EP0139168A1 - Composition métallique à grains fins - Google Patents

Composition métallique à grains fins Download PDF

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Publication number
EP0139168A1
EP0139168A1 EP84110109A EP84110109A EP0139168A1 EP 0139168 A1 EP0139168 A1 EP 0139168A1 EP 84110109 A EP84110109 A EP 84110109A EP 84110109 A EP84110109 A EP 84110109A EP 0139168 A1 EP0139168 A1 EP 0139168A1
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EP
European Patent Office
Prior art keywords
alloy
composition
metal
uniform
heating
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.)
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Application number
EP84110109A
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German (de)
English (en)
Inventor
Kenneth Peter Young
Curtis Paul Kyonka
James Alan Courtois
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.)
Alumax Inc
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Deutsche ITT Industries GmbH
Alumax Inc
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Filing date
Publication date
Application filed by Deutsche ITT Industries GmbH, Alumax Inc filed Critical Deutsche ITT Industries GmbH
Publication of EP0139168A1 publication Critical patent/EP0139168A1/fr
Withdrawn legal-status Critical Current

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    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous 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
    • C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon

Definitions

  • This invention relates to a metal alloy composition.
  • U.S. patents 3,948,650 and 3,954,455 disclose a process for making possible such shaping processes by the prior vigorous agitation of a metal or metal alloy while it is in a semi-solid condition. This converts the normally dendritic microstructure of the alloy into a non-dendritic form comprising discrete degenerate dendrites in a lower melting matrix. The resulting alloy is capable of being shaped in a semi-solid condition by casting, forging or other known forming processes.
  • the first part of the process normally involves the production of cast bars having the required non-dendritic structure.
  • the technical feasibility of casting diameters of less than about 25.4 mm on a practical scale is very low and, because of the nature of the process even were it feasible, would result in extremely low output.
  • the casting process in may instances produces cast bars which exhibit less than desirable skin microstructure which must be trimmed mechanically or otherwise treated for subsequent processing.
  • the generation of diameters of varying size is cumbersome and expensive since each diameter necessitates a complete casting cycle including set-up, mold preparation and runn- iag, Flexibility is, therefore, low.
  • a metal alloy composition having a uniform, fine grained microstructure comprising uniform discrete spheroidal particles contained within a lower melting matrix
  • said alloy being a magnesium, ferrous or copper alloy
  • a solid metal alloy composition having an essentially directional grain structure heating said directional grain composition to a temperature above the solidus and below the liquidus to produce a partially solid, partially liquid mixture, containing at least 0.05 volume fraction liquid, said composition prior to heating having a strain level introduced such that upon heating, the mixture comprises uniform discrete spheroidal particles contained within a matrix composition having a lower melting point than said particles and solidifying said heated alloy compositions.
  • the solidified composition has a uniform, fine grained microstructure comprising uniform discrete spheroidal particles contained within a lower melting matrix.
  • the metal compositions produced by the foregoing process have a more uniform and finer grain structure than are obtainable by any other known process.
  • patents 3,988,180, 4,106,956, 4,019,927 heat an alloy to just above the solidus temperature and hold the alloy at thac temperature until the dendritic phase becomes globular.
  • the present invention involves a technique for inducing heterogeneities into the structure. in such a fashion that the structures can be transformed into a homogeneous mixture of very uniform discrete particles.
  • the product of the present process is a metal composition having a uniform, fine grained microstructure consisting of spheroidal particles engulfed in a solidified liquid phase.
  • the microstructure is more uniform and the particles are generally rounder and of smaller size than comparable alloys of the prior art. In the case of aluminum and virtually every otler alloy tested, these particles are less than 30 ⁇ in diameter.
  • the process of the invention has a number of very significant advantages. Casting of the starting billet may be carried out in a single convenient diameter, e.g. 152.4 mm,
  • a directional grain structure is produced by hot working a metal composi- t ion, as by extrusion, rolling, forging, swaging or other means, at a temperature below the solidus temperature.
  • hot working is meant any process which deforns a netal or alloy between the recrystallization temperature (typically, 7T solidus Kelvin) and the solidus temperature (T solidus ), such that it produces a striated or directional grain structure.
  • the directional grain structure is produced by extrusion.
  • the extrusion ratio should normally be greater than 10/1 to produce the desired directional grain structure and may range as high as economically practical. We have found useful extrusion ratios frequently range from about 19/1 to about 60/1.
  • a critical level of strain must be introduced into the metal or alloy either concurrently with and as an integral part of the hot working step, or as a separate step subsequent to hot working and prior to heating to above the solidus temperature.
  • Strain is introduced integral with the hot working operation, for example, by an in-line straightening operation, by rapid chilling of the hot worked naterial to introduce thermal strains or by extruding at lower temperatures such as to leave residual strains in the extruded product.
  • Lower extrusion or other hot working tamperatures tend to leave higher residual strains in the extrusion since the extrusion pressures go up as the temperatures go down, i.e. more energy is used u p by the extrusion process.
  • strain is introduced by cold working.
  • strain level is meant to represent any residual strain remaining within a grain after the deformation process is completed.
  • the actual strain level will vary with the specific metal or alloy and with the type and conditions of hot working. In the case of extruded aluminum alloy, the strain level should be equivalent to at least a 12% cold worked alloy.
  • the level of strain can be determined empirically by determining whether, after heating to above the solidus temperature, the partially solid, partially liquid mixture comprises uniform discrete spheroidal solid particles contained within a lower melting matrix composition. Alloys, in which the directional grain structure is produced by hot working and particularly by extrusion, and which are separately cold worked, have been found to possess a particularly improved uniform, fine grained nicrostructure unavailable by other processes.
  • the alloy Upon completion of hot working and any required cold working, the alloy is then reheated to a temperature above the solidus and below the liquidus.
  • the specific temperature is generally such as to produce a 0.05 to 0.8 volume fraction liquid, preferably at least 0.10 volume fraction liquid and in most cases a 0.15 to 0.5 volume fraction liquid.
  • the reheated alloy may then be solidified and again reheated for shaping in a partially solid, partially liquid condition or the shaping step may be integral with the original reheat of the alloy to a partially solid, partially liquid state.
  • the second reheat of the alloy may be to a higher fraction solid than the first reheat, but it is preferable not more than 0.20 fraction solid greater.
  • the alloy is heated to a Semi-solid stats and shaped at the same time in a press forging operation.
  • the alloy charge is heated to the requisite partially solid, partially liquid temperature, placed in a die cavity and shaped under pressure. Both shaping and solidification times are extremely short and pressures are comparatively low.
  • This press forging process is more completely disclosed in German application DE - OS 29 29 812 and DE-OS 29 29 845, the disclosure of which is hereby incorporated by reference.
  • Other semi-solid forming processes which may be used are die casting, send-solid extrusion and related shaping techniques.
  • Figure 1 is a typical time-temperature profile of a process in accordance with the invention.
  • the vertical axis is temperature; the horizontal axis is time.
  • the graph is intended to graphically portray a relative time-temperature relationship rather than set forth precise values.
  • a metal is melted and solidified to form a cast billet, either dendritic or non-dendritic.
  • the cast billet is pre- heated, e.g. approximately 30 minutes for a typical aluminum casting alloy, to above the recrystallization temperature, extruded and quenched to produce a solid metal composition having a directional grain structure.
  • the extruded metal composition is then cold worked at room temeprature to introduce a proper level of strain. It is then reheated above the solidus temperature, e.g. about 100 seconds for a typical aluminum alloy, to a semi-solid condition and rapidly quenched.
  • the starting material for practice of the present process may be a dendritic metal or alloy of the type conventionally cast into billets or a non-dendritic metal or alloy of the type in which a billet has been vigorously agitated during freezing in accordance with the teachings of the aforementioned U.S. patent 3,948,650.
  • Such agitation produces a so-called slurry cast structure, that is one having discrete, degenerate dendritic particles within a lower melting matrix.
  • Copending application S.N. 363,621 filed March 30, 1982 is directed to a process in which the starting material is a billet having a slurry cast structure in which the slurry cast structure is rehabilitated by heating to a semi-solid state.
  • Billets which have beenelled under conditions of vigorous agitation may be produced-by the continuous direct chill casting process set forth in published British patent application 2,042,306A, the disclosure of which is also hereby incorproated by reference.
  • molten metal is cooled while it is vigorously agitated in a rotating magnetic field.
  • the process is continuous and produces continuous lengths of billets having a discrete degenerate dendritic structure.
  • Billets are referred to below as billets which have been chill cast under a shearing environment during solidification to distinguish those which have been vigorously agitated from those which have not.
  • microstructure of non-dendritic compositions produced in accordance with the aforementioned U.S. patent 3 , 9 48,650 and which is also produced in accordance with the process of the pressnt invention may be variously described as comprising discrete spheroidal particles contained within a matrix composition having a lower melting point or, alternatively, as discrete primary phase particles enveloped by a solute-rich matrix.
  • Such a structure will hereinafter be described in accordance with the first-mentioned description, but it should be understood that the various descriptions are essentially alternative ways of describing the same microstructure.
  • a section of the cast bar was preheated to 380°C in less than 1/2 hour and extruded at a 50/1 ratio into a 22.2 mm diameter rod.
  • Extrusion pressure was 67,000 psi.
  • the rod exited at 7.62/minute and at 460°C and was fan quenched.
  • the extruded bar was stretched straight (approximately 1% peman- ent set) to introduce strain into the bar as an integral step of the extrusion process.
  • Figure 3 is a photomicrograph of a longitudinal section of the extruded stretched bar. Its directional grain structure is very evident.
  • FIG. 4 is a micrograph cf a crosssection of the reheated and quenched sample.
  • Fig. 4 demonstrates the dramatic refinement of the microstructure obtained over that of the starting billet (Fig. 2). It further demonstrates that the severely worked microstructure of the extruded section can be converted to a slurry microstructure by heating to a 0.1 or higher fraction liquid.
  • Example 1 An aluminum casting alloy (Aluminum Association Alloy 357) was cast as in Example 1, preheated to 380°C.within 1/2 hour and extruded into 31.75 mmdiameter rod.
  • the ex- trusion pressure was 9840 bar.
  • the extruded bar was stretched straight approximately 1% permanent set. Portions of the rod were then drawn 36% to 25.4mm diameter.
  • Samples were taken of the as-extruded and drawn material and inductively reheated and press forged as in Example 1 but this time into a 1.27 mm wall cup.
  • Figure 5 is a representativte micrograph of a section through the final product again showing a uniform, fine grained "slurry-type" microstructure.
  • An aluminum wrought alloy (Aluminum Association Alloy 2024) was direct chill cast, homogenized (to reduce extrusion pressure and tendency to hot tear during hot working) and 25.4 mm extruded to a / diameter.
  • the alloy had the following composition:
  • Example 3 was again repeated with an aluminum wrought alloy (Rluminum Association Alloy 6262) having the following composition:
  • Example 5 was again repeated with an aluminum wrought alloy (Aluminum Association Alloy 7075) having the following composition:
  • Results were as set forth in Examples 3-5.
  • An aluminum alloy (Aluminum Association Alloy 357) was direct chill cast under a shearing environment to a 152.4 mm diameter.
  • the alloy had the following percent composition: A 559 mm length was preheated to 520°C in less than 1/2 hour and extruded into a 22.23 mm diameter rod. Extrusion pressure was 7031 bar. The rod exited at 7.3m/minute and at 520°C and was fan quenched.25.4 mm sections were then axially compressed at room temperature between two parallel plates so that the length was reduced 5, 10, and 16%.
  • a 25 gram 25.4 mm section of the extruded billet was then axially compressed 25% and press forged into a threaded plug in accordance with the process of the aforementioned copending application S.N. 290,217 in a partially solid, partially liquid condition.
  • Reheat time was 50 seconds
  • fraction solid was 0.85
  • dwell time was 0.5 seconds
  • . pressure was 1054 bar with respect to atmosphere.
  • Photomicrographs at various stages of the process were .taken.
  • the starting / diameter billet exhibited particles of approximately 100 microns diameter.
  • the extruded billet showed a directional grain microstructure in which the grains were very elongated.
  • Micrographs of the center section of reheated billets, which were as-extruded and compressed 5, 10 and 16% respectively, showed that particle size and shape continued to improve as the strain was increased, particularly as strain was increased over 10%.
  • the microstructure of a sample which was compressed 25% and press forged into a threaded plug showed much finer scale microstructure and more uniform shape and distribution of the grains in the final product as compared with the starting billet. It also showed the remarkable influence of the residual strain upon the reheated grain structure of the extruded product.
  • Fig. 8 is a micrograph of a crosssection of the press forged final product.
  • Example 11 was hot worked by extrusion and cold worked an additional 50%.
  • Example 12 was also hot worked by extrusion and cold worked an additional 29%.
  • Example 13 was also hot worked by extrusion and cold worked an additional 20%, and then cold worked approximately 20-25%.
  • Example 11 was alloy C110 which is 99.9% copper, balance oxygen and thus represents an almost pure metal.
  • Example 12 was alloy C187 which is 99% copper and 1 % lead.
  • Exarple 13 was alloy C360 which is 60% copper, 3% lead, balance zinc.
  • Example 12 Example 12
  • Fig. 11 Example 13
  • the alloys of these three examples were reheated to a temp- erature of about 1070°C, 980°C and 390°C respectively.
  • the microstructures shown in these micrographs show substantial grain refinement relative to comparable microstructures . of alloys produced by vigorous agitation of the alloy while in a semi-solid condition.
  • Magnesium alloy A231B (4%Al, 1% Zn, 0.2% Mn, balance Mg) was prepared and hot worked as set forth in preceding-Examples 11-13 and the bars were then subjected to an additional 12% compressive cold work.
  • Fig. 12 shows the microstructure of a crosse ction of the final alloy reheated to about 610°C and quenched.Again, the structure is superior in boch particle size and shape to the most closely analogous alloys of the prior art - comparable magnesium alloys prepared by vigorous agitation during freezing of the alloy while in semi-solid condition.
  • Stainless steel alloy 316 (17% Ni, 12% Cr, 2.5% Mo, balance Fe) was hot worked by hot rolling and cold worked an additional 40%.
  • Fig. - 13 is a micrograph of a crossection of the alloy reheated to about 1380°C and quenched. Particle sizes are considerably finer and more uniform than comparable particles of vigorously agitated stainless steel alloys.
  • a stainless steel alloy 440C (.95-1.2%C, 16-18% Cr, Max 1% Mn, Max. 1%Si, Max. 75% Mo, balance Fe) was cast, . hot rolled and cold worked an additional 20% by cold compression. The microstructure of the alloy reheated to about 1330°C and quenched is shown in Fig. 14.
  • the process is applicable to other metals and metal alloys as long as the metal is capable of forming a two-phase system having solid particles in a lower melting matrix phase.
  • Representative additional alloys which may be used are those of nickel, cobalt, lead, zinc and titanium.
  • the alloys may be so-called casting alloys such as aluminum alloys 356 and 357 or wrought alloys such as aluminum alloys 6061,2024 and 7075 and copper alloys C544 and C360.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Extrusion Of Metal (AREA)
  • Heat Treatment Of Steel (AREA)
  • Forging (AREA)
EP84110109A 1983-09-20 1984-08-24 Composition métallique à grains fins Withdrawn EP0139168A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US53399783A 1983-09-20 1983-09-20
US533997 1983-09-20

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EP0139168A1 true EP0139168A1 (fr) 1985-05-02

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JP (1) JPS60149751A (fr)
AU (1) AU3310084A (fr)
BR (1) BR8404599A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5037489A (en) * 1986-05-12 1991-08-06 The University Of Sheffield Thixotropic materials
EP0822994A1 (fr) * 1995-04-14 1998-02-11 Northwest Aluminum Company Transformation thermique et formation a l'etat semi-solide d'alliages d'aluminium
CN115433862A (zh) * 2022-08-05 2022-12-06 太原理工大学 一种无Ni可降解镁基材料的制备方法

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69327195T2 (de) * 1992-01-13 2000-04-06 Honda Motor Co Ltd Verfahren zum Giessen von Aluminiumlegierungen und Gusstücken
JP4332889B2 (ja) * 2003-05-30 2009-09-16 住友電気工業株式会社 マグネシウム基合金成形体の製造方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2266749A1 (fr) * 1974-04-04 1975-10-31 Pechiney Aluminium
EP0090253A2 (fr) * 1982-03-30 1983-10-05 Alumax Inc. Composition métallique à grains fins

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2266749A1 (fr) * 1974-04-04 1975-10-31 Pechiney Aluminium
FR2266748A1 (fr) * 1974-04-04 1975-10-31 Pechiney Aluminium
EP0090253A2 (fr) * 1982-03-30 1983-10-05 Alumax Inc. Composition métallique à grains fins

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5037489A (en) * 1986-05-12 1991-08-06 The University Of Sheffield Thixotropic materials
US5133811A (en) * 1986-05-12 1992-07-28 University Of Sheffield Thixotropic materials
EP0822994A1 (fr) * 1995-04-14 1998-02-11 Northwest Aluminum Company Transformation thermique et formation a l'etat semi-solide d'alliages d'aluminium
EP0822994A4 (fr) * 1995-04-14 1998-12-23 Northwest Aluminum Co Transformation thermique et formation a l'etat semi-solide d'alliages d'aluminium
CN115433862A (zh) * 2022-08-05 2022-12-06 太原理工大学 一种无Ni可降解镁基材料的制备方法

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Publication number Publication date
AU3310084A (en) 1985-03-28
JPS60149751A (ja) 1985-08-07
BR8404599A (pt) 1985-08-06

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