Aluminum alloy heat exchanger for exhaust gas recirculation system
US-2021025663-A1 · Jan 28, 2021 · US
US11591674B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11591674-B2 |
| Application number | US-202017065995-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 8, 2020 |
| Priority date | Oct 9, 2019 |
| Publication date | Feb 28, 2023 |
| Grant date | Feb 28, 2023 |
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An aluminum-alloy sheet has a chemical composition containing Si: 2.3-3.8 mass %, Mn: 0.35-1.05 mass %, Mg: 0.35-0.65 mass %, Fe: 0.01-0.45 mass %, and at least one element selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %. The ratio of the Si content to the Mn content is 2.5 or more and 9.0 or less. The aluminum-alloy sheet exhibits an elongation of 23% or more and a strain hardening exponent of 0.28 or more at a nominal strain of 3%. Such an aluminum-alloy sheet is well suited for press forming (stamping) applications, such as forming automobile body panels.
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We claim: 1. An aluminum-alloy sheet comprising: Si: 2.3-3.8 mass %, Mn: 0.35-1.05 mass %, Mg: 0.35-0.65 mass %, Fe: 0.01-0.45 mass %, and at least one element selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %, wherein the aluminum-alloy sheet has an Si/Mn mass ratio of 3.0-9.0, an elongation of at least 23%, and a strain hardening exponent of at least 0.28 at a nominal strain of 3%. 2. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet further contains Ni: 0.0050-0.15 mass %. 3. The aluminum-alloy sheet according to claim 2 , wherein the strain hardening exponent is at least 0.29 at a nominal strain of 3%. 4. The aluminum-alloy sheet according to claim 3 , wherein the aluminum-alloy sheet has a Cu content of 0.0010-0.20 mass %. 5. The aluminum-alloy sheet according to claim 3 , wherein the aluminum-alloy sheet has a Cu content of 0.10-0.20 mass %. 6. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet contains at least two elements selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %. 7. The aluminum-alloy sheet according to claim 6 , wherein the aluminum-alloy sheet further contains Ni: 0.0050-0.15 mass %. 8. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet contains Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %. 9. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet has an Si content of 2.4-3.6 mass %. 10. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet has an Mn content of 0.4-1.05 mass %. 11. The aluminum-alloy sheet according to claim 1 , wherein the Si/Mn mass ratio is 3.0-8.0. 12. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet has an Mg content of 0.4-0.6 mass %. 13. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet has an Fe content of 0.1-0.4 mass %. 14. The aluminum-alloy sheet according to claim 1 , wherein the aluminum-alloy sheet has a thickness of 0.8-2.5 mm. 15. An aluminum-alloy sheet comprising: Si: 2.3-3.8 mass %, Mn: 0.35-1.05 mass %, Mg: 0.35-0.65 mass %, Fe: 0.01-0.45 mass %, and at least one element selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %, wherein the aluminum-alloy sheet has an Si/Mn mass ratio of 2.5-9.0, an elongation of at least 23%, and a strain hardening exponent of at least 0.28 at a nominal strain of 3%, and the aluminum-alloy sheet is an automobile body panel. 16. The aluminum-alloy sheet according to claim 15 , wherein: the automobile body panel is a three-dimensionally shaped product having a thickness of 0.8-2.5 mm; and the Si/Mn mass ratio is 3.0-9.0. 17. A method for manufacturing the aluminum-alloy sheet according to claim 1 , comprising: providing an aluminum alloy material that contains Si: 2.3-3.8 mass %, Mn: 0.35-1.05 mass %, Mg: 0.35-0.65 mass %, Fe: 0.01-0.45 mass %, and at least one element selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %, the aluminum alloy material having an Si/Mn mass ratio of 2.5-9.0; hot rolling the aluminum-alloy material to form a sheet, the aluminum-alloy material being heated to 300-550° C. prior to hot-rolling and the hot-rolled sheet being at a temperature of 200-350° C. at the end of the hot rolling; cold rolling the sheet formed by the hot rolling such that a total rolling reduction of the cold rolling is at least 50%; subjecting the sheet formed by the cold rolling to a solution heat treatment in a temperature range of 480-560° C. and quenching at a cooling rate of at least 100° C./min until the sheet reaches 150° C.; and after the solution heat treatment, subjecting the sheet to a pre-aging treatment in a temperature range of 50-150° C. for 1-100 hours; wherein after the pre-aging, the aluminum alloy sheet exhibits an elongation of at least 23% and a strain hardening exponent of at least 0.28 at a nominal strain of 3%. 18. The method according to claim 17 , further comprising press forming the aluminum alloy sheet to form an automobile body panel. 19. An aluminum-alloy sheet produced by a process comprising: providing an aluminum alloy material that contains Si: 2.3-3.8 mass %, Mn: 0.35-1.05 mass %, Mg: 0.35-0.65 mass %, Fe: 0.01-0.45 mass %, and at least one element selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %, the aluminum alloy material having an Si/Mn mass ratio of 3.0-9.0; hot rolling the aluminum-alloy material to form a sheet, the aluminum-alloy material being heated to 300-550° C. prior to hot-rolling and the hot-rolled sheet being at a temperature of 200-350° C. at the end of the hot rolling; cold rolling the sheet formed by the hot rolling such that a total rolling reduction of the cold rolling is at least 50%; subjecting the sheet formed by the cold rolling to a solution heat treatment in a temperature range of 480-560° C. and quenching at a cooling rate of at least 100° C./min until the sheet reaches 150° C.; and after the solution heat treatment, subjecting the sheet to a pre-aging treatment in a temperature range of 50-150° C. for 1-100 hours; wherein after the pre-aging, the aluminum alloy sheet exhibits an elongation of at least 23% and a strain hardening exponent of at least 0.28 at a nominal strain of 3%. 20. The aluminum-alloy sheet according to claim 19 , wherein the aluminum-alloy sheet contains at least two elements selected from the group consisting of Cu: 0.0010-1.0 mass %, Cr: 0.0010-0.10 mass %, Zn: 0.0010-0.50 mass %, and Ti: 0.0050-0.20 mass %. 21. The aluminum-alloy sheet according to claim 20 , wherein the aluminum-alloy sheet further contains Ni: 0.0050-0.15 mass %. 22. The aluminum-alloy sheet according to claim 21 , wherein: the aluminum-alloy sheet has a Cu content of 0.0010-0.20 mass %, an Si content of 2.4-3.3 mass %, an Mn content of 0.4-0.8 mass %, an Mg content of 0.4-0.6 mass %, and an Fe content of 0.1-0.4 mass %, the Si/Mn mass ratio is 4.0-6.5; the aluminum-alloy material is heated to 500-550° C. prior to the hot-rolling, the hot-rolled sheet being at a temperature of 280-350° C. at the end of the hot rolling; the total rolling reduction of the cold rolling is at least 70%; the solution heat treatment performed in a temperature range of 510-560° C.; the strain hardening exponent after pre-aging is at least 0.29 at a nominal strain of 3%; and the aluminum-alloy sheet is an automobile body panel. 23. The aluminum-alloy sheet according to claim 22 , wherein: after the cold rolling, the aluminum-alloy sheet has a thickness of 0.8-2.5 mm; and the aluminum-alloy sheet has been stamped into the form of a three-dimensionally shaped automobile body panel. 24. An automobile body panel produced by a process comprising: stamping the aluminum-alloy sheet of claim 19 , to form a three-dimensionally shaped final product.
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