Apparatus for suppressing a fire

• US 5,613,562 A
• Filed: 08/28/1996
• Issued: 03/25/1997
• Est. Priority Date: 06/24/1993
• Status: Expired due to Term

• Current Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Original Assignee: OLIN Aerospace Company
• Inventors: Poole, Donald R., Holland, Gary F., Mitchell, Robert M., Galbraith, Lyle D.
• Primary Examiner(s): Pike, Andrew C.
• Application Number:
  US08/704,214
• Time in Patent Office: 209 Days
• Field of Search: 149/19.6, 149/35, 149/36, 149/61, 149/77, 169/5, 169/6, 169/7, 169/8, 169/9, 169/11, 169/12, 169/26, 169/27, 169/28, 169/30, 169/35, 169/43, 169/44, 169/45, 169/46, 169/47, 169/60, 169/61, 169/62, 169/71, 169/72, 169/78, 169/84, 169/85, 252/2, 252/3, 252/4, 252/5, 252/6, 252/7
• 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

There is disclosed an apparatus for suppressing a fire. The apparatus includes a gas generator containing as a propellant, a mixture of a fuel, strontium nitrate as an oxidizer, and magnesium carbonate. When the propellant is ignited, a nitrogen rich effluent is generated that is effective to suppress the fire. By providing the propellant with at least 35%, by weight, of magnesium carbonate, the generation of effluent by-products that are corrosive to aluminum is inhibited.

Claims

1. An apparatus for suppressing a fire, said apparatus comprising:

a gas generator containing a propellant that is a mixture of a fuel, strontium nitrate as an oxidizer, and magnesium carbonate, wherein the magnesium carbonate content of said propellant is at least 35% by weight that is sufficient to inhibit the generation of effluent by-products that are corrosive to aluminum; and

a passageway between said gas generator and said fire.

2. The apparatus of claim 1 wherein a fire suppressant selected from the group consisting of magnesium hydroxide, calcium hydroxide, strontium hydroxide, barium hydroxide, aluminum hydroxide, and potassium hydroxide is mixed with said propellant.

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

1 to about 1;

2.

4. The apparatus of claim 3 wherein said fuel is 5-aminotetrazole.

5. The apparatus of claim 4 wherein said propellant contains from about 35% to about 70%, by weight, of said magnesium carbonate.