초록 ▼

System and method for pressurizing and dispersing fire retardant from an aircraft, particularly aircraft structured and equipped for retarding or extinguishing forest fires, that includes a small power pack having a plenum operatively interconnecting a plurality of individual solid propellant gas ge

System and method for pressurizing and dispersing fire retardant from an aircraft, particularly aircraft structured and equipped for retarding or extinguishing forest fires, that includes a small power pack having a plenum operatively interconnecting a plurality of individual solid propellant gas generator devices each containing solid propellant materials that react pyrotechnically when initiated electrically to generate large quantities of high-pressure gas in a few seconds for discharging a liquid retardant reservoir.

대표청구항 ▼

1. A system for pressurizing and dispersing fire retardant from an aircraft, comprising: (a) a substantially closed reservoir for containing liquid, said reservoir having an inlet and an outlet; (b) a source of liquid fire retardant disposed within said reservoir; (c) a high pressure-manifold o

1. A system for pressurizing and dispersing fire retardant from an aircraft, comprising: (a) a substantially closed reservoir for containing liquid, said reservoir having an inlet and an outlet; (b) a source of liquid fire retardant disposed within said reservoir; (c) a high pressure-manifold operatively connected to said inlet of said reservoir; (d) a power pack operatively connected to said manifold and communicating therethrough with said inlet of said reservoir, said power pack including a plurality of solid propellant gas generator cartridges each containing solid propellant material that reacts pyrotechnically for generating propulsive pressurization gas for selectively discharging said liquid retardant from said outlet of said reservoir; and (e) a movable platform for supporting the system. 2. The system of claim 1 further comprising electrical means for selectively initiating one or more of said cartridges. 3. The system of claim 1 wherein said fire retardant comprises a material selected from the group consisting of ammonium phosphate, ammonium sulfate and ammonium polyphosphate. 4. The system of claim 1 wherein said reservoir has a capacity of about 4000 gallons. 5. The system of claim 1 wherein said propellant material is selected from the group consisting of sodium azide, ammonium nitrate, guanidine nitrate, cellulose acetate, strontium nitrate, 5-aminotetrazole and nitroguanidine.