Secondary chamber combustion control mechanism

• US 9,643,565 B1
• Filed: 03/26/2015
• Issued: 05/09/2017
• Est. Priority Date: 03/26/2014
• Status: Active Grant

• Current Assignee: Joyson Safety Systems Acquisition, LLC
• Original Assignee: TK Holdings Incorporated (Ningbo Junsheng Investment Group Co., Ltd.)
• Inventors: Henck, Jeremy M.
• Primary Examiner(s): GOODEN JR, BARRY J
• Application Number:
  US14/670,373
• Time in Patent Office: 775 Days
• CPC Class Codes: B60R 2021/2633 with a plurality of inflation levels
• CPC Class Codes: B60R 2021/2642 comprising a plurality of combustion chambers or sub-chambers
• CPC Class Codes: B60R 21/263 using a variable source, e.g. plural stage or controlled output hybrid inflators B60R21/272
• CPC Class Codes: B60R 21/264 using instantaneous generation of gas, e.g. pyrotechnic B60R21/268 takes precedence
• CPC Class Codes: C06D 5/00 Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets explosive compositions containing an oxidizer, fuels for rocket engines intended for reaction with an oxidant other than air C06B

Abstract

A gas generating system includes a primary combustion chamber and a secondary combustion chamber. The secondary chamber includes a shell and a cap secured to the shell such that the cap is movable in a first direction responsive to a pressure differential wherein a pressure within the shell is greater than a pressure exterior of the shell. At least one gas flow passage is bounded by the shell and by a cavity extending along an exterior of the cap.

Claims

1. A gas generating system comprising a primary combustion chamber and a secondary combustion chamber, the secondary chamber including:

a shell;

a cap secured to the shell such that the cap is movable in a first direction responsive to a pressure differential wherein a pressure within the shell is greater than a pressure exterior of the shell; and

at least one gas flow passage defined between the shell and a cavity defined along an exterior surface of the cap,

wherein a portion of the exterior surface of the cap that defines an open end of the cavity is positioned entirely within the shell and remains in the shell before, during, and after combustion of gas generant in the primary and secondary combustion chambers.

2. The system of claim 1 wherein the cavity has a closed end opposite the open end, and wherein the closed end is positioned so as to exit the shell responsive to movement of the cap in the first direction, thereby forming a gas exit opening enabling gas flow from the shell.

3. An airbag module comprising a gas generating system in accordance with claim 1.

4. A vehicle occupant protection system comprising a gas generating system in accordance with claim 1.

5. A vehicle comprising a gas generating system in accordance with claim 1.

6. The system of claim 1 wherein the at least one gas flow passage comprises a plurality of gas flow passages, each of said gas flow passages defined between the shell and by an associated cavity defined along the exterior surface of the cap.

7. The system of claim 6 wherein a first passage of the plurality of passages has a first length and a second passage of the plurality of passages has a second length different from the first length.

8. A gas generating system comprising a primary combustion chamber and a secondary combustion chamber, the secondary chamber including a shell and a cap secured to the shell such that the cap is movable in a first direction responsive to a pressure differential wherein a pressure within the shell is greater than a pressure exterior of the shell, wherein the cap and the shell define at least one gas flow passage therebetween, the at least one gas flow passage being structured such that a cross-sectional area of an entry into the at least one gas flow passage from the secondary chamber remains constant as the cap moves in the first direction, wherein the entry into the at least one gas flow passage is defined by a portion of an outer perimeter surface of the cap and an inner surface of the shell, and the portion of the cap defining the entry remains in the shell before, during, and after combustion of gas generant in the primary and secondary combustion chambers.

9. The system of claim 8 wherein the cap and the shell are structured to form a plurality of gas flow passages therebetween.

10. The system of claim 8 wherein the cap is movably secured to the shell so as to prevent fluid communication between the primary and secondary chambers prior to activation of the gas generating system.

11. The system of claim 8 wherein the portion of the cap defining the at least one gas flow passage is positioned within the shell prior to activation of the gas generating system.

12. An airbag module comprising a gas generating system in accordance with claim 8.

13. A vehicle occupant protection system comprising a gas generating system in accordance with claim 8.

14. A vehicle comprising a gas generating system in accordance with claim 8.

15. The system of claim 8 wherein the at least one gas flow passage comprises a gas exit opening, and a cross-sectional area of the gas exit opening increases as the cap moves in the first direction.

16. The system of claim 15 wherein the cap and the shell are structured such that motion of the cap in the first direction is limited to a first distance from the shell, by contact with another element of the gas generating system, and wherein a ratio D/d_SHELL is within the range 0<

D/d_SHELL<

0.5, where d_SHELL is an outer radius of the shell and D is the first distance from the shell moved by the cap.

17. The system of claim 8 wherein the secondary combustion chamber resides within the primary combustion chamber.

18. The system of claim 17 wherein the cap is structured so as to abut the shell to form a substantially gas-tight seal therebetween responsive to a pressure differential wherein a pressure exterior of the shell is greater than a pressure inside the shell.

19. The system of claim 8 wherein the portion of the outer perimeter surface of the cap defines a cavity extending along the outer perimeter surface of the cap.

20. The system of claim 19 wherein the cavity has an open end positioned within the shell and a closed end opposite the open end, and wherein the closed end is positioned so as to exit the shell responsive to movement of the cap in the first direction, thereby forming the gas exit opening.

21. A gas generating system comprising a primary combustion chamber and a secondary combustion chamber, the secondary chamber including:

a shell;

a cap secured to the shell such that the cap is movable in a first direction responsive to a pressure differential wherein a pressure within the shell is greater than a pressure exterior of the shell; and

a plurality of gas flow passages, each passage bounded by the shell and by an associated cavity extending along an exterior of the cap,

wherein a first passage of the plurality of passages has a first length and a second passage of the plurality of passages has a second length different from the first length.