Propellant cage for an inflator, inflator comprising such propellant cage operating method and method of guiding a shock wave of an inflator

Patent metadata

Field	Value
Publication number	US-11077820-B2
Application number	US-201916409971-A
Country	US
Kind code	B2
Filing date	May 13, 2019
Priority date	May 18, 2018
Publication date	Aug 3, 2021
Grant date	Aug 3, 2021

Abstract

The invention relates to a propellant cage ( 10 ) for an inflator, especially for a tubular inflator of an airbag module, comprising a substantially tubular base ( 11 ) which forms, on the one hand, a gas inlet opening ( 12 a ) and, on the other hand, a gas outlet opening ( 12 b ) along its longitudinal axis (L), wherein at least one lateral gas flow opening ( 13 ) is configured in a circumferential wall ( 12 ) of the base ( 11 ), wherein the base ( 11 ) includes a radially outwardly extending collar ( 11 c ) having at least one frontal gas flow opening ( 14 ) in the area of the gas flow opening ( 12 c ).

First claim

The invention claimed is:

1. A propellant cage ( 10 ) for an inflator of an airbag module, comprising a substantially tubular base ( 11 ) which along its longitudinal axis (L) forms a gas inlet opening ( 12 a ) and a gas outlet opening ( 12 c ), the base ( 11 ) defining a passageway that longitudinally extends through the propellant cage ( 10 ) from the gas inlet opening ( 12 a ) to the gas outlet opening ( 12 c ), at least one lateral gas flow opening ( 13 ) being formed in a circumferential wall ( 12 ) of the base ( 11 ), wherein the base ( 11 ) includes a radially outwardly extending collar ( 11 c ) which has at least one frontal gas flow opening ( 14 ) in the area of the gas outlet opening ( 12 c ).

2. The propellant cage ( 10 ) according to claim 1 , wherein the base ( 11 ) includes a substantially funnel-shaped portion ( 11 b ) widening toward the gas outlet opening ( 12 c ), and wherein the at least one lateral gas flow opening ( 13 ) is arranged in the funnel-shaped portion ( 11 b ) or is disposed in a hollow-cylindrical portion ( 11 a ) of the base ( 11 ) comprising the gas inlet opening ( 12 a ).

3. The propellant cage ( 10 ) according to claim 1 , wherein at least one of the at least one lateral gas flow opening ( 13 ) and the at least one frontal gas flow opening ( 14 ) is designed to be at least one of circular, slotted, and gill-type.

4. The propellant cage ( 10 ) according to claim 3 , wherein the at least one lateral gas flow opening ( 13 ) is formed by a radially inwardly shaped part ( 15 ) of the circumferential wall ( 12 ) of the base ( 11 ).

5. The propellant cage ( 10 ) according to claim 4 , wherein the shaped part ( 15 ) of the circumferential wall ( 12 ) forms a flow guiding element by which part of an axial ignition gas flow can be deflected to the outside.

6. The propellant cage ( 10 ) according to claim 2 , wherein at least one of the circumferential wall ( 12 ), the funnel-shaped portion ( 11 b ), and the hollow-cylindrical portion ( 11 a ) comprises plural lateral gas flow openings ( 13 ) which jointly form a hole pattern.

7. The propellant cage ( 10 ) according to claim 6 , wherein the lateral gas flow openings ( 13 ) of the hole pattern are configured to be geometrically different, wherein the lateral gas flow openings ( 13 ) are arranged to be regularly or irregularly distributed in the circumferential direction and/or in the longitudinal direction of the base ( 11 ).

8. The propellant cage ( 10 ) according to claim 2 , wherein the base ( 11 ) is integrally formed and the hollow-cylindrical portion ( 11 a ) merges into the funnel-shaped portion ( 11 b ), wherein the lateral gas flow openings ( 13 ) and/or the hole pattern extend(s) into the hollow-cylindrical portion ( 11 a ) and/or into the funnel-shaped portion ( 11 b ).

9. An inflator for an airbag module comprising a tubular housing ( 31 ) and a propellant cage ( 10 ) according to claim 1 , wherein the propellant cage ( 10 ) is arranged inside the tubular housing ( 31 ), and wherein the tubular housing ( 31 ) delimits a propellant chamber ( 17 ) which includes gas-generating propellant bodies.

10. The inflator according to claim 9 , wherein the at least one lateral gas flow opening ( 13 ) forms a gas inlet of the propellant chamber ( 17 ) and the at least one frontal gas flow opening ( 14 ) forms a gas outlet of the propellant chamber ( 17 ).

11. The inflator according to claim 9 , wherein an igniter unit ( 20 ) is arranged in the tubular housing ( 42 ), the igniter unit ( 20 ) being in fluid communication with the gas inlet opening ( 12 a ) of the propellant cage ( 10 ), wherein the igniter unit ( 20 ) is inserted into the gas inlet opening ( 12 a ) and includes an inlet-side bursting diaphragm ( 24 ) that closes the gas inlet opening ( 12 a ).

12. The inflator according to claim 9 , wherein the housing ( 31 ) forms a compressed gas tank ( 30 ) which is filled with biased compressed gas, with the collar ( 11 c ) of the propellant cage ( 10 ) being adjacent to a circumferential taper ( 32 ) of the housing ( 31 ).

13. An airbag module comprising an inflator, an airbag inflatable by the inflator and a securing unit for attaching the airbag module to a vehicle, wherein the inflator is configured according to claim 9 .

14. A vehicle safety system comprising the inflator of claim 9 , an airbag inflatable by inflator as part of an airbag module, and an electronic control unit for activating the inflator when a trigger situation is given.

15. A method of operating an inflator according to claim 9 , comprising the following steps of:
triggering an igniter unit ( 20 ) for generating ignition gas inside an ignition chamber ( 23 );
axially introducing the ignition gas into a flow passage ( 12 b ) tubularly encompassed by a propellant cage ( 10 );
discharging part of the ignition gas via lateral gas flow openings ( 13 ) of the propellant cage ( 10 ) into a propellant chamber ( 17 ) radially inwardly delimited by the propellant cage ( 10 );
igniting propellant bodies, especially propellant pellets, within the propellant chamber ( 14 ) by the discharged part of the ignition gas, wherein propellant gas is generated; and
passing the propellant gas out of the propellant chamber ( 17 ) through frontal gas flow openings ( 14 ) of the propellant cage ( 10 ).

16. A method of guiding a shock wave within an inflator claim 9 , comprising the following steps of:
triggering an igniter unit ( 20 ) for generating excess pressure inside an ignition chamber ( 23 );
generating a shock wave by bursting an inlet-side bursting diaphragm ( 24 ) by means of the excess pressure, the bursting diaphragm being disposed in the area of a gas inlet opening ( 12 a ) of a tubular base ( 11 ) of a propellant cage ( 10 );
guiding the shock wave along the base ( 11 ); and
radially widening the shock wave along a funnel-shaped widening portion ( 11 b ) of the base ( 11 ).

17. The propellant cage ( 10 ) according to claim 6 , wherein the lateral gas flow openings ( 13 ) of the hole pattern are configured to be at least one of circular, slotted, and gill-type, and wherein the lateral gas flow openings ( 13 ) are arranged to be regularly or irregularly distributed in the circumferential direction and/or in the longitudinal direction of the base ( 11 ).

18. The propellant cage ( 10 ) according to claim 1 , wherein the propellant cage ( 10 ) is formed as a single piece.

Assignees

• Trw Airbag Sys Gmbh

Inventors

• Hillmann Daniel
• Jung Christian
• Seidl Lorenz
• Tautschnig Georg
• Tengler Wolfgang

Classifications

• B60R2021/26029

  Ignitors · CPC title

• B60R21/261

  with means other than bag structure to diffuse or guide inflation fluid · CPC title

• B60R2021/2612

  Gas guiding means, e.g. ducts · CPC title

• B60R21/272 Primary

  with means for increasing the pressure of the gas just before or during liberation, e.g. hybrid inflators · CPC title

• B60R21/274

  characterised by means to rupture or open the fluid source · CPC title