Hybrid inflator

• US 5,076,607 A
• Filed: 11/27/1990
• Issued: 12/31/1991
• Est. Priority Date: 11/27/1990
• Status: Expired due to Term

• Current Assignee: Bendix-Atlantic Inflator Company
• Original Assignee: Bendix-Atlantic Inflator Company
• Inventors: Rose, James M., Bishop, Robert J., Renfroe, Donald W., Frantom, Richard L., Woods, Charles D., Ocker, Klaus F., Bazel, Teresa L., Kremer, Robert M.
• Primary Examiner(s): Marmor, Charles A.
• Assistant Examiner(s): Tyson, Karin
• Application Number:
  US07/618,428
• Time in Patent Office: 399 Days
• Field of Search: 280/736, 280/737, 280/741, 280/728, 222/5, 137/68.2, 102/530, 102/531, 422/164, 422/165, 422/166
• US Class Current: 280/737
• 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

An inflator (10) comprising: a pressure tank (12, 14, 16, 20) for storing a quantity of stored inflation gas under pressure. The pressure tank comprising a first burst disk (46) in communication with the stored inflation gas; a sliding piston (72) including at one end thereof a sharp edge (74) for puncturing the first rupture disk and at its other end a second rupture disk (80). The sliding piston (72) movable into engagement with the first rupture disk in response to the build up of pressure acting on the second rupture disk (80) in response to the burning of propellant material (90) thereby permitting egress of the stored inflation gas. The second burst disk being ruptured by the continued build up of pressure due to the burning propellant whereupon after the rupturing of same the heated products of combustion resulting from the burning propellant flow through the sliding piston (72) to increase the temperature of the stored inflation gas prior to its exit from the inflator.

Claims

1. An inflator (10) comprising:

a pressure tank (12, 14, 16,

     20) for storing a quantity of stored inflation gas under pressure, the pressure tank comprising a first burst disk (46) in communication with the store inflation gas and preventing egress of the gas from the chamber;

a sliding piston (72) having an opening and including at one end thereof first means (74) for puncturing the first burst disk (46) and at its other end a second burst disk (80); and

a propellant material (90) provided near the second burst disk (80), said propellant producing gaseous combustion products when burned;

the sliding piston (72) movable into engagement with the first burst disk to puncture said first burst disk in response to the build up of pressure acting on the second burst (80) in response to burning of the propellant material (90) thereby permitting egress of the stored inflation gas, the second burst disk being ruptured by the continued build up of pressure due to the burning propellant material whereupon after the rupturing of the second burst disk the heated products of combustion resulting from the burning propellant material flow through the opening of the sliding piston (72) to increase the temperature of the stored inflation gas prior to its exit from the inflator.

2. The inflator (10) as defined in claim 1 wherein the pressure tank (12) comprises a cylindrical sleeve (14), a first end cap (16) secured at one end (14) thereof and a second end cap (20) secured at another end (18) thereof, the second end cap (20) being of generally cylindrical shape and including a narrowed portion (40) extending into the sleeve (14), the narrowed portion defining a first opening (44), the first burst disk (46) being secured to the narrow portion to close the first opening (44), the second end cap (20) further including at lease one orifice opening (120) through which gases escape upon the puncturing of the first burst disk (46).

3. The inflator (10) as defined in claim 1 wherein the first end cap (16) supports a pressure sensor (30) positioned interior to the pressure tank (12).

4. The inflator as defined in claim 1 wherein a propellant housing (52) is positioned within, secured to and generally spaced from the interior of the second end cap (20), the housing (52) including a second opening (54) facing the first burst disk (46),

a hollow sleeve member (60) is secured to the housing (52) and extends through the second opening (54), the sliding piston (72) is received and movable within the sleeve member (60).

5. The inflator (10) as defined in claim 4 including first means (84) for restraining the motion of the sliding piston (72) in a direction toward the first burst disk (46), the first means restraining the movement of the sliding piston (72) until the pressure generated by the burning propellant has reached a first predetermined value.

6. The inflator (10) as defined in claim 5 wherein the sleeve member (60) includes at an end facing away from the first burst disk (46), second means (86) for preventing the sliding piston from moving in a direction toward the propellant housing (52).

7. The inflator (10) as defined in claim 6 wherein the second means (86) includes a narrow band or wire.

8. The inflator (10) as defined in claim 4 wherein the propellant material (90) is secured within the propellant housing (52) spaced from the sliding piston (72), an initiator means (100, 102) responsive to a control signal indicative of a crash situation, generating heat to cause the propellant to burn, bias means (104, 106) interposing the initiator means and propellant material (90) for preloading the propellant material to prevent movement of same.

9. The inflator (10) as defined in claim 8 wherein the bias means (104, 106) comprises a screen (104) in contact with the propellant material (90) the screen (104) functions as a means of uniformly distributing the heat generated by the initiator means to the propellant.

10. The inflator (10) as defined in claim 8 wherein the bias means further includes a resilient material which preloads the screen (104) onto the propellant material.

11. The inflator (10) as defined in claim 1 wherein a diffuser (130) is positioned about the inflator to distribute gas of inflation to an air bag (140), such air bag mounted about the diffuser (130).

12. The inflator (10) as defined in claim 8 wherein the initiator means includes an initiator housing (100) secured to the propellant housing (52) and a squib or initiator (102) for initiating the burning of the propellant material, and ignition enhancing means (110) positioned between the squib and the propellant material (90) for increasing the heat supplied to the propellant material (90).

13. The inflator (10) as defined in claim 4 wherein the sleeve member (60) includes means for retaining the sliding piston (72) in its burst disk piercing position.

14. The inflator (10) as defined in claim 13 wherein the last mentioned means includes means for creating an interference fit between the sleeve member (60) and sliding piston (72).

15. The inflator (10) as defined in claim 1 wherein the second burst disk (80) is formed as an integral part of the sliding piston (72).

16. The inflator (10) as defined in claim 10 wherein the resilient material is silicone.