Chattaway
Adam Chattaway, Windsor GB
Patent application number | Description | Published |
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20100236796 | FIRE SUPPRESSION SYSTEM AND METHOD - A fire suppression system includes a high pressure inert gas source that is configured to provide a first inert gas output and a low pressure inert gas source that is configured to provide a second inert gas output. A distribution network is connected with the high and low pressure inert gas sources to distribute the first and second inert gas outputs. A controller is operatively connected with at least the distribution network to control how the respective first and second inert gas outputs are distributed. | 09-23-2010 |
20110308823 | PROGRAMMABLE CONTROLLER FOR A FIRE PREVENTION SYSTEM - A programmable controller for a fire suppression system includes a rewritable memory module and a processor module as well as multiple sensor inputs and control signal outputs. | 12-22-2011 |
20120217027 | EXTENDED DISCHARGE OF ODORANT - A method for fire suppression includes flowing a first inert gas output into an enclosed space at a high rate of discharge and flowing a second inert gas output into the enclosed space at a low rate of discharge. The method further includes metering an odorant into the second inert gas to provide an extended warning that inert gas is present in the enclosed space. | 08-30-2012 |
20120217028 | ACTIVE ODORANT WARNING - A fire suppression and warning system for an aircraft includes an inert gas delivery system, an inert gas indicator, an on-ground indicator, and a warning device. The inert gas delivery system delivers an inert gas output to an enclosed space on the aircraft. The inert gas indicator signals that the inert gas delivery system has delivered the inert gas output to the enclosed space. The on-ground indicator signals that the aircraft is located on the ground. The warning device actively warns that the inert gas output is present in the enclosed space in response to a signal from the inert gas indicator and a signal from the on-ground indicator. | 08-30-2012 |
20150034342 | FREIGHTER CARGO FIRE PROTECTION - An automated fire protection system for a freighter such as an aircraft may include a single fire retardant source for a first deck and a second deck. The system may further include a plurality of sensors for detecting fire and a plurality of nozzles for dispersing the retardant, wherein each nozzle is paired with one of the plurality of sensors. Once a fire is detected by one of the sensors, the fire protection system may eject fire retardant through only one or more nozzles paired with the sensor that detected the fire. Because retardant may be accurately dispersed close to the detected fire location through less than the plurality of nozzles, an amount of on-board retardant may be decreased, thereby decreasing weight of the fire suppression system. In an embodiment, the fire retardant may only be discharged during the descent, further decreasing the weight of the fire system. | 02-05-2015 |
Adam Chattaway, Berkshire GB
Patent application number | Description | Published |
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20120012346 | ODORANT FOR FIRE SUPPRESSION SYSTEM - A method for protecting a user in an enclosed environment includes providing an enclosed environment that holds cargo that has first odor; flowing a gas to the enclosed environment; and adding an odorant having a second odor to the gas, the first odor being distinctive from the second odor such that a presence of the second odorant provides a warning that the gas is present. | 01-19-2012 |
20140110137 | THERMODYNAMICALLY-OPTIMIZED ADVANCED FIRE SUPPRESSION SYSTEM - A fire suppression system for an aircraft includes an air separation module configured to receive exhaust air and ram air, conditioned compressor bleed air, and any combination thereof. The air separation module is also configured to provide nitrogen-enriched air and inert gas. The nitrogen-enriched air flows into a nitrogen-enriched air distribution network for fuel tank inerting. The inert gas flows into an inert gas distribution network for fire suppression in areas of the aircraft other than fuel tanks. | 04-24-2014 |
20150107685 | POPPET VALVE WITH A FRANGIBLE SEALING DISC FOR A PRESSURE VESSEL - A valve assembly for a pressure vessel is disclosed that includes a valve housing operatively associated with an outlet of the pressure vessel, a frangible hermetic disc sealing the outlet of the pressure vessel, and a poppet valve mounted for movement within the valve housing between a first position supporting the frangible hermetic disc within the outlet of the pressure vessel and a second position spaced apart from the frangible hermetic disc to permit the frangible disc to burst under pressure and permit the egress of pressurized material from the pressure vessel through the outlet. | 04-23-2015 |
Adam Chattaway US
Patent application number | Description | Published |
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20120145416 | COMBINED FIRE EXTINGUISHING SYSTEM - A fire suppression system includes a divert valve downstream of a fire suppressant source. The divert valve is selectively movable between an initial first position which communicates extinguishing agent into a first distribution network and a second position which communicates extinguishing agent into a second distribution network. | 06-14-2012 |
Adam Chattaway, Moormede GB
Patent application number | Description | Published |
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20120186831 | DISCHARGE OF FIRE EXTINGUISHING AGENT - Apparatus for rapid discharge of one or more fire extinguishing agent(s). The apparatus includes a sealed container forming an interior volume in communication with a rapidly opening valve assembly. The interior volume contains fire extinguishing agent(s), super-pressurised by a gas such as nitrogen. A portion of the nitrogen is dissolved into the fire extinguishing agent(s). When an incident is detected which requires the discharge of the fire extinguishing agent(s) the valve is opened. Opening the valve causes rapid dissolution of the nitrogen from the fire extinguishing agent(s), forming a two-phase mixture (like a foam or mousse) which substantially fills the volume and causing the discharge of fire extinguishing agent(s) from the valve assembly. | 07-26-2012 |
Adam Chattaway, Cambridge GB
Patent application number | Description | Published |
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20150306436 | FIRE SUPPRESSION SYSTEM ACTUATION APPARATUS AND SYSTEM - 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). | 10-29-2015 |