US2931722A - Aluminum-titanium master alloys - Google Patents
Aluminum-titanium master alloys Download PDFInfo
- Publication number
- US2931722A US2931722A US623735A US62373556A US2931722A US 2931722 A US2931722 A US 2931722A US 623735 A US623735 A US 623735A US 62373556 A US62373556 A US 62373556A US 2931722 A US2931722 A US 2931722A
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- Prior art keywords
- alloys
- aluminum
- titanium
- master
- master alloys
- 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
- 229910045601 alloy Inorganic materials 0.000 title description 43
- 239000000956 alloy Substances 0.000 title description 43
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 title description 4
- 239000010936 titanium Substances 0.000 description 25
- 229910052719 titanium Inorganic materials 0.000 description 24
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 20
- 229910052782 aluminium Inorganic materials 0.000 description 18
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 18
- 229910018575 Al—Ti Inorganic materials 0.000 description 10
- 229910000838 Al alloy Inorganic materials 0.000 description 9
- 238000000034 method Methods 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 238000011084 recovery Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- 229910001018 Cast iron Inorganic materials 0.000 description 2
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- 229910052783 alkali metal Inorganic materials 0.000 description 2
- 150000001340 alkali metals Chemical class 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000007865 diluting Methods 0.000 description 2
- 229910000765 intermetallic Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052700 potassium Inorganic materials 0.000 description 2
- 239000011591 potassium Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 229910018137 Al-Zn Inorganic materials 0.000 description 1
- 229910018182 Al—Cu Inorganic materials 0.000 description 1
- 229910018573 Al—Zn Inorganic materials 0.000 description 1
- 229910018571 Al—Zn—Mg Inorganic materials 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000002585 base Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000006228 supernatant 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
Definitions
- Titanium is extensively used in aluminum alloys as a grain refining agent. For this purpose, it is added in amounts up to about 0.25% to alloys such as those of the Al-Zn, Al-Zn-Mg and Al-Cu types.
- a method used widely by producers of aluminum alloys for introducing the desired amount of titanium into the alloys has been the addition to the molten alloy of so-called master alloys containing 2V2%6% titanium with the remainder aluminum.
- master alloys have, prior to the present invention, been made by diluting a 50% Ti-50% Al alloy with molten aluminum at temperatures of 2200 F. to 2400 F.
- .It is an object of the present invention to provide Al-Ti master alloys containing from about 6% to 20% titanium which are readily soluble in aluminum and aluminum alloys at the desired working temperatures.
- Another object of the present invention is to provide Al-Ti master alloys containing from 6% to 20% 'tanium which have novel and useful structures.
- a further object of the present invention is to provide Al-Ti master alloys containing 6% to 20% titanium which are useful for the addition of titanium to aluminum and aluminum base alloys.
- Al-Ti master alloys containing about 6% to 20% titanium which are produced by a process of an entirely diiferent type not hitherto used for this purpose readily dissolve in molten aluminum and aluminum alloys at the normal working temperatures of 1300" F.-l400 F.
- These soluble master alloys it has been found, have a structure that is quite unlike the structure of Al-Ti alloys of similar composition formed by mixing the molten metals.
- novel master alloys of the present invention are produced by reacting an alkali-metal fiuotitanate such as K TiF with aluminum. While the precise reaction involved is not certain, it is believed that it may proceed v with some of thealuminu'm according to the following equation:
- the titanium thus liberated combines, of course, with aluminum to form the intermetallic compound Al Ti.
- Example I 46 parts of aluminum was melted in a graphite crucible and 25.5 parts of potassium fluotitanate (K TiF was added thereto in small increments with stirring, the temperature of the bath being maintained at about l500 F. or above. After all the K TiF was mixed in, the molten spent salt on top of the bath was ladled oil and the metal was poured into cast-iron ingot molds. The ingots thus produced were analyzed and found to contain 6.3% titanium.
- K TiF potassium fluotitanate
- Example 2 Aluminum parts was melted in a graphite crucible and brought to a temperature of 1600 F. To the molten metal there was added 50 parts of K TiF in increments with stirring after each addition. When the addition was completed the supernatant spent salt was decanted from the crucible and the metal was poured into cast iron ingot molds. Analysis of the ingots showed an 11.6% titanium content.
- Example 3 Forty parts of aluminum was placed in a graphite crucible and heated to 1300 F. Then 51 parts of K TiF was added, a little at a time, to the molten aluminum while maintaining the temperature. The .K TiF was stirred into the bath and when the addition was completed the crucible and contents were allowed to cool. The pig or ingot of metal removed from the cooled crucible was analyzed and 19.1% Ti was found.
- novel and improved Al-Ti master alloys which are quite useful as alloying addition agents. These novel master alloys are characterized by being readily soluble in molten aluminum and aluminum alloys at the normal working temperatures of 1300 F.-1400 F. with resulting high titanium recovery.
- Aluminum-titanium master alloys containing more than about 20% Ti can be produced by the process described above. However, excessively high temperatures are required since the melting points of such alloys are high. Their use is, therefore, not ordinarily practical.
- alkali metal fluotitanates may be used in making Al-T i master alloys according to the invention.
- Potassium fiuotitanate is preferred merely because of its greater availability.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
ALUMINUM-TITANIUM MASTER ALLOYS Stephen F. Urban, Kenmore, N.Y., assignor to National Lead Company, New York, N.Y., a corporation of New Jersey No Drawing. Application November 21, 1956 Serial No. 623,735
1' Claim. (Cl. 75-438)- This invention relates to aluminum-titanium alloys and is particularly concerned with such alloys in which the titanium content is between about 6% and about 20%.
Titanium is extensively used in aluminum alloys as a grain refining agent. For this purpose, it is added in amounts up to about 0.25% to alloys such as those of the Al-Zn, Al-Zn-Mg and Al-Cu types. A method used widely by producers of aluminum alloys for introducing the desired amount of titanium into the alloys has been the addition to the molten alloy of so-called master alloys containing 2V2%6% titanium with the remainder aluminum. These master alloys have, prior to the present invention, been made by diluting a 50% Ti-50% Al alloy with molten aluminum at temperatures of 2200 F. to 2400 F. Since this is a relatively expensive method of preparation and since, because of the low titanium content, they must be used in rather large amounts, such master alloys have not been entirely satisfactory commercially. Use of Al-Ti alloys of this type containing more than about 6% titanium has not been feasible because of the slow rates at which such alloys dissolve in molten aluminum and aluminum alloys at the preferred working temperatures of l300 F.-l400 F. and the low recoveries of dissolved titanium in the final alloys.
.It is an object of the present invention to provide Al-Ti master alloys containing from about 6% to 20% titanium which are readily soluble in aluminum and aluminum alloys at the desired working temperatures.
Another object of the present invention is to provide Al-Ti master alloys containing from 6% to 20% 'tanium which have novel and useful structures.
A further object of the present invention is to provide Al-Ti master alloys containing 6% to 20% titanium which are useful for the addition of titanium to aluminum and aluminum base alloys.
Other objects and advantages of the present invention will be apparent from the following description thereof.
It has been discovered that, unlike the master alloys discussed above, Al-Ti master alloys containing about 6% to 20% titanium which are produced by a process of an entirely diiferent type not hitherto used for this purpose readily dissolve in molten aluminum and aluminum alloys at the normal working temperatures of 1300" F.-l400 F. These soluble master alloys, it has been found, have a structure that is quite unlike the structure of Al-Ti alloys of similar composition formed by mixing the molten metals.
The difference in structure mentioned above is readily seen by comparison under the microscope of unetched specimens of the two types of alloys. In so examining Al-Ti master alloys made by the process of the present invention it will be observed that the intermetallic compound Al Ti appears as light particles which are relatively small and nodular or rounded in shape. In contrast, the Al Ti particles in an Al-Ti master alloy made by the previously used method of diluting a 50% Ti- 50% Al alloy with molten aluminum at temperatures between 2200' F. and 2400 F. are large and acicular or needle-like. This is found .to be the case even though the titanium contents ofthe two alloys are approximately identical. Moreover, it has been ascertained that the same ditierence in structure is found in alloys of the two types where the titanium contents range from approximately 20% down to about 6%, the Al Ti particles in alloys produced by the present process being present essentially in nodular or rounded form.
The novel master alloys of the present invention are produced by reacting an alkali-metal fiuotitanate such as K TiF with aluminum. While the precise reaction involved is not certain, it is believed that it may proceed v with some of thealuminu'm according to the following equation:
The titanium thus liberated combines, of course, with aluminum to form the intermetallic compound Al Ti.
The following examples illustrate the use of the abovedescribed method in producing novel Ai-Ti master alloys according to the present invention.
Example I 46 parts of aluminum was melted in a graphite crucible and 25.5 parts of potassium fluotitanate (K TiF was added thereto in small increments with stirring, the temperature of the bath being maintained at about l500 F. or above. After all the K TiF was mixed in, the molten spent salt on top of the bath was ladled oil and the metal was poured into cast-iron ingot molds. The ingots thus produced were analyzed and found to contain 6.3% titanium.
Example 2 Aluminum parts) was melted in a graphite crucible and brought to a temperature of 1600 F. To the molten metal there was added 50 parts of K TiF in increments with stirring after each addition. When the addition was completed the supernatant spent salt was decanted from the crucible and the metal was poured into cast iron ingot molds. Analysis of the ingots showed an 11.6% titanium content.
Example 3 Forty parts of aluminum was placed in a graphite crucible and heated to 1300 F. Then 51 parts of K TiF was added, a little at a time, to the molten aluminum while maintaining the temperature. The .K TiF was stirred into the bath and when the addition was completed the crucible and contents were allowed to cool. The pig or ingot of metal removed from the cooled crucible was analyzed and 19.1% Ti was found.
In tests of novel master alloys produced in accordance with the present invention it has been found that, when added to molten aluminum at temperatures of 1300 F.-- 1400 F., they dissolve readily and give high recoveries of dissolved titanium. In a number of such tests the dissolved titanium content of the finished aluminum alloys averaged of theoretical content based on the amount of master alloy added. Comparative tests employing master alloys containing from 6%20% Ti made by dilution of 50% Al-50% Ti alloys showed recoveries of between 20% and 10% (average 14%) of theoretical. Solution of the latter master alloys was very slow in all cases and in a test with such a master alloy containing 27% Ti the master alloy did not even melt.
It will be evident from the foregoing that by the present invention there are provided novel and improved Al-Ti master alloys which are quite useful as alloying addition agents. These novel master alloys are characterized by being readily soluble in molten aluminum and aluminum alloys at the normal working temperatures of 1300 F.-1400 F. with resulting high titanium recovery.
3 They also are characterized by the occurrence of the Al Ti of the alloy essentially in dispersed nodular particles instead of the essentially acicular form characteristic of known master alloys of similar compositions.
Aluminum-titanium master alloys containing more than about 20% Ti can be produced by the process described above. However, excessively high temperatures are required since the melting points of such alloys are high. Their use is, therefore, not ordinarily practical.
Likewise, of course, other alkali metal fluotitanates may be used in making Al-T i master alloys according to the invention. Potassium fiuotitanate is preferred merely because of its greater availability.
Where, in the specification and the appended claim, parts or percentages are stated or referred to, it is to be understood that these are parts or percentages by weight.
I claim:
An Al-Ti master alloy containing 6% to about 20% titanium with the balance substantially aluminum and characterized by being readily dissolved in aluminum at temperatures of 1300 F.l400 F. and by the appearance in said master alloy of the Al 'l'i constituent essentially in nodular particles.
References Cited in the file of this patent UNITED STATES PATENTS 451,404 Langley Apr. 28, 1891 451,405 Langley Apr. 28, 1891. 451,406 Langley Apr. 28, 1891 15 2,781,261 Kamlet Feb. 12, 1957
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US623735A US2931722A (en) | 1956-11-21 | 1956-11-21 | Aluminum-titanium master alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US623735A US2931722A (en) | 1956-11-21 | 1956-11-21 | Aluminum-titanium master alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2931722A true US2931722A (en) | 1960-04-05 |
Family
ID=24499212
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US623735A Expired - Lifetime US2931722A (en) | 1956-11-21 | 1956-11-21 | Aluminum-titanium master alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2931722A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3104252A (en) * | 1958-12-29 | 1963-09-17 | Continental Oil Co | Preparation of organoaluminum compounds in the presence of a catalytic amount of ti, zr, nb, v, sc, u, or hf |
| US3180728A (en) * | 1960-10-03 | 1965-04-27 | Olin Mathieson | Aluminum-tin composition |
| US3391999A (en) * | 1964-08-17 | 1968-07-09 | Texaco Inc | Preparation of metal aluminides |
| US3503738A (en) * | 1967-09-15 | 1970-03-31 | Hugh S Cooper | Metallurgical process for the preparation of aluminum-boron alloys |
| US3857705A (en) * | 1972-02-14 | 1974-12-31 | Nippon Light Metal Res Labor | Small grain promoting aluminum-titanium-boron mother alloy |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US451404A (en) * | 1891-04-28 | Process of manufacturing alloys of aluminium | ||
| US451406A (en) * | 1891-04-28 | Alloy | ||
| US451405A (en) * | 1891-04-28 | Aluminium alloy | ||
| US2781261A (en) * | 1953-10-30 | 1957-02-12 | Nat Distillers Prod Corp | Process for the manufacture of titanium-aluminum alloys and regeneration of intermediates |
-
1956
- 1956-11-21 US US623735A patent/US2931722A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US451404A (en) * | 1891-04-28 | Process of manufacturing alloys of aluminium | ||
| US451406A (en) * | 1891-04-28 | Alloy | ||
| US451405A (en) * | 1891-04-28 | Aluminium alloy | ||
| US2781261A (en) * | 1953-10-30 | 1957-02-12 | Nat Distillers Prod Corp | Process for the manufacture of titanium-aluminum alloys and regeneration of intermediates |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3104252A (en) * | 1958-12-29 | 1963-09-17 | Continental Oil Co | Preparation of organoaluminum compounds in the presence of a catalytic amount of ti, zr, nb, v, sc, u, or hf |
| US3180728A (en) * | 1960-10-03 | 1965-04-27 | Olin Mathieson | Aluminum-tin composition |
| US3391999A (en) * | 1964-08-17 | 1968-07-09 | Texaco Inc | Preparation of metal aluminides |
| US3503738A (en) * | 1967-09-15 | 1970-03-31 | Hugh S Cooper | Metallurgical process for the preparation of aluminum-boron alloys |
| US3857705A (en) * | 1972-02-14 | 1974-12-31 | Nippon Light Metal Res Labor | Small grain promoting aluminum-titanium-boron mother alloy |
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