End closure with double anti-missile score
An end closure for food and beverage containers provides controlled opening characteristics to prevent the unintentional missiling of a tear panel. The end closure comprises a score line that defines a portion of the tear panel, and the end closure may comprise one or more anti-missile features that inhibit the propagation of a fracture down a score line, which reduces the likelihood that a tear panel will inadvertently detach from the end closure and injure the user or another.
1. A method of forming a metallic end closure with an anti-missile feature, comprising:
providing a blank metallic material;
forming an end closure comprising a peripheral curl, a central panel, and a countersink positioned therebetween;
forming a first score line on said central panel, wherein said first score line substantially defines a tear panel;
providing a tool with at least one shaped feature disposed on a distal end of said tool;
pressing said tool into at least one of said central panel and said tear panel such that said at least one shaped feature contacts said at least one of said central panel and said tear panel at a location proximate said first score line to form a first anti-missile feature positioned proximate a second anti-missile feature in said end closure, wherein said first and second anti-missile features have a shallower depth than said first score line, and wherein said first anti-missile feature and said second anti-missile feature are disposed on said tear panel and oriented substantially parallel to each other; and
interconnecting a pull tab to said central panel of said end closure, wherein a nose of said pull tab is positioned over said tear panel to facilitate opening of said end closure when a downward force is applied to said tear panel with said nose of said pull tab.
2. The method of claim 1 , further comprising:
forming a second score line substantially parallel to said first score line, wherein said second score line has a shallower depth than said first score line.
3. The method of claim 2 , wherein said first and second anti-missile features are disposed over said second score line.
4. The method of claim 1 , wherein said first and second anti-missile features have longitudinal axes which are oriented at an acute angle relative to said first score line.
5. The method of claim 4 , wherein said angle is between approximately 15 and 60 degrees.
6. The method of claim 1 , wherein said first and second anti-missile features have a shape of at least one of a rectangle, a circle, an ovoid, a polygonal, a trapezium, and an arc shape.
7. A method of forming a metallic end closure with an anti-missile feature, comprising:
providing a blank metallic material;
forming an end closure comprising a peripheral curl, a central panel, and a countersink positioned therebetween;
forming a first score line on said central panel, wherein said first score line substantially defines a tear panel, and said first score line comprises a check slot having a first end and a second end;
providing a tool with at least one shaped feature disposed on a distal end of said tool;
pressing said tool into at least one of said central panel and said tear panel such that said at least one shaped feature contacts said at least one of said central panel and said tear panel at a location proximate to said first score line to form a first anti-missile feature positioned proximate a second anti-missile feature in said end closure, and wherein an end of said first anti-missile feature is positioned proximate to said check slot between said ends of said check slot, and an end of said second anti-missile feature is positioned proximate to said check slot between said ends of said check slot; and
interconnecting a pull tab to said central panel of said end closure, wherein a nose of said pull tab is positioned over said tear panel to facilitate opening of said end closure when a downward force is applied to said tear panel with said nose of said pull tab.
8. The method of claim 7 , further comprising:
forming a second score line substantially parallel to said first score line, wherein said second score line has a shallower depth than said first score line.
9. The method of claim 8 , wherein said first and second anti-missile features are disposed over said second score line.
10. The method of claim 7 , wherein said first and second anti-missile features have longitudinal axes which are oriented at an acute angle relative to said first score line.
11. The method of claim 10 , wherein said angle is between approximately 15 and 60 degrees.
12. The method of claim 7 , wherein said first and second anti-missile features have a shape of at least one of a rectangle, a circle, an ovoid, a polygonal, a trapezium, and an arc shape.
13. The method of claim 7 , wherein said first and second anti-missile features are disposed on the tear panel side of said first score line.
14. The method of claim 7 , wherein said first and second anti-missile features have a shallower depth than said first score line.
15. A method of forming a metallic end closure with anti-missile features, comprising:
providing a blank metallic material;
forming an end closure comprising a peripheral curl, a central panel, and a countersink positioned therebetween;
forming a first score line on said central panel, wherein said first score line substantially defines a tear panel;
providing a tool with a first shaped feature and a second shaped feature disposed on a distal end of said tool, wherein an end of said first shaped feature is offset from an end of said second shaped feature by a first offset distance, and a longitudinal axis of said first shaped feature is offset from a longitudinal axis of said second shaped feature by a second offset distance;
pressing said tool into at least one of said central panel and said tear panel such that said first shaped feature forms a first anti-missile feature and said second shaped feature forms a second anti-missile feature in said end closure; and
interconnecting a pull tab to said central panel of said end closure, wherein a nose of said pull tab is positioned over said tear panel to facilitate opening of said end closure when a downward force is applied to said tear panel with said nose of said pull tab.
16. The method of claim 15 , wherein said first offset distance is between approximately 0.026 and 0.022 inches.
17. The method of claim 15 , wherein said second offset distance is approximately 0.029 inches.
18. The method of claim 15 , wherein a direction of said second offset distance is substantially perpendicular to a direction of said first offset distance.
19. The method of claim 15 , wherein said first and second anti-missile features have a shallower depth than said first score line.
20. The method of claim 15 , wherein said first and second anti-missile features are disposed on the tear panel side of said first score line.