US3502448A - Aluminum alloy sheet - Google Patents
Aluminum alloy sheet Download PDFInfo
- Publication number
- US3502448A US3502448A US688740A US3502448DA US3502448A US 3502448 A US3502448 A US 3502448A US 688740 A US688740 A US 688740A US 3502448D A US3502448D A US 3502448DA US 3502448 A US3502448 A US 3502448A
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- sheet
- strength
- aluminum alloy
- inch
- alloy sheet
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- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
Definitions
- the extra hard temper is achieved by cold rolling to effect a reduction in thickness of at least 85% BACKGROUND OF THE INVENTION
- aluminum alloy sheet has found increasing acceptance in applications involving its use as an end on a can, or the like, for beverages, food and other goods.
- These can ends usually include some sort of easy open feature such as the integral drawn rivet pull tab feature described in U.S. Patent 3,191,797.
- This type of feature is one of the prime reasons for the increasingly widespread use of aluminumsheet in can ends but also creates certain problems in selecting a ⁇ suitable material.
- the can end must have suicient strength to safely contain the material within the can, and this strength must be retained after exposures to the baking temperatures employed in curing the coatings applied to the can ends.
- the material must be suiciently workable to be fashioned into an integral rivet easy open type can end.
- U.S. Patent 3,191,797 it becomes immediately apparent that a can end is subjected to a rather substantial deformation in forming the integral rivet employed to secure the easy open tab to the can end.
- several aluminum alloy sheet compositions might have suiicient strength before andl after any -baking operations, many lack the required formability.
- Work hardened aluminum-magnesium-manganese alloy sheet as provided herein has a thickness of 0.008 to 0.017 inch and is composed of an alloy consisting essentially of 4 to 5.5% magnesium, 0.2 to 0.7% manganese, the balance being aluminum and incidental elements and impurities.
- the maximum amounts of impurities in the alloy are as follows: 0.2% copper, 0.4% iron, 0.3% silicon, 0.1% titanium, 0.2% chromium, all other impurities being limited to 0.05% each and a total of 0.15%. It is 3,502,448 Patented Mar. 24, 1970 ICC Percent Mur-1.700 0.9 (1n percent Mg) i0.15%
- the sheet For the sheet to perform as desired, it is essential that it be in the state resulting from a cold rolling reduction of at least of the thickness of material in the recrystallized state to provide an extra hard internal structure.
- the sheet Iin this state exhibits tensile and yield strengths of, respectively, 57,000 p.s.i. and 53,000 p.s.i., an elongation, 2 inches, of 3% or more together with an Olsen cupping value of 0.14 inch.
- the sheet l is characterized by tensile and yieldvstrengths olf, respectively, 53,000 and 45,000 p.s.i., an elongation of 8 and an Olsen cupping value of 0.16 inch.
- composition limits mentioned in the preceding paragraph must be closely followed in order to achieve the combination of strength and workability required which characterizes the improved sheet.
- the formability falls below that at which integral rivet easy open can ends can be consistently manufactured on a commercial scale. If it falls below that established by the equation, the strength is decreased below the level contemplated by the invention.
- the alloy composition as set forth herein may be provided as a continuous cast ingot.
- the ingot may be homogenized by heating for about 24 hours at a temperature of at least 800 F. but below the melting point.
- the ingot is then prepared for rolling and hot rolled to some intermediate thickness, usually about 0.15 inch, according to conventional hot rolling practice and may then be annealed by heating to about 600 F. -for a period of time ysuicient to recrystallize the internal structure.
- this material iscold rolled to effect a reduction in thickness of at least 85%, and preferably 90% or more to provide sheet ranging in thickness, 0.008 to 0.015 inch.
- the temperature of the sheet as it leaves the rolls not exceed 200 F.
- the pressure deflection characteristic In addition to standard tensile tests, another measure of the strength capacity of a sheet to serve as a can end is the pressure deflection characteristic. This characteristic is determined by providing a beverage can with its end fashioned from the sheet being tested. Pressure is applied within the can and gradually increased until the can end buckles and plastically deforms. The pressureat which the can end buckles is then designated as the buckle pressure. In bucklingl tests comparing sheets A and B, it has been found that 0.0135 inch thick can ends of sheet A withstand the same pressure as 0.0145 inch thick can ends of sheet B, which is the sheet currently employed widely in easy open beer can ends. This represents a rather signi'iicant savings in material.
- the improved sheet provides a useful new material for use in integral rivet easy open type can ends. It demonstrates a clear improvement in combining workability and strength such that such can ends can now be fashioned from a substantially thinner sheet gauge.
- the balance being aluminum and impurities, the maximum amounts of said impurities being as follows: 0.2% copper, 0.4% iron, 0.3% silicon, 0.1% titanium, 0.2% chromium, all other impurities being limited to 0.05% each and a total of 0.15%, said sheet being characterized in said extra hard condition by a tensile strength of 57,000 p.s.i., a yield strength of 53,000 p.s.i. and an elongation, in 2 inches of 3%, together with an Olsen cupping value of 0.14 inch and further characterized after an exposure of -up to 20 minutes to a temperature of up to 400 F. by a tensile strength of 53,000 p.s.i., a yield strength of 45,000 p.s.i., an elongation of 8% and an Olsen cupping value of 0.16 inch.
- the sheet in accordance with claim 1 which has received a cold reduction of at least 3.
- the sheet in accordance with claim 1 which contains 4.2 to 4.8% magnesium and 0.25 to 0.5% manganese.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Metal Rolling (AREA)
- Closures For Containers (AREA)
- Containers Opened By Tearing Frangible Portions (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Heat Treatment Of Steel (AREA)
Description
March 24, 1970 w. A. ANDERSON ET AL 3,502,448
ALUMINUM ALLOY SHEET Filed Dec. 7, 1967 l I l 48 52 56 Tf/VS/E 57556/6737'- 77/00071/3'10 PSL United States Patent O M 3,502,448 ALUMINUM ALLOY SHEET William A. Anderson, Pittsburgh, and John K. McBride,
New Kensington, Pa., assigiors to Aluminum Company of America, Pittsburgh, Pa., a corporation of Pennsylvania l Filed Dec. 7, 1967, Ser. No. 688,740 Int. Cl. B21b 3/00 U.S. Cl. 29-183.5 4 Claims ABSTRACT OF THE DISCLOSURE Work hardened aluminum alloy sheet, 0.008 to 0.017 inch thick, in the extra hard temper and containing 4 to 5.5% magnesium, 0.2 to 0.7% manganese, the balance being essentially aluminum, possesses a combination of strength and formability which make it especially useful for aluminum can ends. To achieve such, the manganese content is related to the magnesium content according to the following relation:
Percent Mn: 1.700 0.9 (ln percent Mg) 10.15%
The extra hard temper is achieved by cold rolling to effect a reduction in thickness of at least 85% BACKGROUND OF THE INVENTION In recent years aluminum alloy sheet has found increasing acceptance in applications involving its use as an end on a can, or the like, for beverages, food and other goods. These can ends usually include some sort of easy open feature such as the integral drawn rivet pull tab feature described in U.S. Patent 3,191,797. This type of feature is one of the prime reasons for the increasingly widespread use of aluminumsheet in can ends but also creates certain problems in selecting a `suitable material. First, the can end must have suicient strength to safely contain the material within the can, and this strength must be retained after exposures to the baking temperatures employed in curing the coatings applied to the can ends. Second, the material must be suiciently workable to be fashioned into an integral rivet easy open type can end. For instance, referring to the above-mentioned U.S. Patent 3,191,797, it becomes immediately apparent that a can end is subjected to a rather substantial deformation in forming the integral rivet employed to secure the easy open tab to the can end. While several aluminum alloy sheet compositions might have suiicient strength before andl after any -baking operations, many lack the required formability. Conversely, While some have the required formability, they often exhibit a strength level `so low as to require an economically excessive thickness to provide a suiciently strong can end. It is generally desired to maintain a rejection level of not more than ve failures in 10,000 easy open can end rivet forming operations. This is a rather severe formability requirement for the can end material which also must be strong enough to be of sufficiently thin gauge to economically compete with other material-s.
STATEMENT OF THE INVENTION Work hardened aluminum-magnesium-manganese alloy sheet as provided herein has a thickness of 0.008 to 0.017 inch and is composed of an alloy consisting essentially of 4 to 5.5% magnesium, 0.2 to 0.7% manganese, the balance being aluminum and incidental elements and impurities. The maximum amounts of impurities in the alloy are as follows: 0.2% copper, 0.4% iron, 0.3% silicon, 0.1% titanium, 0.2% chromium, all other impurities being limited to 0.05% each and a total of 0.15%. It is 3,502,448 Patented Mar. 24, 1970 ICC Percent Mur-1.700 0.9 (1n percent Mg) i0.15%
For the sheet to perform as desired, it is essential that it be in the state resulting from a cold rolling reduction of at least of the thickness of material in the recrystallized state to provide an extra hard internal structure. The sheet Iin this state exhibits tensile and yield strengths of, respectively, 57,000 p.s.i. and 53,000 p.s.i., an elongation, 2 inches, of 3% or more together with an Olsen cupping value of 0.14 inch. Further, after an exposure of 20 minutes to a baking oven temperature of 400 F., the sheet lis characterized by tensile and yieldvstrengths olf, respectively, 53,000 and 45,000 p.s.i., an elongation of 8 and an Olsen cupping value of 0.16 inch.
DETAILED DESCRIPTION A further understanding of the invention will proceed from this detailed description and from the drawing which is a plot demonstrating the improved strength and workability of the improved alloy.
The composition limits mentioned in the preceding paragraph must be closely followed in order to achieve the combination of strength and workability required which characterizes the improved sheet.
If the manganese content exceeds that established by the equation, the formability falls below that at which integral rivet easy open can ends can be consistently manufactured on a commercial scale. If it falls below that established by the equation, the strength is decreased below the level contemplated by the invention.
The alloy composition as set forth herein may be provided as a continuous cast ingot. The ingot may be homogenized by heating for about 24 hours at a temperature of at least 800 F. but below the melting point. The ingot is then prepared for rolling and hot rolled to some intermediate thickness, usually about 0.15 inch, according to conventional hot rolling practice and may then be annealed by heating to about 600 F. -for a period of time ysuicient to recrystallize the internal structure. Next, this material iscold rolled to effect a reduction in thickness of at least 85%, and preferably 90% or more to provide sheet ranging in thickness, 0.008 to 0.015 inch. In performing the cold reduction it is preferred that the temperature of the sheet as it leaves the rolls not exceed 200 F. The use of water base lubricants is helpful in maintaining this temperature level. This cold reduction imparts to the sheet and extremely hard temper. While the sheet in this temper is characterized by a high degree of strength, it also exhibits a very good degree of Iformability such that integral rivets can be drawn as shown in the various patents, such as U.S. 3,191,797, covering this type of easy open feature. It is also highly significant that sufficient strength is retained after a thermal exposure comparable to that encountered in the production of can ends where a coating is applied to the sheet and baked. A thermal exposure of 400 F. for 20 minutes is a conservative approximation of the more severe baking treat-l TABLE I Sheet Mg Mn Fe Si Cu Cr Ti Zu A 4. 54 0. 37 O. 21 0. 10 0. 01 0. 02 0. 02 0. 01 B 4. 45 0. 01 0. 19 0. 08 0. 02 0. 00 0. 01 0. 0l
Each alloy was continuously cast to provide an ingot which was homogenized by heating for 24 hours at a temperature of 900 F. after which it was brought to a temperature of about 750 F. and then hot rolled to provide plate approximately `0.15 inch thick. This plate was then annealed at 600 F. to recrystallize the grain structure after which it was cold rolled without any intermediate annealing to sheet 0.013 inch thick. This cold reduction of over 90% imparted to the sheet an extremely cold hard temper. Tensile test specimens were removed from the sheet and, on testing, indicated the average tensile data set forth in Table II. Also included in the Table is an Olsen cupping value which is a measure of the formability of the sheet. This test is Widely recognized in the industry and is described in the Procedings of ASTM 20, Part II, p. 398, 1920.
It can be seen in Table II that the improved sheet exhibits a significant improvement in strength, about over sheet B although the latter demonstrates a higher Olsen cupping value.
Additional samples of sheets A and B were exposed to a temperature of 400 F. for 20 minutes, an approximation of the conditions encountered by the sheet when an organic coating is applied thereto and cured in a baking oven. It is after such an exposure that the properties of the sheet are of great importance since these are the properties which will be exhibited by the sheet when provided as a can end. The average properties, strength and Olsen cuppng, for sheets A and B after the thermal exposure, are listed in Table III.
TABLE III Tensile Yield Elongation strength, strength, in 2 inches, Olsen eupping Sheet p.s.1. p.s.i. percent value level of strength, the improved sheet, sheet A, is characterized by a significantly higher Olsen cupping value than sheet B.
In addition to standard tensile tests, another measure of the strength capacity of a sheet to serve as a can end is the pressure deflection characteristic. This characteristic is determined by providing a beverage can with its end fashioned from the sheet being tested. Pressure is applied within the can and gradually increased until the can end buckles and plastically deforms. The pressureat which the can end buckles is then designated as the buckle pressure. In bucklingl tests comparing sheets A and B, it has been found that 0.0135 inch thick can ends of sheet A withstand the same pressure as 0.0145 inch thick can ends of sheet B, which is the sheet currently employed widely in easy open beer can ends. This represents a rather signi'iicant savings in material.
From the foregoing it is apparent that the improved sheet provides a useful new material for use in integral rivet easy open type can ends. It demonstrates a clear improvement in combining workability and strength such that such can ends can now be fashioned from a substantially thinner sheet gauge.
What is claimed is:
1. A Work hardened aluminum-magnesium-manganese alloy sheet of 0.008 to 0.017 inch in thickness that has received a reduction in thickness of at least by cold rolling to provide an extra hard internal structure, said aluminum alloy consisting essentially of 4 to 5.5% magnesium, 0.2 to `0.7% manganese, the manganese content being related to the magnesium content in accordance with the following:
percent Mn=l.700-0.9 (ln percent Mg) i0.15%
the balance being aluminum and impurities, the maximum amounts of said impurities being as follows: 0.2% copper, 0.4% iron, 0.3% silicon, 0.1% titanium, 0.2% chromium, all other impurities being limited to 0.05% each and a total of 0.15%, said sheet being characterized in said extra hard condition by a tensile strength of 57,000 p.s.i., a yield strength of 53,000 p.s.i. and an elongation, in 2 inches of 3%, together with an Olsen cupping value of 0.14 inch and further characterized after an exposure of -up to 20 minutes to a temperature of up to 400 F. by a tensile strength of 53,000 p.s.i., a yield strength of 45,000 p.s.i., an elongation of 8% and an Olsen cupping value of 0.16 inch.
2. The sheet in accordance with claim 1 which has received a cold reduction of at least 3. The sheet in accordance with claim 1 which contains 4.2 to 4.8% magnesium and 0.25 to 0.5% manganese.
4. The sheet in accordance with claim 1 in the state resulting from a thermal exposure.
References Cited UNITED STATES PATENTS RICHARD O. DEAN, Primary Examiner U.S. Cl. X.R.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US68874067A | 1967-12-07 | 1967-12-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3502448A true US3502448A (en) | 1970-03-24 |
Family
ID=24765577
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US688740A Expired - Lifetime US3502448A (en) | 1967-12-07 | 1967-12-07 | Aluminum alloy sheet |
Country Status (5)
Country | Link |
---|---|
US (1) | US3502448A (en) |
JP (1) | JPS5248088B1 (en) |
DE (1) | DE1813192B2 (en) |
GB (1) | GB1214370A (en) |
NL (1) | NL6817578A (en) |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3661657A (en) * | 1970-12-07 | 1972-05-09 | Kaiser Aluminium Chem Corp | Method for making aluminum sheet |
US3691972A (en) * | 1970-07-09 | 1972-09-19 | Reynolds Metals Co | Aluminous metal articles and method |
US3857973A (en) * | 1971-03-12 | 1974-12-31 | Aluminum Co Of America | Aluminum alloy container end and sealed container thereof |
US3963143A (en) * | 1975-06-30 | 1976-06-15 | Aluminum Company Of America | Container including an aluminum panel having a portion removable by tearing |
US4035201A (en) * | 1975-06-30 | 1977-07-12 | Aluminum Company Of America | Method of making a container including an aluminum panel having a portion removable by tearing |
US4043840A (en) * | 1976-07-09 | 1977-08-23 | Swiss Aluminium Ltd. | Aluminum alloys possessing improved resistance weldability |
US4111721A (en) * | 1976-06-14 | 1978-09-05 | American Can Company | Strip cast aluminum heat treatment |
US4269632A (en) * | 1978-08-04 | 1981-05-26 | Coors Container Company | Fabrication of aluminum alloy sheet from scrap aluminum for container components |
US4284437A (en) * | 1979-12-18 | 1981-08-18 | Sumitomo Light Metal Industries, Ltd. | Process for preparing hard tempered aluminum alloy sheet |
US4469537A (en) * | 1983-06-27 | 1984-09-04 | Reynolds Metals Company | Aluminum armor plate system |
US4582541A (en) * | 1982-12-16 | 1986-04-15 | Swiss Aluminium Ltd. | Process for producing strip suitable for can lid manufacture |
US4626294A (en) * | 1985-05-28 | 1986-12-02 | Aluminum Company Of America | Lightweight armor plate and method |
WO1996026299A1 (en) * | 1995-02-24 | 1996-08-29 | Pechiney Rhenalu | PRODUCT FOR OBTAINING WELDED AlMgMn ALLOY STRUCTURES WITH IMPROVED MECHANICAL RESISTANCE |
FR2731018A1 (en) * | 1995-02-24 | 1996-08-30 | Pechiney Rhenalu | Rolled or extruded aluminium@ alloy sections suitable for welding |
EP0769564A1 (en) * | 1995-10-18 | 1997-04-23 | Pechiney Rhenalu | Aluminium-magnesium alloys for welded structures with improved mechanical properties |
US5908518A (en) * | 1996-08-06 | 1999-06-01 | Pechiney Rhenalu | AlMgMn alloy product for welded construction with improved corrosion resistance |
CN1051945C (en) * | 1992-12-28 | 2000-05-03 | 凯泽铝和化学公司 | Method of manufacturing can body sheet using two sequences of continuous, in-line operations |
US6102102A (en) * | 1992-06-23 | 2000-08-15 | Kaiser Aluminum & Chemical Corporation | Method and apparatus for continuous casting of metals |
US6238495B1 (en) | 1996-04-04 | 2001-05-29 | Corus Aluminium Walzprodukte Gmbh | Aluminium-magnesium alloy plate or extrusion |
US6485682B1 (en) * | 2000-11-06 | 2002-11-26 | Dieter Backhaus | Hardened aluminum alloy for use in the manufacture of printed circuit boards |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0267793U (en) * | 1988-11-07 | 1990-05-22 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2601206A (en) * | 1948-10-22 | 1952-06-17 | Reynolds Metals Co | Medium-strength corrosion-resistant aluminum alloys |
US3187428A (en) * | 1960-10-19 | 1965-06-08 | Reynolds Metals Co | Method of treating aluminum and aluminum alloys preparatory to bright finishing |
-
1967
- 1967-12-07 US US688740A patent/US3502448A/en not_active Expired - Lifetime
-
1968
- 1968-12-04 GB GB57684/68A patent/GB1214370A/en not_active Expired
- 1968-12-06 NL NL6817578A patent/NL6817578A/xx unknown
- 1968-12-06 DE DE1813192A patent/DE1813192B2/en not_active Ceased
- 1968-12-07 JP JP43089882A patent/JPS5248088B1/ja active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2601206A (en) * | 1948-10-22 | 1952-06-17 | Reynolds Metals Co | Medium-strength corrosion-resistant aluminum alloys |
US3187428A (en) * | 1960-10-19 | 1965-06-08 | Reynolds Metals Co | Method of treating aluminum and aluminum alloys preparatory to bright finishing |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3691972A (en) * | 1970-07-09 | 1972-09-19 | Reynolds Metals Co | Aluminous metal articles and method |
US3661657A (en) * | 1970-12-07 | 1972-05-09 | Kaiser Aluminium Chem Corp | Method for making aluminum sheet |
US3857973A (en) * | 1971-03-12 | 1974-12-31 | Aluminum Co Of America | Aluminum alloy container end and sealed container thereof |
US3963143A (en) * | 1975-06-30 | 1976-06-15 | Aluminum Company Of America | Container including an aluminum panel having a portion removable by tearing |
US4035201A (en) * | 1975-06-30 | 1977-07-12 | Aluminum Company Of America | Method of making a container including an aluminum panel having a portion removable by tearing |
US4111721A (en) * | 1976-06-14 | 1978-09-05 | American Can Company | Strip cast aluminum heat treatment |
US4043840A (en) * | 1976-07-09 | 1977-08-23 | Swiss Aluminium Ltd. | Aluminum alloys possessing improved resistance weldability |
US4269632A (en) * | 1978-08-04 | 1981-05-26 | Coors Container Company | Fabrication of aluminum alloy sheet from scrap aluminum for container components |
US4284437A (en) * | 1979-12-18 | 1981-08-18 | Sumitomo Light Metal Industries, Ltd. | Process for preparing hard tempered aluminum alloy sheet |
US4582541A (en) * | 1982-12-16 | 1986-04-15 | Swiss Aluminium Ltd. | Process for producing strip suitable for can lid manufacture |
US4469537A (en) * | 1983-06-27 | 1984-09-04 | Reynolds Metals Company | Aluminum armor plate system |
US4626294A (en) * | 1985-05-28 | 1986-12-02 | Aluminum Company Of America | Lightweight armor plate and method |
US6102102A (en) * | 1992-06-23 | 2000-08-15 | Kaiser Aluminum & Chemical Corporation | Method and apparatus for continuous casting of metals |
CN1051945C (en) * | 1992-12-28 | 2000-05-03 | 凯泽铝和化学公司 | Method of manufacturing can body sheet using two sequences of continuous, in-line operations |
WO1996026299A1 (en) * | 1995-02-24 | 1996-08-29 | Pechiney Rhenalu | PRODUCT FOR OBTAINING WELDED AlMgMn ALLOY STRUCTURES WITH IMPROVED MECHANICAL RESISTANCE |
FR2731018A1 (en) * | 1995-02-24 | 1996-08-30 | Pechiney Rhenalu | Rolled or extruded aluminium@ alloy sections suitable for welding |
EP0769564A1 (en) * | 1995-10-18 | 1997-04-23 | Pechiney Rhenalu | Aluminium-magnesium alloys for welded structures with improved mechanical properties |
FR2740144A1 (en) * | 1995-10-18 | 1997-04-25 | Pechiney Rhenalu | ALMG ALLOY FOR WELDED CONSTRUCTIONS WITH IMPROVED MECHANICAL CHARACTERISTICS |
EP1178125A3 (en) * | 1995-10-18 | 2009-04-01 | Alcan Rhenalu | AlMg alloy with improved mechanical properties for welded constructions |
US6238495B1 (en) | 1996-04-04 | 2001-05-29 | Corus Aluminium Walzprodukte Gmbh | Aluminium-magnesium alloy plate or extrusion |
US6342113B2 (en) | 1996-04-04 | 2002-01-29 | Corus Aluminium Walzprodukte Gmbh | Aluminum-magnesium alloy plate or extrusion |
US5908518A (en) * | 1996-08-06 | 1999-06-01 | Pechiney Rhenalu | AlMgMn alloy product for welded construction with improved corrosion resistance |
US6485682B1 (en) * | 2000-11-06 | 2002-11-26 | Dieter Backhaus | Hardened aluminum alloy for use in the manufacture of printed circuit boards |
Also Published As
Publication number | Publication date |
---|---|
JPS5248088B1 (en) | 1977-12-07 |
NL6817578A (en) | 1969-06-10 |
DE1813192B2 (en) | 1973-11-15 |
GB1214370A (en) | 1970-12-02 |
DE1813192A1 (en) | 1971-02-11 |
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