Apparatus for suppressing a fire

• US 5,423,384 A
• Filed: 05/25/1994
• Issued: 06/13/1995
• Est. Priority Date: 06/24/1993
• Status: Expired due to Term

• Current Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Original Assignee: OLIN Corporation
• Inventors: Holland, Gary F., Mitchell, Robert M., Galbraith, Lyle D., Poole, Donald R.
• Primary Examiner(s): Pike, Andrew C.
• Application Number:
  US08/248,932
• Time in Patent Office: 384 Days
• Field of Search: 169/5, 169/6, 169/7, 169/8, 169/9, 169/11, 169/12, 169/26, 169/27, 169/28, 169/30, 169/71, 169/72, 169/78, 169/84, 169/85, 169/35, 169/43, 169/44, 169/45, 169/46, 169/47, 169/60, 169/61, 169/62, 252/2, 252/3, 252/4, 252/5, 252/6, 252/7, 252/8, 149/19.6, 149/35, 149/36, 149/61, 149/77, 149/21
• US Class Current: 169/12
• CPC Class Codes: A62C 35/023 the extinguishing material being expelled by compressed gas, taken from storage tanks, or by generating a pressure gas for foam generation A62C5/02
• CPC Class Codes: A62C 99/0018 using gases or vapours that do not support combustion, e.g. steam, carbon dioxide
• CPC Class Codes: C06D 5/06 by reaction of two or more solids

Abstract

An apparatus for suppressing a fire comprises a gas generator containing a propellant and a fire suppressant as a mixture of compacted powders. The average diameter of a fire suppressant particle is larger than the average diameter of a propellant particle and the larger fire suppressant particles form discrete cooling sites that do not dramatically reduce the propellant burn rate.

Claims

1. An apparatus for suppressing a fire comprising:

a gas generator containing a propellant and a fire suppressant as a mixture of compacted powders with the average diameter of a fire suppressant particle being larger than the average diameter of a propellant particle; and

a passageway between said gas generator and said fire.

2. The apparatus of claim 1 wherein said fire suppressant is selected from the group consisting of magnesium carbonate, magnesium hydroxide, calcium hydroxide, strontium hydroxide, barium hydroxide, aluminum hydroxide, potassium sulfate, and mixtures thereof.

3. The apparatus of claim 2 wherein the average diameter of a fire suppressant particle is from about 150 microns to about 200 microns and the average diameter of a propellant particle is from about 50 microns to about 75 microns.

4. The apparatus of claim 3 wherein said propellant is a mixture of a nitrogen rich fuel and an oxidizer in a fuel-to-oxidizer ratio, by weight, of from about 1:

1 to about 1;

2.

5. The apparatus of claim 4 wherein said fuel is 5-aminotetrazole and said oxidizer is selected from the group consisting of strontium nitrate, potassium chlorate, and mixtures thereof.

6. The apparatus of claim 5 wherein the fire suppressant is at least 35% by weight magnesium carbonate to inhibit the generation of corrosive effluent by-products.

7. The apparatus of claim 6 wherein said oxidizer is strontium nitrate.

8. The apparatus of claim 4 wherein said fuel is selected from the group consisting of 5-aminotetrazole and guanidine nitrate, said oxidizer is strontium nitrate, and said flame suppressant is at least 35% by weight magnesium carbonate.