US3594133A - Aluminum alloy - Google Patents

Aluminum alloy Download PDF

Info

Publication number
US3594133A
US3594133A US680323A US3594133DA US3594133A US 3594133 A US3594133 A US 3594133A US 680323 A US680323 A US 680323A US 3594133D A US3594133D A US 3594133DA US 3594133 A US3594133 A US 3594133A
Authority
US
United States
Prior art keywords
amount
max
weight
zinc
copper
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US680323A
Inventor
Jacques F Cote
William Ernest Cooke
Roy C Spooner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Alcan Research and Development Ltd
Original Assignee
Alcan Research and Development Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alcan Research and Development Ltd filed Critical Alcan Research and Development Ltd
Application granted granted Critical
Publication of US3594133A publication Critical patent/US3594133A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12993Surface feature [e.g., rough, mirror]

Definitions

  • An aluminum base alloy capable of receiving an a1ka line etch treatment to produce a uniform mat finish contains silicon in an amount in the range 0.2-0.6%, iron in the amount 0.35% max., manganese in the amount 0.10% max., magnesium in an amount in the range 0.450.9%, chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in the amount in the range 0.030.25% and copper in an amount in the weight ratio 1:1 to 2:1 on a Cu-Zn weight basis ratio, others each in the amount 0.05% max., said others total in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percent by weight.
  • the copper when the zinc content is in the range 0.100.25% the copper should be present in an amount in the weight ratio 2:1 on a Cu-Zn weight basis ratio and, also, in the above alloys when zinc is present in an amount in the range 0.030.10% the copper should be present in an amount in the Weight ratio 1:1 on a Cu-Zn weight basis ratio.
  • This invention relates to aluminum alloys. More particularly, this invention relates to aluminum alloys capable of being extruded in a wide variety of forms or shapes and having utility in the architectural and other fields. More particularly this invention relates to aluminum alloys of the type known as AA6063.
  • Aluminum alloys of the type No. 6063 have the com position in percents by Weight Si 0.20-0.6, Fe 0.35 max., Mn 0.10 max., Mg 0.45;0.9, Cr 0.10 max., Ti 0.10 max., Zn 0.10 max., Cu 0.10 max., others, each 0.05 max. and said others, total 0.15 max., the remainder being aluminum.
  • zinc-containing aluminum alloys particularly aluminum alloys of the type No. 6063 having a zinc content greater than 0.03% by weight
  • a uniform etch finish such as a uniform mat finish
  • copper when the zinc content of such alloys is present in an amount in the range 0.030.10% copper should be present in the alloy in the Weight ratio 1:1 on a Cu-Zn Weight basis ratio so that when the alloy is subjected to an alkaline etch treatment, such as by contact with a sodium hydroxide-containing solution or its equivalent, the resulting etched alloy receives a uniform mat finish.
  • an aluminum alloy of the type No. 6063 contains a zinc content in the range 0.030.10% there should also be included copper in an amount substantially the same as or the same as the zinc content on a Cu-Zn weight basis ratio of 1:1.
  • the zinc content of such alloys is 0.05% by Weight
  • the copper content of such alloys should be 0.05% by weight also so that such alloy can be subjected to an alkaline etch treatment to yield a uniform mat finish.
  • the zinc content of such alloys is in the amount 0.10% by weight, the copper content of such alloy should be 0.10%.
  • the amount of copper in such alloys should :be twice the zinc content such that the weight basis ratio CuzZn is 2:1.
  • the copper content of such alloy should be 0.30% by weight so that when the alloy is subjected to an alkaline etch treatment the resulting etched alloy receives a uni-form mat finish.
  • the copper content of the alloys should be 0.50% by weight so that the alloy when subjected to an alkaline etch treatment will receive a uniform mat finish.
  • EXAMPLE 1 When an aluminum alloy having the composition in the following percents by weight, Fe 0.17, Mg 0.51, Mn 0.1, Si 0.46, Ti 0.01, Zn 0.088 and Cu 0.01, the remainder being aluminum, was etched with a standard etching solution (50 g./l. Diversey Aluminux, a proprietary caustic etchant solution, plus 0.2 g./l. of dissolved alluminum) at 65 C. for 2, 5 and 10 minutes,
  • the resulting etched aluminum alloy showed a pronounced grainy appearance indicating a pronounced preferential grain type of attack during etching.
  • the copper content was much less than the zinc content with the result that a satisfactory etch finish was not obtained.
  • EXAMPLE 2 Aluminum alloys of type No. 6063 containing various level combinations of zinc and copper content were etched in a solution of 50 g./l. of Diversey Al'uminux plus 0.2 g./l. of dissolved aluminum at 65 C. for 10 minutes. The effects of zinc and copper content in the alloys upon the etched fiinsh are indicated in the accompanying table:
  • P.G.A. preferential grain attack.
  • P.G.B.A. preferential grain boundary attack.
  • EXAMPLE 3 Additional tests were carried out on extruded aluminum alloys of type No. 6063 and it was found that for such alloys having a zinc content up to 0.10% by Weight the presence of copper in the alloy in an amount equal to the zinc, i.e. on a 1:1 Weight basis ratio, there were produced acceptable etched surface finishes free of grainy ap pearance. With respect to artificially aged (T5 temper) similar etched alloys the same affect was also noticed with a zinc content of 0.05%. However, with a zinc content greater than 0.10% an increase in addition of copper amounting to twice the zinc content, i.e. on the 2:1 weight basis ratio of CuzZn, is called for so that a satisfactory etch finish is obtained.
  • An etched article consisting essentially of silicon in an amount in the range 0.200.6%, iron in the amount 0.35% max., manganese in the amount 0.10% max., magnesium in an amount in the range 0.450.9%, chro rnium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.030.10% and copper in the amount at the weight ratio 1:1 on a CuzZn weight basis ratio, others or impurities each in the amount 0.05% max., the total of said others or impurities being in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percents by Weight, and characterized by a uniform mat finish produced by perferential grain boundary attack, said etched article having been subjected to an alkaline etch treatment.
  • An etched article consisting essentially of silicon in an amount in the range 0.20-0.6%, iron in the amount 0.35% max., manganese inthe amount 0.10% max., magnesium in an amount in the range OAS-0.9%, chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.10-0.25% and copper in an amount at the weight ratio 2:1 on a CuzZn weight basis ratio, others or impurities each in the amount 0.05 max., the total of said others or impurities being in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percents by weight, and characterized by a uniform mat finish produced by preferential grain boundary attack, and etched article having been subjected to an alkaline etch treatment.
  • An etched article consisting essentially of silicon in an amount in the range 0.200.6%, iron in the amount 0.35% max., manganese in the amount 0.10 max., magnesium in an amount in the range OAS-0.9% chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.03-0.25 others or impurities each in the amount 0.05% max., the total of said others or impurities being in the amount 0.15% max., copper being present in an amount at the weight ratio 1:1 on a CuzZn weight basis ratio when zinc is present in an amount in the range 0.03-0.10% and copper being present in an amount at the weight ratio 2:1 on a CuzZn weight basis ratio when zinc is present in an amount in the range 0.10-0.25%, the remainder being aluminum, all the aforesaid percentages being percents by weight, and characterized by a uniform mat finish produced by preferential grain boundary attack, said etched article having been subjected to an alkaline etch treatment.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • ing And Chemical Polishing (AREA)

Abstract

AN ALUMINUM BASE ALLOY CAPABLE OF RECEIVING AN ALKALINE ETCH TREATMENT TO PRODUCE A UNIFORM MAT FINISH CONTAINS SILICON IN AN AMOUNT IN THE RNGE 0.2-0.6%, IRON IN THE AMOUNT 0.35% MAX., MANGENESE IN THE AMOUNT 0.10% MAX., MAGNESIUM IN AN AMOUNT IN THE RANGE 0.45-0.9%, CHROMIUM IN THE AMOUNT 0.1% MAX., TITANIUM IN THE AMOUNT 0.10% MAX., ZINC IN THE AMOUNT IN THE RANGE 0.03-0.25% AND COPPER IN AN AMOUNT IN THE WEIGHT RATIO 1:1 TO 2:1 ON A CU-ZN WEIGHT BASIS RATIO, OTHERS EACH IN THE AMOUNT 0.05% MAX., SAID OTHERS TOTAL IN THE AMOUNT 0.15% MAX., THE REMAINDER BEING ALUMINUM, ALL THE AFORESAID PERCENTAGES BEING PERCENT BY WEIGHT. OF THE ABOVE-MENTIONED ALLOYS WHEN THE ZINC CONTENT IS IN THE RANGE 0.10-0.25% THE COPPER SHOULD BE PRESENT IN AN AMOUNT IN THE WEIGHT RATIO 2:1 ON A CU-ZN WEIGHT BASIS RATIO AND, ALSO, IN THE ABOVE ALLOYS WHEN ZINC IS PRESENT IN AN AMOUNT IN THE RANGE 0.03-0-10% THE COPPER SHOULD BE PRESENT IN AN AMOUNT IN THE WEIGHT RATIO 1:1 ON A CU-ZN WEIGHT BASIS RATIO.

Description

United States Patent Int. Cl. C23f 1/00 US. Cl. 29-183 3 Claims ABSTRACT OF THE DISCLOSURE An aluminum base alloy capable of receiving an a1ka line etch treatment to produce a uniform mat finish contains silicon in an amount in the range 0.2-0.6%, iron in the amount 0.35% max., manganese in the amount 0.10% max., magnesium in an amount in the range 0.450.9%, chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in the amount in the range 0.030.25% and copper in an amount in the weight ratio 1:1 to 2:1 on a Cu-Zn weight basis ratio, others each in the amount 0.05% max., said others total in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percent by weight. Of the above-mentioned alloys when the zinc content is in the range 0.100.25% the copper should be present in an amount in the weight ratio 2:1 on a Cu-Zn weight basis ratio and, also, in the above alloys when zinc is present in an amount in the range 0.030.10% the copper should be present in an amount in the Weight ratio 1:1 on a Cu-Zn weight basis ratio.
This invention relates to aluminum alloys. More particularly, this invention relates to aluminum alloys capable of being extruded in a wide variety of forms or shapes and having utility in the architectural and other fields. More particularly this invention relates to aluminum alloys of the type known as AA6063.
Aluminum alloys of the type No. 6063 have the com position in percents by Weight Si 0.20-0.6, Fe 0.35 max., Mn 0.10 max., Mg 0.45;0.9, Cr 0.10 max., Ti 0.10 max., Zn 0.10 max., Cu 0.10 max., others, each 0.05 max. and said others, total 0.15 max., the remainder being aluminum. These alloys prior to use, particularly prior to anodizing, receive an alkaline etch treatment, such as by contact with a sodium hydroxide containing solution, so as to produce thereon an attractive finish.
It has been established that in the etching of aluminum alloys an undesirable etched surface appearance, i.e. a grainy or spangle appearance results from the grains of the alloy structure being attacked at the different rates during etching. This is due to the presence of excessive zinc in the alloy. Generally, zinc in these alloys is present as an impurity and comes from either the bauxite from which the aluminum constituent of the alloy is derived and/or from the scrap material used in the preparation of the alloy.
It has been observed that when alloys of the type No. 6063 containing zinc in an amount in excess of 0.03%, such as 0.05%, are etched in a solution of sodium hydroxide, these alloys tend to yield a grainy surface appearance. Since it is difficult to consistently produce on a commercial scale type No. 6063 alloys having a zinc content below about 0.03%, the development of a method of etching type No. 6063 alloys having a zinc content greater than 0.03% to yield a uniform mat finish would be useful and of major commercial importance.
Accordingly, it is an object of this invention to provide a type No. 6063 aluminum alloy having a zinc content greater than 0.03% and capable when subjected to 3,594,133 Patented July 20, 1971 an alkaline etch treatment of yielding a uniform etch finish, such as a uniform mat finish.
It is another object of this invention to provide an aluminum alloy of the type No. 6063 and containing zinc in an amount in the range 0.030.25% and capable, when subjected to an alkaline etch treatment, of yielding a uniform etch finish, such as a uniform mat finish.
How these and other objects of this invention are attained will become apaprent in the light of the accompanying disclosure.
It has been discovered that zinc-containing aluminum alloys, particularly aluminum alloys of the type No. 6063 having a zinc content greater than 0.03% by weight, can be etched to produce a uniform etch finish, such as a uniform mat finish, provided there is present in the zinc-containing aluminum alloy an amount of copper in the weight ratio 1:1 to 2:1 on a Cu-Zn weight basis ratio. Specifically, and in accordance with one embodiment of this invention, when the zinc content of such alloys is present in an amount in the range 0.030.10% copper should be present in the alloy in the Weight ratio 1:1 on a Cu-Zn Weight basis ratio so that when the alloy is subjected to an alkaline etch treatment, such as by contact with a sodium hydroxide-containing solution or its equivalent, the resulting etched alloy receives a uniform mat finish. In accordance with yet another embodiment of the practice of this invention, when such zinc-containing aluminum alloys contain an amount of zinc in the range 0.10-0.25%, copper should be present in an amount in the weight ratio 2:1 on a Cu-Zn weight basis ratio so that when such alloys are subjected to an alkaline etch treatment the resulting etched alloy receives a uniform mat finish.
Accordingly, in accordance with this invention, when an aluminum alloy of the type No. 6063 contains a zinc content in the range 0.030.10% there should also be included copper in an amount substantially the same as or the same as the zinc content on a Cu-Zn weight basis ratio of 1:1. Specifically, when the zinc content of such alloys is 0.05% by Weight, the copper content of such alloys should be 0.05% by weight also so that such alloy can be subjected to an alkaline etch treatment to yield a uniform mat finish. Likewise, when the zinc content of such alloys is in the amount 0.10% by weight, the copper content of such alloy should be 0.10%. When, however, the zinc content of such alloys is greater than 0.10% by Weight, such as an amount in the range 0.120.25% by weight, the amount of copper in such alloys should :be twice the zinc content such that the weight basis ratio CuzZn is 2:1. Specifically, in accordance with this embodiment of the invention when the zinc content of these alloys is 0.15% by weight the copper content of such alloy should be 0.30% by weight so that when the alloy is subjected to an alkaline etch treatment the resulting etched alloy receives a uni-form mat finish. Likewise, when the zinc content of such alloys is 0.25% by Weight, the copper content of the alloys should be 0.50% by weight so that the alloy when subjected to an alkaline etch treatment will receive a uniform mat finish.
The following examples are illustrative of the practice of this invention:
EXAMPLE 1 When an aluminum alloy having the composition in the following percents by weight, Fe 0.17, Mg 0.51, Mn 0.1, Si 0.46, Ti 0.01, Zn 0.088 and Cu 0.01, the remainder being aluminum, was etched with a standard etching solution (50 g./l. Diversey Aluminux, a proprietary caustic etchant solution, plus 0.2 g./l. of dissolved alluminum) at 65 C. for 2, 5 and 10 minutes,
the resulting etched aluminum alloy showed a pronounced grainy appearance indicating a pronounced preferential grain type of attack during etching. In this alloy tested the copper content was much less than the zinc content with the result that a satisfactory etch finish was not obtained.
EXAMPLE 2 Aluminum alloys of type No. 6063 containing various level combinations of zinc and copper content were etched in a solution of 50 g./l. of Diversey Al'uminux plus 0.2 g./l. of dissolved aluminum at 65 C. for 10 minutes. The effects of zinc and copper content in the alloys upon the etched fiinsh are indicated in the accompanying table:
P.G.A.=preferential grain attack. P.G.B.A.=preferential grain boundary attack.
The results reported in above Table I indicated that when the zinc content is less than 0.03% a uniform etch appearance is obtainable. When, however, the zinc con tent is greater than 0.03% by weight a uniform etch appearance is not obtainable save the instance where copper is present in said alloys in an amount equal to or at least equal to the zinc content. The tests further show that when the zinc content is 0.10% a grainy etched appearance is obtained if the copper content of the alloy is much less than the zinc content but when the copper content is equal to the zinc content there is produced a uniform etched appearance. The above test results show that the etfect of zinc is minimized by including copper in the alloy on a substantially 1:1 Weight basis ratio with respect to the zinc.
EXAMPLE 3 Additional tests were carried out on extruded aluminum alloys of type No. 6063 and it was found that for such alloys having a zinc content up to 0.10% by Weight the presence of copper in the alloy in an amount equal to the zinc, i.e. on a 1:1 Weight basis ratio, there were produced acceptable etched surface finishes free of grainy ap pearance. With respect to artificially aged (T5 temper) similar etched alloys the same affect was also noticed with a zinc content of 0.05%. However, with a zinc content greater than 0.10% an increase in addition of copper amounting to twice the zinc content, i.e. on the 2:1 weight basis ratio of CuzZn, is called for so that a satisfactory etch finish is obtained.
As will be apparent to those skilled in the art in the light of the foregoing disclosure, many modifications,
4 alterations and substitutions are possible in the practice of this invention without departing from the spirit or scope thereof.
We claim:
1. An etched article consisting essentially of silicon in an amount in the range 0.200.6%, iron in the amount 0.35% max., manganese in the amount 0.10% max., magnesium in an amount in the range 0.450.9%, chro rnium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.030.10% and copper in the amount at the weight ratio 1:1 on a CuzZn weight basis ratio, others or impurities each in the amount 0.05% max., the total of said others or impurities being in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percents by Weight, and characterized by a uniform mat finish produced by perferential grain boundary attack, said etched article having been subjected to an alkaline etch treatment.
2. An etched article consisting essentially of silicon in an amount in the range 0.20-0.6%, iron in the amount 0.35% max., manganese inthe amount 0.10% max., magnesium in an amount in the range OAS-0.9%, chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.10-0.25% and copper in an amount at the weight ratio 2:1 on a CuzZn weight basis ratio, others or impurities each in the amount 0.05 max., the total of said others or impurities being in the amount 0.15% max., the remainder being aluminum, all the aforesaid percentages being percents by weight, and characterized by a uniform mat finish produced by preferential grain boundary attack, and etched article having been subjected to an alkaline etch treatment.
3. An etched article consisting essentially of silicon in an amount in the range 0.200.6%, iron in the amount 0.35% max., manganese in the amount 0.10 max., magnesium in an amount in the range OAS-0.9% chromium in the amount 0.1% max., titanium in the amount 0.10% max., zinc in an amount in the range 0.03-0.25 others or impurities each in the amount 0.05% max., the total of said others or impurities being in the amount 0.15% max., copper being present in an amount at the weight ratio 1:1 on a CuzZn weight basis ratio when zinc is present in an amount in the range 0.03-0.10% and copper being present in an amount at the weight ratio 2:1 on a CuzZn weight basis ratio when zinc is present in an amount in the range 0.10-0.25%, the remainder being aluminum, all the aforesaid percentages being percents by weight, and characterized by a uniform mat finish produced by preferential grain boundary attack, said etched article having been subjected to an alkaline etch treatment.
References Cited UNITED STATES PATENTS 3,104,189 9/1963 Wagner 141 RICHARD O. DEAN, Primary Examiner US. Cl. X.R.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION 1.59 8 33 Dated July 20, 1971 Patent No.
Spooner Inventor(s) Jacques F. Cote, William Ernest Cooke and Roy C.
It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column 1, line +2, "O.H5;O.9, should read 0. +5-O.9
line 63, the word "etched" should appear after "grainy" Column 3, Table I, under the heading "Predominant type of attack" the phrase "Light P.G.B.Ag" should read Light P.G.B.A.
Column t, Claim 2, line 13, "and" should read said Claim 3, line 3, "0.10 max., should read 0.10% max.,
Signed and sealed this 15th day of February 1972.
(SEAL) Attest:
ROBERT GOTTSCHALK EDWARD M.FLETCHER, JR.
Commisioner of Patents Attesting Officer FORM E D-1 01 1 USCOMM-DC 6O37fi-D614 U 5. GOVERNMENT FRFNTING OFFICE I959 ()366'J34
US680323A 1967-11-03 1967-11-03 Aluminum alloy Expired - Lifetime US3594133A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68032367A 1967-11-03 1967-11-03

Publications (1)

Publication Number Publication Date
US3594133A true US3594133A (en) 1971-07-20

Family

ID=24730633

Family Applications (1)

Application Number Title Priority Date Filing Date
US680323A Expired - Lifetime US3594133A (en) 1967-11-03 1967-11-03 Aluminum alloy

Country Status (1)

Country Link
US (1) US3594133A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5384808A (en) * 1977-01-05 1978-07-26 Hitachi Ltd Aluminum alloy with damping capacity and manufacture thereof
US4589932A (en) * 1983-02-03 1986-05-20 Aluminum Company Of America Aluminum 6XXX alloy products of high strength and toughness having stable response to high temperature artificial aging treatments and method for producing
US5342459A (en) * 1993-03-18 1994-08-30 Aluminum Company Of America Aluminum alloy extruded and cold worked products having fine grain structure and their manufacture
US5507888A (en) * 1993-03-18 1996-04-16 Aluminum Company Of America Bicycle frames and aluminum alloy tubing therefor and methods for their production
US5607524A (en) * 1994-02-02 1997-03-04 Aluminum Company Of America Drive shafts for vehicles and other applications and method for production
WO1997011203A1 (en) * 1995-09-19 1997-03-27 Alcan International Limited Precipitation-hardened aluminum alloys for automotive structural applications
WO2017093304A1 (en) * 2015-12-02 2017-06-08 Norsk Hydro Asa Aluminium extrusion alloy suitable for etched and anodized components
WO2021254852A1 (en) 2020-06-15 2021-12-23 Dimitri Fotij Reliable high extrusion rate production method for high corrosion resistance powdercoated recycle friendly aluminum soft alloys

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5384808A (en) * 1977-01-05 1978-07-26 Hitachi Ltd Aluminum alloy with damping capacity and manufacture thereof
JPS579414B2 (en) * 1977-01-05 1982-02-22
US4589932A (en) * 1983-02-03 1986-05-20 Aluminum Company Of America Aluminum 6XXX alloy products of high strength and toughness having stable response to high temperature artificial aging treatments and method for producing
US5342459A (en) * 1993-03-18 1994-08-30 Aluminum Company Of America Aluminum alloy extruded and cold worked products having fine grain structure and their manufacture
US5507888A (en) * 1993-03-18 1996-04-16 Aluminum Company Of America Bicycle frames and aluminum alloy tubing therefor and methods for their production
US5607524A (en) * 1994-02-02 1997-03-04 Aluminum Company Of America Drive shafts for vehicles and other applications and method for production
WO1997011203A1 (en) * 1995-09-19 1997-03-27 Alcan International Limited Precipitation-hardened aluminum alloys for automotive structural applications
US6267922B1 (en) 1995-09-19 2001-07-31 Alcan International Limited Precipitation-hardened aluminum alloys for automotive structural applications
WO2017093304A1 (en) * 2015-12-02 2017-06-08 Norsk Hydro Asa Aluminium extrusion alloy suitable for etched and anodized components
US11542576B2 (en) 2015-12-02 2023-01-03 Norsk Hydro Asa Aluminium extrusion alloy suitable for etched and anodized components
WO2021254852A1 (en) 2020-06-15 2021-12-23 Dimitri Fotij Reliable high extrusion rate production method for high corrosion resistance powdercoated recycle friendly aluminum soft alloys

Similar Documents

Publication Publication Date Title
US3594133A (en) Aluminum alloy
US4737246A (en) Anodizing process for producing highly reflective aluminum materials without preliminary brightening processing
JP6595344B2 (en) Watch made from rose gold alloy
US4164434A (en) Aluminum alloy capacitor foil and method of making
GB1490648A (en) Aluminum alloy
US3164494A (en) Bright finished aluminum alloy system
GB440287A (en) Improvements in or relating to composite metallic articles
US3171797A (en) Method of sealing anodic aluminum oxide coatings
US2726436A (en) Metal-clad aluminum alloys
US4601796A (en) High reflectance semi-specular anodized aluminum alloy product and method of forming same
JPS5918457B2 (en) Magnesium-based alloy with high mechanical strength and low corrosion tendency
US3187428A (en) Method of treating aluminum and aluminum alloys preparatory to bright finishing
JPS6314830A (en) Sulfidization-resisting hard silver alloy
US3047939A (en) Composite electroplate
US3729391A (en) Surface treatment of zinc/aluminium alloys
US2058429A (en) Mirror
GB633154A (en) An improved aluminium base alloy
US3098724A (en) Aluminous metal article
US1840562A (en) Method of heat-treating aluminum and articles thereby
US2372546A (en) Zinc base alloy
US2094332A (en) Alloy
JPH0234741A (en) Aluminum alloy for automobile bumper and its manufacture
US2134830A (en) Process of producing corrosion resistant coatings on magnesium and high percentage magnesium alloys
JPS5943839A (en) Aluminum-magnesium alloy for die casting
CN110983390B (en) Composition for surface treatment of aluminum strip flexible connection