Gas generating apparatus

• US 6,176,517 B1
• Filed: 10/23/1998
• Issued: 01/23/2001
• Est. Priority Date: 10/23/1998
• Status: Expired due to Fees

• Current Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Original Assignee: Autoliv Aspinc
• Inventors: Kafadar, Charles B., Hamilton, Brian K., Harrington, Paul
• Primary Examiner(s): Swann, J. J.
• Assistant Examiner(s): BOTTORFF, CHRISTOPHER
• Application Number:
  US09/178,380
• Time in Patent Office: 823 Days
• Field of Search: 280/736, 280/737, 280/741, 280/742, 280/729, 280/733, 149/46, 149/36, 149/19.91, 102/288, 102/289
• US Class Current: 280/736
• CPC Class Codes: B60R 2021/23123 Heat protection panels
• CPC Class Codes: B60R 2021/26058 using a combination of inflators
• CPC Class Codes: B60R 21/232 Curtain-type airbags deploying mainly in a vertical direction from their top edge
• CPC Class Codes: B60R 21/2346 Soft diffusers
• CPC Class Codes: B60R 21/26 characterised by the inflation fluid source or means to control inflation fluid flow arrangement or mounting thereof to the vehicle B60R21/20; blasting cartridges for producing gas under pressure in general F42B3/04; initiators or igniters therefor F42B3/10
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: B60R 21/2646 the reacting substances being supported by the inflatable member walls, or by a flexible support within it
• CPC Class Codes: B60R 21/272 with means for increasing the pressure of the gas just before or during liberation, e.g. hybrid inflators
• CPC Class Codes: C06B 31/32 with a nitrated organic compound
• CPC Class Codes: C06D 5/06 by reaction of two or more solids

Abstract

A gas generating apparatus for outputting a gas is provided. In one embodiment, the apparatus is an inflator having a propellant for supplying inflation gas(es) to an inflatable located in a vehicle. A confining member is located adjacent to the propellant. A number of spaced holes are provided in the confining member, either before or after activation of the propellant. Inflation gas is received through the spaced holes for subsequent passage to the inflatable. In that regard, the inflation gas first passes through a chamber defined in a timing member that has metering orifices. Such orifices regulate the flow of the inflation gas to the inflatable. The confining member is able to withstand significant pressures without rupturing. Each of the confining member and the timing member is preferably made of a non-metallic material. The propellant includes a fuel-rich material and an oxidizer material, preferably ammonium nitrate.

Claims

1. A gas generating apparatus, comprising:

a propellant for generating products of combustion including a gas;

a confining member located outwardly of said propellant and being adjacent thereto, said confining member including a plurality of spaced holes having an unexpanded state and an expanded state and in which the size of each of said holes in said expanded state is at least 10% greater than the size of each of said holes in said unexpanded state, said holes being defined by at least one of the following;

(a) said holes being present before activation of said propellant; and

(b) said holes being covered by weakened areas before activation of said propellant;

a timing member located outwardly of said confining member for regulating flow of gas; and

an ignition assembly for igniting said propellant and operatively joined to said propellant.

2. A gas generating apparatus, comprising:

a propellant for generating products of combustion including a gas;

a confining member located outwardly of said propellant and being adjacent thereto, said confining member having holes at least after activation of said propellant;

a timing member located outwardly of said confining member for regulating flow of gas;

an ignition assembly for igniting said propellant and operatively joined to said propellant; and

at least one membrane extending from an inner wall from said timing member inwardly thereof and in which said at least one membrane absorbs heat from the gas.

3. A gas generating apparatus that can be operably connected to an inflatable, comprising:

a propellant for generating products of combustion including at least a propellant gas when activated;

a confining member surrounding said propellant, said confining member allowing passage of the propellant gas;

a timing member located outwardly of said confining member and including a number of orifices for regulating flow of the propellant gas, at least a majority of each of said confining member and said timing member being disposed inside of the inflatable when the gas generating apparatus is operably connected to the inflatable; and

an ignition assembly for igniting said propellant and operatively joined thereto;

wherein each of said number of timing member orifices separately communicates with the inflatable and in which the propellant gas flows substantially radially from each of said orifices into the inflatable.

4. An apparatus, as claimed in claim 3, wherein:

said confining member is made of a material that withstands a pressure of at least about 3,000 psi.

5. An apparatus, as claimed in claim 3, wherein:

each of said confining member and said timing member is substantially non-metallic.

6. An apparatus, as claimed in claim 3, wherein:

said propellant includes a fuel-rich material, an oxidizer material and a porosity-producing material.

7. An apparatus, as claimed in claim 3, wherein:

said propellant has a cross-sectional area and said confining member has an inner diameter with a cross-sectional area that defines a ratio of said cross-sectional area of said propellant to said cross-sectional area of said inner diameter of said confining member being in the range of about 0.10-0.60.

8. An apparatus, as claimed in claim 3, wherein:

said propellant has an oxidizer material that includes ammonium nitrate.

9. An apparatus, as claimed in claim 3, wherein:

said propellant includes a uniform mixture of a fuel-rich material, an oxidizer material and a porosity-producing composition.

10. An apparatus, as claimed in claim 3, further including:

at least one membrane joined to said timing member and extending inwardly thereof for absorbing heat from the gas.

11. A gas generating apparatus, comprising:

a propellant for generating products of combustion including at least one gas when activate;

,

a confining member surrounding said propellant, said confining member allowing passage of the gas;

a timing member located outwardly of said confining member and including a number of metering orifices for regulating flow of the gas; and

an ignition assembly for igniting said propellant and operatively joined thereto;

wherein said propellant has a cross-sectional area and said confining member has an inner diameter with a cross-sectional area, a ratio being defined by said cross-sectional area of said propellant to said cross-sectional area of said inner diameter of said confining member, said ratio being in the range of about 0.10-0.60 and in which a gap area is disposed between said cross-sectional area of said propellant and said inner diameter cross-sectional area of said confining member and a center bore is disposed interiorly of said cross-sectional area of said propellant.

12. A gas generating apparatus, comprising:

a propellant including a first end and a second end and having an outer surface and a length, said propellant for generating products of combustion including a propellant gas;

a confining member located outwardly of said propellant and being adjacent thereto, said confining member allowing passage of the propellant gas;

at least one of;

(a) a bore devoid of propellant located inwardly of said outer surface of said propellant and extending along at least portions of said length of said propellant and (b) a gap located between said confining member and said outer surface of said propellant and extending along at least portions of said length of said propellant;

a timing member located outwardly of said confining member for regulating flow of gas; and

an ignition assembly for igniting said propellant and operatively joined to said propellant;

wherein, after activation of said propellant, a combustion wave is generated in which ignition of said propellant proceeds from said first end of said propellant to said second end thereof, said combustion wave having a propagation rate of at least 100 meters of said propellant/second and in which said propagation rate of said combustion wave is a function of said at least one of said bore and said gap.

13. An apparatus, as claimed in claim 12, wherein:

said propellant has a length-to-diameter ratio and said ratio is at least about 100 in providing said combustion wave.