TRIM PANEL HAVING FOAM BRIDGE SUPPORTED HIDDEN TEAR SEAM

• US 20060261578A1
• Filed: 06/22/2006
• Published: 11/23/2006
• Est. Priority Date: 12/22/2003
• Status: Active Grant

• Current Assignee: International Automotive Components Group North America (Lear Corporation)
• Original Assignee: Lear Corporation
• Inventors: Depue, Todd L., Cowelchuk, Glenn A., Hier, Michael J.
• Granted Patent: US 7,690,677 B2
• Time in Patent Office: Days
• US Class Current: 280/728.300
• CPC Class Codes: B60R 21/2165 characterised by a tear line for defining a deployment opening
• CPC Class Codes: Y10T 29/49 Method of mechanical manufacture

Abstract

In at least one embodiment, the present invention relates to a trim panel for concealing an air bag. The panel comprises a substrate and a cover over the substrate. The cover includes a cover skin. The panel also comprises a tear seam having at least a portion comprising a pattern of alternating residual wall thicknesses in the panel. At least one embodiment of the present invention also relates to a method for making a trim panel for concealing an air bag.

Claims

1. A trim panel for concealing an air bag, said panel comprising:

a substrate;

a cover over the substrate, the cover including a foam layer and a cover skin, the foam layer being between the substrate and the cover skin; and

a tear seam, the tear seam having at least a portion comprising a pattern of alternating residual wall thicknesses in the panel, wherein the pattern comprises spaced-apart bridges of foam having a length of 0.1 to 100 mm and a width of 0.05 to 5.0 mm to provide support to the cover skin, and wherein the alternating residual wall thickness comprises alternating first and second sets of voids, with the first set of voids having a first depth D₁, and the second set of voids having a second depth D₂, less than the first depth, with the voids of the first sets of voids extending into the cover skin such that the cover skin adjacent to the first set of voids has a first residual wall thickness (RWT₁) of 2.5% to 30% of the thickness T of the remainder of the skin.

2. The panel of claim 1 wherein the pattern provides support to the cover skin.

3. The panel of claim 2 wherein the tear seam has a structure which prevents the cover from forming a visually detectable physical weakened portion on the passenger side of the panel.

4. The panel of claim 2 wherein the RWT₁ is 5% to 25% of the thickness T of the remainder of the skin.

5. The panel of claim 2 wherein the RWT₁ is 10% to 20% of the thickness T of the remainder of the skin.

6. The panel of claim 5 wherein the alternating residual wall thicknesses in the panel comprises a plurality of first wall portions having a first thickness and a plurality of second wall portions having a second thickness, greater than the first thickness, at least a substantial number of each first wall portion being between two adjacent second wall portions.

7. The panel of claim 1 wherein the first thickness T₁ comprises 0.01 to 6.0 mm and the second thickness T₂ comprises 2.0 to 35.0 mm.

8. The panel of claim 4 wherein a space of 0.1 to 100.0 mm extends between adjacent foam portions.

19. The panel of claim 3 wherein the second set of voids have a length L₂ that is between 1.0 and 200 mm.

20. The panel of claim 1 wherein the second set of voids have a length L₂ that is between 1.0 and 200 mm.

9. A trim panel for concealing an air bag, said panel comprising:

a substrate; and

a cover over the substrate, the cover including a foam layer and a cover skin, the foam layer being between the substrate and the cover skin; and

a tear seam, the tear seam having at least a portion comprising a pattern of alternating residual wall thicknesses in the panel, wherein the pattern comprises spaced-apart bridges of foam having a length of 0.1 to 100 mm and a width of 0.05 to 5.0 mm to provide support to the cover skin, and wherein the alternating residual wall thickness comprises alternating first and second sets of holes, with the first set of holes having a first depth D₁, and the second set of holes having a second depth D₂, less than the first depth, with the holes of the first sets of holes extending into the cover skin such that the tear seam has a structure which prevents the cover from forming a visually detectable physical weakened portion on the passenger side of the panel.

10. The panel of claim 9 wherein the cover skin adjacent to the first set of holes has a residual wall thickness of 2.5% to 30% of the thickness T of the remainder of the skin.

11. The panel of claim 9 wherein the cover skin has a residual wall thickness that is less than half of the thickness T of the remainder of the skin.

12. A method of forming a trim panel for concealing an air bag, said method comprising:

providing a panel comprising a substrate and a cover over the substrate, the cover including a foam layer and a cover skin, the foam layer being between the substrate and the cover skin, and the cover skin having a thickness T; and

forming a tear seam in the panel having at least a portion comprising a pattern of alternating residual wall thicknesses in the panel, wherein the pattern comprises spaced-apart bridges of foam having a length of 0.1 to 100 mm and a width of 0.05 to 5.0 mm to provide support to the cover skin, and wherein the alternating residual wall thickness comprises alternating first and second sets of voids, with the first set of voids having a first depth D₁, and the second set of voids having a second depth D₂, less than the first depth, with the voids of the first sets of voids extending into the cover skin such that the cover skin adjacent to the first set of voids has a residual wall thickness (RWT) of 2.5% to 30% of the thickness T of the remainder of the skin.

13. The method of claim 12 comprises employing a laser to form the pattern of alternating residual wall thicknesses in the panel.

14. The method of claim 12 wherein the pattern comprises spaced-apart bridges of material which provide support to the cover skin and a foam layer is provided between the substrate and the cover skin, with the bridges comprising foam portions below the cover skin.

15. The method of claim 14 wherein a space of 0.1-100.0 mm extends between each foam portion and the portions of the cover over the spaces have a depth of 0.01-6.0 mm.

16. The method of claim 15 wherein the alternating residual wall thicknesses in the panel comprises a plurality of first wall portions having a first thickness and a plurality of second wall portions having a second thickness, greater than the first thickness, at least a substantial number of each first wall portion being between two adjacent second wall portions.

17. The method of claim 13 wherein the voids comprise score lines.

18. The method of claim 13 wherein the voids comprise holes.