Container for gas generating propellant

• US 4,414,902 A
• Filed: 12/29/1980
• Issued: 11/15/1983
• Est. Priority Date: 12/29/1980
• Status: Expired due to Term

• Current Assignee: Ford Motor Company
• Original Assignee: Ford Motor Company
• Inventors: Strasser, Robert A., Goch, Stephen W.
• Primary Examiner(s): TUDOR, HAROLD JAY
• Application Number:
  US06/220,347
• Time in Patent Office: 1,051 Days
• Field of Search: 280/736, 280/737, 280/741, 220/89 A, 220/89 B, 102/530, 102/531, 102/314, 102/370, 428/461, 428/483, 229/3.5 MF
• US Class Current: 102/531
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: F42B 3/04 for producing gas under pressure generators of inflation fluid especially adapted for vehicle air bags B60R21/26
• CPC Class Codes: F42B 8/04 Blank cartridges, i.e. primed cartridges without projectile but containing an explosive or combustible powder charge
• CPC Class Codes: Y10T 428/31692 Next to addition polymer from unsaturated monomers
• CPC Class Codes: Y10T 428/31797 Next to addition polymer from unsaturated monomers

Abstract

A container and a method for making the same for a gas generating propellant such as used in vehicle air bag systems. The container comprises an elongated thin wall metal cylinder having a plurality of perforations extending substantially the length thereof. A hermetic liner is attached to the inner surface of the cylinder to seal the perforated area of the wall. The hermetic liner comprises a laminated plastic film and metal foil composite having a thickness less than that of the cylinder wall and being rupturable under the pressure of gas generated within the cylinder. The ends of the cylinder are closed by metal end caps.

Claims

1. A container for a gas generating propellant comprising:

an elongated thin wall metal cylinder having a plurality of perforations extending substantially around the periphery of the cylinder and for substantially the length of the latter;

a hermetic liner sealingly attached to the imperforate portions of the inner surface of the cylinder to seal the perforated area of the wall;

the hermetic liner comprising a laminated plastic film and metal foil composite having a thickness less than that of the cylinder wall and being rupturable under the pressure of gas generated within the cylinder;

the laminated plastic film and metal foil composite including a first layer of an ionomer resin film, a layer of aluminum foil, a second layer of ionomer resin film, and a layer of polyester film;

the first layer of ionomer resin film being in contact with the inner metal surface of the cylinder;

the layer of aluminum foil being between the two layers of ionomer resin films;

the layer of polyester film covering the second layer of ionomer film to isolate the latter from the gas generating propellant; and

metal end caps closing the ends of the cylinder.

2. A container according to claim 1, in which:

the wall of the metal cylinder is approximately 0.3±

0.03 millimeters thick;

and the first layer of ionomer resin has a thickness of approximately 0.08 millimeters;

the layer of aluminum foil has a thickness of approximately 0.1 millimeter;

the second layer of ionomer resin has a thickness of approximately 0.05 millimeters;

and the layer of polyester film has a thickness of approximately 0.048 millimeters;

the total thickness of the laminated hermetic liner not exceeding approximately 0.278 millimeters in preinstalled condition.