INFLATOR-AIRBAG INTERFACE

• US 20110025023A1
• Filed: 07/29/2009
• Published: 02/03/2011
• Est. Priority Date: 07/29/2009
• Status: Abandoned Application

• Current Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Original Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Inventors: Hatfield, Mark S., Button, Kevin
• Application Number:
  US12/511,810
• Publication Number:
  US 20110025023A1
• Time in Patent Office: Days
• US Class Current: 280/728.2
• CPC Class Codes: B60R 21/2171 specially adapted for elongated cylindrical or bottle-like inflators with a symmetry axis perpendicular to the main direction of bag deployment, e.g. extruded reaction canisters B60R21/2176 takes precedence

Abstract

An airbag deployed by pressurized gas emitted from an inflator in a vehicle passenger safety module includes an inflation portion that captures pressurized gas from the inflator and an inlet portion that communicates with the inflation portion and is configured to receive and to be secured to the outer surface of the discharge end of the inflator. A substantially continuous elastomeric gasket made of cured liquid silicone is carried on the interior surface of the inlet portion at a location that circumscribes the outer surface of the discharge end of the inflator, when the discharge end is received into the inlet portion. The transverse extent of the gasket is substantially smaller than its longitudinal extent, while the thickness of the gasket is greater than the thickness of the wall of the inlet portion of the airbag upon which the gasket is carried. Thus, a coupling structure for effecting the interconnection between an inflator and an airbag in a vehicle passenger safety module takes the from of a cured band of liquid sealant that is disposed between an exterior surface of the discharge end of the inflator and an interior surface of an inlet portion of the airbag due to being is secured directly to the interior surface of the inlet portion.

Claims

1. A coupling structure for effecting interconnection between an inflator and an airbag in a vehicle passenger safety module, the coupling structure comprising a cured band of liquid sealant disposed between an exterior surface of a discharge end of the inflator and an interior surface of an inlet portion of the airbag, when the discharge end of the inflator is received into the inlet portion of the airbag.

2. A coupling structure as recited in claim 1, wherein the cured band is substantially continuous in longitudinal extent.

3. A coupling structure as recited in claim 2, wherein the cured band has a transverse extent, and the transverse extent of the cured band is substantially smaller than the longitudinal extent of the cured band.

4. A coupling structure as recited in claim 2, wherein the cured band circumscribes the discharge end of the inflator, when the discharge end of the inflator is received into the inlet portion of the airbag.

5. A coupling structure as recited in claim 2, wherein the cured band has a thickness, and the thickness of the cured band is greater than the thickness of the wall of the inlet portion of the airbag.

6. A coupling structure as recited in claim 1, wherein the cured band is comprised of cured liquid silicone.

7. A coupling structure as recited in claim 1, wherein the cured band is carried on the interior surface of the inlet portion of the airbag, when the discharge end of the inflator is received into the inlet portion of the airbag.

8. A coupling structure as recited in claim 7, wherein the cured band is secured directly to the interior surface of the inlet portion of the airbag.

9. An airbag for a vehicle passenger safety module, the airbag being deployed by pressurized gas emitted from a discharge end of an inflator of the safety module, and the airbag comprising:

(a) an inflation portion in which to capture the pressurized gas from the inflator;

(b) an inlet portion in pneumatic communication with the inflation portion, the inlet portion being configured to receive the discharge end of the inflator and to be secured to an outer surface thereof, and

(c) an elastomeric gasket carried on an interior surface of the inlet portion at a location opposing the outer surface of the discharge end of the inflator, when the discharge end of the inflator is received into the inlet portion.

10. An airbag as recited in claim 9, wherein the gasket is substantially continuous, and the gasket circumscribes the discharge end of the inflator, when the discharge end of the inflator is received into the inlet portion of the airbag.

11. An airbag as recited in claim 10, wherein the gasket has a longitudinal extent, a transverse extent substantially smaller than the longitudinal extent thereof, and a thickness greater than the thickness of the wall of the inlet portion of the airbag.

12. An airbag as recited in claim 9, wherein the gasket is comprised of cured liquid silicone.

13. A method for manufacturing an airbag for a vehicle passenger safety module, the airbag including an inlet portion configured to receive therein the discharge end of an inflator of the safety module, the method comprising the steps of:

(a) forming a substantially continuous band of curable liquid sealant against an interior surface of the inlet portion of the airbag at a location opposing and circumscribing the outer surface of the discharge end of the inflator, when the discharge end of the inflator is received into the inlet portion of the airbag; and

(b) curing the substantially continuous band of liquid sealant into an elastomeric gasket carried on the interior surface of the inlet portion of the airbag, the gasket engaging the outer surface of the discharge end of the inflator, when the discharge end of the inflator is received into the inlet portion of the airbag.

14. A method as recited in claim 13, wherein the curable liquid sealant comprises a liquid silicone.

15. A method as recited in claim 13, wherein the inlet portion of the airbag comprises first and second circumferentially-defined neck segments of respective first and second flexible constituent airbag panels, and the step of forming comprises the steps of:

(a) applying a first bead of curable liquid sealant to an interior surface of the first neck segment in substantial alignment with a circumferential direction about the inlet portion of the airbag;

(b) disposing an elongated mandrel against the first bead of the sealant in longitudinal alignment with the neck segment, forming from the first bead of sealant a first band of the sealant;

(c) applying a second bead of the sealant to a side of the mandrel opposite from the first bead of sealant in substantial alignment with the first bead of the sealant; and

(d) urging an interior surface of the second neck segment against the second bead of the sealant with the second neck segment in longitudinal alignment with the first neck segment, forming from the second bead of sealant a second band of the sealant.

16. A method as recited in claim 15, further comprising the step of securing the first neck segment to the second neck segment along respective of the edges of the mandrel, the first neck segment and the second neck segment thereby forming the inlet portion of the airbag.

17. A method as recited in claim 15, wherein the first band of the sealant and the second band of the sealant together form the substantially continuous band of the sealant, and the step of curing is conducted with the mandrel between the first neck segment and the second neck segment contacting and circumscribed by the substantially continuous band of the sealant.

18. A method as recited in claim 17, wherein following the step of curing the substantially continuous band of liquid sealant into an elastomeric gasket, the elastomeric gasket adheres to the first neck segment and to the second neck segment, while the mandrel is nondestructively disengageable from the elastomeric gasket.

19. A method as recited in claim 15, wherein the mandrel has a width measured transverse the longitudinal extent thereof and a thickness measured normal to the longitudinal extent thereof, and the width of the mandrel is substantially greater than the thickness thereof.

20. A method as recited in claim 15, wherein the perimeter of a transverse cross section of the discharge end of the inflator is less than the perimeter of a transverse cross section of the mandrel.