![]() The aircraft of claim 3 wherein said fire suppression system further comprises: a first flow control device on said first supply line and a second flow control device on said second supply line.ĥ. ![]() ![]() The aircraft of claim 2 wherein said fire suppression system further comprises a conduit network comprising: a main line fluidly coupled with said nozzle a first supply line fluidly coupling said inert gas source with said main line and a second supply line fluidly coupling said fire suppression agent source with said main line.Ĥ. The aircraft of claim 1 wherein said fire suppression system further comprises a nozzle positioned in said compartment, wherein said fire suppression mixture is introduced to said compartment by way of said nozzle.ģ. An aircraft comprising: a compartment and a fire suppression system comprising: an inert gas source in selective fluid communication with said compartment and a fire suppression agent source in selective fluid communication with said compartment, wherein an inert gas from said inert gas source and a fire suppression agent from said fire suppression agent source are at least partially combined to form a fire suppression mixture.Ģ. METHOD AND APPARATUS IN CONNECTION WITH SPRAYING HEAD AND PROTECTIVE ELEMENT OF SPRAYING HEADĪPPARATUS AND METHOD FOR INSTALLING FIRE SUPPRESSION FOAM DISPERSAL DEVICEĪPPARATUS AND METHOD TO MONITOR FOR FIRE EVENTS AND DYNAMICALLY ACTIVATE FIRE SPRINKLERSġ. SELF SERVICING FIRE EXTINGUISHER WITH INTERNAL MIXING AND EXTERNAL CO2 CHAMBER System and Method of Automatic Hose Bay Jam Preventionįire Truck Capable Of Rapid High-Rise RescuesįIRE RETARDANT DEVICE FOR PROTECTING WOODEN STRUCTURES FROM FIRE ![]()
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