Claims
- 1. In a method of continuously casting molten aluminum and hot forming said cast metal in substantially its as-cast condition at a hot-forming temperature by a plurality of substantial compressions, the improvement comprising the steps of:
- following casting of said metal and prior to said substantial compression of said metal, forming a substantially uniform subgrain structure at least at the surface of said metal by at least one preliminary light compression of said metal wherein said metal is selected from the group consisting of aluminum and aluminum alloys.
- 2. The method of claim 1 wherein said preliminary light compression reduces the cross-section of said metal by between 5 and 25%.
- 3. The method of claim 1, wherein said substantial compressions following the forming of said substantially uniform subgrain structure includes a first compression providing at least 30% reduction of the cross-section of said metal.
- 4. The method of claim 1 wherein said light compressions comprise a first 7% reduction of the cross-section of said metal followed by a second 7% reduction along an axis of compression 90.degree. removed from said first 7% reduction.
- 5. The method of claim 1 wherein said light compressions comprise a first 7% reduction of the cross-section of said metal followed by at least one additional 7% reduction along an axis of compression 60.degree. removed from the axis of said immediately prior 7% reduction.
- 6. The method of claim 1, wherein the total of said light compressions results in less than a 30% reduction of the cross-section of said metal.
- 7. The method of claim 1 wherein said metal is a 2000 series aluminum alloy.
- 8. The method of claim 1 wherein said metal is a 7000 series aluminum alloy.
- 9. The method of claim 1 wherein said metal is a 6000 series aluminum alloy.
- 10. The method of claim 1 wherein said metal is a 5000 series aluminum alloy.
- 11. The method of claim 7 wherein said metal is 2024 aluminum alloy.
- 12. The method of claim 7 wherein said metal is 2117 aluminum alloy.
- 13. The method of claim 8 wherein said metal is 7075 aluminum alloy.
- 14. The method of claim 8 wherein said metal is 7079 aluminum alloy.
- 15. The method of claim 9 wherein said metal is 6061 aluminum alloy.
- 16. The method of claim 9 wherein said metal is 6101 aluminum alloy.
- 17. The method of claim 9 wherein said metal is 6201 aluminum alloy.
- 18. The method of claim 10 wherein said metal is 5052 aluminum alloy.
- 19. The method of claim 10 wherein said metal is 5056 aluminum alloy.
- 20. A method of hot forming a continuously cast aluminum bar without cracking said bar comprising the steps of:
- passing said bar in substantially its as-cast condition and at a hot-forming temperature from a continuous casting machine to a hot-forming means;
- conditioning said bar for subsequent hot forming by forming a substantially uniform subgrain structure at least at the surface of said bar by a plurality of preliminary light sequential compressions of said bar each reducing the cross-section of said bar by from 5% to 25% each and a total reduction of less than 30%;
- hot forming said bar by a single compression of said bar to reduce its cross-sectional area by at least 40%; and
- hot forming said bar by a plurality of sequential compressions in each of which the cross-section of said bar is changed to the extend necessary to provide a hot-formed product having a predetermined cross-section.
- 21. The method of claim 20 wherein said conditioning of said bar includes passing said bar between rolls in a plurality of sequential roll stands.
- 22. The method of claim 21 wherein said hot forming of said bar includes passing said bar through sequential roll stands of a rolling mill.
CROSS REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of co-pending application Ser. No. 80,368, filed Oct. 1, 1979, now U.S. Pat. No. 4,352,697.
US Referenced Citations (7)
Foreign Referenced Citations (1)
Number |
Date |
Country |
49930 |
Apr 1979 |
JPX |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
80368 |
Oct 1979 |
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