Rapid buring propellant charge for automobile air bag inflators, rocket motors, and igniters therefor

• US 4,798,142 A
• Filed: 08/18/1986
• Issued: 01/17/1989
• Est. Priority Date: 08/18/1986
• Status: Expired due to Fees

• Current Assignee: Morton-Thiokol, Inc. (Howmet Aerospace, Inc.), Alliant Techsystems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Morton-Thiokol, Inc. (Howmet Aerospace, Inc.)
• Inventors: Canterberry, J. B., Flanigan, David A.
• Primary Examiner(s): Nelson, Peter A.
• Application Number:
  US06/908,763
• Time in Patent Office: 883 Days
• Field of Search: 264/3.1-3.6, 428/909, 102/289-290
• US Class Current: 102/290
• CPC Class Codes: B60R 21/2644 using only solid reacting substances, e.g. pellets, powder
• CPC Class Codes: C06B 21/0083 Treatment of solid structures, e.g. for coating or impregnating with a modifier compositions therefor C06B23/00
• CPC Class Codes: C06B 45/00 Compositions or products which are defined by structure or arrangement of component of product explosive charges of particular form or shape F42B1/00, F42B3/00
• 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
• 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 5/16 characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder chemical composition C06B; F42B5/24 takes precedence

Abstract

A rapid burning propellant charge for applications including igniters, launch eject motors, and gas generators for automobile air gags. The propellant charge comprises a reticulated substrate having a quantity of interconnected ligaments and a coating of solid propellant material on the ligaments. In order to provide a large amount of surface area for a fast burn time, interstices are between coated ligaments to define propellant surface area for combustion. In applications where minimum smoke is desired, the reticulated substrate is preferably composed of carbon, graphite, or a non-combustible material, and the solid propellant material is preferably a minimum smoke type.

Claims

1. A propellant charge comprises a reticulated substrate having a quantity of interconnected ligaments and a coating of solid propellant material on said ligaments, said coating has a thickness such that interstices are between coated ligaments which interstices define propellant surface area for combustion.

2. A propellant charge according to claim 1 wherein said reticulated substrate is composed of a material selected from the group consisting of a minimum smoke material and a non-combustible material, and said solid propellant material is a minimum smoke propellant.

3. A propellant charge according to claim 1 wherein said reticulated substrate is composed of a material selected from the group consisting of carbon and graphite.

4. A method of making a propellant charge comprises the steps of:

a. preparing a reticulated substrate having a quantity of interconnected ligaments,

b. coating the ligaments with a solid propellant material, and

c. maintaining the thickness of the coating such that interstices are between coated ligaments which interstices define propellant surface area for combustion.

5. A method according to claim 4 wherein the step of coating the ligaments comprises dip coating the ligaments in a propellant lacquer prepared by dissolving the solid propellant material in a solvent, and further comprises allowing the dip coated ligaments to dry.

6. A method according to claim 4 wherein the step of coating the ligaments comprises spraying propellant material which is dissolved in a solvent onto the ligaments and allowing the spray coated ligaments to dry.

7. A method according to claim 4 further comprises composing the reticulated substrate from a non-combustible or minimum smoke material, and composing the solid propellant material from a minimum smoke propellant.