GB2174103A - Grain refiner for aluminum containing silicon - Google Patents
Grain refiner for aluminum containing silicon Download PDFInfo
- Publication number
- GB2174103A GB2174103A GB08605589A GB8605589A GB2174103A GB 2174103 A GB2174103 A GB 2174103A GB 08605589 A GB08605589 A GB 08605589A GB 8605589 A GB8605589 A GB 8605589A GB 2174103 A GB2174103 A GB 2174103A
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- United Kingdom
- Prior art keywords
- alloy
- aluminum
- ratio
- grain
- alloys
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
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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)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Abstract
Disclosed is an Al-Ti-B master alloy consisting of 0.1 to 9.8% Ti, 0.1 to 7% Boron balance Aluminium plus impurities designed to grain refine cast aluminum alloys containing silicon. The alloy composition goes contrary to present known art. Present commercial master alloys contain a ratio of Ti to B exceeding 2.2 to promote a mixture of TiB2 and TiAl3 crystals. This invention provides an Al-Ti-B alloy wherein the Ti to B ratio is between 0.1 and 2.1. It contains a preponderance of mixed boride crystals. The optimum composition of the alloy of this invention is Al-3Ti-3B.
Description
SPECIFICATION
Grain refiner for aluminum containing silicon
This invention relates to aluminum-titanium-boron grain refiners that are used to control the grain size of aluminum and its alloys during solidification. More particularly, it relates to a grain refiner especially suited for aluminum casting alloys containing silicon.
Grain refiners for aluminum castings generally contain titanium and boron in an aluminum base.
Examples of these refiners may be found disclosed in U.S. Patents Nos. 3,785,807, 3,857,705,4,298,408 and 3,634,075. U.S. Patent No. 3,676,111 discloses a method of refining aluminum base alloys by means of separate additions of boron and titanium. The invention teaches that (1) boron must be added to the aluminum base alloy, then (2) titanium is added with additional boron as may be required. Examples and suggestions of master alloy compositions for the titanium and boron additions in step (2) are limited to the well known Al-3%B alloy and Al-5% Ti-1%B master alloys. The final cast alloy contains a Ti:B ratio between 1.4 and 2.2.
The subject of the best titanium-to-boron ratio for grain refinement of aluminum has been the subject of several studies. Cornish1, Miyasaka and Namekawa2, and Pearson and Birch3 have all studied the question and concluded that the Ti; B ratio must be greater than 2.2 (the stoichiometric value for TiB2) for grain refinement to occur. The results are perhaps most clearly shown in Figure 1, which is reproduced from
Cornish's paper1. The dark circles represent grain refiner alloy compositions that grain refined well in high purity aluminum. Open circles represent ineffective alloys.
A.J. Cornish: Metal Science, 1975, Vol. 9, pg. 477-484.
2 Y. y Miyasaka & Y. Namekawa: Light Metals, 1975, pg. 197-211, AIME, New York 1975.
3 J. Pearson and M.E. J. Birch, Light Metals, 1984, pg. 1217-1229, AIME, New York, 1984.
These patents and literature references relate to various modifications of titanium-boron contents together with additional elements or certain processing steps.
The effectiveness of grain refinement is somewhat dependent upon the composition of the aluminum grain refiner and also the aluminum alloy being refined. For example, the most useful commercial aluminum-base grain refiners generaily contain a titanium-to-boron ratio greater than about three. In practice, it was sometimes found that the effectiveness of these commercial grain refiners was erratic and not predictable. Thus, it was necessary to determine the cause and effect of this problem. It was found, however, that such standard commercial grain refiners were ineffective when used in casting aluminum alloys containing about one percent or more of dissolved silicon. It appears that the higher silicon contents found in casting alloys somehow interferes with the effect of titanium, and promotes that of boron, as a grain refiner.
A report entitled "lnfluence of Grain Refiner Master Alloy Addition on A-356 Aluminum Alloy" published in the Journal of the Chinese Foundryman's Association, June1981, Viol.29, pg. 10-18, discloses results of an investigation of this subject. Casting Alloy A-356 contains 6.5 to 7.5 percent silicon, 0.2 to 0.4% magnesium, less than 0.2% each of iron and titanium and the balance aluminum plus normal low-level impurities. The
Chinese investigation determined that an Al-4%B alloy was the best grain refiner for A-356 alloy, followed by Al-5%Ti-1%B alloy; then by AI-5% Ti alloy as the poorest grain refiner. Figure 2 is a graphic presentation of the data.
The Cornish reference discloses a graphic relationship of Ti to B ratio. Figure 1, herein, shows the result of the Cornish reference. The conclusions clearly teach that the ratio of Ti to B must be more than about 2 for effective results. All tests of alloys at a ratio of 1.48 indicated poor grain refinement (coarse grains). The best grain refiners were found to be with Ti to B ratios above 2.22 which is the stoichiometric proportion of TiB2.
Figure 1 clearly shows this teaching.
The Pearson and Birch literature reference also teaches the Ti to B ratio to beoverthestoichimetricvalue of 2.22. A grain refiner containing 3%Ti-1 %B is reported to be the optimum composition.
Thus, the results of the Chinese study made in the Al-7%Si casting alloy (A-356) run counter to the results of Cornish1 and Pearson and Birch3 for higher purity (low Si) aluminum. In our own laboratory studies, we have cofirmed the results of the Chinese experiments, but plant trials of the Al-4%B alloy gave many problems. So, it seemed as if there were no satisfactory grain refiners for the high silicon content aluminum casting alloys.
It is an object of this invention to provide a master alloy especially suitable for grain refining siliconscontaining aluminum alloys.
Another object is to provide a master alloy that may be readily produced by processes known in the art.
Other objects may. be discerned by those skilled in the art from subsequent descriptions of the invention, figures and examples.
Summary ofthe invention
The present invention provides a novel aluminum-titanium-boron master alloy that grain refines aluminum-silicon alloys more uniformly. Table 1 presents the composition ranges of the alloy of this invention. Ternary Al-Ti-B master alloys are well known in the art and the science of aluminum grain refining.
The gist of this invention resides in the critical ratio of Ti to B required to obtain grain refinement in aluminum alloys containing silicon.
The compositions in Table 1 contain aluminum plus impurities as balance. In the production of aluminum master alloys of this class, impurities from many sources are found in the final product. These so-called "impurities" are not necessarily always harmful and some may actually be beneficial or have an innocuous effect, for example, iron and copper.
Some of the "impurities" may be present as residual elements resulting from certain processing steps, or adventitiously present in the charge materials: for example, silicon, manganese, sodium, lithium, calcium, magnesium, vanadium, zinc, and zirconium.
In actual practice, certain impurity elements are kept within established limits with maximum and/or minimum to obtain uniform products as well known in the art and skill of melting and processing thse alloys.
Sodium, lithium, calcium, zinc, and zirconium must generally be kept at the lowest possible levels.
Thus, the alloy of this invention may contain these and other impurities, within the limits usually associated with alloys of this class.
Although the exact mechanism of the invention is not completely understood, it is believed that the required control of the titanium-to-boron ratio provides the proper balance of mixed aluminum and titanium borides that is essential to effectively grain refine aluminum alloys containing silicon.
TABLE 1
Alloy of this invention
Composition, in weight percent
Broad Range Intermediate Range Preferred Range
Titanium .1 to 9.8 1.5 to 7 2.5 to 3.5
Boron .1 to 7.0 1.5 to 7 2.5 to 3.5
Aluminum plus impurities Balance Balance Balance Ratio Ti:B 0.1 to 2.1 0.25 to 1.8 0.7 to 1.4 Total AIB2 + TiB2 > 50% > 75% > 90% Examples
Five heats of experimental alloys were made by reacting a salt mixture of KBF4 and K2TiF6 with molten aluminum. This salt mixture is called a "flux" herein. Three flux compositions and three different reaction temperatures were employed, as shown in table 2 together with the compositions of the Al-Ti-B alloys made from the reaction.
TABLE 2
Flux Ratio and Alloy Composition 40%K2Ti F6/60%KBF4 20%K2TiF6/80%KB F4 10%K2Ti F6/90%KB F4 Reaction
Temp. (2.8%Ti-1.8%B) (1.4%Ti-2.4%B) (0.7%Ti-2.7%B) 725"C Heat -29 Heat -31 Heat -39 800"C Heat -37 850"C Heat -40
The experimental alloys were used as grain refiners for an AI-7%Si alloy. Each was generally effective as grain refiners. However, Heats 29,40,31 and 37 were outstanding because the products had cleaner microstructures. Table 3 presents a tabular display of the test results.
TABLE 3
Heat No. Approx. Ti:B ratio Effectiveness
29 1.5:1 excellent
40 1.5:1 excellent
31 0.6:1 excellent
37 0.6:1 excellent
39 1:4 poorest
Another series of alloys was prepared to examine the effect of other flux ratios. Table 4 presents the flux ratios and reaction temperatures employed.
TABLE 4
Flux Ratio Reaction
Heat No. (%K2TiF6/%KBF4) Temperature
54 25/75 760 C (1400"F)
55 15/85 760 C (1400 F) 56 30/70 760 C (1400 F)
48 20/80 800 C (1472 F) Atest of the grain refining effectiveness of these Al-Ti-B master alloys in cast aluminum-7% silicon alloy revealed that Heat No. 56 was the outstanding master alloy of this entire series. Heat 56 has a 30:70 flux ratio and a reaction temperature of 760 C.
Results of the two series of tests suggest that the best practice of the invention lies between 0.7:1 and 1.4:1 ratios (preferably 1:1 ratio) of Ti: B and a flux ratio of 30:70. To verify this conclusion a 45.4 Kg (100 Ib) experimental alloy (No. 3-40) was made and tested. This alloy contained 3.1% titanium and 3.2% boron. It was produced by reacting a 30:70 flux ratio at a temperature of 760 C (14000F) as indicated for alloy 56 described above.
Alloy 3-40 was used to refine the grain of commercial alloy no.356, which contains 7%Si, .3% Mg, .1% Fe, and .02% Ti. The casting temperature was 7250C (1350 F) and the time the grain refiner was in contact with the melt before casting was 5 minutes.
Prior art alloys, 5%Ti-1 %B, and Al-3%B were used under the same conditions as the experimental alloy 3-40. Results of the test are shown graphically in Figure 3. The average grain size of the prior art alloys are plotted as curve (a); the average grain size of alloy 3-40 is plotted as curve (b). Clearly, these data show the alloy of this invention to be superior over the prior art alloys.
In further testing, commercial aluminum alloy no.319 (which contains 6%Si, 3.5%Cu, 1%Fe, 1%Zn and 0.5%Mn) was also grain refined by the three master alloys mentioned above. Figure 4 is a graphic presentation of the test results. Here, also the alloy of this invention alloy (No. 3-40) was superior over the prior art alloys. Prior art alloy 5%Ti-1%B is a well known commercial master alloy with a Ti to B ratio of 5:1.
A metallographic study of all master alloys described above was made. The alloy described in this invention contained a preponderance of mixed aluminum and titanium borides, that is from 50% to over 90% mixed borides. This is in contradiction with the known art which teaches that solely titanium boride phases (especially TiB2) and titanium aluminides (TiAl3) are preferred.
Claims (8)
1. A master alloy chatacterised by being capable of grain refining aluminum alloys containing silicon consisting of, in weight percent, 0.1 to 9.8 titanium. 0.1 to 7 boron, and the balance aluminum plus impurities wherein the Ti:B ratio is between 0.1 to 2.1 to provide at least 50% mixed borides in the grain refined aluminum alloy casting.
2. The master alloy of claim 1, containing 1.5 to 7.0 titanium and 1.5 to 7.0 boron, and having a Ti.B ratio from 0.25 to 1.8.
3. The master alloy of claim 1, containing Al 3%Ti-3%B.
4. The master alloy of claim 1,wherein the ratio of Ti: B is between 0.25 to 1.8.
5. The master alloy of claim 4 wherein the ratio of Ti:B is 1.
6. An aluminum alloy casting grain refined with the master alloy of claim 1 and containing over 75% mixed aluminum and titanium borides.
7. The alloy of claim 6 containing over 90% mixed borides.
8. The alloy of claim 6 containing at least 1% silicon.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US71532885A | 1985-03-25 | 1985-03-25 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8605589D0 GB8605589D0 (en) | 1986-04-09 |
GB2174103A true GB2174103A (en) | 1986-10-29 |
GB2174103B GB2174103B (en) | 1989-06-21 |
Family
ID=24873591
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8605589A Expired GB2174103B (en) | 1985-03-25 | 1986-03-06 | Grain refiner for aluminum containing silicon |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS61223156A (en) |
BR (1) | BR8600976A (en) |
CA (1) | CA1277855C (en) |
DE (1) | DE3608713A1 (en) |
FR (1) | FR2579227B1 (en) |
GB (1) | GB2174103B (en) |
NL (1) | NL8600394A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0553533A1 (en) * | 1992-01-08 | 1993-08-04 | Elkem Aluminium Ans | Method for grain refining of aluminium and grain refining alloy |
EP0601972A1 (en) * | 1992-12-07 | 1994-06-15 | ALUMINIUM RHEINFELDEN GmbH | Grain refining agent for cast aluminium alloys especially cast aluminium-silicon alloys |
WO2005056846A1 (en) * | 2003-12-02 | 2005-06-23 | Worcester Polytechnic Institute | Casting of aluminum based wrought alloys and aluminum based casting alloys |
RU2644221C1 (en) * | 2016-12-27 | 2018-02-08 | Общество с ограниченной ответственностью "Безотходные и малоотходные технологии" (ООО "БМТ") | Aluminium-titanium-boron master alloy |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1264903B1 (en) * | 2001-06-07 | 2006-09-20 | Bayerische Motoren Werke Aktiengesellschaft | Refining of aluminium casting alloys by boron addition |
TR200504376A2 (en) * | 2005-11-02 | 2008-05-21 | T�B�Tak-T�Rk�Ye B�L�Msel Ve Tekn�K Ara�Tirma Kurumu | A process for producing grain-reducing pre-alloys |
JP6011998B2 (en) * | 2012-12-25 | 2016-10-25 | 日本軽金属株式会社 | Method for producing aluminum alloy in which Al-Fe-Si compound is refined |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1244082A (en) * | 1968-03-13 | 1971-08-25 | Kawecki Berylco Ind | Improvements in introducing a grain refining or alloying agent into molten metals and alloys |
US3676111A (en) * | 1971-03-01 | 1972-07-11 | Olin Corp | Method of grain refining aluminum base alloys |
US3785807A (en) * | 1970-04-28 | 1974-01-15 | Graenges Aluminium Ab | Method for producing a master alloy for use in aluminum casting processes |
US3857705A (en) * | 1972-02-14 | 1974-12-31 | Nippon Light Metal Res Labor | Small grain promoting aluminum-titanium-boron mother alloy |
GB1452165A (en) * | 1973-04-04 | 1976-10-13 | Pechiney Aluminium | Aluminiu-titanium-boron mother alloy and a process for its production |
GB2067222A (en) * | 1980-01-07 | 1981-07-22 | Cabot Berylco Inc | Aluminium-titanium-boron master alloy |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1041695B (en) * | 1955-03-29 | 1958-10-23 | Metallgesellschaft Ag | Grain refinement of cast aluminum |
GB802071A (en) * | 1957-04-15 | 1958-10-01 | Kawecki Chemical Company | Improvements in aluminium-base alloys |
-
1986
- 1986-02-17 NL NL8600394A patent/NL8600394A/en not_active Application Discontinuation
- 1986-03-06 GB GB8605589A patent/GB2174103B/en not_active Expired
- 1986-03-06 BR BR8600976A patent/BR8600976A/en not_active IP Right Cessation
- 1986-03-15 DE DE19863608713 patent/DE3608713A1/en not_active Ceased
- 1986-03-17 CA CA000504223A patent/CA1277855C/en not_active Expired - Lifetime
- 1986-03-19 JP JP6193486A patent/JPS61223156A/en active Granted
- 1986-03-24 FR FR8604191A patent/FR2579227B1/en not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1244082A (en) * | 1968-03-13 | 1971-08-25 | Kawecki Berylco Ind | Improvements in introducing a grain refining or alloying agent into molten metals and alloys |
US3785807A (en) * | 1970-04-28 | 1974-01-15 | Graenges Aluminium Ab | Method for producing a master alloy for use in aluminum casting processes |
US3676111A (en) * | 1971-03-01 | 1972-07-11 | Olin Corp | Method of grain refining aluminum base alloys |
US3857705A (en) * | 1972-02-14 | 1974-12-31 | Nippon Light Metal Res Labor | Small grain promoting aluminum-titanium-boron mother alloy |
GB1452165A (en) * | 1973-04-04 | 1976-10-13 | Pechiney Aluminium | Aluminiu-titanium-boron mother alloy and a process for its production |
GB2067222A (en) * | 1980-01-07 | 1981-07-22 | Cabot Berylco Inc | Aluminium-titanium-boron master alloy |
US4298408A (en) * | 1980-01-07 | 1981-11-03 | Cabot Berylco Inc. | Aluminum-titanium-boron master alloy |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0553533A1 (en) * | 1992-01-08 | 1993-08-04 | Elkem Aluminium Ans | Method for grain refining of aluminium and grain refining alloy |
US5424031A (en) * | 1992-01-08 | 1995-06-13 | Elkem Aluminium Ans | Grain refining alloy and a method for grain refining of aluminum and aluminum alloys |
US5582791A (en) * | 1992-01-08 | 1996-12-10 | Elkem Aluminum Ans | Method for grain refining of aluminum and grain refining alloy |
EP0601972A1 (en) * | 1992-12-07 | 1994-06-15 | ALUMINIUM RHEINFELDEN GmbH | Grain refining agent for cast aluminium alloys especially cast aluminium-silicon alloys |
WO2005056846A1 (en) * | 2003-12-02 | 2005-06-23 | Worcester Polytechnic Institute | Casting of aluminum based wrought alloys and aluminum based casting alloys |
US7201210B2 (en) | 2003-12-02 | 2007-04-10 | Worcester Polytechnic Institute | Casting of aluminum based wrought alloys and aluminum based casting alloys |
RU2644221C1 (en) * | 2016-12-27 | 2018-02-08 | Общество с ограниченной ответственностью "Безотходные и малоотходные технологии" (ООО "БМТ") | Aluminium-titanium-boron master alloy |
Also Published As
Publication number | Publication date |
---|---|
FR2579227B1 (en) | 1988-11-25 |
GB8605589D0 (en) | 1986-04-09 |
CA1277855C (en) | 1990-12-18 |
FR2579227A1 (en) | 1986-09-26 |
DE3608713A1 (en) | 1986-10-09 |
NL8600394A (en) | 1986-10-16 |
JPS61223156A (en) | 1986-10-03 |
GB2174103B (en) | 1989-06-21 |
JPH0159345B2 (en) | 1989-12-15 |
BR8600976A (en) | 1986-11-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19970306 |