Patent US5372380A successfully refreshed from Google Patents.
US5372380A
Expired / Lapsed
US
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Filter and method of forming
Assignee: Ultramet Inc
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Filing: 1993-05-20
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Granted: 1994-12-13
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Expires: 2013-05-20
Abstract
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.
Inventors
- 👤 Andrew J. Duffy
- 👤 Richard B. Kaplan
- 👤 Stanley A. Racik
- 👤 Edwin P. Stankiewicz
- 👤 Robert H. Tuffias
- 👤 Brian E. Williams
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 13:57
CPC Classifications
B; B60; B60R; B60R21/00; B60R21/02; B60R21/16; B60R21/26; B60R21/264; B60R21/2644; B01; B01D; B01D39/00; B01D39/14; B01D39/20; B01D39/2055; B01D46/00; B01D46/10; B01D46/24; B01D46/56; B01D46/62; B01D2239/00; B01D2239/04; B01D2239/0471; B01D2239/0478; B01D2239/10; B01D2279/00; B01D2279/10; Y; Y10; Y10S; Y10S55/00; Y10S55/42
Claims Analysis
Total Claims: 17
Claim 1
Independent Claim
98 words
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.
Claim 2
Dependent Claim
98 words
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.
Claim 3
Dependent Claim
14 words
An airbag assembly of claim 1 including a containment vessel for said propellant charge.
Claim 4
Dependent Claim
36 words
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.
Claim 5
Dependent Claim
37 words
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.
Claim 6
Dependent Claim
20 words
An airbag assembly of claim 1 wherein said propellant gas generator is contained within porous interstices in said filter member.
Claim 7
Dependent Claim
32 words
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.
Claim 8
Dependent Claim
43 words
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.
Claim 9
Dependent Claim
27 words
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.
Claim 10
Dependent Claim
18 words
An airbag assembly of claim 1 including a prefilter between the propellant gas generator and the filter member.
Claim 11
Dependent Claim
25 words
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.
Claim 12
Dependent Claim
57 words
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.
Claim 13
Dependent Claim
57 words
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.
Claim 14
Dependent Claim
21 words
An airbag assembly of claim 11 wherein said propellant charge is confined within an axially formed opening within said annular member.
Claim 15
Dependent Claim
20 words
An airbag assembly of claim 11 wherein said propellant charge is confined within axially positioned pores within said annular member.
Claim 16
Dependent Claim
99 words
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.
Claim 17
Dependent Claim
99 words
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.
References Cited (Backward Citations)
US5064459A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-12-12 | 1998-06-13 | 1998-12-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-12-12 | 2002-06-13 | 2002-12-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-12-12 | 2006-06-13 | 2006-12-13 | $7700.00 | Window Closed / Lapsed |