Safety bag inflation apparatus using a liquid propellant gas generator

• US 5,487,561 A
• Filed: 12/09/1994
• Issued: 01/30/1996
• Est. Priority Date: 12/09/1994
• Status: Expired due to Term

• Current Assignee: General Dynamics OTS Incorporated (General Dynamics Corporation)
• Original Assignee: Martin Marietta Corporation
• Inventors: Degler, David S., Mandzy, John
• Primary Examiner(s): Rice, Kenneth R.
• Application Number:
  US08/352,949
• Time in Patent Office: 417 Days
• Field of Search: 280/736, 280/741
• US Class Current: 280/741
• CPC Class Codes: B60R 21/264 using instantaneous generation of gas, e.g. pyrotechnic B60R21/268 takes precedence

Abstract

To deploy an inflatable member, such as an occupant restraint safety bag in a motor vehicle, a buffer zone is pressurized by the firing of inflation initiator to release liquid propellant into the buffer zone through ruptured frangible seals in a stationary separator disk or in a movable piston for controlled ignition. The ignited liquid propellant generates a large volume of gas that is cooled and pressurize buffered prior to inflating introduction into the safety bag.

Claims

1. Occupant restraint apparatus for a motor vehicle, comprising:

an inflatable safety bag;

a housing having at least one vent in inflating fluid flow communication with the safety bag;

a reservoir of liquid propellant positioned in the housing;

a buffer zone positioned in the housing;

a first frangible seal separating the liquid propellant reservoir from the buffer zone;

a second frangible seal blocking fluid flow communication between the buffer zone and the housing vent; and

an inflation initiator, operating in response to a high impact vehicular accident, for pressurizing the buffer zone to initiate rupture of the first and second frangible seals and to ignite the liquid propellant in the buffer zone, ignition of the liquid propellant generating by exothermic reaction, a gas flowing from the buffer zone through the housing vent to inflate the safety bag.

2. The occupant restraint apparatus of claim 1, which further includes a cooling zone positioned between the buffer zone and the housing vent for cooling the safety bag inflating gas.

3. The occupant restraint apparatus of claim 2, wherein the buffer zone pressurized by the inflation initiator is a first buffer zone, the apparatus further including a second buffer zone positioned between the cooling zone and the housing vent.

4. The occupant restraint apparatus of claim 1, wherein the buffer zone contains air or a gas of greater density than air.

5. The occupant restraint apparatus of claim 3, wherein the first and second buffer zones contain air or a gas of greater density than air.

6. The occupant restraint apparatus of claim 2, wherein the cooling zone contains a gas cooling medium.

7. The occupant restraint apparatus of claim 6, wherein the gas cooling medium is a liquid capable of vaporization by the safety bag inflating gas.

8. The occupant restraint apparatus of claim 6, wherein the gas cooling medium is a porous metallic medium.

9. Apparatus for deploying an inflatable member, comprising:

a housing having an exit vent communicating with the inflatable member;

a reservoir of liquid propellant centrally located in the housing;

an air chamber centrally located in the housing adjacent the reservoir;

a first frangible seal blocking fluid communication between the reservoir and the air chamber;

an annular cooling chamber surrounding at least the air chamber and containing a gas cooling medium;

a second frangible seal blocking fluid communication between the air chamber and the cooling chamber; and

an inflation initiator operable to pressurize the air chamber, rupture the first frangible seal and ignite the liquid propellant released from the reservoir into the air chamber, the ignited liquid propellant generating, by exothermic reaction, a gas to further pressurize the air chamber and rupture the second frangible seal, whereupon the gas flows from the air chamber through the gas cooling medium in the cooling chamber and out the housing exit vent to inflate the member.

10. The apparatus of claim 9, wherein the inflation initiator is a pyrotechnic detonator located in the air chamber.

11. The apparatus of claim 9, wherein the annular cooling chamber includes a cylinder inner wall and a cylindrical outer wall, the inner wall including at least one first port in fluid communication with the air chamber and normally closed by the second frangible seal, the outer wall including at least one second port in fluid communication with the housing exit vent and in axially displaced relation with the first port.

12. The apparatus of claim 11, wherein the cooling chamber surrounds both the liquid propellant reservoir and the air chamber.

13. The apparatus of claim 11, wherein the first port comprising an annular array of the first ports, each closed by separate second frangible seals, an annular array of the-second ports, and an annular array of the exit vents.

14. The apparatus of claim 13, which further includes an annular air chamber surrounding the cooling chamber in fluid communication with the exit vents, the second ports being in fluid communication with the annular air chamber.

15. The apparatus of claim 14, which further includes a third frangible seal closing each of the second ports, the third frangible seals rupturing upon pressurization of the cooling chamber by the gas entering the cooling chamber from the centrally positioned air chamber.

16. The apparatus of claim 9, wherein the cooling medium is a porous metallic medium.

17. The apparatus of claim 9, wherein the cooling medium is liquid capable of vaporization by the gas.

18. Apparatus for deploying an inflatable member, comprising:

a housing having a plurality of vents in fluid communication with the inflatable member;

a cylinder positioned in the housing;

a piston slidably received in the cylinder and including a piston head dividing the cylinder into a reservoir containing a liquid propellant and an air chamber;

a plurality of first ports in the piston head between the reservoir and the air chamber, the first ports being normally closed by first frangible seals;

a plurality of second ports in the cylinder providing fluid communication between the air chamber and the housing vents, the second ports being normally closed by second frangible seals; and

an inflation initiator operable to pressurize the air chamber and drive the piston in a direction contracting the reservoir, whereupon the first frangible seals rupture and liquid propellant flowing through the first ports into the air chamber is ignited to generate a gas, by exothermic reaction, further pressurizing the air chamber to rupture the second frangible seals and allow the gas to flow through the second ports and the housing vents, deploying the inflatable member.

19. The apparatus of claim 18, which further includes an annular cooling chamber surrounding the cylinder and through which the gas flows from the second ports to the housing vents, the cooling chamber containing a gas cooling medium consisting of a porous metallic medium or a liquid capable of vaporization by the gas.

20. The apparatus of claim 19, which further includes an annular air chamber surrounding the cooling chamber, the gas flowing through the annular air chamber from the cooling chamber to the housing vents.

21. The apparatus of claim 20, which further includes third ports between the cooling chamber and the annular air chamber, the third ports being normally closed by third frangible seals that rupture upon pressurization of the cooling chamber by the gas, and the third ports being axially displaced relative to the second ports and the housing vents.

22. The apparatus of claim 18, wherein the piston further includes a cylindrical support member extending from the piston head in a direction away from the air chamber, the liquid propellant reservoir provided within the support member, the apparatus further comprising:

an annular cooling chamber provided between the support member and the cylinder, the cooling chamber containing a vaporizable liquid;

an annular air chamber surrounding the cylinder in fluid communication with the housing vents and the second ports;

a plurality of third ports in the cylinder between the cooling chamber and the annular air chamber, the third ports normally closed by third frangible seals,

whereby, upon pressurization of the air chamber, the piston is driven in the direction to contract both the reservoir and the cooling chamber, the third frangible seals rupturing to allow the liquid to flow through the third ports into the annular air chamber where the liquid is vaporized by the gas flowing through the second ports into the annular air chamber.

23. The apparatus of claim 22, wherein the second and third ports are oriented to direct the gas and the fluid respectively, in converging directions to enhance vaporization of the liquid and cooling of the gas in the annular air chamber.

24. The apparatus of claim 18, wherein the piston has a support member with a free end opposite from the piston head, and wherein the free end is slidingly received through an opening in the housing.

25. The apparatus of claim 22, wherein the inflation initiator is pyrotechnic detonator situated in the air chamber.

26. The apparatus of claim 24, wherein the housing includes an extension in the form of a truncated cone structure positioned to collapse at least a portion of the free end of the support member protruding from the housing as the piston is driven in the reservoir and cooling chamber contracting direction.

27. A method for deploying an inflatable member, comprising the steps of:

providing a reservoir of liquid propellant;

providing a buffer zone containing air;

providing a member initially separating the reservoir and the buffer zone;

releasing the liquid propellant through the separating member at the time deployment is desired;

igniting the liquid propellant released from the reservoir into the buffer zone to generate a gas by exothermic reaction;

cooling the gas; and

inflating the member with the cooled gas.

28. The method of claim 27, wherein the separating member is a stationary frangible seal, and wherein the releasing and igniting steps are performed by detonating an explosive charge to pressurize the buffer zone and rupture the frangible seal, detonation of the charge generating combusting matter in the buffer zone for igniting the liquid propellant released from the reservoir.

29. The method of claim 27, wherein the separating member is a movable piston having ports initially closed by frangible seals, wherein the releasing and igniting steps are performed by detonating an explosive charge to pressurize the buffer zone and rupture the frangible seals, detonation of the charge generating combusting matter in the buffer zone for igniting the liquid propellant released from the reservoir through the ports.