EP0902842B1 - Element de construction - Google Patents

Element de construction Download PDF

Info

Publication number
EP0902842B1
EP0902842B1 EP97920475A EP97920475A EP0902842B1 EP 0902842 B1 EP0902842 B1 EP 0902842B1 EP 97920475 A EP97920475 A EP 97920475A EP 97920475 A EP97920475 A EP 97920475A EP 0902842 B1 EP0902842 B1 EP 0902842B1
Authority
EP
European Patent Office
Prior art keywords
component according
alloy
max
weight
alloy contains
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
EP97920475A
Other languages
German (de)
English (en)
Other versions
EP0902842B2 (fr
EP0902842A1 (fr
Inventor
Pius Schwellinger
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.)
3A Composites International AG
Original Assignee
Alusuisse Technology and Management Ltd
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=8225612&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0902842(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Alusuisse Technology and Management Ltd filed Critical Alusuisse Technology and Management Ltd
Priority to EP97920475A priority Critical patent/EP0902842B2/fr
Publication of EP0902842A1 publication Critical patent/EP0902842A1/fr
Application granted granted Critical
Publication of EP0902842B1 publication Critical patent/EP0902842B1/fr
Publication of EP0902842B2 publication Critical patent/EP0902842B2/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043—Changing 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 silicon as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
    • 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
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05—Changing 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 of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

Definitions

  • the invention relates to a component according to the preamble of claim 1.
  • Crash behavior is increasingly important in vehicle construction Aspect. This applies to road traffic as well as to rail transport.
  • the requirements for the finished component must also be observed.
  • the construction can be, for example certain strength level, certain minimum values of Elongation, corrosion resistance or other essential Characteristic values must be specified.
  • the alloy AA6005A currently used in wagon construction brings with it a number of problems in manufacturing, related to the tendency to recrystallize grainy.
  • With a coarse grain structure it is difficult to comply with the prescribed bending radii, which reduces the inclination to form grain boundary openings during welding is reinforced. This leads to a high number of non-conformities at the production. If you want to avoid this, you have to be produced so that the profile cross section predominantly Has fiber structure. This is currently only with one Alloy composition possible, which leads to higher pressing forces and significantly lower press speeds leads. However, this must result in major productivity losses in Purchase.
  • An alloy according to one of the features of claim 1 is in the DE-A-32 43 371 and disclosed in US-A-5 527 404. From aluminum pocket book (1983), pp. 141-143 is the course of the Hot curing at AlMgSi, known.
  • the invention has for its object a material with particularly good ductility with good mechanical To provide properties of the component.
  • the material is a comparable with the alloy AA6005A or have a lower strength level, but a higher one Ensure manufacturing reliability and higher productivity.
  • a component with the features of claim 1 leads to the achievement of the object according to the invention.
  • the alloy used is in terms of strength and stretch much less sensitive to quench than that Alloy AA6005A, and occurs even with wall thicknesses of 6 mm still a fine grain throughout. So that's it Alloy basically for use with large profiles suitable.
  • the content limits for silicon and magnesium in% by weight are preferably set as follows: silicon 0.45 to 0.75, in particular 0.55 to 0.65 magnesium 0.45 to 0.65, in particular 0.50 to 0.60
  • silicon 0.45 to 0.60 In particular 0.45 to 0.55 magnesium 0.40 to 0.60, especially 0.45 to 0.55
  • alloy composition according to the invention for the production of components with high energy absorption capacity leads to a favorable microstructure of the component structure.
  • the to improve the deformation properties The smallest possible grain size is achieved with the one according to the invention Alloy composition reached.
  • the special heat treatment gives the component particularly good properties Energy absorption with good strength values.
  • This first heat treatment consists in the generation of the aged or partially cured state T64, i.e. the alloy is not cured to maximum strength.
  • the Aged condition can be caused by a glow in the area between 120 and 170 ° C are produced, the annealing time in the range is between 4 and 16 h.
  • the desired degree of aging can be determined using a simple series of experiments become.
  • the second heat treatment in particular in the automotive industry also with paint baking can be combined consists in the generation of the outdated condition, T72, which is caused by a glow between and reached 230 ° C during an annealing period of 1 to 5 hours can be.
  • the components according to the invention are in the simplest case Extruded profiles. However, components are also conceivable that starting from an extruded profile as a preform, are finished by hydroforming. After a Another variant of the invention can also be a component Be a forged part.
  • a preferred use of the component according to the invention is seen as a safety part in vehicle construction.
  • the characteristic values of the tensile test can fluctuate depending on the precise analysis, degree of deformation, profile thickness and cooling conditions.
  • the following minimum values have been established based on previous experience: Profile thickness range 2 - 4 mm 4 - 8 mm Rp0.2 Rm A5 Rp0 Rm A5 [MPa] [MPa] [%] [MPa] [MPa] [%] Basic material 230 275 10 230 270 8th Butt joint (MIG) 120 180 .. 115 165 ..
  • the typical yield strength values are around 240 MPa the strength in the basic material lengthways around 290 MPa, the strains A5 by 12%. In the transverse direction are the yield strength and strength about the same height. A5 drops to 6%.
  • Cross samples were determined by profile and sample shape Press seams included. In no case was a break in the immediate Proximity of the press seam determined what on the due to the high degree of deformation particularly fine grain in the Press seam area is attributable. The hardness is in the range from 94 to 105 HB.
  • the characteristics of the welded joint apply to MIG machine welds. Differentiate in the specified thickness range the characteristic values when using SG-AlMg4, 5Mn-, SG-AlMg5- and SG-AlSi5 filler materials only a little. Error, such as edge misalignment, which is related to the problems with Welding can be attributed to large profiles the results stronger.
  • the typical values of the processed Weld connections are 130 for Rp0.2 MPa, for Rm at 210 MPa and for A100 at 4%. These are at one test was achieved about 30 days after welding. Cold curing in the heat affected zone is after not yet completed this time. In an exam after around 90 days there will be a further increase in Rp0.2 by around 10 MPa was found, while the strength only slightly increases, and the elongation within the measurement accuracy remains constant.
  • N 10 4 > 10 7 ⁇ ⁇ [MPa] [MPa] Basic material (lengthways) 110 Butt joint (MIG) 90 45 with raised seams 95 55 without night cant
  • the value for the base material was on 3 mm thick sections determined. Under comparable conditions, for AA6005A generally reaches values ⁇ 100 MPa. The values of Welded joints were determined on 4 mm thick samples.
  • the typical values of strength in the basic material lengthways are at 255 MPa, the strains A5 by 22%. In the transverse direction the strength drops slightly to 250 MPa. A5 falls to 12% from. Press seams are included in all tested cross samples. In no case was a break in the immediate vicinity of the Press seam determined. The hardness is in the range from 74 to 85 HB.
  • the typical values of the welded joint processed are 130 MPa for Rp0.2, 210 MPa for Rm and A100 at 10%. Such a high elongation is exceptional. This has a very favorable effect in the event of a crash. Also be here even higher after about 90 days of storage at room temperature Rp0.2 values reached.
  • Position 1 is entirely in the weld metal, position 5 in the unaffected basic material.
  • the behavior in the event of a crash essentially depends on the material properties, shape and dimension of the crash element used.
  • a first requirement for the suitability of a material in a certain shape and dimension is folding without premature breakage.
  • Sections of pipes or hollow sections of rectangular cross-section that are compressed are used to test the crash behavior.
  • Alloys A, B and C were compared in a first series of experiments, and alloys B, D and E in a second series of experiments with the compositions below.
  • Si Fe Cu Mn Mg Cr Zn V Ti A 0.45 0.21 0.02 0.02 0.43 - 0.03 - 0.02 B 0.54 0.21 - 0.08 0.59 - - - 0.01 C.
  • D 0.52 0.21 - 0.08 0.57 - - 0.09 0.01 E 0.51 0.21 0.11 0.06 0.49 - - 0.10 0.01
  • Alloys D and E have the highest values of the absorbed Energy related to the mass of the crash element.
  • the alloy recrystallizes fine-grained when pressed, with a remnant of a deformation structure in the grains remains. This is the main foundation for the below many aspects better properties compared to the alloy AA6005A.
  • the fine-grained recrystallization requires a sufficient degree of deformation in relation to time.
  • the alloy according to the invention is easy to weld. At Butt joints from profile sections, from large profiles worked out and welded with SG-AlMg4.5Mn filler material are never significant for wall thicknesses up to 6 mm Grain boundary openings have been observed.
  • the alloy according to the invention is well suited for the Use in vehicle construction.
  • the for the basic material and the Welded connection required characteristic values of the tensile test will be reached safely.
  • the alloy is for small and for large profiles can be used in the same way. It is for Crash elements and for components that are formed by hydroforming are produced, equally suitable.
  • the production security is due to the lower quench sensitivity and fine-grained recrystallization the alloy according to the invention much better than for the alloy AA6005A.
  • the pressing speed can be compared to AA6005A in general be increased by more than 50%.
  • the alloy according to the invention has proven to be one Alloy with a good combination of properties of strength, Elongation, weldability and production security proven.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Body Structure For Vehicles (AREA)
  • Glass Compositions (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Laminated Bodies (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Conductive Materials (AREA)
  • Extrusion Of Metal (AREA)

Claims (15)

  1. Elément de construction fabriqué dans un alliage de type AlMgSi, à haut pouvoir d'absorption d'énergie cinétique par déformation plastique, caractérisé en ce que l'alliage contient en % en poids silicium 0,40 à 0,80 magnésium 0,40 à 0,70 fer max. 0,30 cuivre max. 0,20 manganèse max. 0,15 vanadium 0,05 à 0,20 chrome max. 0,10 titane max. 0,10 zinc max. 0,10
    ainsi que d'autres éléments d'alliage max. 0,05 de chacun, au total max. 0,15 et le reste sous forme d'aluminium, et en ce que l'alliage se trouve à l'état partiellement vieilli T64 ou dans l'état survieilli T72.
  2. Elément de construction suivant la revendication 1, caractérisé en ce que l'alliage contient en % en poids du silicium et 0,45 à 0,75, de préférence 0,55 à 0,65, du magnésium 0,45 à 0,65, de préférence 0,50 à 0,60.
  3. Elément de construction suivant la revendication 1, caractérisé en ce que l'alliage contient en % en poids du silicium et 0,40 à 0,60, de préférence 0,45 à 0,55, du magnésium 0,40 à 0,60, de préférence 0,45 à 0,55.
  4. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient de 0,18 à 0,25% en poids de fer.
  5. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient de 0,12 à 0,16% en poids de cuivre.
  6. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient de 0,05 à 0,10% en poids de manganèse.
  7. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient de 0,06 à 0,15% en poids de vanadium.
  8. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient au max. 0,08, de préférence max. 0,01% en poids de chrome.
  9. Elément de construction suivant l'une des revendications 1 à 3, caractérisé en ce que l'alliage contient au max. 0,05% en poids de titane.
  10. Elément de construction suivant l'une des revendications 1 à 9, caractérisé en ce que l'alliage se trouve dans l'état partiellement vieilli T64 après un traitement thermique pendant 4 à 16 heures à 120 à 170°C.
  11. Elément de construction suivant l'une des revendications 1 à 9, caractérisé en ce que l'alliage se trouve dans l'état survieilli T72 après un traitement thermique pendant 1 à 5 heures à 190 à 230°C.
  12. Elément de construction suivant l'une des revendications 1 à 11, caractérisé en ce qu'il est fabriqué sous forme de profilé extrudé.
  13. Elément de construction suivant l'une des revendications 1 à 11, caractérisé en ce qu'il est fabriqué par formage sous haute pression intérieure à partir d'un profilé extrudé.
  14. Elément de construction suivant l'une des revendications 1 à 11, caractérisé en ce qu'il est fabriqué par forgeage.
  15. Utilisation d'un élément de construction suivant l'une des revendications 1 à 14 comme élément de sécurité dans la construction de véhicules.
EP97920475A 1996-05-22 1997-05-16 Methode de production d'un element de construction Expired - Lifetime EP0902842B2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP97920475A EP0902842B2 (fr) 1996-05-22 1997-05-16 Methode de production d'un element de construction

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
EP96810325A EP0808911A1 (fr) 1996-05-22 1996-05-22 Elément de construction
EP96810325 1996-05-22
EP97920475A EP0902842B2 (fr) 1996-05-22 1997-05-16 Methode de production d'un element de construction
PCT/CH1997/000193 WO1997044501A1 (fr) 1996-05-22 1997-05-16 Element de construction

Publications (3)

Publication Number Publication Date
EP0902842A1 EP0902842A1 (fr) 1999-03-24
EP0902842B1 true EP0902842B1 (fr) 2001-09-05
EP0902842B2 EP0902842B2 (fr) 2007-06-06

Family

ID=8225612

Family Applications (2)

Application Number Title Priority Date Filing Date
EP96810325A Withdrawn EP0808911A1 (fr) 1996-05-22 1996-05-22 Elément de construction
EP97920475A Expired - Lifetime EP0902842B2 (fr) 1996-05-22 1997-05-16 Methode de production d'un element de construction

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP96810325A Withdrawn EP0808911A1 (fr) 1996-05-22 1996-05-22 Elément de construction

Country Status (8)

Country Link
US (1) US6685782B1 (fr)
EP (2) EP0808911A1 (fr)
AT (1) ATE205261T1 (fr)
AU (1) AU2688197A (fr)
DE (1) DE59704542D1 (fr)
ES (1) ES2162285T3 (fr)
WO (1) WO1997044501A1 (fr)
ZA (1) ZA974318B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1785499A2 (fr) 2005-11-14 2007-05-16 Otto Fuchs KG Elément de construction pour l'absorption d'énergie
EP2072628A1 (fr) * 2007-12-19 2009-06-24 Aleris Aluminum Bonn GmbH Alliage d'aluminium haute résistance résistant aux collisions

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69825414T3 (de) * 1998-02-17 2011-05-05 Aleris Aluminum Bonn Gmbh Aluminium-Legierung und Verfahren zu ihrer Herstellung
GB2376337B (en) * 1998-05-05 2003-01-22 Jay Chieh Chen A cryptographic method for electronic transactions
CH693673A5 (de) * 1999-03-03 2003-12-15 Alcan Tech & Man Ag Verwendung einer Aluminiumlegierung vom Typ AlMgSi zur Herstellung von Strukturbauteilen.
EP1118686B1 (fr) * 2000-01-19 2003-09-17 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
US20050000609A1 (en) * 2002-12-23 2005-01-06 Butler John F. Crash resistant aluminum alloy sheet products and method of making same
DE102004030021B4 (de) * 2003-07-09 2009-11-26 Aleris Aluminum Duffel Bvba Gewalztes Produkt
FR2857376B1 (fr) * 2003-07-09 2008-08-22 Corus Aluminium Nv ALLIAGE DE AlMgSi
DE102007012894A1 (de) * 2007-03-17 2008-04-03 Daimler Ag Verwendung eines Schweißzusatzwerkstoffs und Bauelement für ein Kraftfahrzeug
CN100482828C (zh) * 2007-05-09 2009-04-29 东北轻合金有限责任公司 一种高精度铝合金波导管的制造方法
JP2013525608A (ja) 2010-04-26 2013-06-20 サパ アーベー 階層状の微細構造を有する損傷耐性アルミ材
EP2518173B1 (fr) 2011-04-26 2017-11-01 Benteler Automobiltechnik GmbH Procédé de fabrication d'un composant de structure en tôle ainsi que composant de structure en tôle
PL3339457T3 (pl) 2012-04-25 2020-12-14 Norsk Hydro Asa Wyciskany profil stopu aluminium al-mg-si o polepszonych właściwościach
CN104046865A (zh) * 2013-03-12 2014-09-17 亚太轻合金(南通)科技有限公司 一种高强度可锻造铝合金棒材及其制备方法
EP2993244B1 (fr) * 2014-09-05 2020-05-27 Constellium Valais SA (AG, Ltd) Procédé de fabrication d'un produit extrudé en aluminium alliage 6xxx avec d'excellentes performances de l'accident
CN104561686A (zh) * 2014-12-31 2015-04-29 东莞市东兴铝业有限公司 能抵受冷热凝变的铝合金材料及其制备工艺
EP3064305A1 (fr) 2015-03-03 2016-09-07 Constellium Valais SA (AG, Ltd) Pièces constituées d'alliages d'aluminium de la série 6xxx, soudées à l'arc, généralement pour des applications de transport
FR3042140B1 (fr) 2015-10-12 2017-10-20 Constellium Neuf-Brisach Composant de structure de caisse automobile presentant un excellent compromis entre resistance mecanique et comportement au crash
CN105483464B (zh) * 2015-12-17 2017-09-22 上海友升铝业有限公司 一种适用于汽车保险杠吸能盒的Al‑Mg‑Si系合金材料
CA3032261A1 (fr) 2016-08-26 2018-03-01 Shape Corp. Procede de formage a chaud et appareil de pliage transversal d'une poutre d'aluminium profilee pour former a chaud un composant structural de vehicule
CN110114498A (zh) 2016-10-24 2019-08-09 形状集团 用于生产车辆零件的多阶段铝合金形成与热加工方法
NO20211429A1 (en) * 2021-11-24 2023-05-25 Norsk Hydro As A 6xxx aluminium alloy with improved properties and a process for manufacturing extruded products
WO2023220830A1 (fr) * 2022-05-18 2023-11-23 Rio Tinto Alcan International Limited Alliage d'aluminium à résistance et ductilité améliorées

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1325565A (fr) † 1962-06-21 1963-04-26 Sulzer Ag Procédé et dispositif de façonnage à froid de corps profilés creux
FR2273077A1 (en) † 1974-05-31 1975-12-26 Cegedur Shock-resistant, deformable aluminium alloy extrusions - contg. silicon and magnesium and suitable for crash barriers and car bumpers
US3938991A (en) * 1974-07-15 1976-02-17 Swiss Aluminium Limited Refining recrystallized grain size in aluminum alloys
JPS544806A (en) * 1977-06-15 1979-01-13 Sumitomo Light Metal Ind Extrusion aluminum alloy having good quenching propertity
DE3243371A1 (de) 1982-09-13 1984-03-15 Schweizerische Aluminium AG, 3965 Chippis Aluminiumlegierung
IT1154589B (it) * 1982-11-26 1987-01-21 Italia Alluminio Leghe di alluminio per apparecchiature nucleari
US4637842A (en) * 1984-03-13 1987-01-20 Alcan International Limited Production of aluminum alloy sheet and articles fabricated therefrom
JPS61163232A (ja) * 1985-01-11 1986-07-23 Kobe Steel Ltd 高強度Ａｌ−Ｍｇ−Ｓｉ系合金およびその製造法
JPS6296640A (ja) * 1985-10-23 1987-05-06 Nippon Light Metal Co Ltd 微細再結晶粒を有するアルミニウム合金
JPS6296638A (ja) * 1985-10-24 1987-05-06 Nippon Light Metal Co Ltd リ−ドフレ−ム用アルミニウム合金
BE906107A (fr) * 1986-12-30 1987-04-16 Alusuisse Alliage a base d'aluminium.
JPH0747804B2 (ja) * 1991-03-18 1995-05-24 住友軽金属工業株式会社 成形性、形状凍結性及び塗装焼付硬化性に優れた異方性の少ないアルミニウム合金材の製造法
JPH04147935A (ja) * 1990-10-11 1992-05-21 Mitsubishi Alum Co Ltd ろう付け性の良好な高強度Ａｌ合金
JPH0747806B2 (ja) * 1991-05-20 1995-05-24 住友軽金属工業株式会社 高強度アルミニウム合金押出形材の製造方法
JPH0747808B2 (ja) * 1993-02-18 1995-05-24 スカイアルミニウム株式会社 成形性および焼付硬化性に優れたアルミニウム合金板の製造方法
JP2626958B2 (ja) * 1993-03-16 1997-07-02 スカイアルミニウム株式会社 成形性および焼付硬化性に優れたアルミニウム合金板の製造方法
DE4421744C2 (de) * 1993-07-02 1996-05-23 Fuchs Fa Otto Verwendung einer Knetlegierung des Types AlMgSiCu zur Herstellung von hochfesten und korrosionsbeständigen Teilen
JPH073371A (ja) * 1994-01-26 1995-01-06 Sky Alum Co Ltd 燐酸亜鉛処理用アルミニウム合金板およびその製造方法
US5571347A (en) * 1994-04-07 1996-11-05 Northwest Aluminum Company High strength MG-SI type aluminum alloy
US5527404A (en) * 1994-07-05 1996-06-18 Aluminum Company Of America Vehicle frame components exhibiting enhanced energy absorption, an alloy and a method for their manufacture
JP3359428B2 (ja) * 1994-08-05 2002-12-24 スカイアルミニウム株式会社 成形加工用アルミニウム合金板の製造方法
FR2726007B1 (fr) † 1994-10-25 1996-12-13 Pechiney Rhenalu Procede de fabrication de produits en alliage alsimgcu a resistance amelioree a la corrosion intercristalline
ATE188259T1 (de) * 1996-04-10 2000-01-15 Alusuisse Lonza Services Ag Bauteil

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1785499A2 (fr) 2005-11-14 2007-05-16 Otto Fuchs KG Elément de construction pour l'absorption d'énergie
EP2072628A1 (fr) * 2007-12-19 2009-06-24 Aleris Aluminum Bonn GmbH Alliage d'aluminium haute résistance résistant aux collisions

Also Published As

Publication number Publication date
EP0902842B2 (fr) 2007-06-06
ES2162285T3 (es) 2001-12-16
EP0808911A1 (fr) 1997-11-26
EP0902842A1 (fr) 1999-03-24
US6685782B1 (en) 2004-02-03
ATE205261T1 (de) 2001-09-15
WO1997044501A1 (fr) 1997-11-27
DE59704542D1 (de) 2001-10-11
ZA974318B (en) 1998-01-30
AU2688197A (en) 1997-12-09

Similar Documents

Publication Publication Date Title
EP0902842B1 (fr) Element de construction
DE19830560B4 (de) Energie-absorbierendes Element
EP3083239B1 (fr) Produit en acier plat pour composants d'un carrosserie de vehicule automobile
DE112010003614B4 (de) Hochfeste Schraube
DE69212602T2 (de) Hochfeste al-ci-legierung mit niedriger dichte
EP0104139B1 (fr) Alliage à base d'aluminium
DE102008033027B4 (de) Verfahren zur Erhöhung von Festigkeit und Verformbarkeit von ausscheidungshärtbaren Werkstoffen
EP0576107B1 (fr) Utilisation d'un acier pour la fabrication de tubes
EP2449145B1 (fr) Bande AIMgSi pour applications ayant des exigences de déformation élevées
DE69517026T2 (de) Kaltgeformte hochfeste stahlprofile
DE202012000616U1 (de) Struktur- und/oder Karosseriebauteil für ein Kraftfahrzeug mit verbesserten Crasheigenschaften und Korrosionsschutz
DE102005014298A1 (de) Panzerung für ein Fahrzeug
DE69620771T2 (de) Verwendung von gewalzte aluminiumlegierungen für konstruktionsteile von fahrzeuge
DE69825414T3 (de) Aluminium-Legierung und Verfahren zu ihrer Herstellung
EP1685268B1 (fr) Procédé de fabrication d'une piece de carrosserie de vehicule automobile
DE2750867C2 (de) Verwendung einer Stahllegierung für Rohre zur Türverstärkung
DE102016113599A1 (de) Wärmebehandlung zur Verringerung von Verzerrung
WO2009090228A1 (fr) Composants en acier moulé solide et ductile, à forte teneur en manganèse, procédé de production et utilisation de ceux-ci
EP1165848B1 (fr) UTILISATION D'UN ALLIAGE D'ALUMINIUM DU TYPE AlMgSi COMME PIECE DE SECURITE DE VEHICULES
EP1785499A2 (fr) Elément de construction pour l'absorption d'énergie
EP1171643B1 (fr) Alliages de magnesium a haute ductilite, leur procede de production et leur utilisation
DE10231437B4 (de) Verfahren zur Herstellung eines Aluminiumknetlegierungsprodukts
EP0811700B1 (fr) Alliage d'aluminium du type AlMgSi soudable et apte à l'emboutissage profond
EP1474538B1 (fr) Utilisation d'alliage d'acier comme materiau pour des tuyaux pour produire des recipients etanches aux gaz ou comme materiau pour produire des elements moules dans le domaine de la construction legere en acier
DE102019103502A1 (de) Verfahren zur Herstellung eines nahtlosen Stahlrohres, nahtloses Stahlrohr und Rohrprodukt

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: 19981222

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE ES FI FR GB IT LI NL SE

17Q First examination report despatched

Effective date: 19990504

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

ITF It: translation for a ep patent filed
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): AT BE CH DE ES FI FR GB IT LI NL SE

REF Corresponds to:

Ref document number: 205261

Country of ref document: AT

Date of ref document: 20010915

Kind code of ref document: T

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20010905

REF Corresponds to:

Ref document number: 59704542

Country of ref document: DE

Date of ref document: 20011011

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: ALCAN TECHNOLOGY & MANAGEMENT AG

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2162285

Country of ref document: ES

Kind code of ref document: T3

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

NLT2 Nl: modifications (of names), taken from the european patent patent bulletin

Owner name: ALCAN TECHNOLOGY & MANAGEMENT AG

ET Fr: translation filed
PLBQ Unpublished change to opponent data

Free format text: ORIGINAL CODE: EPIDOS OPPO

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PLBQ Unpublished change to opponent data

Free format text: ORIGINAL CODE: EPIDOS OPPO

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PLBF Reply of patent proprietor to notice(s) of opposition

Free format text: ORIGINAL CODE: EPIDOS OBSO

26 Opposition filed

Opponent name: ERBSLOEH AG

Effective date: 20020517

26 Opposition filed

Opponent name: PECHINEY

Effective date: 20020604

Opponent name: ERBSLOEH AG

Effective date: 20020517

NLR1 Nl: opposition has been filed with the epo

Opponent name: ERBSLOEH AG

NLR1 Nl: opposition has been filed with the epo

Opponent name: PECHINEY

Opponent name: ERBSLOEH AG

PLBF Reply of patent proprietor to notice(s) of opposition

Free format text: ORIGINAL CODE: EPIDOS OBSO

PLBF Reply of patent proprietor to notice(s) of opposition

Free format text: ORIGINAL CODE: EPIDOS OBSO

PLBP Opposition withdrawn

Free format text: ORIGINAL CODE: 0009264

RDAF Communication despatched that patent is revoked

Free format text: ORIGINAL CODE: EPIDOSNREV1

PLAB Opposition data, opponent's data or that of the opponent's representative modified

Free format text: ORIGINAL CODE: 0009299OPPO

PLBQ Unpublished change to opponent data

Free format text: ORIGINAL CODE: EPIDOS OPPO

APBP Date of receipt of notice of appeal recorded

Free format text: ORIGINAL CODE: EPIDOSNNOA2O

R26 Opposition filed (corrected)

Opponent name: ERBSLOEH AG

Effective date: 20020517

APBQ Date of receipt of statement of grounds of appeal recorded

Free format text: ORIGINAL CODE: EPIDOSNNOA3O

NLR1 Nl: opposition has been filed with the epo

Opponent name: ERBSLOEH AG

APAA Appeal reference recorded

Free format text: ORIGINAL CODE: EPIDOS REFN

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

Ref country code: NL

Payment date: 20050429

Year of fee payment: 9

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

Ref country code: AT

Payment date: 20050504

Year of fee payment: 9

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

Ref country code: GB

Payment date: 20050511

Year of fee payment: 9

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

Ref country code: SE

Payment date: 20050519

Year of fee payment: 9

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

Ref country code: FI

Payment date: 20050520

Year of fee payment: 9

Ref country code: CH

Payment date: 20050520

Year of fee payment: 9

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

Ref country code: ES

Payment date: 20050609

Year of fee payment: 9

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

Ref country code: BE

Payment date: 20050624

Year of fee payment: 9

APAH Appeal reference modified

Free format text: ORIGINAL CODE: EPIDOSCREFNO

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: 20060516

Ref country code: FI

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

Effective date: 20060516

Ref country code: AT

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

Effective date: 20060516

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

Ref country code: SE

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

Effective date: 20060517

Ref country code: ES

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

Effective date: 20060517

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

Ref country code: LI

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

Effective date: 20060531

Ref country code: CH

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

Effective date: 20060531

Ref country code: BE

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

Effective date: 20060531

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

Ref country code: IT

Payment date: 20060531

Year of fee payment: 10

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 NON-PAYMENT OF DUE FEES

Effective date: 20061201

APBU Appeal procedure closed

Free format text: ORIGINAL CODE: EPIDOSNNOA9O

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

EUG Se: european patent has lapsed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20060516

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20061201

RTI2 Title (correction)

Free format text: METHOD OF PRODUCING A COMPONENT

PUAH Patent maintained in amended form

Free format text: ORIGINAL CODE: 0009272

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

Free format text: STATUS: PATENT MAINTAINED AS AMENDED

27A Patent maintained in amended form

Effective date: 20070606

AK Designated contracting states

Kind code of ref document: B2

Designated state(s): AT BE CH DE ES FI FR GB IT LI NL SE

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20060517

ET3 Fr: translation filed ** decision concerning opposition
BERE Be: lapsed

Owner name: *ALUSUISSE TECHNOLOGY & MANAGEMENT A.G.

Effective date: 20060531

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

Effective date: 20070516

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

Owner name: CONSTELLIUM SWITZERLAND AG, CH

Effective date: 20111130

Ref country code: FR

Ref legal event code: CD

Owner name: CONSTELLIUM SWITZERLAND AG, CH

Effective date: 20111130

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 59704542

Country of ref document: DE

Owner name: CONSTELLIUM SWITZERLAND AG, CH

Free format text: FORMER OWNER: ALUSUISSE TECHNOLOGY & MANAGEMENT AG, NEUHAUSEN AM RHEINFALL, CH

Effective date: 20120302

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 20

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

Ref country code: DE

Payment date: 20160527

Year of fee payment: 20

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

Ref country code: FR

Payment date: 20160530

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 59704542

Country of ref document: DE