A fire suppressant for cooling a battery pack includes a pressurized mixture of a dry chemical and carbon dioxide. The dry chemical is an inorganic particulate chemical. The dry chemical particles are small enough to be carried by a flow of depressurizing carbon dioxide. A mass of the dry chemical is between 5% and 50% of a mass of the carbon dioxide. The carbon dioxide, when depressurized, vaporizes and cools the dry chemical and the battery pack. The dry chemical can adhere to the battery pack when the mixture is depressurized. An amount of the fire suppressant used to cool the battery pack is equal to or greater than an inerting volume of fire suppressant for the battery pack.

A fire suppressant for cooling a battery cell in a battery pack includes a pressurized mixture of an organic compound and carbon dioxide. The organic compound is 1,1,1,2,2,4,4,5,5,5-nonafluoro-4-(trifluoromethyl)-3-pentanone. A ratio of a mass of the organic compound to a mass of the carbon dioxide is between 1:4 and 4:1. The mixture is pressurized above a vapor pressure of the carbon dioxide. The carbon dioxide, when depressurized, evaporates and cools the organic compound and the battery cell. The mixture, when depressurized, flows through the battery cell. An amount of the fire suppressant flowed through the battery pack is equal to or greater than an inerting volume of fire suppressant for the battery pack.

A battery pack includes a pack case including a base plate including a plurality of module regions each having the battery module located therein, a side wall extending along an edge of the base plate and vertically coupled to the base plate to surround the module regions, and a partition wall coupled to the side wall and configured to partition the base plate to form the plurality of module regions, wherein the side wall includes a gas-filled part that is filled with a high-pressure extinguishing gas therein and corresponds to the module region, a discharge port that is open to allow the gas-filled part to communicate with the module region, and a sealing plate coupled to the discharge port to seal the extinguishing gas, wherein the sealing plate is coupled to the discharge port so as to be separable in response to a temperature change in the module region.

When it comes to extinguishing destructive fires, one of the greatest tragedies of property loss in fires is the damage done by the water during the extinguishing process. It can be extreme. This invention eliminates the water and the resulting damage and greatly reduces the cost of cleanup and repair after the fire is extinguished.

Furthermore, the greatest threat to fire emergency personnel is close proximity to the fire. Often times, in order to put out a fire, such as in a building, a firefighter must enter the building to get access to the fire. This entails great danger and sometimes death or injury. This invention makes it easier and faster for firefighters to apply fire-extinguishing agents to the fire without entering the building.

Current technology does not offer these benefits.

An aircraft including a fuselage defining a cabin and baggage bay, engine compartments for receiving engines, an auxiliary power unit compartment for receiving an auxiliary power unit, and a fire suppression system including first and second reservoirs containing a fire suppressant. The reservoirs are each connected to all of the engine compartments for distribution of the fire suppressant thereto. The first reservoir is connected to only one of the auxiliary power unit compartment and baggage bay, and the second reservoir is connected to only the other of the auxiliary power unit compartment and baggage bay. A fire suppression system for an aircraft and a method of connecting a fire suppression system of an aircraft are also discussed.

A system includes a pressure vessel defining an interior space with a discharge outlet. A valve or burst disc is connected in fluid communication with the discharge outlet. Discharge piping is included in fluid communication with the valve or burst disc to receive discharge from the interior space. One or more discharge nozzles are in fluid commination with discharge piping for issuing a spray from the discharge piping into the environment external of the pressure vessel. A mixture of liquid Carbon Dioxide (CO.sub.2) and a dry chemical fire extinguishing agent is housed under pressure within the interior space.

The present invention relates to a perforator for breaking a closing member at a gas outlet of a gas bottle to allow a gas to flow out. The perforator includes a cylindrical housing having three openings, namely, a first opening at a first end portion, a second opening at a second end portion which is opposite to the first end portion, and a third opening formed in a circumferential wall portion, an ignition device being fixed at the first opening, the second opening to be connected to the gas bottle and the third opening serving as a gas discharge portion, and when a pressure created by actuation of the ignition device is received, the first piston moving in an axial direction, and the second piston moving towards the second opening by receiving the movement of the first piston.

Fuel tank inerting and fire suppression systems and methods for an aircraft are provided. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank, the first source arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first reactant from the first source and a second reactant from the second source to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, and a fire suppression inert gas supply system arranged to direct the inert gas to a fire suppression system, wherein the fire suppression inert gas supply system includes a fire suppression inert gas supply controller to control a flow of inert gas to the fuel tank and the fire suppression system.

Noise and room air overpressure on discharge of a gas extinguisher system is reduced. During the discharge, an extinguishing fluid is conveyed from a pressurized container via a container valve and line system to an extinguishing nozzle. At the beginning of the discharge the extinguishing fluid is predominantly present in the line system in liquid phase and after discharge it assumes a predominantly gaseous phase. In a phase transition period, which is accompanied by a significant reduction in the extinguishing fluid mass flow and a significant increase in the noise and the room air pressure, the mass flow is then reduced or stopped. Due to the reduction of the mass flow, the sound level of the noise arising is advantageously reduced to a value of a maximum of 100 dB and the room air pressure to an overpressure value ranging from 200 to 1000 Pa.

Noise and room air overpressure on discharge of a gas extinguisher system is reduced. During the discharge, an extinguishing fluid is conveyed from a pressurized container via a container valve and line system to an extinguishing nozzle. At the beginning of the discharge the extinguishing fluid is predominantly present in the line system in liquid phase and after discharge it assumes a predominantly gaseous phase. In a phase transition period, which is accompanied by a significant reduction in the extinguishing fluid mass flow and a significant increase in the noise and the room air pressure, the mass flow is then reduced or stopped. Due to the reduction of the mass flow, the sound level of the noise arising is advantageously reduced to a value of a maximum of 100 dB and the room air pressure to an overpressure value ranging from 200 to 1000 Pa.