Bicycle seat rail manufacturing method
US-2024410042-A1 · Dec 12, 2024 · US
US9950355B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9950355-B2 |
| Application number | US-201013509364-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 15, 2010 |
| Priority date | Nov 13, 2009 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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Method of forming a component of complex shape from an Al-alloy sheet or a Mg-alloy sheet. The method includes the steps of: a) heating the sheet to a temperature below the solution heat treatment (SHT) temperature for the alloy; b) forming the heated sheet between heated dies into or towards the complex shape; c) heating the sheet to at least its SHT temperature and substantially maintaining that temperature until SHT has been completed; and d) quenching the solution heat treated sheet between cold dies and at the same time completing the forming into the complex shape or maintaining that shape.
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The invention claimed is: 1. A method of forming a sheet component of multi-dimensional shape from an Al-alloy or Mg-alloy sheet, the method comprising the following sequence of steps in order: (a) heating an Al-alloy or Mg-alloy sheet to a temperature below the solution heat treatment (SHT) temperature for the alloy; (b) forming the heated sheet between heated dies into a shape whilst maintaining the sheet at a temperature below the solution heat treatment (SHT) temperature for the alloy; (c) solution heat treating the sheet by heating the sheet to its SHT temperature and substantially maintaining that temperature until SHT has been completed; and (d) quenching the solution heat treated sheet between cold dies and at the same time completing the formation of the sheet into a finished shape, wherein step (a) includes either: heating the Al-alloy sheet to a temperature between 430° C. and 493° C.; or heating the Mg-alloy sheet to a temperature between 400° C. and 480° C. 2. The method according to claim 1 , wherein step (a) includes heating the sheet to a temperature below that at which inclusions in the alloy melt. 3. The method according to claim 1 , wherein step (a) includes heating the sheet to a temperature at which formability of the alloy is greater than that at the SHT temperature. 4. The method according to claim 1 , wherein step (a) includes heating the sheet to a temperature at which formability of the alloy is substantially maximized. 5. The method according to claim 1 , wherein step (b) includes forming the sheet in hot dies arranged to minimize heat loss from the sheet. 6. The method according to claim 1 , wherein, in step (b), the dies are at substantially the same temperature as that to which the sheet is heated in step (a). 7. The method according to claim 1 , wherein, during step (b), the temperature of the dies is kept substantially constant. 8. The method according to claim 1 , wherein the dies of step (b) comprise one or more heating elements. 9. The method according to claim 1 , wherein the dies of step (d) are cooled. 10. The method according to claim 1 , wherein the method includes the subsequent step of (e) artificially ageing the resulting component. 11. The method according to claim 1 , wherein the sheet is an AZ31 or AZ91 Mg-alloy. 12. The method according to claim 1 , wherein the sheet is a 2XXX series Al-alloy. 13. The method according to claim 12 , wherein the 2XXX series Al-alloy is AA2024. 14. The method according to claim 9 , wherein the dies of step (d) comprise one or more cooling elements, cooling channels, or both.
of alloys with magnesium as the next major constituent · CPC title
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