US2214433A - Aluminum alloy containing copper, silicon, iron, and columbium - Google Patents
Aluminum alloy containing copper, silicon, iron, and columbium Download PDFInfo
- Publication number
- US2214433A US2214433A US290075A US29007539A US2214433A US 2214433 A US2214433 A US 2214433A US 290075 A US290075 A US 290075A US 29007539 A US29007539 A US 29007539A US 2214433 A US2214433 A US 2214433A
- Authority
- US
- United States
- Prior art keywords
- columbium
- aluminum
- alloy
- iron
- silicon
- 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
- 239000010955 niobium Substances 0.000 title description 27
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 title description 26
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title description 22
- 229910052742 iron Inorganic materials 0.000 title description 11
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 title description 10
- 229910052802 copper Inorganic materials 0.000 title description 10
- 239000010949 copper Substances 0.000 title description 10
- 229910000838 Al alloy Inorganic materials 0.000 title description 9
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title description 9
- 229910052710 silicon Inorganic materials 0.000 title description 9
- 239000010703 silicon Substances 0.000 title description 9
- 229910045601 alloy Inorganic materials 0.000 description 25
- 239000000956 alloy Substances 0.000 description 25
- 229910052782 aluminium Inorganic materials 0.000 description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 16
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 238000005266 casting Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 239000004848 polyfunctional curative Substances 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 3
- 238000005242 forging Methods 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 229910000592 Ferroniobium Inorganic materials 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010348 incorporation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- PEQFPKIXNHTCSJ-UHFFFAOYSA-N alumane;niobium Chemical class [AlH3].[Nb] PEQFPKIXNHTCSJ-UHFFFAOYSA-N 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- WPPDFTBPZNZZRP-UHFFFAOYSA-N aluminum copper Chemical compound [Al].[Cu] WPPDFTBPZNZZRP-UHFFFAOYSA-N 0.000 description 1
- CYUOWZRAOZFACA-UHFFFAOYSA-N aluminum iron Chemical compound [Al].[Fe] CYUOWZRAOZFACA-UHFFFAOYSA-N 0.000 description 1
- -1 aluminum-iron-columbium Chemical compound 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 235000011121 sodium hydroxide Nutrition 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- 239000002023 wood 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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
Definitions
- Patented Sept. 10, 1940 UNITED STATES PATENT OFFICE.
- the object of the invention is to produce aluminum alloys having a fine grain, and possessing in consequence of this fine grain superior mechanical properties in the cast condition and also when forged and also after heat-treatment of the castings and forgings according to known processes.
- a relatively small 40 proportion of columbium also known sometimes as niobium
- an aluminum alloy particularly an alloy of one of the classes referred to, the alloy thereby acquiring a fine grain, which is maintained over a wide range of .conditions of melting, casting and working.
- the beneficial effect of the columbium is not dependent upon the manner in which it is incorporated in the alloy, but a convenient procedure is to add it in the form of a hardener or mother alloy or prealloy relatively rich in columbium.
- the first stage in the incorporation of the columbium in the aluminum alloy is the preparation of an aluminum alloy relatively rich in columbium from ferro-columbium and aluminum.
- the f-erro-columbium may be in the form of an alloy containing approximately equal parts of iron and .columbium with impurities such as tantalum, silicon and carbon in small proportions.
- Aluminum Remainder I The hardener alloys employed 'are: aluminumnickel with 20% nickel, aluminum-iron-columbium with 5% iron and 5% columbium; aluminum-iron with 10% iron, aluminum-copper with copper, aluminum-silicon with 20% silicon. Aluminum is melted in a crucible and the calculated quantities of hardeners are stirred in successively in the order in which they are menfacture of castings and forgings, and responds effectively to the known processes of heat-treat ment applicable to aluminum alloys containing copper, nickel, magnesium, silicon and iron.
- a large improvement in mechanical properties of forgings of the alloy is obtained by a two-stage heat-treatment in which the parts are first heated for 4 hours at 530 C., then quenched in water, reheated for 16 hours at C. and finally quenched in water again.
- a valuable feature of the grain refining action of columbium is that it is effective even when the aluminum alloy is raised to a high temperature before casting.
- the eflicacy of the'grain refining action of columbium it may be mentioned that, when an alloy of the composition stated above is cast at 800 C. into a dried sand mold to form a cylindrical block 3" high and 3" diameter, the grains visible in the macrostructure after etching have diameters of 0.2 to 1 mm., whereas the same alloy not containing columbium, cast under the same conditions, shows a grain diameter of 2.5 to 5 mm.
- the alloy described above has the advantage, due to the fine grain structure which columbium confers, that the ductility associated with a certain tensile strength is greater.
- the simple alloys of aluminum with copper In the simple alloys of aluminum with copper,
- the incorporation of columbium in the form of an aluminum-columbium alloy refines the grain and improves the strength and ductility of castings.
- Aluminum base alloy containing 0.5% to 12% copper, 0.2% to 2.5% silicon, iron in a proportion not over 2%, 0.1% to 0.5% columbium, remainder aluminum.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Description
Patented Sept. 10, 1940 UNITED STATES PATENT OFFICE.
ALUMINUM ALLOY CONTAINING COPPER, SILICON, IRON, AND COLUMBIUM Alfred John Murphy, Petts Wood, and Stanley Alfred Edward Wells, Te'ddington, England, assignors, by'mesne assignments, to Electro Metallurgical Company, New York,-N. Y., a corporation of West Virginia No Drawing. Original application April 16, 1937, Serial No. 137,280. Divided and this application August 14, 1939, Serial No. 290,075; In Great Britain May 5, 1936 2 Claims.
division of our application Serial No. 137,280,-
filed April 16, 1937.
10 In the production of cast pieces of aluminum base alloys, by which may be'understood alloys containing more than 70% of aluminum, it is desirable to secure the finest possible size of grain. The grain referred to is the macrostrucr ture, which is recognizable by the naked eye on smooth surfaces or sections of the cast pieces after they have been etched in suitable reagents, such asan aqueous solution of caustic soda, or hydrofluoric acid.
In castings a diminution in grain size improves the mechanical properties. The finer the grain size characteristic of an aluminum alloy, other things being equal, the better its founding properties in that the tendency 'to cracking in the mold is reduced and the production of sound -oastings is facilitated. In cast pieces intended to be forged, pressed, extruded or otherwise worked mechanically, a fine grain size is desirable because it assists the attainment of good mechanical properties in the subsequent Workmg.
The object of the invention is to produce aluminum alloys having a fine grain, and possessing in consequence of this fine grain superior mechanical properties in the cast condition and also when forged and also after heat-treatment of the castings and forgings according to known processes.
According to this invention, a relatively small 40 proportion of columbium, also known sometimes as niobium, is added to an aluminum alloy, particularly an alloy of one of the classes referred to, the alloy thereby acquiring a fine grain, which is maintained over a wide range of .conditions of melting, casting and working. We have found it convenient to make the proportion of columbium 0.1% to 0.2% of the total weight of the alloy. We haveobserved appreciable grain 50 refinement with as little as 0.05% of columbium, and on the other hand we have not found it generally necessary or desirable to exceed 0.5%
of columbium.
We have discovered that these beneficial ef- 55 fects are exhibited in the classes of alloy mentioned above containing the'elements set out below in the proportions stated by way of example:
Per cent Copper 0.5 to 12 Nickel 0.5 to Magnesium 0.1 to 3 Silicon 0.2 to 2.5 Iron 0.2 to 2 Columbium 0.05 to 1 The beneficial effect of the columbium is not dependent upon the manner in which it is incorporated in the alloy, but a convenient procedure is to add it in the form of a hardener or mother alloy or prealloy relatively rich in columbium. According to one practical process, the first stage in the incorporation of the columbium in the aluminum alloy is the preparation of an aluminum alloy relatively rich in columbium from ferro-columbium and aluminum. The f-erro-columbium may be in the form of an alloy containing approximately equal parts of iron and .columbium with impurities such as tantalum, silicon and carbon in small proportions. In preparing the columbium hardener alloy, aluminum is melted in a crucible and its temperature raised to 1100 to 1200 C. A weight of ferro-columbium equal to approximately onetenth of the weight of aluminum is stirred into the molten aluminum, or is carried in a perforated container which is moved up and down in the aluminum, until the addition is entirely dissolved. In this way an alloy containing ap-' proximately 5% columbium, 5% iron, with the balance substantially aluminum, is obtained. This is cast into molds, remelted in a crucible, allowed to-solidify and remelted without unnecessary superheating, in order to eliminate gases which may have become absorbed through the heating to high temperatures in the initial operation. After this presolidification treatment, the alloy is cast into suitable ingot molds.
One practical process for making up an alloy using the aluminum hardener" alloy relatively rich in columbium may be described. The final alloy to be made according to this example has the following nominal composition;
Per cent Copper 2.5 Nickel 1.5 Magnesium 0.8
Silicon 1 .2 Iron 1.2 Columbium 0.1
Aluminum Remainder I .The hardener alloys employed 'are: aluminumnickel with 20% nickel, aluminum-iron-columbium with 5% iron and 5% columbium; aluminum-iron with 10% iron, aluminum-copper with copper, aluminum-silicon with 20% silicon. Aluminum is melted in a crucible and the calculated quantities of hardeners are stirred in successively in the order in which they are menfacture of castings and forgings, and responds effectively to the known processes of heat-treat ment applicable to aluminum alloys containing copper, nickel, magnesium, silicon and iron. For example, a large improvement in mechanical properties of forgings of the alloy is obtained by a two-stage heat-treatment in which the parts are first heated for 4 hours at 530 C., then quenched in water, reheated for 16 hours at C. and finally quenched in water again.
A valuable feature of the grain refining action of columbium is that it is effective even when the aluminum alloy is raised to a high temperature before casting. As an illustration of the eflicacy of the'grain refining action of columbium, it may be mentioned that, when an alloy of the composition stated above is cast at 800 C. into a dried sand mold to form a cylindrical block 3" high and 3" diameter, the grains visible in the macrostructure after etching have diameters of 0.2 to 1 mm., whereas the same alloy not containing columbium, cast under the same conditions, shows a grain diameter of 2.5 to 5 mm.
As compared with a similar alloy not containing columbium, the alloy described above has the advantage, due to the fine grain structure which columbium confers, that the ductility associated with a certain tensile strength is greater. In the simple alloys of aluminum with copper,
. such as that containing 7% copper, the incorporation of columbium in the form of an aluminum-columbium alloy refines the grain and improves the strength and ductility of castings.
We claim:
1. Aluminum base alloy containing 0.5% to 12% copper, 0.2% to 2.5% silicon, iron in a proportion not over 2%, 0.05% to 1% columbium, remainder aluminum. I
2. Aluminum base alloy containing 0.5% to 12% copper, 0.2% to 2.5% silicon, iron in a proportion not over 2%, 0.1% to 0.5% columbium, remainder aluminum.
ALFRED JOHN MURPHY.
STANLEY ALFRED EDWARD 30
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US290075A US2214433A (en) | 1937-04-16 | 1939-08-14 | Aluminum alloy containing copper, silicon, iron, and columbium |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US137280A US2273061A (en) | 1936-05-05 | 1937-04-16 | Aluminum base alloys |
US290075A US2214433A (en) | 1937-04-16 | 1939-08-14 | Aluminum alloy containing copper, silicon, iron, and columbium |
Publications (1)
Publication Number | Publication Date |
---|---|
US2214433A true US2214433A (en) | 1940-09-10 |
Family
ID=26835095
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US290075A Expired - Lifetime US2214433A (en) | 1937-04-16 | 1939-08-14 | Aluminum alloy containing copper, silicon, iron, and columbium |
Country Status (1)
Country | Link |
---|---|
US (1) | US2214433A (en) |
-
1939
- 1939-08-14 US US290075A patent/US2214433A/en not_active Expired - Lifetime
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