US20120027639A1
2012-02-02
12/846,156
2010-07-29
An alloy for use in die casting having improved thermal conductivity and strength includes at least about 86.0 percent aluminum by weight, from about 9.70 to about 10.70 percent silicon, by weight, from about 0.40 to about 0.70 percent iron, by weight, about 0.25 percent copper, by weight, about 0.50 percent manganese, by weight, from about 0.10 to about 0.20 percent titanium, by weight; and from about 0.010 to about 0.025 percent strontium, by weight.
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C22C21/04 » CPC main
Alloys based on aluminium with silicon as the next major constituent Modified aluminium-silicon alloys
C22F1/043 » CPC further
Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
C22C21/02 IPC
Alloys based on aluminium with silicon as the next major constituent
The present invention relates generally to aluminum alloys and more specifically aluminum alloys for casting such as for pressure die-casting.
Die casting is a process in which molten metal is forced into metal dies under pressure to form dimensioned components that require little or no post processing. Aluminum is a widely used base for alloys in the casting of dimensional components. For example, aluminum alloys are used extensively in die-casting due to the excellent flow characteristics and dimensional stability achieved by aluminum alloys.
The use of various alloying agents to improve the strength, ductility, wear resistance, corrosion resistance, and thermal conductivity of aluminum may result in significant variations in the physical properties of the resulting alloy. The alloying agents also affect the ability of the resulting alloys to be die-cast successfully and with maintenance of the dimensional stability of the resulting parts. Various alloying agents are known to be used with aluminum. For example, copper, manganese, silicon, magnesium, zinc, and even iron, in some cases, may be used to form aluminum alloys with varying properties.
In addition, the resulting structures may be treated after the die casting process to modify physical characteristics. Coatings such as paint or anodize may improve the strength, wear resistance, and corrosion resistance of the final products. Various heat treatments may also be used to modify the mechanical properties of the parts after the die casting process has been completed.
Strontium is an elemental metal that reacts with water and burns in air. Strontium has been used in magnesium alloys which also include relatively small amounts of aluminum to form creep resistant magnesium based alloys. In such applications, the strontium is used to refine eutectic silicon. For example, U.S. Pat. No. 7,108,042 discloses that strontium, sodium, or calcium may be used to refine the eutectic silicon.
According to the present disclosure, an alloy for use in die casting has improved thermal conductivity and strength. The alloy includes at least about 86.0 percent aluminum by weight, from about 9.70 to about 10.70 percent silicon, by weight, from about 0.40 to about 0.70 percent iron, by weight, up to about 0.25 percent copper, by weight, up to about 0.50 percent manganese, by weight, from about 0.10 to about 0.20 percent titanium, by weight; and from about 0.010 to about 0.025 percent strontium, by weight.
The alloy may include up to about 90.0 percent aluminum. In some embodiments, the alloy may include up to about 0.30 percent magnesium, by weight. In some embodiments, the alloy may include impurities. For example, the alloy may include up to about 0.25 percent nickel, up to about 0.50 percent zinc, by weight, and up to about 0.15 percent tin by weight. The alloy may be used to produce articles of manufacture.
Additional features and advantages of the invention will become apparent to those skilled in the art upon consideration of the following detailed description of illustrated embodiments exemplifying the best mode of carrying out the invention as presently perceived.
The detailed description of the drawings particularly refers to the accompanying figures in which:
FIG. 1 is a graph comparing the thermal conductivity of alloy of the present disclosure to other alloys; and
FIG. 2 is a graph comparing the strength of the present alloy to aluminum 365.
The aluminum alloy of the present disclosure has been shown to provide improved thermal conductivity and strength over the A413 such that the new alloy provides mechanical properties that compare to the 365 alloy with a significantly lower cost. In the special 413 alloy of the present disclosure, hereinafter referred to as SP413, strontium is added in amounts between about 0.01 and 0.02% to modify silicon included in the alloy.
Strontium improves the tensile strength and the thermal conductivity of the SP413 as compared to the A413. A comparison of the thermal conductivity of several alloys is shown below in Table 1.
| TABLE 1 |
| THERMAL CONDUCTIVITY (W/K-m) |
| Heat | Die Cast | Die Cast | Die Cast | SP413 | SP413 |
| Treatment | 356 | 380 | A413 | w/o Sr | w/Sr |
| As cast | 143 | 96.2 | 121 | 144 | 150 |
| 300 F. | 144 | 97 | 124 | 147 | 150 |
| 400 F. | 145 | 104 | 127 | 155 | 156 |
| 500 F. | 148 | 116 | 130 | 158 | 165 |
| 600 F. | 145 | 119 | 131 | 159 | 163 |
The addition of Strontium also improves the yield strength of the SP413 alloy as shown in table 2.
| TABLE 2 | |||
| Tensile Strength | Yield Strength | ||
| Material | KSI(MPa) | KSI(MPa) | Elongation % |
| 413 As-Cast | 42.9(296) | 21.0(145) | 2.5 |
| SP413 As-Cast | 39.8(274) | 15.6(108) | 6.7 |
| SP413 As-Cast w/Sr | 44.6(308) | 17.7(122) | 9.9 |
| TABLE 3 | |||
| Tensile Strength | Yield Strength | ||
| Material | KSI(MPa) | KSI(MPa) | Elongation % |
| 365 As-Cast | 47.6(328) | 21.6(149) | 8.2 |
| SP413 As-Cast w/Sr | 44.6(308) | 17.7(122) | 9.9 |
The chemistry of each of the A413, SP413, and 365 alloys is presented in Table 4.
| TABLE 4 | ||
| ALLOY |
| ELEMENT | A413 | SP413 | 365 |
| Silicon (wt. %) | 11.0-13.0 | β9.70-10.70 | β9.5-11.5 |
| Iron (wt. %) | 1.30 | 0.40-0.70 | 0.15 |
| Copper (wt. %) | 1.00 | 0.25 | 0.03 |
| Manganese (wt. %) | 0.35 | 0.50 | 0.5-0.8 |
| Magnesium (wt. %) | 0.10 | 0.30 | 0.1-0.5 |
| Nickel (wt. %) | 0.50 | 0.25 | β |
| Zinc (wt. %) | 0.50 | 0.50 | 0.07 |
| Tin (wt. %) | 0.15 | 0.15 | β |
| Titanium (wt. %) | β | 0.10-0.20 | 0.04-0.15 |
| Strontium (wt. %) | β | 0.010-0.025 | 0.010-0.020 |
| Aluminum (wt. %) | 83.1-89.0 | 86.38-89.79 | 86.78-89.85 |
Thus, it can be seen that the SP413 alloy of the present disclosure provides an alloy having improved thermal conductivity and strength at a lower cost than known alloys. The combination of the improved thermal conductivity with improved strength provides a new option for the preparation of structural components in applications subjected to high thermal loads.
Although certain illustrative embodiments have been described in detail above, variations and modifications exist within the scope and spirit of this disclosure as described and as defined in the following claims.
1. An alloy for use in die casting comprising
at least about 86.0 percent aluminum by weight;
from about 9.70 to about 10.70 percent silicon, by weight;
from about 0.40 to about 0.70 percent iron, by weight;
up to about 0.25 percent copper, by weight;
up to about 0.50 percent manganese, by weight;
from about 0.10 to about 0.20 percent titanium, by weight; and
from about 0.010 to about 0.025 percent strontium, by weight.
2. The alloy of claim 1, further comprising up to about 0.25 percent nickel, by weight.
3. The alloy of claim 2, further comprising up to about 0.50 percent zinc, by weight.
4. The alloy of claim 3, further comprising up to about 0.15 percent tin, by weight.
5. The alloy of claim 2, further comprising up to about 0.15 percent tin, by weight.
6. The alloy of claim 1, further comprising up to about 0.15 percent tin, by weight.
7. The alloy of claim 6, further comprising up to about 0.50 percent zinc, by weight.
8. The alloy of claim 1, further comprising between about 86.0 to about 90.0 percent aluminum, by weight.
9. The alloy of claim 8, further comprising up to about 0.25 percent nickel, by weight.
10. The alloy of claim 9, further comprising up to about 0.50 percent zinc, by weight.
11. The alloy of claim 10, further comprising up to about 0.15 percent tin, by weight.
12. The alloy of claim 9, further comprising up to about 0.15 percent tin, by weight.
13. The alloy of claim 8, further comprising up to about 0.15 percent tin, by weight.
14. The alloy of claim 6, further comprising up to about 0.50 percent zinc, by weight.
15. An article of manufacturing comprising
between about 86.0 to about 90.0 percent aluminum, by weight;
from about 9.70 to about 10.70 percent silicon, by weight;
from about 0.40 to about 0.70 percent iron, by weight;
about 0.25 percent copper, by weight;
about 0.50 percent manganese, by weight;
from about 0.10 to about 0.20 percent titanium, by weight; and
from about 0.010 to about 0.025 percent strontium, by weight.
16. The alloy of claim 15, further comprising up to about 0.25 percent nickel, by weight.
17. The alloy of claim 16, further comprising up to about 0.50 percent zinc, by weight.
18. The alloy of claim 17, further comprising up to about 0.15 percent tin, by weight.
19. The alloy of claim 16, further comprising up to about 0.15 percent tin, by weight.
20. The alloy of claim 15, further comprising up to about 0.15 percent tin, by weight.
21. The alloy of claim 6, further comprising up to about 0.50 percent zinc, by weight.