Claims
- 1. A method of forming an aluminum alloy product having preferred mechanical properties, comprising:(a) providing a metal matrix of aluminum; (b) providing said metal matrix in a liquid state containing a liquid titanium; (c) reacting a salt bath containing a carbon with said liquid titanium element to form a uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix; and (d) providing an aluminum alloy product having preferred mechanical properties formed from said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix, wherein said providing an aluminum alloy product having preferred mechanical properties comprises providing an uncrystallized structure during a deformation operation.
- 2. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 1, comprising increasing dispersion strengthening in said aluminum alloy product having preferred mechanical properties.
- 3. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 1, wherein said uniform distribution consists of a substantially cluster-free distribution of no more than two particles attached to one another at a magnification of 500×.
- 4. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 3, wherein said finely sized ceramic phase particles have an average particle diameter of less than about 2.5 microns.
- 5. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 4, wherein said finely sized ceramic phase particles comprise titanium carbide particles having an average particle diameter of less than about 1 micron formed and dispersed in situ in said aluminum metal matrix.
- 6. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 5, wherein said finely sized ceramic phase particles comprise titanium carbide particles having an average particle diameter of less than about 0.3 micron formed and dispersed in situ in said aluminum metal matrix.
- 7. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 6, wherein said reacting step comprises vigorously stirring to form a mixture of said liquid titanium in contact with a portion of said carbon particles at an elevated temperature for sufficient residence time to form said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ in said metal matrix.
- 8. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 6, wherein said reacting a salt bath containing a carbon with said liquid titanium element comprises reacting a halide salt containing carbon particles in said molten metal or metal alloy with said carbide-forming titanium liquid to form said uniform distribution of finely sized ceramic phase particles formed and dispersed in-situ in a metal matrix.
- 9. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 6, wherein said aluminum alloy product having preferred mechanical properties comprises a high strength, light weight aluminum alloy having a high strength to weight ratio.
- 10. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 6, wherein said aluminum alloy product having preferred mechanical properties comprises an aluminum airframe.
- 11. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 6, wherein said preferred mechanical properties comprise a property selected from the group consisting of increased recrystallization temperature, decreased grain growth in hot working, and elevated temperature strength.
- 12. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 2, wherein said uniform distribution consists of a substantially cluster-free distribution of no more than two particles attached to one another at a magnification of 500×.
- 13. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 12, wherein said finely sized ceramic phase particles have an average particle diameter of less than about 2.5 microns.
- 14. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 13, wherein said finely sized ceramic phase particles comprise titanium carbide particles having an average particle diameter of less than about 1 micron formed and dispersed in situ in said aluminum metal matrix.
- 15. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 14, wherein said finely sized ceramic phase particles comprise titanium carbide particles having an average particle diameter of less than about 0.3 micron formed and dispersed in situ in said aluminum metal matrix.
- 16. A method of forming an aluminum alloy product having preferred mechanical properties formed by the process of claim 15, wherein said reacting step comprises vigorously stirring to form a mixture of said liquid titanium in contact with a portion of said carbon particles at an elevated temperature for sufficient residence time to form said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ in said metal matrix.
- 17. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 15, wherein said reacting a salt bath containing a carbon with said liquid titanium element comprises reacting a halide salt containing carbon particles in said molten metal or metal alloy with said carbide-forming titanium liquid to form said uniform distribution of finely sized ceramic phase particles formed and dispersed in-situ in a metal matrix.
- 18. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 15, wherein said aluminum alloy product having preferred mechanical properties comprises a high strength light weight aluminum alloy having a high strength to weight ratio.
- 19. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 15, wherein said aluminum alloy product having preferred mechanical properties comprises an aluminum airframe.
- 20. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 15, wherein said preferred properties comprise a property selected from the group consisting of increased recrystallization temperature, decreased grain growth in hot working, and elevated temperature strength.
- 21. A method of forming an aluminum alloy product having preferred mechanical properties as set forth in claim 1, wherein said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix provide increased nuclei for grain refining in said aluminum metal matrix.
- 22. A method of forming an aluminum alloy product having preferred mechanical properties, comprising:(a) providing a metal matrix of aluminum; (b) providing said metal matrix in a liquid state containing a liquid titanium; (c) reacting a salt bath containing a carbon with said liquid titanium element by vigorously stirring to form a mixture of said liquid titanium in contact with a portion of said carbon particles at an elevated temperature for sufficient residence time to form a uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix, wherein said uniform distribution consists of a substantially cluster-free distribution of no more than two particles attached to one another at a magnification of 500× at an average particle diameter of less than about 0.3 micron formed and dispersed in situ in said aluminum metal matrix; (d) providing an uncrystallized structure during a deformation operation to form an aluminum alloy product having preferred mechanical properties; and (f) forming a high strength, light weight aluminum alloy airframe product from said aluminum alloy product having preferred mechanical properties, wherein said high strength, light weight aluminum alloy airframe product exhibits a high strength to weight ratio, increased recrystallization temperature, decreased grain growth in hot working, and elevated temperature strength.
- 23. A method of forming an aluminum alloy product having preferred mechanical properties, comprising:(a) providing a metal matrix of aluminum; (b) providing said metal matrix in a liquid state containing a liquid titanium; (c) reacting a salt bath containing a carbon with said liquid titanium element by vigorously stirring to form a mixture of said liquid titanium in contact with a portion of said carbon particles at an elevated temperature for sufficient residence time to form a uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix, wherein said uniform distribution consists of a substantially cluster-free distribution of no more than two particles attached to one another at a magnification of 500× at an average particle diameter of less than about 0.3 micron formed and dispersed in situ in said aluminum metal matrix; (d) providing an aluminum alloy having preferred mechanical properties formed from said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix; (e) increasing dispersion strengthening in said aluminum alloy product to form an aluminum alloy product having preferred mechanical properties; and (f) forming a high strength, light weight aluminum alloy airframe product from said aluminum alloy product having preferred mechanical properties, wherein said high strength, light weight aluminum alloy airframe product exhibits a high strength to weight ratio, increased recrystallization temperature, decreased grain growth in hot working, and elevated temperature strength.
- 24. A method of forming an aluminum alloy product having preferred mechanical properties, comprising:(a) providing a metal matrix of aluminum; (b) providing said metal matrix in a liquid state containing a liquid titanium; and (c) reacting a salt bath containing a carbon with said liquid titanium element by vigorously stirring to form a mixture of said liquid titanium in contact with a portion of said carbon particles at an elevated temperature for sufficient residence time to form a uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix, wherein said uniform distribution consists of a substantially cluster-free distribution of no more than two particles attached to one another at a magnification of 500× at an average particle diameter of less than about 0.3 micron formed and dispersed in situ in said aluminum metal matrix; (d) wherein said uniform distribution of finely sized titanium carbide ceramic phase particles formed and dispersed in-situ uniformly in said aluminum metal matrix provide increased nuclei for grain refining in said aluminum metal matrix.
Parent Case Info
This patent application is a continuation-in-part of prior, U.S. patent application Ser. No. 09/053,033, filed Apr. 1, 1998, now U.S. Pat. No. 6,036,792. Continuation-in-part of application Ser. No. 08/594,966, Jan. 31, 1996, U.S. Pat. No. 5,735,976.
US Referenced Citations (6)
Continuation in Parts (2)
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Number |
Date |
Country |
Parent |
09/053035 |
Apr 1998 |
US |
Child |
09/523883 |
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US |
Parent |
08/594966 |
Jan 1996 |
US |
Child |
09/053035 |
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US |