US3502448A - Aluminum alloy sheet - Google Patents

Aluminum alloy sheet Download PDF

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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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William A Anderson
John K Mcbride
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Howmet Aerospace Inc
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Aluminum Company of America
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    • 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/923Physical 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.

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  • 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.
US688740A 1967-12-07 1967-12-07 Aluminum alloy sheet Expired - Lifetime US3502448A (en)

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Cited By (20)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0267793U (en) * 1988-11-07 1990-05-22

Citations (2)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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JPS5248088B1 (en) 1977-12-07
NL6817578A (en) 1969-06-10
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GB1214370A (en) 1970-12-02
DE1813192A1 (en) 1971-02-11

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