EP3342890A1 - Alliage de fonderie d'aluminium - Google Patents

Alliage de fonderie d'aluminium Download PDF

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Publication number
EP3342890A1
EP3342890A1 EP16382663.9A EP16382663A EP3342890A1 EP 3342890 A1 EP3342890 A1 EP 3342890A1 EP 16382663 A EP16382663 A EP 16382663A EP 3342890 A1 EP3342890 A1 EP 3342890A1
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alloy
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document
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EP16382663.9A
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German (de)
English (en)
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EP3342890B1 (fr
Inventor
Iban Vicario Gómez
Francisco Sáenz de Tejada Picornell
Jessica Montero García
Patricia CABALLERO OGUIZA
Alejandro Obregón Jubeto
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Befesa Aluminio SL
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Befesa Aluminio SL
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/02—Alloys based on aluminium with silicon 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
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent

Definitions

  • the field of the invention is related to aluminium casting alloys.
  • the present invention relates to a hypoeutectic secondary aluminium-silicon alloy, useful to produce, by high pressure die casting, components which have to fulfill premium abrasion resistance requirements in as-cast condition at room temperature.
  • Aluminium casting alloys have not been traditionally well suited for abrasion applications in which, among others, high hardness properties must be present.
  • abrasion requirements are, among others, piston cylinders, brake discs or steering boxes.
  • Brake discs and piston cylinders must support not only abrasion but also thermal fatigue resistance, and if aluminium is employed instead of steel, hypereutectic alloys have been traditionally applied to produce automotive components by gravity die casting (GC).
  • GC gravity die casting
  • Hypereutectic alloys present primary silicon grains that are normally refined with phosphorous and T5 thermal treatments to resist abrasion.
  • Nickel is the most important alloying element, with also Copper and dissoluted Zinc, to keep mechanical properties at high temperatures.
  • hypereutectic alloys are not so well suited. They do not fulfill the required hardness (above 80HB for EN-AC 43000 Aluminium alloys), Nickel is superfluous and Phosphorous is so volatile that requires skilled technicians to melt the alloy, which must be hold at temperatures above 750°C. Only high hardness and high strength are the objective properties, which opens the door to components produced by high pressure die casting (HPDC) with hypoeutectic aluminum.
  • HPDC high pressure die casting
  • HPDC process has been widely employed to new applications in the last twenty years, due to its low cost for big series, a high component reproducibility and reliability, and it is hence mostly preferred when compared with GC.
  • Document DE 19524564 discloses an aluminium-silicon alloy for casting cylinder heads. Minor variations in the composition of the alloys produce a change over the different proprieties of the alloys. By a minor addition of alloying elements or by varying the concentration of an alloying element, non-expected properties can be obtained. This document is silent about the obtained mechanical properties of the alloy and it doesn't mention the high pressure die casting (HPDC) process. This document discloses an alloy with a 5-11 wt % and 8-11 wt % of Si and 0.8-2 wt % of Cu.
  • HPDC high pressure die casting
  • the mechanical properties that can be achieved change completely, as shown in the DIN 1706 Standard, where mechanical properties change for sand, permanent mould casting, pressure die casting (HPDC) and investment casting.
  • Annex A of standard EN AC 43000 series discloses mechanical properties of pressure die cast alloys (Table A.1 - Mechanical properties of pressure die cast alloys).
  • Document EP 1978120A1 discloses an aluminium-silicon alloy for engine components. In this document there are no references to the HPDC process. This documents discloses very low elongation values of the obtained samples at room temperature in the as cast state ( ⁇ 0.7%). All the samples disclosed in this document have Si values with an eutectic or hypereutectic composition. This document also discloses an alloy with a 5-25% by weight of Si and 0.0007-0.1% by weight of C.
  • Secondary aluminium alloys disclosed in the prior art have limited elongation properties due to the presence of detrimental ⁇ -iron Al5FeSi needles.
  • the prior art discloses different ways of suppressing the formation of ⁇ -Al5FeSi phase: addition of sufficient manganese and, in alloys without manganese, high cooling rates.
  • Another way to avoid this problem is based on the development of primary aluminium alloys with small percentages of iron, as the AuralTM alloys with iron approximately less than 0.22% and 0.03% by weight of copper. It has also been disclosed alloys with high elongation with less than 0.2% by weight of iron content and others. It has also been disclosed limiting the silicon content to a maximum of 0.15% in weight in order to obtain high elongation alloys.
  • Document EP 2771493A2 discloses an AlSiMgCu casting alloy. This document discloses 0.5-2% by weight of copper and discloses the use of thermal treatments. This document discloses that an increasing Cu content can increase the strength due to higher amount of ⁇ '-Al2Cu and Q' precipitates, but reducing the ductility. This document aims to optimize the alloy composition, the solution and aging heat treatments to minimize/eliminate un-dissolved Q-phase (AlSiMgSi) and maximize solid solution/precipitation strengthening.
  • Document JPH093610 (A ) proposes a die-casting alloy having 5 to 13 wt % Si, up to 0.5 wt % Mg, 0.1 to 1.0 wt % Mn, 0.1 to 2.0 wt % Fe.
  • Cu and Zn contaminants are not taken into consideration, as these usually occur in significant amounts in the case of secondary aluminium.
  • the document discloses that thermal treatments are necessary to improve ductility because eutectic Si becomes roundish by heat treatment.
  • Document EP2657360 discloses a die casting alloy consisting of 6-12% by weight of Si, at least 0.3% by weight of iron, 0.25% by weight of Mn, 0.1 % by weight of Cu, 0.24 to 0.8% by weight of Mg and 0.4 to 1.5% by weight of Zn.
  • This document discloses the use of eutectic modifiers, as Sr, Na and Sb, alone or in combination, and grain refiners as Ti, Zr, V.
  • Document EP 1612286 discloses an aluminium die casting alloy having 8 to 11.5% by weight of Si, 0.3 to 0.8% by weight of Mn, 0.08 to 0.4% by weight of Mg, max. 0.4% by weight of Fe, max. 0.1 % by weight of Cu, max. 0.1 % by weight of Zn, max. 0.15% by weight of Ti and 0.05 to 0.5% by weight of Mo.
  • Cu and Zn content have been limited and the content of secondary aluminium is very restricted, which leads the production of the alloy by electrolysis.
  • elongation and mechanical properties elongation (A) equal to or more than 2%, yield strength (Rp0.2) equal to or more than 160 MPa, ultimate tensile strength (Rm) equal to or more than 250 MPa and Brinell Hardness (HB) equal to or more than >80 HB.
  • elongation and mechanical properties are required for components designed to support simultaneously high abrasion and high static bending/torsion loads, maintaining a minimal ductility and other processing properties as alloy fluidity, low die soldering, easy welding or high machinability, among others.
  • the present invention provides an aluminium casting alloy, wherein said alloy is consisting of:
  • silicon content is restricted to the range 11.5-12% by weight to reduce as much as possible the eutectic fraction, what helps to maximize the elongation but maintaining the fluidity at minimal values that allow an adequate mold filling.
  • copper content is restricted to 0.05-0.4% by weight to guarantee a minimum elastic yield and ultimate tensile strength, and alloying the use of secondary aluminum, and also to obtain the required hardness above 80 HB and high strength.
  • iron content is restricted to the range 0.3-1% by weight to guarantee both low mold soldering and small volume fraction of Al 5 FeSi intermetallics, which at the same time are minimized by the manganese content, implying an elongation above 2%.
  • manganese content is restricted to less than 0.75% by weight to transform the Al 5 FeSi intermetallics into alpha-Al 12 (Mn,Fe)Si 2 and to reduce as much as possible the negative effect of those intermetallics, and to avoid the sludge problem that occurs with high percentages of Mn in combination with Fe and other alloying elements. Values of manganese above 0.75% by weight were not found to be useful in terms of Al 5 FeSi intermetallics transformation.
  • magnesium content is also a key element to maximize the hardness and mechanical properties, whose content must be coupled with the copper content, showing best performance when are set to 0.45-0.8% by weight of Mg and 0.05-0.4% by weight of Cu.
  • Magnesium content helps to increase the yield strength, but always with a minimum percentage of copper and iron to avoid elongation to be affected. For small increases of magnesium percentages if enough silicon is available Mg 2 Si intermetallics can be produced.
  • the desired properties are obtained due to the formation of a very fine eutectic phase, the semi-globular shape of the dendrites, the absence of fragile ⁇ -iron needles, and the presence of labyrinthine Al 11.7-16.5 (Fe,Mn,Cr) 2.3-3.3 Si 2 and Mg 2 Si in the HPDC samples due to the combination of the different elements with the iron in the new developed alloy and the good distribution of Mg 2 Si. There is also very few micro-porosity in studied HPDC, probably related with the near eutectic composition of obtained parts.
  • the alloy according to the invention differs from WO 2006/0066314 in that it contains 0.05-0.4% by weight of Cu, where in the nine alloys disclosed in WO 2006/0066314 Cu % by weight is above 3.1%. % by weight and Ni is less than 0.3% in the alloy according to the invention.
  • the values of the Ni content in WO 2006/0066314 are over the values of the range of the present application.
  • the present application increases the alloy hardness in the as cast state to values higher than 80 HB, in order to obtain HPDC casted parts with high resistance to wearing and high strength.
  • the objective of defining an alloy into a determinate range of composition is in relation with the obtained hardness and mechanical properties, which clearly vary with small changes in the composition, as can be seen in the present application, which discloses changes in the properties with minor composition variations in test alloys 1 to 3.
  • the present solution solves the problem of obtaining secondary aluminium alloys with high hardness in the as cast state for the high pressure die casting manufacturing process.
  • Nickel is commonly used with copper to enhance elevated temperature properties. It also reduces the thermal expansion coefficient. Nickel is characterized by low solubility in (Al) (maximum ⁇ 0.01-0.03%) and do not form supersaturated solid solutions even after relatively rapid solidification. Their introduction into aluminum alloys always causes the formation of excessive phases (constituent particles) that often reduce formability and corrosion resistance.
  • Ni can be used as alloying element.
  • the high percentage of Ni can be related with the development of a new thermal treatment for the alloys.
  • the alloy according to the invention differs from the alloy of DE 19524564 in that it contains 11.5-12% by weight of silicon and 0.05-0.4% by weight of copper.
  • the content of the alloying elements in the alloy according to the invention is related to the obtained mechanical properties of the alloy. These mechanical properties clearly vary with small changes in the composition. This can be seen in the alloys of the example, which shows changes of the properties with minor composition variations.
  • the alloy according to the invention differs from EP 1978120A1 in that it contains 11.5-12% by weight of silicon and that it does not contain C.
  • the alloy according to the invention differs from EP 2771493A2 in that it contains 0.05-0.4% by weight of copper.
  • the concentration of copper in the alloy according to the invention lead to an increase in the elongation, in comparison with the values mentioned in EP 2771493A2 , which discloses that an increasing Cu content can increase the strength due to higher amount of ⁇ '-Al2Cu and Q' precipitates but reducing ductility.
  • a thermal treatment of the alloy according to the invention is not necessary, due to the appearance of a very fine eutectic and a quite globular dendrite structure in the alloy.
  • the reduced content of Cu and Zn in comparison with the alloy of document JPH093610 (A ) avoids the use of secondary aluminum as disclosed in JPH093610 (A ).
  • the alloy according to the invention differs from the alloy of document EP2657360 in that it contains less than 0.35% by weight of Zn.
  • An increase in the Zn percentage leads to a lower corrosion resistance, and because of that, the Zn percentage has been limited in the alloy according to the invention, in order to obtain parts that don't need extra surface treatments.
  • the alloy according to the invention has high ductility.
  • the alloy according to the invention differs from document EP 1612286 in that it does not contain Mo.
  • Example 1 Aluminium casting alloys (preparation, composition and mechanical properties)
  • Aluminium compositions have been prepared by melting a standard EN-AC 43000 alloy in a holding furnace at 690°C and later poured into the injection vessel, being injected into the mold cavity of a 950 tonnes closing force HPDC machine at 685°C. No vacuum conditions were applied.
  • Alloy 1 is a comparative example, not according to the invention.
  • Alloys 2 and 3 are according to the invention. The obtained results are also specified in Table 1.
  • Table 1 Alloy 1 Alloy 2 Alloy 3 Si (% by weight) 9.02 11.82 11.64 Fe (% by weight) 1.05 0.96 0.96 Cu (% by weight) 0.294 0.106 0.078 Mn (% by weight) 0.81 0.108 0.078 Mg (% by weight) 0.382 0.52 0.53 Zn (% by weight) 0.063 0.175 0.125 Ti (% by weight) 0.171 0.109 0.267 Cr (% by weight) 0.066 0.141 0.162 Ni (% by weight) 0.207 0.109 0.075 Pb (% by weight) 0.21 0.11 0.083 Sn (% by weight) 0.02 0.046 0.033 Sr (% by weight) 0.048 0.023 0.01 Rp0.2 (MPa) 145 177 178.4 Rm (MPa) 2
  • Alloys 2 and 3 have Brinell hardness (HB) values equal or above 81 HB, yield strength (Rp0.2) values above 177 Mpa and ultimate tensile strength values (Rm) above 260 MPa and elongation values above 2.4%. Small variations of the alloy composition out of the claimed values give values out of the objectives. For comparison, Alloy 1 with a composition out the one of the invention and having Mn wt.% higher than 0.75 wt.% (0.81 wt.%) has Rp0.2, Rm and Hb smaller values that the minimum to be obtained in the presented invention.
  • Patent EP2657360 (B1 ) discloses the use of eutectic modifiers, as Sr, Na and Sb, alone or in combination, and grain refiners as Ti, Zr, V.
  • the alloy according to the invention has less than 0.3% by weight of titanium and less than 0.05% by weight of strontium.
  • Sr in the alloys of the example don't shown a significant benefit over the elongation, with for example the modified Alloy 1 with much higher Sr content wt. % than Alloy 3 but with a smaller elongation value.
  • the alloys of the example don't show a significant benefit over the elongation, with similar values.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
EP16382663.9A 2016-12-28 2016-12-28 Alliage de fonderie d'aluminium Active EP3342890B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES16382663T ES2753168T3 (es) 2016-12-28 2016-12-28 Aleación de aluminio para fundición
EP16382663.9A EP3342890B1 (fr) 2016-12-28 2016-12-28 Alliage de fonderie d'aluminium

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EP16382663.9A EP3342890B1 (fr) 2016-12-28 2016-12-28 Alliage de fonderie d'aluminium

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EP3342890A1 true EP3342890A1 (fr) 2018-07-04
EP3342890B1 EP3342890B1 (fr) 2019-05-29

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109332631A (zh) * 2018-11-02 2019-02-15 广东鸿图科技股份有限公司 一种通讯箱体低温压铸工艺
CN111349829A (zh) * 2020-04-17 2020-06-30 江苏鼎胜新能源材料股份有限公司 一种皮材铝带的生产方法
CN113564431A (zh) * 2021-08-10 2021-10-29 广州立中锦山合金有限公司 一种轮毂用高强度铝合金及其制备方法

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573606A (en) 1995-02-16 1996-11-12 Gibbs Die Casting Aluminum Corporation Aluminum alloy and method for making die cast products
DE19524564A1 (de) 1995-06-28 1997-01-02 Vaw Alucast Gmbh Aluminiumguß-Legierung
JPH093610A (ja) 1995-06-15 1997-01-07 Nippon Light Metal Co Ltd 寸法精度及び延性に優れた薄肉アルミダイカスト製品及び製造方法
EP1612286A2 (fr) 2004-06-29 2006-01-04 ALUMINIUM RHEINFELDEN GmbH Alliage d'aluminium pour moulage sous pression
WO2006066314A1 (fr) 2004-12-23 2006-06-29 Commonwealth Scientific And Industrial Research Organisation Traitement thermique d'articles coules en alliage d'aluminium, moules sous haute pression
EP1978120A1 (fr) 2007-03-30 2008-10-08 Technische Universität Clausthal Alliage de fonte, d'aluminium et de silice et son procédé de fabrication
EP2653579A1 (fr) * 2012-04-17 2013-10-23 Georg Fischer Druckguss GmbH & Co. KG Alliage d'aluminium
EP2657360A1 (fr) 2012-04-26 2013-10-30 Audi Ag Alliage à coulée sous pression à base d'Al-Si présentant en particulier un aluminium secondaire
EP2771493A2 (fr) 2011-10-28 2014-09-03 Alcoa Inc. Alliage de moulage par coulée d'alsimgcu à haute performance
EP2865772A1 (fr) * 2013-10-23 2015-04-29 Befesa Aluminio, S.L. Alliage de fonderie d'aluminium

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573606A (en) 1995-02-16 1996-11-12 Gibbs Die Casting Aluminum Corporation Aluminum alloy and method for making die cast products
JPH093610A (ja) 1995-06-15 1997-01-07 Nippon Light Metal Co Ltd 寸法精度及び延性に優れた薄肉アルミダイカスト製品及び製造方法
DE19524564A1 (de) 1995-06-28 1997-01-02 Vaw Alucast Gmbh Aluminiumguß-Legierung
EP1612286A2 (fr) 2004-06-29 2006-01-04 ALUMINIUM RHEINFELDEN GmbH Alliage d'aluminium pour moulage sous pression
WO2006066314A1 (fr) 2004-12-23 2006-06-29 Commonwealth Scientific And Industrial Research Organisation Traitement thermique d'articles coules en alliage d'aluminium, moules sous haute pression
EP1978120A1 (fr) 2007-03-30 2008-10-08 Technische Universität Clausthal Alliage de fonte, d'aluminium et de silice et son procédé de fabrication
EP2771493A2 (fr) 2011-10-28 2014-09-03 Alcoa Inc. Alliage de moulage par coulée d'alsimgcu à haute performance
EP2653579A1 (fr) * 2012-04-17 2013-10-23 Georg Fischer Druckguss GmbH & Co. KG Alliage d'aluminium
EP2657360A1 (fr) 2012-04-26 2013-10-30 Audi Ag Alliage à coulée sous pression à base d'Al-Si présentant en particulier un aluminium secondaire
EP2657360B1 (fr) 2012-04-26 2014-02-26 Audi Ag Alliage à coulée sous pression à base d'Al-Si présentant en particulier un aluminium secondaire
EP2865772A1 (fr) * 2013-10-23 2015-04-29 Befesa Aluminio, S.L. Alliage de fonderie d'aluminium

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109332631A (zh) * 2018-11-02 2019-02-15 广东鸿图科技股份有限公司 一种通讯箱体低温压铸工艺
CN111349829A (zh) * 2020-04-17 2020-06-30 江苏鼎胜新能源材料股份有限公司 一种皮材铝带的生产方法
CN111349829B (zh) * 2020-04-17 2021-10-22 江苏鼎胜新能源材料股份有限公司 一种皮材铝带的生产方法
CN113564431A (zh) * 2021-08-10 2021-10-29 广州立中锦山合金有限公司 一种轮毂用高强度铝合金及其制备方法

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EP3342890B1 (fr) 2019-05-29
ES2753168T3 (es) 2020-04-07

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