US1572490A - Aluminum alloy - Google Patents
Aluminum alloy Download PDFInfo
- Publication number
- US1572490A US1572490A US8517A US851725A US1572490A US 1572490 A US1572490 A US 1572490A US 8517 A US8517 A US 8517A US 851725 A US851725 A US 851725A US 1572490 A US1572490 A US 1572490A
- Authority
- US
- United States
- Prior art keywords
- per cent
- alloy
- silicon
- aluminum
- zinc
- 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 5
- 229910045601 alloy Inorganic materials 0.000 description 24
- 239000000956 alloy Substances 0.000 description 24
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 18
- 229910052710 silicon Inorganic materials 0.000 description 18
- 239000010703 silicon Substances 0.000 description 18
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 14
- 229910052725 zinc Inorganic materials 0.000 description 14
- 239000011701 zinc Substances 0.000 description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 13
- 229910052802 copper Inorganic materials 0.000 description 13
- 239000010949 copper Substances 0.000 description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- 229910052782 aluminium Inorganic materials 0.000 description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 11
- 239000002184 metal Substances 0.000 description 7
- 229910052742 iron Inorganic materials 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 229910052783 alkali metal Inorganic materials 0.000 description 5
- 238000005266 casting Methods 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 150000001340 alkali metals Chemical class 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- 239000004576 sand Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 241000210674 Clathrus archeri Species 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 230000000717 retained effect Effects 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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
Definitions
- RODERICK L. JOHNSTON OF PLAINFIELD, NEW JERSEY, ROBERT S. ARCHER, OF LAKE- :WOOD, AND ZAY JEFFRIES, OF SHAKER HEIGHTS, OHIO, ASSIGNORS TO ALUMINUM COMPANY OF AMERICA, 0]? PITTSBURGH, PENNSYLVANIA, A CORPORATION OF.
- the metals capable of forming solid solutions in the aluminum we have found copper and zinc particularly advantageous.
- the metals referred to may be used singly or in combination.
- the silicon content of the alloy should in general be not less than about 3 percent nor more than about 10 per cent, and the copper should be preferably from about 2 per cent to about 5 per cent; the proportions of copper and silicon being variable, however, according to the particular combination of properties desired.
- the attainment of good casting qualities depends largely upon the relative proportions of the silicon and copper, the latter being preferably reduced as the former is increased, and vice versa.
- Such a bar after heat treatment by the method described in the above mentioned patent, showed an increase of tensile strength up to 30,000 pounds per square inch and an increase of elongation up to 2.5 per cent.
- a chill-cast heat-treated bar of an alloy containing about 6 per cent silicon and about 4: per cent copper was found to have a tensile strength exceeding 42,000 pounds per square inch and an elongat-ion exceeding 8 per cent in 2 inches. Alloys of aluminum, silicon and copper are described and claimed in our copending application identified hereinafter.
- an alloy containing about 10 per cent zinc and about 8 per cent silicon, to which alkali metal had been added and which was cast in a chill mold has been found to have a tensile strength exceeding 42,000 pounds per square inch, with an elongation up to 7 per cent in two inches.
- alloys described herein are also well adapted to forging and like operations.
- An alloy composed chie fly of aluminum, containing silicon between 3 and 10 per cent, and zinc, the latter not exceeding about 15 per cent.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
Description
Patented Feb. 9, 1926.
UNITED STATES PATENT OFFICE.
RODERICK L. JOHNSTON, OF PLAINFIELD, NEW JERSEY, ROBERT S. ARCHER, OF LAKE- :WOOD, AND ZAY JEFFRIES, OF SHAKER HEIGHTS, OHIO, ASSIGNORS TO ALUMINUM COMPANY OF AMERICA, 0]? PITTSBURGH, PENNSYLVANIA, A CORPORATION OF.
PENNSYLVANIA.
ALUMINUM ALLOY.
No Drawing- 0rigina1 application filed November 27, 1920, Serial No. 426,793. Divided and this application filed February 11, 1925. Serial No. 8,517.
To all whom it may concern:
Be it known that we, RODERICK L. J OHNS- TON, of Plainfield, county of Union, and State of New Jersey, ROBERT S. ARCHER, of Lakewood, and ZAY J EFFRIES, of Shaker Heights, both in the county of Cuyahoga and State of Ohio, all citizens of the United States of America, have invented certain new and useful Improvements in Aluminum Alloys, of which the following is a full, clear, and exact description.
The presence of small amounts of silicon in aluminum and in aluminum alloys is usually considered objectionable. In the course of an investigation upon the effects of silicon we have discovered that by using a substantial amount of silicon, materially greater than the quantity usually found as an impurity, with the addition of a metal or metals, for example one or more of those hereinafter named, it is possible to produce an alloy having excellent casting qualities combined with good physical properties.
Among the metals capable of forming solid solutions in the aluminum we have found copper and zinc particularly advantageous. The metals referred to may be used singly or in combination. In the use of copper alone, the silicon content of the alloy should in general be not less than about 3 percent nor more than about 10 per cent, and the copper should be preferably from about 2 per cent to about 5 per cent; the proportions of copper and silicon being variable, however, according to the particular combination of properties desired. In general, the attainment of good casting qualities depends largely upon the relative proportions of the silicon and copper, the latter being preferably reduced as the former is increased, and vice versa. Increasing the copper, at least up to the limit of its capacity for entering into solid solution in the aluminum, tends in general to increase the tensile strength, especially if subjected to a suitable heat treatment, say that described in Patent No. 1,508,556, issued September 16, 1924, to Zay Jeflries and Robert S. Archer. A test bar cast in sand in the ordinary way, of an aluminum alloy containing 10 per cent silicon and 3 per cent copper, showed a tensile strength of about 23,000 pounds per square inch and an elongation of about 1.5 per cent in two inches. Such a bar, after heat treatment by the method described in the above mentioned patent, showed an increase of tensile strength up to 30,000 pounds per square inch and an increase of elongation up to 2.5 per cent. A bar of the same alloy but cast in a chill mold, in order to cause rapid solidification of the molten metal, was found to have a tensile strength of about 30,000 pounds per square inch and an elongation of about 2.7 per cent, even without heat treatment. A similar bar, heat treated, had a tensile strength of 40,000 pounds per square inch and 6 per cent elongation. On the other hand, a chill-cast heat-treated bar of an alloy containing about 6 per cent silicon and about 4: per cent copper was found to have a tensile strength exceeding 42,000 pounds per square inch and an elongat-ion exceeding 8 per cent in 2 inches. Alloys of aluminum, silicon and copper are described and claimed in our copending application identified hereinafter.
The addition of zinc up to about 5 per cent has a slight effect on the tensile strength of the alloy. Above that amount a greater increase of tensile strength is observed. The presence of the zinc is often an advantage by reason of the whiter color of the polished alloy. We have found that with the addition of an alkali metal or metals to the alloy, as described in patent of Junius D. Edwards, Francis C. Frary and Harry V. Churchill, No. 1,410,461, issued March 21, 1922, very satisfactory physical properties can be obtained along with the other advantages incident to the presence of the zinc, particularly if the alloy to which alkali metal has been added is cast in such a manner, as for example by the use of a chill mold, that the molten metal is caused to solidify rapidly. For instance, an alloy containing about 10 per cent zinc and about 8 per cent silicon, to which alkali metal had been added and which was cast in a chill mold, has been found to have a tensile strength exceeding 42,000 pounds per square inch, with an elongation up to 7 per cent in two inches. A similar casting, after being subjected to and an elongation of 1.5 per cent.
the heat treatment described in the above mentioned patent of Archer and Jefiries, showed a decrease of tensile strength to about 35,000 pounds per square inch, but an increase of elongation up to 14 per cent.
In the case of aluminum-silicon alloys containing both copper and zinc, a sand cast test bar of an alloy containing 8 per cent silicon, 10 per cent zinc and 2.5 per cent copper, was found to have a tensile strength of 27,000 pounds per square inch This alloy is also susceptible to improvement by addition of alkali metal before casting; sand cast specimens of the alloy'so treated having a tensile strength of 30,000 pounds per square inch with an elongation of 2 per cent, while chill cast specimens have a tensile strength of 38,000 pounds per square inch and an elongation of 3.5 per cent. Heat treatment by the method described in the patent of Archer and Jefiries before referred to has been found to increase the tensile strength of the chill cast alloy up to 45,000 pounds per square inch and at the same time increase the elongation to 7.5 per cent.
In the alloys referred to above we have observed that the elongation is better if the iron content is low, and for that reason there are many cases where the iron should not exceed about 0.6 per cent. In other cases much higher iron can be used, especially in chill castings, as for example pressure die castings.
The alloys described herein are also well adapted to forging and like operations.
While in certain of the claims certain percentages and limits have been stated it is to be understood that they may be somewhat departed from without departing from the invention sought to be protected, so long as the properties of the alloy are retained.
This application is a division of our copending application, Serial No. 426,793, filed November 27, 1920.
We claim:
1. An alloy composed chiefly of aluminum, containing, approximately, silicon 8 per cent, zinc 1.0 per cent, and copper 2.5 per cent.
2. An alloy. composed chie fly of aluminum, containing silicon between 3 and 10 per cent, and zinc, the latter not exceeding about 15 per cent.
3. An alloy composed chiefly of aluminum, containing silicon between 3 and 10 per cent, and zinc between 5 and 15 per cent, approximately.
4. An alloy composed chiefly of aluminum, containing about 8 per cent silicon, an:l about 10 per cent zinc.
5. An alloy composed chiefly of aluminum, containing, approximately, silicon 8 per cent, zinc 10 per cent, and copper 2.5 per cent, with an iron content not exceed ing about 0.6 per cent.
6. An alloy composed chiefly of aluminum, containing silicon between 3 and 10 per cent and zinc, the latter not exceeding about 15 per cent, with an iron content not exceeding about 0.0 per cent.
7. An alloy composed chiefly of aluminum, containing about 8 per cent silicon and about 10 per cent zinc, with an iron content not exceeding about 0.0 per cent.
In testimony whereof we hereto afiix our signatures.
RODERICK L. JOHNSTON. ROBERTS. ARCHER. ZAY JEFFRIES.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US8517A US1572490A (en) | 1920-11-27 | 1925-02-11 | Aluminum alloy |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US426793A US1572489A (en) | 1920-11-27 | 1920-11-27 | Aluminum alloy |
US8517A US1572490A (en) | 1920-11-27 | 1925-02-11 | Aluminum alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US1572490A true US1572490A (en) | 1926-02-09 |
Family
ID=23692227
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US426793A Expired - Lifetime US1572489A (en) | 1920-11-27 | 1920-11-27 | Aluminum alloy |
US8517A Expired - Lifetime US1572490A (en) | 1920-11-27 | 1925-02-11 | Aluminum alloy |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US426793A Expired - Lifetime US1572489A (en) | 1920-11-27 | 1920-11-27 | Aluminum alloy |
Country Status (2)
Country | Link |
---|---|
US (2) | US1572489A (en) |
FR (1) | FR543938A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2568180A (en) * | 1949-04-12 | 1951-09-18 | William F Jobbins Inc | Aluminum base alloys |
US2568179A (en) * | 1949-04-12 | 1951-09-18 | William F Jobbins Inc | Aluminum base alloys |
US2584772A (en) * | 1949-05-10 | 1952-02-05 | William F Jobbins Inc | Aluminum base alloys |
-
1920
- 1920-11-27 US US426793A patent/US1572489A/en not_active Expired - Lifetime
-
1921
- 1921-11-26 FR FR543938D patent/FR543938A/en not_active Expired
-
1925
- 1925-02-11 US US8517A patent/US1572490A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US1572489A (en) | 1926-02-09 |
FR543938A (en) | 1922-09-12 |
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