Classifications

• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/02—Making non-ferrous alloys by melting
  • C22C1/026—Alloys based on aluminium
• • 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
  • B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
  • B22D21/04—Casting aluminium or magnesium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/02—Making non-ferrous alloys by melting
  • C22C1/03—Making non-ferrous alloys by melting using master alloys
• • 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
  • C22C—ALLOYS
  • C22C21/00—Alloys based on aluminium
  • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
  • C22C21/04—Modified aluminium-silicon alloys
• • 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 invention relates to the field of metallurgy of aluminium alloys, and more precisely to aluminium - silicon casting alloys.
• the invention also relates to castings, that is to say to cast and solidified pieces, made from said alloy.
• the invention also relates to heat- treatments applicable to aluminium-silicon alloy castings.
• the invention also relates to certain cast pieces produced by casting said alloy into a given shape and heat-treating the solidified piece. These cast pieces, also called castings, need to comply with certain requirements, such as high mechanical strength, high elongation and high corrosion resistance.
• the invention relates in particular to aluminium - silicon casting alloys with a rather low silicon content, not exceeding about 5 weight percent, and containing a small amount of magnesium.
• Casting alloys of the AISi5Mg type are known for a long time. They are age-hardenable.
• Aluminium und Aluminiumlegierungen » published in 1965 (Springer Verlag) by D. Altenpohl (see p. 811 )
• a solution heat treatment between 525 °C and 530 °C (5h) and an artificial ageing to a T6-like temper after water quench between 155 °C and 160 °C for 10 h is disclosed for this alloy.
• EP 3 370 900 (Mubea Performance Wheels) describes compositions with silicon from 3.5% to 5.0 %, magnesium 0.2 % to 0.7 %, and titanium 0.07 % to 0.12 %, and in particular an alloy for low pressure die casting containing Si 4.0 %, Mg 0.4 %, Ti 0.008 %, B 0.006 %, Cu 400 ppm, Zn 400 ppm, Sr 100 ppm, Sn 200 ppm, Ni 400 ppm, Mn 400 ppm, TiB 2 20 ppm; no heat treatment is described for this alloy.
• US 2019/011 8251 discloses an alloy for low pressure die casting and gravity casting containing silicon from 4 % to 7 %, manganese less than 0.5 %, chromium between 0.15 % and 0.5 %, and magnesium not exceeding 0.8 %.
• US 10,612,116 discloses a composition range with silicon 4 % to 6 %, chromium 0.2 % to 0.4 %, magnesium 0.1 % to 0.5 %; the use of this alloy is recommended for wheels.
• CN 106319 299 (Citic Dicastal) described two alloys with the following compositions : Si 4.0 %, Mg 0.4 %, Cr 0.10 %, B 0.01 % with an elongation of 12 % and a yield strength of 280 MPa in T6 temper, and Si 0.4 %, Mg 0.6 %, Cr 0.15 %, B 0.001 % with an elongation of 11 % and a yield strength of 290 MPa in T6 temper.
• JP 2015/045 033 discloses a die casting alloy with 4.5 % to 7.5 % silicon, 0.25 % to 0.75 % magnesium, and zinc up to 0.3 %.
• EP 2 700 727 (KSM Castings) describes an alloy composition with 3.0 % to 3.8 % of silicon, 0.3 % to 0.6 % magnesium, 0.25 % to 0.35 % of chromium; this alloy can be heat treated to a T6 temper.
• EP 2 954 081 discloses a casting alloy with silicon from 3.0 % to 3.8 %, magnesium from 0.3 % to 0.6 %, chromium 0.05 % to 0.25 %, and strontium between 0.010 % and 0.030 %.
• These alloys can be used in particular in T6-like tempers, i.e. after solution heat treatment and age hardening to peak stength, where they usually exhibit mechanical properties which represent a certain compromise between mechanical strength and elongation at rupture, knowing that these two properties are usually following a conflicting path when optimizing the composition of the alloy or the heat treatment conditions of the cast piece : it is usually not difficult to increase one of the two properties while decreasing at the same time the other one.
• These alloys can in particular be used for making wheels, in particular for cars and trucks. Their resistance to atmospheric corrosion is usually good. For this specific use, there is however an additional requirement, namely corrosion resistance in contact with water and seawater. There is now a need for aluminium-based casting alloys that have higher mechanical strength and, at the same time, higher elongation, and that also have an excellent corrosion resistance. This is the problem addressed by the present invention.
• the aluminium casting alloy comprises, expressed in weight percent : from 3.5 % to 4.5 % of silicon; from 0.35 % to 0.55 % of magnesium; from 0.05 % to 0.25 % of chromium; from 0.05 % to 0.30 % of nickel; from 0.005 % to 0.020 % of strontium; not more than 0.12 % of iron; not more than 0.15 % of titanium; not more than 0.05 %, and preferably not more than 0.03 %, of manganese; optionally comprising from 0.05 % to 0.20 % of copper; optionally comprising from 0.05 % to 0.30 % of silver; other impurities not more than 0.02 each and not more than 0.10 in total, the remainder being aluminium.
• This alloy is the first object of the present invention.
• a second object of the invention is an aluminium alloy casting made from this alloy, presenting the following set of properties : yield strength R p0 ,2 is comprised between about 255 MPa and about 300 MPa, tensile strength R m is comprised between about 340 MPa and about 370 MPa, and elongation at fracture is comprised between about 11.0 % and about 20.0 %.
• a third object of the invention is a process for obtaining an aluminium casting according to the second object of the invention, comprising solidifying a liquid aluminium casting alloy according to the first object, carrying out a solution heat treatment of 4 h to 10 h at a temperature comprised between 535 °C and 555 °C, and preferably of 4 h to 8 h between 540 °C and 550 °C, followed by quenching and artifial aging treatment of 4 h to 10 h at a temperature between 150 °C and 170 °C, and preferably of 6 h to 8 h at a temperature between 160 °C and 170 °C.
• the aluminium casting alloy comprises, expressed in weight percent : from 3.5 % to 4.5 % of silicon; from 0.35 % to 0.55 % of magnesium; from 0.05 % to 0.25 % of chromium; from 0.05 % to 0.30 % of nickel; from 0.005 % to 0.020 % of strontium; not more than 0.12 % of iron; not more than 0.15 % of titanium; not more than 0.05 %, and preferably not more than 0.03 %, of manganese; optionally comprising from 0.05 % to 0.20 % of copper; optionally comprising from 0.05 % to 0.30 % of silver; other impurities not more than 0.02 % each and not more than 0.10 % in total, the remainder being aluminium.
• the silicon content is comprised between 3.7 % and 4.3 %, and still more preferably between 3.8 % and 4.3 %, and even more preferably between 3.85 % and 4.25 %;
• the strontium content does not exceed 0.015 %;
• the chromium content does not exceed 0.20 %, and still more preferably the chromium content is comprised between 0.06 % and 0.15 %;
• the nickel content is comprised between 0.08 % and 0.22 %, and preferably between 0.10 % and 0.20 %;
• the manganese content is comprised between 0.001% and 0.03 %; other impurities do not exceed 0.015 % each and 0.10 % in total (and preferably do not exceed 0.09 % in total).
• Nickel is an essential feature of the alloy according to the invention.
• the addition of nickel to the base alloy results in a fundamental change in the microstructure.
• the inventors have found that a nickel concentration as low as 0.05 wt-% modifies the phase profile and the distribution of other elements.
• excess magnesium is consumed by AI 3 Ni phases, and very few Mg 2 Si phases are formed, thereby enabling higher solution heat treatment temperatures. With Ni 0.15 % nearly all magnesium is dissolved in the matrix. To a significant extent, AI 3 Ni phases survive the heat treatments leading to T6 temper.
• Chromium combines with nickel to AICrNi(Fe) phases which are stable and present in T6 temper.
• this allow further comprises from 0.05 % to 0.20 % of copper, and preferably between 0.07 % and 0.15 %.
• this alloy further comprises from 0.05 % to 0.30 % of silver, and preferably between 0.05 % and 0.20 %.
• this alloy further comprises from 0.05 % to 0.20 % of copper and from 0.05 % to 0.30 % of silver; it preferably comprises between 0.07 % and 0.15 % of copper and between 0.05 % and 0.20 % of silver.
• the alloy composition in all of its variants and embodiments, can comprise controlled amounts of certain minor elements; these controlled amount can result from the voluntary addition of said minor elements, or from the control of their impurity level.
• the calcium content is less than 200 ppm ; this increases the corrosion resistance of the castings in certain tempers.
• vanadium does not exceed 0.02 %, and/or gallium does not exceed 0.02 %.
• the iron content is below 0.10 %; this low iron content leads to a higher elongation at rupture of the castings, which is desirable.
• a minor addition of manganese may be desirable.
• the preferentiel manganese range is between 0.001 % and 0.03 %, and preferably between 0.003 % and 0.03 %, and even more preferably between 0.005 % and 0.02 %.
• the inventors have found that this presence of a minute amout of manganese promotes the formation of Mn-Fe intermetallic phases which act as strain hardeners; this increases strenghth of the castings, but does not lead to a decrease in elongation at rupture.
• titanium is introduced into the alloy in the form of an AITi 3 master alloy or another master alloy that does not contain boron, but not as TiB 2 .
• the casting alloy according to the invention can be used for making cast parts, also called castings, using various casting processes, depending on the purpose. These casting techniques are known as such; in general the liquid metal is admitted into a die (possibly under pressure), where is solidifies.
• casting of remelting ingots can be carried out as open casting or direct chill casting.
• Casting of parts, such as wheels, suspension parts - subframes, cross members, knuckles can be carried out in particular by low pressure die casting, by gravity die casting or counter pressure die casting.
• Cast parts according to the invention can be heat treated in various ways.
• An advantageous heat treatment comprises a specific combination of solution heat treatment and artificial ageing. In this way, a T6 like temper can be obtained.
• This temper is a particularly interesting one for making parts that need to exhibit both high mechanical strength and high elongation; such parts are in particular wheels for cars and trucks.
• An advantageous process for obtaining such a heat treated aluminium casting comprises a first step of solution heat treatment of about 4 h to about 10 h at a temperature comprised between about 535 °C and about 555 °C, and preferably of 4 h to 8 h between 540 °C and 550 °C. This solution heat treatment can be terminated by quenching.
• the casting is submitted to artificial ageing of about 4 h to about 10 h at a temperature between about 150 °C and about 170 °C, and preferably of 6 h to 9 h at a temperature between 160 °C and 170 °C.
• the duration of the ageing treatment is a particularly critical parameter that determines the mechanical properties of the cast part. For this reason, the most preferred ageing conditions are betwen 6 h and 8 h at a temperature between 160 °C and 170 °C.
• yield strength R p0 ,2 is comprised between about 255 MPa and about 310 MPa
• tensile strength R m is comprised between about 340 MPa and about 370 MPa
• elongation at fracture is comprised between about 11 .0 % and about 20.0 %.
• yield strength R p0 ,2 is comprised between about 255 MPa and about 285 MPa
• tensile strength is R m comprised between about 340 MPa and about 370 MPa
• elongation at fracture is comprised between about 14.0 % and about 20.0 %.
• yield strength R p0 ,2 is comprised between 265 MPa and 280 MPa
• tensile strength is R m comprised between 350 MPa and 365 MPa
• elongation at fracture is comprised between 15.0 % and 18.0 %.
• the solution heat treatment is carried out at a temperature comprised between 541 °C and 549 °C for a duration comprised between 5 h and 7 h
• the artificial ageing is carried out a temperature comprised between 157 °C and 163 °C for a duration between 6 h and 9 h.
• the artifical ageing treatment can also be carried out in two or more steps at different temperatures; this will however render the industrial production more complex.
• a base alloy composition was prepared with the following target composition:
• the following amounts of elements were added: Cr 0.10 % and Ni 0.15 %.
• the alloy was cast in a mould. After solidification the following heat treatment was applied: solution heat treatment of 6 hours at 545 °C followed by artifical ageing at varying conditions, as explained in Table 1 which summarizes the results.
• Example 9 is the same chemical composition as examples 1 to 6.
• Example 10 is the same chemical composition as examples 7 and 8.
• Examples 9 and 10 have been submitted to the same solution heat treatment as in Examples 1 to 8, namely 6 h at 545 °C.
• Examples 9 and 10 have then been submitted to a two-step ageing treatment, as follows: a first step of 1 h at 110 °C, and a second step of 2 h at 170°C.
• Mg 2 Si Mg 2 Si
• tt-AIFeSi applying usually as needles or branched
• AI 3 Ni applying usually blocky, sometimes elongated
• AICrNi(Fe) applying usually blocky.
• Higher Mg values (up to 20 at-%) are found in tt-AIFeSi, but also Ni concentrations up to 2.5 at-%.
• Chromium resides in tt-AIFeSi and AI 3 Ni phases (about 0.1 - 0.2 at-%) but shows a major function in AICrNi(Fe) phases.
• AI3Ni phases had a blocky, sometimes acicular morphology, and a typical size between 1 pm to 5 pm (blocky); needles were rare and could be up to 10 pm. They were often found close to tt-AIFeSi phases, and between tt-AIFeSi and AICrNi(Fe) phases.
• the chemical composition of AI 3 Ni phases was as follows: Al 70 - 75 at-%; Ni 7.5 - 17.5 at-%; Si 2 - 19 at-%;
• AICrNi(Fe) phases had a blocky morphology, and a typical size between 1 pm to 5 pm (sometimes up to 7.5 pm). They were often found close to tt-AIFeSi and AI 3 Ni phases.
• the chemical composition of AICrNi(Fe) phases was as follows:
• Al about 70 at-%; Ni 4 - 6 at-%; Si 10 - 15 at-%; Mg 0.5 - 1 .5 at-%; Fe 2 at-%; Cr 5 - 7.5 at-%.
• tt-AIFeSi applying usually as fragments
• AI 2 oNi 2 Fe applying usually as fragments, blocky or acicular
• AI 3 Ni applying usually blocky, rounded
• AICrNi(Fe) applying usually blocky
• AI 3 Ni phases had a small rounded or blocky morphology, and a typical size between 1 pm to 3 pm. Very few of these phases were found; upon heat treatment theses phases tend to fragment or to dissolve.
• the chemical composition of AI 3 Ni phases was as follows:
• AICrNi(Fe) phases had a blocky morphology, and a typical size between 1 pm to 5 pm (sometimes up to 7.5 pm). They were often found close to tt-AIFeSi and AI3Ni phases. Upon heat treatment AICrNi(Fe) phases showed hardly any change.
• the chemical composition of AICrNi(Fe) phases was as follows:
• AI 2 oNi 2 Fe phases had a fragmented or acicular morphology, mostly comprised between 1 pm to 10 pm.
• the chemical composition of these phases was as follows:

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• Crystallography & Structural Chemistry (AREA)
• Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
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• 2021
  • 2021-06-07 EP EP21178006.9A patent/EP4101941A1/de not_active Withdrawn
• 2022
  • 2022-06-07 EP EP22819725.7A patent/EP4352273A1/de active Pending
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