Airbag covering provided with a specified rupture line and method for the production thereof

• US 20020190505A1
• Filed: 05/24/2002
• Published: 12/19/2002
• Est. Priority Date: 09/27/2000
• Status: Abandoned Application

• Current Assignee: Jenoptik Automatisierungstechnik Gmbh (Jenoptik AG)
• Original Assignee: Jenoptik Automatisierungstechnik Gmbh (Jenoptik AG)
• Inventors: Taenzer, Wolfgang, Feistel, Ulf, Preuss, Norbert
• Application Number:
  US10/130,947
• Publication Number:
  US 20020190505A1
• Time in Patent Office: Days
• US Class Current: 280/728.3
• CPC Class Codes: B23K 2103/172 wherein at least one of the layers is non-metallic
• CPC Class Codes: B23K 26/364 for making a groove or trench, e.g. for scribing a break initiation groove
• CPC Class Codes: B23K 26/40 taking account of the properties of the material involved
• CPC Class Codes: B29C 2035/0838 using laser
• CPC Class Codes: B29C 59/007 Forming single grooves or ribs, e.g. tear lines, weak spots by moulding B29C37/0057; folding lines B29C53/06; in metal articles B21D17/00; by cutting B26D3/08
• CPC Class Codes: B29L 2031/3008 Instrument panels
• CPC Class Codes: B60R 21/2165 characterised by a tear line for defining a deployment opening

Abstract

An airbag cover is defined by a predetermined breaking line which is introduced into a shaped flat material in a recessed manner. The recesses are achieved by removing material by means of laser radiation. According to the invention, the flat material is provided with a barrier layer. The barrier layer, by reason of its material properties, has greater resistance to removal of material by laser action than the material of the rest of the flat material. The recesses made by removing material extend along the predetermined breaking line in the flat material up to the barrier layer. The barrier layer makes it possible to produce a predetermined breaking line by means of laser machining which allows an exact residual wall thickness of the airbag cover in the area of the predetermined breaking line, so that the tearing strength can be adjusted very accurately, which is critically important for a reliable deployment of an airbag. Further, a method for the efficient production of an airbag cover of this type is indicated.

Claims

1. Airbag cover which is integrated in shaped flat material and whose contour is defined by a predetermined breaking line (S) that has been introduced into the flat material in a recessed manner, wherein the flat material has, at least in the area of the predetermined breaking line (S), a barrier layer (3) made from a material which, by reason of its properties, has greater resistance to removal of material by laser action than the rest of the flat material, and wherein the recesses in the flat material extend along the predetermined breaking line (S) essentially up to the barrier layer (3).

2. Airbag cover according to claim 1, characterized in that the predetermined breaking line (S) is formed of a plurality of holes of limited depth which are introduced adjacent to one another in the flat material by means of laser radiation.

3. Airbag cover according to claim 1 or 2, characterized in that the barrier layer (3) is arranged on one of the outer surfaces (4, 5) of the flat material.

4. Airbag cover according to claim 1 or 2, characterized in that the barrier layer (3) is embedded in the flat material so as to extend parallel to the outer surfaces (4, 5) of the flat material.

5. Airbag cover according to one of claims 1 to 4, characterized in that the barrier layer (3) is provided only in an area following the predetermined breaking line (S),

6. Airbag cover according to one of claims 1 to 4, characterized in that the barrier layer (3) is provided only in the form of a pattern covering portions of the flat material, particularly in the form of stripes or grids.

7. Method for producing an airbag cover which is integrated in shaped flat material and whose contour is defined by a predetermined breaking line (S) that has been introduced into the depth of the flat material, characterized in that a flat material is produced initially which has, at least in the area in which the predetermined breaking line (S) is to be introduced, a barrier layer (3) comprising a material which, by reason of its properties, has a greater resistance to removal of material by laser action than the rest of the flat material, and the predetermined breaking line (S) is subsequently introduced in that recesses are made in the flat material by means of laser radiation at a plurality of adjacent locations, wherein the intensity of the laser radiation is selected in such a way in relation to the properties of the barrier layer (3) and the rest of the flat material that only the flat material, but not the material of the barrier layer (3), is removed at each of these locations.

8. Method according to claim 7, characterized in that the flat material which is provided with the barrier layer (3) is given the desired spatial shape, for example, the shape of a console, before introducing the plurality of recesses which, in their entirety, form the predetermined breaking line (S).

9. Method according to claim 7 or 8, characterized in that the barrier layer (3) is integrated in the flat material at a constant distance from the outer surface of the flat material on which the laser radiation acts.

10. Method according to claim 9, characterized in that the barrier layer (3) is arranged on the opposite outer surface of the flat material.

11. Method according to claim 9 or 10, characterized in that the barrier layer (3) is provided only in the areas that are subsequently machined by laser.

12. Method according to one of claims 7 to 11, characterized in that the intensity of the laser radiation is adjusted to a constant level.

13. Method according to one of claims 7 to 12, characterized in that the barrier layer (3) is provided in an arrangement pattern at the flat material which only partially covers the flat material, particularly in the shape of stripes or grids or symmetric partial surfaces.

14. Method according to one of claims 7 to 13, characterized in that the tearing strength of the predetermined breaking line (S) is adjusted through the selected thickness of the barrier layer (3).

15. Method according to one of claims 7 to 13, characterized in that the tearing strength of the predetermined breaking line (S) is adjusted through the selected position of the barrier layer (3) in the depth of the flat material.

16. Method according to one of claims 7 to 13, characterized in that the tearing strength of the predetermined breaking line (S) is adjusted through the selected distance between the adjacent recesses introduced by removal of material.

17. Method according to one of claims 7 to 16, characterized in that the flat material is essentially produced from a hardenable material, a metal or nonmetal foil serving as barrier layer (3) is pressed into this flat material before it has hardened and is joined to it.

18. Method according to one of claims 7 to 16, characterized in that a metal or nonmetal foil serves as barrier layer (3) and is connected to the material of the flat material by the action of heat or ultrasound.

19. Method according to one of claims 7 to 16, characterized in that a liquid, hardening polymer material serves as barrier layer (3) and is sprayed onto the flat material or, conversely, a polymer material serving as flat material is sprayed onto the barrier layer.

20. Method according to one of claims 7 to 19, characterized in that the flat material is produced by overlaying and connecting a plurality of layers of material, wherein the barrier layer (3) is arranged between two of these layers.