US1934281A - Aluminum-silicon alloy - Google Patents
Aluminum-silicon alloy Download PDFInfo
- Publication number
- US1934281A US1934281A US424726A US42472630A US1934281A US 1934281 A US1934281 A US 1934281A US 424726 A US424726 A US 424726A US 42472630 A US42472630 A US 42472630A US 1934281 A US1934281 A US 1934281A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- silicon
- titanium
- alloy
- casting
- 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
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 title description 16
- 229910000676 Si alloy Inorganic materials 0.000 title description 13
- 238000005266 casting Methods 0.000 description 32
- 229910045601 alloy Inorganic materials 0.000 description 31
- 239000000956 alloy Substances 0.000 description 31
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 22
- 239000010936 titanium Substances 0.000 description 22
- 229910052719 titanium Inorganic materials 0.000 description 22
- 229910052782 aluminium Inorganic materials 0.000 description 17
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 17
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 14
- 239000010703 silicon Substances 0.000 description 14
- 229910052710 silicon Inorganic materials 0.000 description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- -1 aluminum-silicon-copper Chemical compound 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 229910000881 Cu alloy Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- WPPDFTBPZNZZRP-UHFFFAOYSA-N aluminum copper Chemical compound [Al].[Cu] WPPDFTBPZNZZRP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000010411 cooking Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 2
- 238000011282 treatment Methods 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 238000011946 reduction process Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 150000003609 titanium compounds Chemical class 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
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47J—KITCHEN EQUIPMENT; COFFEE MILLS; SPICE MILLS; APPARATUS FOR MAKING BEVERAGES
- A47J36/00—Parts, details or accessories of cooking-vessels
- A47J36/02—Selection of specific materials, e.g. heavy bottoms with copper inlay or with insulating inlay
Definitions
- the invention relates to aluminum-silicon casting alloys and it is particularly concerned with new alloy compositions having improved casting properties.
- the physical properties of aluminum-silicon alloys are especially advantageous for small and intricate castings such as motor parts and miscellaneous fittings, and for east articles such as cooking utensils, as well as comparatively large structural shapes of various design.
- the aluminum silicon alloys generally used for these purposes contain between about 3 to 15 per cent of silicon together with a small amount of iron as impurity, and sometimes copper, nickel, zinc, magnesium or similar alloying elements added in varying amounts to impart certain particular and beneficial properties.
- alloys of this type the aluminum-silicon-copper alloys are, for example, well known. Alloys containing somewhat smaller amounts than 3 per cent of silicon together with copper, nickel, etc., are used to some extent for casting purposes.
- shrinks or draws When, however, aluminum-silicon alloys are cast there are often formed small depressions or holes on the surface of the casting which are usually known as shrinks or draws. These are apparently due to shrinkage at the boundaries of the grains within the metal. In any casting these shrinks are undesirable, and in many cases they are so numerous and their effect on the strength, appearance and other properties of the casting is so objectionable as to preclude the use of the casting for its intended purpose, thus necessitating numerous rejections of castings which otherwise are perfectly good.
- the present invention is predicated upon my discovery that this serious tendency of aluminumsilicon alloy to form shrinks or draws on solidification may be inhibited, in some cases completely, by the presence of a small amount of titanium in the alloy, and I have found that the addition will allow the use of aluminumsilicon alloys for castings which had not heretofore been considered possible with these alloys. Furthermore, the addition of the titanium to these alloys does not appear to decrease their natural strength.
- One of the desirable features of my invention is the small amount of titanium required to eliminate these shrinks or draws.
- the amount of alloyed titanium which will produce the most beneficial results may vary slightly according to the particular aluminum-silicon alloys with which it is used but will usually fall within the range of 0.1 to 0.5 per cent. Ordinarily it is not necessary to have present in the alloy more than about 0.1 to 0.2 per cent of titanium. In some cases the titanium content may be even less. Greater amounts ithan 0.5 per cent may be added but the segregation caused by the high melting titanium constituent which is formed when titanium is added to aluminum makes it inadvisable to exceed this concentration.
- titanium-bearing ore for example titanium oxide, or alumina containing titanium oxide, may be added to the fluoride bath in the electrolytic pot, so that the titanium compound will, during the reduction process, be reduced to metallic titanium which will alloy with the aluminum. Silicon may then be added to this titanium-bearing aluminum in any convenient form, such as a silicon-rich aluminumsilicon alloy, or as metallic silicon.
- the aluminum which is used in making these alloys may be of any commercial grade or may be aluminum of the highest purity. Usually, however, it is ad vantageous for economic reasons to use aluminum of commercial grade, though containing small amounts of iron and other impurities.
- Castings of the aluminum-silicon-titanium a1- loy may be made from the untreated molten alloy and also from the alloy which has, before casting, been treated to modify or improve its internal structure.
- Treatments for such purposes are well known and may consist, for example, in the addition of metallic sodium or potassium or a compound or compounds thereof to the molten alloy directly before casting. The ultimate eifect of this treatment is to produce a casting having substantially higher strength and ductility than is found in the so-called unmodified alloy.
- aluminum-silicon-titanium alloy is used in the appended claims as a generic expression to include the following alloys and none other: (a) Alloys consisting entirely of aluminum, silicon, and titanium; and (b) alloys consisting of aluminum, silicon, titanium, and one or more metals of the class composed of copper, nickel, zinc, magnesium and the like; the titanium in each case serving to substantially inhibit the formation of surface shrinks or draws in casting the alloy.
- I claim- 1 An aluminum-silicon-titanium casting alloy composed chiefly of aluminum, having about 3 to 15 per cent silicon and about 0.1 to 0.5 per cent titanium, the latter element serving to substantially inhibit the formation of surface shrinks or draws when the alloy is cast.
- An aluminum-silicon-titanium casting alloy composed chiefly of aluminum, having about 3 to 15 per cent silicon and about 0.1 to 0.2 per cent titanium, the latter element serving to substantially inhibit the formation of surface shrinks or draws when the alloy is cast.
- An aluminum base casting alloy consisting of silicon between about 3 and 15 per cent, titanium between about 0.1 and 0.5 per cent, and the balance aluminum, characterized, in the cast condition, by substantial freedom from surface shrinks or draws.
- An aluminum base casting alloy consisting of silicon between about 3 and 15 per cent, titanium from about 0.1 to about 0.2 per cent, and the remainder aluminum, characterized, in the cast condition, by substantial freedom from surface shrinks and draws.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Food Science & Technology (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Patented Nov. 7, 1933 UNITED STATES PATENT OFFICE ALUIHINUM- SILICON ALLOY No Drawing. Application January 30, 1936 Serial No. 424,726,
4 Claims.
The invention relates to aluminum-silicon casting alloys and it is particularly concerned with new alloy compositions having improved casting properties.
5 The use of aluminum alloys in cast articles has received considerable impetus in recent years because of the adaptability of these alloys to various conditions of casting practice and their desirable combination of strength, lightness and excellent appearance in the cast condition. Among those aluminum alloys which have obtained wide-spread application in the casting art the aluminum-silicon alloys containing substantial amounts of silicon are, in importance and extensive use, second only to aluminum base alloys containing copper.
The physical properties of aluminum-silicon alloys, including their resistance to the corrosive agencies commonly encountered, are especially advantageous for small and intricate castings such as motor parts and miscellaneous fittings, and for east articles such as cooking utensils, as well as comparatively large structural shapes of various design. The aluminum silicon alloys generally used for these purposes contain between about 3 to 15 per cent of silicon together with a small amount of iron as impurity, and sometimes copper, nickel, zinc, magnesium or similar alloying elements added in varying amounts to impart certain particular and beneficial properties. Among alloys of this type the aluminum-silicon-copper alloys are, for example, well known. Alloys containing somewhat smaller amounts than 3 per cent of silicon together with copper, nickel, etc., are used to some extent for casting purposes.
When, however, aluminum-silicon alloys are cast there are often formed small depressions or holes on the surface of the casting which are usually known as shrinks or draws. These are apparently due to shrinkage at the boundaries of the grains within the metal. In any casting these shrinks are undesirable, and in many cases they are so numerous and their effect on the strength, appearance and other properties of the casting is so objectionable as to preclude the use of the casting for its intended purpose, thus necessitating numerous rejections of castings which otherwise are perfectly good.
The present invention is predicated upon my discovery that this serious tendency of aluminumsilicon alloy to form shrinks or draws on solidification may be inhibited, in some cases completely, by the presence of a small amount of titanium in the alloy, and I have found that the addition will allow the use of aluminumsilicon alloys for castings which had not heretofore been considered possible with these alloys. Furthermore, the addition of the titanium to these alloys does not appear to decrease their natural strength.
One of the desirable features of my invention is the small amount of titanium required to eliminate these shrinks or draws. I have determined that the amount of alloyed titanium which will produce the most beneficial results may vary slightly according to the particular aluminum-silicon alloys with which it is used but will usually fall within the range of 0.1 to 0.5 per cent. Ordinarily it is not necessary to have present in the alloy more than about 0.1 to 0.2 per cent of titanium. In some cases the titanium content may be even less. Greater amounts ithan 0.5 per cent may be added but the segregation caused by the high melting titanium constituent which is formed when titanium is added to aluminum makes it inadvisable to exceed this concentration.
In any casting operation there are, as is well known, a number of variables, many of them 8 elusive and diflicult to control, which must be favorably adjusted before good castings can be obtained, but even the most careful observance of these well known conditions is insufficient, in the case of aluminum-silicon alloys, to secure uniformly good castings in respect to freedom from shrinks and'- draws, whereas with my aluminum-silicon-titanium alloy this important uni" formity of results is readily obtainable when conditions which are known to give poor results are avoided.
In casting the alloy the best results will be obtained if the temperature of. the molten metal be kept as low as possible consistent with proper pouring and the time of holding the metal molten before pouring the casting be not too long. However, in the usual foundry practice it is at times necessary to pour at a higher temperature because of the casting design and section thickness or to hold the metal molten for a considerable time before pouring. This latter practice will have an injurious tendency which I have found to be offset by the use of titanium as described in this specification.
The manner in which titanium is added to the alloy is not important and in so far as the final result is concerned, any of the well known methods of addition may be used. However, the usual precautionsemployedwith good melting and casting practice should be observed. It has been found advantageous to add the titanium in the course of. the electrolytic production of the aluminum rather than to add it to the final aluminum-silicon alloy. A titanium-bearing ore, for example titanium oxide, or alumina containing titanium oxide, may be added to the fluoride bath in the electrolytic pot, so that the titanium compound will, during the reduction process, be reduced to metallic titanium which will alloy with the aluminum. Silicon may then be added to this titanium-bearing aluminum in any convenient form, such as a silicon-rich aluminumsilicon alloy, or as metallic silicon. The aluminum which is used in making these alloys may be of any commercial grade or may be aluminum of the highest purity. Usually, however, it is ad vantageous for economic reasons to use aluminum of commercial grade, though containing small amounts of iron and other impurities.
Castings of the aluminum-silicon-titanium a1- loy may be made from the untreated molten alloy and also from the alloy which has, before casting, been treated to modify or improve its internal structure. Treatments for such purposes are well known and may consist, for example, in the addition of metallic sodium or potassium or a compound or compounds thereof to the molten alloy directly before casting. The ultimate eifect of this treatment is to produce a casting having substantially higher strength and ductility than is found in the so-called unmodified alloy.
The importance of the elimination of the shrinkage defect in aluminum-silicon alloy may be illustrated by the case of a large foundry which makes a variety of cast aluminum cooking utensils of more or less intricate design. This foundry had encountered the usual difficulty in obtaining good castings of aluminum-silicon alloys containing 5 per cent of silicon, particularly in some of the more intricate castings, these latter always showing so large a number of shrinks or draws on their surface as to be unsuitablefor use. Because of this it was found necessary to substitute for the aluminum-silicon alloy an aluminum-copper alloy containing 5 per cent of copper which, although not entirely overcoming the difficulty, made posisble the production ofa better casting. This substitution, however, was objectionable because of the inferior corrosionresisting properties of the aluminum-copper alloy. But with aluminum-silicon alloy containing 5 per cent of silicon to which there had been added, in accordance with my discovery, 0.1 per cent of titanium, the trouble was obviated and castings were regularly produced of a quality which had theretofore been considered impossible. This specific instance is given only by way of illustration.
The term aluminum-silicon-titanium alloy is used in the appended claims as a generic expression to include the following alloys and none other: (a) Alloys consisting entirely of aluminum, silicon, and titanium; and (b) alloys consisting of aluminum, silicon, titanium, and one or more metals of the class composed of copper, nickel, zinc, magnesium and the like; the titanium in each case serving to substantially inhibit the formation of surface shrinks or draws in casting the alloy.
It is to be understood that the invention is not limited to the specific details herein described but may be carried out in other ways without departure from its spirit.
I claim- 1. An aluminum-silicon-titanium casting alloy composed chiefly of aluminum, having about 3 to 15 per cent silicon and about 0.1 to 0.5 per cent titanium, the latter element serving to substantially inhibit the formation of surface shrinks or draws when the alloy is cast.
2. An aluminum-silicon-titanium casting alloy composed chiefly of aluminum, having about 3 to 15 per cent silicon and about 0.1 to 0.2 per cent titanium, the latter element serving to substantially inhibit the formation of surface shrinks or draws when the alloy is cast.
3. An aluminum base casting alloy consisting of silicon between about 3 and 15 per cent, titanium between about 0.1 and 0.5 per cent, and the balance aluminum, characterized, in the cast condition, by substantial freedom from surface shrinks or draws.
4. An aluminum base casting alloy consisting of silicon between about 3 and 15 per cent, titanium from about 0.1 to about 0.2 per cent, and the remainder aluminum, characterized, in the cast condition, by substantial freedom from surface shrinks and draws.
THERON D. STAY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US424726A US1934281A (en) | 1930-01-30 | 1930-01-30 | Aluminum-silicon alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US424726A US1934281A (en) | 1930-01-30 | 1930-01-30 | Aluminum-silicon alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1934281A true US1934281A (en) | 1933-11-07 |
Family
ID=23683642
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US424726A Expired - Lifetime US1934281A (en) | 1930-01-30 | 1930-01-30 | Aluminum-silicon alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1934281A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2511551A (en) * | 1947-06-19 | 1950-06-13 | Cornell Aeronautical Labor Inc | Aluminium alloys |
| US2782493A (en) * | 1952-01-02 | 1957-02-26 | Kaiser Aluminium Chem Corp | Aluminum coated ferrous article |
| US4902475A (en) * | 1987-09-30 | 1990-02-20 | Metallurgical Products & Technologies, Inc. | Aluminum alloy and master aluminum alloy for forming said improved alloy |
| WO2007127724A3 (en) * | 2006-04-27 | 2008-01-24 | L & P Property Management Co | Sleep over recliner chair |
| US11130578B1 (en) * | 2019-10-24 | 2021-09-28 | B/E Aerospace, Inc. | Adjustable ottoman |
-
1930
- 1930-01-30 US US424726A patent/US1934281A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2511551A (en) * | 1947-06-19 | 1950-06-13 | Cornell Aeronautical Labor Inc | Aluminium alloys |
| US2782493A (en) * | 1952-01-02 | 1957-02-26 | Kaiser Aluminium Chem Corp | Aluminum coated ferrous article |
| US4902475A (en) * | 1987-09-30 | 1990-02-20 | Metallurgical Products & Technologies, Inc. | Aluminum alloy and master aluminum alloy for forming said improved alloy |
| WO2007127724A3 (en) * | 2006-04-27 | 2008-01-24 | L & P Property Management Co | Sleep over recliner chair |
| US11130578B1 (en) * | 2019-10-24 | 2021-09-28 | B/E Aerospace, Inc. | Adjustable ottoman |
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