Liquid propellant inflator for vehicle occupant restraint apparatus

• US 5,060,973 A
• Filed: 07/23/1990
• Issued: 10/29/1991
• Est. Priority Date: 07/23/1990
• Status: Expired due to Term

• Current Assignee: General Dynamics Armament and Technical Products Incorporated (General Dynamics Corporation)
• Original Assignee: General Electric Company
• Inventors: Giovanetti, Anthony J.
• Primary Examiner(s): Marmor, Charles A.
• Assistant Examiner(s): GRAYSAY, TAMARA L
• Application Number:
  US07/556,226
• Time in Patent Office: 463 Days
• Field of Search: 280/728, 280/736, 280/737, 280/740, 280/741, 280/742, 222/3, 149/46, 149/58, 149/59, 149/92, 60/205, 60/217, 60/218, 102/530, 102/531, 102/478, 102/705
• US Class Current: 280/736
• CPC Class Codes: B60R 2021/23123 Heat protection panels
• CPC Class Codes: B60R 21/264 using instantaneous generation of gas, e.g. pyrotechnic B60R21/268 takes precedence
• CPC Class Codes: C06B 31/00 Compositions containing an inorganic nitrogen-oxygen salt
• CPC Class Codes: C06B 47/00 Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
• CPC Class Codes: Y10S 102/705 Separated explosive constituents

Abstract

To deploy an inflatable member, such as an occupant restraint safety bag in a motor vehicle, a liquid propellant is expelled from a storage reservoir into a reaction chamber through ports created at frangible pressure points in the reservoir wall and ignited by detonation of an explosive charge to generate a non-toxic, bag inflating gas by exothermic reaction.

Claims

1. Apparatus for deploying an inflatable member comprising, in combination:

A. a reaction chamber connected in fluid flow communication with the inflatable member;

B. a reservoir disposed within said reaction chamber, said reservoir having a plurality of ports communicating with said reaction chamber and pressure sensitive sealing means normally closing said ports;

C. a quantity of liquid propellant stored in said reservoir; and

D. means for pressurizing said liquid propellant to open said sealing means and to expel said liquid propellant from said reservoir into said reaction chamber through said ports and for igniting said liquid propellant only after entry into said reaction chamber, thereby generating gas by exothermic reaction to inflate the inflatable member.

2. The apparatus defined in claim 1, wherein said liquid propellant pressurizing and igniting means includes a plunger disposed adjacent one end of said reservoir and an explosive charge, said plunger being driven away from said one reservoir end to expel said liquid propellant into said reaction chamber in response to the generation of hot gas by the detonation of said explosive charge, said hot gas entering said reaction chamber through said ports to ignite said liquid propellant.

3. The apparatus defined in claim 2, wherein said reservoir is tubular in shape and having a closed end in opposed relation to said one end, said ports provided at distributed locations along the reservoir length between said closed and one ends of said reservoir.

4. The apparatus defined in claim 3, wherein said liquid propellant is an aqueous solution of hydroxyl ammonium nitrate as an oxidizer and a nitrated hydrocarbon salt as a fuel.

5. Occupant restraint apparatus for a motor vehicle, said apparatus comprising, in combination:

A. an inflatable safety bag;

B. a reaction chamber connected in fluid flow communication with said safety bag;

C. a reservoir disposed in fluid flow relation with said reaction chamber;

D. a quantity of liquid propellant stored in said reservoir; and

E. an inflation initiator responsive to a high impact vehicle accident for expelling said liquid propellant from said reservoir into said reaction chamber and igniting said liquid propellant therein to generate by exothermic reaction a large volume of gas for

inflating said safety bag, said initiator including means for preventing ignition of said liquid propellant while in said reservoir.

6. The apparatus defined in claim 5, wherein said reservoir includes a plurality of ports normally closed by frangible seals, said initiator acting to rupture said seals, thereby permitting expulsion of said liquid propellant into said reaction chamber through said ports.

7. The apparatus defined in claim 6, wherein said initiator means includes a plunger disposed adjacent one end of said reservoir, said initiator further including an explosive charge, said plunger being driven away from said one reservoir end in response to detonation of said explosive charge to pressurize said liquid propellant in said reservoir and rupture said seals to expel said liquid propellant from said reservoir into said reaction chamber.

8. The apparatus defined in claim 7, wherein said explosive charge is disposed on the opposite side of said plunger from said liquid propellant in said reservoir, said detonated explosive charge generating a hot gas which enters said reaction chamber through said ports to ignite said liquid propellant therein.

9. The apparatus defined in claim 8, wherein said reservoir is tubular in shape and having a closed end in opposed relation to said one end, said ports provided at distributed locations along the reservoir length between said closed and one ends of said reservoir.

10. The apparatus defined in claim 9, wherein the side of said plunger facing said liquid propellant is shaped in conformity with said closed end of said reservoir.

11. The apparatus defined in claim 9, wherein said liquid propellant is a monopropellant comprising an aqueous solution of hydroxyl ammonium nitrate as a oxidizer and triethanol ammonium nitrate as a fuel.

12. The apparatus defined in claim 9, wherein said explosive charge is comprised of a smokeless powder.

13. The apparatus defined in claim 9, wherein said explosive charge is liquid propellant.

14. The apparatus defined in claim 9, wherein said reaction chamber includes passages through which inflating gas flows into the interior of said safety bag, said apparatus further including a heat shield releaseably disposed over said passages to protect said safety bag during initial inflation.

15. The apparatus defined in claim 9, wherein said reaction chamber further includes a central, threaded opening, said reservoir, plunger and explosive charge being pre-assembled with a threaded plug as an initiator module, said plug being threaded in said central opening to assembly said initiator module to said reaction chamber.

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

A. providing a reaction chamber in fluid flow communication with the inflatable member;

B. providing a reservoir containing a liquid propellant;

C. positioning the reservoir within the reaction chamber;

D. forcing the liquid propellant from the reservoir into the reaction chamber to initiate deployment; and

E. igniting the liquid propellant solely in the reaction chamber to generate by exothermic reaction a large volume of gas for inflating the inflatable member.

17. The method defined in claim 16, wherein said liquid propellant forcing step includes pressurizing the liquid propellant to rupture the reservoir at discrete pressure points and create a plurality of ports through which the liquid propellant is expelled into the reaction chamber.

18. The method step defined in claim 17, wherein said igniting step includes detonating an explosive charge to generate combusting matter which enters the reaction chamber through the ports to ignite the liquid propellant in a controlled manner.

19. The method defined in claim 18, wherein the detonation of the explosive charge drives a plunger through the reservoir to pressurize the liquid propellant.