Hinge mechanism for inflatable restraint apparatus

• US 7,210,700 B2
• Filed: 08/24/2004
• Issued: 05/01/2007
• Est. Priority Date: 08/24/2004
• Status: Expired due to Fees

• Current Assignee: SMRC Automotive Holdings Netherlands BV (Samvardhana Motherson International Ltd.)
• Original Assignee: Visteon Global Technologies Incorporated (Visteon Corporation)
• Inventors: Stamm, Gregory, Charre, David, Zagrodnicki, Bernard, Haibach, Ralf, Moreau, Marc
• Primary Examiner(s): Dickson; Paul N.
• Assistant Examiner(s): Brown; Drew J.
• Application Number:
  US10/925,052
• Publication Number:
  US 20060043701A1
• Time in Patent Office: 980 Days
• Field of Search: 280/728.3, 280/732, 280/743.2
• US Class Current: 280/728.3
• CPC Class Codes: B60R 2021/21537 characterised by hinges
• CPC Class Codes: B60R 21/215 characterised by the covers for the inflatable member B60R21/2176 takes precedence

Abstract

An inflatable restraint apparatus provides deployment in a very short duration while at the same time controlling and decelerating the moving parts upon deployment. The apparatus includes an interior panel and an airbag deployment door formed in the interior panel and designed to break free from the panel upon deployment of the airbag. An airbag chute is suitably supported behind the employment door and directs deployment of the airbag outwardly towards the deployment door. A metal hinge connects the airbag chute and the deployment door, and is structured to control and decelerate the door during deployment.

Claims

1. An inflatable restraint apparatus having a deployable airbag, the apparatus comprising:

an interior panel;

an airbag deployment door formed in the interior panel and designed to break free from the interior panel upon deployment of the airbag;

an airbag chute suitably supported behind the deployment door and directing deployment of the airbag outwardly towards the deployment door;

a metal hinge connecting the airbag chute and the deployment door, the hinge including a first hinge portion connected to the deployment door, a second hinge portion adjacent to the air bag chute and a third hinge portion connected to the air bag chute, the hinge having a first transition area and a second transition area independent of one another, the first transition area interconnecting the first hinge portion and the second hinge portion, the second transition area being spaced inwardly from the first transition area and the deployment door and interconnecting the second hinge portion to the third hinge portion;

the first transition area structured to promote rotation of the first hinge portion relative to the second hinge portion;

the second transition area structured to promote outward translation of the second hinge portion relative to the third hinge portion without significant rotation of the second hinge portion relative to the third hinge portion; and

the deployment door first moving outwardly and then rotating upon deployment of the airbag.

2. The apparatus of claim 1, wherein the second transition area comprises a wave structure formed into the metal hinge, the wave structure being drawn out upon deployment of the airbag.

3. The apparatus of claim 2, wherein the wave structure is positioned proximate the airbag chute, and wherein the airbag chute guides the drawing out of the wave structure.

4. The apparatus of claim 2, wherein the wave structure includes at least one crest projecting laterally, the crest directed slightly inwardly.

5. The apparatus of claim 1, wherein the second transition area comprises a rivot and slot structure formed into the second and third hinge portions.

6. The apparatus of claim 1, wherein the second transition area is positioned proximate the airbag chute, the airbag chute guiding the movement of the second hinge portion relative to the third hinge portion.

7. The apparatus of claim 1, wherein the first transition area comprises an S-shape formed into the metal hinge, the S-shape guiding the rotation of the first hinge portion relative to the second hinge portion.

8. The apparatus of claim 1, wherein the second hinge portion extends parallel to the airbag chute.

9. The apparatus of claim 8, wherein the second hinge portion is positioned inside the airbag chute.

10. The apparatus of claim 1, wherein the second transition area is positioned rearwardly from the first transition area.

11. The apparatus of claim 1, further comprising a corner plate attached to the metal hinge proximate the first transition area, the corner plate limiting rotation of the first hinge portion relative to the second hinge portion.

12. An inflatable restraint apparatus having a deployable airbag, the apparatus comprising:

an interior panel;

an airbag deployment door formed in the interior panel and designed to break free from the interior panel upon deployment of the airbag;

an airbag chute suitably supported behind the deployment door and directing deployment of the airbag outwardly towards the deployment door;

a metal hinge connecting the airbag chute and the deployment door, the hinge having a first transition area and a second transition area independent of one another, the first transition area interconnecting a first hinge portion and a second hinge portion, the second transition area interconnecting the second hinge portion and a third hinge portion, the first hinge portion connected to the deployment door;

the second transition area comprising a wave structure formed into the metal hinge including at least two crests and one trough, the trough extending along the airbag chute, the wave structure being drawn out upon deployment of the airbag;

the first transition area structured to promote rotation of the first hinge portion relative to the second hinge portion;

the second transition area structured to promote outward translation of the second hinge portion relative to the third hinge portion; and

the deployment door first moving outwardly and then rotating upon deployment of the airbag.

13. An inflatable restraint apparatus having a deployable air bag, the apparatus comprising:

an interior panel;

an air bag deployment door formed in the interior panel and designed to break free from the interior panel upon deployment of the airbag;

an airbag chute suitably supported behind the deployment door and directing deployment of the airbag outwardly towards the deployment door;

a metal hinge connecting the airbag chute and the deployment door, the hinge having a first transition area and a second transition, the first transition area interconnecting a first hinge portion and a second hinge portion, the second transition area interconnecting the second hinge portion and a third hinge portion, the first hinge portion connected to the deployment door;

the first transition area structured to promote rotation of the first hinge portion relative to the second hinge portion;

the second transition area structured to promote outward translation of the second hinge portion relative to the third hinge portion;

a corner plate attached to the second hinge portion, the corner plate limiting rotation of the first hinge portion relative to the second hinge portion; and

the deployment door first moving outwardly and then rotating upon deployment of the airbag, the corner plate braking the rotation of the deployment door.

14. The apparatus of claim 13, wherein the corner plate provides resistance relative to the hinge and to the rotation of the first hinge portion relative to the second hinge portion.

15. The apparatus of claim 13, wherein the corner plate decelerates the rotation of the deployment door.

16. The apparatus of claim 13, wherein the corner plate limits rotation of the deployment door to a position where the deployment door cannot reach a window panel of the vehicle, or cannot reach another portion of the interior panel.

17. The apparatus of claim 13, wherein the corner plate comprises a first plate portion and a second plate portion defining pivot line therebetween.

18. The apparatus of claim 17, wherein the first plate includes bulldozer tabs formed into the corner plate to adjust the amount of resistance.

19. The apparatus of claim 17, wherein the first plate portion is attached to the second hinge portion, and wherein the second plate portion is unattached to but overlying the first transition area of the metal hinge.

20. The apparatus of claim 19, wherein the second hinge portion translates outwardly a predetermined distance to provide clean separation of the deployment door from the interior panel.

21. The apparatus of claim 13, wherein the second hinge portion includes a section spaced away from the airbag chute, and wherein at least a portion of the corner, plate is positioned between the metal hinge and the airbag chute.

22. The apparatus of claim 13, wherein the corner plate moves outwardly with the metal hinge as the second hinge portion translates outwardly relative to the third hinge portion.