly from it, for example the anti -adherent, are kept.
  • FIG. 14 represents counts of the number of pulses, as a function of the duration of the heat treatment, received on the analyzer of a Castaing probe set on the oxygen emission line for the coated substrates R16 and R17 , and for the aforementioned comparative substrates, the temperature being fixed at 400 ° C.
  • FIG. 15 represents counts of the number of pulses, as a function of the heat treatment temperature, received on the analyzer of a Castaing probe calibrated on the oxygen emission line for the coated substrates R16 and R17 , and for the aforementioned comparative substrates, in 144 hours.
  • the quasicrystalline coatings of the present invention resist oxidation better than the comparative substrates of AU5GT alloy and stainless steel, and this more particularly at 400 ° C.
  • the thickness of the deposit after brushing using a wire brush almost completely disappeared the open porosity of the coating. Only a closed porosity of 15% remains.
  • a comparison of all the characteristics of the coatings according to the invention and of the coatings of the prior art, and in particular the adhesion index, the coefficient of friction and the proportion of quasi-crystal for the coatings shows that the choice of materials with a high proportion of quasi-crystalline phase makes it possible to obtain better quality coatings.
  • the coatings not only do not mask the good properties of the alloys of the prior art, but also they exhibit good adhesion to the substrate due to the temperature stability of their structure.
  • the coatings according to the invention are suitable for different uses.
  • the lubricating agent coated on the substrate coated with a material according to the invention permeates the pores of the coating.
  • a bleeding phenomenon occurs. This property is useful for cooking utensils that are not not subjected to washing with detergents.
  • the coating materials according to the invention are particularly suitable for grills, crepe makers. Their great hardness allows them to be cleaned by scraping, without the need to use detergents.
  • the materials according to the invention having a large porosity find another interesting application in the field of anti-friction bearings.
  • the coatings according to the invention are particularly suitable for the production of anti-wear surfaces (reinforcement frame airborne, jackets and pistons, soles of iron) or in the manufacture of reference surfaces (for example for machine tool tables, for precision devices). They are also suitable for various cooking utensils without fat: for these utensils, the smoother the cooking surface, that is to say, the lower the porosity, the less the food will tend to adhere during cooking.

Abstract

The invention relates to materials for the coating of metal alloys or metals, in order to improve the performances of said alloys or metals. Said materials have a composition corresponding to the general formula Al Cu Fe X I, wherein X is one or a plurality of elements selected amongst V, Mo, Ti, Zr, Nb, Cr, Mn, Ru, Rh, Ni, Mg, W, Si and the rare earthes, I represents the inevitable elaboration impurities, e </= 2, 14 </= b </= 30, 7 </= c </= 20, 0 </= d </= 10, with c + d >/= 10 and a + b + c + d + e = 100 % in number of atoms and they contain at least 40 % by mass of an icosahedral quasi-crystalline phase and/or a decagonal quasi-crystalline phase. These materials are useful particularly as a coating on copper, aluminium alloys or copper alloys for the fabrication of cooking utensils, antifriction bearings, antiwear surfaces and reference surfaces.

Description

La présente invention concerne des matériaux de revêtement pour des substrats métalliques, les substrats revêtus de ces matériaux et les applications de ces substrats revêtus.The present invention relates to coating materials for metallic substrates, the substrates coated with these materials and the applications of these coated substrates.

Divers métaux ou alliages métalliques, par exemple les alliages d'aluminium, ont trouvé jusqu'ici de nombreuses application en raison de leur propriétés intéressantes et notamment leurs propriétés mécaniques, leur bonne conductibilité thermique, leur légèreté, leur faible coût. Ainsi, on connaît par exemple les ustensiles et appareils de cuisson, les paliers anti-friction, les chassis ou supports d'appareillage, diverses pièces obtenues par moulage. Le cuivre, à cause de son excellente conductibilité thermique, est également très utilisé pour les appareils de cuisson.Various metals or metal alloys, for example aluminum alloys, have so far found many applications because of their advantageous properties and in particular their mechanical properties, their good thermal conductivity, their lightness, their low cost. Thus, for example, cooking utensils and appliances are known, anti-friction bearings, chassis or apparatus supports, various parts obtained by molding. Copper, because of its excellent thermal conductivity, is also widely used for cooking appliances.

Toutefois, ces métaux ou alliages métalliques présentent des inconvénients liés à leur faible dureté, leur faible résistance à l'usure, leur faible résistance à la corrosion.However, these metals or metal alloys have drawbacks related to their low hardness, their low resistance to wear, their low resistance to corrosion.

Pour ce qui concerne les ustensiles de cuisson, deux problèmes essentiels se posent. D'une part, les aliments ont tendance à attacher sur les surfaces en alliage d'aluminium en cours de cuisson. D'autre part, le nettoyage des dispositifs de cuisson comportant des surfaces de dureté insuffisante (par exemple les grils en alliage d'aluminium) est difficile. Ce type de dispositif se nettoie de façon commode par grattage. Un tel procédé est toutefois difficilement utilisable pour les surfaces en alliage de faible dureté car il entraîne une dégradation rapide de l'état de surface.With regard to cooking utensils, two essential problems arise. On the one hand, food tends to attach to aluminum alloy surfaces during cooking. On the other hand, cleaning cooking devices with surfaces of insufficient hardness (for example aluminum alloy grills) is difficult. This type of device is conveniently cleaned by scraping. However, such a method is difficult to use for surfaces of low hardness alloy because it causes rapid deterioration of the surface condition.

On connaît également les ustensiles de cuisson en cuivre qui comportent traditionnellement un revêtement interne d'étain. Ce revêtement, bien que particulièrement adapté au contact alimentaire, présente cependant l'inconvénient d'être rapidement détérioré du fait de sa ductilité.Copper cooking utensils are also known, which traditionally have an internal coating of tin. This coating, although particularly suitable for food contact, has the disadvantage of being rapidly deteriorated due to its ductility.

Différentes solutions ont été proposées pour tenter de résoudre ces problèmes. L'une des solutions consiste à remplacer les alliages d'aluminium par d'autres matériaux, par exemple des aciers éventuellement inoxydables ou munis de revêtements métalliques. Les avantages liés à la bonne conductibilité thermique sont alors perdus. En outre, pour éviter l'adhérence des aliments, on a proposé des revêtements, par exemple en téflon. Mais de tels revêtements résistent moins bien au grattage que le substrat en alliage d'aluminium lui-même et leur stabilité thermique est relativement faible.Various solutions have been proposed in an attempt to resolve these problems. One solution is to replace aluminum alloys with other materials, for example steels that may be stainless or that have metallic coatings. The advantages linked to good thermal conductivity are then lost. In addition, to avoid the adhesion of food, coatings have been proposed, for example in teflon. However, such coatings are less resistant to scraping than the aluminum alloy substrate itself and their thermal stability is relatively low.

Différentes tentatives ont été faites pour obtenir des alliages d'aluminium améliorés. Ainsi, le brevet européen 100287 décrit une famille d'alliages amorphes ou microcristallins présentant une dureté améliorée, utilisables comme éléments de renforcement d'autres matériaux ou pour l'obtention de revêtements superficiels améliorant la résistance à la corrosion ou à l'usure. Mais un grand nombre des alliages décrits dans ce brevet présentent un inconvénient majeur dès lors que, au cours de leur mise en oeuvre, ils sont soumis à une température supérieure à 200°C. En effet, ils ne sont pas stables à la température, et lors d'un traitement thermique, notamment le traitement auquel ils sont soumis lors du dépôt sur un substrat, ils changent de structure: retour à l'état microcristallin lorsqu'il s'agit d'alliages essentiellement amorphes, grossissement des grains pour les alliages essentiellement microcristallins qui ont initialement une dimension de grains inférieure au micron. Ce changement de structure cristalline ou morphologique induit un changement des caractéristiques physiques du matériau qui affecte essentiellement sa densité. Il en résulte l'apparition de micro-fissures, d'où une fragilité, qui nuisent à la stabilité mécanique des dépôts.Various attempts have been made to obtain improved aluminum alloys. Thus, European patent 100287 describes a family of amorphous or microcrystalline alloys having improved hardness, usable as reinforcing elements of other materials or for obtaining surface coatings improving the resistance to corrosion or wear. However, a large number of the alloys described in this patent have a major drawback since, during their use, they are subjected to a temperature above 200 ° C. Indeed, they are not stable at temperature, and during a heat treatment, in particular the treatment to which they are subjected during deposition on a substrate, they change their structure: return to the microcrystalline state when it acts of essentially amorphous alloys, grain magnification for essentially microcrystalline alloys which initially have a grain size less than one micron. This change in crystalline or morphological structure induces a change in the physical characteristics of the material which essentially affects its density. This results in the appearance of micro-cracks, hence a brittleness, which adversely affects the mechanical stability deposits.

Les inventeurs ont maintenant découvert que, parmi l'ensemble des alliages du brevet européen 100287, certains présentent une structure particulière thermiquement stable.The inventors have now discovered that, among all the alloys of European patent 100287, some have a particular thermally stable structure.

La présente invention a pour objet de fournir un matériau de revêtement permettant de conserver les bonnes propriétés de certains substrats métalliques utilisés habituellement tout en supprimant les inconvénients qu'ils présentent en surface. Les matériaux constituant ces revêtements présentent une dureté améliorée, un coefficient de frottement plus faible, une bonne stabilité à des températures supérieures à 300°C nécessaire notamment pour les ustensiles du cuisson.The object of the present invention is to provide a coating material which makes it possible to retain the good properties of certain metallic substrates commonly used while eliminating the disadvantages which they present on the surface. The materials constituting these coatings have an improved hardness, a lower coefficient of friction, good stability at temperatures above 300 ° C. necessary in particular for cooking utensils.

Les matériaux de revêtement selon l'invention sont caractérisés en ce qu'ils répondent à la formule AlaCubFecXdIe dans laquelle X représente un ou plusieurs éléments choisis parmi V, Mo, Ti, Zr, Nb, Cr, Mn, Ru, Rh, Ni, Mg, W, Si et les terres rares, I représente les impuretés d'élaboration inévitables, e≦2, 14≦b ≦30, 7≦c ≦20, 0≦d≦10, avec c+d≧10 et a+b+c+d+e=100% en nombre d'atomes et en ce qu'ils contiennent au moins 40 % en masse d'une phase quasi-cristalline.The coating materials according to the invention are characterized in that they correspond to the formula Al a Cu b Fe c X d I e in which X represents one or more elements chosen from V, Mo, Ti, Zr, Nb, Cr , Mn, Ru, Rh, Ni, Mg, W, Si and the rare earths, I represents the inevitable impurities of elaboration, e ≦ 2, 14 ≦ b ≦ 30, 7 ≦ c ≦ 20, 0 ≦ d ≦ 10, with c + d ≧ 10 and a + b + c + d + e = 100% by number of atoms and in that they contain at least 40% by mass of a quasi-crystalline phase.

Par phase quasi-cristalline, on entend une phase ou un composé métallique dont l'étude par diffraction du rayonnement révèle l'existence de symétries de rotation normalement incompatibles avec la symétrie de translation, c'est-à-dire l'existence d'axes d'ordre 5, 8, 10 ou 12. Comme exemple de telles phases ou composés, on peut citer les phases quasi-cristallines icosaédriques qui sont des phases métalliques solides qui diffractent les électrons comme un cristal simple, mais qui présentent un groupe de symétrie m35 par rapport à un point qui est incompatible avec les translations de réseau. (Cf. D. Shechtman, I.Blech, D. Gratian, J.W. Cahn, Metallic Phase with Long-Range Orientational Order and No Translational Symmetry, Physical Review Letters, Vol. 53, N° 20, 1984 page 1951-1953). On peut également citer les phases quasi-cristallines décagonales, qui sont des phases métalliques solides qui diffractent les électrons comme un cristal simple, mais qui présentent un groupe de symétrie 10/m ou 10/mmm par rapport à un point, un ordre à longue distance et une symétrie de translation à une dimension. (Cf. L. Bendersky, Quasicrystal with One Dimensional Translational Symmetry and a Tenfold Rotation Axis, Physical Review Letters, Vol. 55, N° 14, 1985 page 1461-1463).By quasi-crystalline phase is meant a phase or a metallic compound whose study by radiation diffraction reveals the existence of rotation symmetries normally incompatible with translation symmetry, that is to say the existence of axes of order 5, 8, 10 or 12. As an example of such phases or compounds, mention may be made of the icosahedral quasicrystalline phases which are solid metal phases which diffract the electrons like a simple crystal, but which have a group of symmetry m35 with respect to a point which is incompatible with network translations. (Cf. D. Shechtman, I. Blech, D. Gratian, JW Cahn, Metallic Phase with Long-Range Orientational Order and No Translational Symmetry, Physical Review Letters, Vol. 53, No. 20, 1984 page 1951-1953). We can also cite the decagonal quasi-crystalline phases, which are solid metallic phases which diffract the electrons like a simple crystal, but which have a group of symmetry 10 / m or 10 / mmm with respect to a point, a long order distance and one-dimensional translational symmetry. (Cf. L. Bendersky, Quasicrystal with One Dimensional Translational Symmetry and a Tenfold Rotation Axis, Physical Review Letters, Vol. 55, N ° 14, 1985 page 1461-1463).

Les phases quasi-cristallines stables des matériaux de revêtement selon l'invention croissent de façon analogue aux cristaux habituels. Elles se comportant par conséquent comme des composés définis et présentent des points de transformation situés à des températures plus élevées que celles des eutectiques des alliages d'aluminium binaires courants, Al/Al₂Cu (547°C), Al/Si (577°C), Al/Al₃Fe (655°C), par exemple. Il en résulte une stabilité qui existe au-delà de ou jusqu'au voisinage de ces points eutectiques.The stable quasi-crystalline phases of the coating materials according to the invention grow in a similar fashion to the usual crystals. They therefore behave as defined compounds and have transformation points located at higher temperatures than those of the eutectics of common binary aluminum alloys, Al / Al₂Cu (547 ° C), Al / Si (577 ° C) , Al / Al₃Fe (655 ° C), for example. This results in a stability which exists beyond or up to the vicinity of these eutectic points.

Les matériaux selon l'invention sont obtenus par des procédés classiques. On peut, par exemple, élaborer un matériau selon l'invention à partir d'éléments purs (99,5% ou mieux) en mélangeant les différents éléments dans les proportions correspondant à la stoechiométrie du matériau souhaité, puis en effectuant la fusion du mélange dans un creuset en graphite sous une pression d'argon de 2.10⁴ Pa dans un four HF. On peut, le cas échéant, effectuer un refroidissement ultrarapide du matériau après fusion (procédé dit "melt spinning"). Ce procédé permet d'obtenir une meilleure homogénéïté du matériau de revêtementThe materials according to the invention are obtained by conventional methods. One can, for example, develop a material according to the invention from pure elements (99.5% or better) by mixing the different elements in the proportions corresponding to the stoichiometry of the desired material, then by melting the mixture in a graphite crucible under an argon pressure of 2.10⁴ Pa in an HF oven. It is possible, if necessary, to carry out an ultra-rapid cooling of the material after melting (process called "melt spinning"). This process allows better homogeneity of the coating material

Comme substrat, on peut utiliser les alliages d'aluminium, les alliages de cuivre et le cuivre. Les matériaux de revêtement selon l'invention sont particulièrement utiles pour les alliages d'aluminium commerciaux, et notamment pour les alliages dits "alimentaires" ou les alliages dits "de fonderie" et pour le cuivre.As a substrate, aluminum alloys, copper alloys and copper can be used. Coating materials according to the invention are particularly useful for commercial aluminum alloys, and in particular for so-called "food" alloys or so-called "foundry" alloys and for copper.

La mise en oeuvre des matériaux selon l'invention comme revêtement de divers substrats se fait par différents procédés selon le résultat souhaité.The implementation of the materials according to the invention as coating of various substrates is done by different methods according to the desired result.

Par exemple, si un revêtement présentant un taux élevé de porosité ouverte est souhaité, le matériau selon l'invention est déposé sur le substrat par projection de gouttelettes du matériau. A cet effet, on peut utiliser un chalumeau à poudres, tel que le "Pistolet Thermospray type 5P" commercialisé par Metco Inc. Avant projection, le matériau selon l'invention sous forme massique est broyé et tamisé pour obtenir une poudre dont les grains ont une dimension comprise entre environ 0,02 mm et 0,2 mm, de préférence inférieure à 0,074 mm. Si un faible taux de porosité ouverte est souhaité, on effectuera le dépôt du matériau selon l'invention par un prodédé en phase vapeur, par exemple par pulvérisation cathodique, ou en utilisant une torche à plasma alimentée en poudre comme indiqué ci-dessus.For example, if a coating having a high rate of open porosity is desired, the material according to the invention is deposited on the substrate by spraying droplets of the material. For this purpose, a powder torch can be used, such as the "Thermospray gun type 5P" sold by Metco Inc. Before projection, the material according to the invention in mass form is ground and sieved to obtain a powder whose grains have a dimension between approximately 0.02 mm and 0.2 mm, preferably less than 0.074 mm. If a low level of open porosity is desired, the material according to the invention will be deposited by a product in the vapor phase, for example by sputtering, or by using a plasma torch supplied with powder as indicated above.

Pour certaines applications, il peut être utile de supprimer ou de réduire le taux de porosité ouverte en surface. Un tel résultat s'obtient par:
- grenaillage, par exemple à l'aide de microbilles en acier ayant un diamètre de 0,5 à 1 mm. On obtient ainsi une surface de porosité ouverte nulle, sans perte de dureté, ni augmentation du coefficient de frottement, ni décohésion à l'interface substrat-revêtement.
- polissage, par exemple à l'aide de papier pour métallographie, à condition que la porosité fermée du revêtement soit négligeable.
- refusion de surface.
For certain applications, it may be useful to suppress or reduce the rate of open porosity at the surface. Such a result is obtained by:
- shot blasting, for example using steel microbeads having a diameter of 0.5 to 1 mm. There is thus obtained a surface of zero open porosity, without loss of hardness, nor increase in the coefficient of friction, or decohesion at the substrate-coating interface.
- polishing, for example using metallography paper, provided that the closed porosity of the coating is negligible.
- surface reflow.

Pour obtenir directement un taux de porosité ouverte voisin de zéro, on peut utiliser une torche à jet supersonique qui accélère la poudre de matériau selon l'invention à des vitesses comprises entre Mach 6 et Mach 14.To directly obtain an open porosity rate close to zero, a supersonic jet torch can be used which accelerates the powder of material according to the invention at speeds between Mach 6 and Mach 14.

La présente invention sera expliquée plus en détail par référence aux exemples non limitatifs suivants.The present invention will be explained in more detail with reference to the following nonlimiting examples.

Les revêtements obtenus ont été caractérisés par leur épaisseur (E.), leur taux de porosité ouverte (P.O.), leur index d'adhérence (I.E.), leur coefficient de frottement (C.F.), leur dureté (D.) et leur taux de phase quasi-cristalline (Q.C.).The coatings obtained were characterized by their thickness (E.), their open porosity rate (PO), their adhesion index (IE), their coefficient of friction (CF), their hardness (D.) and their rate of quasi-crystalline phase (QC).

Le taux de porosité ouverte (P.O.) a été estimé à partir des images de microscopie à balayage, obtenues à l'aide d'un microscope à balayage SEM 505, de Philips.The open porosity (P.O.) rate was estimated from scanning microscopy images obtained using a SEM 505 scanning microscope from Philips.

Les index d'adhérence (I.A.) ont été attribués après fracture au cours d'un essai de résilience de la manière suivante:
- index A lorsqu'il n'y a pas de décollement visible à l'interface substrat/dépôt; l'adhérence est considérée comme parfaite.
- index B lorsque 3 fissures au plus sont visibles à l'interface substrat/dépôt, en métallographie optique, avec un grossissement de 50.
- index E lorsqu'un décollement est visible à l'interface substrat/dépôt.
The adhesion indexes (IA) were assigned after fracture during a resilience test as follows:
- index A when there is no visible detachment at the substrate / deposition interface; grip is considered perfect.
- index B when at most 3 cracks are visible at the substrate / deposition interface, in optical metallography, with a magnification of 50.
- index E when a detachment is visible at the substrate / deposition interface.

Le coefficient de frottement C.F. a été évalué au cours d'un essai de résistance à la rayure par un indenteur diamant Vickers. Le coefficient de frottement C.F. est égal à tangenteα, α étant la pente de la courbe Ft=f(Fn), Ft étant la force tangentielle de résistance à la rayure, Fn étant la force appliquée à l'indenteur, croissant linéairement en fonction du temps.The coefficient of friction C.F. was evaluated during a scratch resistance test by a Vickers diamond indenter. The coefficient of friction CF is equal to tangent α, α being the slope of the curve Ft = f (Fn), Ft being the tangential force of resistance to scratching, Fn being the force applied to the indentor, increasing linearly as a function of the time.

La dureté (Hv₃₀) a été déterminée à l'aide du duromètre WOLPERT V-Testor 2, sous charge de 30 grammes.The hardness (Hv₃₀) was determined using the WOLPERT durometer V-Testor 2, under load of 30 grams.

L'existence de phases quasi-cristallines est confirmée par diffraction des rayons X. Les diagrammes de diffraction des rayons X ont été effectués à l'aide d'un diffractomètre Siemens à acquisiton rapide, compteur linéaire à fil, avec le rayonnement Kα1du cobalt, λ=0,17889 nm.The existence of quasi-crystalline phases is confirmed by X-ray diffraction. The X-ray diffraction diagrams were carried out using a Siemens fast acquisition diffractometer, linear wire counter, with the K α1 radiation from the cobalt, λ = 0.17889 nm.

La stabilité thermique des matériaux selon l'invention a été étudiée par calorimétrie différentielle à balayage à l'aide d'un calorimètre SETARAM.The thermal stability of the materials according to the invention was studied by differential scanning calorimetry using a SETARAM calorimeter.

Les revêtements obtenus ont été caractérisés et les figures 1 à 16 illustrent certaines caractérisations. Ainsi:

  • -les fig. 1 à 4 représentent les diagrammes de diffraction des rayons X de revêtements selon l'invention.
  • -les fig. 5 et 6 représentent les diagrammes de diffraction des rayons X de revêtements selon l'art antérieur:
The coatings obtained have been characterized and Figures 1 to 16 illustrate certain characterizations. So:
  • - fig. 1 to 4 represent the X-ray diffraction diagrams of coatings according to the invention.
  • - fig. 5 and 6 represent the X-ray diffraction diagrams of coatings according to the prior art:

Sur ces diagrammes, l'angle de diffraction 20 est porté en abscisse, le nombre d'impulsions comptées, correspondant à l'intensité, est porté en ordonnée.

  • -les fig. 7, 8 et 9 représentent la courbe Ft=f(Fn) respectivement pour un substrat, un revêtement selon l'invention et un revêtement de l'art antérieur, obtenue lors de l'essai de résistance à la rayure.
  • -la fig. 10 représente une image de microscopie à balayage pour un revêtement selon l'invention portant trois rayures telles qu'effectuées au cours de l'essai de résistance à la rayure.
  • -les fig. 11 et 12 représentent des images de microscopie à balayage respectivement pour deux revêtements selon l'invention.
  • -les fig. 13a à 13e représentent la variation de la dureté respectivement pour les substrats revêtus R11 à R15, le long d'une droite perpendiculaire à la surface des substrats.
  • -la fig. 14 représente la courbe donnant le nombre d'impulsions reçues sur l'analyseur d'une sonde de Castaing à température constante en fonction du temps, pour différents substrats.
  • -la fig. 15 représente la courbe donnant le nombre d'impulsions reçues sur l'analyseur d'une sonde de Castaing à un instant donné en fonction de la température.
  • -la fig. 16 représente la variation de la dureté du substrat revêtu R18 de l'exemple 7, le long d'une droite perpendiculaire à la surface du substrat, pour différents substrats.
On these diagrams, the diffraction angle 20 is plotted on the abscissa, the number of pulses counted, corresponding to the intensity, is plotted on the ordinate.
  • - fig. 7, 8 and 9 represent the curve Ft = f (Fn) respectively for a substrate, a coating according to the invention and a coating of the prior art, obtained during the scratch resistance test.
  • - fig. 10 shows a scanning microscopy image for a coating according to the invention bearing three scratches as carried out during the scratch resistance test.
  • - fig. 11 and 12 represent scanning microscopy images respectively for two coatings according to the invention.
  • - fig. 13a to 13e show the variation in hardness respectively for the coated substrates R11 to R15, along a straight line perpendicular to the surface of the substrates.
  • - fig. 14 represents the curve giving the number of pulses received on the analyzer of a Castaing probe at constant temperature as a function of time, for different substrates.
  • - fig. 15 represents the curve giving the number of pulses received on the analyzer of a Castaing probe at a given time as a function of the temperature.
  • - fig. 16 shows the variation in the hardness of the coated substrate R18 of Example 7, along a straight line perpendicular to the surface of the substrate, for different substrates.

EXEMPLE 1EXAMPLE 1 Préparation de matériaux de revêtement selon l'inventionPreparation of coating materials according to the invention

Différents matériaux de revêtement ont été préparés par fusion des éléments constitutifs dans les proportions stoechimétriques correspondant à la composition souhaitée dans un creuset en graphite à l'aide d'un four HF sous une pression de 2.10⁴ Pa d'argon. Le tableau 1 ci-dessous donne la composition des matériaux M1-M5, M9 et M10 préparés. TABLEAU 1 Matériau Composition M1 Al65Cu20Fe15 M2 Al69Cu17Fe10Mo1Si3 M3 Al72Cu16Fe8Mo1Si3 M4 Al75Cu14Fe7Mo1Si3 M5 Al68Cu17Fe10V5 M9 Al65Cu22Fe13 M10 Al65,5Cu18,5Fe8Cr8 Different coating materials were prepared by melting the constituent elements in stoichiometric proportions corresponding to the desired composition in a graphite crucible using an HF oven under a pressure of 2.10 Pa of argon. Table 1 below gives the composition of the materials M1-M5, M9 and M10 prepared. TABLE 1 Material Composition M1 Al65Cu20Fe15 M2 Al69Cu17Fe10Mo1Si3 M3 Al72Cu16Fe8Mo1Si3 M4 Al75Cu14Fe7Mo1Si3 M5 Al68Cu17Fe10V5 M9 Al65Cu22Fe13 M10 Al65.5Cu18.5Fe8Cr8

EXEMPLE 2EXAMPLE 2 Dépôt des matériaux M1 à M5 sur un substratDeposition of materials M1 to M5 on a substrate

Le substrat était un alliage d'aluminium AU4G, présentant une dureté Hv=95±5 et un coefficient de frottement C.F.=1,6.The substrate was an AU4G aluminum alloy, having a hardness Hv = 95 ± 5 and a coefficient of friction CF = 1.6.

Un matériau brut de coulée obtenu dans l'exemple précédent a été broyé dans un broyeur à galets d'acier carburé. La poudre résultante a été tamisée et la fraction ayant un diamètre inférieur à 0,074 mm a été retenue.A raw casting material obtained in the previous example was ground in a carbide steel roller mill. The resulting powder was sieved and the fraction having a diameter of less than 0.074 mm was retained.

Cette fraction a été projectée à l'aide d'un chalumeau à poudre, le Pistolet Thermospray Metco.This fraction was projected using a powder torch, the Thermospray Metco Pistol.

Le débit de l'hydrogène était de 47 l/mn et le débit de l'oxygène était de 28 l/mn.The hydrogen flow rate was 47 l / min and the oxygen flow rate was 28 l / min.

La pièce a été maintenue sous une atmosphère de N₂ à 5% de H₂.The part was maintained under an atmosphere of N₂ at 5% of H₂.

La température du substrat est restée inférieure à 200°C pendant la durée de la projection.The substrate temperature remained below 200 ° C for the duration of the projection.

Les revêtements ont été polis au papier pour métallographie de grain 1200.The coatings were polished with 1200 grit metallography paper.

Les caractéristiques des revêtements R1 à R7 obtenus à partir des matériaux M1 à M5 sont rassemblées dans la tableau 2 ci-dessous. TABLEAU 2 Rev. Mat. E. (µm) P.O. I.A. C.F. D.(Hv30) Q.C(% en masse) R1 M1 30±10 10 % B 0,5 560 > 90% R2 M1 50±10 35 % A 0,5 410 > 90% R3 M1 50±10 40 % A 0,5 370 > 90% R4 M2 40±10 30 % A 500 > 80% R5 M3 40±10 30 % A 480 > 80% R6 M4 50±10 40 % B 510 > 60% R7 M5 30±10 30 % A 0,55 510 > 60% The characteristics of the coatings R1 to R7 obtained from the materials M1 to M5 are collated in Table 2 below. TABLE 2 Rev. Mast. E. (µm) PO IA CF D. (Hv30) QC (% by mass) R1 M1 30 ± 10 10% B 0.5 560 > 90% R2 M1 50 ± 10 35% AT 0.5 410 > 90% R3 M1 50 ± 10 40% AT 0.5 370 > 90% R4 M2 40 ± 10 30 % AT 500 > 80% R5 M3 40 ± 10 30 % AT 480 > 80% R6 M4 50 ± 10 40% B 510 > 60% R7 M5 30 ± 10 30 % AT 0.55 510 > 60%

Pour les revêtements R1, R2 et R3, les phases résiduelles sont en proportion trop faible pour pourvoir être identifiées. Dans les revêtements R4, R5 et R6, la phase résiduelle contient un mélange de Al₂Cu, Al₇Cu₂Fe, Al₆Fe, Al et Si. Dans le revêtement R7, la phase résiduelle contient un mélange de Al₂Cu et Al₃V.For coatings R1, R2 and R3, the residual phases are too small in proportion to be identified. In coatings R4, R5 and R6, the residual phase contains a mixture of Al₂Cu, Al₇Cu₂Fe, Al₆Fe, Al and Si. In coating R7, the residual phase contains a mixture of Al₂Cu and Al₃V.

Le structure quasicristalline des matériaux de l'invention induit une grande stabilité thermique des revêtements obtenus.The quasicrystalline structure of the materials of the invention induces great thermal stability of the coatings obtained.

La température de première transformation Tx des divers matériaux avant dépôt et des substrats munis des revêtements obtenus a été déterminée par calorimétrie à balayage avec α=10°C/mn.The first transformation temperature Tx of the various materials before deposition and of the substrates provided with the coatings obtained was determined by scanning calorimetry with α = 10 ° C / min.

La mesure a été effectuée sur les matériaux suivants:
- les matériaux M1 à M4.
- les matériaux M1′ à M4′, de même composition respectivement que M1 à M4, mais ayant subi une solidification rapide par projection sur un tambour tournant (melt spinning). M2′, M3′ et M4′ présentent une proportion non négligeable de phase amorphe, contrairement à M1′.
- le substrat AU4G, revêtu respectivement par les 8 matériaux ci-dessus.
The measurement was made on the following materials:
- materials M1 to M4.
- the materials M1 ′ to M4 ′, of the same composition respectively as M1 to M4, but having undergone rapid solidification by projection on a rotating drum (melt spinning). M2 ′, M3 ′ and M4 ′ have a significant proportion of amorphous phase, unlike M1 ′.
- the AU4G substrate, coated respectively with the 8 above materials.

Pour les substrats revêtus, la température Tx déterminée est celle du substrat, compte-tenu de la faible épaisseur relative du revêtement.For coated substrates, the temperature Tx determined is that of the substrate, taking into account the small relative thickness of the coating.

Pour les matériaux M1 à M4 et M1′ à M4′, les résultats figurent au tableau 3 ci-dessous. TABLEAU 3 Matériau % de phase amorphe (en masse) Tx M1 ≃0 >800°C M2 ≃0 >800°C M3 ≃0 >800°C M4 ≃0 >800°C M1′ ≃0 >800°C M2′ ≃10 540°C M3′ ≃20 420°C M4′ - 40 380°C For materials M1 to M4 and M1 ′ to M4 ′, the results are shown in Table 3 below. TABLE 3 Material % of amorphous phase (by mass) Tx M1 ≃0 > 800 ° C M2 ≃0 > 800 ° C M3 ≃0 > 800 ° C M4 ≃0 > 800 ° C M1 ′ ≃0 > 800 ° C M2 ′ ≃10 540 ° C M3 ′ ≃20 420 ° C M4 ′ - 40 380 ° C

Il apparaît que, après dépôt sur un substrat, la phase amorphe des matériaux M2′ à M4′ a disparu. Le revêtement a une stabilité au moins égale à celle du support.It appears that, after deposition on a substrate, the amorphous phase of the materials M2 ′ to M4 ′ has disappeared. The coating has a stability at least equal to that of the support.

Lors du traitement thermique lié au procédé de dépôt du revêtement, la phase quasi-cristalline du matériau selon l'invention ne subit pas de transformation: ni grossissement des grains, ni changement de structure des grains et l'éventuelle phase amorphe est transformée en phase cristalline. Le revêtement sera par conséquent thermiquement stable quelque soit le procédé d'obtention du matériau selon l'invention.During the heat treatment linked to the coating deposition process, the quasi-crystalline phase of the material according to the invention does not undergo any transformation: neither grain enlargement, nor change in grain structure and the possible amorphous phase is transformed into phase crystalline. The coating will therefore be thermally stable whatever the process for obtaining the material according to the invention.

Les phases quasi-cristallines ont été identifiées par les diagrammes de diffraction des rayons X. Sur tous ces diagrammes, les raies d'intensité négligeable n'ont pas été indexées.

  • La figure 1 représente le diagramme RX du revêtement R1. Sur cette figure, I désigne les raies de la phase icosaédrique, et D les raies de la phase décagonale.
  • La figure 2 représente le diagramme RX du revêtement R3. I et D ont la même signification que pour la fig. 1.
  • La figure 3 représente le diagramme RX du revêtement R4. Sur cette figure, I désigne les raies de la phase icosaédrique et t désigne le composé Al₂Cu quadratique. On n'observe plus de phase décagonale.
  • La figure 4 représente le diagramme RX du revêtement R5. Sur cette figure, I désigne les raies de la phase icosaédrique, t désigne les raies du composé Al₂Cu quadratique et A les raies de l'aluminium cubique à faces centrées.
The quasi-crystalline phases have been identified by the X-ray diffraction diagrams. On all these diagrams, the lines of negligible intensity have not been indexed.
  • FIG. 1 represents the RX diagram of the coating R1. In this figure, I denotes the lines of the icosahedral phase, and D denotes the lines of the decagonal phase.
  • FIG. 2 represents the RX diagram of the coating R3. I and D have the same meaning as in fig. 1.
  • FIG. 3 represents the RX diagram of the coating R4. In this figure, I denotes the lines of the icosahedral phase and t denotes the quadratic Al₂Cu compound. We no longer observe a decagonal phase.
  • FIG. 4 represents the RX diagram of the coating R5. In this figure, I denotes the lines of the icosahedral phase, t denotes the lines of the quadratic Al₂Cu compound and A denotes the lines of cubic aluminum with centered faces.

La proportion de phase quasi-cristalline correspond au rapport de l'aire des pics attribués à la phase quasi-cristalline à l'aire totale des pics visibles.The proportion of quasi-crystalline phase corresponds to the ratio of the area of the peaks attributed to the quasi-crystalline phase to the total area visible peaks.

Le coefficient de frottement a été déterminé à l'aide des courbes Ft=f(Fn) définies précédemment. Les figures 7 et 8 représentent cette courbe respectivement pour le substrat seul et pour le substrat revêtu R3.The coefficient of friction was determined using the curves Ft = f (Fn) defined above. Figures 7 and 8 show this curve respectively for the substrate alone and for the coated substrate R3.

La pente de la courbe donne un coefficient de frottement de 1,6 pour le substrat seul et de 0,5 pour R3. Pour celui-ci, à partir du point A de la courbe, la pente est modifiée: l'indenteur ayant traversé la couche de revêtement, a pénétré dans le substrat et la pente de la courbe à partir de ce point est équivalente à la celle de la courbe de la fig. 7.The slope of the curve gives a coefficient of friction of 1.6 for the substrate alone and 0.5 for R3. For this one, from the point A of the curve, the slope is modified: the indentor having crossed the coating layer, penetrated into the substrate and the slope of the curve from this point is equivalent to that from the curve in fig. 7.

En outre, des observations au microscope à balayage associées à des analyses à la microsonde de Castaing ont permis de préciser le mode de fissuration et la profondeur de pénétration de l'indenteur lors de l'essai de résistance à la rayure. L'examen du fond de la rayure révèle l'apparition de fissures intergranulaires dans le dépôt selon l'invention sans décohésion notable de celui-ci par rapport au substrat. Le dosage d'un élément présent dans le substrat et absent du revêtement (Mn) montre que le revêtement ne subit pas décohésion du substrat de part et d'autre de la rayure avant que la force normale Fn atteigne la valeur suffisante pour que l'indenteur traverse le revêtement. L'image de microscopie à balayage de la fig.10 représente trois rayures effectuées dans le revêtement R3. Sur cette figure, la longueur totale d'une rayure correspond aux 60 N portés en abscisse sur la courbe de la fig.8. On en déduit que l'indenteur ne traverse le revêtement que sur le tiers final de la rayure. A partir du point où l'indenteur a traversé le revêtement, il se forme sur l'image une bordure blanche caractéristique du matériau du substrat déplacé par l'indenteur. Le revêtement est abimé, mais non pas arraché par plaques. Ces observations confirment la bonne adhérence des revêtements sur le substrat.In addition, observations with a scanning microscope associated with analyzes with the Castaing microprobe made it possible to specify the mode of cracking and the depth of penetration of the indenter during the scratch resistance test. Examination of the bottom of the scratch reveals the appearance of intergranular cracks in the deposit according to the invention without significant decohesion of the latter relative to the substrate. The assay of an element present in the substrate and absent from the coating (Mn) shows that the coating does not undergo decohesion of the substrate on either side of the scratch before the normal force Fn reaches the value sufficient for the indenter through the coating. The scanning microscopy image in fig. 10 represents three scratches made in the coating R3. In this figure, the total length of a stripe corresponds to the 60 N plotted on the abscissa on the curve in fig. 8. We deduce that the indentor crosses the coating only on the final third of the scratch. From the point where the indentor has passed through the coating, a white border characteristic of the substrate material displaced by the indentor is formed on the image. The coating is damaged, but not torn off by plates. These observations confirm the good adhesion of the coatings to the substrate.

Le taux de porosité ouverte a été évalué à partir d'images de microscope à balayage. La fig.11 représente l'image de microscopie à balayage du revêtement R1 (la portion blanche du trait horizontal au bas de l'image représente 1 mm) et la fig.12 celle du revêtement R2 (la portion blanche du trait horizontal au bas de l'image représente 0,1 mm).The open porosity rate was evaluated from scanning microscope images. Fig. 11 represents the scanning microscopy image of the coating R1 (the white portion of the horizontal line at the bottom of the image represents 1 mm) and Fig. 12 that of the coating R2 (the white portion of the horizontal line at the bottom 0.1 mm).

Pour déterminer le taux de porosité ouverte, on a mesuré, sur une surface de référence d'aire S d'une telle image, l'aire A occupée par les particules déposées P.O.= 1-(A/S).To determine the open porosity rate, the area A occupied by the deposited particles P.O. = 1- (A / S) was measured on a reference surface of area S of such an image.

EXEMPLE 3 (COMPARATIF)EXAMPLE 3 (COMPARATIVE)

Trois matériaux de l'art antérieur ont été préparés en mettant en oeuvre le procédé de l'exemple 1. Les compositions de ces matériaux sont rassemblées au tableau 5. TABLEAU 4 Mat. Composition M6 Al78Cu12Fe6Mo1Si3 M7 Al60Cu10Fe30 M8 Al65Cu18V12Mo2Si3 Three materials of the prior art were prepared by implementing the method of Example 1. The compositions of these materials are collated in Table 5. TABLE 4 Mast. Composition M6 Al78Cu12Fe6Mo1Si3 M7 Al60Cu10Fe30 M8 Al65Cu18V12Mo2Si3

EXEMPLE 4 (COMPARATIF)EXAMPLE 4 (COMPARATIVE)

Les matériaux de l'exemple 3, bruts de coulée, ont été déposés sur un substrat identique à celui de l'exemple 2, en mettant en oeuvre le procédé de l'exemple 2. Les substrats revêtus obtenus ont été caractérisés et les résultats sont rassemblés au tableau 5. TABLEAU 5 Rev. Mat. E.(µm) P.O. I.A. C.F. D.(Hv30) Q.C(% en vol) R8 M6 45±10 40 % E 380 0% R9 M7 40±10 E 0,95 400 0% R10 M8 40±10 E 370 < 20% The materials of Example 3, crude casting, were deposited on a substrate identical to that of Example 2, using the method of Example 2. The coated substrates obtained were characterized and the results are collated in Table 5. TABLE 5 Rev. Mast. E. (µm) PO IA CF D. (Hv30) QC (% in vol) R8 M6 45 ± 10 40% E 380 0% R9 M7 40 ± 10 E 0.95 400 0% R10 M8 40 ± 10 E 370 <20%

Conformément à la figure 5 qui représente le diagramme RX du revêtement R8, le revêtement R8 est essentiellement constitué par un mélange de Al₂Cu (raies t), d'aluminium cubique à faces centrées (raie A) et de composé amorphe ou mal cristallisé indéterminé (raies a). Les raies I de la phase icosaédrique et les raies D de la phase décagonale n'existent pas.In accordance with FIG. 5 which represents the RX diagram of the coating R8, the coating R8 essentially consists of a mixture of Al₂Cu (t-lines), cubic aluminum with centered faces (line A) and of indeterminate amorphous or poorly crystallized compound ( lines a). The I lines of the icosahedral phase and the D lines of the decagonal phase do not exist.

Conformément à la figure 6 qui représente le diagramme RX du revêtement R9, le revêtement R9 comprend, outre la faible proportion de phase quasi-cristalline, un mélange de Al₂Cu et de Al₃V. L'absence des raies élargies en 2ϑ=31,8° et 2ϑ=53,9° (positions marquées par des tirets verticaux) prouve la disparition de la phase icosaédrique.In accordance with FIG. 6 which represents the RX diagram of the coating R9, the coating R9 comprises, in addition to the low proportion of quasi-crystalline phase, a mixture of Al₂Cu and Al₃V. The absence of the lines widened at 2ϑ = 31.8 ° and 2ϑ = 53.9 ° (positions marked with vertical dashes) proves the disappearance of the icosahedral phase.

La fig.9 représente la courbe Ft=f(Fn) pour le revêtement R9, obtenue de la même manière que ci-dessus. Elle fait apparaître que le coefficient de frottement du revêtement varie entre 0,95 et 1,15 entre le début et la fin de la rayure.Fig.9 shows the curve Ft = f (Fn) for the coating R9, obtained in the same way as above. It shows that the coefficient of friction of the coating varies between 0.95 and 1.15 between the start and the end of the scratch.

EXEMPLE 5EXAMPLE 5 Dépôt de matériau M1 par jet supersoniqueM1 material deposition by supersonic jet

Cinq substrats ont été préparés par brossage à la brosse métallique et/ou par sablage. Ensuite, une poudre du matériau M1, obtenue selon le procédé de l'exemple 2, a été appliquée sur chacun des substrats au jet supersonique. La poudre a ainsi subi une accélération dans un jet d'azote à haute pression, jusqu'à une vitesse de Mach 10; elle a fondu par passage à travers une flamme réductrice et elle a été déposée sur les substrats pour donner les substrats revêtus R11 à R15.Five substrates were prepared by brushing with a wire brush and / or by sandblasting. Then, a powder of the material M1, obtained according to the method of Example 2, was applied to each of the substrates with a supersonic jet. The powder was thus accelerated in a high pressure nitrogen jet, up to a speed of Mach 10; it melted by passing through a reducing flame and it was deposited on the substrates to give the coated substrates R11 to R15.

La nature des substrats et les conditions du traitement de surface avant application de la poudre de M1 sont rassemblées dans le tableau 6 ci-dessous, pour chacun des substrats revêtus. TABLEAU 6 Revêtement Substrat Etat de surface Taille des grains de sablage R11 AU4G sablage 0,12 mm R12 AU4G brossage + sablage 1,6 mm R13 AU4G sablage 1,6 mm R14 AU5GT brossage + sablage 1,6 mm R15 AU7GT sablage 0,12 mm The nature of the substrates and the conditions of the surface treatment before application of the M1 powder are collated in Table 6 below, for each of the coated substrates. TABLE 6 Coating Substrate Surface condition Sanding grain size R11 AU4G sandblasting 0.12mm R12 AU4G brushing + sanding 1.6mm R13 AU4G sandblasting 1.6mm R14 AU5GT brushing + sanding 1.6mm R15 AU7GT sandblasting 0.12mm

Les revêtements R11 à R15 ainsi obtenus adhèrent parfaitement aux substrats. Leur porosité ouverte est négligeable et leur porosité fermée inférieure à 15%. Ce procédé permet d'atteindre des épaisseurs importantes, voisines de ou supérieures à 100 µm. Les figures 13a, 13b, 13c, 13d et 13 e représentent les microduretés Hv₃₀ obtenues respectivement avec les substrats revêtus R11, R12, R13, R14 et R15. La microdureté a été mesurée sur la tranche des substrats revêtus, le long d'une droite perpendiculaire à la surface du substrat. Il est à noter que certains substrats revêtus ont une dureté superficielle qui dépasse 500 kg/mm².The coatings R11 to R15 thus obtained adhere perfectly to the substrates. Their open porosity is negligible and their closed porosity less than 15%. This process allows to reach significant thicknesses, close to or greater than 100 µm. FIGS. 13a, 13b, 13c, 13d and 13 e represent the Hv₃₀ microduretures obtained respectively with the coated substrates R11, R12, R13, R14 and R15. The microhardness was measured on the edge of the coated substrates, along a straight line perpendicular to the surface of the substrate. It should be noted that certain coated substrates have a surface hardness which exceeds 500 kg / mm².

EXEMPLE 6EXAMPLE 6 Dépôt des matériaux M9 et M10 sur un substratDeposit of materials M9 and M10 on a substrate

Les alliages M9 et M10 de l'exemple 1 ont été élaborés et réduits en poudre selon le procédé de l'exemple 2. Ces alliages ont été appliqués sur un substrat AU5GT selon le mode opératoire de l'exemple 3. Les substrats revêtus obtenus R16 et R17 ont été utilisés pour évaluer la résistance à l'oxydation des revêtements et donc leurs performances lors de leur utilisation dans le domaine de la cuisson alimentaire. A cet effet, les substrats revêtus ont été d'abord polis mécaniquement pour obtenir un poli optique, puis soumis à l'air à des traitements isothermes à 300°C et 400°C de durée égale à 30 heures et 144 heures. Par comparaison, une plaque du substrat non revêtu et une plaque d'acier inoxydable 18/8 ont été soumises aux mêmes traitements.The alloys M9 and M10 of Example 1 were prepared and reduced to powder according to the method of Example 2. These alloys were applied to a AU5GT substrate according to the procedure of Example 3. The coated substrates obtained R16 and R17 were used to evaluate the resistance to oxidation of coatings and therefore their performance when used in the field of food cooking. To this end, the coated substrates were first mechanically polished to obtain an optical polish, then subjected to air in treatments isotherms at 300 ° C and 400 ° C with a duration of 30 hours and 144 hours. By comparison, an uncoated substrate plate and an 18/8 stainless steel plate were subjected to the same treatments.

Les micrographies optiques des éprouvettes obtenues, sans polissage postérieur au traitement thermique, font apparaître que les dépôts quasicristallins M9 et M10 ne présentent pas de dégradation visible de leur surface, alors que le substrat AU5GT et l'acier inoxydable montrent une altération très nette de leur surface. Cette altération est due à la formation d'oxydes comme l'attestent les figures 14 et 15. L'état de surface des dépôts quasicristallins M9 et M10 n'étant pratiquement pas modifié, les propriétés qui en découlent directement, par exemple les propriétés anti-adhérentes, sont conservées.The optical micrographs of the test pieces obtained, without polishing after the heat treatment, show that the quasicrystalline deposits M9 and M10 show no visible degradation of their surface, while the substrate AU5GT and the stainless steel show a very marked deterioration in their area. This deterioration is due to the formation of oxides as shown in FIGS. 14 and 15. The surface condition of the quasicrystalline deposits M9 and M10 being practically unchanged, the properties which result directly from it, for example the anti -adherent, are kept.

La figure 14 représente des comptages du nombre d'impulsions, en fonction de la durée du traitement thermique, reçues sur l'analyseur d'une sonde de Castaing calé sur la raie d'émission de l'oxygène pour les substrats revêtus R16 et R17, et pour les substrats comparatifs précités, la température étant fixée à 400°C.FIG. 14 represents counts of the number of pulses, as a function of the duration of the heat treatment, received on the analyzer of a Castaing probe set on the oxygen emission line for the coated substrates R16 and R17 , and for the aforementioned comparative substrates, the temperature being fixed at 400 ° C.

La figure 15 représente des comptages du nombre d'impulsions, en fonction de la température de traitement thermique, reçues sur l'analyseur d'une sonde de Castaing calé sur la raie d'émission de l'oxygène pour les substrats revêtus R16 et R17, et pour les substrats comparatifs précités, en 144 heures.FIG. 15 represents counts of the number of pulses, as a function of the heat treatment temperature, received on the analyzer of a Castaing probe calibrated on the oxygen emission line for the coated substrates R16 and R17 , and for the aforementioned comparative substrates, in 144 hours.

Il apparaît clairement sur ces figures que les revêtements quasicristallins de la présente invention résistent mieux à l'oxydation que les substrats comparatifs en alliage AU5GT et en acier inoxydable, et ceci plus particulièrement à 400°C.It is clear from these figures that the quasicrystalline coatings of the present invention resist oxidation better than the comparative substrates of AU5GT alloy and stainless steel, and this more particularly at 400 ° C.

EXEMPLE 7EXAMPLE 7

Dépôt du matériau M10 sur un substrat de cuivreDeposition of the M10 material on a copper substrate

L'alliage M10, élaboré et réduit en poudre comme précédemment, a été déposé, à l'aide d'un chalumeau à plasma utilisé dans l'exemple 2, sur une plaque de cuivre métallique. Cette plaque avait une microdureté moyenne de Hv₃₀ = 50 ± 1 kg/mm². La figure 16 montre que la dureté du dépôt, mesurée sur la tranche du matériau revêtu R18 obtenu, est au moins de Hv₃₀ = 500 kg/mm², ce qui correspond à un gain de dureté d'un ordre de grandeur. L'épaisseur de dépôt après brossage à l'aide d'une brosse métallique a fait disparaître presque totalement la porosité ouverte du revêtement. Il ne reste qu'une porosité fermée de 15%.The M10 alloy, prepared and reduced to powder as above, was deposited, using a plasma torch used in Example 2, on a metallic copper plate. This plate had an average microhardness of Hv₃₀ = 50 ± 1 kg / mm². FIG. 16 shows that the hardness of the deposit, measured on the edge of the coated material R18 obtained, is at least Hv₃₀ = 500 kg / mm², which corresponds to a gain in hardness of an order of magnitude. The thickness of the deposit after brushing using a wire brush almost completely disappeared the open porosity of the coating. Only a closed porosity of 15% remains.

La comparaison de l'ensemble des caractéristiques des revêtements selon l'invention et des revêtements de l'art antérieur, et notamment l'index d'adhérence, le coefficient de frottement et la proportion de quasi-cristal pour les revêtements fait apparaître que le choix de matériaux présentant une forte proportion de phase quasi-cristalline permet d'obtenir des revêtements de meilleure qualité. Non seulement les revêtements ne masquent pas les bonnes propriétés des alliages de l'art antérieur, mais en outre ils présentent une bonne adhérence au substrat du fait de la stabilité en température de leur structure.A comparison of all the characteristics of the coatings according to the invention and of the coatings of the prior art, and in particular the adhesion index, the coefficient of friction and the proportion of quasi-crystal for the coatings shows that the choice of materials with a high proportion of quasi-crystalline phase makes it possible to obtain better quality coatings. The coatings not only do not mask the good properties of the alloys of the prior art, but also they exhibit good adhesion to the substrate due to the temperature stability of their structure.

Les revêtements selon l'invention sont appropriés à différents usages.The coatings according to the invention are suitable for different uses.

Lorsqu'ils sont obtenus avec une porosité ouverte importante, par exemple supérieure à 20% en volume, ils sont particulièrement utiles pour les applications nécessitant une lubrification. En effet, l'agent lubrifiant enduit sur le substrat revêtu d'un matériau selon l'invention imprègne les pores du revêtement. Lorsque la température du substrat s'élève en cours d'utilisation, il se produit un phénomène de ressuage. Cette propriété est utile pour les ustensiles de cuissson qui ne sont pas soumis au lavage à l'aide de détergents. Ainsi, les matériaux de revêtement selon l'invention sont particulièrement adaptés pour les grils, les crêpières. Leur grande dureté permet de les nettoyer par grattage, sans la nécessité de recourir à des détergents.When they are obtained with a large open porosity, for example greater than 20% by volume, they are particularly useful for applications requiring lubrication. In fact, the lubricating agent coated on the substrate coated with a material according to the invention permeates the pores of the coating. When the temperature of the substrate rises during use, a bleeding phenomenon occurs. This property is useful for cooking utensils that are not not subjected to washing with detergents. Thus, the coating materials according to the invention are particularly suitable for grills, crepe makers. Their great hardness allows them to be cleaned by scraping, without the need to use detergents.

Les matériaux selon l'invention ayant une porosité importante trouvent une autre application intéressante dans le domaine des paliers anti-friction.The materials according to the invention having a large porosity find another interesting application in the field of anti-friction bearings.

Lorsque leurs porosité ouverte est faible, soit en raison du procédé de dépôt du revêtement, soit à la suite d'un traitement de surface, les revêtements selon l'invention sont particulièrement adaptés à la réalisation de surfaces anti-usure (chassis d'armement aéroporté, chemises et pistons, semelles de fer à repasser) ou à la fabrication de surfaces de référence (par example pour les tables de machine-outil, pour des appareils de précision). Ils conviennent également pour divers ustensiles de cuisson sans matière grasse: pour ces ustensiles, plus la surface de cuisson est lisse, c'est-à-dire, plus la porosité est faible, moins les aliments auront tendance à adhérer en cours de cuisson.When their open porosity is low, either due to the coating deposition process or following a surface treatment, the coatings according to the invention are particularly suitable for the production of anti-wear surfaces (reinforcement frame airborne, jackets and pistons, soles of iron) or in the manufacture of reference surfaces (for example for machine tool tables, for precision devices). They are also suitable for various cooking utensils without fat: for these utensils, the smoother the cooking surface, that is to say, the lower the porosity, the less the food will tend to adhere during cooking.

Claims (13)

1. Matériau de revêtement en alliage d'aluminium, caractérisé en ce que: 1) il a une composition correspondant à la formule générale AlaCubFecXdIe, dans laquelle X représente un ou plusieurs éléments choisis parmi V, Mo, Ti, Zr, Nb, Cr, Mn, Ru, Rh, Ni, Mg, W, Si et les terres rares, I représente les impuretés d'élaboration inévitables, e≦2, 14≦b ≦30, 7≦c ≦20, 0 ≦d≦10, avec c+d≧ 10 et a+b+c+d+e=100% en nombre d'atomes.
2) il contient au moins 40% en masse d'une phase quasi-cristalline.
1. Coating material of aluminum alloy, characterized in that: 1) it has a composition corresponding to the general formula Al a Cu b Fe c X d I e , in which X represents one or more elements chosen from V, Mo, Ti, Zr, Nb, Cr, Mn, Ru, Rh, Ni, Mg, W, Si and the rare earths, I represents the inevitable processing impurities, e ≦ 2, 14 ≦ b ≦ 30, 7 ≦ c ≦ 20, 0 ≦ d ≦ 10, with c + d ≧ 10 and a + b + c + d + e = 100% in number of atoms.
2) it contains at least 40% by mass of a quasi-crystalline phase.
2. Matériau selon la revendication 1, caractérisé en ce que la phase quasi-cristalline est une phase icosaédrique.2. Material according to claim 1, characterized in that the quasi-crystalline phase is an icosahedral phase. 3. Matériau selon la revendication 1, caractérisé en ce que la phase quasi-cristalline est une phase décagonale.3. Material according to claim 1, characterized in that the quasi-crystalline phase is a decagonal phase. 4. Substrat revêtu d'un matériau selon l'une quelconque des revendications 1 à 3.4. Substrate coated with a material according to any one of claims 1 to 3. 5. Substrat selon la revendication 4, caractérisé en ce que le revêtement présente une porosité ouverte supérieure à 20%.5. Substrate according to claim 4, characterized in that the coating has an open porosity greater than 20%. 6. Substrat selon l'une des revendications 4 ou 5, caractérisé en ce que le matériau de revêtement a été déposé en phase vapeur.6. Substrate according to one of claims 4 or 5, characterized in that the coating material has been deposited in the vapor phase. 7. Substrat selon la revendication 4, caractérisé en ce que la porosité ouverte est inférieure ou égale à 20%.7. Substrate according to claim 4, characterized in that the open porosity is less than or equal to 20%. 8. Substrat selon la revendication 7, caractérisé en ce qu'il a été obtenu par traitement de la surface d'un revêtement ayant une porosité ouverte supérieure à 20%.8. Substrate according to claim 7, characterized in that it was obtained by treatment of the surface of a coating having an open porosity greater than 20%. 9. Substrat selon la revendication 7, caractérisé en ce que le matériau de revêtement a été appliqué par jet supersonique.9. Substrate according to claim 7, characterized in that the coating material has been applied by supersonic jet. 10. Application d'un substrat revêtu selon l'une des revendications 4 à 9, à la fabrication d'ustensiles et de dispositifs de cuisson.10. Application of a coated substrate according to one of claims 4 to 9 for the manufacture of utensils and cooking devices. 11. Application d'un substrat revêtu selon l'une des revendications 4 à 6 à la fabrication de paliers antifriction.11. Application of a coated substrate according to one of claims 4 to 6 to the manufacture of anti-friction bearings. 12. Application d'un substrat revêtu selon l'une des revendications 7 à 9 à la fabrication de surfaces anti-usure.12. Application of a coated substrate according to one of claims 7 to 9 to the manufacture of anti-wear surfaces. 13. Application d'un substrat revêtu selon la revendication 7 à la fabrication de surfaces de référence.13. Application of a coated substrate according to claim 7 for the manufacture of reference surfaces.
EP89402187A 1988-08-04 1989-08-02 Cladding materials for metal alloys and for metals Expired - Lifetime EP0356287B1 (en)

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FR2671808A1 (en) * 1991-01-18 1992-07-24 Centre Nat Rech Scient ALUMINUM ALLOYS WITH SPECIFIC PROPERTIES.
EP0504048A1 (en) * 1991-03-13 1992-09-16 Centre National De La Recherche Scientifique (Cnrs) Wire for coating by torch spraying and its use for depositing a quasi crystalline phase on a substrate
FR2685349A1 (en) * 1991-12-20 1993-06-25 Centre Nat Rech Scient THERMAL PROTECTION ELEMENT CONSISTING OF A QUASI-CRYSTALLINE ALUMINUM ALLOY.
EP0645464A2 (en) * 1993-09-29 1995-03-29 Tsuyoshi Masumoto Ultrafine particle of quasi-crystalline aluminum alloy and process for producing aggregate thereof
US5432011A (en) * 1991-01-18 1995-07-11 Centre National De La Recherche Scientifique Aluminum alloys, substrates coated with these alloys and their applications
EP0757114A1 (en) * 1995-07-31 1997-02-05 Gaz De France Quasicrystallic coating and process for coating
FR2745300A1 (en) * 1996-02-23 1997-08-29 Peugeot Protecting engine parts against wear and thermal shock
FR2766239A1 (en) * 1997-07-16 1999-01-22 Sagem High pressure direct fuel injector for i. c. engine
FR2840177A1 (en) 2002-05-30 2003-12-05 Seb Sa EASY-TO-CLEAN COOKING SURFACE AND HOUSEHOLD ARTICLE COMPRISING SUCH A SURFACE
WO2005083139A1 (en) * 2004-02-16 2005-09-09 Saint Gobain Centre De Recherches Et D'etudes Europeen Metal coating for a kitchen utensil
WO2008014531A1 (en) * 2006-08-02 2008-02-07 Miba Gleitlager Gmbh Anti-friction lacquer
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FR2671808A1 (en) * 1991-01-18 1992-07-24 Centre Nat Rech Scient ALUMINUM ALLOYS WITH SPECIFIC PROPERTIES.
WO1992013111A1 (en) * 1991-01-18 1992-08-06 Centre National De La Recherche Scientifique Aluminium alloys, substrates coated with same and their applications
US5652877A (en) * 1991-01-18 1997-07-29 Centre National De La Recherche Aluminum alloys, substrates coated with these alloys and their applications
US5432011A (en) * 1991-01-18 1995-07-11 Centre National De La Recherche Scientifique Aluminum alloys, substrates coated with these alloys and their applications
US5424127A (en) * 1991-03-13 1995-06-13 Dubois; Jean-Marie Ribbon for coating by torch spraying and its use for depositing a quasi-crystalline phase on a substrate
FR2673871A1 (en) * 1991-03-13 1992-09-18 Centre Nat Rech Scient CORD FOR PROJECTION COATING AT THE TORCH AND ITS USE FOR DEPOSITING A QUASI CRYSTALLINE PHASE OVER A SUBSTRATE.
EP0504048A1 (en) * 1991-03-13 1992-09-16 Centre National De La Recherche Scientifique (Cnrs) Wire for coating by torch spraying and its use for depositing a quasi crystalline phase on a substrate
US5571344A (en) * 1991-12-10 1996-11-05 Centre National De La Recherche Scientifique Heat protection element consisting of a quasicrystalline aluminum alloy
US5888661A (en) * 1991-12-20 1999-03-30 Centre National De La Recherche Scientifique Quasicrystalline aluminum heat protection element and thermal spray method to form elements
FR2685349A1 (en) * 1991-12-20 1993-06-25 Centre Nat Rech Scient THERMAL PROTECTION ELEMENT CONSISTING OF A QUASI-CRYSTALLINE ALUMINUM ALLOY.
US5649282A (en) * 1991-12-20 1997-07-15 Centre National De La Recherche Scientifique Heat protection element consisting of a quasicrystalline aluminum alloy
WO1993013237A1 (en) * 1991-12-20 1993-07-08 Centre National De La Recherche Scientifique Thermal protection element made of a quasicrystalline aluminium alloy
US6183887B1 (en) 1991-12-20 2001-02-06 Centre National De La Recherche Scientifique Heat protection element consisting of a quasicrystalline aluminum alloy
EP0645464A2 (en) * 1993-09-29 1995-03-29 Tsuyoshi Masumoto Ultrafine particle of quasi-crystalline aluminum alloy and process for producing aggregate thereof
EP0645464A3 (en) * 1993-09-29 1995-11-02 Tsuyoshi Masumoto Ultrafine particle of quasi-crystalline aluminum alloy and process for producing aggregate thereof.
EP0757114A1 (en) * 1995-07-31 1997-02-05 Gaz De France Quasicrystallic coating and process for coating
FR2737505A1 (en) * 1995-07-31 1997-02-07 Gaz De France COATING IN QUASI-CRYSTALLINE MATERIAL AND ITS DEPOSIT PROCESS
FR2745300A1 (en) * 1996-02-23 1997-08-29 Peugeot Protecting engine parts against wear and thermal shock
FR2766239A1 (en) * 1997-07-16 1999-01-22 Sagem High pressure direct fuel injector for i. c. engine
FR2840177A1 (en) 2002-05-30 2003-12-05 Seb Sa EASY-TO-CLEAN COOKING SURFACE AND HOUSEHOLD ARTICLE COMPRISING SUCH A SURFACE
WO2003102259A1 (en) 2002-05-30 2003-12-11 Seb S.A. Easy-clean cooking surface and electrical household appliance comprising such a surface
EP2316982A3 (en) * 2002-05-30 2016-04-27 Seb Sa Cooking surface which is easy to clean and household appliance having such a surface
WO2005083139A1 (en) * 2004-02-16 2005-09-09 Saint Gobain Centre De Recherches Et D'etudes Europeen Metal coating for a kitchen utensil
US7563517B2 (en) 2004-02-16 2009-07-21 Saint Gobain Centre de Recherches et d-Etudes European “Les Miroirs” Metal coating for a kitchen utensil
WO2008014531A1 (en) * 2006-08-02 2008-02-07 Miba Gleitlager Gmbh Anti-friction lacquer
US8324138B2 (en) 2006-08-02 2012-12-04 Miba Gleitlager Gmbh Anti-friction lacquer
CN109403771A (en) * 2017-08-17 2019-03-01 大同金属工业株式会社 The guide roller of vehicle sliding door
CN109403771B (en) * 2017-08-17 2020-09-25 大同金属工业株式会社 Guide roller of sliding door for vehicle

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JP2792701B2 (en) 1998-09-03

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