Variable output driver side hybrid inflator

• US 5,851,027 A
• Filed: 09/09/1996
• Issued: 12/22/1998
• Est. Priority Date: 09/09/1996
• Status: Expired due to Term

• Current Assignee: Arc Automotive Incorporated (The Jordan Co. LP)
• Original Assignee: Bendix-Atlantic Inflator Company
• Inventors: Gold, Stephen, Bishop, Robert, Woods, Charles, Husband, Richard, Copperthite, Chester, DiGiacomo, Michael
• Primary Examiner(s): Rice, Kenneth R.
• Application Number:
  US08/711,028
• Time in Patent Office: 834 Days
• Field of Search: 280/736, 280/737, 280/741, 280/742
• US Class Current: 280/736
• CPC Class Codes: B60R 2021/2633 with a plurality of inflation levels
• CPC Class Codes: B60R 21/272 with means for increasing the pressure of the gas just before or during liberation, e.g. hybrid inflators

Abstract

A variable output inflator (20) for use in inflating an air bag or air cushion comprising: a pressure vessel (22) comprising a thin walled toroidal pressure vessel portion (23) and a cylindrical pressure vessel portion (60) circumscribed by, in physical contact and in fluid communication with the toroidal pressure vessel portion, the cylindrical pressure vessel portion including a rupturable disk (74) and at least one exit port (78) communicable with an air bag; a pyrotechnic member (200a,b) for heating stored inflation gas within the pressure vessel to a pressure level to rupture the rupturable disk, allowing heated inflation gas to exit and fill an adjacently attached air bag.

Claims

1. An inflator device (20) for use in inflating an air bag or air cushion comprising:

a pressure vessel (22) defining an enclosed volume (44) containing stored inflation gas, said pressure vessel comprising a toroidal pressure vessel portion (23) having circular inner wall and outer wall portions, the inner wall portions defining an annular space (25), and reinforcing means (60, 62, 60'"'"') secured to at least an exterior of the inner wall portion about the annular space for reinforcing the pressure vessel in relation to internal pressure forces;

pyrotechnic means (200a,b or

     310) in said toroidal pressure vessel portion for heating said stored inflation gas within the pressure vessel to a pressure level to open a rupturable disk to permit said stored inflation gas to exit the inflator device.

2. The device as defined in claim 1 wherein the reinforcing means includes a cylindrical pressure vessel portion (60, 60'"'"') circumscribed by, in physical contact with, in fluid communication with and forming part of the toroidal pressure vessel portion, the cylindrical pressure vessel portion including the rupturable disk (74) and at least one exit port (78) communicable with an air bag.

3. The device as defined in claim 1 wherein the reinforcing means includes a circular member (352) secured to the pressure vessel portion, circumscribed by the inner wall portion.

4. The device as defined in claim 3 wherein the circular member is formed in the shape of a short cylinder having a center fill port (354) into which inflation gas is received.

5. The device as defined in claim 2 wherein the cylindrical pressure vessel portion comprises a cylindrical tube (62) having a wall (63) secured to an outside of said inner wall portion of the toroidal pressure vessel and an open top (82),

a rupture disk support member (70) with a central opening (72), wherein the rupturable disk is secured to the support member to seal the central opening (72) and wherein an outer edge of the support member (70) is secured to the toroidal pressure vessel portion (22), the support member, the exterior of the toroidal pressure vessel portion and the exterior of the cylindrical pressure vessel portion (60) defining an intermediate annular pressure vessel portion (28).

6. The device as defined in claim 5 wherein a portion of the support structure which surrounds the central opening (72) is smoothly curved to receive a portion of the rupturable disk subsequent to rupture.

7. The device as defined in claim 5 wherein the toroidal pressure vessel portion and the cylindrical pressure vessel portion each respectively include at least one flow opening (45,64) in communication with the intermediate annular pressure vessel portion (28).

8. The device as defined in claim 1 wherein the toroidal pressure vessel portion (22) comprises an upper (24) and lower (26) half toroidal section joined together along an inner seam (30b, 38b) and an outer seam (30a, 38a) forming the toroidal pressure vessel portion (23) and wherein the cylindrical pressure vessel portion (60) abuts the inner seam.

9. The device as defined in claim 1 wherein the toroidal pressure vessel portion (23) includes at least one outwardly extending boss (35a,b) having a generally flat bottom (40) with a respective initiator opening (46) therein.

10. The device as defined in claim 9 including an initiator assembly (100a,b) associated with each initiator opening (46a,b) comprising:

a sleeve (106) having a closed end (108) extending into the toroidal pressure vessel portion (23) and another end (114) sealed to the toroidal pressure vessel portion about the initiator opening (46a,b);

initiator means for generating products of combustion for rupturing a portion of the closed end of the sleeve (106) in response to a received control signal;

initiator support means (120) located within the sleeve (106) in abutting relationship with the initiator means and the toroidal pressure vessel portion for supporting the initiator means and for transferring any forces acting in the initiator means directly to the toroidal pressure vessel portion.

11. The device as defined in claim 1 wherein the pyrotechnic means (200a,b) includes an initiator (116a,b) positioned in the toroidal pressure vessel portion (23) and a pyrotechnic capsule (202) having a cap (210) and bottom (250).

12. The device as defined in claim 10 further comprising a quantity of slow burning propellant material and a quantity of rapidly burning material positioned to be ignited by the initiator.

13. The device as defined in claim 12 wherein the inflator includes two remotely located initiators and two corresponding pyrotechnic capsules.

14. The device as defined in claim 2 further comprising a rupture disk support element having an exterior edge attached to the toroidal pressure vessel portion.

15. The device as defined in claim 1 wherein the toroidal pressure vessel portion contains a set of holes proximate the rupturable disk and also located generally opposite an initiator (116).

16. The device as defined in claim 1 wherein a separator (300,300'"'"') is provided between the pyrotechnic means and the rupturable disk.

17. The device as defined in claim 16 wherein the separator (300,300'"'"') is concave upwardly shaped to divert products of combustion generated by an initiator and a fast burning propellant downwardly to flow passages located near the bottom of the cylindrical pressure vessel portion to a quantity of slow burning propellant located within the toroidal pressure vessel portion.

18. An inflator device (20) for use in inflating an air bag or air cushion comprising:

a pressure vessel (22) comprising a toroidal pressure vessel portion (23)

pyrotechnic means (200a,b) disposed within the toroidal pressure portion, for heating stored inflation gas within the pressure vessel for delivery to an air bag.

19. The device as defined in claim 18 further comprising a cylindrical pressure vessel portion (60) circumscribed by, in physical contact and in fluid communication with the toroidal pressure vessel portion, the cylindrical pressure vessel portion including a rupturable disk (74), and at least one exit port (78) communicable with the air bag.