WO2003074747A1 - Tole ou ba 0nde en alliage al-mg pour la fabrication de pieces pliees a faible rayon de pliage - Google Patents

Tole ou ba 0nde en alliage al-mg pour la fabrication de pieces pliees a faible rayon de pliage Download PDF

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Publication number
WO2003074747A1
WO2003074747A1 PCT/FR2003/000691 FR0300691W WO03074747A1 WO 2003074747 A1 WO2003074747 A1 WO 2003074747A1 FR 0300691 W FR0300691 W FR 0300691W WO 03074747 A1 WO03074747 A1 WO 03074747A1
Authority
WO
WIPO (PCT)
Prior art keywords
sheet
mpa
strip according
strip
thickness
Prior art date
Application number
PCT/FR2003/000691
Other languages
English (en)
French (fr)
Inventor
Jean-Luc Hoffmann
Bruce Morere
Fabrice Helfer
Original Assignee
Pechiney Rhenalu
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
Application filed by Pechiney Rhenalu filed Critical Pechiney Rhenalu
Priority to DE60310381T priority Critical patent/DE60310381T2/de
Priority to PL369769A priority patent/PL198511B1/pl
Priority to AU2003238148A priority patent/AU2003238148A1/en
Priority to YUP-784/04A priority patent/RS50328B/sr
Priority to EP03735766A priority patent/EP1481106B1/de
Publication of WO2003074747A1 publication Critical patent/WO2003074747A1/fr

Links

Classifications

    • 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 invention relates to the manufacture of folded parts with a small bending radius, and most often stamped, intended in particular for automobile construction, from sheets or strips of aluminum alloy of the aluminum-magnesium type, that is to say - to say of the 5000 series according to the nomenclature of the Aluminum Association.
  • Aluminum-magnesium alloys with more than 4% magnesium are widely used in automobile construction for parts other than body skins, for example reinforcements or structural parts, possibly shaped by stamping or bending. They allow good mechanical resistance without requiring, like the skin alloys of the 6000 series, heat treatment for dissolution and quenching. Mention may be made, for example, of alloys 5019, 5182 and 5083, the composition of which (% by weight) registered with the Aluminum Association is indicated in Table 1:
  • stamped and folded parts requires a material having sufficient formability to produce the stamped parts of the parts, and a folding ability that is all the better when one wishes to obtain very small folding radii, typically of the order of 1. 'sheet thickness. This ability must be as good in the rolling direction as in the pe ⁇ endicular direction.
  • the sheet or strip must have as high a mechanical resistance as possible so as to reduce the thickness as much as possible, and thus obtain the optimal lightening effect resulting from the use of aluminum compared to the steel.
  • the object of the invention is to provide sheets and strips of Al-Mg alloy enabling these requirements to be satisfied.
  • the subject of the invention is a sheet or strip of aluminum alloy with a thickness of between 1 and 5 mm, intended for the manufacture of stamped and bent parts with a small bending radius, of composition (% by weight):
  • the invention also relates to a sheet or strip of preferential composition: Si ⁇ 0.3 Fe: 0.2 - 0.4 Mn: 0.3 - 0.45 Mg: 4.5 - 5.5 Cr ⁇ 0 , 04 - 0.1 Cu ⁇ 0.1 Zn ⁇ 0.1 other elements ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum, and, for this particular composition, Ro > 2 directions T> 240 MPa, At 8 o> 15% and R m - R 0.2 > 90 MPa.
  • It also relates to a process for manufacturing such a sheet or strip, comprising the casting of a plate of the above composition, its hot rolling up to a thickness e c , cold rolling to a final thickness ef between 70 and 40% of e c , and a restorative annealing at a temperature between
  • Example 1 The single figure illustrates the results of Example 1 in yield strength Ro > 2 and bending radius.
  • the invention is based on the combination of the close selection of an Al-Mg alloy composition with more than 4% Mg, and a particular manufacturing range to obtain a compromise of properties, in particular between the limit of elasticity, elongation and folding ability, particularly favorable for the production of stamped and bent parts with a small bending radius.
  • the alloys according to the invention are alloys with more than 4% of Mg like the alloys 5182, 5019 or 5083 mentioned above, and preferably with more than 4.5%.
  • Magnesium contributes to mechanical resistance and its content can be adjusted according to the mechanical resistance desired. Above 5.5% of Mg, the alloy becomes more difficult to cast and to process.
  • a particularly well-suited composition is as follows: Si ⁇ 0.3 Fe: 0.2 - 0.4 Mn -. 0.3 - 0.45 Mg: 4.5 - 5.5 Cu ⁇ 0.1 l Cr: 0.04 - 0.1
  • the control of the total content of manganese and chromium is an important point to obtain all the desired properties.
  • a content greater than 0.7% improves the elastic limit without reducing the elongation too much, but, surprisingly, gives a poor bending radius.
  • the method of manufacturing the strips according to the invention comprises the casting of a plate of the alloy considered, its hot rolling to obtain a strip of thickness e c , then its cold rolling to the final thickness e f , between 1 and 5 mm.
  • the final thickness ef must be between 40 and 10% of the thickness of the hot-rolled strip e c . If the cold rolling rate is insufficient, the desired yield strength cannot be reached. If it is too large, the work hardening coefficient n becomes too low and the formability is insufficient.
  • the cold rolled strip is then subjected to a restorative annealing at a temperature between 180 and 280 ° C.
  • the control of this temperature is important: an absence of restoration or a too low temperature harms the elongation. Conversely, an annealing temperature above 280 ° C leads to a recrystallized state, with insufficient mechanical strength.
  • An essential characteristic of the method of manufacturing strips and sheets according to the invention is the absence of re-hardening after the restoration annealing, either by cold rolling or by tensioning under tension. Admittedly, such a work hardening would increase the elastic limit, but would reduce too much the elongation and the coefficient of work hardening, which would be unfavorable to formability and to the ability to bend. In addition, the gain in elastic limit is lost very quickly during the curing treatment of the paints, while for restored and not rewashed products, the loss of mechanical resistance to the curing of the paints is more reduced.
  • Another advantage of the absence of work hardening, in particular by leveling, after restoration is to obtain sheets and strips having a low anisotropy, with a difference between the elastic limits in the directions L and T of less than 15 MPa , and most often less than 10 MPa ..
  • the sheets and strips according to the invention are particularly well suited to the production of stamped and folded parts with a small bending radius, in particular for the automotive industry. 180 ° bending radii are obtained which are less than the thickness of the sheet or strip, or even less than 80% of this thickness.
  • the work hardening coefficient n is greater than 0.10, which contributes to the rapid increase in the mechanical resistance of the parts during their shaping, and therefore to the use of smaller thicknesses.
  • the reinforcements of anti-intrusion sashes which include stamped and folded parts and which are subjected to the baking treatment of paints, in particular cataphoresis layers, may be mentioned.
  • the loss of yield strength remains below 20 MPa.
  • Another advantageous use of the sheets and strips according to the invention is the manufacture of jacks, which allow a significant weight gain compared to steel jacks.
  • the plates were hot rolled to obtain strips 5 mm thick, then cold rolled to 3 mm, ie 60% of the thickness of the hot strip.
  • the strips underwent restorative annealing at 200 ° C.
  • the elastic limit Ro j2 sense L, the elongation at break A 8 o according to standard NF EN 10002-1 relating to tensile tests on metallic materials, and the radius of folding at 180 ° were measured. The results are shown in Table 2: Table 2
  • FIG. 1 shows the compromise between the elastic limit Ro, 2 and the folding radius.
  • a radius of 1.5 mm is considered acceptable for an R 0j2 of 200 MPa and 2.5 mm for a Ro ; 2 of 280 MPa.
  • the points corresponding to the 5 alloys according to the invention are to the left of the right, and show a good compromise between the two properties.
  • the points corresponding to alloys F and G are to the right of the right and therefore do not present an acceptable compromise.
  • a 20 min heat treatment was carried out respectively at 170 ° C, 185 ° C and 200 ° C, simulating baking treatments of the paints of a motor vehicle, on sheet metal samples of Example 1 made of alloy C and E, and on a sample of the alloy C having undergone in addition a work hardening by planing by traction.
  • the mechanical characteristics were measured in the long direction, namely the tensile strength R m , the elastic limit R 0j2 and the elongation Ago, before and after heat treatment.
  • the results are shown in Tables 3 (for alloy C restored), 4 (for E) and 5 (for C hardened).
  • the thickness of the hot rolling outlet was varied, the final thickness remaining at 3 mm, so that the ratio ⁇ f / e c was varied between 70%> and 40%.
  • the final annealing temperature was also varied between 200 and 320 ° C. No work hardening after the final annealing was carried out. In each case, the tensile strength Rm, the elastic limit Ro , 2 , the elongation A and the work hardening coefficient n were measured. The results, corresponding to the average of 5 measurements, are shown in Table 7:

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Body Structure For Vehicles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Metal Rolling (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Electrolytic Production Of Metals (AREA)
PCT/FR2003/000691 2002-03-07 2003-03-04 Tole ou ba 0nde en alliage al-mg pour la fabrication de pieces pliees a faible rayon de pliage WO2003074747A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE60310381T DE60310381T2 (de) 2002-03-07 2003-03-04 Blech oder band aus al-mg-legierung zur herstellung von gebogenen teilen mit kleinem biegeradius
PL369769A PL198511B1 (pl) 2002-03-07 2003-03-04 Blacha lub taśma ze stopu glinu, sposób jej wytwarzania i jej zastosowanie
AU2003238148A AU2003238148A1 (en) 2002-03-07 2003-03-04 Al-mg alloy sheet or strip for the production of bent parts having a small bend radius
YUP-784/04A RS50328B (sr) 2002-03-07 2003-03-04 LIM ILI TRAKA OD Al-Mg LEGURE ZA PROIZVODNJU SAVIJENIH DELOVA MALOG RADIJUSA SAVIJANJA
EP03735766A EP1481106B1 (de) 2002-03-07 2003-03-04 Blech oder band aus al-mg-legierung zur herstellung von gebogenen teilen mit kleinem biegeradius

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0202897A FR2836929B1 (fr) 2002-03-07 2002-03-07 Tole ou bande en alliage a1-mg pour la fabrication de pieces pliees a faible rayon de pliage
FR02/02897 2002-03-07

Publications (1)

Publication Number Publication Date
WO2003074747A1 true WO2003074747A1 (fr) 2003-09-12

Family

ID=27763621

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2003/000691 WO2003074747A1 (fr) 2002-03-07 2003-03-04 Tole ou ba 0nde en alliage al-mg pour la fabrication de pieces pliees a faible rayon de pliage

Country Status (9)

Country Link
EP (1) EP1481106B1 (de)
AT (1) ATE348199T1 (de)
AU (1) AU2003238148A1 (de)
DE (1) DE60310381T2 (de)
ES (1) ES2279123T3 (de)
FR (1) FR2836929B1 (de)
PL (1) PL198511B1 (de)
RS (1) RS50328B (de)
WO (1) WO2003074747A1 (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140157894A1 (en) * 2012-12-12 2014-06-12 Tung Thih Electronic Co., Ltd. Transducer Case
CN103900629A (zh) * 2012-12-24 2014-07-02 同致电子企业股份有限公司 传感器外壳
EP3303649B1 (de) * 2015-06-05 2023-09-13 Novelis, Inc. Kraftfahrzeugkarosserieteil beinhaltend eine aluminiumlegierung und verfahren zur herstellung des kraftfahrzeugkarosserieteils

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4186034A (en) * 1978-07-05 1970-01-29 Swiss Aluminium Ltd. Method of manufacturing aluminum alloy sheets containing magnesium and zinc
US4284437A (en) * 1979-12-18 1981-08-18 Sumitomo Light Metal Industries, Ltd. Process for preparing hard tempered aluminum alloy sheet
JPH02149634A (ja) * 1988-11-30 1990-06-08 Kobe Steel Ltd 繰り返し曲げ性に優れたタブ用Al合金板とその製造方法
EP0385257A1 (de) * 1989-02-23 1990-09-05 Sumitomo Light Metal Industries Limited Verfahren zur Herstellung gehärteter Bleche aus Aluminiumlegierungen mit hoher Festigkeit und sehr guter Korrosionsbeständigkeit
JPH07316711A (ja) * 1994-05-30 1995-12-05 Sumitomo Light Metal Ind Ltd 曲げ加工性に優れた成形加工用アルミニウム合金板材およびその製造方法
US5512111A (en) * 1993-04-14 1996-04-30 Sumitomo Light Metal Industries, Ltd. Aluminum alloy material for shutter of recording medium cassette, process for producing the same, and aluminum alloy shutter made of the same
EP0799900A1 (de) * 1996-04-04 1997-10-08 Hoogovens Aluminium Walzprodukte GmbH Hochfeste Aluminium-Magnesium-Legierung für grosse Schweissstrukturen
US5985058A (en) * 1997-06-04 1999-11-16 Golden Aluminum Company Heat treatment process for aluminum alloys
EP1045043A1 (de) * 1999-04-12 2000-10-18 Pechiney Rhenalu Verfahren zur Herstellung von Formteilen aus Aluminiumlegierung vom Typ 2024
US6248193B1 (en) * 1997-09-11 2001-06-19 Nippon Light Metal Company, Ltd. Process for producing an aluminum alloy sheet
US6261391B1 (en) * 1994-05-11 2001-07-17 Honda Giken Kogyo Kabushiki Kaisha Aluminum alloy plate for super plastic molding capable of cold pre-molding, and production method for the same

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4186034A (en) * 1978-07-05 1970-01-29 Swiss Aluminium Ltd. Method of manufacturing aluminum alloy sheets containing magnesium and zinc
US4284437A (en) * 1979-12-18 1981-08-18 Sumitomo Light Metal Industries, Ltd. Process for preparing hard tempered aluminum alloy sheet
JPH02149634A (ja) * 1988-11-30 1990-06-08 Kobe Steel Ltd 繰り返し曲げ性に優れたタブ用Al合金板とその製造方法
EP0385257A1 (de) * 1989-02-23 1990-09-05 Sumitomo Light Metal Industries Limited Verfahren zur Herstellung gehärteter Bleche aus Aluminiumlegierungen mit hoher Festigkeit und sehr guter Korrosionsbeständigkeit
US5512111A (en) * 1993-04-14 1996-04-30 Sumitomo Light Metal Industries, Ltd. Aluminum alloy material for shutter of recording medium cassette, process for producing the same, and aluminum alloy shutter made of the same
US6261391B1 (en) * 1994-05-11 2001-07-17 Honda Giken Kogyo Kabushiki Kaisha Aluminum alloy plate for super plastic molding capable of cold pre-molding, and production method for the same
JPH07316711A (ja) * 1994-05-30 1995-12-05 Sumitomo Light Metal Ind Ltd 曲げ加工性に優れた成形加工用アルミニウム合金板材およびその製造方法
EP0799900A1 (de) * 1996-04-04 1997-10-08 Hoogovens Aluminium Walzprodukte GmbH Hochfeste Aluminium-Magnesium-Legierung für grosse Schweissstrukturen
US5985058A (en) * 1997-06-04 1999-11-16 Golden Aluminum Company Heat treatment process for aluminum alloys
US6248193B1 (en) * 1997-09-11 2001-06-19 Nippon Light Metal Company, Ltd. Process for producing an aluminum alloy sheet
EP1045043A1 (de) * 1999-04-12 2000-10-18 Pechiney Rhenalu Verfahren zur Herstellung von Formteilen aus Aluminiumlegierung vom Typ 2024

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 014, no. 397 (C - 0752) 28 August 1990 (1990-08-28) *
PATENT ABSTRACTS OF JAPAN vol. 1996, no. 04 30 April 1996 (1996-04-30) *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140157894A1 (en) * 2012-12-12 2014-06-12 Tung Thih Electronic Co., Ltd. Transducer Case
EP2743918A1 (de) * 2012-12-12 2014-06-18 Tung Thih Electronic Co., Ltd. Wandlergehäuse
CN103900629A (zh) * 2012-12-24 2014-07-02 同致电子企业股份有限公司 传感器外壳
EP3303649B1 (de) * 2015-06-05 2023-09-13 Novelis, Inc. Kraftfahrzeugkarosserieteil beinhaltend eine aluminiumlegierung und verfahren zur herstellung des kraftfahrzeugkarosserieteils

Also Published As

Publication number Publication date
EP1481106B1 (de) 2006-12-13
ES2279123T3 (es) 2007-08-16
PL369769A1 (en) 2005-05-02
AU2003238148A1 (en) 2003-09-16
RS50328B (sr) 2009-09-08
DE60310381T2 (de) 2007-09-20
EP1481106A1 (de) 2004-12-01
DE60310381D1 (de) 2007-01-25
PL198511B1 (pl) 2008-06-30
RS78404A (sr) 2006-12-15
FR2836929A1 (fr) 2003-09-12
ATE348199T1 (de) 2007-01-15
FR2836929B1 (fr) 2005-01-07

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