US1903842A - Aluminum alloy - Google Patents
Aluminum alloy Download PDFInfo
- Publication number
- US1903842A US1903842A US612651A US61265132A US1903842A US 1903842 A US1903842 A US 1903842A US 612651 A US612651 A US 612651A US 61265132 A US61265132 A US 61265132A US 1903842 A US1903842 A US 1903842A
- Authority
- US
- United States
- Prior art keywords
- alloys
- magnesium
- boron
- tungsten
- aluminum
- 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
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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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
Definitions
- My invention relates to a series of aluminum alloys of novel composition and properties.
- the alloys of my invention are articularly characterized by the presence boron and magnesium and by-the absence of substantial amounts of silicon, copper and iron.
- the presence of one or more metals of the group comprising vanadium, tungsten, molybdenum, chromium and cobalt, is also characteristic of the preferred form of my new alloys.
- the alloys of the invention combine light weight with a high hardness and tensile strength.
- a surprisin property ofthe new alloys is their high e ectrical conductivity and resistance to corrosion.
- the metals may be utilized either in the cast condition, or they maybe rolled, drawn orotherwise worked.
- Mechanical working is preferably carried out at a temperature of l50450 C. and such working efiects a material increase in the tensile strength of the alloys.
- Wire drawn from the alloys of the invention is particularly valuable, since it combines a relatively high tensile strength with a relatively high conductivity. A further valuable property of such wires is that sleet and snow do not readily stick to them.
- a particularly valuable alloy embodying my invention has the following composition:
- Aluminum -rema'inder The amount of magnesium may vary from about 0.25% to about 2.25%, the preferred 7 40 amount being from 0.75% to 1.5% and the boron from 0.05% to 2%, although at"lea,st'
- vanadiumor tungsten may be used alone in these alloys, and either or both may be replaced in whole or in part b one or more of the metals molybdenum, c romium and cobalt. In neral it Wis advantageous to use the meta s of the als as oxides.
- a principal I function of boron in the'alloys of the invention is to increase the hardness; a principal function of the magnesium is to decrease the specific gravity and increase the resistance of the alloys against corrosion; and the rincipal function of the tungs'ten, vana ium, molybdenum, cobalt andchromium is to increase-the tensile strength of the alloys.
- An advantageous method of producing the alloys of the invention is as follows: The aluminum is melted in a crucible and covered with a layer of powderedcharcoal. The charcoal servesto protect the metal from oxidation and to reduce those metals which are added in the form of oxides.
- the magnesium is added as metal and the boron, tungsten and vanadium or their substituting met-
- the added metals or their oxides are advantageously added enclosed in aluminum capsules.
- the boronoxide is pref-, erahly added first, although it may be added together with the magnesium.
- the other metal oxides may be added together.
- Anv alloy consisting principally ofaluminum and containing from 0.25 to 0.75%
Description
Patented Apr. 18,
oouar c. mus, onmiw YORK, 11.x.
ALUMINUM ALLOY Ho Drawing.
My invention relates to a series of aluminum alloys of novel composition and properties. The alloys of my invention are articularly characterized by the presence boron and magnesium and by-the absence of substantial amounts of silicon, copper and iron. The presence of one or more metals of the group comprising vanadium, tungsten, molybdenum, chromium and cobalt, is also characteristic of the preferred form of my new alloys.
The alloys of the invention combine light weight with a high hardness and tensile strength. A surprisin property ofthe new alloys is their high e ectrical conductivity and resistance to corrosion.
The metals may be utilized either in the cast condition, or they maybe rolled, drawn orotherwise worked. Mechanical working is preferably carried out at a temperature of l50450 C. and such working efiects a material increase in the tensile strength of the alloys. Wire drawn from the alloys of the invention is particularly valuable, since it combines a relatively high tensile strength with a relatively high conductivity. A further valuable property of such wires is that sleet and snow do not readily stick to them.
A particularly valuable alloy embodying my invention has the following composition:
Magnesium 1.25% Boron 0.75% Vanadium 0.75% 85 Tungsten 0.7 5%
Aluminum -rema'inder The amount of magnesium may vary from about 0.25% to about 2.25%, the preferred 7 40 amount being from 0.75% to 1.5% and the boron from 0.05% to 2%, although at"lea,st'
I higher amounts. Either vanadiumor tungsten may be used alone in these alloys, and either or both may be replaced in whole or in part b one or more of the metals molybdenum, c romium and cobalt. In neral it Wis advantageous to use the meta s of the als as oxides.
.s. Applic'ationflcd lay 20.1w. mm No. 818,651.
group including vanadium, tungsten,-molybenum, chromium and cobalt in amounts of from 0.25% to 3.0%; larger amounts may be used, but the" tend to increase the specific. gravity and t e cost of the alloy.
In general it may be said that a principal I function of boron in the'alloys of the invention is to increase the hardness; a principal function of the magnesium is to decrease the specific gravity and increase the resistance of the alloys against corrosion; and the rincipal function of the tungs'ten, vana ium, molybdenum, cobalt andchromium is to increase-the tensile strength of the alloys.
Alloys of the invention as described above have been obtained having a specific gravity .of 2.66 to 2.70; a tensile strength when cast of 30,000to 41,000 pounds per square inch, and when mechanically worked of from 51,000 to 56,000 pounds; and an. electrical conductivity of 50-58 (Ag=100).
An advantageous method of producing the alloys of the invention is as follows: The aluminum is melted in a crucible and covered with a layer of powderedcharcoal. The charcoal servesto protect the metal from oxidation and to reduce those metals which are added in the form of oxides. The magnesium is added as metal and the boron, tungsten and vanadium or their substituting met- The added metals or their oxides are advantageously added enclosed in aluminum capsules. The boronoxide is pref-, erahly added first, although it may be added together with the magnesium. The other metal oxides may be added together.
I claim: 1. An alloy consisting principally of aluminum and containing from 0.05 to 2% of boron, from 0.25 to 2.25% of magnesium, and
from 0.25 to 3% of at least one metal of the group consisting of vanadium, tungsten,v
molybdenum and chromium. f
2. Anv alloy consisting principally ofaluminum and containing from 0.25 to 0.75%
of boron, from 0.75 to 1.5% of magnesium,
and from 0.25% to 3% of at least one metal of the group consisting of vanadium, tungsten,
molybdenum and chromium.
2 amsms 3. An alloy of about the following cmpw sition Magnesium 1.25% Boron 0.75% 5 Vanadium 0.75%
Tungsten 0.75%;
and the remainder rincipally aluminum. 4. An alloy consisting principally of aluminum and containing from 0.05130 2% 0i? boron, from 0.25 to 2.25% of magnesium and from 0.25% to 3% of vanadium. In testimony whereoibl afiix my signature.
C URT Q. TKTUS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US612651A US1903842A (en) | 1932-05-20 | 1932-05-20 | Aluminum alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US612651A US1903842A (en) | 1932-05-20 | 1932-05-20 | Aluminum alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US1903842A true US1903842A (en) | 1933-04-18 |
Family
ID=24454066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US612651A Expired - Lifetime US1903842A (en) | 1932-05-20 | 1932-05-20 | Aluminum alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US1903842A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0110190A1 (en) * | 1982-11-26 | 1984-06-13 | ALUMINIA S.p.A. | Aluminium alloys for nuclear apparatus |
-
1932
- 1932-05-20 US US612651A patent/US1903842A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0110190A1 (en) * | 1982-11-26 | 1984-06-13 | ALUMINIA S.p.A. | Aluminium alloys for nuclear apparatus |
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