High strength 6XXX aluminum alloys and methods of making the same
US-11920229-B2 · Mar 5, 2024 · US
US2016130686A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016130686-A1 |
| Application number | US-201614991722-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 8, 2016 |
| Priority date | Oct 5, 2012 |
| Publication date | May 12, 2016 |
| Grant date | — |
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Disclosed herein is an aluminum alloy composition and a method of heat treating the aluminum alloy, to improve process control and strength of the aluminum alloy for a rear safety plate mounted on a truck, etc., complying with safety regulations wherein the aluminum alloy composition includes Silicon (Si) about 0.8 to 1.3% by weight, Iron (Fe) up to about 0.5% by weight, Copper (Cu) about 0.15 to 0.4% by weight, Manganese (Mn) up to about 0.15% by weight, Magnesium (Mg) about 0.8 to 1.2% by weight, Chromium (Cr) up to about 0.25% by weight, Zinc (Zn) up to about 0.2% by weight, Titanium (Ti) up to about 0.1% by weight and the remaining percent by weight of Aluminum (Al) of the entire composition.
Opening claim text (preview).
1 - 3 . (canceled) 4 . A heat treatment method of an aluminum alloy composition, comprising: heat treating the aluminum alloy; and after heat treating the aluminum alloy, age heat treating the aluminum alloy at about 205° C. to 215° C. for 4 to 5 hours. 5 . The heat treatment method of claim 4 , wherein the aluminum alloy composition comprises Silicon (Si) about 0.8 to 1.3% by weight, Iron (Fe) up to about 0.5% by weight, Copper (Cu) about 0.15 to 0.4% by weight, Manganese (Mn) up to about 0.15% by weight, Magnesium (Mg) about 0.8 to 1.2% by weight, Chromium (Cr) up to about 0.25% by weight, Zinc (Zn) up to about 0.2% by weight, Titanium (Ti) up to about 0.1% by weight and the remaining percent by weight of Aluminum (Al) of the entire composition. 6 . The heat treatment method of claim 5 , wherein the aluminum alloy composition further comprises Beryllium (Be) and Zirconium (Zr). 7 . The heat treatment method of claim 6 , wherein the Beryllium (Be) is about 0.04 to 0.07% by weight and the Zirconium (Zr) is about 0.2 to 0.3% by weight of the entire composition. 8 . The heat treatment method of claim 4 , further comprising: age heat treating the aluminum alloy at 210° C. for 5 hours. 9 . A heat treatment method of claim 4 , further comprising: solution heat treating the aluminum alloy at about 520° C. to 560° C. for 1.5 to 2.5 hours. 10 . The heat treatment method of claim 9 , further comprising: solution heat treating the aluminum alloy at 540° C. for 2 hours. 11 . (canceled)
of alloys with magnesium as the next major constituent · CPC title
with silicon · CPC title
of alloys with silicon as the next major constituent · CPC title
of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions · CPC title
with silicon as the next major constituent · CPC title
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