EP0064468A1 - Verfahren zur Herstellung von Blechen aus untereutektischen Aluminium-Eisen-Legierungen - Google Patents

Verfahren zur Herstellung von Blechen aus untereutektischen Aluminium-Eisen-Legierungen Download PDF

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Publication number
EP0064468A1
EP0064468A1 EP82420049A EP82420049A EP0064468A1 EP 0064468 A1 EP0064468 A1 EP 0064468A1 EP 82420049 A EP82420049 A EP 82420049A EP 82420049 A EP82420049 A EP 82420049A EP 0064468 A1 EP0064468 A1 EP 0064468A1
Authority
EP
European Patent Office
Prior art keywords
grains
annealing
semi
thickness
sheet
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.)
Granted
Application number
EP82420049A
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English (en)
French (fr)
Other versions
EP0064468B1 (de
Inventor
François-Régis Boutin
Salim Dermarkar
Jacques Vernier
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.)
Cegedur Societe de Transformation de lAluminium Pechiney SA
Original Assignee
Cegedur Societe de Transformation de lAluminium Pechiney SA
Societe de Conditionnement en Aluminium SCAL GP SA
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.)
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Publication date
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Application filed by Cegedur Societe de Transformation de lAluminium Pechiney SA, Societe de Conditionnement en Aluminium SCAL GP SA filed Critical Cegedur Societe de Transformation de lAluminium Pechiney SA
Priority to AT82420049T priority Critical patent/ATE10116T1/de
Publication of EP0064468A1 publication Critical patent/EP0064468A1/de
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon

Definitions

  • the present invention relates to a process for manufacturing sheets of hypoeutectic aluminum-iron alloys, intended more particularly for the production of light dishes, flexible pipes, plugs and for all applications requiring said sheet of mechanical characteristics which favor stamping. , folding and stiffness.
  • hypoeutectic aluminum-iron alloys are understood here to mean those which contain less than 1.7% of iron.
  • Such alloys are known in particular from French patent FR No. 1,438,096 which protects a product suitable for the production of metal sheets with a thickness of less than 76 ⁇ m, characterized in that it contains from 0.6 to 1.2 % iron, the rest being aluminum.
  • Such a sheet is obtained by conventional semi-continuous casting followed by cold rolling and has interesting mechanical characteristics, namely a tensile breaking strength of the order of 80 MPa and an elongation of 7%.
  • the Applicant has directed its research towards alloys with a composition which is quite far from eutectic and contains at most 1.3% iron.
  • Those skilled in the art know that, under these conditions, solidification begins with the appearance of so-called primary aluminum crystals in the form of dentrites and ends with an eutectic deposit composed of intermetallics of Al n Fe which separates the grains from each other. This leads to a heterogeneous structure quite different from the homogeneous structure obtained in the case of a eutectic composition.
  • the French patent, n ° ' 1.438 096 shows by means of curves, the variations of the mechanical characteristics, such as the tensile breaking strength and the elongation, in as a function of the rate of thickness reduction that the metal undergoes during rolling.
  • This rate also called hardening rate, corresponding to the formula x 100, in which E represents the thickness before rolling and e, the final thickness.
  • the hypoeutectic Al n Fe has a significantly better elongation characteristic than that of the conventional alloys 1100 and 5005. This property means that, as the patent teaches: "the alloy s' adapts better to thin sheet manufacturing operations and makes the product obtained superior for packaging applications, for which better mechanical strength would be ineffective if it were accompanied by a significant loss of elongation ".
  • the metal hardens or better hardens, that is to say that it gradually loses all capacity for plastic elongation while acquiring greater strength. It can then be heated to a temperature close to 400 ° C. and thus carry out an annealing known as recrystallization, operation during which the mechanical characteristics change considerably and are oriented towards a reduction in the breaking load and an increase in elongation. Admittedly, this significantly improves the elongation, but more often than not, the resistance has become insufficient.
  • the metal bath is treated with a refiner, it is poured semi-continuously in an ingot mold or continuously between cylinders, it is cold rolled and annealed between 380 ° C and 430 ° C, this process being characterized in that '.
  • the refiner is added in such a quantity that it generates a pouring structure in which the grains have a maximum dimension of less than 100 ⁇ m and the spacing between dendrite arms is between 8 and 30 ⁇ m and in that the rolling is 'performs according to a thickness reduction rate between 98 and 99.8%.
  • the method according to the invention consists in implementing the conventional steps in metallurgy, of refining of the alloy in the liquid state, of casting, of rolling, of final annealing. It can be noted, however, that the method applies indifferently to a product cast semi-continuously using ingot molds or type 3C cylinder casting machines, provided that the refining parameters and. hardening are adapted to the type of casting so as to lead to the same final structure.
  • the process is first characterized by the addition of a refiner in quantity such that it generates a pouring structure in which the grains have a maximum dimension of less than 100 ⁇ m.
  • This refining can be obtained by means of any general agent used in aluminum metallurgy and, in particular, products based on boron and titanium such as, for example, AT5B.
  • alloy compositions which move as far as possible from the eutectic zone, but nevertheless retaining sufficient iron to benefit from the particular properties of this element and, in particular, from its action as an agent for blocking recrystallization.
  • a content of between 1.1 and 1.3% of iron is preferred.
  • the alloy is avoided from being poured into a cylinder machine of the HUNTER type because the solidification speed is too high and leads to dendrites which are too fine less than 5 ⁇ m.
  • the 3C machine turns out to be particularly advantageous in the process of the invention because it gives rise to the formation of dendrites which are still sufficiently large so that the zones with and without eutectic can be clearly distinguished on the structure.
  • the method is also characterized in that the cold rolling, applied directly to the casting structure, is carried out according to a thickness reduction rate of between 98 and 99.8%.
  • the process also includes an annealing between 380 and 430 ° C after laninage at a rate of temperature rise and of a duration such that the desired semi-recrystallized structure is developed and which is then composed of recrystallized grains of smaller diameter at 30 ⁇ m and generally between 5 and 15 ⁇ m, isolated in a restored matrix with sub-grains of 1 to 2 ⁇ m.
  • the semi-recrystallized structure thus obtained seems mainly due to a dispersion in the distribution of the distances between the intermetallic particles allowing both recrystallization when this distance is large and blocking of recrystallization when this distance is small.
  • the low volume occupied by the recrystallized grains seems essential because it provides the alloy with a significant improvement in ductility while the structure of the sub-grains still allows a high elastic limit to be retained.
  • alloy sheet an advantageous compromise between its characteristics, which is particularly favorable for subsequent processing operations such as stamping for example.
  • the invention can be illustrated by means of the following examples which give the results of mechanical characteristics obtained with sheets of 100 ⁇ m thickness, produced according to the claimed process.
  • the structure of the cast product was composed of primary aluminum grains having a maximum dimension less than 150 ⁇ m separated from each other by eutectic zones of Al n Fe.
  • the plate was cold rolled at a thickness reduction rate of 99.8% so as to give a sheet 100 ⁇ m thick which was annealed at 420 ° C for 30 hours.
  • the final structure of this sheet had 30% of its volume in the recrystallized state and its mechanical characteristics were as follows: compromise of values particularly favorable to the preparation of dishes obtained by stamping.
  • the structure of the cast product included primary aluminum grains of dimensions between 30 and 80 ⁇ m separated from each other by eutectic zones of Al n Fe.
  • the sheet was cold rolled at a thickness reduction rate of 99% so as to form a sheet of thickness 80 ⁇ m which was annealed at 400 ° C for 30 hours.
  • the sheet had a final structure recrystallized at 20% and its mechanical characteristics were as follows: characteristics which made it possible to use this sheet for the preparation of deep-drawn dishes, with a practically zero rate of reject.
  • the present invention finds its application in the aluminum industry whenever it is desired to obtain sheets with a thickness of between 50 and 150 ⁇ m having a pair of optimum values with regard to the tensile breaking load. and elongation.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Metal Rolling (AREA)
  • Coating With Molten Metal (AREA)
  • Soft Magnetic Materials (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
  • Continuous Casting (AREA)
  • Powder Metallurgy (AREA)
  • Coloring Foods And Improving Nutritive Qualities (AREA)
  • Forging (AREA)
  • Laminated Bodies (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Manufacturing Cores, Coils, And Magnets (AREA)
EP82420049A 1981-04-13 1982-04-08 Verfahren zur Herstellung von Blechen aus untereutektischen Aluminium-Eisen-Legierungen Expired EP0064468B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT82420049T ATE10116T1 (de) 1981-04-13 1982-04-08 Verfahren zur herstellung von blechen aus untereutektischen aluminium-eisen-legierungen.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8107844 1981-04-13
FR8107844A FR2503738A1 (fr) 1981-04-13 1981-04-13 Procede de fabrication de feuilles en alliages d'aluminium-fer hypoeutectiques

Publications (2)

Publication Number Publication Date
EP0064468A1 true EP0064468A1 (de) 1982-11-10
EP0064468B1 EP0064468B1 (de) 1984-10-31

Family

ID=9257574

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82420049A Expired EP0064468B1 (de) 1981-04-13 1982-04-08 Verfahren zur Herstellung von Blechen aus untereutektischen Aluminium-Eisen-Legierungen

Country Status (9)

Country Link
EP (1) EP0064468B1 (de)
AT (1) ATE10116T1 (de)
DE (1) DE3261110D1 (de)
DK (1) DK159682A (de)
ES (1) ES511308A0 (de)
FR (1) FR2503738A1 (de)
GR (1) GR69198B (de)
NO (1) NO156572C (de)
TR (1) TR21267A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002064849A1 (en) * 2001-02-13 2002-08-22 Alcan International Limited Production of aluminum alloy foils having high strength and good rollability

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2155226A5 (de) * 1971-08-09 1973-05-18 Comalco Alu
FR2229779A1 (de) * 1973-05-17 1974-12-13 Alcan Res & Dev
FR2291285A1 (fr) * 1974-11-15 1976-06-11 Alcan Res & Dev Procede de fabrication de produits ameliores d'alliages metalliques
FR2429844A1 (fr) * 1978-06-27 1980-01-25 Norsk Hydro As Procede de production de toles ou plaques en un alliage d'aluminium ayant de meilleures proprietes mecaniques et thermo-mecaniques

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2155226A5 (de) * 1971-08-09 1973-05-18 Comalco Alu
FR2229779A1 (de) * 1973-05-17 1974-12-13 Alcan Res & Dev
FR2291285A1 (fr) * 1974-11-15 1976-06-11 Alcan Res & Dev Procede de fabrication de produits ameliores d'alliages metalliques
FR2429844A1 (fr) * 1978-06-27 1980-01-25 Norsk Hydro As Procede de production de toles ou plaques en un alliage d'aluminium ayant de meilleures proprietes mecaniques et thermo-mecaniques

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002064849A1 (en) * 2001-02-13 2002-08-22 Alcan International Limited Production of aluminum alloy foils having high strength and good rollability
US6663729B2 (en) 2001-02-13 2003-12-16 Alcan International Limited Production of aluminum alloy foils having high strength and good rollability
CN1294284C (zh) * 2001-02-13 2007-01-10 诺维尔里斯公司 高强度和良好可轧制性的铝合金箔的生产

Also Published As

Publication number Publication date
ES8304214A1 (es) 1983-02-16
DK159682A (da) 1982-10-14
DE3261110D1 (en) 1984-12-06
ATE10116T1 (de) 1984-11-15
TR21267A (tr) 1984-01-01
ES511308A0 (es) 1983-02-16
EP0064468B1 (de) 1984-10-31
FR2503738B1 (de) 1983-05-13
GR69198B (de) 1982-05-06
NO821164L (no) 1982-10-14
NO156572B (no) 1987-07-06
NO156572C (no) 1987-10-14
FR2503738A1 (fr) 1982-10-15

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