PROCESS FOR OBTAINING A METALLURGICAL BOND BETWEEN A METAL MATERIAL, OR A COMPOSITE MATERIAL HAVING A METAL MATRIX, AND A METAL CASTING OR A METAL-ALLOY CASTING

Abstract: Disclosed is a process for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting, or a metal alloy casting, which comprises carrying out a surface treatment on said material by means of the deposition of a thin layer of a metal, generally different from the metals contained in the material and in the casting, which is capable of increasing the wettability between the metal of the casting and the material, as well as the heat transfer coefficient between said two partners; and a step of casting around the same material, positioned inside a mould, of the metal, or of the metal alloy the same casting is constituted by.

Description: The present invention relates to a process for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting piece, or a metal-alloy casting according to the preamble of claim 1. In particular, such a process makes it possible predetermined regions of stationary, or moving, mechanical components to be reinforced by means of the introduction of inserts, or makes it also possible two or more cast pieces to be coupled with one another. The methods known from technical literature in order to generate a reinforced region inside a cast piece can be substantially reconducted to the following two kinds of procedures: Mechanical constriction of the insert by the solidified cast piece: this method uses the difference in thermal expansion between the cast piece and the insert. In this case, the bond is hence of non-metallurgical type: the obtained material is not continuous, and through the interface the seepage of corrosive agents can take place. The insert should be surrounded by the cast material, and therefore cannot be positioned at a corner of the end product. Infiltration, by means of the "squeeze casting" technique, of preformed pieces: according to this technique, an insert is not used, but, on the contrary, a preformed piece, made in general from ceramic fibres, and adequately positioned, is used, through which the cast material is infiltrated by means of the application of a high pressure. In this case, a bond between the cast material and the insert is not obtained; this is, on the contrary, a technique for preparing composite materials. On the other hand, the methods known from the prior art for generating a bond between a metal casting and another casting, or a composite material as for example disclosed in US-A- 384 1386, upon which the preamble of claim 1 is based, can all be reconducted to welding or brazing techniques; such operations require anyway on operating step to be carried out subsequently to the production of the cast pieces (or of the composite pieces). The present Applicant has found now that by means of a suitable surface treatment of the material (either a reinforcing material or a material to be coupled), a strong metallurgical bond can be obtained between the same material and the casting. In particular, the process according to the present invention, which could be given the name of "welding by casting" or "cast-welding", guarantees that all of the classic requirements of the welding operations are met: namely, the removal of the surface impurities and oxides, intimate contact and coalescence of the materials to be mutually bonded. However, this type of welding is extremely different from other methods, in that it takes place while the casting is being carried out. Furthermore, metals not easily coupled by means of other techniques can be bonded to each other by means of such a type of welding. The process according to the present invention for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting, or a metal-alloy casting is characterized by the features as laid out in the characterizing portion of claim 1. The metal material, which can be constituted by a single metal or by a metal alloy, or the metal-matrix composite can be, e.g., an insert for reinforcing predetermied regions of either stationary or moving mechanical components subject to wear, (such as guides, pistons, gearwheels, and so forth), or a cast piece to be coupled with one or more cast piece(s) on order to possibly constitute a complex shaped piece, which otherways cannot be obtained, or which can be difficultly obtained (owing to hindrances due to the geometry of the piece or to the type of material, or to a too high cost). The metal composite material and the cast material can have different compositions, and the therein contained metals can be preferably selected from the group consisting of Al, Zn, Pb, Mg, Cu, Sn, In, Ag, Au, It and their alloys. As hereinabove mentioned, the material can also be a composite having a metal matrix: such a type of material is constituted by a metal phase (or by a metal-alloy phase), which surrounds and bonds other phases, which constitute the reinforcement (powders or ceramic fibres). The reinforcement is endowed with high values of mechanical strength and hardness, and to it the stresses are transferred, which the matrix is submitted to; the matrix, in its turn, should display suitable characteristics as a function of the forecast application type. The reinforcement can be constituted by long or short ceramic fibres (Al₂O₃, SiC, C, BN, SiO₂, glass), or by ceramic "whiskers" (SiC, Si₃N₄, B₄C, Al₂O₃), or by non-metal powders (SiC, BN, Si₃N₄, B₄C, SiO₂, Al₂O₃, glass, graphite), or by metal fibres (Be, W, SiC-coated W, B₄C-coated W, steel). The methods for preparing the composited can be the following: Dispersion of the reinforcement throughout the matrix in the molten state; Dispersion of the reinforcement throughout the matrix in a partially solid state; Powder metallurgy; Fibre metallization; Layer compacting; Infiltration. The composite material can be obtained either directly, or by means of a subsequent mechanical machining. The metal which constitutes the thin layer to be deposited in a thickness preferably comprised within the range of from 10 to 200 nm on the surface of the metal material or the metal-matrix composite material, which thin-layer metal may be different from the metals contained in the material and in the casting, can be preferably selected from the group consisting of Au, Ag, Cu, Ni, Pt, Pd, Cr, W, Ir, Mo, Ta, Nb, Os, Re, Rh, Ru and Zr. The deposition of said thin layer can be preferably carried out by sputtering, or by means of an electrochemical deposition process. Any other known methods, of chemical, physical, etc., nature for generating surface coatings can be used as well: the methods of "plasma-spraying", laser-assisted deposition, thermal-evaporation deposition, magnetron-assisted deposition, CVD (Chemical Vapour Deposition), and the like, can be cited for exemplifying purposes. By using a proper coating, the liquid to be submitted to the casting process will be capable of wetting the metal, or metal-matrix composite, material, to a high enough exent in order to transfer heat to it, to wash away the oxide layer existing on the surface of said material and to form a direct bond with the material, in case of a metal material, or with the metal matrix, in case of a composite material. Once that the material is adequately cleaned, coated and positioned inside the mould, the operating parameters of the casting step have to be so adjusted, as to secure that a proper stream of overheated liquid laps the surfaces of the material. It is important that the position of the material be suitably selected and that the shape of the downwards ducts (feed ducts) and of the upwards ducts (outflow) inside the mould be so studied as to oblige the liquid metal to lap, wet and wash the walls of the material before becoming too cold. Summing-up, the matter is of keeping controlled the following three parameters: temperature of material preheating, metal (or alloy) casting temperature, flow conditions. In that way, an excellent metallurgical bond between the material and the cast material can be obtained. The metal materials can be obtained by means of techniques known from the prior art (e.g.: gravity casting, pressure casting, or "squeeze casting"), either, directly or with a subsequent processing step. Some examples are now given in order to better illustrate the invention. In no way such examples should be regarded as being limitative of the same invention: Example 1 The insert is constituted by an Al-Si alloy at 12% by weight of Si. The insert is coated with a thin gold layer by sputtering. The insert and the mould are pre-heated at the temperature of 300°C. The material which constitutes the casting is a ZA11C1 alloy (11% by weight of Al, 1% by weight of Cu, the balance to 100% by weight of Zn). The temperature of the cast material is of 625°C. The volume of cast material is of about 200 cm³. The material is cast in a slow enough way (10 cm³/second) through an orifice of 0.5 cm² of surface area from a height of about 10 cm above the upper edge of the mould, under a normal atmosphere. In figure 1: 1 is the graphite mould; 2 is the insert; 3 is the flowing direction of the casting stream; 4 is the tank. Result of the experimental test: excellent bond, with practically indistinguishable interface after an examination carried out under the optical microscope on a cross section, after polishing and metallographic etching, as one can see from Figure 2. The gray phase of Al-Si alloy results to be inside the ZA11C1 alloy, without any evidence of a planar interface, or of cracks. Example 2 The insert is a composite with a metal matrix constituted by ZA11C1 alloy (12% by weight of Al, 1% by weight of Cu, the balance to 100% by weight of Zn), the reinforcement is SiC powder at 15% by volume (average diameter 20µ); it is obtained by infiltration. The insert is coated with a thin gold layer by sputtering. The insert and the mould are pre-heated at the temperature of 300°C. The cast material is a ZA11C1 alloy. The temperature of the cast material is of 600°C. The volume of cast material is of about 200 cm³. The material is cast in a fast enough way (30 cm³/second) through an orifice of 1 cm² of surface area from a height of about 10 cm through a steel pipe, under an atmosphere of Ar. In figure 3: 1 is the mould; 2 is the insert; 3 is the flowing direction of the casting stream; 4 is the tank; 5 is the steel pipe. Result of the experimental test: excellent bond, like in the preceding example, as it can be seen from Figure 4. This microphotograph shows that, even at a high magnification, an interface between the cast material and the insert of the composite product cannot be identified. Example 3 The insert is a composite with a metal matrix constituted by an Al-Si alloy at 13% by weight of Si, the reinforcement is SiC powder at 50% by volume (average diameter 20µ). The insert is obtained by infiltration. The temperature of the insert and of the mould is of 300°C. The coating of the insert is obtained by means of the electrochemical deposition of Cu. The cast material is an Al-Si alloy at 13% by weight of Si. The temperature of the cast material is 650°C. The volume of cast material is of about 200 cm³, and said material is cast in a slow enough way (20 cm³/second) through an orifice of 0.75 cm² of surface area into the mould. In figure 5: 1 is the mould; 2 is the insert; 3 is the flowing direction of the casting stream; 4 is the tank. Result of the experimental test: excellent bond. From the obtained piece specimens were prepared, which were submitted to tensile stress tests. The tensile strength is higher than 200 MPa and the specimens undergo breakage either inside the interior of the composite portion, or inside the matrix, and they do never break at the interface. Example 4 Example 4 was carried out in the same way as Example 1, with the following exceptions: The insert is constituted by a composite with a metal matrix constituted by an Al-Si alloy (at 12% by weight of Si, 0.5% by weight of Mg, 0.3% by weight of Mn, with the balance to 100% being Al), to which Mg (2% by weight) is furthermore added. The reinforcement is constituted by SiC powder at 52% by volume. The insert is coated with a thin Cu layer, deposited by means of an electrochemical deposition method. The insert and the mould are pre-heated at 270°C. The cast material is a ZA27C2 alloy (an alloy consisting of a Zn-Al alloy at 27% by weight of Al and 2% by weight of Cu). The temperature of the cast material is of 560°C. The volume of cast material is of 200 cm³. Said material is cast in a slow enough way (10 cm³/second, through an orifice of 0.5 cm² of surface area) from a height of about 10 cm above the upper edge of the mould under a normal atmosphere. Result of the experimental test: excellent bond. Example 5 Example 5 was carried out in the same way as Example 2, with the following exceptions: The insert is constituted by a composite with a metal matrix constituted by a ZA27C2 alloy (27% by weight of Al, 2% by weight of Cu, balance to 100% by weight = Zn). The reinforcement is constituted by SiC powder at 50% by volume. The insert is coated with a thin Cu layer by sputtering, after carrying out a preliminary etching cycle inside the same sputtering equipment. The insert and the mould are pre-heated at 200°C. The cast material is an Al-Si alloy ( 0.36% by weight of Fe, 0.05% of Mn, 1.20% of Mg, 11.6% of Si, 1.21% of Cu, 0.05% of Zn, 0.02% of Ti, 1.13% of Ni, balance to 100 = Al), often used for manufacturing pistons. The temperature of the cast material is of 650°C. The volume of cast material is of about 150 cm³. Said material is cast into a mould in a fast enough way (30 cm³/second, through an orifice of about 1 cm² of surface area) from a height of 60 cm, through a steel pipe under an N₂ atmosphere. Result of the experimental test: excellent bond. Example 6 Example 6 was carried out in the same way as Example 3, with the following exceptions: The insert is constituted by a composite with a metal matrix constituted by an Al-Si alloy ( 0.36% by weight of Fe, 0.05% of Mn, 1.20% of Mg, 11.6% of Si, 1.21% of Cu, 1.13% of Ni, 0.05% of Zn, 0.02% of Ti). The reinforcement is constituted by SiC powder at 30% by volume. The insert is coated with a thin layer of Ag by sputtering. The temperature of the insert and of the mould is of 300°C. The cast material is a ZA11C1 alloy. The temperature of the cast material is of 650°C. The volume of cast material is of 150 cm³, and said material is cast in a slow enough way (20 cm³/second, through an orifice of 0.75 cm² of surface area). Result of the experimental test: excellent bond. The specimens submitted to the tensile stress tests gave a value of 200 MPa before the breakage occurred inside the alloy of the cast material, very far away from the interface.

Claims: Process for obtaining a metallurgical bond between: (a) a metal material , or a composite material having a metal matrix, said composite material being reinforced by a reinforcing material selected from long and short ceramic fibres, ceramic whiskers, non-metallic powders and metallic fibres, and (b) a metal- or a metal alloy casting, wherein the metals of (a) and (b) are selected from Al, Zn, Pb, Mg, Cu, Sn, In, Ag, Au, Ti and alloys thereof, comprising the steps of carrying out a surface treatment on (a) by depositing thereon a thin layer of a metal other than any of those contained in (a) and (b) , positioning (a) in a mould and casting therearound the metal- or metal alloy (b), characterized in that the metal other than those contained in (a) and (b) is selected from Au, Ag, Ni, Pt, Pd, Cr, W, Ir, Mo, Ta, Nb, Os, Re, Rh, Zr,the deposition of said thin layer takes place by a method selected from: sputtering; plasma spraying; laser assisted deposition; thermal-evaporation deposition; magnetron-assisted deposition, and chemical vapour deposition (CVD). Process according to Claim 1 , wherein the reinforcing ceramic fibres for the composite material (a) are selected from ceramic fibres of Al₂O₃, SiC, BN, SiO₂ and glass. Process according to Claim 1 , wherein the reinforcing whiskers for the composite material (a) are selected from whiskers of SiC, Si₃N₄, B₄C and Al₂O₃. Process according to Claim 1 , wherein the reinforcing non-metallic powders for the composite material (a) are selected from powdered SiC, BN, B₄C, Si₃N₄, SiO₂, Al₂O₃, glass and graphite. Process according to Claim 1 , wherein the reinforcing metallic fibres for the composite material (a) are selected from metallic fibres of Be, W, SiC-coated W, B₄C-coated W, or steel. Process according to Claim 1 , wherein the material (a) is produced by gravity casting,pressure casting or squeeze casting. Process according to Claim 1, wherein the material (b) is produced by gravity casting,pressure casting or squeeze casting. Process according to Claim 1 , wherein the composite material (b) having a metal matrix is produced by dispersing the reinforcing material in the matrix in the molten or the partially solid state, or by powder metallurgy, or fibre metalization, or layer-compacting or infiltration. Process according to Claim 8, further comprising a machining step of the as-produced material. Process according to Claim 1 , wherein the deposited thin layer of metal has a thickness of from 10 nm to 200 nm.

Inventors: GEDEON, STEVEN ANTONY, GUERRIERO, RENATO, TANGERINI, ILARIO
Applicants: TEMAV S.P.A.
Application year: 1989
Main classification: B22D19
IPC codes: B22D18, B22D19