Igniter for a pyrotechnic gas bag inflator

• US 4,358,998 A
• Filed: 02/04/1980
• Issued: 11/16/1982
• Est. Priority Date: 02/04/1980
• Status: Expired due to Term

• Current Assignee: Autoliv ASP Incorporated (Autoliv Incorporated)
• Original Assignee: Thiokol Corporation (Howmet Aerospace, Inc.)
• Inventors: Schneiter, Fred E., Cadwell, David C.
• Primary Examiner(s): TUDOR, HAROLD JAY
• Application Number:
  US06/118,344
• Time in Patent Office: 1,016 Days
• Field of Search: 102/39, 102/276-280, 102/202, 102/202.1, 102/202.13, 102/275.3, 102/275.7, 102/530, 102/531, 280/736, 280/741
• US Class Current: 102/530
• CPC Class Codes: B60R 2021/26041 of elongated shape
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: F42C 19/0826 comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators

Abstract

For an inflator for pyrotechnically inflating protective gas bags for vehicles, an igniter is provided which causes the propellant in the inflator to ignite in a progressive manner so as to inflate the bag slowly at the onset but more rapidly later as inflation progresses. The overall inflation time is very rapid but the slow onset of bag deployment starts gentle movement against a vehicle'"'"'s occupant and thus reduces the possibility of injury as compared with a more sudden movement by rapid inflation from the outset.

Claims

1. A dual pressure rise igniter for the propellant in a protective gas bag inflator comprising

a first igniter segment,

at least one additional igniter segment,

with igniter powder contained in each of said segments,

means for igniting said first igniter segment,

combustible fuse means including a delay propellant disc and a fuse, said delay propellant disc having a first side and a second side, said fuse having a first end and a second end,

a first tubular igniter powder enclosing housing for said first igniter segment, said delay propellant disc being positioned within said first housing with said first side thereof in contact with the igniter powder in said first housing,

a second tubular igniter powder enclosing housing for the next adjacent igniter segment,

said first and second housing each having at least one outlet port through the side wall thereof in communication with the igniter powder therein,

pressure sensitive cover means for the outlet port in each of said first and second housings, said cover means on said second housing being thicker than that on said first housing,

an interconnecting member having a hole therein, said fuse extending through said hole in said interconnecting member;

said first and second housings being interconnected by said interconnecting member in coaxial tandem arrangement with said first end of said fuse contacting said second side of said delay propellant disc in said first housing and with said second end of said fuse contacting the igniter powder in said second housing, and

additional cover means for the outlet port in said second housing for providing thermal protection from external heat for the igniter powder contained therein thereby to preclude ignition from external heat transfer prior to receipt of an ignition signal acting through said combustible fuse means.

2. The invention set forth in claim 1 wherein said pressure sensitive cover means for the outlet port in said first housing comprises a single thickness wrapping of pressure sensitive aluminum tape and said pressure sensitive cover means for the outlet port in said second housing comprises a quadruple thickness wrapping of pressure sensitive aluminum tape.

3. The invention set forth in claim 2 wherein said additional cover means for said second housing comprises a covering of silicone rubber tape.

4. The invention set forth in claim 3 wherein said first housing includes a first end and a second end and said second housing includes a third end and a fourth end, and further including a steel sleeve positioned in said first end of said first housing for supporting said delay propellant disc and wherein said interconnecting member is made of steel and has first and second cylindrical ends with a common longitudinal axis and including an intermediate shoulder, said hole being in alignment with said longitudinal axis, said first cylindrical end being positioned in said sleeve and said second cylindrical end being positioned in said third end of said second housing.

5. The invention set forth in claim 4 wherein said solid propellant disc contains 60 to 80% of ammonium perchlorate and up to 16 percent aluminum and polymer binder.

6. The invention set forth in claim 5 wherein said fuse comprises a lead sheathed pyrotechnic material having a flame propagation rate of about 8400 inches per second.

7. The invention set forth in claim 4 including first plug means closing said second end of said first housing, said first plug means being combustible, wherein said means for igniting said first igniter segment includes an initiator adjacent said second end of said first housing, and including second plug means for closing and sealing off said fourth end of said second housing.

8. The invention set forth in claim 7 with the igniter located inside an inflator in close proximity to propellant in the inflator and the outlet ports of said first and second housings in proximity to different areas of said propellant.