Hybrid inflator, airbag unit and vehicle safety system comprising such hybrid inflator as well as method of forming a shock wave

Patent metadata

Field	Value
Publication number	US-11247634-B2
Application number	US-201715440244-A
Country	US
Kind code	B2
Filing date	Feb 23, 2017
Priority date	Mar 11, 2016
Publication date	Feb 15, 2022
Grant date	Feb 15, 2022

Abstract

The invention relates to a hybrid inflator especially for a vehicle safety system, comprising an igniter (10), a combustion chamber (16) including a propellant charge (18) which is separated from the igniter (10) by a first bursting element (14) held by a bursting element holder (13), and comprising a compressed gas tank (20) filled with compressed gas and having at feast one discharge opening, the discharge opening being closed by a second bursting element (24) and the compressed gas tank (20) being fluid-communicated with the combustion chamber (16) so that the compressed gas surrounds the propellant charge (18). The invention excels by the fact that the bursting element holder (13) at least in portions delimits an ignition chamber (30) containing a booster charge (15), wherein a shock wave (SW) for opening the second bursting element (24) can be formed only when both the igniter (10) and the booster charge (15) have been ignited and, respectively, activated. The invention further deals with an airbag unit and a vehicle safety system comprising said hybrid inflator or said airbag unit. Moreover, the invention states a method of forming a shock wave within a hybrid inflator.

First claim

The invention claimed is:

1. A hybrid inflator, especially for a vehicle safety system, having an axial longitudinal direction (A) and comprising:
an igniter ( 10 ),
a combustion chamber ( 16 ) including a propellant charge ( 18 ) which is separated from the igniter ( 10 ) by a first bursting element ( 14 ) held by a bursting element holder ( 13 ) with the propellant charge ( 18 ) being located outside the bursting element holder ( 13 ), and comprising
a compressed gas tank ( 20 ) filled with compressed gas which includes at least one discharge opening, with the at least one discharge opening being closed by a second bursting element ( 24 ) and the compressed gas tank ( 20 ) being fluid-communicated with the combustion chamber ( 16 ) so that the compressed gas surrounds the propellant charge ( 18 ),
wherein the bursting element holder ( 13 ) at least in portions delimits an ignition chamber ( 30 ) containing a booster charge ( 15 ) that contacts the bursting element holder ( 13 ) and the igniter ( 10 ) prior to activation of the igniter ( 10 ), the first bursting element ( 14 ) separating the ignition chamber ( 30 ) from the combustion chamber ( 16 ), wherein a shock wave (SW) for opening the second bursting element ( 24 ) can be formed only when both the igniter ( 10 ) and the booster charge ( 15 ) have been ignited and activated, wherein the ignition chamber ( 30 ) which is delimited at least in portions by the bursting element holder ( 13 ) extends substantially completely through the combustion chamber ( 16 ).

2. The hybrid inflator according to claim 1 , wherein the first bursting element ( 14 ) is arranged so that a shock wave (SW) capable of being triggered by the igniter ( 10 ) and the booster charge ( 15 ) can be initiated and triggered in the axial longitudinal direction (A) of the hybrid inflator only downstream of the propellant charge ( 18 ) or starting from a second plane (E 2 ) delimiting the propellant charge ( 18 ) at its end facing away from the igniter ( 10 ).

3. The hybrid inflator according to claim 1 , wherein the bursting element holder ( 13 ) including the first bursting element ( 14 ) and at least one end face of the igniter ( 10 ) define the ignition chamber ( 30 ) in which the booster charge ( 15 ) exposed to atmospheric pressure prior to activation of the igniter ( 10 ) is accommodated.

4. The hybrid inflator according to claim 1 , wherein the propellant charge ( 18 ) comprises propellant pellets ( 18 a ) arranged within a ring-shaped cage ( 17 ), with the ignition chamber ( 30 ) or the bursting element holder ( 13 ) preferably extending through a central through-passage ( 31 ) of the cage ( 17 ).

5. A vehicle safety system comprising a hybrid inflator according to claim 1 .

6. The hybrid inflator according to claim 1 , wherein the booster charge is separate from the igniter.

7. The hybrid inflator according to claim 1 , wherein the first bursting element closes an end of the bursting element holder that is opposite the igniter.

8. The hybrid inflator according to claim 1 , wherein the ignition chamber is delimited by the igniter and the first bursting element.

9. The hybrid inflator according to claim 1 , wherein the igniter is exposed to the booster charge prior to activation of the igniter.

10. The hybrid inflator according to claim 1 , wherein the first and second bursting elements are located at opposite longitudinal ends of the compressed gas tank and exposed to the compressed gas prior to activation of the igniter.

11. The hybrid inflator according to claim 1 , wherein a shock wave (SW) triggered by the igniter and booster charge travels through the compressed gas in the compressed gas tank prior to rupturing the second bursting element.

12. The hybrid inflator according to claim 1 , wherein the compressed gas contacts the propellant charge prior to activation of the igniter.

13. A gas bag unit, especially airbag unit, for a vehicle safety system comprising a hybrid inflator according to claim 1 .

14. A vehicle safety system comprising an airbag unit according to claim 13 .

15. A method of forming a shock wave within a hybrid inflator according to claim 1 , the method comprising the following steps of:
a) activating the igniter ( 10 ); then
b) igniting the booster charge ( 15 ) arranged downstream of the igniter ( 10 ) in the axial longitudinal direction (A) of the hybrid inflator and arranged in the ignition chamber ( 30 ); after that
c) opening a bursting element of the ignition chamber by at least partly burning off the booster charge so that a shock wave (SW) is generated; and after that
d) igniting the propellant charge ( 18 ) within the combustion chamber ( 16 ) which is fluid-communicated with the opened ignition chamber ( 30 ).

16. The method according to claim 15 , wherein the shock wave (SW) is generated or forms in the axial longitudinal direction (A) of the hybrid inflator downstream of the propellant charge ( 18 ) arranged in the combustion chamber ( 16 ).

17. A hybrid inflator, especially for a vehicle safety system, having an axial longitudinal direction (A) and comprising:
an igniter ( 10 ),
a combustion chamber ( 16 ) including a propellant charge ( 18 ) which is separated from the igniter ( 10 ) by a first bursting element ( 14 ) held by a bursting element holder ( 13 ) with the propellant charge ( 18 ) being located outside the bursting element holder ( 13 ), and comprising
a compressed gas tank ( 20 ) filled with compressed gas which includes at least one discharge opening, with the at least one discharge opening being closed by a second bursting element ( 24 ) and the compressed gas tank ( 20 ) being fluid-communicated with the combustion chamber ( 16 ) so that the compressed gas surrounds the propellant charge ( 18 ),
wherein the bursting element holder ( 13 ) at least in portions delimits an ignition chamber ( 30 ) containing a booster charge ( 15 ) exposed to the bursting element holder ( 13 ) prior to activation of the igniter ( 10 ), the first bursting element ( 14 ) separating the ignition chamber ( 30 ) from the combustion chamber ( 16 ), wherein a shock wave (SW) for opening the second bursting element ( 24 ) can be formed only when both the igniter ( 10 ) and the booster charge ( 15 ) have been ignited and activated,
wherein the first bursting element ( 14 ) is arranged so that a shock wave (SW) capable of being triggered by the igniter ( 10 ) and the booster charge ( 15 ) can be initiated and triggered in the axial longitudinal direction (A) of the hybrid inflator between a first plane (El) delimiting the propellant charge ( 18 ) at its end facing the igniter ( 10 ) and a second plane (E 2 ) delimiting the propellant charge ( 18 ) at its end facing away from the igniter ( 10 ), and
wherein the axial longitudinal direction (A) of the hybrid inflator, starting from the igniter ( 10 ), a deflector ( 25 ) including a central through-hole ( 27 ) is arranged behind the combustion chamber ( 16 ), wherein a ring-shaped bulge ( 26 ) is formed in the deflector ( 25 ) so that ignition gas released by the booster charge ( 15 ) can be deflected radially outwardly and/or along the longitudinal axis opposite to the axial longitudinal direction (A).

Assignees

• Trw Airbag Sys Gmbh

Inventors

• Bierwirth Sebastian

Classifications

• B60R21/2644 Primary

  using only solid reacting substances, e.g. pellets, powder · CPC title

• B60R21/274

  characterised by means to rupture or open the fluid source · 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

• B60R2021/26029

  Ignitors · CPC title

• B60R21/268

  using instantaneous release of stored pressurised gas {(B60R21/26005 takes precedence)} · CPC title