EP0559694B1 - Method of preparing improved hyper-eutectic alloys and composites based thereon - Google Patents

Method of preparing improved hyper-eutectic alloys and composites based thereon Download PDF

Info

Publication number
EP0559694B1
EP0559694B1 EP91920402A EP91920402A EP0559694B1 EP 0559694 B1 EP0559694 B1 EP 0559694B1 EP 91920402 A EP91920402 A EP 91920402A EP 91920402 A EP91920402 A EP 91920402A EP 0559694 B1 EP0559694 B1 EP 0559694B1
Authority
EP
European Patent Office
Prior art keywords
particles
alloy
refractory
eutectic
hyper
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP91920402A
Other languages
German (de)
French (fr)
Other versions
EP0559694A1 (en
Inventor
David James Lloyd
Iljoon Jin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rio Tinto Alcan International Ltd
Original Assignee
Alcan International Ltd Canada
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CA002030928A external-priority patent/CA2030928A1/en
Application filed by Alcan International Ltd Canada filed Critical Alcan International Ltd Canada
Publication of EP0559694A1 publication Critical patent/EP0559694A1/en
Application granted granted Critical
Publication of EP0559694B1 publication Critical patent/EP0559694B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals
    • C22C1/1036Alloys containing non-metals starting from a melt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-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

Definitions

  • This invention relates to a method of preparing improved hyper-eutectic alloys and metal matrix composites containing such alloys.
  • Metal matrix composite materials have gained increasing acceptance as structural materials. Such composites typically are composed of reinforcing particles, such as fibres, grit, powder or the like that are embedded within a metallic matrix.
  • the reinforcement imparts strength, stiffness and other desirable properties to the composite, while the matrix protects the fibres and transfers load within the composite.
  • the two components, matrix and reinforcement thus cooperate to achieve results which are improved over what either could provide on its own.
  • a typical composite is an aluminum alloy reinforced with particles of silicon carbide or alumina.
  • a major difficulty in the production of good quality metal matrix composites is segregation of the reinforcing particles.
  • the segregation of particles occurs in the liquid state as well as during solidification.
  • the segregation in the liquid state can be overcome by a proper mixing of the liquid.
  • the particles may still segregate during solidification.
  • the reinforcing particles can be rejected ahead of the solidification interface, and may agglomerate in the interdendritic liquid which solidifies last.
  • reinforcement particles are pushed by the solidification interface or are engulfed is primarily dependent upon the degree of wetting between the particles and the solid surface. If the solid surface wets the particles, they are engulfed by the solid surface. In this case the particle distribution in the solidified material is as uniform as it was in the liquid state. On the other hand, if the solid surface, e.g. aluminum dendrite surface, does not wet the particles, they are pushed away, resulting in interdendritic segregation.
  • intermetallic compounds may precipitate directly from a melt of the alloy. These intermetallic compounds often tend to be coarse, brittle particles, and these particles tend to segregate due to density difference, particularly when the solidification rate is slow.
  • a hypereutectic LM30 Al-Si alloy containing 3 wt.% of graphite particles is analyzed.
  • the LM30 alloy specification defines an alloy composition which contains,among others, from 16 to 18 wt.% Si, from 0.3 to 0.7 wt.% Mg, up to 1.1 wt.% Fe, and up to 0.3 wt.% Mn.
  • Fig. 2 shows a preferential nucleation of primary silicon on the surface of the graphite.
  • non-metallic refractory particles when added to a molten hyper-eutectic Al-Si-Mn alloy can be engulfed durina solidification by an intermetallic phase which solidifies first from the molten hypereutectic alloy during solidification thereof such that the refractory particles are engulfed by the intermetallic phase as it grows during solidification. Because the intermetallics engulf the refractory particles, there is no longer a tendency for the refractory particles to segregate to the interdendritic regions and they remain homogeneously distributed throughout an as-solidified ingot. The presence of excess alloying elements in the hyper-eutectic alloy beyond eutectic amounts is the mechanism for the formation of the desired intermetallic phase and this intermetallic phase forms automatically during cooling provided the alloy being cooled is a hyper-eutectic alloy.
  • One embodiment of the invention is a method for preparing a composite of an aluminum alloy and particles of a non-metallic refractory material, which comprise melting an aluminum alloy; adding particles of non-metallic refractory material to the molten aluminum matrix; mixing together the molten aluminum alloy and the particles of refractory material; and casting the resulting mixture.
  • the aluminum alloy is a hyper-eutectic aluminum alloy comprising, in percentages by weight, 7-16% silicon, 0.5-3.0% manganese, 0-5.0% copper, 0-5.0% nickel, 0-1.0% iron, 0-0.2% titanium and 0.3-2.0% magnesium and the balance of the alloy being aluminum and inevitable impurities and the excess alloying element or elements of the hyper-eutectic molten aluminum alloy solidify first from the molten aluminum matrix during solidification thereof to form intermetallics comprising Mn 3 Si 2 Al 15 which engulf said refractory particles and keep them homogeneously distributed throughout the solidified product.
  • the refractory particles act as a refiner for precipitating intermetallics.
  • the use of unreinforced hyper-eutectic alloys is very restricted because they often form coarse, brittle intermetallic particles on solidification, and the intermetallic particles tend to segregate due to the density difference, particularly when the solidification rate is not rapid.
  • phosphorus additions and fluxing have previously been required to refine the primary silicon to a size suitable for good wear properties.
  • the efficiency of phosphorus to refine primary silicon decreases with increasing holding time of the melt, complicating the casting practice.
  • refractory particles such as silicon carbide particles
  • the addition of refractory particles, such as silicon carbide particles, according to the present invention can nucleate and refine these intermetallics, as well as modify their morphology, so that the deleterious effect of coarse intermetallics is reduced. This is of particular value for alloys that are intended for high temperature use.
  • Such high temperature alloys may be used in casting applications, or as wrought products, such as forgings and extrusions.
  • the alloy composites of this invention in which the refractory particles act as a refiner for precipitating intermetallics have superior high temperature strength, making them useful for applications such as cast brake rotors.
  • the refractory particles may also serve as reinforcing particles in a composite with a hyper-eutectic alloy.
  • they may be used not only to refine a hyper-eutectic alloy, but also to form a composite therewith.
  • the particles are typically used in very small sizes, e.g. less than 1 ⁇ m.
  • they when they are used also for reinforcing the alloy, they may be used in much larger sizes, e.g. up to 20 ⁇ m.
  • For reinforcing they are typically used in sizes in the range of 5-20 ⁇ m and preferably 10-15 ⁇ m.
  • the non-metallic refractory material is preferably a metal oxide, metal nitride, metal carbide or metal silicide.
  • the most preferred refractory material is silicon carbide or aluminum oxide particulate.
  • the procedure of the present invention for making a composite functions best with reinforcing particles which are relatively equi-dimensional, e.g. having an aspect ratio in any direction of no more than 5:1.
  • the reinforcing particles are typically added in amounts of 5-40% by volume, preferably 10-25% by volume. It has been found that silicon carbide reinforcing particles are engulfed by silicon crystals formed during solidification of the composite.
  • the invention also relates to new aluminum alloy products having improved high temperature properties.
  • One of the novel products is a particle reinforced aluminum alloy casting in which the alloy is a hyper-eutectic alloy and the excess alloying element or elements of the hypereutectic alloy have solidified first from the molten metal matrix and have formed intermetallics during solidification which have engulfed the refractory particles and kept them homogeneously distributed throughout the solidified product.
  • Another novel product is a refined aluminum alloy casting in which intermetallics formed during solidification are uniformly dispersed as fine particles because of the refining effect of particles of non-metallic refractory material contained in the alloy.
  • the alloy of the novel products is a hyper-eutectic aluminum alloy containing silicon, magnesium and manganese, preferably in the amounts 7-16 wt% silicon, 0.5-3.0 wt% manganese, 0-5.0 wt% copper, 0-5.0 wt% nickel, 0-1.0 wt% iron, 0-0.2 wt% titanium and 0.3-2.0 wt% magnesium and the balance of the alloy being aluminum and inevitable impurities.
  • the silicon assists fluidity and stabilizes the refractory particles; below 7% silicon the refractory material tends to be unstable while above 16% coarse intermetallics are formed and the composite becomes embrittled.
  • the magnesium improves wetting and provides strengthening; below 0.3% magnesium the wetting is poor, while above 2% there is shrinkage porosity.
  • the manganese forms intermetallics providing uniform refractory particle distribution and improved high temperature strength; below 0.5% manganese there is no improvement in high temperature strength and above 3.0% the casting temperature becomes too high.
  • the alloy also preferably contains up to 5.0 wt% copper. This improves elevated temperature strength with amounts above 5.0% providing poor casting fluidity and embrittlement.
  • Another optional component is nickel which may also be present in amounts up to 5.0 wt%. It also improves elevated temperature strength, although amounts above 5.0% cause coarse intermetallics and embrittlement.
  • a further common optional element is iron which may be present in amounts up to 1.0 wt%. At amounts above 1.0 wt% there is the danger of forming coarse intermetallics which cannot be refined by the refractory particles.
  • the alloy may also contain up to 0.2 wt%, preferably 0.1-0.2 wt%, titanium as a grain refiner.
  • Alloys of particular interest for high temperature applications are those containing substantial amounts of Mn.
  • Such alloys may be produced by adding Mn to traditional high temperature alloy compositions until the hyper-eutectic range is reached. This is mixed with refractory particles, e.g. which refine the intermetallics and distribute the particles uniformly throughout the matrix.
  • intermetallic While a typical intermetallic is a compound formed of at least two metallic components, within the process of this invention, silicon behaves in the manner of an intermetallic in its ability to wet and engulf refractory particles. Accordingly, the term "intermetallic" as used in this invention includes silicon.
  • An aluminum matrix composite was prepared by mixing 15% by volume of silicon carbide particles having sizes in the range of 10-15 ⁇ m with a melt of A356 aluminum alloy containing 6.5 to 7.5% Si and 0.3 to 0.45% Mg. This was cast and solidified to form an ingot having the microstructure shown in Figure 1. It will be seen that the reinforcing particles have been pushed ahead of the solidification interface and are not uniformly dispersed throughout the ingot.
  • Another ingot was prepared from a melt of Al - 16% Si alloy and 15% by volume of silicon carbide particles having particle sizes in the range of 10-15 ⁇ m. These were thoroughly mixed and the mixture was then cast and solidified to form an ingot.
  • the ingot formed had the microstructure shown in Figure 2 and it will be seen that the reinforcing particles are uniformly spaced and are engulfed by silicon crystals.
  • the silicon carbide particles also refined the silicon.
  • Two melts were prepared by heating aluminum containing 16 wt% silicon to a temperature of 750°C.
  • One melt was cast "as is” to form an ingot and a second melt was mixed with 15% by volume of silicon carbide particles having sizes in the range of 10-15 microns and then cast to form an ingot.
  • the ingots were identical in size and were cooled and solidified under identical conditions.
  • Figure 8 shows the microstructure of the ingot without the refractory particles
  • Figure 9 shows the microstructure of the ingot with the refractory particles. The refinement of the silicon is clearly evident.
  • Example 2 To illustrate the effectiveness of the refinement according to this invention, the procedure of Example 2 was repeated using a melt of Al - 7% Si - 2% Mn alloy. One cast ingot was made from the alloy itself and a second cast ingot was made from a composite of the alloy and 15% by volume of silicon carbide particles. Fig. 10 shows the microstructure of the cast alloy and Fig. 11 shows the microstructure of the cast composite. It can be seen that the primary Mn 3 Si 2 Al 15 intermetallic dendrites in the cast alloy are completely refined by the SiC particles.
  • Three aluminum matrix composites were prepared by mixing 15% by volume of silicon carbide particles having sizes in the range of 10-15 ⁇ m with three different aluminum alloy melts.
  • the matrix alloys had the following compositions:
  • the composites so formed were cast and solidified in the form of 12.7 mm diameter as-cast test bars and 57 mm diameter ingots.
  • the as-cast test bars were held for 100 hours at 250°C, and tensile tested at the soak temperature.
  • the 57 mm diameter ingots were extruded at 450°C to 9.5 mm diameter rod.
  • Test bars were machined from the rod, and held at between 200 and 400°C for various times to examine the effect of long time exposure on the high temperature strength. The results are shown in Figure 12-15.
  • High temperature composite alloys may be used in casting applications, or as wrought products such as forgings and extrusions.
  • Figure 12 shows the strength retention of as-cast material after 100 hrs at 250°C, which is relevant for applications such as cast brake rotors. The figure shows that the new alloy composites have superior high temperature strength to the presently used A356-SiC composite. It is also apparent that adding SiC reinforcement to the unreinforced alloys adds to the high temperature performance of these materials.
  • the invention provides techniques for improving hyper-eutectic alloys, which alloys can be used for the manufacture of a variety of industrial products by conventional techniques.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

A method is described for preparing a refined or reinforced eutectic or hyper-eutectic metal alloy, comprising: melting the eutectic or hyper-eutectic metal alloy, adding particles of non-metallic refractory material to the molten metal matrix, mixing together the molten metal alloy and the particles of refractory material, and casting the resulting mixture under conditions causing precipitation of at least one intermetallic phase from the molten metal matrix during solidification thereof such that the intermetallics formed during solidification wet and engulf said refractory particles. The added particles may be very small and serve only to refine the precipitating intermetallics in the alloy or they may be larger and serve as reinforcing particles in a composite with the alloy. The products obtained are also novel.

Description

Technical Field
This invention relates to a method of preparing improved hyper-eutectic alloys and metal matrix composites containing such alloys.
Background Art
Metal matrix composite materials have gained increasing acceptance as structural materials. Such composites typically are composed of reinforcing particles, such as fibres, grit, powder or the like that are embedded within a metallic matrix. The reinforcement imparts strength, stiffness and other desirable properties to the composite, while the matrix protects the fibres and transfers load within the composite. The two components, matrix and reinforcement, thus cooperate to achieve results which are improved over what either could provide on its own. A typical composite is an aluminum alloy reinforced with particles of silicon carbide or alumina.
A major difficulty in the production of good quality metal matrix composites is segregation of the reinforcing particles. The segregation of particles occurs in the liquid state as well as during solidification. The segregation in the liquid state can be overcome by a proper mixing of the liquid. However, even if the particles are uniformly distributed in the liquid state, they may still segregate during solidification. When metal matrix composites are in the process of solidifying, the reinforcing particles can be rejected ahead of the solidification interface, and may agglomerate in the interdendritic liquid which solidifies last. For instance, in aluminum matrix composites, solid α-aluminum dendrites are formed and the reinforcing particles are pushed ahead of the growing dendrites to be finally trapped in the last to solidify interdendritic liquid. The reinforcing particles are not found inside the aluminum dendrites and, in this sense, it can be said that the aluminum dendrites do not "wet" the reinforcing particles. This results in a highly inhomogeneous distribution of reinforcing particles in the as-cast materials.
Whether reinforcement particles are pushed by the solidification interface or are engulfed is primarily dependent upon the degree of wetting between the particles and the solid surface. If the solid surface wets the particles, they are engulfed by the solid surface. In this case the particle distribution in the solidified material is as uniform as it was in the liquid state. On the other hand, if the solid surface, e.g. aluminum dendrite surface, does not wet the particles, they are pushed away, resulting in interdendritic segregation.
In certain alloy systems, such as eutectic or hyper-eutectic systems, intermetallic compounds may precipitate directly from a melt of the alloy. These intermetallic compounds often tend to be coarse, brittle particles, and these particles tend to segregate due to density difference, particularly when the solidification rate is slow.
There is some evidence in the prior art of a degree of wetting between refractory particles and intermetallic surfaces. For instance P.K. Rohatgi, "Interfaces in Metal Matrix Composites", p. 185, The Metallurgical Society/AIME, New Orleans, 2-6 March 1986, has shown an example of primary NiAl3 nucleating on graphite particles during the solidification of a hyper-eutectic Al-Ni alloy. He also noted that there is a tendency for primary Si to nucleate on graphite and alumina particles during the solidification of a hyper-eutectic Al-Si alloy.
Solidification studies of grain refining Al-Ti-B alloys are described in K. Kuisalaas and L. Backerud, Solidification Process 1987, p. 137, Institute of Metals, Sheffield, U.K., 21-24 September, 1987. These studies noted that TiAl3 inter-metallics tended to adhere to the surface of TiB2 particles.
A study on aluminum alloys far elevation temperature applications is described in D.A. Granger et al.,
"Aluminum Alloys for Elevated Temperature Applications" p. 777-778, AFS Transactions, 86-143. Traditionally, casting alloys for elevated temperature applications were made by adding large amounts of Cu or Ni, e.g. up to about 8 wt% Cu and 5.5 wt% Ni. It has been generally understood that high volume fractions of the intermetallics so formed improve the high temperature properties. However, the amount of these elements which could be added was restricted because they formed large brittle intermetallic primaries on solidification if the addition was beyond a certain limit. The amount of Mn that could be added was limited to less than 0.5 wt%.
U.S. Patent No. 3,951,651 issued April 20, 1976 describes aluminum-silicon-iron alloys which can also contain reinforcing particles. However, the US patent does not describe a system where the excess elements from a hyper-eutectic alloy solidify first thereby engulfing the reinforcing particles by the intermetallics thus formed.
In S. Das et al., "Some Modified Structures of the Matrix in Cast Al-Alloy-Graphite Particle Composites", Z. Metallkde., Vol. 80 (1989) 6, p. 444-446, a hypereutectic LM30 Al-Si alloy containing 3 wt.% of graphite particles is analyzed. The LM30 alloy specification defines an alloy composition which contains,among others, from 16 to 18 wt.% Si, from 0.3 to 0.7 wt.% Mg, up to 1.1 wt.% Fe, and up to 0.3 wt.% Mn. Fig. 2 shows a preferential nucleation of primary silicon on the surface of the graphite.
It is the object of the present invention to provide a technique for improving hyper-eutectic alloys and for solving the problem of the segregation of the reinforcement particles in metal matrix composites made from hyper-eutectic alloys which tends to occur during solidification. It is a further object of the invention to produce new alloy products having improved high temperature properties.
Disclosure of the Invention
According to the present invention, it has now been discovered that non-metallic refractory particles when added to a molten hyper-eutectic Al-Si-Mn alloy can be engulfed durina solidification by an intermetallic phase which solidifies first from the molten hypereutectic alloy during solidification thereof such that the refractory particles are engulfed by the intermetallic phase as it grows during solidification. Because the intermetallics engulf the refractory particles, there is no longer a tendency for the refractory particles to segregate to the interdendritic regions and they remain homogeneously distributed throughout an as-solidified ingot. The presence of excess alloying elements in the hyper-eutectic alloy beyond eutectic amounts is the mechanism for the formation of the desired intermetallic phase and this intermetallic phase forms automatically during cooling provided the alloy being cooled is a hyper-eutectic alloy.
One embodiment of the invention is a method for preparing a composite of an aluminum alloy and particles of a non-metallic refractory material, which comprise melting an aluminum alloy; adding particles of non-metallic refractory material to the molten aluminum matrix; mixing together the molten aluminum alloy and the particles of refractory material; and casting the resulting mixture. According to the novel feature, the aluminum alloy is a hyper-eutectic aluminum alloy comprising, in percentages by weight, 7-16% silicon, 0.5-3.0% manganese, 0-5.0% copper, 0-5.0% nickel, 0-1.0% iron, 0-0.2% titanium and 0.3-2.0% magnesium and the balance of the alloy being aluminum and inevitable impurities and the excess alloying element or elements of the hyper-eutectic molten aluminum alloy solidify first from the molten aluminum matrix during solidification thereof to form intermetallics comprising Mn3Si2Al15 which engulf said refractory particles and keep them homogeneously distributed throughout the solidified product.
Best Modes For Carrying Out the Invention
In one preferred embodiment of the invention, the refractory particles act as a refiner for precipitating intermetallics. The use of unreinforced hyper-eutectic alloys is very restricted because they often form coarse, brittle intermetallic particles on solidification, and the intermetallic particles tend to segregate due to the density difference, particularly when the solidification rate is not rapid. For instance, in commercial hyper-eutectic Al-Si alloys, such as A390 alloy, used for engine block applications, phosphorus additions and fluxing have previously been required to refine the primary silicon to a size suitable for good wear properties. However, the efficiency of phosphorus to refine primary silicon decreases with increasing holding time of the melt, complicating the casting practice. On the other hand, the addition of refractory particles, such as silicon carbide particles, according to the present invention can nucleate and refine these intermetallics, as well as modify their morphology, so that the deleterious effect of coarse intermetallics is reduced. This is of particular value for alloys that are intended for high temperature use.
There is a need for aluminum alloy products capable of extended use at high temperatures. Such high temperature alloys may be used in casting applications, or as wrought products, such as forgings and extrusions. The alloy composites of this invention in which the refractory particles act as a refiner for precipitating intermetallics have superior high temperature strength, making them useful for applications such as cast brake rotors.
According to a further preferred embodiment, the refractory particles may also serve as reinforcing particles in a composite with a hyper-eutectic alloy. Thus, they may be used not only to refine a hyper-eutectic alloy, but also to form a composite therewith. When the particles are used solely to refine an alloy, they are typically used in very small sizes, e.g. less than 1 µm. On the other hand, when they are used also for reinforcing the alloy, they may be used in much larger sizes, e.g. up to 20 µm. For reinforcing, they are typically used in sizes in the range of 5-20 µm and preferably 10-15 µm. When the particles are used in reinforcing sizes, the wetting and engulfment of them by the intermetallic phase prevent the problem of segregating to the interdendritic regions during cooling.
The non-metallic refractory material is preferably a metal oxide, metal nitride, metal carbide or metal silicide. The most preferred refractory material is silicon carbide or aluminum oxide particulate.
The procedure of the present invention for making a composite functions best with reinforcing particles which are relatively equi-dimensional, e.g. having an aspect ratio in any direction of no more than 5:1. The reinforcing particles are typically added in amounts of 5-40% by volume, preferably 10-25% by volume. It has been found that silicon carbide reinforcing particles are engulfed by silicon crystals formed during solidification of the composite.
The invention also relates to new aluminum alloy products having improved high temperature properties. One of the novel products is a particle reinforced aluminum alloy casting in which the alloy is a hyper-eutectic alloy and the excess alloying element or elements of the hypereutectic alloy have solidified first from the molten metal matrix and have formed intermetallics during solidification which have engulfed the refractory particles and kept them homogeneously distributed throughout the solidified product. Another novel product is a refined aluminum alloy casting in which intermetallics formed during solidification are uniformly dispersed as fine particles because of the refining effect of particles of non-metallic refractory material contained in the alloy.
The alloy of the novel products is a hyper-eutectic aluminum alloy containing silicon, magnesium and manganese, preferably in the amounts 7-16 wt% silicon, 0.5-3.0 wt% manganese, 0-5.0 wt% copper, 0-5.0 wt% nickel, 0-1.0 wt% iron, 0-0.2 wt% titanium and 0.3-2.0 wt% magnesium and the balance of the alloy being aluminum and inevitable impurities. The silicon assists fluidity and stabilizes the refractory particles; below 7% silicon the refractory material tends to be unstable while above 16% coarse intermetallics are formed and the composite becomes embrittled. The magnesium improves wetting and provides strengthening; below 0.3% magnesium the wetting is poor, while above 2% there is shrinkage porosity. The manganese forms intermetallics providing uniform refractory particle distribution and improved high temperature strength; below 0.5% manganese there is no improvement in high temperature strength and above 3.0% the casting temperature becomes too high.
The alloy also preferably contains up to 5.0 wt% copper. This improves elevated temperature strength with amounts above 5.0% providing poor casting fluidity and embrittlement. Another optional component is nickel which may also be present in amounts up to 5.0 wt%. It also improves elevated temperature strength, although amounts above 5.0% cause coarse intermetallics and embrittlement.
A further common optional element is iron which may be present in amounts up to 1.0 wt%. At amounts above 1.0 wt% there is the danger of forming coarse intermetallics which cannot be refined by the refractory particles.
The alloy may also contain up to 0.2 wt%, preferably 0.1-0.2 wt%, titanium as a grain refiner.
A series of aluminum alloys and the intermetallic phases that precipitate therefrom are shown in Table 1 below:
Alloy Intermetallic
Al - 16 wt% Si --- Si
Al - 12 wt% Si - 1.5 wt% Fe FeSiAl5
Al - 7 wt% Si - 2 wt% Fe Fe2SiAl8
Al - 12 wt% Si - 1.5 wt% Mn Mn3Si2Al15
Al - 11 wt% Si - 5 wt% Ni NiAl3
Al - 10 wt% Si - 10 wt% Mg Mg2Si
Al - 10 wt% Si - 2 wt% Cr Cr5Si8Al2
Al - 16 wt% Si - 0.3 wt% Ti Ti(AlSi)2
Al - 10 wt% Si - 0.5 wt% Zr ZrAl3
Alloys of particular interest for high temperature applications are those containing substantial amounts of Mn. Such alloys may be produced by adding Mn to traditional high temperature alloy compositions until the hyper-eutectic range is reached. This is mixed with refractory particles, e.g. which refine the intermetallics and distribute the particles uniformly throughout the matrix.
Examples of new composites thus produced are given in Table II below:
Alloy
Al-10 wt% Si-1.2 wt% Mn-0.4 wt% Mg-15 vol% SiC
Al-10 wt% Si-1.2 wt% Mn-0.4 wt% Mg-5 wt% Ni-15 vol% SiC
Al-10 wt% Si-1.2 wt% Mn-1.0 wt% Mg-5 wt% Ni-2.5 wt% Cu -15 vol% SiC
While a typical intermetallic is a compound formed of at least two metallic components, within the process of this invention, silicon behaves in the manner of an intermetallic in its ability to wet and engulf refractory particles. Accordingly, the term "intermetallic" as used in this invention includes silicon.
Brief Description of the Drawings
In the drawings which illustrate the present invention:
  • Figure 1 is a photomicrograph of an A-356 alloy casting with refractory particles,
  • Figures 2-7 are photomicrographs of hyper-eutectic castings with refractory particles,
  • Figure 8 is a photomicrograph of a hyper-eutectic alloy casting without refractory particles,
  • Figure 9 is a photomicrograph of a hyper-eutectic alloy casting with refractory particles,
  • Figure 10 is a photomicrograph of a further hyper-eutectic alloy casting without refractory particles,
  • Figure 11 is a photomicrograph of a casting of the alloy of Fig. 10 with refractory particles,
  • Figure 12 is bar graphs showing yield strengths of different matrix alloys and composites of the invention, and
  • Figures 13-15 are plots of stress as a function of soak time for three different cast composites of the invention.
  • Example 1 (Comparative)
    An aluminum matrix composite was prepared by mixing 15% by volume of silicon carbide particles having sizes in the range of 10-15 µm with a melt of A356 aluminum alloy containing 6.5 to 7.5% Si and 0.3 to 0.45% Mg. This was cast and solidified to form an ingot having the microstructure shown in Figure 1. It will be seen that the reinforcing particles have been pushed ahead of the solidification interface and are not uniformly dispersed throughout the ingot.
    Example 2 (a) (Comparative)
    Another ingot was prepared from a melt of Al - 16% Si alloy and 15% by volume of silicon carbide particles having particle sizes in the range of 10-15 µm. These were thoroughly mixed and the mixture was then cast and solidified to form an ingot. The ingot formed had the microstructure shown in Figure 2 and it will be seen that the reinforcing particles are uniformly spaced and are engulfed by silicon crystals. The silicon carbide particles also refined the silicon.
    Example 2 (b) (Comparative)
    The above procedure was repeated using a melt of Al-12 Si-1.5 Mn, to which was added 15% by volume of the same silicon carbide particles. The results in Figure 3 show particle engulfment by Mn3Si2Al15 crystals.
    Example 2 (c) (Comparative)
    The above procedure was again repeated using a melt of Al-7Si-2Fe, to which was added 15% by volume of the same silicon carbide particles. The results in Figure 4 show particle engulfment by α-AlFeSi crystals (Fe2SiAl8).
    Example 2 (d) (Comparative)
    The above procedure was again repeated using a melt of Al-12Si-1.5 Fe, to which was added 15% by volume of the same silicon carbide particles. The results in Figure 5 show particle engulfment by β-AlFeSi crystals (FeSiAl5).
    Example 2 (e) (Comparative)
    The above procedure was again repeated using a melt of Al-11Si-5Ni, to which was added 15% by volume of the same silicon carbide particles. The result in Figure 6 show particle engulfment by NiAl3 crystals.
    Example 2 (f) (Comparative)
    The above procedure was again repeated using a melt of Al-10Si-10Mg, to which was added 15% by volume of the same silicon carbide particles. The results in Figure 7 show particle engulfment by Mg2Si crystals.
    Example 3 (Comparative)
    Two melts were prepared by heating aluminum containing 16 wt% silicon to a temperature of 750°C. One melt was cast "as is" to form an ingot and a second melt was mixed with 15% by volume of silicon carbide particles having sizes in the range of 10-15 microns and then cast to form an ingot. The ingots were identical in size and were cooled and solidified under identical conditions. Figure 8 shows the microstructure of the ingot without the refractory particles, while Figure 9 shows the microstructure of the ingot with the refractory particles. The refinement of the silicon is clearly evident.
    Example 4 (Comparative)
    To illustrate the effectiveness of the refinement according to this invention, the procedure of Example 2 was repeated using a melt of Al - 7% Si - 2% Mn alloy. One cast ingot was made from the alloy itself and a second cast ingot was made from a composite of the alloy and 15% by volume of silicon carbide particles. Fig. 10 shows the microstructure of the cast alloy and Fig. 11 shows the microstructure of the cast composite. It can be seen that the primary Mn3Si2Al15 intermetallic dendrites in the cast alloy are completely refined by the SiC particles.
    Example 5
    Three aluminum matrix composites were prepared by mixing 15% by volume of silicon carbide particles having sizes in the range of 10-15 µm with three different aluminum alloy melts. The matrix alloys had the following compositions:
    Alloy A:
    Al - 10 wt% Si - 1.2 wt% Mn - 0.4 wt% Mg
    Alloy B:
    Al - 10 wt% Si - 1.2 wt% Mn - 0.4 wt% Mg - 5 wt% Ni
    Alloy C:
    Al - 10 wt% Si - 1.2 wt% Mn - 1.0 wt% Mg - 5 wt% Ni - 2.5 wt% Cu
    The composites so formed were cast and solidified in the form of 12.7 mm diameter as-cast test bars and 57 mm diameter ingots. The as-cast test bars were held for 100 hours at 250°C, and tensile tested at the soak temperature. The 57 mm diameter ingots were extruded at 450°C to 9.5 mm diameter rod. Test bars were machined from the rod, and held at between 200 and 400°C for various times to examine the effect of long time exposure on the high temperature strength. The results are shown in Figure 12-15.
    High temperature composite alloys may be used in casting applications, or as wrought products such as forgings and extrusions. Figure 12 shows the strength retention of as-cast material after 100 hrs at 250°C, which is relevant for applications such as cast brake rotors. The figure shows that the new alloy composites have superior high temperature strength to the presently used A356-SiC composite. It is also apparent that adding SiC reinforcement to the unreinforced alloys adds to the high temperature performance of these materials.
    In wrought products additional softening mechanisms, such as sub-structure and grain size coarsening, may operate which are usually absent in as-cast material. Figures 13-15 show the time dependence of the softening at 250, 300 and 400°C. All 3 alloys show rapid softening in the first 10 hours of exposure, but beyond this are relatively stable. This initial softening is due to normal, precipitate coarsening and resolution, while after this has occurred the alloys have excellent long term stability. Comparing the extrusion results with those for as-cast test bars in Figure 12, the extruded composites have somewhat superior strength.
    Industrial Applicability
    It will be apparent from the above disclosure that the invention provides techniques for improving hyper-eutectic alloys, which alloys can be used for the manufacture of a variety of industrial products by conventional techniques.

    Claims (16)

    1. A method for preparing a composite of an aluminum alloy and particles of a non-metallic refractory material, comprising:
      melting an aluminum alloy;
      adding particles of non-metallic refractory material to the molten aluminum matrix;
      mixing together the molten aluminum alloy and the particles of refractory material; and
      casting the resulting mixture;
         characterized in that the aluminum alloy is a hyper-eutectic metal alloy comprising, in percentages by weight, 7-16% silicon, 0.5-3.0% manganese, 0-5.0% copper, 0-5.0% nickel, 0-1.0% iron, 0-0.2% titanium and 0.3-2.0% magnesium and the balance of the alloy being aluminum and inevitable impurities and the excess alloying element or elements of the hyper-eutectic molten aluminum alloy solidify first from the molten aluminum matrix during solidification thereof to form intermetallics which comprise Mn3Si2Al15 and which engulf said refractory particles and keep them homogeneously distributed throughout the solidified product.
    2. A method according to claim 1 characterized in that the refractory particles are selected from the group consisting of a metal oxide, metal nitride, metal carbide and metal silicide.
    3. A method according to claim 2 characterized in that the refractory particles comprise silicon carbide.
    4. A method according to any one of claims 1-3 characterized in that the refractory particles are reinforcing particles and have sizes up to 20 µm.
    5. A method according to any one of claims 1-3 characterized in that the refractory particles are reinforcing particles having sizes in the range of 10 - 15 µm.
    6. A method according to any one of claims 1-3 characterized in that the refractory particles have sizes of less than 1 µm.
    7. A method according to claim 6 characterized in that the refractory particles nucleate and refine the intermetallics.
    8. An aluminum alloy composite casting comprising a matrix of aluminum alloy having dispersed therethrough particles of non-metallic refractory material,
         characterized in that the aluminum alloy is an Al-Si-Mn hyper-eutectic alloy comprising, in percentage by weight, 7-16% silicon, 0.5-3.0% manganese, 0-5.0% copper, 0-5.0% nickel, 0-1.0% iron, 0-0.2% titanium and 0.3-2.0% magnesium and the balance of the alloy being aluminum and inevitable impurities, in which the excess alloying element or elements of the hyper-eutectic alloy have solidified first from the molten aluminum matrix and have formed intermetallics comprising Mn3Si2Al15 during solidification which have engulfed the refractory particles and kept them homogenerously distributed throughout the solidified product.
    9. A casting according to claim 8 characterized in that the refractory particles are selected from the group consisting of a metal oxide, metal nitride, metal carbide and metal silicide.
    10. A casting according to claim 8 characterized in that the refractory particles comprise silicon carbide.
    11. A casting according to any one of claims 8-10 characterized in that the refractory particles have sizes up to 20 µm.
    12. A casting according to any one of claims 8-10 characterized in that the refractory particles have sizes in the range of 10 - 15 µm.
    13. A casting according to any one of claims 8-10 characterized in that the refractory particles have sizes of less than 1 µm.
    14. A casting according to any one of claims 8-13 characterized in that the particles have an aspect ratio in any direction of no more than 5:1.
    15. A casting according to any one of claims 8-14 characterized in that the particles are present in an amount of 5-40% by volume.
    16. A casting according to any one of claims 8-15 characterized in that titanium is present in the alloy in an amount of 0.1-0.2%.
    EP91920402A 1990-11-27 1991-11-27 Method of preparing improved hyper-eutectic alloys and composites based thereon Expired - Lifetime EP0559694B1 (en)

    Applications Claiming Priority (5)

    Application Number Priority Date Filing Date Title
    CA2030928 1990-11-27
    CA002030928A CA2030928A1 (en) 1990-11-27 1990-11-27 Method of preparing improved eutectic or hyper-eutectic alloys and composites based thereon
    US77012491A 1991-10-02 1991-10-02
    US770124 1991-10-02
    PCT/CA1991/000418 WO1992009711A1 (en) 1990-11-27 1991-11-27 Method of preparing eutectic or hyper-eutectic alloys and composites based thereon

    Publications (2)

    Publication Number Publication Date
    EP0559694A1 EP0559694A1 (en) 1993-09-15
    EP0559694B1 true EP0559694B1 (en) 1998-09-16

    Family

    ID=25674383

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP91920402A Expired - Lifetime EP0559694B1 (en) 1990-11-27 1991-11-27 Method of preparing improved hyper-eutectic alloys and composites based thereon

    Country Status (4)

    Country Link
    EP (1) EP0559694B1 (en)
    JP (1) JP3492681B2 (en)
    DE (1) DE69130227T2 (en)
    WO (1) WO1992009711A1 (en)

    Families Citing this family (10)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US6086688A (en) * 1997-07-28 2000-07-11 Alcan International Ltd. Cast metal-matrix composite material and its use
    GB9804599D0 (en) * 1998-03-05 1998-04-29 Aeromet International Plc Cast aluminium-copper alloy
    JP3690171B2 (en) * 1999-03-16 2005-08-31 株式会社日立製作所 Composite material and its production method and application
    WO2010013080A1 (en) * 2008-07-29 2010-02-04 Indian Institute Of Science A process for preparation of nano ceramic-metal matrix composites and apparatus thereof
    CN101787454B (en) * 2010-04-12 2011-11-23 中国船舶重工集团公司第十二研究所 Method for preparing multicomponent reinforced aluminum-base composite material
    US10370742B2 (en) 2013-03-14 2019-08-06 Brunswick Corporation Hypereutectic aluminum-silicon cast alloys having unique microstructure
    US9650699B1 (en) 2013-03-14 2017-05-16 Brunswick Corporation Nickel containing hypereutectic aluminum-silicon sand cast alloys
    US9109271B2 (en) * 2013-03-14 2015-08-18 Brunswick Corporation Nickel containing hypereutectic aluminum-silicon sand cast alloy
    KR101964347B1 (en) * 2017-11-06 2019-04-01 한국생산기술연구원 Aluminium alloy die-casting products and manufacturing method thereof
    CN114210987B (en) * 2021-12-21 2022-12-09 上海交通大学 High-volume-fraction particle reinforced titanium-based composite material powder and preparation method thereof

    Family Cites Families (3)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US3993478A (en) * 1972-02-09 1976-11-23 Copper Range Company Process for dispersoid strengthening of copper by fusion metallurgy
    US3951651A (en) * 1972-08-07 1976-04-20 Massachusetts Institute Of Technology Metal composition and methods for preparing liquid-solid alloy metal compositions and for casting the metal compositions
    JPS58110652A (en) * 1981-12-25 1983-07-01 Nissan Motor Co Ltd Wear resistant composite aluminum material and its manufacture

    Non-Patent Citations (4)

    * Cited by examiner, † Cited by third party
    Title
    Aluminum Alloys: Structure and Properties, L.F. Mondolfo, Butterworths, 1976, pp.592-594 *
    Fabrication of particulates reinforced metal composites, Materials Park, OH, ASM International, Ed.J.Masounave et al., 1990, pp.47-52 *
    Int. Mtrls Rev., 1986, 31(3), pp.115-139 *
    Z. Metallkde, 1989, 80(M-6), pp.444-446 *

    Also Published As

    Publication number Publication date
    JPH06502689A (en) 1994-03-24
    EP0559694A1 (en) 1993-09-15
    JP3492681B2 (en) 2004-02-03
    DE69130227D1 (en) 1998-10-22
    DE69130227T2 (en) 1999-01-21
    WO1992009711A1 (en) 1992-06-11

    Similar Documents

    Publication Publication Date Title
    US5484492A (en) Al-Si alloys and method of casting
    US5523050A (en) Method of preparing improved eutectic or hyper-eutectic alloys and composites based thereon
    CA2825253C (en) Aluminium-copper alloy for casting
    US4973522A (en) Aluminum alloy composites
    CA2094369C (en) Aluminum-base metal matrix composite
    US6132532A (en) Aluminum alloys and method for their production
    US6036792A (en) Liquid-state-in-situ-formed ceramic particles in metals and alloys
    EP0559694B1 (en) Method of preparing improved hyper-eutectic alloys and composites based thereon
    JP2002535488A (en) Hypereutectic aluminum-silicon alloy products for forming in the semi-solid state
    WO2000071772A1 (en) Aluminum-silicon alloy having improved properties at elevated temperatures
    WO2000071767A1 (en) Aluminum-silicon alloy having improved properties at elevated temperatures and articles cast therefrom
    JP2004256873A (en) Aluminum alloy for casting having excellent high temperature strength
    Lloyd et al. Properties of shape cast Al-SiC metal matrix composites
    US5366691A (en) Hyper-eutectic aluminum-silicon alloy powder and method of preparing the same
    EP0897994B1 (en) Cast-alumina metal matrix composites and method of manufacturing the same
    US6843865B2 (en) Aluminum alloy product refinement and applications of aluminum alloy product refinement
    US5669990A (en) Si-containing magnesium alloy for casting with melt thereof
    US4193822A (en) High strength aluminium base alloys
    EP0592665B1 (en) Hypereutectic aluminum/silicon alloy powder and production thereof
    JP3283550B2 (en) Method for producing hypereutectic aluminum-silicon alloy powder having maximum crystal grain size of primary silicon of 10 μm or less
    JPH06306521A (en) Hyper-eutectic al-si series alloy for casting and casting method
    CN111485139A (en) Al-RE-Y alloy and preparation method thereof
    JPH062057A (en) Al base composite material
    US6398882B1 (en) Uniformly dispersed, finely sized ceramic particles in metals and alloys
    CA2257536A1 (en) Strontium-aluminum intermetallic alloy granules

    Legal Events

    Date Code Title Description
    PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

    Free format text: ORIGINAL CODE: 0009012

    17P Request for examination filed

    Effective date: 19930526

    AK Designated contracting states

    Kind code of ref document: A1

    Designated state(s): CH DE ES FR GB IT LI NL

    17Q First examination report despatched

    Effective date: 19931217

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAH Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOS IGRA

    GRAH Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOS IGRA

    GRAA (expected) grant

    Free format text: ORIGINAL CODE: 0009210

    AK Designated contracting states

    Kind code of ref document: B1

    Designated state(s): CH DE ES FR GB IT LI NL

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: NL

    Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

    Effective date: 19980916

    Ref country code: LI

    Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

    Effective date: 19980916

    Ref country code: ES

    Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

    Effective date: 19980916

    Ref country code: CH

    Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

    Effective date: 19980916

    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: EP

    REF Corresponds to:

    Ref document number: 69130227

    Country of ref document: DE

    Date of ref document: 19981022

    ET Fr: translation filed
    NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: PL

    PLBE No opposition filed within time limit

    Free format text: ORIGINAL CODE: 0009261

    STAA Information on the status of an ep patent application or granted ep patent

    Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

    26N No opposition filed
    REG Reference to a national code

    Ref country code: GB

    Ref legal event code: IF02

    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: GB

    Payment date: 20031119

    Year of fee payment: 13

    Ref country code: FR

    Payment date: 20031119

    Year of fee payment: 13

    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: DE

    Payment date: 20031231

    Year of fee payment: 13

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: GB

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20041127

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: DE

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20050601

    GBPC Gb: european patent ceased through non-payment of renewal fee

    Effective date: 20041127

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: FR

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20050729

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: ST

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: IT

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

    Effective date: 20051127