EP0660882B1 - Procede de fabrication d'une feuille mince apte a la confection d'elements constitutifs de boites - Google Patents

Procede de fabrication d'une feuille mince apte a la confection d'elements constitutifs de boites Download PDF

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Publication number
EP0660882B1
EP0660882B1 EP94922899A EP94922899A EP0660882B1 EP 0660882 B1 EP0660882 B1 EP 0660882B1 EP 94922899 A EP94922899 A EP 94922899A EP 94922899 A EP94922899 A EP 94922899A EP 0660882 B1 EP0660882 B1 EP 0660882B1
Authority
EP
European Patent Office
Prior art keywords
strip
process according
less
carried out
annealing
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
EP94922899A
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German (de)
English (en)
French (fr)
Other versions
EP0660882A1 (fr
Inventor
Jean-Marc Legresy
Guy-Michel Raynaud
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.)
Constellium Issoire SAS
Original Assignee
Pechiney Rhenalu SAS
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 FR9308987A external-priority patent/FR2707668A1/fr
Application filed by Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Publication of EP0660882A1 publication Critical patent/EP0660882A1/fr
Application granted granted Critical
Publication of EP0660882B1 publication Critical patent/EP0660882B1/fr
Anticipated expiration legal-status Critical
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • B22D11/0622Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by two casting wheels
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • 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
    • C22F1/047Changing 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 magnesium as the next major constituent

Definitions

  • the present invention relates to a manufacturing process by casting continuous between cylinders of a thin sheet of suitable aluminum alloy for the production of components for beverage or use boxes food.
  • said sheets In order to be suitable for these mechanical operations as well as for stresses resulting from the manipulations and pressures exerted on the inside of boxes with certain foods such as drinks carbonated, said sheets must have both a suitability for suitable deformation and a sufficient elastic limit.
  • German document DE 3247698 (Alusuisse) teaches a method of manufacture of a strip intended for the manufacture of box covers aluminum alloy from a continuous casting machine characterized in that an alloy containing by weight 0.15 to 0.50% of Si is poured, 0.3 to 0.8% Fe, 0.05 to 0.25% Cu, 0.5 to 1% Mn, 2.5 to 3.5% Mg and up to 0.20% of Ti between two cooled casting rolls constituting a casting gap of 5 to 10 mm and that the resulting strip is cold rolled to a final thickness of 0.4 to 0.2 mm.
  • the document JP 04276047 (Sky Aluminum) describes a process for obtaining hard sheets of aluminum alloy for the production of covers of boxes, method comprising a thin strip casting to a thickness less than 15 mm, with a cooling rate greater than 50 ° C / sec; the sheet obtained is submitted immediately or after rolling cold to a first intermediate annealing, to cold rolling with a reduction rate from 30 to 85%, at the second intermediate annealing and finally in the final cold rolling with a reduction rate higher than 30%, this the latter can be followed by a final annealing.
  • the alloy has the following composition: Mg: 1.2 to 3%, Cu: 0.05 to 0.5%, Mn: 0.5 to 2%, Fe: 0.1 to 0.7%, Si: 0.1 to 0.5% , the balance being Al.
  • a 6 mm thick sheet was obtained according to this process. having an elastic limit, at 45 ° relative to the direction of rolling, from 305 to 310 N / mm2.
  • Document EP 99739 describes a process for obtaining a strip of Al alloy suitable for drawing and drawing, for example for obtaining boxes. It includes continuous strip casting thickness less than 2.54 cm, preferably between 6 and 12 mm, heating to 510-620 °, followed by cold rolling with reduction at least 25% thick, annealed, second cold rolled with a thickness reduction of at least 10%, a heating of recrystallization and final cold rolling.
  • Strips 12.1 mm thick and of different compositions were obtained and treated according to the method described; the final products obtained have the following characteristics (tab. XIX) Elastic limit from 280 to 294 MPa Breaking load from 291 to 308 MPa Elongation 2.2 to 2.5%
  • the breaking strength obtained is 272 MPa, the elastic limit of 245 MPa and the elongation of 4.1%.
  • the object of the invention is, with at least equal properties, to reduce the rolling rate and eliminating the intermediate annealing steps when cold rolling, which simplifies the process and makes it more economic.
  • the invention consists of a method of manufacturing a sheet of aluminum alloy intended for the housing which has for composition by weight: Mg between 1 and 4%, Mn between O and 1.6%, balance Al with its unavoidable impurities and optionally additions of Cu and / or Cr.
  • said sheet is obtained by casting said alloy in the liquid state between two cylinders in the form of a strip having a thickness at most equal to 4 mm, followed by at least one heat treatment at a temperature between 400 and 580 ° C so that the sheet is at least partially recrystallized, from cold rolling up to a final thickness of less than 0.3 mm and optionally of a coating operation.
  • the subject of the invention is a process first characterized by the casting a strip between two cylinders at a lower thickness or equal to 4 mm so that to reach the thickness of a cover of box to manufacture, the rolling rate is less than 95%; this avoids the recourse to intermediate annealing between the rolling passes, which is the case as soon as the thickness is greater than 4 mm, as has been seen upper.
  • casting between cylinders is meant a continuous casting of strips in which the liquid metal is introduced, using a nozzle refractory, between two cooled cylinders, between which it solidifies.
  • This invention is made possible by the use of the ranges of specific concentrations, cited above, of the various elements of the alloy constituting the sheet; it provides properties improved, in particular increased mechanical characteristics.
  • pouring at a thickness of less than 4 mm is favorable with regard to the quality of the tape, in particular as regards the segregations which are much reduced if not absent hence a improved formability and obtaining productivity in the vicinity of its optimum.
  • Another characteristic of the invention is the obtaining of a structure partially recrystallized (for example greater than about 50%) or completely, after heat treatment between 400 and 580 ° C of the strip after casting. This recrystallization of the metal is necessary to obtaining excellent formability of the alloy.
  • This operation can be carried out discontinuously on the wound strip or in the process either on the strip leaving continuously from the casting machine, or on a strip previously wound after casting.
  • the duration of the heat treatment and the temperature depend on the rate of temperature rise.
  • the heating rate is generally between 20 and 200 ° C / h.
  • the heating rate is at least 3000 ° C / h.
  • the parade treatment also offers particular advantages for alloys containing less than about 0.75% of Mn. Indeed, it leads to a recrystallization with fine and isotropic grains of dimensions less than 40 micrometers while the batch annealing gives grains of dimensions between 200 and 50 micrometers; this has the effect of improving the formability of the sheet.
  • the parade treatment is preferably obtained by heating in a induction oven or in a hot air circulating oven but, all other means of processing the parade of a strip can be envisaged.
  • the strip After heat treatment, the strip is cold rolled to the final thickness and the sheet obtained can be covered with a plastic material intended to protect it from the environment. It can be, for example, a varnishing on both sides with a varnish which is then dried by heating at a temperature between 200 and 280 ° C.
  • This magnesium is preferably combined with manganese in proportion by weight up to 1.6%.
  • a content higher than the maximum value prevents proper recrystallization during annealing and causes the appearance of large grains harmful to mechanical properties.
  • magnesium and manganese satisfying the condition: (3 Mn% + 2 Mg%) greater than or equal to 6% and less than or equal to 9%, so to obtain the best compromise between mechanical strength and formability.
  • the magnesium content is less than 3.2% but, the best results are obtained for an Mg content of less than 2.8%; indeed, this reduces the risks of segregation during casting, associated with high Mg contents.
  • Mn makes it possible to limit the content of Mg and therefore to decrease the risk of segregation; it is advantageously greater than 0.4% about.
  • the addition of a small amount of copper less than or equal to 0.4% and preferably less than 0.2% and / or the addition of chromium up to about 0.2% makes it possible to improve the mechanical strength of the alloy.
  • the content of these elements is limited because in too large a quantity they limit the ductility of the metal and therefore its formability.
  • silicon and iron these are mainly impurities whose presence is a function of the quality of the aluminum used.
  • the silicon is less than 0.3% or better than 0.2% and the iron at 0.5% or better at 0.3%.
  • the silicon leads after casting or after heat treatment by maturation to the formation of intermetallic precipitates of Mg2Si which limit the formability of the alloy.
  • iron it gives rise to the formation of eutectic precipitates during casting and therefore of segregations which are also harmful to ductility.
  • alloys A, B and C Three types of alloys A, B and C have been used, their composition by weight: Alloy Mg% Mn% Fe% Yes% Cu% AT 3.20 0.40 0.20 0.05 0.20 B 2.50 0.75 0.20 0.05 0.20 VS 1.5 1.4 0.19 0.05 0.20
  • the annealed strip is then subjected to 6 rolling passes without annealing intermediate to bring it in the form of a thick sheet final of 270 micrometers.
  • Said sheet is then degreased, subjected to a chemical treatment conversion to be then varnished on both sides.
  • the characteristics necessary to obtain covers suitable are a yield strength greater than 320 MPa, an index Ericksen greater than 4 and a delamination of the varnish less than 0.6 mm, it can be seen that the objectives are achieved by the process according to the invention, in particular in the case where a treatment is carried out type II or III thermal.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Metal Rolling (AREA)
  • Laminated Bodies (AREA)
  • Table Devices Or Equipment (AREA)
  • Details Of Rigid Or Semi-Rigid Containers (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
EP94922899A 1993-07-16 1994-07-11 Procede de fabrication d'une feuille mince apte a la confection d'elements constitutifs de boites Expired - Lifetime EP0660882B1 (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FR9308987A FR2707668A1 (fr) 1993-07-16 1993-07-16 Procédé de fabrication d'une feuille mince apte à la confection de couvercles de boîtes.
FR9308987 1993-07-16
FR9311814 1993-09-29
FR9311814A FR2707669B1 (fr) 1993-07-16 1993-09-29 Procédé de fabrication d'une feuille mince apte à la confection d'éléments constitutifs de boîtes.
PCT/FR1994/000861 WO1995002708A1 (fr) 1993-07-16 1994-07-11 Procede de fabrication d'une feuille mince apte a la confection d'elements constitutifs de boites

Publications (2)

Publication Number Publication Date
EP0660882A1 EP0660882A1 (fr) 1995-07-05
EP0660882B1 true EP0660882B1 (fr) 1999-05-19

Family

ID=26230496

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94922899A Expired - Lifetime EP0660882B1 (fr) 1993-07-16 1994-07-11 Procede de fabrication d'une feuille mince apte a la confection d'elements constitutifs de boites

Country Status (12)

Country Link
US (1) US5616190A (zh)
EP (1) EP0660882B1 (zh)
JP (1) JP3689106B2 (zh)
CN (1) CN1043580C (zh)
BR (1) BR9405520A (zh)
CA (1) CA2144757C (zh)
DE (1) DE69418581T2 (zh)
ES (1) ES2131696T3 (zh)
FR (1) FR2707669B1 (zh)
IL (1) IL110237A (zh)
SA (1) SA94150111B1 (zh)
WO (1) WO1995002708A1 (zh)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5655593A (en) * 1995-09-18 1997-08-12 Kaiser Aluminum & Chemical Corp. Method of manufacturing aluminum alloy sheet
US5913989A (en) * 1996-07-08 1999-06-22 Alcan International Limited Process for producing aluminum alloy can body stock
FR2805827B1 (fr) * 2000-03-03 2002-04-12 Pechiney Rhenalu Procede de fabrication de bandes en alliage d'aluminium aptes a la fabrication de corps de boites
US6581675B1 (en) 2000-04-11 2003-06-24 Alcoa Inc. Method and apparatus for continuous casting of metals
US6672368B2 (en) * 2001-02-20 2004-01-06 Alcoa Inc. Continuous casting of aluminum
AU2003215101A1 (en) * 2002-02-08 2003-09-02 Nichols Aluminum Method of manufacturing aluminum alloy sheet
US20040011438A1 (en) * 2002-02-08 2004-01-22 Lorentzen Leland L. Method and apparatus for producing a solution heat treated sheet
CN100413986C (zh) * 2003-04-15 2008-08-27 日本轻金属株式会社 具有优异模压成型性及连续电阻点焊性的铝合金板及其生产方法
RU2501881C2 (ru) * 2010-04-08 2013-12-20 Леонид Мордухович Коганов Способ холодной многопроходной прокатки тонких лент из алюминиевых сплавов
JP5675447B2 (ja) * 2011-03-10 2015-02-25 株式会社神戸製鋼所 樹脂被覆缶胴用アルミニウム合金板およびその製造方法
JP2012188703A (ja) * 2011-03-10 2012-10-04 Kobe Steel Ltd 樹脂被覆缶胴用アルミニウム合金板およびその製造方法
RU2602583C2 (ru) * 2015-04-20 2016-11-20 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ изготовления тонких полос из труднодеформируемых алюминий-литиевых сплавов
WO2018187406A1 (en) * 2017-04-05 2018-10-11 Novelis Inc. Anodized quality 5xxx aluminum alloys with high strength and high formability and methods of making the same
DE102018215254A1 (de) * 2018-09-07 2020-03-12 Neuman Aluminium Austria Gmbh Aluminiumlegierung, Halbzeug, Dose, Verfahren zur Herstellung eines Butzen, Verfahren zur Herstellung einer Dose sowie Verwendung einer Aluminiumlegierung

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4235646A (en) * 1978-08-04 1980-11-25 Swiss Aluminium Ltd. Continuous strip casting of aluminum alloy from scrap aluminum for container components
US4407679A (en) * 1980-11-19 1983-10-04 National Steel Corporation Method of producing high tensile aluminum-magnesium alloy sheet and the products so obtained
US4411707A (en) * 1981-03-12 1983-10-25 Coors Container Company Processes for making can end stock from roll cast aluminum and product
US4435213A (en) * 1982-09-13 1984-03-06 Aluminum Company Of America Method for producing aluminum powder alloy products having improved strength properties
SU1748899A1 (ru) * 1989-09-01 1992-07-23 Институт машиноведения Уральского отделения АН СССР Способ обработки материалов в водородсодержащей среде
US5186235A (en) * 1990-10-31 1993-02-16 Reynolds Metals Company Homogenization of aluminum coil
EP0504077B1 (fr) * 1991-03-14 1996-10-09 Pechiney Rhenalu Alliages d'al pour emboutissage-étirage résistants, formables et isotropes
CA2081055C (en) * 1991-11-05 1999-12-21 John R. Eppeland Method and apparatus for heat treatment of metal parts utilizing infrared radiation
US5514228A (en) * 1992-06-23 1996-05-07 Kaiser Aluminum & Chemical Corporation Method of manufacturing aluminum alloy sheet
CA2096366C (en) * 1992-06-23 2008-04-01 Gavin F. Wyatt-Mair A method of manufacturing can body sheet
JP3290274B2 (ja) * 1993-11-15 2002-06-10 富士写真フイルム株式会社 平版印刷版支持体の製造方法

Also Published As

Publication number Publication date
IL110237A (en) 1998-02-22
ES2131696T3 (es) 1999-08-01
FR2707669A1 (fr) 1995-01-20
WO1995002708A1 (fr) 1995-01-26
EP0660882A1 (fr) 1995-07-05
CN1043580C (zh) 1999-06-09
CN1113659A (zh) 1995-12-20
US5616190A (en) 1997-04-01
DE69418581D1 (de) 1999-06-24
BR9405520A (pt) 1999-09-08
JPH08501604A (ja) 1996-02-20
CA2144757A1 (fr) 1995-01-26
CA2144757C (fr) 2004-06-08
FR2707669B1 (fr) 1995-08-18
DE69418581T2 (de) 1999-10-28
SA94150111B1 (ar) 2005-06-14
JP3689106B2 (ja) 2005-08-31
IL110237A0 (en) 1994-10-21

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