Airbag cover

• US 6,337,461 B1
• Filed: 10/19/1999
• Issued: 01/08/2002
• Est. Priority Date: 07/03/1997
• Status: Expired due to Term

• Current Assignee: Sanko Gosei UK, Ltd. (Sanko Gosei Limited)
• Original Assignee: Sanko Gosei UK, Ltd. (Sanko Gosei Limited)
• Inventors: Yasuda, Mitsuo, Kusumi, Amen
• Primary Examiner(s): Heinrich, Samuel M.
• Application Number:
  US09/403,190
• Time in Patent Office: 812 Days
• Field of Search: 219/121.62, 219/121.68, 219/121.69, 219/121.7, 219/121.71, 219/121.83
• US Class Current: 219/121.62
• CPC Class Codes: B23K 26/032 using optical means
• CPC Class Codes: B23K 26/364 for making a groove or trench, e.g. for scribing a break initiation groove
• CPC Class Codes: B23K 26/389 of fluid openings, e.g. nozzles, jets laser machining of inkjet nozzles B41J2/1634
• CPC Class Codes: B60R 21/205 in dashboards
• CPC Class Codes: B60R 21/2165 characterised by a tear line for defining a deployment opening

Abstract

An airbag cover and method is disclosed. The cover comprises a laminate formed from a thermoplastic substrate base layer, a foamed thermoplastic intermediate layer and a thermoplastic decorative foil layer, wherein a panel for permitting release of an airbag is outlined in the cover by laser cuts extending into the laminate from said base layer, said laser cuts having a substantially uniform depth into the laminate.

Claims

1. A method of producing an air bag cover by using a laser to form a line of mechanical weakness in a motor vehicle trim piece or panel, said method comprising the steps of:

i) scoring the trim piece from its underside with a laser beam to form a line of mechanical weakness, and

ii) forming a plurality of microperforations along said line of mechanical weakness,

iii) sensing the energy of the laser beam penetrating each microperforation and utilizing the microperforation as a calibration point to control the energy of the laser between sequential microperforations to thereby maintain a substantially constant thickness of intact material between microperforations along said line of mechanical weakness.

2. The method according to claim 1, wherein the trim piece is a laminate.

3. The method according to claim 1, wherein the trim piece comprises a polypropylene (PP) substrate, a foamed polypropylene (PP) intermediate layer, and an acrylonitrile-butadiene-styrene/polyvinyl chloride (ABS/PVC) composite or a thermoplastic polyolefin (TOP) foil.

4. The method according to claim 1, wherein the laser beam is of constant intensity.

5. The method according to claim 1, wherein the laser beam is pulsed.

6. The method according to claim 4, wherein the laser beam is moved along a predetermined score path in a stepwise manner.

7. The method according to claim 1, wherein the laser is a carbon dioxide gas laser.

8. The method according to claim 1, wherein microperforations are made every 0.2-5.0 mm along the predetermined score path.

9. The method according to claim 1, wherein a computer interpolates the thickness of material lying between adjacent microperforations and varies the laser beam accordingly.

10. The method according to claim 1, further comprising the step of reinforcing the air bag cover with a back plate.

11. The method according to claim 10, wherein the plate is aluminium.

12. The method according to claim 1, wherein the trim piece is for a steering wheel.

13. The method according to claim 1, wherein the trim piece is for a dashboard.

14. The method as claimed in claim 1, wherein a sensor is positioned on the opposite side of the trim piece or panel to the laser and said sensor is calibrated to utilize the energy of the laser beam detected at the microperforations as a reference point to control the thickness of uncut material along the score line between said microperforations and to maintain such thickness substantially constant.

15. The method as claimed in claim 14, wherein the panel is a laminate made up of a plurality of layers, the depth of penetration of the laser cut into the panel between the microperforations is controlled by counting the pulses required to form a microperforation and deducting a number of pulses calculated to stop at the junction between the final face side layer and the adjacent layer.

16. The method as claimed in claim 15, wherein the adjacent layer is a foamed plastics material and the final layer is a foil.

17. The method as claimed in claim 14, wherein the laser beam is operated to produce a series of microperforations spaced lengthwise of the score line.

18. The method as claimed in claim 14, wherein said score line is formed to outline the air bag cover and a hinge is provided on the underside of the panel between the outline of the cover and the panel so that, in use, the cover is severed from the panel along said score line but remains attached to the panel by said hinge.