Injection termination feature

• US 5,746,445 A
• Filed: 12/03/1996
• Issued: 05/05/1998
• Est. Priority Date: 12/03/1996
• Status: Expired due to Fees

• Current Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Original Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Inventors: Harris, Bradley D., Johnson, Darrin L.
• Primary Examiner(s): Dickson, Paul N.
• Application Number:
  US08/770,380
• Time in Patent Office: 518 Days
• Field of Search: 280/741, 280/736, 280/737, 102/530, 102/531
• US Class Current: 280/741
• CPC Class Codes: B60R 21/264 using instantaneous generation of gas, e.g. pyrotechnic B60R21/268 takes precedence

Abstract

In an inflator of a vehicle safety restraint system utilizing liquid propellant as the inflation gas generator, decomposition of residual liquid propellant within the inflator produces undesirable gases which can result in unacceptable inflator effluent. The injection termination features of the present invention are formed onto an encapsulation or plug of a regenerative piston inflator. Upon completion of the piston stroke, the injection termination feature makes contact with the injection ports and plugs the injection ports to prevent combustion and decomposition reactions from propagating through the piston.

Claims

1. An inflator of a vehicle safety restraint system, comprising:

a housing, the housing including a reservoir of liquid propellant;

a combustion chamber disposed in the housing in communication with the liquid propellant reservoir;

regenerative piston means for separating the liquid propellant reservoir and the combustion chamber, the piston means including a plurality of injection ports for delivering the liquid propellant to the combustion chamber in a controlled manner; and

injection termination means disposed in the housing, wherein upon completion of a stroke of the piston means, the injection termination means seals the injection ports of the piston means for preventing combustion and decomposition reactions of any residual liquid propellant from propagating through the piston means.

2. The inflator of claim 1, further comprising means for encapsulating the liquid propellant reservoir within the housing.

3. The inflator of claim 2, wherein the piston means comprises a piston including a head separating the combustion chamber from the liquid propellant reservoir and a piston stem extending through the encapsulation means, the piston being movably disposed within the encapsulation means.

4. The inflator of claim 3, further comprising a quantity of ignitor material disposed within the stem of the piston and initiating means disposed within the housing for igniting the material, wherein upon ignition the piston head is driven into the liquid propellant reservoir and the liquid propellant flows through the injection ports disposed in the piston head into the combustion chamber.

5. The inflator of claim 3, wherein the encapsulation means comprises an encapsulation cup contacting the housing, the encapsulation cup being molded from a non-corrosive material.

6. The inflator of claim 5, wherein the injection termination means is located within the encapsulation cup.

7. The inflator of claim 6, wherein the injection termination means comprises a plurality of buttons of material molded integrally with the encapsulation cup, wherein upon completion of the stroke of the piston the plurality of buttons seal the plurality of injection ports.

8. The inflator of claim 6, wherein the injection termination means comprises a plurality of buttons of material adhered to the encapsulation cup, wherein upon completion of the stroke of the piston the plurality of buttons seal the plurality of injection ports.

9. The inflator of claim 6, wherein the piston head includes a circular groove in a bottom portion thereof, the plurality of injection ports being disposed in the groove.

10. The inflator of claim 9, wherein the injection termination means comprises a ring of material located on the encapsulation cup, wherein upon completion of the stroke of the piston, the ring fits within the groove of the piston head to seal the plurality of injection ports.

11. The inflator of claim 6, wherein the injection termination means comprises a washer of material disposed within the encapsulation cup, wherein upon completion of the stroke of the piston, the washer seals the plurality of injection ports.

12. The inflator of claim 3, wherein the encapsulation means comprises an encapsulation tube of non-corrosive material contacting the housing.

13. The inflator of claim 12, wherein the encapsulation tube includes a cap sealing an end thereof.

14. The inflator of claim 13, wherein the injection termination means comprises a plurality of buttons of material molded integrally with the cap of the encapsulation tube, wherein upon completion of the stroke of the piston the plurality of buttons seal the plurality of injection ports in the piston head.

15. The inflator of claim 13, wherein the injection termination means comprises a plurality of buttons of material adhered to the cap of the encapsulation tube, wherein upon completion of the stroke of the piston the plurality of buttons seal the plurality of injection ports of the piston head.

16. The inflator of claim 13, wherein the piston head includes a circular groove in a bottom portion thereof, the plurality of injection ports being disposed in the groove.

17. The inflator of claim 16, wherein the injection termination means comprises a ring of material located on the cap of the encapsulation tube, wherein upon completion of the stroke of the piston, the ring fits within the groove of the piston head to seal the plurality of injection ports of the piston head.

18. The inflator of claim 6, wherein the injection termination means comprises a chamber of non-combustible material located within the encapsulation cup, the chamber being separated from the liquid propellant reservoir by a frangible membrane, wherein upon completion of the stroke of the piston, the piston head fractures the membrane and the non-combustible material flows into and seals the plurality of injection ports of the piston head.

19. A method of terminating injection of a liquid propellant in a regenerative piston inflator of a vehicle safety restraint system, comprising the steps of:

movably positioning a piston within a housing of the inflator, the housing including a reservoir of liquid propellant and a combustion chamber separated from the liquid propellant reservoir by a head of the piston;

driving the piston head into the liquid propellant reservoir, the piston head including a plurality of injection ports in fluid communication with the liquid propellant reservoir, the liquid propellant flowing through the injection ports into the combustion chamber;

combusting the liquid propellant in the combustion chamber;

continuing to drive the piston into the liquid propellant reservoir; and

sealing the injection ports of the piston head by injection termination means disposed in the housing to prevent combustion and decomposition reactions of any remaining liquid propellant from propagating through the injection ports of the piston.

20. The method of claim 19, wherein the injection termination means comprises a quantity of material disposed within an encapsulation means enclosing the liquid propellant, and the step of sealing the injection ports of the piston head comprises sealing the injection ports with the quantity of material.