Filter and method of forming

• US 5,372,380 A
• Filed: 05/20/1993
• Issued: 12/13/1994
• Est. Priority Date: 05/20/1993
• Status: Expired due to Term

• Current Assignee: Ultramet Co.
• Original Assignee: Ultramet Co.
• Inventors: Stankiewicz, Edwin P., Duffy, Andrew J., Racik, Stanley A., Williams, Brian E., Kaplan, Richard B., Tuffias, Robert H.
• Primary Examiner(s): Rice, Kenneth R.
• Application Number:
  US08/063,707
• Time in Patent Office: 572 Days
• Field of Search: 280/728 R, 280/736, 280/740, 280/741, 280/742
• US Class Current: 280/740
• CPC Class Codes: B01D 2239/0478 on a layer of the filter
• CPC Class Codes: B01D 2239/10 Filtering material manufacturing
• CPC Class Codes: B01D 2279/10 for air bags, e.g. inflators therefor
• CPC Class Codes: B01D 39/2055 Carbonaceous material solid sorbent compositions comprising free carbon B01J20/20
• CPC Class Codes: B01D 46/10 Particle separators, e.g. dust precipitators, using filter plates, sheets or pads having plane surfaces
• CPC Class Codes: B01D 46/24 Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
• CPC Class Codes: B01D 46/62 connected in series
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: Y10S 55/42 Foam filter materials

Abstract

An airbag assembly including an inflatable airbag, an ignitable propellant charge for generating inflating gas and a filter between the interior of the airbag and the propellant charge. The filter comprising a porous carbon foam substrate coated substantially throughout with a thermally and structurally stable material which has been formed in situ by chemical vapor deposition techniques.

Claims

1. An air bag assembly comprising a propellant gas generator, an igniter for said propellant gas generator, an airbag, and a filter member between said propellant gas generator and said airbag, said filter member comprising a rigid porous composite having a pyrolyzed carbon substrate and a thermally and structurally stable coating, said filter member having the unaided structural strength and toughness to withstand an instantaneous pressure pulse of at least approximately 4,000 pounds per square inch and an instantaneous temperature pulse of at least approximately 2,700 degrees Fahrenheit, whereby propellant gas is dispensed substantially uniformly from said filter member.

2. An airbag assembly of claim 1 including a containment vessel for said propellant charge.

3. An airbag assembly of claim 1 including a containment vessel for said propellant gas generator, said containment vessel having walls substantially surrounding said propellant gas generator, said filter member defining at least part of said walls.

4. An airbag assembly of claim 3 wherein said filter member is adapted to withstand initial pressure pulses of at least approximately 2,000 pounds per square inch and initial temperature pulses of at least approximately 2,000 degrees Fahrenheit.

5. An airbag assembly of claim 1 wherein said propellant gas generator is contained within porous interstices in said filter member.

6. An airbag assembly of claim 1 including a containment vessel for said propellant gas generator and a housing enclosing said containment vessel, said housing being positioned at least partially within said airbag.

7. An airbag assembly of claim 1 including a containment vessel for said propellant gas generator and a housing enclosing said containment vessel, a prefilter positioned generally between said filter member and said propellant gas generator, said filter member being positioned within said housing.

8. An airbag assembly of claim 1 wherein said filter member is generally spherical and said propellant gas generator is located within and generally centrally of said filter.

9. An airbag assembly of claim 1 including a prefilter between the propellant gas generator and the filter member.

10. An airbag assembly of claim 1 wherein baffles between the filter member and the propellant gas generator are adapted to direct the flow of gas.

11. An airbag assembly comprising an airbag, a propellant charge, an igniter for said charge, a containment vessel for said charge located within said airbag, the walls of said containment vessel comprising a generally uniformly porous annular member comprising carbon foam coated with structurally and thermally stable material, said propellant charge being confined axially within said annular member.

12. An airbag assembly of claim 11 wherein said propellant charge is confined within an axially formed opening within said annular member.

13. An airbag assembly of claim 11 wherein said propellant charge is confined within axially positioned pores within said annular member.

14. A process for forming an airbag assembly comprising forming a porous rigid foam substrate having generally uniform tortuous paths extending therethrough, applying a thermally and structurally stable coating substantially throughout said substrate utilizing chemical vapor deposition techniques to form a filter member, providing an ignitable propellant gas generating charge, providing an airbag element adapted to be inflated by propellant gas emitted from said gas generating charge, and positioning said filter member between said gas generating charge and the interior of said airbag element, whereby said propellant gas passes through said tortuous paths before entering the interior of said airbag.