Gaseous propellant fire extinguishing agent for aircraft dry chamber extinguishment
A fire extinguishing agent and propulsion technology, applied in fire prevention equipment and other directions, can solve the problems of high temperature of ejected gas and low fire extinguishing efficiency, and achieve the effects of fast cooling speed, high fire extinguishing efficiency and efficiency improvement.
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Embodiment 1
[0039] 21.8 parts of solid fuel 5-aminotetrazole
[0040] Oxidant ammonium nitrate 35.2 parts
[0041] Adhesive polybutyl acetate 3 parts
[0042] Coolant calcium carbonate 34.5 parts
[0043] Fire extinguishing agent Ammonium phosphate dry powder fire extinguishing agent 5 parts
[0044] Lubricant talcum powder 0.1 parts
[0045] Catalyst carbon black 0.4 parts
Embodiment 2
[0047] Solid fuel 3,6-bis(1hydro-1,2,3,4-tetrazol-5-amino)-1,2,4,5-tetrazine 15 parts
[0048] Oxidant strontium nitrate 5 parts
[0049] Adhesive polyvinyl alcohol 1 part
[0050] Coolant magnesium carbonate 31.5 parts
[0051] Fire extinguishing agent Sodium bicarbonate dry powder fire extinguishing agent 20 parts
[0052] Lubricant talcum powder 0.5 parts
[0053] Catalyst carbon black 2 parts
Embodiment 3
[0055] Solid fuel Nitroguanidine 34 parts
[0056]Oxidant potassium nitrate 10 parts, potassium perchlorate 10 parts
[0057] Adhesive 3 parts of polybutadiene, 2 parts of polyvinyl chloride
[0058] Coolant aluminum hydroxide 5 parts
[0059] Fire extinguishing agent Sodium bicarbonate dry powder fire extinguishing agent 5 parts
[0060] Lubricant mica 0.5 parts
[0061] Catalyst carbon black 0.2, graphite 0.3 parts
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