An inert gas-generating fire suppression composition is disclosed, consisting essentially of an oxidizer, comprising ammonium dinitramide and strontium nitrate, a fuel, comprising potassium isocyanurate, a gas-generate fuel, comprising guanidine nitrate and a quantity of carbon black.

A ratio controller includes a housing defining a mixing chamber. The housing has a water inlet configured to receive water from a water supply, an agent inlet configured to receive agent from an agent supply, an outlet configured to output an agent-water solution, a first pressure port extending through a sidewall of the housing at a first position proximate the water inlet, and a second pressure port extending through the sidewall of the housing at a second position proximate the mixing chamber.

A supply system for providing at least oxygen depleted air and water in a vehicle includes a catalytic converter, at least one hydrogen supply means, at least one air supply means, at least one outlet for oxygen depleted air, and a control unit coupled with the catalytic converter. The catalytic converter is couplable with the hydrogen supply means and is adapted for producing water under consumption of hydrogen from the at least one hydrogen supply means and oxygen. The catalytic converter is further couplable with the at least one air supply means for additionally producing oxygen depleted air. Further, the control unit is adapted for selectively operating the catalytic converter based on a demand of water and oxygen depleted air.

Fire suppression systems for aircraft are described. The fire suppression systems include a first fire suppression material source containing a first constituent, a second fire suppression material source containing a second constituent different from the first constituent, and a fluid supply line connecting the first fire suppression material source and the second fire suppression material source to at least one dispenser configured to dispense the first constituent in the form of a first agent in a high rate discharge operation to extinguish a detected fire, and to dispense the second constituent in the form of a second agent in a low rate discharge operation after the high rate discharge operation.

Fire suppression systems for aircraft are described. The fire suppression systems include a first fire suppression material source containing a first constituent, a second fire suppression material source containing a second constituent different from the first constituent, and a fluid supply line connecting the first fire suppression material source and the second fire suppression material source to at least one dispenser configured to dispense the first constituent in the form of a first agent in a high rate discharge operation to extinguish a detected fire, and to dispense the second constituent in the form of a second agent in a low rate discharge operation after the high rate discharge operation.

A panel (10) for use as a fire suppressing system which comprises a substrate (12) and an exothermic gas producing charge (14) wherein the exothermic gas producing charge (14) is integral with the substrate.

A fire suppression nozzle includes a body including a cylindrical portion having a first end and a second end and a conical portion connected to the second end of the cylindrical portion, a main channel extending through the cylindrical portion, a flow deflector connected to the body, and a flow foil ring positioned adjacent the flow deflector and the conical portion of the body. The flow deflector includes a top portion in alignment with the main channel, an annular flange extending out of a side of the flow deflector, and a conical base extending out of the side of the flow deflector at an angle.

A method of manufacturing a self-expanding fire-fighting foam solution is disclosed. Here, the method can include purging air from a container, wherein the purging is performed via flowing an inert gas into the container, such that substantially inert environment is created within the container. In addition, the method can further include dispensing or filling a pre-determined amount of foam concentrate into a container, dispensing or filling a pre-determined amount of water into the container, and mixing the foam concentrate and water within the container, wherein the mixed foam and water within the inert container provide the self-expanding fire-fighting foam solution and having a pH ranging from about 6.8 to 7.8 moles per liter.

A fire engine including a vehicle frame, a liquid nitrogen storage tank, a liquid nitrogen conveying pipeline, a gasification device, a plurality of electric valves, a water pipe adapter, a liquid nitrogen spray gun, and a mixed spray gun. The liquid nitrogen conveying pipeline includes a first pipeline and a second pipeline. The first pipeline connects the lower part of the liquid nitrogen storage tank, the gasification device, and the upper part of the liquid nitrogen storage tank sequentially in that order. The second pipeline connects the liquid nitrogen storage tank, an input end of the liquid nitrogen spray gun, and a first input end of the mixed spray gun. The mixed spray gun includes a first input end, a second input end, a liquid nitrogen nozzle, and a spray pipe. The spray pipe includes a contraction section, an expansion section, and an acceleration section.

Described are inerting systems that may be used on board an aircraft or other passenger transportation vehicle to reduce a risk of fire due to electronic components or to other elements in a compartment and to assist in preventing or extinguishing any fire or hazardous condition that may occur. The systems include a source of inert gas such as oxygen depleted air generated from a fuel cell on board the aircraft. The oxygen depleted air or other inert gas is conveyed through ducts to compartments that house the electronics, thus changing the conditions in the compartment to be less conducive to fire.