Sport Ball Casing And Methods Of Manufacturing The Casing
US-2015202500-A1 · Jul 23, 2015 · US
US10016935B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10016935-B2 |
| Application number | US-201615366407-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 1, 2016 |
| Priority date | Mar 20, 2009 |
| Publication date | Jul 10, 2018 |
| Grant date | Jul 10, 2018 |
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A method of making a spherical sport ball includes forming a casing having a first and a second substantially hemispherical panel component. The first panel component is a first unitary structure and has a first central panel, a first plurality of polygonal peripheral panels adjacent to the first central panel and having a first plurality of edges, and a plurality of flange areas extending from the first plurality of edges. The second panel component is a second unitary structure and has a second central panel and a second plurality of polygonal peripheral panels adjacent to the second central panel. The method includes joining together the first panel component and the second panel component at a non-linear, circumferential seam between the first and second plurality of polygonal peripheral panels. The method also includes forming a vertex between adjacent ones of the plurality of flange areas.
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The invention claimed is: 1. A method of making a spherical sport ball, the method comprising: forming a casing having a first substantially hemispherical panel component and a second substantially hemispherical panel component; wherein the first substantially hemispherical panel component is a first unitary structure and has: a first central panel; a first plurality of polygonal peripheral panels adjacent to the first central panel and having a first plurality of edges; and a plurality of flange areas extending from the first plurality of edges; wherein the second substantially hemispherical panel component is a second unitary structure and has: a second central panel; and a second plurality of polygonal peripheral panels adjacent to the second central panel; and joining together the first substantially hemispherical panel component and the second substantially hemispherical panel component at a non-linear, circumferential seam between the first plurality of polygonal peripheral panels and the second plurality of polygonal peripheral panels; and forming a vertex between adjacent ones of the plurality of flange areas. 2. The method of claim 1 , wherein forming the vertex includes converging together adjacent ones of the plurality of flange areas. 3. The method of claim 1 , wherein forming the vertex includes orienting the vertex to extend radially away from a center of the first central panel. 4. The method of claim 1 , wherein forming the vertex includes defining a slit between the adjacent ones of the plurality of flange areas. 5. The method of claim 1 , wherein forming the vertex includes tapering together the adjacent ones of the plurality of flange areas. 6. The method of claim 1 , wherein forming the vertex includes cutting a stress relief opening between the adjacent ones of the plurality of flange areas. 7. The method of claim 1 , wherein forming the vertex includes folding the adjacent ones of the plurality of flange areas upon one another. 8. The method of claim 1 , wherein forming the vertex includes arranging the adjacent ones of the plurality of flange areas to be coextensive. 9. The method of claim 1 , wherein forming the vertex includes sealing together the adjacent ones of the first plurality of polygonal peripheral panels without cutting the adjacent ones of the plurality of flange areas. 10. The method of claim 1 , further including shaping the first central panel and the second central panel as a convex polygon. 11. The method of claim 1 , further including shaping the first central panel and the second central panel as a convex pentagon. 12. The method of claim 1 , further including shaping at least some of the first plurality of polygonal peripheral panels as a pentagon. 13. The method of claim 1 , wherein joining includes welding together the first substantially hemispherical panel component and the second substantially hemispherical panel component. 14. A method of making a spherical sport ball, the method comprising: forming a first substantially hemispherical panel component, wherein the first substantially hemispherical panel component is a first unitary structure and has: a first central panel; a first plurality of polygonal peripheral panels adjacent to the first central panel and having a first plurality of edges; and a plurality of flange areas extending from the first plurality of edges; forming a second substantially hemispherical panel component, wherein the second substantially hemispherical panel component is a second unitary structure and has: a second central panel; and a second plurality of polygonal peripheral panels adjacent to the second central panel; and welding together the first substantially hemispherical panel component and the second substantially hemispherical panel component at a non-linear, circumferential seam between the first plurality of polygonal peripheral panels and the second plurality of polygonal peripheral panels such that adjacent ones of the plurality of flange areas abut one another; impressing a plurality of elongated indentations in the first substantially hemispherical panel component to thereby form a first plurality of sides of the first central panel; and folding adjacent ones of the plurality of flange areas upon one another to thereby form a vertex between adjacent ones of the first plurality of polygonal peripheral panels. 15. The method of claim 14 , wherein impressing the plurality of elongated indentations includes forming a plurality of seams between adjacent ones of the first plurality of polygonal peripheral panels. 16. The method of claim 15 , further including bending the first substantially hemispherical panel component along at least one of the plurality of seams to thereby arrange the first central panel as a convex pentagon. 17. The method of claim 14 , wherein impressing the plurality of elongated indentations includes compressing and heating the first substantially hemispherical panel component along a plurality of elongated regions. 18. The method of claim 14 , wherein forming the first substantially hemispherical panel component includes cutting an entirety of the first substantially hemispherical panel component from a single sheet.
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