US1960916A - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- US1960916A US1960916A US675866A US67586633A US1960916A US 1960916 A US1960916 A US 1960916A US 675866 A US675866 A US 675866A US 67586633 A US67586633 A US 67586633A US 1960916 A US1960916 A US 1960916A
- Authority
- US
- United States
- Prior art keywords
- per cent
- aluminium alloy
- cerium
- aluminium
- alloy
- 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
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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
Description
Patented May 29, 1934 PATENT OFFICE 1,960,916 ALUMINIUM ALLOY Alfred John Murphy and Stanley Alfred Edward Wells, Teddington, England, assignors to J.
' Stone & Company Limited, Deptford, England,
a corporation of Great Britain i No Drawing. Application June 14, 1933, Serial No. 675,866. In Great Britain June 29, 1932 2 Claims.
This invention comprises improvements in aluminium alloys and in particular aluminium alloys of the class containing copper, nickel, magnesium, iron and silicon.
The object of the invention is to produce an alloy of this class having its grain refined, possessing improved running and casting qualities, having high mechanical strength capable of being' enhanced by appropriate heat treatment, and, without detriment to any of these characteristics, having a capacity for carrying a high iron content.
According to this invention, cerium is added to an aluminium alloy of the class referred to, the alloy thereby being cleansed and acquiring the properties referred to and being enabled to carry an iron content which is added to it in predetermined proportion and in accordance with the value of the cerium addition. The alloy has particularly advantageous casting qualities. It may be submitted to appropriate high and/or low temperature treatment, the final product being highly cleansed and possessing a refined grain and high mechanical strength. Certain micrographical constituents which make for structural weakness, are reduced by the addition of cerium, as compared with the results obtained when other metals are employed for a similar purpose. The approximate ranges of composition 01. the alloys in which we have discovered that these beneficial effects are exhibited are as follows:
According to one practical process in accordance with these improvements, an alloy is made up as Iollowsz-Ferro-aluminium, containing 10 per cent iron, is added to molten aluminium in the desired proportion. The following are then added in succession and in the proportions required to give the desired compositionz cerium-iron-aluminium alloy containing 5 per cent cerium, 10 per cent iron and 85 per cent aluminium; nickel-aluminium alloy containing 20 per cent nickel; copper-aluminium alloy containing 50 per cent copper; silicon-aluminium alloy containing 12 per cent silicon, and, finally magnesium. Alternatively, the cerium may be added as the pure metal, or as an alloy with any of the other components of the final alloy. The sequence of additions may also be altered from the above. a
The subsequent treatment for enhancing the mechanical properties of the alloys may be carried out by quenching or rapidly cooling them from a temperature of 480 C. to 570 C. followed by ageing at a temperature not exceeding 300 C. Thus the treatment may be carried out in two stages. The'first, for a period of four hours at 560 C. and the second for a period of sixteen hours at 200 C. These periods and temperatures have been found suitable for ordinary purposes but they may be varied so as to give other combinations of high and low temperatures and periods of treatment. Alternatively, the alloys may be aged at a temperature not exceeding 300 0. without previous treatment at higher temperatures after casting.
It will be understood that the cerium addition is the important consideration for the purpose described. In some alloys, manganese, chromium and titanium may be introduced in predetermined proportions as further additions but not as substitutes for the cerium.
It is desirable to increase the cerium content as the iron content is increased and the duration of the first heat treatment stage may be increased as the iron content is increased, the said period also varying,'of course, with the type of microstructure desired. I
Within the general limits above indicated some alloys are preferred for castings and others for forgings. This will be seen from the following examples:-
Remainder.
Another advantage obtained when using cerium, as compared with a metal such as titanium, is that the melting point is lower so that the making upof the alloy is facilitated.
We claim:-
1. An aluminium alloy containing 0.5 to 5.0 per cent copper, 0.5 to 3.0 per cent nickel, 0.1 to 2.5
per cent magnesium, 0.2 to 2.5 per cent silicon, 0.2 to 2.0 per cent iron, 0.02 to 1.0 per cent cerium, and the balance substantially all aluminium.
2. An aluminium alloy containing 0.5 to 5.0
mium and manganese for imparting the characteristics of resisting corrosion and increasing hardness, in the proportions of 0.02 to 0.20 per cent chromium and 0.1 to 0.5 per cent mangaper cent copper, 0.5 to 3.0 per cent nickel, 0.1 to nese, and the balance substantially all aluminium.
ALFRED JOHN MURPHY. STANLEY ALFRED EDWARD WELLS.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1960916X | 1932-06-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1960916A true US1960916A (en) | 1934-05-29 |
Family
ID=10894669
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US675866A Expired - Lifetime US1960916A (en) | 1932-06-29 | 1933-06-14 | Aluminium alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US1960916A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4831449B1 (en) * | 1968-04-29 | 1973-09-29 | ||
US3983274A (en) * | 1970-06-09 | 1976-09-28 | Swiss Aluminium Ltd. | Aluminum-copper-nickel alloy for the production of heat resistant pans and utensils coated with enamels and/or other non-metallic materials and corresponding aluminous metal articles |
US11761061B2 (en) * | 2017-09-15 | 2023-09-19 | Ut-Battelle, Llc | Aluminum alloys with improved intergranular corrosion resistance properties and methods of making and using the same |
-
1933
- 1933-06-14 US US675866A patent/US1960916A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4831449B1 (en) * | 1968-04-29 | 1973-09-29 | ||
US3983274A (en) * | 1970-06-09 | 1976-09-28 | Swiss Aluminium Ltd. | Aluminum-copper-nickel alloy for the production of heat resistant pans and utensils coated with enamels and/or other non-metallic materials and corresponding aluminous metal articles |
US11761061B2 (en) * | 2017-09-15 | 2023-09-19 | Ut-Battelle, Llc | Aluminum alloys with improved intergranular corrosion resistance properties and methods of making and using the same |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2915390A (en) | Aluminum base alloy | |
US1620082A (en) | Aluminum alloy containing lithium | |
US1254987A (en) | Alloy. | |
US1928747A (en) | Nonferrous alloy | |
US1960916A (en) | Aluminium alloy | |
US3392015A (en) | Aluminum-base alloy for use at elevated temperatures | |
US1952048A (en) | Aluminum-beryllium alloy | |
US1799837A (en) | Aluminum base alloy and piston made therefrom | |
US1933390A (en) | Copper zinc silicon alloys | |
US3082082A (en) | High strength, corrosionresistant alloy | |
US2022686A (en) | Aluminum alloy casting and method of making the same | |
US3372068A (en) | Heat treatment for improving proof stress of nickel-chromium-cobalt alloys | |
US2086604A (en) | Copper-titanium-silicon alloys | |
US3370945A (en) | Magnesium-base alloy | |
US2214432A (en) | Aluminum alloy containing copper, iron, and columbium | |
US1932843A (en) | Aluminum alloys | |
US2098081A (en) | Aluminum alloy | |
US2026209A (en) | Copper alloy | |
US1261987A (en) | Method of making aluminum-alloy articles. | |
US1723922A (en) | Copper cobalt alloy | |
US1572744A (en) | Nickel alloy and method of making the same | |
US2123886A (en) | Heat treated aluminum base alloy | |
US2239744A (en) | Thermal treatment for aluminum base alloys | |
US1860947A (en) | Aluminum alloy casting and process of making the same | |
US1932841A (en) | Aluminum alloys |