Claims
- 1. A method of manufacturing a can end, comprising:
i) forming an end shell comprising a radially outer seaming flange, a chuck wall adjacent the seaming flange, a center panel, and an axially downward countersink joining the center panel to the chuck wall below the level of the seaming flange; ii) converting the shell to an easy-open can end by:
a) forming a score on a portion of the center panel; b) raising a rivet on the center panel; and c) forming a tab and attaching the tab to the rivet; and iii) subsequently forming the end by moving the center panel and the seaming flange one with respect to the other to raise the center panel above the level of the seaming flange.
- 2. A method of manufacturing a can end, comprising:
i) forming an end shell comprising a radially outer seaming flange, a chuck wall adjacent the seaming flange, a center panel, and an axially downward countersink joining the center panel to the chuck wall below the level of the seaming flange; ii) converting the shell to an easy-open can end by:
a) forming a score on a portion of the center panel; b) raising a rivet on the center panel; and c) forming a tab and attaching the tab to the rivet; iii) subsequently forming the end by moving the center panel and the seaming flange one with respect to the other to raise the center panel above the level of the seaming flange; iv) securing the end to a can body which has been filled with product; and v) performing a second reforming operation on the can end to move the center panel and the seaming flange one with respect to the other to lower the center panel to a height below the level of the seaming flange, thereby reducing the headspace within the package.
- 3. A method of manufacturing a can end, comprising:
i) forming an end shell comprising a radially outer seaming flange, a chuck wall adjacent the seaming flange, a center panel, and an axially downward countersink joining the center panel to the chuck wall below the level of the seaming flange; ii) supporting the end shell on a carrier belt; iii) moving the carrier belt to transport the end shell to a conversion station, where the shell is converted to an easy-open end by:
a) forming a score on a portion of the center panel; b) raising a rivet on the center panel; and c) forming a tab and attaching the tab to the rivet; and iv) moving the carrier belt to transport the converted end to a reform station, where the end is reformed by moving the center panel and the seaming flange one with respect to the other to raise the center panel above the level of the seaming flange.
- 4. The method according to claim 1, wherein reforming the can end comprises:
i) clamping the radially outer seaming flange of the end by means of a clamping ring; and ii) moving the clamping ring and a punch one with respect to the other so as to push the center panel upwardly to a position above the level of the seaming flange.
- 5. The method according to claim 4, wherein reforming the can end comprises moving the punch upwardly with respect to the clamping ring.
- 6. A method of manufacturing a can end comprising the steps of:
i) forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less so that the end shell comprises a radially outer seaming flange, a chuck wall adjacent the seaming flange, a center panel, and an axially downward countersink joining the center panel to the chuck wall below the level of the seaming flange; ii) converting the shell to an easy-open can end by:
a) forming a score on a portion of the center panel; b) raising a rivet on the center panel; and c) forming a tab and attaching the tab to the rivet; and iii) subsequently forming the end by moving the center panel and the seaming flange one with respect to the other to raise the center panel above the level of the seaming flange.
- 7. The method according to claim 6, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming an end shell from an aluminum alloy material having a proof strength of approximately 225 N/mm2 or less.
- 8. The method according to claim 7, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming an end shell from an aluminum alloy material having a proof strength within a range of approximately 190 N/mm2 to approximately 220 N/mm2.
- 9. The method according to claim 6, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from a 5000 series alloy.
- 10. The method according to claim 9, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from a 5052 alloy.
- 11. The method according to claim 9, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from one of a 5352 alloy, a 5042 alloy, a 5154 alloy, a 5182 alloy, and a 5082 alloy.
- 12. The method according to claim 6, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from a 3000 series alloy.
- 13. The method according to claim 12, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from one of a 3004 alloy, a 3104 alloy, and a 3105 alloy.
- 14. The method according to claim 6, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming the end shell from an 8000 series alloy.
- 15. The method according to claim 6, wherein forming an end shell from an aluminum alloy material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 250 N/mm2 or less comprises forming a stay-on-tab easy-open can end.
- 16. The method according to claim 6, further comprising securing the end to a can body which has been filled with product, and performing a second reforming operation on the can end to move the center panel and the seaming flange one with respect to the other to lower the center panel to a height below the level of the seaming flange, thereby reducing the headspace within the package.
- 17. An easy-open can end formed from one of a 3000 series aluminum alloy, a 5000 series aluminum alloy, and an 8000 series aluminum alloy, the end being formed from a material having a thickness of approximately 0.22 mm or less and a proof strength of approximately 225 N/mm2 or less.
- 18. The easy-open can end according to claim 17, wherein the material has a proof strength within a range of approximately 190 N/mm2 to approximately 220 N/mm2.
- 19. An easy-open can end formed from 5053 aluminum alloy material heat treated to an H44 temper (Euronom Desigantion) so that the material has a prof strength of approximately 225 N/mm2 or less and a thickness of approximately 0.22 mm or less.
- 20. The easy-open can end according to claim 17, wherein the can end is a stay on tab easy-open can end.
Priority Claims (2)
Number |
Date |
Country |
Kind |
9707688.9 |
Apr 1997 |
GB |
|
9707678.0 |
Apr 1997 |
GB |
|
Parent Case Info
[0001] This application is a continuation in part of prior application Ser. No. 09/403,110, filed Oct. 14, 1999, which is a national phase filing of PCT/GB98/01073, filed Apr. 14, 1998 and claiming priority to Great Britain application serial number 9707688.9, filed Apr. 16, 1997; and prior application Ser. No. 09/403,209, filed Oct. 14, 1999, which is a national phase filing of PCT/GB98/01072, filed Apr. 14, 1998 and claiming priority to Great Britain application serial number 9707678.0, filed Apr. 16, 1997.
Continuation in Parts (2)
|
Number |
Date |
Country |
Parent |
09403110 |
Oct 1999 |
US |
Child |
09862293 |
May 2001 |
US |
Parent |
09403209 |
Oct 1999 |
US |
Child |
09862293 |
May 2001 |
US |