EP1440177A1 - Procede de production d'alliages d'aluminium de serie 5xxx a proprietes mecaniques superieures par coulee entre cylindres - Google Patents
Procede de production d'alliages d'aluminium de serie 5xxx a proprietes mecaniques superieures par coulee entre cylindresInfo
- Publication number
- EP1440177A1 EP1440177A1 EP01970501A EP01970501A EP1440177A1 EP 1440177 A1 EP1440177 A1 EP 1440177A1 EP 01970501 A EP01970501 A EP 01970501A EP 01970501 A EP01970501 A EP 01970501A EP 1440177 A1 EP1440177 A1 EP 1440177A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- hours
- strip
- cold rolling
- period
- applying
- 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.)
- Withdrawn
Links
- 238000005266 casting Methods 0.000 title claims abstract description 37
- 238000000034 method Methods 0.000 title claims abstract description 37
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 12
- 230000008569 process Effects 0.000 title claims description 27
- 238000005097 cold rolling Methods 0.000 claims abstract description 25
- 238000000265 homogenisation Methods 0.000 claims abstract description 20
- 238000001953 recrystallisation Methods 0.000 claims abstract description 20
- 238000000137 annealing Methods 0.000 claims abstract description 17
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 5
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 5
- 229910045601 alloy Inorganic materials 0.000 claims description 39
- 239000000956 alloy Substances 0.000 claims description 39
- 238000011282 treatment Methods 0.000 claims description 33
- 229910052782 aluminium Inorganic materials 0.000 claims description 21
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 20
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- 239000000155 melt Substances 0.000 claims description 4
- 238000011143 downstream manufacturing Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 17
- 238000005260 corrosion Methods 0.000 abstract description 10
- 230000007797 corrosion Effects 0.000 abstract description 10
- 238000004519 manufacturing process Methods 0.000 description 12
- 230000000694 effects Effects 0.000 description 6
- 238000005204 segregation Methods 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910018134 Al-Mg Inorganic materials 0.000 description 3
- 229910018467 Al—Mg Inorganic materials 0.000 description 3
- 230000001747 exhibiting effect Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 239000007795 chemical reaction product Substances 0.000 description 2
- 210000001787 dendrite Anatomy 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000003887 surface segregation Methods 0.000 description 2
- 208000016261 weight loss Diseases 0.000 description 2
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000011164 primary particle Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000010186 staining Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
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
- C22F1/047—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 magnesium as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
- B22D11/003—Aluminium alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0622—Continuous 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
Definitions
- the present invention is directed to a process for the production of 5XXX series aluminum alloys, from continuously cast aluminum strip suitable for using in automotive and transportation applications, exhibiting superior or at least equivalent mechanical, microstructural, corrosion resistance and formability properties than those of similar alloys produced by the DC casting routes.
- Weight reduction is a primary goal in transportation industry including especially automotive and marine technologies not only to improve fuel economy, but also to improve performance, safety & durability and to reduce emissions.
- the use of light-weight materials is one of the most promising ways of achieving this goal and aluminum currently offers the greatest potential for cost-effective weight savings in automotive body structures.
- Aluminum has the advantage over competitive materials due to a very attractive combination of density, strength, formability and ease of recycling. Although there is extensive use of aluminum in die-cast parts, wrought aluminum has so far been confined to relatively few applications.
- Al-Mg 5XXX series
- Al-Mg alloys have been used to form auto body trim parts, doors, hood, truck vessels, fuel tanks, pressurized air vessels of trucks, truck tanks, ships and their infrastructure and superstructure, dump truck bodies, cryogenic vessels and LPG tanks.
- Present invention relates to an aluminum alloy with high mechanical properties and method for its manufacture. Therefore, the invention has industrial applicability in the field of processing metals.
- a wrought Al-Mg alloy sheet produced through Twin Roll Casting technique and accordingly processed to its final gauge aiming to provide superior or at least equivalent microstructural, mechanical, corrosion resistance and formability properties compared to their counter parts produced by DC casting and mill route is provided.
- the sheet product contains essentially between 0,5-6,5 %Mg, 0, 0-0,50 % Si, 0, 0- 0,60 % Fe, 0, 0-1,2 % Mn, 0, 0-0,50%Cr by weight.
- Figure 1 is the flowchart showing the casting process according to the present invention
- Figure 2-a is the flowchart showing cold rolling and annealing processes according to an embodiment of the invention where no homogenization treatment is applied.
- Figure 2-b is the flowchart showing cold rolling and annealing processes according to another embodiment of the invention where a homogenization treatment is applied immediately after casting.
- Figure 2-c is the flowchart showing cold rolling and annealing processes according to a further embodiment of the invention where a homogenization treatment is applied following a cold rolling process.
- FIG 3 shows photographs of very fine discrete particles near the surface of (a) Alloy A, (c) Alloy B and (e) Alloy C in as-cast materials where interdendritic network of primary phases in the interior of the same strips are shown for (b) Alloy A, (d) Alloy B and (f) Alloy C.
- Figure 4 shows photographs of the staining observed after 96 hrs exposure to salt spray, on following samples (a) DC-cast A, (b) DC-cast B (c) strip cast A w/homog, (d) strip cast A w/o homog., (e) strip cast B w/homog., (f) strip cast B w/o homog. and (g) strip cast C w/homog.
- the present invention is directed to a process for the preparation of 5XXX series aluminum alloys, from continuously cast aluminum strip suitable for using in automotive and other transportation applications, exhibiting superior or at least equivalent mechanical, microstructural, corrosion resistance and formability properties than those of similar alloys produced by the DC casting routes.
- Twin Roll Casting technology When compared to the DC casting and hot mill method, Twin Roll Casting technology has a relatively shorter process route (Fig. 1) with less working of the metal. As is claimed in number of publications, the processing route, that comprises DC casting and successive hot mill operations, is envisioned as a unique way for the production of 5XXX series aluminum alloys in different thickness.
- the microstructure of the as-cast strip is characterized by a dendritic structure of the aluminum solid solution with the primary phases marking the dendrite boundaries.
- the interdendritic network of the primary phases is well defined in the interior of the strip whereas it is deteriorated somewhat and is replaced by a very fine dispersion of discrete particles near the surface.
- the dendritic structure is quite uniform across the thickness of all strip samples.
- the microstructural features, i.e. dendrite arm spacing, primary particle size are relatively smaller at the surface and coarsened only slightly when approaching the center of the strip.
- variations across the thickness of the 5XXX as-cast strip are not as prominent as they are in some common foil and finstock alloys. The extent of supersaturation was largest in the alloys having high Mg content.
- Alloy B strip shows traces of surface segregation with eutectic rich bands, running in the casting direction, only along the edges of the cast strip. These bands, however, do not penetrate deep into the strip and were estimated to be less than 5 ⁇ m deep in the most severe cases. It should be noted that this edge region of any cast strip is removed by an edge trimming operation during cold rolling. There is hardly any evidence of surface segregation in Alloy A and Alloy C strip. Some intergranular and centerline segregation is also observed in all strip samples. The latter occasionally produced channels of solute-rich material and is most prominent in the Alloy B. Although centerline segregation is believed to have negative effects on mechanical properties -at least to some extent-, these effects may be minimized with appropriate casting parameters.
- Two different processing routes (Fig. 2a and 2b-2c)wherein existence of homogenization treatment determining this difference, can be applied to the as-cast strip.
- Homogenization treatment of the strip is performed at the temperature between 420° and 550 °C for a period of time, preferably not less than 4 hours and not more than 15 hours.
- Homogenization treatment is carried out in an inert gas atmosphere of the batch annealing furnaces.
- two different methods are employed depending on when it is applied: While homogenization treatment can be performed at the casting gauge (Fig. 2b), it can also be applied after a first cold rolling pass that must provide at least 25% reduction in the thickness of as-cast strip (Fig. 2c).
- the grain structure at the final gauge is improved in a profound way when cast strip is homogenized after a cold rolling pass .
- the homogenized strip material is subjected to cold rolling wherein no recrystallization anneal is applied until a critical gauge. Recrystallization anneal at this critical gauge and subsequently applied predetermined amount of cold working and application of back annealing procedure at the final gauge, as a final step in the production cycle, provides strain hardened and partially annealed, H2X tempers, final products including, H22, H24, H26.
- Recrystallization at the final gauge in practice of the present invention is in the range of 280° to about 375°C, preferably for about 2 to 8 hours.
- as-cast strip Prior to the recrystallization anneal applied to obtain 0 temper material at the final gauge, as-cast strip is cold rolled to the final gauge without applying any intermediate annealing in processing route as shown in Fig. 2a.
- the material that is subjected to the homogenization treatment, according to the processing routes shown in Fig. 2b and 2c is also cold rolled to the aimed gauge without application of intermediate annealing.
- Intermediate annealing applied at the predetermined stage of the processing route is also considered as recrystallization anneal and carried out by applying the same temperature and time combination.
- Back annealing temperatures to render H2X temper materials at the final gauge are in the range of 130°-250°C, preferably 2 to 8 hours.
- Aforementioned processing routes of the present invention that comprises a homogenization treatment, can be altered in the way of eliminating homogenization treatment by keeping the other down stream operations in effect (Fig. 2-a). Absence of homogenization step in the processing route does not create substantial changes in the mechanical properties, microscopic features, corrosion resistance and formability properties of the Twin Roll Cast 5XXX series alloys at different tempers (soft, strain hardened, or H2X/H3X) of final gauges. This radical alteration in the processing route provides significant contribution to the economical aspect of Twin Roll Cast 5XXX series alloys, as well.
- the melt was thoroughly mixed and then in-line refining was applied with chlorine and inert gas mixture to reduce the hydrogen content of the melt below 0,20ml/100 grams of metal and its inclusion content. Hydrogen gas level was reduced to 0,12ml/100 grams of metal.
- the metal was cast in the form of 1750 mm wide, 5,35 mm thick industrial size coils. Prior to cold rolling operation, one of the cast coil was homogenized in inert atmosphere. Coil was cold rolled in successive passes to its final gauge of 1mm without any intermediate recrystallization anneal. Soft temper of the material was achieved with final a recrystallization anneal. Another coil was processed through the same processing route, with the exception of homogenization treatment, to the final gauge of 1mm.
- An aluminum alloy in accordance with the present invention designated "B” consisted essentially of the elements stated in Table 3. This alloy was cast into 5,45 mm thick strip.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Metal Rolling (AREA)
- Continuous Casting (AREA)
Abstract
L'invention concerne un procédé de fabrication de bandes d'alliage d'aluminium à grain fin façonnables qui contiennent (en poids) essentiellement entre 0,5-6,5 % Mg, 0-0,50 % Si, 0-0,60 % Fe, 0-1,2 % Mn, 0-0,50 % Cr. Ce procédé comporte les étapes consistant à mettre en oeuvre une coulée entre cylindres en vue d'obtenir une épaisseur comprise entre 4 et 6,5 mm ; à laminer à froid les bandes à une épaisseur intermédiaire ; et à recuire et laminer à nouveau le matériau d'épaisseur intermédiaire. Le matériau recuit et relaminé est ensuite laminé à froid à une épaisseur de feuille finale, cette étape étant suivie d'une recristallisation finale ou recuit inverse. Le réglage combiné des paramètres de coulée, des quantités de Fe, Si, Mn, Cr et Mg et des températures de relaminage et de recuit final, permet d'obtenir un produit feuille amélioré du point de vue de la finesse du grain, qui présente un allongement et une aptitude au façonnage accrues ainsi que de bonnes propriétés d'adoucissement dû à l'âge et de résistance à la corrosion. L'homogénéisation peut être mise en oeuvre à une température comprise entre 420 °C et 550 °C pendant une durée de 4 à 15 heures, et la recristallisation est mise en oeuvre à une température comprise entre 280 °C et 375 °C pendant une durée d'au moins 4 heures, et de 8 heures au maximum.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/TR2001/000046 WO2003027345A1 (fr) | 2001-09-25 | 2001-09-25 | Procede de production d'alliages d'aluminium de serie 5xxx a proprietes mecaniques superieures par coulee entre cylindres |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1440177A1 true EP1440177A1 (fr) | 2004-07-28 |
Family
ID=21619333
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP01970501A Withdrawn EP1440177A1 (fr) | 2001-09-25 | 2001-09-25 | Procede de production d'alliages d'aluminium de serie 5xxx a proprietes mecaniques superieures par coulee entre cylindres |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20040256079A1 (fr) |
| EP (1) | EP1440177A1 (fr) |
| WO (1) | WO2003027345A1 (fr) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2002951075A0 (en) * | 2002-08-29 | 2002-09-12 | Commonwealth Scientific And Industrial Research Organisation | Twin roll casting of magnesium and magnesium alloys |
| CN1647870B (zh) * | 2004-01-20 | 2010-04-14 | 李华伦 | 金属薄板双辊异步铸轧机 |
| US7260972B2 (en) * | 2004-03-10 | 2007-08-28 | General Motors Corporation | Method for production of stamped sheet metal panels |
| US20060042727A1 (en) * | 2004-08-27 | 2006-03-02 | Zhong Li | Aluminum automotive structural members |
| WO2006077779A1 (fr) * | 2005-01-19 | 2006-07-27 | Kabushiki Kaisha Kobe Seiko Sho | Plaque en alliage d’aluminium et procede pour la fabriquer |
| JP5135684B2 (ja) * | 2006-01-12 | 2013-02-06 | 日本軽金属株式会社 | 高温高速成形性に優れたアルミニウム合金板およびその製造方法 |
| JP4203508B2 (ja) | 2006-03-08 | 2009-01-07 | 株式会社神戸製鋼所 | アルミニウム合金鋳造板の製造方法 |
| JP5728580B2 (ja) * | 2011-07-25 | 2015-06-03 | 日本軽金属株式会社 | アルミニウム合金板及びアルミニウム合金板の製造方法 |
| CN102989770B (zh) * | 2012-11-17 | 2015-03-04 | 镇江鼎胜铝业股份有限公司 | 用3004合金铸轧坯料生产窗帘铝板带的方法 |
| CN103834885B (zh) * | 2014-03-14 | 2016-06-08 | 重庆大学 | 一种提高铝合金板材塑性的热处理方法 |
| CN105886856B (zh) * | 2014-12-29 | 2018-12-25 | 通力股份公司 | 一种铝合金,由其制造的机械部件,以及其用途 |
| MX2018015415A (es) * | 2016-06-28 | 2019-05-27 | Novelis Inc | Aleaciones de aluminio de calidad anodizado y productos y metodos relacionados. |
| CN112159915A (zh) * | 2020-09-27 | 2021-01-01 | 酒泉钢铁(集团)有限责任公司 | 一种应用铜辊套铸轧制备1070铝合金带坯的方法 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU507351B2 (en) * | 1974-12-23 | 1980-02-14 | Hunter Engineering Co. Inc. | Roll casting |
| JPS5822363A (ja) * | 1981-07-30 | 1983-02-09 | Mitsubishi Keikinzoku Kogyo Kk | 超塑性アルミニウム合金板の製造方法 |
| 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 |
-
2001
- 2001-09-25 US US10/490,111 patent/US20040256079A1/en not_active Abandoned
- 2001-09-25 WO PCT/TR2001/000046 patent/WO2003027345A1/fr not_active Ceased
- 2001-09-25 EP EP01970501A patent/EP1440177A1/fr not_active Withdrawn
Non-Patent Citations (1)
| Title |
|---|
| See references of WO03027345A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| US20040256079A1 (en) | 2004-12-23 |
| WO2003027345A1 (fr) | 2003-04-03 |
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