EP3485051B1 - Alliage cuivre-nickel-étain, procédé de préparation et utilisation de celui-ci - Google Patents

Alliage cuivre-nickel-étain, procédé de préparation et utilisation de celui-ci Download PDF

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EP3485051B1
EP3485051B1 EP17736569.9A EP17736569A EP3485051B1 EP 3485051 B1 EP3485051 B1 EP 3485051B1 EP 17736569 A EP17736569 A EP 17736569A EP 3485051 B1 EP3485051 B1 EP 3485051B1
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copper
borides
nickel
silicides
phases
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EP3485051A1 (fr
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Kai Weber
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Wieland Werke AG
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Wieland Werke AG
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C9/00—Alloys based on copper
    • C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002—Castings of light metals
    • B22D21/005—Castings of light metals with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C9/00—Alloys based on copper
    • C22C9/02—Alloys based on copper with tin as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents

Definitions

  • the invention relates to a copper-nickel-tin alloy with excellent castability, hot workability and cold workability, high resistance to abrasive wear, adhesive wear and fretting wear and improved corrosion resistance and stress relaxation resistance according to the preamble of one of claims 1 or 2, a method their production according to the preamble of claims 9 or 10 and their use according to the preamble of claims 16 to 18.
  • the binary copper-tin alloys Due to their good strength properties, their good corrosion resistance and conductivity for heat and electricity, the binary copper-tin alloys are of great importance in mechanical engineering and vehicle construction as well as in many areas of electronics and electrical engineering.
  • This group of materials has a high resistance to abrasive wear.
  • the copper-tin alloys ensure good sliding properties and high fatigue strength, which is why they are extremely suitable for sliding elements in engine and vehicle construction as well as in general mechanical engineering.
  • the copper-nickel-tin alloys have compared to the binary copper-tin materials improved mechanical properties such as hardness, tensile strength and yield point.
  • the increase in the mechanical characteristics is achieved through the hardenability of the Cu-Ni-Sn alloys.
  • the precipitation processes are essential for the adjustment of the properties of this group of materials.
  • These copper alloys also include the copper-nickel-tin materials. Therefore, to ensure cold working of the as-cast condition of such alloys, a strip casting process with precise control of the solidification rate of the melt is recommended.
  • Dynamic friction wear also known as fretting in technical terms, is friction wear that occurs between oscillating contact surfaces.
  • fretting In addition to the geometric wear or volume wear of the components, the reaction with the surrounding medium leads to fretting corrosion.
  • the damage to the material can significantly reduce the local strength in the wear zone, in particular the fatigue strength. Fatigue cracks can emanate from the damaged component surface, leading to fatigue fractures/friction fractures. In the case of fretting corrosion, the fatigue strength of a component can fall well below the fatigue limit value of the material.
  • the mechanism of oscillating friction wear is significantly different from the types of sliding wear with unidirectional movement.
  • the effects of corrosion are particularly pronounced in the case of dynamic friction wear.
  • connection elements In motors and machines, electrical connectors are often placed in an environment in which they are subjected to mechanical vibrational movements. If the elements of a connection arrangement are located on different assemblies which, as a result of mechanical loads, carry out movements relative to one another, a corresponding relative movement of the connection elements can occur. These relative movements lead to oscillating wear and fretting corrosion of the contact zone of the connector. Microcracks form in this contact zone, which greatly reduces the fatigue strength of the connector material. A failure of the connector due to fatigue fracture can be the result. Furthermore, due to the fretting corrosion, there is an increase in the contact resistance.
  • a combination of the material properties of wear resistance, ductility and corrosion resistance is therefore decisive for sufficient resistance to dynamic friction wear/fretting corrosion/fretting.
  • the teaching disclosed in this publication specifies a particularly high P content of 0.2 to 0.6% by weight with a mandatory Si content of the alloy of 0.05 up to 0.15% by weight. This underlines the superficial demand for the self-flowing properties of the material. With this high P content, the hot workability of the alloy will be poor and the spinodal segregability of the structure will be insufficient.
  • the size of the hard particles precipitated in a copper-based alloy has a major impact on its wear resistance.
  • the element tin is not contained in this material. This material is applied to a suitable substrate by build-up welding as a wear protection layer.
  • the pamphlet U.S. 5,004,581A describes the same copper alloy as the previous one U.S. 4,818,307 A with an additional content of tin in the content range of 5 to 15% by weight and/or of zinc in the content range of 3 to 30% by weight.
  • the addition of Sn and/or zinc in particular increases the material's resistance to adhesive wear.
  • This material is also applied to a suitable substrate as a wear-resistant layer by means of build-up welding.
  • the copper alloy according to the publications U.S. 4,818,307 A and U.S. 5,004,581A due to the required size of the silicide formations/boride formations of the elements nickel and iron of 5 to 100 ⁇ m only have a very limited cold formability.
  • the publication discloses a precipitation-hardenable copper-nickel-tin alloy U.S. 5,041,176 A out.
  • This copper base alloy contains 0.1 to 10 wt% Ni, 0.1 to 10 wt% Sn, 0.05 to 5 wt% Si, 0.01 to 5 wt% Fe and 0.0001 to 1 % by weight of boron.
  • This material contains dispersely distributed intermetallic phases of the Ni-Si system.
  • the properties of the alloy are also explained using exemplary embodiments that have no Fe content.
  • alloying elements Zn, Mn, Mg, P and B are added to the melt of the alloy for deoxidation.
  • the elements Ti, Cr, Zr, Fe and Co have a grain-refining and strength-enhancing function.
  • alloying with metalloids such as boron, silicon and phosphorus By alloying with metalloids such as boron, silicon and phosphorus, the reduction in processing technology, which is important high base melting temperature. This is why these alloying additions are used in particular in the field of wear-resistant coating materials and high-temperature materials, which include, for example, the alloys of the Ni-Si-B and Ni-Cr-Si-B systems. In these materials, the alloying elements boron and silicon in particular are responsible for the strong reduction in the melting temperature of hard nickel-based alloys, which is why their use as self-fluxing hard nickel-based alloys becomes possible.
  • the silicon borides which are mostly present in the modifications SiB 3 , SiB 4 , SiB 6 and/or SiB n determined by the boron content, differ significantly from silicon in their properties. These silicon borides have a metallic character, which is why they are electrically conductive. They have an extraordinarily high temperature resistance and oxidation resistance.
  • the modification of SiB 6 which is preferred for sintered products, is used, for example, in the manufacture and processing of ceramics because of its very high hardness and its high abrasive wear resistance.
  • the usual wear-resistant hard alloys for surface coating consist of a relatively ductile matrix of the metals iron, cobalt and nickel with embedded silicides and borides as hard particles ( Knotek, O.; Lugscheider, E.; Reimann, H.: A contribution to the assessment of wear-resistant nickel-boron-silicon hard alloys. Journal of Materials Engineering 8 (1977) 10, pp. 331-335 ).
  • the wide use of hard alloys of the Ni-Cr-Si, Ni-Cr-B, Ni-B-Si and Ni-Cr-B-Si systems is based on the increase in wear resistance caused by these hard particles.
  • the Ni-B-Si alloys also contain the borides Ni 3 B and the Ni-Si borides/Ni silicoborides Ni 6 Si 2 B.
  • a certain inertia is also reported of silicide formation in the presence of the element boron.
  • Further investigations of the alloy system Ni-B-Si led to the detection of the high-melting Ni-Si borides Ni 6 Si 2 B and Ni 4.29 Si 2 B 1.43 ( Lugscheider, E.; Reimann, H.; Knotek, O.: The ternary system nickel-boron-silicon.
  • the element zinc is added to copper-nickel-tin alloys to lower the metal price. Functionally, the alloying element zinc causes the stronger formation of Sn-rich or Ni-Sn-rich phases from the melt. In addition, zinc increases the formation of precipitates in the Cu-Ni-Sn spinodal alloys.
  • a certain Pb content is added to the copper-nickel-tin alloys to improve the emergency running properties and for better machinability.
  • the invention is based on the object of providing a high-strength copper-nickel-tin alloy which has excellent hot workability over the entire range of the nickel content and tin content of 2 to 10% by weight in each case. It should be possible to use a starting material for hot forming that has been produced by means of conventional casting processes without the absolute necessity of carrying out spray compacting or thin-strip casting.
  • the copper-nickel-tin alloy After casting, the copper-nickel-tin alloy should be free of gas pores and shrinkage pores as well as stress cracks and be characterized by a structure with a uniform distribution of the tin-enriched phase components.
  • the structure of the copper-nickel-tin alloy should already contain intermetallic phases after casting. This is important so that the alloy already has high strength, high hardness and sufficient wear resistance in the cast state.
  • the as-cast state should already be characterized by high corrosion resistance.
  • the as-cast state of the copper-nickel-tin alloy should not first have to be homogenized by means of a suitable annealing treatment in order to be able to produce sufficient hot workability.
  • a fine-grained structure containing hard particles with high strength, high heat resistance, high hardness, high resistance to stress relaxation and corrosion, sufficient electrical conductivity and a high Degree of resistance to the mechanisms of Set sliding wear and oscillating friction wear which includes at least one annealing or at least one hot forming and/or cold forming in addition to at least one annealing, a fine-grained structure containing hard particles with high strength, high heat resistance, high hardness, high resistance to stress relaxation and corrosion, sufficient electrical conductivity and a high Degree of resistance to the mechanisms of Set sliding wear and oscillating friction wear.
  • the invention is represented by the features of one of claims 1 or 2 in relation to a copper-nickel-tin alloy, by the features of claims 9 or 10 in relation to a production method and by the features of claims 16 to 18 in relation to a use.
  • the further dependent claims relate to advantageous configurations and developments of the invention.
  • the first phase components and/or the second phase components are contained with at least 1% by volume in the cast structure of the alloy.
  • Segregations of this type are understood to mean accumulations of the first phase components and/or the second phase components in the cast structure, which are formed as grain boundary segregations which, when the casting is subjected to thermal and/or mechanical stress, cause damage to the structure in the form of cracks that can lead to fracture.
  • the structure is still free of gas pores, shrinkage pores, stress cracks and discontinuous precipitations of the (Cu, Ni)-Sn system.
  • the alloy is in the as-cast state.
  • the continuous precipitates of the (Cu,Ni)-Sn system are contained with at least 0.1% by volume in the structure of the further processed state of the alloy.
  • the structure is free of segregation.
  • segregations are accumulations of the first phase components and/or the second phase components in the structure, which are formed as grain boundary segregations, which damage the structure in cause cracks that can lead to breakage.
  • the structure of the alloy is free of gas pores, shrinkage pores and stress cracks. It should be emphasized as an essential feature of the invention that the microstructure in the further processed state is free of discontinuous precipitations of the (Cu,Ni)-Sn system.
  • the alloy is in the processed state.
  • the invention is based on the consideration that a copper-nickel-tin alloy with Si-containing and B-containing phases and with phases of the systems Ni-Si-B, Ni-B, Fe-B, Ni-P, Fe-P, Mg-P, Ni-Si, Mg-Si and is provided with other Fe-containing phases and Mg-containing phases.
  • These phases significantly improve the processing properties castability, hot workability and cold workability.
  • these phases improve the performance of the alloy by increasing strength and resistance to abrasive wear, adhesive wear and fretting wear.
  • These phases additionally improve corrosion resistance and stress relaxation resistance as other performance properties of the invention.
  • the copper-nickel-tin alloy according to the invention can be produced by means of the sand casting process, shell mold casting process, investment casting process, full mold casting process, die casting process, lost foam process and permanent mold casting process or with the aid of continuous or semi-continuous casting method are produced.
  • the use of process-technically complex and cost-intensive primary shaping techniques is possible, it is not mandatory for the production of the copper-nickel-tin alloy according to the invention Necessity.
  • the use of spray compacting or thin strip casting can be dispensed with.
  • the cast shapes of the copper-nickel-tin alloy according to the invention can be hot-formed directly over the entire range of Sn content and Ni content, for example by hot rolling, extrusion or forging, without carrying out a homogenization anneal that is absolutely necessary.
  • no complex forging processes or upsetting processes have to be carried out at elevated temperature in order to weld, ie close, pores and cracks in the material. This largely eliminates the processing restrictions that previously existed in the manufacture of semi-finished products and components made of copper-nickel-tin alloys.
  • the metallic matrix of the structure of the copper-nickel-tin alloy according to the invention consists in the as-cast state with increasing Sn content of the alloy, depending on the casting process, from increasing proportions of tin-enriched phases, which are distributed evenly in the copper mixed crystal ( ⁇ -phase). are.
  • phase components can be specified with the molecular formula Cu h Ni k Sn m and have a ratio (h+k)/m of the element content in atom % of 2 to 6.
  • the second phase components can be specified with the molecular formula Cu p Ni r Sn s and have a ratio (p+r)/s of the element content in atom % of 10 to 15.
  • the alloy according to the invention is characterized by Si-containing and B-containing Phases that can be divided into two groups.
  • the first group relates to the Si-containing and B-containing phases, which are in the form of silicon borides and can be present in the modifications SiB 3 , SiB 4 , SiB 6 and SiB n .
  • the "n" in the compound SiB n indicates the high solubility of the element boron in the silicon lattice.
  • the second group of Si-containing and B-containing phases relates to the silicate compounds of borosilicates and/or borophosphorus silicates.
  • the structural proportion of the Si-containing and B-containing phases which are in the form of silicon borides and borosilicates and/or borophosphorus silicates, is a minimum of 0.01 and a maximum of 10% by volume.
  • the Ni-Si borides and the Ni borides are each contained in the structure at 1 to 15% by volume.
  • the Ni phosphides and Ni silicides are each present with a structural proportion of 1 to 5% by volume.
  • the Fe borides, Fe phosphides, Mg phosphides and the Fe silicides and/or Fe-rich particles each account for 0.1 to 5% by volume of the structure.
  • the Mg silicides and the Cu-containing and Mg-containing phases and/or Cu-containing and Sn-containing and Mg-containing phases are each present in the structure with 0.1 to 5% by volume.
  • crystallization nuclei These phases are referred to below as crystallization nuclei.
  • the element tin and/or the first phase constituents and/or the second phase constituents of the metallic matrix preferentially crystallize in the regions of the nuclei, whereby the nuclei are coated by tin and/or the first phase constituents and/or the second phase constituents.
  • Hard particles This encased by tin and / or the first phase components and / or the second phase components nuclei are hereinafter referred to as Hard particles called first class.
  • the hard particles of the first class have a size of less than 80 ⁇ m.
  • the size of the first-class hard particles is less than 50 ⁇ m.
  • the island-like arrangement of the first phase components and/or the second phase components changes into a network-like arrangement in the structure.
  • the first phase components can have a proportion of up to 30% by volume.
  • the second phase components take on a structural proportion of up to 20% by volume.
  • the first phase components and/or the second phase components are contained with at least 1% by volume in the as-cast structure of the alloy.
  • the conventional copper-nickel-tin alloys have a relatively large solidification interval. This large solidification interval increases the risk of gas absorption during casting and causes uneven, coarse, mostly dendritic crystallization of the melt. The result is often gas pores and coarse Sn-rich segregations, at the phase boundary of which shrinkage pores and stress cracks often occur. In this group of materials, the Sn-rich segregations also occur preferentially at the grain boundaries.
  • the combined content of boron, silicon and phosphorus activates various processes in the melt of the alloy according to the invention, which significantly change its solidification behavior compared to conventional copper-nickel-tin alloys.
  • the elements boron, silicon and phosphorus perform a deoxidizing function in the melt of the invention.
  • By adding boron and silicon it is possible to reduce the phosphorus content without reducing the intensity of the deoxidation of the melt.
  • This measure makes it possible to suppress the disadvantageous effects of sufficient deoxidation of the melt by means of a phosphorus additive.
  • a high P content would further extend the already very large solidification interval of the copper-nickel-tin alloy, which would increase the susceptibility to porosity and segregation of this type of material.
  • the adverse effects of adding phosphorus are reduced by limiting the P content in the alloy of the present invention to the range of 0.004 to 0.3 wt%.
  • the cast state of the invention has a very uniform structure with a fine distribution of the individual phase components.
  • segregations enriched with tin do not occur in the alloy according to the invention, particularly at the grain boundaries.
  • the elements boron, silicon and phosphorus bring about a reduction in the metal oxides.
  • the elements are oxidized themselves, mostly rise to the surface of the castings and form there as boron silicates and/or boron phosphorus silicates as well as phosphorus silicates a protective layer that protects the castings from gas absorption.
  • Extraordinarily smooth surfaces of the castings made from the alloy according to the invention were found, which indicate the formation of such a protective layer.
  • the structure of the as-cast state of the invention was also free of gas pores over the entire cross-section of the cast parts.
  • a basic idea of the invention is the transfer of the effect of boron silicates, boron phosphorus silicates and phosphorus silicates with regard to the adjustment of the different thermal expansion coefficients of the joining partners during diffusion soldering to the processes during casting, hot forming and thermal treatment of the copper-nickel-tin materials. Due to the wide solidification interval of these alloys, large mechanical stresses occur between the staggered crystallizing Sn-poor and Sn-rich structural areas, which can lead to cracks and pores. Furthermore, these damage characteristics can also occur during hot forming and high-temperature annealing of copper-nickel-tin alloys due to the different hot forming behavior and the different thermal expansion coefficients of the Sn-poor and Sn-rich microstructure components.
  • the combined addition of boron, silicon and phosphorus to the copper-nickel-tin alloy according to the invention causes, on the one hand, a structure with a uniform island-like and/or network-like distribution of the first phase components and/or the second phase components during the solidification of the melt by means of the effect of the crystallization nuclei phase components of metallic matrix.
  • the Si-containing and B-containing phases formed during solidification of the melt which are in the form of boron silicates and/or boron phosphorus silicates, ensure, together with the phosphorus silicates, the necessary adjustment of the thermal expansion coefficients of the first phase components and/or the second Phase components and the copper mixed crystal of the metallic matrix. This prevents the formation of pores and stress cracks between the phases with different Sn contents.
  • the alloy content of the copper-nickel-tin alloy according to the invention also causes a significant change in the grain structure in the cast state. It could be determined that a substructure with a grain size of the subgrains of less than 30 ⁇ m is formed in the primary cast structure.
  • the alloy according to the invention can be subjected to further processing by annealing or by hot working and/or cold working in addition to at least one annealing.
  • One possibility for further processing of the copper-nickel-tin alloy according to the invention consists in converting the castings into the final shape with the required properties by means of at least one cold forming together with at least one annealing.
  • the alloy according to the invention already has high strength in the cast state. As a result, the castings have lower cold formability, which makes further processing more difficult. For this reason, carrying out a homogenization annealing of the castings before cold forming has proved to be a good idea proven beneficial.
  • accelerated cooling after the homogenization annealing processes has proven to be advantageous. It has been shown that due to the inertia of the precipitation mechanisms and segregation mechanisms, cooling methods with a lower cooling rate can be used in addition to water quenching. The use of accelerated air cooling has thus proven to be just as practicable in order to sufficiently reduce the effect of the precipitation processes and demixing processes in the structure, which increase hardness and increase strength, during the homogenization annealing of the invention.
  • the outstanding effect of the crystallization nuclei for the recrystallization of the structure of the invention can be seen in the structure, which can be adjusted after cold forming by means of annealing in the temperature range from 170 to 880° C. and an annealing time of between 10 minutes and 6 hours.
  • the extraordinarily fine structure of the recrystallized alloy enables further cold forming steps with a degree of forming ⁇ of mostly over 70%. In this way, extremely high-strength states of the alloy can be produced.
  • the level of the parameter R p0.2 is significant for the sliding elements and guide elements. Furthermore, a high value of R p0.2 is a prerequisite for the necessary spring properties of connectors in electronics and electrical engineering.
  • the structure of the alloy according to the invention remains free of discontinuous precipitations of the (Cu,Ni)-Sn system, regardless of the degree of cold working. It was thus possible to establish for particularly advantageous embodiments of the invention that the microstructure of the invention remains free of discontinuous precipitations of the (Cu,Ni)—Sn system even with extremely small degrees of cold deformation of less than 20%.
  • the conventional, spinodally separable Cu-Ni-Sn materials are considered to be very difficult or impossible to hot-work.
  • the effect of the crystallization nuclei could also be observed during the process of hot working the copper-nickel-tin alloy according to the invention.
  • the crystallization nuclei are primarily to be held responsible for the fact that the dynamic recrystallization takes place favorably during hot forming of the alloy according to the invention in the temperature range from 600 to 880.degree. This results in a further increase in the uniformity and fine-grained structure.
  • the semi-finished products and components can be cooled after hot forming in calmed or accelerated air or with water.
  • an extraordinarily smooth surface of the parts could also be determined after the hot forming of the castings.
  • Si-containing and B-containing phases which are in the form of boron silicates and/or boron phosphorus silicates, and of phosphorus silicates, which takes place in the material during hot forming.
  • the silicates, together with the crystallization nuclei, also cause the different thermal expansion coefficients of the phases of the metallic matrix of the invention to be equalized during hot working.
  • the surface of the hot-formed parts and the structure were free of cracks and pores, just as they were after casting.
  • At least one annealing treatment of the cast state and/or the hot-formed state of the invention can be carried out in the temperature range from 170 to 880°C for a period of 10 minutes to 6 hours, alternatively with cooling in calmed or accelerated air or with water.
  • One aspect of the invention relates to an advantageous method for further processing the as-cast state or the hot-formed state or the annealed as-cast state or the annealed hot-formed state, which comprises carrying out at least one cold-forming step.
  • At least one annealing treatment of the cold-formed state of the invention can preferably be carried out in the temperature range from 170 to 880° C. for a period of 10 minutes to 6 hours, alternatively with cooling in calmed or accelerated air or with water.
  • Stress relief annealing/ageing annealing can advantageously be carried out in the temperature range from 170 to 550° C. with a duration of 0.5 to 8 hours.
  • crystallization nuclei encased by precipitations of the (Cu,Ni)-Sn system, are referred to below as second-class hard particles.
  • the size of the second-class hard particles decreases in comparison to the size of the first-class hard particles.
  • there is progressive comminution of the hard particles of the second class since these, as the hardest components of the alloy, cannot support the change in shape of the surrounding metallic matrix.
  • the resulting second-class hard particles and/or the resulting segments of the second-class hard particles have a size of less than 40 ⁇ m to even less than 5 ⁇ m, depending on the degree of cold forming.
  • the Ni content and the Sn content of the invention range between 2.0 and 10.0% by weight.
  • a Ni content and/or a Sn content of less than 2.0% by weight would result in insufficient strength and hardness values.
  • the running properties of the alloy would be insufficient under a sliding load.
  • the alloy's resistance to abrasive and adhesive wear would not meet the requirements.
  • With a Ni content and/or a Sn content of more than 10.0% by weight the toughness properties of the alloy according to the invention would deteriorate rapidly, as a result of which the dynamic load capacity of the components made from the material is reduced.
  • the content of nickel and tin in the range of 3.0 to 9.0 wt. In this respect, the range of 4.0 to 8.0% by weight each for the content of the elements nickel and tin is particularly preferred for the invention.
  • Ni-containing and Sn-containing copper materials that the degree of spinodal segregation of the structure increases with an increasing Ni/Sn ratio of the element contents in % by weight of the elements nickel and tin. This is valid for a Ni content and a Sn content from about 2% by weight.
  • the mechanism of precipitation formation in the (Cu,Ni)-Sn system becomes more important, which leads to a reduction in the proportion of the spinodally segregated microstructure.
  • One consequence is, in particular, a more pronounced formation of discontinuous precipitations of the (Cu,Ni)-Sn system as the Ni/Sn ratio decreases.
  • One of the essential features of the copper-nickel-tin alloy according to the invention is the decisive suppression of the influence of the Ni/Sn ratio on the formation of discontinuous precipitations in the structure.
  • the microstructure of the invention largely independent of the Ni/Sn ratio and independent of the aging conditions, there is no precipitation of discontinuous precipitates of the (Cu,Ni)-Sn system.
  • the continuous precipitates of the (Cu,Ni)-Sn system are contained with at least 0.1% by volume in the structure of the further processed state of the alloy.
  • the element iron is added to the alloy according to the invention at 0.01 to 1.0% by weight. Iron contributes to increasing the proportion of crystallization nuclei and thus supports the fine-grain formation of the structure during the casting process.
  • the Fe-containing hard particles in the structure increase the strength, hardness and wear resistance of the alloy. If the Fe content is below 0.01% by weight, these effects on the structure and the properties of the alloy are only observed to an insufficient extent. If the Fe content exceeds 1.0% by weight, the structure increasingly contains cluster-like accumulations of Fe-rich particles. The Fe content of these clusters would only be available to a lesser extent for the formation of crystallization nuclei and hard particles. In addition, the toughness properties of the invention would deteriorate. An Fe content of 0.02 to 0.6% by weight is advantageous. An Fe content in the range from 0.06 to 0.4% by weight is preferred.
  • Ni-Fe-Si borides Due to the similarity relationship between the elements nickel and iron, Fe-Si borides and/or Ni-Fe-Si borides can also form in the structure of the alloy according to the invention in addition to the Ni-Si borides.
  • the structure of the invention also contains other Fe-containing phases.
  • these other Fe-containing phases are present as Fe silicides and/or as Fe-rich particles structure.
  • the element magnesium is added to the alloy according to the invention at 0.01 to 0.8% by weight.
  • Magnesium contributes to increasing the proportion of crystallization nuclei and thus supports the uniform formation of the structure during the casting process.
  • the Mg-containing hard particles in the structure increase the strength, hardness and wear resistance of the alloy. If the Mg content is below 0.01% by weight, these effects on the structure and the properties of the alloy are observed to an insufficient extent. When the Mg content exceeds 0.8% by weight, castability of the alloy deteriorates. In addition, the toughness properties of the alloy would deteriorate.
  • An Mg content of 0.05 to 0.6% by weight is advantageous.
  • a Mg content of 0.1 to 0.4% by weight is particularly preferred.
  • the structure of the invention also contains other Mg-containing phases.
  • Mg borides can form as further Mg-containing phases.
  • Mg borides can be present in the modifications MgB 2 and/or MgB 12 with a proportion of 0.1 to 5% by volume in the structure as hard particles of the first and second class.
  • Cu-containing and Mg-containing phases are also present in the structure of the alloy according to the invention as further Mg-containing phases.
  • these phases can be partially or fully replaced by Cu-containing and Sn-containing and Mg-containing phases.
  • Cu-containing and Mg-containing phases and/or Cu-containing and Sn-containing and Mg-containing phases are present in the structure of the copper-nickel-tin alloy according to the invention.
  • the effect of the crystallization nuclei during the solidification/cooling of the melt, the effect of the crystallization nuclei as recrystallization nuclei and the effect of the silicate-based phases for the purpose of wear protection and corrosion protection can only reach a technically significant level in the alloy according to the invention if the silicon content is at least 0 .01% by weight and the boron content is at least 0.002% by weight. On the other hand, if the Si content exceeds 1.5% by weight and/or the B content exceeds 0.45% by weight, the casting performance deteriorates. The excessively high content of crystallization nuclei would make the melt significantly more viscous. In addition, reduced toughness properties of the alloy according to the invention would result.
  • the range for the Si content within the limits of 0.05 to 0.9% by weight is rated as advantageous.
  • a silicon content of 0.1 to 0.6% by weight has proven to be particularly advantageous.
  • a content of 0.01 to 0.4% by weight is considered advantageous for the element boron.
  • a boron content of 0.02 to 0.3% by weight has proven particularly advantageous.
  • a lower limit for the element ratio of the elements silicon and boron has proven to be important in order to ensure a sufficient content of Ni-Si borides and of phases containing Si and B, which are in the form of borosilicates and/or borophosphorus silicates. For this reason, the minimum Si/B ratio of the element contents of the elements silicon and boron in % by weight of the alloy according to the invention is 0.4.
  • the minimum Si/B ratio of the element contents of the elements silicon and boron in % by weight of 0.8 is advantageous for the alloy according to the invention.
  • the minimum Si/B ratio of the element contents of the elements silicon and boron in % by weight of 1 is preferred.
  • Important for another important feature of the invention is the determination of an upper limit of 8 for the Si/B ratio of the element contents of the elements silicon and boron in % by weight. After casting, parts of the silicon are dissolved in the metallic matrix and bound in the hard particles of the first class.
  • the maximum Si/B ratio of the element contents of the elements silicon and boron in wt to be reduced to below 3 ⁇ m. Furthermore, this limits the content of silicides. Limiting the Si/B ratio of the element contents of the elements silicon and boron in % by weight to the maximum value of 6 has proven to be particularly advantageous in this regard.
  • the precipitation of the crystallization nuclei influences the viscosity of the melt of the alloy according to the invention. This circumstance underlines why the addition of phosphorus must not be dispensed with. Phosphorus causes the melt to be sufficiently thin despite the crystallization nuclei, which is of great importance for the castability of the invention.
  • the phosphorus content of the alloy according to the invention is 0.004 to 0.3% by weight.
  • the P content no longer contributes to ensuring sufficient castability of the invention. If the phosphorus content of the alloy assumes values above 0.3% by weight, then on the one hand an excessive Ni content is bound in the form of phosphides, which reduces the spinodal segregability of the structure. On the other hand, with a P content above 0.3% by weight, the hot workability of the invention would deteriorate significantly. For this reason, a P content of 0.01 to 0.3% by weight has proven particularly advantageous. A P content in the range from 0.02 to 0.2% by weight is preferred.
  • the alloying element phosphorus is very important for another reason. Together with the required maximum Si/B ratio of the element contents of the elements silicon and boron in % by weight of 8, it is due to the phosphorus content of the alloy that Ni phosphides, Fe phosphides, Mg Phosphides, Ni silicides, Fe silicides and/or Fe-rich particles, Mg silicides and Cu-containing and Mg-containing phases and/or Cu-containing and Sn-containing and Mg-containing phases, individually and/or are present as addition compounds and/or mixed compounds and are encased by precipitations of the (Cu, Ni)-Sn system, with a maximum size of 3 ⁇ m and with a content of 2 to 35% by volume in the structure.
  • the hard particles of the third class even have a size of less than 1 ⁇ m.
  • these third-class hard particles supplement the second-class hard particles in their function as wear carriers. They increase the strength and hardness of the metallic matrix and thus improve the resistance of the alloy to abrasive wear. On the other hand, the third-class hard particles increase the alloy's resistance to adhesive wear. Finally, these third-class hard particles bring about a significant increase in the high-temperature strength and the stress relaxation resistance of the alloy according to the invention. This represents an important prerequisite for the use of the alloy according to the invention, in particular for sliding elements and components and connecting elements in electronics/electrical engineering.
  • the alloy according to the invention Due to the content of hard particles of the first class in the structure of the cast state and of hard particles of the second and third class in the structure of the further processed state, the alloy according to the invention has the character of a precipitation-hardenable material.
  • the invention corresponds to a precipitation hardenable and spinodally demixable copper-nickel-tin alloy.
  • the sum of the element contents of the elements is silicon, boron and phosphorus advantageously at least 0.25% by weight.
  • the cast variant and the further processed variant of the alloy according to the invention can contain the following optional elements:
  • the element cobalt can be added to the copper-nickel-tin alloy according to the invention in a content of up to 2.0% by weight. Due to the similarity relationship between the elements nickel, iron and cobalt and due to the Si-boride-forming, boride-forming, silicide-forming and phosphide-forming properties of cobalt with regard to nickel and iron, the alloying element cobalt can be added to participate in the formation of crystallization nuclei and hard particles first, second and third class of the alloy. Thereby, the Ni content bound in the hard particles can be reduced.
  • Ni content that is effectively available in the metallic matrix for the spinodal segregation of the structure increases.
  • Advantagely 0.1 to 2.0% by weight of Co it is thus possible to increase the strength and hardness of the invention considerably.
  • the copper-nickel-tin alloy according to the invention can have small amounts of lead, which are above the impurity limit, up to a maximum of 0.25% by weight.
  • the copper-nickel-tin alloy is free of lead except for any unavoidable impurities, which means that current environmental standards are met.
  • lead contents of up to a maximum of 0.1% by weight of Pb are contemplated.
  • Si-containing and B-containing phases which are in the form of borosilicates and/or boron phosphorus silicates, as well as phosphorus silicates, not only leads to a significant reduction in the content of pores and cracks in the structure of the alloy according to the invention. Together with the Mg oxides, these silicate-based phases also assume the role of a wear-resistant and anti-corrosive coating on the components.
  • the alloying element tin contributes to the formation of a so-called tribolayer between the sliding partners. This mechanism is particularly important under mixed friction conditions when the emergency running properties of a material are more important.
  • the tribological layer leads to a reduction in the purely metallic contact surface between the sliding partners, which prevents the elements from welding or seizing.
  • the parts made of the alloy according to the invention form, similar to casting and hot forming, phases containing Si and B, which are in the form of boron silicates and/or boron phosphorus silicates, as well as phosphorus silicates .
  • phases containing Si and B which are in the form of boron silicates and/or boron phosphorus silicates, as well as phosphorus silicates .
  • the alloy of the invention ensures a combination of Features Wear resistance and corrosion resistance.
  • This combination of properties leads to a high resistance to the mechanisms of sliding wear, as required, and to a high material resistance to fretting corrosion.
  • the invention is excellently suited for use as a sliding element and plug connector, since it has a high degree of resistance to sliding wear and oscillating wear, so-called fretting.
  • the hard particles of the third class make a significant contribution to increasing the fatigue strength.
  • the third-class hard particles, together with the second-class hard particles, represent obstacles to the propagation of fatigue cracks, which can be introduced into the stressed component, particularly in the case of dynamic friction wear.
  • the hard particles of the second and third class supplement in particular the anti-wear and anti-corrosion effect of the Si-containing and B-containing phases, which are designed as boron silicates and/or boron phosphorus silicates, as well as the phosphorus silicates and the Mg oxides with regard to increasing the resistance of the alloy according to the invention compared to oscillating wear, so-called fretting.
  • Si-containing and B-containing phases which are designed as boron silicates and/or boron phosphorus silicates, as well as the phosphorus silicates and the Mg oxides
  • High temperature strength and stress relaxation resistance are other important properties of an alloy used in higher temperature applications.
  • a high density of fine precipitates is considered to be advantageous in order to ensure sufficiently high heat resistance and stress relaxation resistance.
  • such precipitations are the hard particles of the third class and the continuous precipitations of the (Cu,Ni)—Sn system.
  • the alloy according to the invention Due to the uniform and fine-grained structure with largely no pores, no cracks and no segregation and the content of first-class hard particles, the alloy according to the invention has a high degree of strength, hardness, ductility, complex wear resistance and corrosion resistance even in the cast state.
  • This combination of properties means that sliding elements and guide elements can be produced from the cast format.
  • the cast state of the invention can also be used for the production of fitting housings and housings of water pumps, oil pumps and fuel pumps.
  • the alloy of the present invention can be used for propellers, blades, propellers and hubs for shipbuilding.
  • the further processed variant of the invention can be used for areas of application with a particularly strong, complex and/or dynamic component stress.
  • the invention is suitable for the metal objects in constructions for the rearing of organisms living in sea water (aquaculture). Furthermore, pipes, seals and connecting bolts which are required in the maritime and chemical industries can be produced from the invention.
  • cymbals of high quality have so far been made from mostly tin-containing copper alloys by means of hot forming and at least one annealing before they are usually put into the be brought to final shape. The basins are then annealed again before their final machining takes place.
  • the production of the different variants of the cymbal eg ride cymbal, hi-hat, crash cymbal, China cymbal, splash cymbal and effect cymbal
  • different structural proportions of the phases of the metallic matrix and the different hard particles can be adjusted in a very wide range. In this way it is already possible to influence the sound of the cymbals on the alloy side.
  • the invention can be used in particular for the production of composite plain bearings in order to be applied to a composite partner by means of a joining method. It is thus possible to produce a composite between disks, plates or strips of the invention and steel cylinders or steel strips, preferably made of heat-treated steel, by means of forging, soldering or welding with the optional implementation of at least one annealing in the temperature range from 170 to 880°C.
  • composite bearing shells or composite bearing bushes can be produced by roll-bonding, inductive or conductive roll-bonding or by laser roll-bonding, also with the optional implementation of at least one annealing in the temperature range from 170 to 880°C.
  • high-performance composite sliding elements such as composite bearing shells or composite bearing bushes can also be produced as a three-layer system, with a bearing back made of steel, the actual bearing made of the alloy according to the invention and the overlay made of tin or the Sn-rich coating.
  • This multi-layer system has a particularly advantageous effect on the adaptability and running-in ability of the plain bearing and improves the embedding ability of foreign particles and abrasive particles, whereby there is no damage caused by the layer composite system being broken up as a result of pore formation and cracking in the boundary area of the individual layers.
  • the great potential of copper-nickel-tin materials can also be used for the field of tin-plated components, line elements, guide elements and connecting elements in electronics and electrical engineering by using the alloy according to the invention.
  • the structure of the invention reduces the damage mechanism of pore formation and cracking in the boundary area between the alloy according to the invention and the tinning, even at elevated temperatures, which counteracts an increase in the electrical contact resistance of the components or even detachment of the tinning.
  • the different hard particles serve as chip breakers.
  • the resulting short crumbly chips and/or tangled chips facilitate machinability, which is why the semi-finished products and components from the cast state and the further processed state of the alloy according to the invention have better machinability.
  • the chemical composition of the exemplary embodiment A and of the reference material R is shown in Table 1.
  • the embodiment A is characterized by an Ni content of 6.19% by weight, an Sn content of 5.78% by weight, an Mg content of 0.30% by weight, an Fe content of 0 20% by weight, an Si content of 0.29% by weight, a B content of 0.12% by weight, a P content of 0.12% by weight and the remainder being copper marked.
  • the reference material R a conventional copper-nickel-tin alloy, has a Ni content of 5.78% by weight, an Sn content of 5.75% by weight and a P content of 0.032% by weight. % and a remainder of copper.
  • the structure of the continuously cast plates of the reference material R shows gas and shrinkage pores as well as Sn-rich segregations, especially at the grain boundaries.
  • the continuous casting of the exemplary embodiment A has a uniformly solidified, pore-free and segregation-free structure due to the effect of the crystallization nuclei.
  • the metallic matrix of the as-cast state of the exemplary embodiment A consists of a copper mixed crystal with, based on the overall structure, approx. 10 to 15% by volume of island-shaped embedded first phase components, which can be specified with the empirical formula Cu h Ni k Sn m and a ratio (h+k)/m of the element contents in atomic % from 2 to 6.
  • the compounds CuNi 14 Sn 23 and CuNi 9 Sn 20 with a ratio (h+k)/m of 3.4 and 4 could be determined.
  • the metallic matrix with, based on the overall structure about 5 to 10% by volume of second phase components are embedded in islands, which can be specified with the molecular formula Cu p Ni r Sn s and a ratio (p + r) / s of Have element contents in atomic percent from 10 to 15.
  • the compounds CuNi 3 Sn 8 and CuNi 4 Sn 7 with a ratio (p+r)/s of 11.5 and 13.3 were detected.
  • the first and second phase components of the metallic matrix are predominantly crystallized in the area of the crystallization nuclei and encase them.
  • the analysis of the first-class hard particles in the cast state of exemplary embodiment A gave indications of the compound SiB 6 as a representative of the Si-containing and B-containing phases, of Ni 6 Si 2 B as a representative of the Ni-Si borides, of Ni 3 B as a representatives of the Ni borides, to FeB as a representative of the Fe borides, to Ni 3 P as a representative of the Ni phosphides, to Fe 2 P as a representative of the Fe phosphides, to Mg 3 P 2 as a representative of the Mg phosphides Ni 2 Si as a representative of the Ni silicides, on Fe-rich Particles, on Mg 2 Si as a representative of the Mg silicides and on Cu 4 SnMg as a representative of the Cu-containing and Sn-containing and Mg-containing phases, which are present individually and/or as addition compounds and/or mixed compounds in the structure.
  • these hard particles are encased by tin and/or the first phase components and
  • Example A During the casting process of Example A, a substructure was formed in the primary casting grains. In the cast structure of embodiment A of the invention, these sub-grains have a grain size of less than 10 ⁇ m. As a result of the sub-grain structure and the hard particles precipitated in the structure of exemplary embodiment A of the invention, the hardness HB of the as-cast state of 131 is significantly higher than the hardness of 94 HB of the continuously cast R (Table 2).
  • Tab. 2 Also shown in Tab. 2 are the hardness values that were determined on the continuously cast alloys A and R aged at 400°C for a period of 3 hours.
  • the increase in hardness from 94 to 145 HB is greatest for the reference material R.
  • the hardening is particularly due to thermally activated segregation of the Sn-rich and Ni-Sn-rich phase in the structure.
  • the phase components enriched with tin are separated out in the structure of exemplary embodiment A in a much finer way in the area of the hard particles. For this reason, the hardness does not increase so markedly from 131 to 146 HB.
  • One aim of the invention is to retain the good cold workability of conventional copper-nickel-tin alloys despite the introduction of hard particles.
  • Production program 1 according to Table 3 was carried out to check the degree of achievement of this goal. This production program consisted of a cycle of cold forming and annealing, with the cold rolling steps being carried out with the maximum possible degree of cold forming.
  • the structure of the further processed exemplary embodiment A contains the hard particles of the second class (in 3 labeled 3).
  • the size of the third-class hard particles of less than 3 ⁇ m is characteristic of the further processed alloy according to the invention.
  • the further processed exemplary embodiment A of the invention after aging at 450° C., it is even less than 1 ⁇ m (in 4 marked 5).
  • This production program 2 pursued the goal of processing the continuously cast plates of materials A and R into strips by means of cold forming and annealing, with identical parameters for the degrees of cold forming and the annealing temperatures being used in each case (Table 5).
  • the strips of example A After the last cold rolling step to the final thickness of 3.0 mm, the strips of example A have the highest strength values and hardness values (Tab. 6).
  • the increase in strength R m (from 498 to 717 MPa) and R p0.2 (from 439 to 649 MPa) as well as the hardness HB (from 166 to 230 MPa) falls due to the spinodal segregation of the structure ) is most evident in alloy R (Table 6).
  • the structure of the aged states of alloy R is very uneven with a grain size between 5 and 30 ⁇ m.
  • the structure of the aged states of the reference material R is characterized by discontinuous precipitations of the system (Cu, Ni)-Sn (in 1 and 2 denoted by 1).
  • the structure of the further processed state of the reference material R also contains Ni phosphides (in 1 and 2 labeled 2).
  • the structure of the retired tapes of embodiment A of the invention On the other hand, with a grain size of 2 to 8 ⁇ m, it is very uniform.
  • the structure of Example A lacks the discontinuous precipitates even after aging at 450°C for 3 hours followed by air cooling.
  • second-class hard particles can be detected in the structure. These phases are in 5 and 6 marked with 3.
  • the strengths R m and R p0.2 of the strips of alloy A assume the values of 704 and 618 MPa as a result of the spinodal segregation of the structure.
  • R m and R p0.2 are therefore lower than the characteristic values of the correspondingly aged state of alloy R. This is due to the fact that in exemplary embodiment A the Ni content, which is bound in the hard particles, is responsible for the strength-increasing spinodal segregation of the structure is missing. If the strength level of R is required, it is possible to add a higher proportion of the alloying element nickel to the alloy according to the invention.
  • the next step included testing the hot formability of the continuously cast alloys A and R.
  • the cast plates were hot rolled at a temperature of 720°C (Table 7).
  • the parameters of production program 2 were adopted for the further process steps of cold forming and intermediate annealing. ⁇ b> ⁇ u>Table 7: ⁇ /u> ⁇ /b> Production program 3 of strips from the continuously cast plates of example A and the reference material R No.
  • the cast plates of the embodiment A of the invention hot-rolled without damage and after several cold-rolling and annealing processes to the final thickness of 3.0 mm.
  • the properties of the outsourced strips (Tab. 8) largely correspond to those of the strips that were produced without hot forming using production program 2 (Tab. 6).
  • microstructure of the strips from embodiment A of the alloy according to the invention which were produced with and without a hot forming step, is also comparable. That's how it goes 7 and 8 the uniform structure of the strips from example A emerges, which were produced with a hot forming stage and a final aging at 400° C./3 h/air cooling. In 7 and 8 the hard particles of the second class, labeled 3, can again be seen.
  • the hard particles of the third class even assume a size of less than 1 ⁇ m (with 5 in 8 designated).
  • Table 9 lists the process steps used as part of production program 4. The production was carried out with a cycle of cold forming and annealing. Again, only the Alloy A cast slabs were annealed at 740°C prior to the first cold rolling.
  • this thermomechanical treatment increased the coverage of the grain boundaries of alloy R with Sn-rich segregations.
  • the crack-free and uniform structure of the belts of example A is characterized by the arrangement of the hard particles of the second and third class.
  • the third-class hard particles also have a size of less than 1 ⁇ m in this production program 4.
  • the exemplary embodiment A has a high degree of outsourcing capability, which is expressed by the interaction of the mechanisms of precipitation hardening and spinodal segregation of the structure.
  • the characteristic values R m and R p0.2 increase from 524 to 655 and from 465 to 589 MPa as a result of aging at 400°C.
  • the degree of precipitation hardening and the degree of spinodal segregation of the structure of the invention can be adapted to the required material properties by varying the chemical composition, the degree of deformation for the cold forming(s) and by varying the aging conditions. In this way, it is possible to tailor the strength, hardness, ductility and electrical conductivity of the alloy according to the invention to the intended area of use.

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Claims (18)

  1. Alliage cuivre-nickel-étain à haute résistance brut de coulée présentant une excellente coulabilité, aptitude au façonnage à chaud et au façonnage à froid, une résistance élevée à l'usure par abrasion, à l'usure par adhérence et à l'usure par fretting ainsi qu'une résistance à la corrosion et une résistance à la relaxation sous tension améliorées, ledit alliage comprenant (en % en poids) :
    2,0 à 10,0 % de Ni,
    2,0 à 10,0 % de Sn,
    0,01 à 1,0 % de Fe,
    0,01 à 0,8 % de Mg,
    0,01 à 1,5 % de Si,
    0,002 à 0,45 % de B,
    0,004 à 0,3 % de P,
    sélectivement encore jusqu'à, au maximum, 2,0 % de Co,
    sélectivement encore jusqu'à, au maximum, 0,25 % de Pb,
    le reste de cuivre et d'impuretés inévitables,
    caractérisé
    - en ce que le rapport Si/B des teneurs élémentaires en % en poids des éléments silicium et bore est au minimum de 0,4 et au maximum de 8 ;
    - en ce que, après la coulée, les composants structuraux suivants sont présents dans l'alliage :
    a) une masse de base métallique contenant du Si et du P, comprenant, par rapport à la structure totale,
    a1) jusqu'à 30 % en volume de premiers composants de phase, qui présentent un rapport (h+k)/m des teneurs élémentaires en % atomique de 2 à 6 avec la formule brute CUhNikSnm,
    a2) jusqu'à 20 % en volume de seconds composants de phase, qui présentent un rapport (p+r)/s des teneurs élémentaires en % atomique de 10 à 15 avec la formule brute CupNirSns et
    a3) un résidu de cristaux mixtes de cuivre ;
    b) des phases qui, par rapport à la structure totale, sont présentes dans la structure
    b1) de 0,01 à 10 % en volume en tant que phases contenant du Si et du B, formées en tant que borures de silicium et borosilicates et/ou borophosphosilicates,
    b2) de 1 à 15 % en volume en tant que borures de Ni-Si de formule brute NixSi2B avec x = 4 à 6,
    b3) de 1 à 15 % en volume en tant que borures de Ni,
    b4) de 0,1 à 5 % en volume en tant que borures de Fe,
    b5) de 1 à 5 % en volume en tant que phosphures de Ni,
    b6) de 0,1 à 5 % en volume en tant que phosphures de Fe,
    b7) de 0,1 à 5 % en volume en tant que phosphures de Mg,
    b8) de 1 à 5 % en volume en tant que siliciures de Ni,
    b9) de 0,1 à 5 % en volume en tant que siliciures de Fe et/ou particules riches en Fe,
    b10) de 0,1 à 5 % en volume en tant que siliciures de Mg,
    b11) de 0,1 à 5 % en volume en tant que phases contenant du Cu et du Mg et/ou phases contenant du Cu et du Sn et du Mg, lesquelles sont présentes individuellement et/ou en tant que composés d'addition et/ou composés de mélange et sont entourées par l'étain et/ou les premiers composants de phase et/ou les seconds composants de phase ;
    - en ce que, lors de la coulée, les phases contenant du Si et du B, formées en tant que borures de silicium, les borures de Ni-Si, borures de Ni, borures de Fe, phosphures de Ni, phosphures de Fe, phosphures de Mg, siliciures de Ni, siliciures de Fe et/ou particules riches en Fe, siliciures de Mg ainsi que les phases contenant du Cu et du Mg et/ou les phases contenant du Cu et du Sn et du Mg, qui sont présentes individuellement et/ou en tant que composés d'addition et/ou composés de mélange, constituent des germes pour une cristallisation régulière pendant la solidification/le refroidissement de la matière fondue, de sorte que les premiers composants de phase et/ou les seconds composants de phase sont répartis régulièrement dans la structure sous forme d'îlots et/ou de réseaux ;
    - en ce que les phases contenant du Si et du B, formées en tant que borosilicates et/ou borophosphosilicates, conjointement avec les phosphosilicates et les oxydes de Mg, remplissent le rôle de revêtement protecteur contre l'usure et la corrosion sur les produits semi-finis et les pièces en ledit alliage.
  2. Alliage cuivre-nickel-étain à haute résistance après recuit ou après façonnage à chaud et/ou façonnage à froid en plus du recuit, présentant une excellente coulabilité, aptitude au façonnage à chaud et au façonnage à froid, une résistance élevée à l'usure par abrasion, à l'usure par adhérence et à l'usure par fretting ainsi qu'une résistance à la corrosion et une résistance à la relaxation sous tension améliorées, ledit alliage comprenant (en % en poids) :
    2,0 à 10,0 % de Ni,
    2,0 à 10,0 % de Sn,
    0,01 à 1,0 % de Fe,
    0,01 à 0,8 % de Mg,
    0,01 à 1,5 % de Si,
    0,002 à 0,45 % de B,
    0,004 à 0,3 % de P,
    sélectivement encore jusqu'à, au maximum, 2,0 % de Co,
    sélectivement encore jusqu'à, au maximum, 0,25 % de Pb,
    le reste de cuivre et d'impuretés inévitables,
    caractérisé
    - en ce que le rapport Si/B des teneurs élémentaires en % en poids des éléments silicium et bore est au minimum de 0,4 et au maximum de 8 ;
    - en ce que, après re-traitement de l'alliage par au moins un recuit ou par au moins un façonnage à chaud et/ou un façonnage à froid en plus d'au moins un recuit, les composants structuraux suivants sont présents dans l'alliage :
    A) une masse de base métallique comprenant, par rapport à la structure totale,
    A1) jusqu'à 15 % en volume de premiers composants de phase, qui présentent un rapport (h+k)/m des teneurs élémentaires en % atomique de 2 à 6 avec la formule brute CuhNikSnm,
    A2) jusqu'à 10 % en volume de seconds composants de phase, qui présentent un rapport (p+r)/s des teneurs élémentaires en % atomique de 10 à 15 avec la formule brute CupNirSns et
    A3) un résidu de cristaux mixtes de cuivre ;
    B) des phases qui, par rapport à la structure totale, sont présentes dans la structure
    B1) de 2 à 40 % en volume en tant que phases contenant du Si et du B, formées en tant que borures de silicium et en tant que borosilicates et/ou borophosphosilicates, borures de Ni-Si de formule brute NixSi2B avec x = 4 à 6, en tant que borures de Ni, borures de Fe, phosphures de Ni, phosphures de Fe, phosphures de Mg, siliciures de Ni, siliciures de Fe et/ou particules riches en Fe, siliciures de Mg, ainsi qu'en tant que phases contenant du Cu et du Mg et/ou phases contenant du Cu et du Sn et du Mg, lesquelles sont présentes individuellement et/ou en tant que composés d'addition et/ou composés de mélange et sont entourées de précipitations du système (Cu, Ni)-Sn,
    B2) jusqu'à 80 % en volume en tant que précipitations continues du système (Cu, Ni)-Sn,
    B3) de 2 à 35 % en volume en tant que phosphures de Ni, phosphures de Fe, phosphures de Mg, siliciures de Ni, siliciures de Fe et/ou particules riches en Fe, siliciures de Mg, ainsi qu'en tant que phases contenant du Cu et du Mg et/ou phases contenant du Cu et du Sn et du Mg, lesquelles sont présentes individuellement et/ou en tant que composés d'addition et/ou composés de mélange, sont entourées de précipitations du système (Cu, Ni)-Sn, et présentent une taille inférieure à 3 µm ;
    - en ce que les phases contenant du Si et du B, formées en tant que borures de silicium, les borures de Ni-Si, borures de Ni, borures de Fe, phosphures de Ni, phosphures de Fe, phosphures de Mg, siliciures de Ni, siliciures de Fe et/ou particules riches en Fe, siliciures de Mg ainsi que les phases contenant du Cu et du Mg et/ou les phases contenant du Cu et du Sn et du Mg, qui sont présentes individuellement et/ou en tant que composés d'addition et/ou composés de mélange, constituent des germes pour une recristallisation statique et dynamique de la structure pendant le re-traitement de l'alliage, moyennant quoi une structure à grains fins et uniforme est induite ;
    - en ce que les phases contenant du Si et du B, formées en tant que borosilicates et/ou borophosphosilicates, conjointement avec les phosphosilicates et les oxydes de Mg, remplissent le rôle de revêtement protecteur contre l'usure et la corrosion sur les produits semi-finis et les pièces en ledit alliage.
  3. Alliage cuivre-nickel-étain selon la revendication 1 ou 2, caractérisé en ce que l'élément fer est présent de 0,02 à 0,6 %.
  4. Alliage cuivre-nickel-étain selon l'une des revendications 1 à 3, caractérisé en ce que l'élément magnésium est présent de 0,05 à 0,6 %.
  5. Alliage cuivre-nickel-étain selon l'une des revendications 1 à 4, caractérisé en ce que l'élément silicium est présent de 0,05 à 0,9 %.
  6. Alliage cuivre-nickel-étain selon l'une des revendications 1 à 5, caractérisé en ce que l'élément bore est présent de 0,01 à 0,4 %.
  7. Alliage cuivre-nickel-étain selon l'une des revendications 1 à 6, caractérisé en ce que l'élément phosphore est présent de 0,01 à 0,3 %.
  8. Alliage cuivre-nickel-étain selon l'une des revendications 1 à 7, caractérisé en ce que l'alliage est exempt de plomb à quelques impuretés inévitables près.
  9. Procédé de production de produits finis et de pièces ayant une forme proche du produit fini à partir d'un alliage cuivre-nickel-étain selon l'une des revendications 1 à 8 à l'aide du procédé de moulage en sable, du procédé de moulage en carapace, du procédé de moulage de précision, du procédé de coulée en moule perdu, du procédé de moulage sous pression ou du procédé de lost-foam.
  10. Procédé de production de bandes, de tôles, de plaques, de boulons, de fils ronds, de fils profilés, de tiges rondes, de tiges profilées, de tiges creuses, de tubes et de profilés à partir d'un alliage cuivre-nickel-étain selon l'une des revendications 1 à 8 à l'aide du procédé de coulée en lingotière ou du procédé de coulée continue ou semi-continue.
  11. Procédé selon la revendication 10, caractérisé en ce que le re-traitement du brut de coulée englobe la réalisation d'au moins un façonnage à chaud dans la plage de températures allant de 600 à 880 °C.
  12. Procédé selon l'une des revendications 9 à 11, caractérisé en ce qu'au moins un traitement de recuit est effectué dans la plage de températures de 170 à 880 °C pendant une durée de 10 minutes à 6 heures.
  13. Procédé selon l'une des revendications 10 à 12, caractérisé en ce que le re-traitement du brut de coulée ou du brut façonné à chaud ou du brut de coulée recuit ou du brut façonné à chaud recuit comprend la réalisation d'au moins un façonnage à froid.
  14. Procédé selon la revendication 13, caractérisé en ce qu'au moins un traitement de recuit est effectué dans la plage de températures de 170 à 880 °C pendant une durée de 10 minutes à 6 heures.
  15. Procédé selon l'une des revendications 13 ou 14, caractérisé en ce qu'un recuit de détente ou un recuit de précipitation est effectué dans la plage de températures de 170 à 550 °C pendant une durée de 0,5 à 8 heures.
  16. Utilisation de l'alliage cuivre-nickel-étain selon l'une des revendications 1 à 8 pour des verrous ou barres de glissement, pour des bagues de friction ou disques de friction, pour des surfaces de paliers lisses dans des composites, pour des éléments de glissement ou des éléments de guidage dans des moteurs à combustion, des vannes, des turbocompresseurs, des engrenages, des systèmes de post-traitement des gaz d'échappement, des systèmes de levage, des systèmes de freinage ou des systèmes de transmission, des groupes hydrauliques ou dans des machines ou des appareils de la construction mécanique générale.
  17. Utilisation de l'alliage cuivre-nickel-étain selon l'une des revendications 1 à 8 pour des éléments de construction, des éléments de conduite, des éléments de guidage ou des éléments de connexion en électronique ou en électrotechnique.
  18. Utilisation de l'alliage cuivre-nickel-étain selon l'une des revendications 1 à 8 pour des objets métallisés dans l'élevage d'organismes vivants dans l'eau de mer, pour des instruments à percussion, pour des propulseurs, des pales, des hélices de bateau ou des moyeux pour la construction navale, pour des carters de pompes à eau, de pompes à huiles ou pompes à carburants, pour des roues directrices, des roues mobiles ou des roues à aubes pour pompes ou turbines hydrauliques, pour des roues dentées, des roues hélicoïdales, des engrenages hélicoïdaux, ainsi que pour des écrous de serrage ou des écrous de broche, ainsi que pour des tubes, des joints, des boulons de liaison dans l'industrie maritime ou chimique.
EP17736569.9A 2016-07-18 2017-06-27 Alliage cuivre-nickel-étain, procédé de préparation et utilisation de celui-ci Active EP3485051B1 (fr)

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DE102016008757.9A DE102016008757B4 (de) 2016-07-18 2016-07-18 Kupfer-Nickel-Zinn-Legierung, Verfahren zu deren Herstellung sowie deren Verwendung
PCT/EP2017/000759 WO2018014994A1 (fr) 2016-07-18 2017-06-27 Alliage cuivre-nickel-étain, procédé de préparation et utilisation de celui-ci

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CN113913646B (zh) * 2021-10-29 2022-09-16 宁波金田铜业(集团)股份有限公司 一种铜镍锡合金铸锭的制备方法
CN115896537B (zh) * 2022-09-20 2024-04-02 宁波兴业鑫泰新型电子材料有限公司 一种高强度耐腐蚀Cu-Ni-Sn合金及其制备方法
CN115786766A (zh) * 2022-11-23 2023-03-14 河南科技大学 一种油气开采用多元Cu-Ni-Sn基合金及其制备方法

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US20190161833A1 (en) 2019-05-30
DE102016008757A1 (de) 2018-01-18
US10982302B2 (en) 2021-04-20
WO2018014994A1 (fr) 2018-01-25
DE102016008757B4 (de) 2020-06-10

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