US1899465A - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- US1899465A US1899465A US450877A US45087730A US1899465A US 1899465 A US1899465 A US 1899465A US 450877 A US450877 A US 450877A US 45087730 A US45087730 A US 45087730A US 1899465 A US1899465 A US 1899465A
- Authority
- US
- United States
- Prior art keywords
- alloy
- aluminium
- aluminium alloy
- silver
- vanadium
- 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
Links
- 229910000838 Al alloy Inorganic materials 0.000 title description 4
- 229910045601 alloy Inorganic materials 0.000 description 10
- 239000000956 alloy Substances 0.000 description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 6
- 229910052720 vanadium Inorganic materials 0.000 description 5
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 229910052709 silver Inorganic materials 0.000 description 4
- 239000004332 silver Substances 0.000 description 4
- 238000005494 tarnishing Methods 0.000 description 4
- 238000007792 addition Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 229910001092 metal group alloy Inorganic materials 0.000 description 3
- 229910052763 palladium Inorganic materials 0.000 description 3
- 229910052716 thallium Inorganic materials 0.000 description 3
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 description 3
- 229910001316 Ag alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910001338 liquidmetal Inorganic materials 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910001631 strontium chloride Inorganic materials 0.000 description 2
- AHBGXTDRMVNFER-UHFFFAOYSA-L strontium dichloride Chemical compound [Cl-].[Cl-].[Sr+2] AHBGXTDRMVNFER-UHFFFAOYSA-L 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- -1 silver-copper-aluminium Chemical compound 0.000 description 1
- 229910000898 sterling silver Inorganic materials 0.000 description 1
- 239000010934 sterling silver Substances 0.000 description 1
Classifications
-
- 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
Definitions
- the new alloy possesses, in comparison with the known aluminium alloys, a number of valuable properties and is especially distinguished by high proofness against tarnishing.
- the new alloy comprises preferably an addition of vanadium or palladium, and for certain purposes a further addition of nickel. Aluminium nickel alloys have become known, which however do not have the additions of this new alloy and therefore do not possess the valuable properties of the same.
- a method of: increasing proofness of the new alloy forms part of the invention.
- This method is characterized in that the alloy, in liquid state, is submitted, at a temperature of approximately 750 0., to a refining and, purification by strontium chloride.
- the strontium chloride is preferably added, after the liquid metal has been left standing for about 5 to 10 minutes without being touched, in an aluminium cartridge at the bottom of the liquid metal, whereupon the bath is thoroughly stirred several times and each time is carefully skimmed.
- the new alloy is extraordinarily proof against tarnishing and shows no inclination to become black, in contrast to pure silver alloys which, when used, become black. This inconvenience of the pure silver alloys exeludes their use for numerous purposes.
- the new alloy can further be easily treated and is at least equal, and in many respects even superior, to the commonly used silver-copper-aluminium alloys as regards color, resistance and hardness. It is proof against tar nishing, for instance in sulphurous atmospheres, and superior in this respect to sterling silver and pure silver.
- the alloy can be cast to casting, chill-casting and extrusion-casting, and then shows resistances, which are equal to those of brass in cast and rolled condition.
- Theallo possesses also extraordinary adaptabihty or heavy drawings and is suitable to be used in the industries engaged in the prothe tarnishing the finest wall thicknesses, as sand- Serial No. 450,877, and in Germany Iarch 8, 1980.
- the semi-manufactured articles made of the alloy can be rolled out in any lengths and widths and they do not smear, when being worked up.
- composition of the new alloy is preferably as follows: copper 2 to 5% or nickel 0.2 to- 0.8% or copper and nickel in a total quantity of about 2 to 5%, silver 0.2 to 1%, thallium 0.02 to 0.2%, vanadium or palladium about 0.1%, the remainder commercial qualityaluminium with the usual iron percentage tolerances.
- a light metal alloy containin 0.2 to 4 vanadium or palladium upto 0.1%, the remainder principally aluminium.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Adornments (AREA)
- Electroplating And Plating Baths Therefor (AREA)
- Conductive Materials (AREA)
Description
Patented Feb. 28,1933
UNITED STATES OTTO KAMIE'S, OF BERLIN, GEEK-ANY ALUMINIUM ALLOY no Drawing. Application filed ma a, 1930,
The new alloy possesses, in comparison with the known aluminium alloys, a number of valuable properties and is especially distinguished by high proofness against tarnishing. The new alloy comprises preferably an addition of vanadium or palladium, and for certain purposes a further addition of nickel. Aluminium nickel alloys have become known, which however do not have the additions of this new alloy and therefore do not possess the valuable properties of the same.
A method of: increasing proofness of the new alloy forms part of the invention. This method is characterized in that the alloy, in liquid state, is submitted, at a temperature of approximately 750 0., to a refining and, purification by strontium chloride. The strontium chloride is preferably added, after the liquid metal has been left standing for about 5 to 10 minutes without being touched, in an aluminium cartridge at the bottom of the liquid metal, whereupon the bath is thoroughly stirred several times and each time is carefully skimmed.
The new alloy is extraordinarily proof against tarnishing and shows no inclination to become black, in contrast to pure silver alloys which, when used, become black. This inconvenience of the pure silver alloys exeludes their use for numerous purposes. The new alloy can further be easily treated and is at least equal, and in many respects even superior, to the commonly used silver-copper-aluminium alloys as regards color, resistance and hardness. It is proof against tar nishing, for instance in sulphurous atmospheres, and superior in this respect to sterling silver and pure silver. The alloy can be cast to casting, chill-casting and extrusion-casting, and then shows resistances, which are equal to those of brass in cast and rolled condition. Theallo possesses also extraordinary adaptabihty or heavy drawings and is suitable to be used in the industries engaged in the prothe tarnishing the finest wall thicknesses, as sand- Serial No. 450,877, and in Germany Iarch 8, 1980.
duction of vessels of any kind, of articlesof decoration and for lighting purposes. It possesses an extraordinarily uniformly fine crystalline structure. The semi-manufactured articles made of the alloy can be rolled out in any lengths and widths and they do not smear, when being worked up.
The composition of the new alloy is preferably as follows: copper 2 to 5% or nickel 0.2 to- 0.8% or copper and nickel in a total quantity of about 2 to 5%, silver 0.2 to 1%, thallium 0.02 to 0.2%, vanadium or palladium about 0.1%, the remainder commercial qualityaluminium with the usual iron percentage tolerances.
I claim:
1. A light metal alloy containin 0.2 to 4 vanadium or palladium upto 0.1%, the remainder principally aluminium.
4. A light metal alloy containing 0.2 to 1.0% of silver, 2 to 5% of copper, 0.02-to 0.2% of thallium, and an appreciable amount of vanadium up to 0.1%, e remainder principally aluminium. 5. A light metal alloy containing 0.2 to
1.0% of silver, 2 to 5% of copper, 0.02 to 0.2% of thallium, an appreciable amount of vanadium up to' 0.1%, and 0.2 to 0.8% of nickel,the remainder principally aluminium.
In testimonywhereof I aflix my signature.
. OTTO. KAMPS.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1899465X | 1930-03-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1899465A true US1899465A (en) | 1933-02-28 |
Family
ID=7748300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US450877A Expired - Lifetime US1899465A (en) | 1930-03-03 | 1930-05-08 | Aluminium alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1899465A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2418881A (en) * | 1944-06-10 | 1947-04-15 | Mallory & Co Inc P R | Sintered aluminum bearing |
| US2823994A (en) * | 1956-01-23 | 1958-02-18 | Fuchs Kg Otto | Al-mg-zn-alloy having high stress corrosion resistance |
-
1930
- 1930-05-08 US US450877A patent/US1899465A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2418881A (en) * | 1944-06-10 | 1947-04-15 | Mallory & Co Inc P R | Sintered aluminum bearing |
| US2823994A (en) * | 1956-01-23 | 1958-02-18 | Fuchs Kg Otto | Al-mg-zn-alloy having high stress corrosion resistance |
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