Kidde Technologies Incorporated

Kidde Graviner Limited

Hamilton Sundstrand Corporation

Adam Chattaway

Terry Simpson

Harlan Hagge

Mark P Fazzio

Eli Baldwin

Qing Edda Liu

Paul Papas

Marios C Soteriou

Dharmendr Len Seebaluck

Tadd F Herron

David William Frasure

Robert G Dunster

Richard Andrew Himmelmann

Lubomir A Ribarov

Josephine Gatsonides

Kevin P Aceves

Robert Glaser

John W Porterfield

Jeffrey Angle

Michael C Miller

Josephine Gabrielle Gatsonides

Robert E Glaser

Qing Liu

Harlan B Hagge

A fire suppressant blend comprises CF3I; at least one hydrofluoro-olefin (HFO) or hydrochlorofluoro-olefin (HCFO), or both; and carbon dioxide.

Fire suppression blends of CF3I, HCFOs and CO2

An adjustable flow splitter for a distribution system, the adjustable flow splitter comprises an inlet channel for receiving fluid at a first end, the inlet channel configured to allow flow from the first end to a second end. The adjustable flow splitter also comprises a first sub-channel and a second sub-channel located at the second end, and a diverter configured to deflect the flow of the fluid from the inlet channel to at least one of the first sub-channel and/or the second sub-channel, wherein the diverter is adjustable. The adjustable flow splitter also comprises means for maintaining the position of the diverter.

Adjustable flow splitter for distribution systems

A fire suppression blends of CF3I and 2-BTP with mol ratios from 1:5 and 5:1 are capable of passing peak inerting and sub-inerting tests. The CF3I:2-BTP fire suppression blends can also include carbon dioxide of up to 80% of the fire suppression blend to provide additional cooling.

Fire suppression blends of CF31 and 2-BTP

A fire suppression composition comprises CFI and CO, wherein said CFI is present in an amount of from 23 mol. % to 39 mol. %, based on the total moles of CFI and COpresent in the fire suppression composition. Alternatively, the fire suppression composition comprises CFI and CO, wherein said CFI is present in an amount of from 53 mol. % to 85 mol. %, based on the total moles of CFI and COpresent in the fire suppression composition.

Fire suppression compositions

A fire suppression system in an aircraft includes a first nozzle within a region to perform discharge of a fire suppression agent in a first direction within a region. The systems also includes a second nozzle within the region to perform discharge of the fire suppression agent in a second direction within the region. The discharge in the first direction by the first nozzle and the discharge in the second direction by the second nozzle generate and maintain a vortex of the fire suppression agent that occupies the region with rotational flow.

Nozzle configurations to create a vortex of fire suppression agent

A fire suppression system includes at least one high pressure gas source containing an inert gas, at least one low pressure gas source containing an organic halide gas, a distribution network connected with the high pressure gas source and the low pressure gas source to distribute the inert gas and the organic halide gas, and a controller in communication with the distribution network. The distribution network includes flow control devices configured to control flow of the inert gas and the organic halide gas. The controller is configured to initially release the inert gas in response to a fire threat to reduce an oxygen concentration at the fire threat below a preset oxygen concentration threshold, and release the organic halide gas to increase an organic halide gas concentration at the fire threat above a preset organic halide gas concentration threshold while the oxygen concentration is below the preset oxygen concentration threshold.

Fire suppression system and method

A system includes a turbo pump to convert compressed gas into power, a storage tank to store the compressed gas, and a fire suppression control valve having a closed position in which the compressed gas is prevented from flowing to the cargo compartment and an open position in which the compressed gas is ported to the cargo compartment to suppress a fire. The system also includes a pump control valve having a closed position in which the compressed gas is prevented from flowing to the turbo pump and an open position in which the compressed gas is ported to the turbo pump to cause the turbo pump to convert the compressed gas into the power. The system also includes an OBIGGS to convert bleed air from a gas turbine engine into an inert gas to provide low rate discharge (LRD) fire suppression to the cargo compartment.

Systems and methods for providing power and fire suppression using a turbo pump, compressed gas, and an OBIGGS

Disclosed herein is a system and method for monitoring a gaseous fire suppression blend. The system includes a sensor array having a plurality of sensors disposed in a protected space, wherein the sensor array can detect and quantify more than one component of the gaseous fire suppression blend.

System and method for monitoring a fire suppression blend

Disclosed is a fire suppression agent composition including CFI and an additional fire suppression agent selected from the group consisting of HFC-23, HFC-125, HFC-227ea, dodecafluoro-2-methylpentan-3-one (Novec 1230), and HCFO-1233zd(E), wherein the fire suppression agent composition passes the FAA aerosol can test.

Fire suppression agent composition

A fire extinguishing agent concentration measuring system including a first window, a second window positioned relative to the first window thereby defining a sensing volume between the first window and the second window, a tube configured to port a flow including the agent from an environment through the sensing volume, and a fluid motion mechanism in operable communication with the tube configured to cause the flow through the tube and through the sensing volume.

Fire extinguishing agent concentration measuring system and method

A fire suppression system for an aircraft cargo compartment comprises a source of fire suppression agent, a supply line for conducting the fire suppression agent to the compartment, at least one first pressure sensor for sensing the pressure within the cargo compartment and at least one second pressure sensor for sensing the pressure in an area within the aircraft but external to the cargo compartment. The system further comprises a first, inlet valve permitting fluid communication between the area external to the cargo compartment and the cargo compartment, a second, outlet valve permitting fluid communication between the cargo compartment and an or the area external to the cargo compartment and a fan for extracting fluid from the cargo compartment through the outlet valve.

Fire suppression systems

A fire suppression system for an aircraft cargo compartment comprises a source of fire suppression agent and a supply line for conducting the fire suppression agent to the compartment. The supply line has one or more flow control valves arranged between the source and the cargo compartment. A controller controls the flow control valve to control the supply of fire suppression agent to the cargo compartment from the source.

A fire suppression agent includes a fluid medium, vermiculite particles suspended in the fluid medium, and a colorant additive proximate at least a subset of the vermiculite particles. The fire suppression agent is capable of suppressing a fire comprising a combustible metal material.

Colorant for solid fire suppression agent

A fire suppression system may comprise a shape memory actuation system. The shape memory actuation system may be configured as a retainer that retains a plug and/or a disk. The shape memory actuation system may be a shape memory plug that is configured to discharge from a vessel exhaust port. The shape memory actuation system may be deployable in response to an electrical stimulus (e.g., resistive heating causing the shape memory alloy to have a temperature exceeding a transition temperature).

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Old Windsor, United Kingdom

Adam Chattaway