US3392062A - Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1% - Google Patents

Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1% Download PDF

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US3392062A
US3392062A US483345A US48334565A US3392062A US 3392062 A US3392062 A US 3392062A US 483345 A US483345 A US 483345A US 48334565 A US48334565 A US 48334565A US 3392062 A US3392062 A US 3392062A
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heat
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temperature
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US483345A
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Altenpohl Dietrich
Zoller Heinrich
Cohen Hans Michael
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Alcan Holdings Switzerland AG
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Alusuisse Holdings AG
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    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B3/00Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
    • 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
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon
    • 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
    • C22F1/05Changing 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 present invention refers to the production of strips and sheets from heat-treatable aluminum alloys, containing less than 1% copper which strips and sheets can reach their maximum strength by subsequent simple aging treatment.
  • the process of the present invention is especially suitable for aluminum-magnesium-silicon alloys, but is also suitable for aluminum-zinc-magnesium alloys with low magnesium content.
  • aluminummagnesium-silicon alloy herein refers to all aluminum alloys with a chemical composition lying between the following limits:
  • the basic metal can be aluminum of commercial purity (i.e. according to ASTN B209) as well as aluminum of high or highest purity (refined aluminum).
  • AA6011, AA6061 or AA6063 according to the Registration Record of Aluminum Association Alloy Designations and Chemical Composition Limites for Wrought Aluminum Alloys, published by The American Association, 420 Lexington Ave., N.Y., N.Y., 10017.
  • the aluminum-zinc-magnesium alloys referred to in this invention may contain Percent Zinc 3.5-5 Magnesium 0.5-1.5 Copper 1 Aluminum Balance Furthermore, these alloys may contain additions like manganese, chromium or other elements. Because of their 3,392,062 Patented July 9, 1968 ice relatively low magnesium content compared to materials like e.g. AA7075, AA7079, AA7178 etc. these alloys are designated as low alloyed.
  • the present invention allows a noticeable increase in the transit speed, thus permitting an economic production of sheets and strips in essentially copper-free, heat-treatable aluminnum alloys suitable for artificially aging.
  • the initial slab or plate has to be homogenized and hot-rolled while still in the warm condition.
  • the hot-rolled strip which should have a temperature of more than 350 C., preferably more than 400 C., then immediately has to be cooled down to a temperature of 200 C., or less preferably quenched to room temperature in less than 2 minutes, preferably less than 1 minute.
  • the material is coldrolled with a thickness reduction of at least 20%, then solution-treated in a continuous furnace for less than 1 minute, preferably less than 30 seconds and immediately quenched after leaving the furnace.
  • Such sheets and strips can, at least, be naturally aged or preferably artificially aged.
  • Hot-rolling speeds for the subsequent passes have to be chosen individually in order to take advantage of the heat produced by rolling down the material, to maintain the metal temperature above 350 C., preferably above 400 C.
  • the process of the invention has the advantage of maintaining the homogenized condition of the initial slab or plate during hot rolling and subsequently in the strip leaving the hot mill by a quench.
  • sheets or strips manufactured according to the present invention can pass a homogenization furnace of given length with a speed which is many times greater than that necessary with the common methods. This rise in efiiciency, therefore, correspondingly achieves an economical increase.
  • the procedure according to the invention is especially suitable for the continuous production of strips.
  • the finished products in this case are sheets instead of strips.
  • the rolling slab is soaked for 6 hours at 530 C. (metal temperature). This is followed by hotrolling it down to a thickness of 7 mm., for instance, starting with a metal temperature of 500 C.
  • the plate temperature after hot-rolling was not less than 380 C.
  • the last hot-rolling pass is followed by an immediate quench of the plate in water, the temperature of the plate falling down to 50-80 C.
  • the transit speed is 30 m./minute, i.e. the total heating cycle takes 20 seconds: 10 seconds are used for heating up the metal, Whilst the remaining 10 seconds count as soaking time. For the subsequent quenching, air blast or water .is used. Finally the strip or sheet is aged by reheating the material for 14 hours at a temperature of 160 C.
  • the strip produced in this way has the following mechanical strength properties:
  • Brinell No. (IO/2.5) 101 An aluminum plant is known where the hot-rolled strip is cooled with water spray before coiling. However, cooling the strip at the run-out of the rolling mill in this plant is not done to maintain the homogeneous structure, but to facilitate the handling of the strip only. They do not roll any heat-treatable aluminum alloys at all in this plant, but exclusively pure aluminum and the non-heattreatable aluminum-manganese alloys.
  • Banbury, Oxfordshire, a few years ago did not suggest the use of strip from heat-treatable aluminum alloys immediately quenched after hot-rolling as a basic material for the production of heat-treatable sheet and strip from aluminum alloys by cold-rolling followed by a heat-treatment in a continuous furnace.
  • the present invention therefore is based on a special treatment combination resulting in a distinct increased effect compared with that attainable by common procedures.
  • step (2) the hot-rolling temperature is maintained at not less than 400 C. and in step (3) the quenching is done from a temperature of at least 400 C. down to a temperature below 200 C. in less than 2 minutes.
  • step (3) the quenching is done in order that the temperature of the hot-rolled member falls below 200 C. in less than 1 minute.
  • step (4) The process as described in claim 1, wherein in step (4) the duration of solution-heat-treatment is less than 30 seconds.
  • step (2) the hot-rolling temperature is maintained at not less than 400 C.
  • the quenching of the rot rolled :member is done from the temperature of at least 400 C. down to below 200 C. in less than 1 minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds.
  • step (2) the hot-rolling temperature is maintained at not less than 400 C.
  • the quenching of the hot rolled member is done from a temperature of at least 400 C. down to 5080 C. in less than one minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds.
  • step (2) the hot-rolling temperature is maintained at not less than 400 C.
  • the quenching of the hot rolled member is done from the temperature of at least 400 C. down to room temperature in less than 1 minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Strip Materials And Filament Materials (AREA)
  • Metal Rolling (AREA)

Description

United States Patent ABSTRACT OF THE DISCLOSURE In a process of producing thin material from an initially-rolled member of aluminum alloy with a copper content of less than 1% which material can reach its maximum strength by subsequent simple aging, the immediate and rapid quenching of a hot rolled aluminum alloy from a temperature of 350 C., preferably 400 C., or more down to a maximum of 200 C. in less than two minutes, preferably less than one minute.
The present invention refers to the production of strips and sheets from heat-treatable aluminum alloys, containing less than 1% copper which strips and sheets can reach their maximum strength by subsequent simple aging treatment.
The process of the present invention is especially suitable for aluminum-magnesium-silicon alloys, but is also suitable for aluminum-zinc-magnesium alloys with low magnesium content.
It is to be understood that the designation aluminummagnesium-silicon alloy herein refers to all aluminum alloys with a chemical composition lying between the following limits:
Percent by wt. Magnesium 0.3-1.5 Silicon 0.2-1.6 Copper 1 Aluminum Balance These alloys may contain one or more of the following additions:
Manganese up to 1% Chrome up to 0.4% Iron up to 0.5% Titanium up to 0.2% Zinc up to 0.2% Copper up to 1% The basic metal can be aluminum of commercial purity (i.e. according to ASTN B209) as well as aluminum of high or highest purity (refined aluminum). As a few examples, there could be mentioned AA6011, AA6061 or AA6063 according to the Registration Record of Aluminum Association Alloy Designations and Chemical Composition Limites for Wrought Aluminum Alloys, published by The American Association, 420 Lexington Ave., N.Y., N.Y., 10017.
The aluminum-zinc-magnesium alloys referred to in this invention may contain Percent Zinc 3.5-5 Magnesium 0.5-1.5 Copper 1 Aluminum Balance Furthermore, these alloys may contain additions like manganese, chromium or other elements. Because of their 3,392,062 Patented July 9, 1968 ice relatively low magnesium content compared to materials like e.g. AA7075, AA7079, AA7178 etc. these alloys are designated as low alloyed.
Today, the heat-treating of light metal sheets and strips tends to follow continuous procedures. In other words, continuous annealing furnaces are used for the heat-treatment of rolled metal products. With a given capacity, the length of the heating track is governed by the soaking time of the metal to be heated at the required temperature. From an economic point of view, a short heating track is more desirable since the longer such a heating track is, the more costly it becomes.
The demand for the smallest possible length of heating track in a furnace also depends on technical reasons, because the handling of material in long furnaces is more difiicult, and this leads to increased danger to the surfaces of the heat-treated material and to increased liability of these surfaces becoming damaged. Every possible provision resulting in reducing the soaking time necessary to obtain the required annealing effect is therefore a considerable technical progress.
An important item in the heat-treatment of sheets and strips from heat-treatable aluminum alloys is the solution heat-treatment followed by quenching. To achieve the required mechanical strength values in the end-condition, the product must be subjected to a solution heattreatment long enough to put into solution practically all alloy components producing the hardening effect.
According to the well-known common practice [Y. Bresson and P. Guesne, Rev. Metallurg. (1961), p. 345- 350], cold-rolled sheets or strips of aluminum-1% magnesium-1% silicon alloy with a thickness of 3 mm. and less, have to be soaked in a continuous furnace at solution heat-treatment temperature of (545 C.:l0 C.) for at least 2 minutes before it is quenched. Such a procedure requires a heating chamber of somewhat more than 10 m. in length and with sheets of 3 mm. and less in thickness, the transit speed ranges between 3 and 5 m./ minute. Compared to the speeds normally attainable in coldrolling and hot-rolling, such a transit speed of 5 m./ minute and less is very slow. The diflierence becomes especially unfavorable when handling strips.
The present invention allows a noticeable increase in the transit speed, thus permitting an economic production of sheets and strips in essentially copper-free, heat-treatable aluminnum alloys suitable for artificially aging.
According to the invention, the initial slab or plate has to be homogenized and hot-rolled while still in the warm condition. The hot-rolled strip which should have a temperature of more than 350 C., preferably more than 400 C., then immediately has to be cooled down to a temperature of 200 C., or less preferably quenched to room temperature in less than 2 minutes, preferably less than 1 minute. Subsequently the material is coldrolled with a thickness reduction of at least 20%, then solution-treated in a continuous furnace for less than 1 minute, preferably less than 30 seconds and immediately quenched after leaving the furnace. Such sheets and strips can, at least, be naturally aged or preferably artificially aged.
Hot-rolling speeds for the subsequent passes have to be chosen individually in order to take advantage of the heat produced by rolling down the material, to maintain the metal temperature above 350 C., preferably above 400 C.
The process of the invention has the advantage of maintaining the homogenized condition of the initial slab or plate during hot rolling and subsequently in the strip leaving the hot mill by a quench. This results in the cold-rolled strip with a thickness of 3 mm. or less, preferably between 1.5 and 0.1 mm., needing only a few seconds (e.g. 5-10 seconds) to stay in the continuous furnace in order to become heated up to the homogenizing temperature and to reach that homogeneous condition which offers the same mechanical strength properties normally reached after quenching and naturally aging or artifically aging. In other words, sheets or strips manufactured according to the present invention can pass a homogenization furnace of given length with a speed which is many times greater than that necessary with the common methods. This rise in efiiciency, therefore, correspondingly achieves an economical increase.
The procedure according to the invention is especially suitable for the continuous production of strips. For the use of the material on other continuous manufacturing lines, it is also possible to cut the strips into any required lengths before cold-rolling as Well as after solution treatment. The finished products in this case are sheets instead of strips.
In the following table, the characteristic values of the common methods are compared with those resulting from the procedure of the present invention.
With the Common Method procedure of the present invention Time for the hot-rolled plate 5 to 50 rninutes Less than 2 after cold-rolling (referred to aluminum-1% magnesium- 1% silicon alloy).
It is also possible to coil and store the material quenched after hot-rolling before starting with coldrolling.
The following example illustrates a certain way in which the principle of the invention can be applied, but it is not to be construed as limiting the broader aspects of the invention.
To manufacture an aluminum-1% magnesium-1% silicon alloy, the rolling slab is soaked for 6 hours at 530 C. (metal temperature). This is followed by hotrolling it down to a thickness of 7 mm., for instance, starting with a metal temperature of 500 C. The plate temperature after hot-rolling was not less than 380 C. The last hot-rolling pass is followed by an immediate quench of the plate in water, the temperature of the plate falling down to 50-80 C. Subsequent cold-rolling results in a strip of e.g. 1 mm. in thickness, which then is solution-treated at a temperature of e.=g. 530 C. (metal temperature) in a continuous furnace with a heating track of all together 10 m. in length. The transit speed is 30 m./minute, i.e. the total heating cycle takes 20 seconds: 10 seconds are used for heating up the metal, Whilst the remaining 10 seconds count as soaking time. For the subsequent quenching, air blast or water .is used. Finally the strip or sheet is aged by reheating the material for 14 hours at a temperature of 160 C. The strip produced in this way has the following mechanical strength properties:
Tensile strength p.s.i 46,400 Yield strength p.s.i 40,100 Elongation percent 14.0
Brinell No. (IO/2.5) 101 An aluminum plant is known where the hot-rolled strip is cooled with water spray before coiling. However, cooling the strip at the run-out of the rolling mill in this plant is not done to maintain the homogeneous structure, but to facilitate the handling of the strip only. They do not roll any heat-treatable aluminum alloys at all in this plant, but exclusively pure aluminum and the non-heattreatable aluminum-manganese alloys.
Publications about this plant (for example the leaflet entitled Continuous Strip Mill at Rogerstone, issued by the former called Northern Aluminum Company Ltd.,
Banbury, Oxfordshire, a few years ago) did not suggest the use of strip from heat-treatable aluminum alloys immediately quenched after hot-rolling as a basic material for the production of heat-treatable sheet and strip from aluminum alloys by cold-rolling followed by a heat-treatment in a continuous furnace. The present invention therefore is based on a special treatment combination resulting in a distinct increased effect compared with that attainable by common procedures.
What is claimed is: 1. In a process of producing strip-like material with a thickness of about 3 mm. and less from an initially rolled member made of a heat-treatable aluminum alloy with a copper content of less than 1%, which material can reach its maximum strength by subsequent simple aging, and which process comprises the steps of:
(1) homogenizing'the initially rolled member, (2) hot-rolling the member in homogenized condition, (3) subsequentlycold rolling the member with at least 20% reduction in the thickness (4) subjecting the cold roller material to a solution heat-treatment in a continuous furnace for a period of less than one minute, and
(5) quenching the product after leaving the continuous furnace, the improvement comprising:
maintaining a temperature up from a minimum of 350 C. during hot rolling, and immediately thereafter quenching the hot-rolled member from said temperature down to a maximum of 200 C. in less than 2 minutes.
2. The process as described in claim 1, wherein in step (2) the hot-rolling temperature is maintained at not less than 400 C. and in step (3) the quenching is done from a temperature of at least 400 C. down to a temperature below 200 C. in less than 2 minutes.
3. The process as described in claim 1 wherein in step (3) the quenching is done in order that the temperature of the hot-rolled member falls below 200 C. in less than 1 minute.
4. The process as described in claim 1, wherein in step (4) the duration of solution-heat-treatment is less than 30 seconds.
5. The process as described in claim 1, wherein in step (2) the hot-rolling temperature is maintained at not less than 400 C., the quenching of the rot rolled :member is done from the temperature of at least 400 C. down to below 200 C. in less than 1 minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds. 3
6. The process as described in claim 1, wherein in step (2) the hot-rolling temperature is maintained at not less than 400 C., the quenching of the hot rolled member is done from a temperature of at least 400 C. down to 5080 C. in less than one minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds.
7. The process as described in claim 1, wherein in step (2) the hot-rolling temperature is maintained at not less than 400 C., the quenching of the hot rolled member is done from the temperature of at least 400 C. down to room temperature in less than 1 minute, and in step (4) the duration of the solution-heat-treatment is of less than 30 seconds.
8. The process as described in claim 1, wherein the hot-rolled material in strip form is coiled and stored after quenching and before cold-rolling.
9. The process as described in claim 1, wherein the successive hot-rolling passes are chosen individually and maintained at a level which makes the heat produced by the hot-rolling operation such as to maintain the temperature of the hot-rolled material at a minimum of 350 C.
10. The process as described in claim 1, wherein the successive hot-rolling passes are chosen individually and maintained at a level which makes the heat produced by 'the hot-rolling operation such as to maintain the temperature of the hot-rolled material at a minimum of 400 C.
References Cited UNITED STATES PATENTS 2,887,422 5/1959 Stone et a1 148156 X 3,194,545 7/1965 Smith 143-159 X 3,093,459 6/1963 Sieoel et a1. 14811.5
6 3,264,143 8/1966 Turner 14811.5 3,312,576 4/1967 Palik 14811.5
OTHER REFERENCES Metal Progress, October 1951, pp. 8892.
HYLAND BIZOT, Primary Examiner.
DAVID L. RECK, Examiner.
W. W. STALLARD, H. F. SAITO, Assistant Examiners.
US483345A 1964-08-27 1965-08-27 Process of producing heat-treatable strips and sheets from heat-treatable aluminum alloys with a copper content of less than 1% Expired - Lifetime US3392062A (en)

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CH1124364A CH480883A (en) 1964-08-27 1964-08-27 Process for the production of hardenable strips and sheets from hardenable aluminum alloys with copper contents below 1%

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3542606A (en) * 1968-03-13 1970-11-24 Kaiser Aluminium Chem Corp Hot worked metal article of aluminum base alloy and method of producing same
US3935007A (en) * 1974-11-13 1976-01-27 Sumitomo Light Metal Industries, Ltd. Aluminum alloy of age hardening type
US3990922A (en) * 1975-10-20 1976-11-09 Swiss Aluminium Ltd. Processing aluminum alloys
US4066480A (en) * 1976-08-11 1978-01-03 Swiss Aluminium Ltd. Process for improving the hot workability of aluminum-magnesium alloys
US4066476A (en) * 1976-08-11 1978-01-03 Swiss Aluminium Ltd. Duplex process for improving the hot workability of aluminum-magnesium alloys
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure
US4151013A (en) * 1975-10-22 1979-04-24 Reynolds Metals Company Aluminum-magnesium alloys sheet exhibiting improved properties for forming and method aspects of producing such sheet
US4163665A (en) * 1978-06-19 1979-08-07 Alumax Mill Products, Inc. Aluminum alloy containing manganese and copper and products made therefrom
US4174232A (en) * 1976-12-24 1979-11-13 Swiss Aluminium Ltd. Method of manufacturing sheets, strips and foils from age hardenable aluminum alloys of the Al-Si-Mg-type
JPS61201749A (en) * 1985-03-05 1986-09-06 Sukai Alum Kk Rolled aluminum alloy sheet for forming and its manufacture
US4614552A (en) * 1983-10-06 1986-09-30 Alcan International Limited Aluminum alloy sheet product
US4808247A (en) * 1986-02-21 1989-02-28 Sky Aluminium Co., Ltd. Production process for aluminum-alloy rolled sheet
US6110297A (en) * 1997-01-10 2000-08-29 Honda Giken Kogyo Kabushiki Kaisha Aluminum alloy sheet with excellent formability and method for manufacture thereof
EP1375691A1 (en) * 2001-03-28 2004-01-02 Sumitomo Light Metal Industries, Ltd. Aluminum alloy sheet excellent in formability and hardenability during baking of coating and method for production thereof
CN100415917C (en) * 2001-03-28 2008-09-03 住友轻金属工业株式会社 Aluminum alloy sheet excellent in formability and hardenability during baking of coating and method for production thereof
WO2011000635A1 (en) 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
CN101550509B (en) * 2008-03-31 2012-07-11 株式会社神户制钢所 Aluminum alloy sheet superior in paint baking hardenability and invulnerable to room temperature aging, and method for production thereof
EP3060358B1 (en) 2013-10-25 2017-11-15 SMS group GmbH Aluminum hot strip rolling train and method for hot rolling an aluminum hot strip

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US4164434A (en) * 1977-11-02 1979-08-14 Swiss Aluminium Ltd. Aluminum alloy capacitor foil and method of making
US4166755A (en) * 1977-11-02 1979-09-04 Swiss Aluminium Ltd. Aluminum alloy capacitor foil and method of making
CA2091355A1 (en) * 1990-08-22 1992-02-23 James Christopher Mohr Aluminium alloy suitable for can making
EP2614170A4 (en) 2010-09-08 2015-10-14 Alcoa Inc Improved 7xxx aluminum alloys, and methods for producing the same
WO2013172910A2 (en) 2012-03-07 2013-11-21 Alcoa Inc. Improved 2xxx aluminum alloys, and methods for producing the same
US9587298B2 (en) 2013-02-19 2017-03-07 Arconic Inc. Heat treatable aluminum alloys having magnesium and zinc and methods for producing the same

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US2887422A (en) * 1950-02-25 1959-05-19 United Eng Foundry Co Method of continuously heat treating aluminum strip
US3093459A (en) * 1958-08-02 1963-06-11 Aluminium Ind Ag Method for manufacturing highly polishable sheets of aluminum
US3194545A (en) * 1960-03-17 1965-07-13 Kaiser Aluminium Chem Corp Apparatus for continuously solution heat-treating aluminum and its alloys
US3264143A (en) * 1962-07-16 1966-08-02 Selas Corp Of America Heat treating strip material
US3312576A (en) * 1963-07-03 1967-04-04 Reynolds Metals Co Method of treating metal

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Publication number Priority date Publication date Assignee Title
US2887422A (en) * 1950-02-25 1959-05-19 United Eng Foundry Co Method of continuously heat treating aluminum strip
US3093459A (en) * 1958-08-02 1963-06-11 Aluminium Ind Ag Method for manufacturing highly polishable sheets of aluminum
US3194545A (en) * 1960-03-17 1965-07-13 Kaiser Aluminium Chem Corp Apparatus for continuously solution heat-treating aluminum and its alloys
US3264143A (en) * 1962-07-16 1966-08-02 Selas Corp Of America Heat treating strip material
US3312576A (en) * 1963-07-03 1967-04-04 Reynolds Metals Co Method of treating metal

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3542606A (en) * 1968-03-13 1970-11-24 Kaiser Aluminium Chem Corp Hot worked metal article of aluminum base alloy and method of producing same
US3935007A (en) * 1974-11-13 1976-01-27 Sumitomo Light Metal Industries, Ltd. Aluminum alloy of age hardening type
US3990922A (en) * 1975-10-20 1976-11-09 Swiss Aluminium Ltd. Processing aluminum alloys
US4151013A (en) * 1975-10-22 1979-04-24 Reynolds Metals Company Aluminum-magnesium alloys sheet exhibiting improved properties for forming and method aspects of producing such sheet
JPS5319117A (en) * 1976-08-05 1978-02-22 Aluminum Co Of America Modified aluminium structure
JPS5939499B2 (en) * 1976-08-05 1984-09-25 アルミナム・カンパニ−・オブ・アメリカ Manufacturing method for structural components for vehicles
US4066480A (en) * 1976-08-11 1978-01-03 Swiss Aluminium Ltd. Process for improving the hot workability of aluminum-magnesium alloys
US4066476A (en) * 1976-08-11 1978-01-03 Swiss Aluminium Ltd. Duplex process for improving the hot workability of aluminum-magnesium alloys
US4174232A (en) * 1976-12-24 1979-11-13 Swiss Aluminium Ltd. Method of manufacturing sheets, strips and foils from age hardenable aluminum alloys of the Al-Si-Mg-type
US4163665A (en) * 1978-06-19 1979-08-07 Alumax Mill Products, Inc. Aluminum alloy containing manganese and copper and products made therefrom
US4614552A (en) * 1983-10-06 1986-09-30 Alcan International Limited Aluminum alloy sheet product
JPS61201749A (en) * 1985-03-05 1986-09-06 Sukai Alum Kk Rolled aluminum alloy sheet for forming and its manufacture
US4808247A (en) * 1986-02-21 1989-02-28 Sky Aluminium Co., Ltd. Production process for aluminum-alloy rolled sheet
US6110297A (en) * 1997-01-10 2000-08-29 Honda Giken Kogyo Kabushiki Kaisha Aluminum alloy sheet with excellent formability and method for manufacture thereof
KR100870164B1 (en) * 2001-03-28 2008-11-25 스미토모 게이 긴조쿠 고교 가부시키가이샤 Aluminum alloy sheet with excellent formability and paint bake hardenability
EP1375691A4 (en) * 2001-03-28 2004-07-21 Sumitomo Light Metal Ind Aluminum alloy sheet excellent in formability and hardenability during baking of coating and method for production thereof
KR100833145B1 (en) * 2001-03-28 2008-05-29 스미토모 게이 긴조쿠 고교 가부시키가이샤 Method for producing aluminum alloy sheet with excellent bendability and paint bake hardenability
CN100415917C (en) * 2001-03-28 2008-09-03 住友轻金属工业株式会社 Aluminum alloy sheet excellent in formability and hardenability during baking of coating and method for production thereof
KR100861036B1 (en) * 2001-03-28 2008-10-01 스미토모 게이 긴조쿠 고교 가부시키가이샤 Aluminum alloy sheet with excellent formability and paint bake hardenability
EP1375691A1 (en) * 2001-03-28 2004-01-02 Sumitomo Light Metal Industries, Ltd. Aluminum alloy sheet excellent in formability and hardenability during baking of coating and method for production thereof
CN101550509B (en) * 2008-03-31 2012-07-11 株式会社神户制钢所 Aluminum alloy sheet superior in paint baking hardenability and invulnerable to room temperature aging, and method for production thereof
WO2011000635A1 (en) 2009-06-30 2011-01-06 Hydro Aluminium Deutschland Gmbh Almgsi strip for applications having high plasticity requirements
US10047422B2 (en) 2009-06-30 2018-08-14 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
EP2449145B1 (en) * 2009-06-30 2019-08-07 Hydro Aluminium Rolled Products GmbH AlMgSi-sheet for applications with high shaping requirements
US10612115B2 (en) 2009-06-30 2020-04-07 Hydro Aluminium Deutschland Gmbh AlMgSi strip for applications having high formability requirements
EP2270249B2 (en) 2009-06-30 2020-05-27 Hydro Aluminium Deutschland GmbH AlMgSi-sheet for applications with high shaping requirements
EP3060358B1 (en) 2013-10-25 2017-11-15 SMS group GmbH Aluminum hot strip rolling train and method for hot rolling an aluminum hot strip

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NL6511155A (en) 1966-02-28
DE1279940B (en) 1968-10-10
GB1055687A (en) 1967-01-18
CH480883A (en) 1969-11-15

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