AU2012201214A1 - System and apparatus for suppression of fires - Google Patents

Abstract

An apparatus and system for suppression of fires are provided. In accordance with one embodiment of the invention, a housing is provided with a first opening (or set of openings), a second opening (or set of openings) and a flow path defined between the first and second openings. A fire-suppressing gas is produced, such as from a solid propellant composition, and is introduced into the flow path in such a way that a volume of ambient air is drawn from a location external to the housing, through the first opening and into the flow path. The volume of ambient air may be subjected to an oxygen-reducing process and mixed with the fire-suppressing gas to form a gas mixture. The gas mixture is discharged from the flow path through the second opening and into an associated environment for suppression of a fire located therein.

Description

AUSTRALIA Patents Act COMPLETE SPECIFICATION (ORIGINAL) Class Int. Class Application Number: Lodged: Complete Specification Lodged: Accepted: Published: Priority Related Art: Name of Applicant: Alliant Techsystems Inc. Actual Inventor(s): Gary K. Lund, James D. Rozanski Address for Service and Correspondence: PHILLIPS ORMONDE FITZPATRICK Patent and Trade Mark Attorneys 367 Collins Street Melbourne 3000 AUSTRALIA Invention Title: SYSTEM AND APPARATUS FOR SUPPRESSION OF FIRES Our Ref: 936255 POF Code: 43783/132180 The following statement is a full description of this invention, including the best method of performing it known to applicant(s): -1- 2 SYSTEM AND APPARATUS FOR SUPPRESSION OF FIRES RELATED APPLICATION The present application is a divisional application from Australian Patent 5 Application No.2010202682, the entire disclosure of which is incorporated herein by reference. TECHNICAL FIELD The present invention relates generally to the suppression of fires and, more particularly, to systems and apparatus for suppressing fires including the suppression 10 of fires within human-occupied spaces and clean room-type environments. BACKGROUND State of the Art: Fire suppression systems may be employed in various situations and locations in an effort to quickly extinguish the undesirable outbreak of a 15 fire and thereby prevent, or at least minimize, the damage caused by such a fire including damage to a building, various types of equipment, as well as injury or loss of human life. A conventional fire suppression system or apparatus may conventionally include a distribution apparatus, such as one or more nozzles, which deploy a fire suppressing substance upon actuation of the system. Actuation of the system may be 20 accomplished through means of a fire or smoke detection apparatus which is operatively coupled to the suppression system, through the triggering of a fire alarm, or through manual deployment. Various types of fire-suppressing substances or compositions may be utilized depending, for example, on where the fire suppression system or apparatus is being employed, how large of an area is to be serviced by the 25 fire suppression system, and what type of fire is expected to be encountered and suppressed by the system. For example, in some commercial and even residential fire suppression systems, a network of sprinklers is employed throughout the associated building and configured to distribute water or some other fire-suppressing liquid to specified 30 locations within the building upon activation of the system. However, a system providing a liquid fire suppressant is not suited for all situations. For example, it would not be generally desirable to employ a fire suppression system utilizing water as the suppressant in a location where grease would likely serve as fuel for an ignited fire at the given location. Similarly, it would not 3 be generally desirable to utilize a liquid suppressant in a location which contained electrical equipment including, for example, costly and sensitive electronic or computer equipment. While a liquid suppressant might adequately suppress a fire in such a location, the suppressant would likely impose substantial damage to the 5 equipment housed therein. Further, a liquid suppressant is not ideally suited for use in a clean room environment where the introduction of a liquid material to the clean room would result in contamination of some article of manufacture (e. g., an integrated circuit device). Other available suppressants include dry chemical suppressants such as, for 10 example, sodium bicarbonate, potassium bicarbonate, ammonium phosphate, and potassium chloride. While such suppressants can be effective in specific implementations, it is often difficult to implement systems which effectively utilize dry chemicals in large areas. Furthermore, use of dry chemicals can pose a health hazard to individuals in the vicinity of their deployment, as well as act as a source of 15 contamination of electronic and computer equipment or even goods being manufactured, for example, in a clean room. Thus, such suppression systems are not conventionally utilized in locations such as clean rooms, computer rooms or spaces designed for human occupation. Another type of suppressant which has been used includes gas suppressants. 20 For example, gases designated generally as Halons have been effectively used as fire suppressants in the past. Halons include a class of brominated fluorocarbons derived from saturated hydrocarbons wherein the hydrogen atoms are essentially replaced with atoms of the halogen elements bromine, chlorine and/or fluorine. Halons, including the widely used varieties designated as Halon 1211, 1301 and 25 2402, have been used for the effective suppression of fires in various environments and situations including human-occupied and clean room-type environments. However, in recent years, an effort to phase out Halons has been undertaken due to their ozone depletion characteristics. Indeed, in the year 1994, production ceased of certain Halons, while others are scheduled to be phased out by the year 2010. 30 Some of the gases which have been used in an attempt to replace the effective Halon gases include, for example, nitrogen and carbon dioxide. Such gases essentially displace the oxygen contained within the air at the location of the fire such that an insufficient amount of oxygen is available for further combustion. However, such gases generally require the distribution of relatively large volumes of the 4 selected gas in order to be effective as a fire suppressant. In order to accommodate such large volumes of gas, expensive and bulky pressure vessels are conventionally required to store the gas in a compressed state in anticipation of its use. Furthermore, such gases sometimes include or produce byproducts which may be harmful to any 5 equipment or individuals located in the area into which the gas suppressant is distributed. Additionally, as noted above, the requirements of storing gas, conventionally at high pressures and in large volumes, often make such systems expensive and cumbersome in size in that the systems require a significant amount of space 10 available for installation and operation. In order to address some of the concerns listed above, including the ability to provide adequate volumes of suppressant while requiring relatively small storage facilities, various attempts have been made to develop alternative fire suppression systems. Some of the approaches to provide alternative fire suppression systems 15 include those disclosed by U. S. Patent No. 6,257, 341 to Bennett, U. S. Patent No. 5,609, 210 to Galbraith et. al., and U. S. Patent No. 6,401, 487 to Kotliar. The Bennett Patent generally discloses a system which utilizes a combination of compressed inert gas and a solid propellant gas generator. Upon ignition, the solid propellant gas generator generates nitrogen, carbon dioxide, or a mixture thereof. The gas ?0 generated from the solid propellant is then mixed and blended with the stored compressed inert gas, which may include argon, carbon dioxide or a mixture thereof, to provide a resulting blended gas mixture for use as a suppressant. The Bennett system claims to provide a system which is smaller in size than prior art systems and, therefore, is more flexible in its installation in various environments. However, due to 25 the fact that the Bennett system utilizes compressed inert gas, appropriate pressure vessels are required which, as discussed above, are conventionally expensive and require a substantial amount of space for their installation, particularly if a large room or area is being serviced by the described system, therefore requiring a large volume of suppressant. 30 The above-referenced Galbraith patent generally discloses, in one embodiment, a system which includes a gas generator charged with a combustive propellant wherein the propellant, upon ignition, generates a volume of gas. The generated gas is directed to a chamber containing a volume of packed powder such as magnesium carbonate. The gas drives the powder from the chamber for 5 distribution of the powder onto a fire. In another embodiment, Galbraith discloses a system wherein the generated gas is used to vaporize a liquid, thereby generating a second gas, wherein the second gas is used as the fire suppressant. However, the use of powders, as noted above, is not desirable in, for example, areas which are 5 intended for regular human occupancy, areas intended to house sensitive electronic equipment, or other clean room-type environments. The use of vaporizable liquids may introduce additional issues regarding long-term storage of the liquid including the prevention of possible corrosion of the associated storage container. The above-referenced Kotliar patent generally discloses a system which 10 includes a hypoxic generator configured to lower the oxygen content of the air contained within a room or other generally enclosed space to a level of approximately 12% to 17% oxygen. One of the embodiments disclosed by Kotliar includes a compressor having an inlet configured to receive a volume of ambient air from the room or enclosure. The compressed air is passed through a chiller or cooler and then 15 through one or more molecular sieve beds. The molecular sieve bed may include a material containing zeolites which allow oxygen to pass through while adsorbing other gases. The oxygen which passes through the molecular sieve bed is discharged to a location external from the room or enclosure being protected. The molecular sieve bed is then depressurized such that the gases captured thereby are released back 20 into the room as an oxygen-depleted gas. While Kotliar discloses that the system may be used as a fire suppressant system, it is not apparent how efficient the system is in rapidly reducing the oxygen level for a given room so as to suppress any fire therein. Moreover, it appears that the Kotliar system is contemplated as being more effective as a fire prevention system 25 wherein the hypoxic generator is continuously running such that the air within a room or other enclosure is continuously maintained at an oxygen-depleted level in order to prevent ignition and combustion of a fuel source in the first place. However, such an operation obviously requires the constant operation of a hypoxic generator and, thus, likely requires additional upkeep and maintenance of the system. Furthermore, while 30 Kotliar asserts that there are no associated health risks to those who spend an extended amount of time in a hypoxic environment (i. e., an oxygen reduced or depleted environment), such a system may not be ideal for those with existing health conditions, including, for example, respiratory ailments such as asthma or bronchitis 6 or cardiovascular conditions, or for individuals who are elderly or who generally lead an inactive lifestyle. The discussion of documents, acts, materials, devices, articles and the like is included in this specification solely for the purpose of providing a context for the 5 present invention. It is not suggested or represented that any or all of these matters formed part of the prior art base or were common general knowledge in the field relevant to the present invention as it existed before the priority date of each claim of this application. Throughout the description and claims of this specification, the word 10 "comprise" and variations of the word, such as "comprising" and "comprises", is not intended to exclude other additives, components, integers or steps. DISCLOSURE OF INVENTION In accordance with one aspect of the invention, a fire suppression apparatus is 15 provided. The apparatus comprising a structure having a first inlet opening therein, a second outlet opening therein and a flow path providing fluid communication between the first inlet opening and the second outlet opening; a gas-generating device located and configured to provide a flow of a first gas through a nozzle of the gas-generating device, the nozzle extending into and at least partially surrounded by a portion of the 20 flow path, and to direct the flow of the first gas out of the nozzle into the flow path downstream from the nozzle such that the flow of the first gas draws a volume of a second gas through the first inlet opening and into the flow path upstream from the nozzle; a diffuser in the flow path downstream of the nozzle, the diffuser located and configured to effect mixing of the first gas with the volume of the second gas drawn 25 into the flow path to form a gas mixture and to expand the gas mixture to reduce the velocity and the temperature of the gas mixture; and a heat transfer device disposed in the flow path between the diffuser and the first inlet opening and configured to allow at least the second gas therepast. In accordance with another aspect of the present invention, a fire suppression 30 system is provided. The fire suppression system comprising at least one fire suppression apparatus comprising: a structure having a first inlet opening therein, a second outlet opening therein and a flow path providing fluid communication between the first inlet opening and the second outlet opening; a gas-generating device located and configured to provide a flow of a first gas through a nozzle of the gas-generating 7 device, the nozzle extending into and at least partially surrounded by a portion of the flow path, and to direct the flow of the first gas out of the nozzle into the flow path downstream from the nozzle such that the flow of the first gas draws a volume of a second gas through the first inlet opening and into the flow path upstream from the 5 nozzle; a diffuser in the flow path downstream from the nozzle, the diffuser located and configured to effect mixing of the first gas with the volume of the second gas drawn into the flow path to form a gas mixture and to expand the gas mixture to reduce the velocity and the temperature of the gas mixture; a heat transfer device disposed in the flow path between the diffuser and the first inlet opening and 10 configured to allow at least the second gas therepast; and a controller configured to generate a signal and transmit the signal to the at least one fire suppression apparatus upon occurrence of a specified event, wherein the gas-generating device is configured to provide a flow of the first gas upon receipt of the signal from the controller. 15 BRIEF DESCRIPTION OF DRAWINGS The foregoing and other advantages of embodiments of the invention will become apparent upon reading the following detailed description and upon reference to the drawings in which: 20 FIG. 1 is a partial cross-sectional view of a fire suppression apparatus in accordance with an embodiment of the present invention; FIG. 2 is a partial cross-sectional view of a gas-generating device utilized in a fire suppression system in accordance with an embodiment of the present invention; FIGS. 3A and 3B are plots of multiple variables associated with an oxygen 25 getting device in accordance with exemplary embodiments of the present invention; FIG. 4 is a plot of temperature vs. percent of oxygen removed for specified exemplary embodiments of an oxygen-getting device; FIG. 5 is a perspective view of a fire suppression system installed in an environment for the protection thereof; 30 FIG. 6 is a schematic view of a fire suppression system in accordance with an embodiment of the present invention; FIGS. 7A and 7B show schematic and partial cross-sectional views, respectively, of a fire suppression apparatus in accordance with an embodiment of the present invention; and 8 FIG. 8 is a partial cross-sectional view of a fire suppression apparatus in accordance with yet another embodiment of the present invention. BEST MODES FOR CARRYING OUT THE INVENTION 5 Referring to FIG. 1, a fire suppression apparatus 100 may include a housing 102 formed of a high-temperature-resistant material such as, for example, steel. A first set of openings 104 and a second set of openings 106 are formed within the housing 102. A flow path 108 is defined between the first and second sets of openings 104 and 106, providing substantial fluid communication therebetween. A 10 mounting structure 109, such as, for example, a flange, may be coupled to or formed with the housing 102 such that the fire suppression apparatus 100 may be fixedly mounted to a structure within a selected environment. A gas-generating device 110 may be disposed at one end of the housing 102 and may contain a propellant 114, such as a solid propellant which is configured to 15 generate a desired gas upon ignition and combustion thereof as described in further detail below. The gas-generating device 110 may be coupled to a nozzle 116 for dispersion of any gas flowing out of the gas-generating device 110. As will be appreciated by those of ordinary skill in the art, through proper configuration of the nozzle 116, the 20 pressure and/or velocity of the gas exiting the gas-generating device 110 via the nozzle 116 may be controlled with considerable accuracy. The nozzle 116 may be configured to discharge any generated gas into a diffuser 118 or other flow control device positioned within the flow path 108 and to promote an expansion of the discharged gas, thereby reducing the velocity and 25 temperature of the gas. Furthermore, as will be further discussed below, the diffuser 118 may be configured to promote the mixing of gas discharged from the nozzle 116 with a volume of ambient air flowing through the first set of openings 104 into the flow path 108. Downstream from the first set of openings 104 within the flow path 108 is an 30 oxygen-getting device 120 configured to remove oxygen from any air flowing through the first set of openings 104 and through the associated flow path 108. The oxygen getting device 120 may be formed of an oxygen reactive material such as, for example, steel, copper, zirconium, iron, nickel or titanium. The material may be configured as, for example, wool, cloth, mesh or shot so that the material may be 9 packed or otherwise distributed within the flow path 108 while also enabling gas to travel therethrough. As shown in FIG. 1, it may be desirable for the oxygen-getting device 120 to be disposed adjacent the nozzle 116 and thermally coupled therewith. For example, a plurality of thermally conductive fins 122 or other heat transfer 5 features may be used to transfer heat produced from the gas-generating device 110 to the oxygen-getting device 120. Other processing or conditioning devices may be placed in the flow path 108 and located downstream of the first oxygen-getting device 120. For example, a second oxygen-getting device 123 may be used to further reduce the level of oxygen 10 from any air flowing through the flow path 108 depending on, for example, the efficiency of the first oxygen-getting device 120 and the desired oxygen content of any gas leaving the flow path 108 through the second set of openings 106. Additionally, an NOx scavenging device 124 may be utilized to remove nitric oxide from gases flowing through the flow path 108 which may be present, for example, depending on 15 the composition of the solid propellant 114 and the gas produced thereby. Alternatively, or additionally, a NH 3 scavenging device may be used to remove ammonia from gases flowing through the flow path 108. A heat transfer device 126 may also be located within the flow path 108 and configured to lower the temperature of any gas flowing therethrough prior to the gas 20 exiting the second set of openings 106. The heat transfer device 126 may exhibit a relatively simple configuration including, for example, thermally conductive fins, tubes or shot, configured to allow gas to flow therethrough (or thereover) and transfer heat away from the gas. In another embodiment, the heat transfer device 126 may exhibit a more complex configuration including, for example, a phase change material or a 25 mechanical heat exchanger employing a circulating fluid medium to transfer heat away from any gas flowing through the flow path 108. Referring now briefly to FIG. 2, a cross-sectional view of the gas-generating device 110 is shown in accordance with an embodiment of the present invention. The gas-generating device 110 includes a housing structure 130 containing a volume of 30 propellant 114 therein. An ignition device 132 is located and configured to ignite the propellant 114 upon the occurrence of a particular event. The ignition device 132 may include, for example, a squib, a semiconductor bridge (SCB), or a wire configured to be heated to incandescence. In one embodiment, the ignition device 132 may be configured to directly ignite the propellant 114 without the aid of an igniting 10 composition. In another embodiment, the ignition device 132 may be in contact with an igniting composition 134 which provides sufficient heat for the ignition of the propellant. Depending on the specific composition being utilized, the igniting composition 5 134 may be configured to produce a hot gas upon ignition thereof wherein the hot gas provides sufficient heat for the subsequent ignition and combustion of the propellant 114. In another embodiment, the igniting composition 134 may be configured to produce a molten material, such as a metal slag, which is sufficiently hot to ignite and initiate combustion of the propellant 114. 10 Exemplary igniting compositions 134 may include those disclosed in United States Patent No. 6,086, 693, which discloses a composition generally comprising about 50 to 75 weight percent composition of an oxidizer suh as strontium nitrate, up to 35 weight percent composition of an aluminum magnesium allow, and up to 20 weight percent of a gas-producing fuel component. It is noted, however, that various 15 igniting compositions may be utilized in the present invention depending, for example, on the composition of the propellant 114, the type of ignition device 132 being employed and the resulting gases that are desired to be produced (or eliminated) during operation of the gas-generating device 110. Upon ignition of the propellant 114, a gas is generated which, in one 20 embodiment, may include an inert gas suitable for introduction into a human-occupied space or for an environment which houses sensitive electronic equipment. For example, in one embodiment, the propellant 114 may include a composition which is configured to produce nitrogen gas, such as N 2 , upon combustion thereof. In another embodiment, the propellant 114 may include a composition which is configured to 25 produce H 2 0 (water vapor), C0 2 (carbon dioxide) gases or various mixtures of such exemplary gases upon the combustion thereof. Various propellant compositions are contemplated as being used with the present invention. However, depending on various factors such as the intended normal use of the environment being protected by the fire suppression apparatus 100, it may be desirable to utilize a composition 30 which produces a gas (or gas mixture) which is free of ozone-depleting gases (e.g., halogenated fluorocarbons) and/or global warming gases (e.g., carbon dioxide) while still being effective at lowering the oxygen content of air contained within a generally enclosed space.

11 In one embodiment, an exemplary propellant composition may include a HACN composition, such as disclosed in United States Patent Nos. 5,439, 537 and 6,039, 820, both to Hinshaw et a/. Of course other compositions may be utilized. In one embodiment, a propellant composition may be configured to produce an inert gas 5 including nitrogen and water vapor. In one example, it may be desirable to produce approximately 1.5 kilograms (kg) to approximately 300 kg of nitrogen gas from the propellant 114 contained within the gas-generating device 110. In producing such a mass of nitrogen, it may be desirable to produce less than 1 % of carbon dioxide by volume with negligible 10 amounts of carbon monoxide. Furthermore, it may be desirable to produce a gas which is substantially residue free so as to not leave a film or coating of residue on any equipment, furniture, etc., which may be located within the environment being protected by the apparatus. The gas-generating device 110 may further include a filter 136 such as, for 15 example, a screen mesh or an amount of steel shot disposed within the housing 130. The filter may be used to prevent slag or molten material produced during combustion of the propellant 114 from leaving the housing 130. The prevention of slag or other solids from leaving the gas-generating device 110 may be desirable to prevent the blocking or clogging of the nozzle 116, to prevent damage to other components 20 located within the flow path 108 (FIG. 1) and to simply prevent damage to equipment or injury to individuals which might otherwise result if such high-temperature materials were allowed to be discharged back into the environment being serviced by the fire suppression apparatus 100. Referring to both FIGS. 1 and 2, operation of the fire suppression apparatus 25 100 is now described. Upon detection of a fire, the ignition device 132 may be actuated such as by providing an electrical signal through one or more conductors 138. The signal may be provided automatically through detection of a fire by an appropriate sensor, or may be the result of the manual actuation of a switch or similar device. The ignition device 132 is configured to ignite the propellant 114 within the 30 gas-generating device 110, either directly or by way of an igniting composition 134 as set forth above. The ignition and subsequent combustion of the propellant 114 results in the generation of a gas which flows through the nozzle 116 of the gas-generating device 110 as indicated by directional arrow 140. The nozzle 116 is configured to 12 substantially control the flow of the generated gas including the velocity of the gas exiting the nozzle 116 as it enters into the flow path 108. In one embodiment, the nozzle 116 is configured such that gas exits the nozzle 116 at sonic or supersonic velocities. The high-velocity gas flow exiting the nozzle, combined with the geometric 5 area ratios and the location of the nozzle 116 within the flow path 108 relative to the first set of openings 104, causes ambient air (i.e., air external to the fire suppression apparatus 100) to be drawn in through the first set of openings 104. In other words, the high-velocity production of gas effects an aspiration or eduction of ambient air located outside the fire suppression apparatus 100 through the first set of openings 10 104 and into the flow path 108 as indicated at 108A. The ambient air drawn into the flow path 108 passes through the oxygen getting device 120 which, through a chemical reaction, reduces the level of oxygen within the ambient air flowing therethrough. For example, the oxygen-getting device 120 may be at least partially formed of a material comprising iron which may adsorb 15 approximately 0,1814 kilograms of oxygen per kilogram of material (kg oxygen/kg mat'l) (approximately 0.4 pounds of oxygen per pound of material (lbs. oxygen/lb. mat'l)). The iron material will react with the ambient air flowing through the oxygen getting device 120 to reduce the oxygen content thereof and produce Fe 3 0 4 within the oxygen-getting device 120. In another exemplary embodiment, the oxygen-getting 20 device 120 may be at least partially formed of a material comprising copper which may adsorb approximately 0.1134 kg oxygen/kg mat'l (approximately 0.25 lbs. oxygen/lb. mat'l). The reaction of the ambient air with the copper will result in the production of CuO within the oxygen-getting device 120. In a further exemplary embodiment, the oxygen-getting device 120 may be at 25 least partially formed of a material comprising nickel which may adsorb approximately 0.1225 kg oxygen/kg mat'l (approximately 0.27 lbs oxygen/lb mat'l). The reaction of the ambient air with the nickel will result in the production of NiO within the oxygen getting device 120. In yet another exemplary embodiment, the oxygen-getting device 120 may be at least partially formed of a material comprising titanium which may 30 adsorb approximately 0.3039 kg oxygen/kg mat'l (approximately 0.67 lbs. oxygen/lb. mat'l.) The reaction of the ambient air with the titanium will result in the production of TiO 2 within the oxygen-getting device 120. Another exemplary material which may be used in the oxygen-getting device includes zirconium which may adsorb approximately 0.0794 kg oxygen/kg mat'l (approximately 0.175 lbs. oxygen/lb. mat'l).

13 It is noted, however, that the above materials are exemplary and that other materials may be used as well as other means and methods of extracting oxygen as will be appreciated by those of ordinary skill in the art. As noted above, heat associated with the combustion of the propellant 114 5 may be transferred to the oxygen-getting device 120. For example, it is estimated that temperatures within the gas-generating device 110 may rise to between approximately 1371*C (approximately 2500 0 F) and approximately 19270C (approximately 3500 0 F) in some embodiments. The transfer of heat away from the gas-generating device 110 provides the benefit of reducing potentially dangerous 10 levels of heat and the dispersement of such heat over a larger area for effective cooling of the gas-generating device 110. Additionally, the transfer of heat to the oxygen-getting device 120 will also enhance the process of removing oxygen from any aspirated air passing therethrough by expediting the chemical reaction which takes place between the ambient air and the material disposed within the oxygen 15 getting device 120. Referring briefly to FIGS. 3A, 3B and 4 while still referring to FIGS. 1 and 2, it is shown how the operating temperature of the oxygen getting device 120 may influence the performance of the fire-suppression apparatus 100. FIG. 3A shows a first graph 200 depicting equilibrium reaction and aspirator relationships for an 20 exemplary embodiment of a fire-suppression apparatus 100 wherein iron (Fe) is used to react with air in an oxygen getting-device 120. More particularly, a first plotline 202 shows the relationship of temperature (left hand, vertical axis 204) with respect to the "air-to-getter ratio" (horizontal axis 206) which is defined as the kilogram (kg) ratio of aspirated air to the iron material present in the oxygen-getting device 120 in an 25 equilibrium reaction (i.e., assuming complete reaction of the air with the iron material). A second plotline 208 shows the relationship of the air-to-getter ratio to the cross sectional area of a given diffuser 118 (represented as a diffuser tube diameter in units of centimeters on the right hand, vertical axis 210). A third plotline 212 shows the relationship of the air-to-getter ratio with the mass flow ratio (also the right hand, 30 vertical axis 210), which is the mass ratio of aspirated air to combustion gas produced by the gas generating device 110. Referring briefly to FIG. 3B, a second graph 214 is shown for an exemplary embodiment wherein copper is used to react with air in an oxygen getting device 120.

14 Again, the first plotline 202' shows the relationship of temperature with the air-to getter ratio; the second plotline 208' shows the relationship of the diffuser tube diameter with the air-to-getter ratio; and the third plotline 212' shows the relationship of the mass flow ratio with the air-to-getter ratio. 5 Referring now briefly to FIG. 4, a graph 220 includes three plotlines 222, 224 and 226 based on kinetic calculations of the percent oxygen removed from the aspirated air (left hand, vertical axis 228) for a stated temperature of the material present in the oxygen getting device 120 (horizontal axis 230). For example, the first plotline shows such a relationship for 4.54 kg (10 Ibm) of copper, the second plotline 10 224 shows a similar relationship for 6.80 kg (15 Ibm) of copper, and the third plotline shows a similar relationship for 9.07 kg (20 Ibm) of copper. Considering the graphs 200, 214 and 220 together as shown in FIGS. 3A, 3B and 4, it can be seen that such relationships may be used to assist in selecting an oxygen-getting material for use in an oxygen getting device 120. The graphs 200, 214 15 and 220 also show the importance of flow path geometry, such as the size of the diffuser 118, in regards to aspiration performance. For example, after a material has been selected for use in the oxygen getting device 120 based on information such as shown in FIG. 4, the further information provided in a corresponding graph (i.e., graph 214 in FIG. 3B) may be used to design 20 other aspects of the fire-suppression apparatus 100. Still using FIGS. 3B and 4 as an example, it is apparent that, when utilizing a copper material, the rate of oxygen removal from aspirated air increases as the temperature of the copper goes up. However, depending on the intended application and environment of the fire suppression apparatus 100, it may be desirable to keep the effluent gas mixture 25 below a specified temperature. The temperature of the effluent gas mixture may be controlled by keeping the temperature of the combustion gas at or below a specified level or, as previously discussed, by providing a heat transfer device 126 to reduce the temperature of the gas mixture prior to its exit from the fire-suppression apparatus 100. In either case, once the operating temperature of the oxygen getting device 120 30 is established, the air-to-getter ratio may be determined and, subsequently, the mass flow ratio and the diffuser tube diameter may similarly be determined utilizing the graph 214 shown in FIG. 3B. Referring more particularly to FIGS. 1 and 2 again, after the ambient air has passed through the oxygen-getting device 120, the now oxygen-depleted (or oxygen- 15 reduced) air is drawn further into the flow path 108 and is mixed and entrained with the gas exiting the nozzle 116 of the gas-generating device 110 as indicated at 108B. The gas mixture (i.e., the generated gas exiting the nozzle 116 combined with the oxygen-depleted air) flows through a diffuser 118 which is configured to reduce the 5 velocity of the gas mixture. The gas mixture flows through the diffuser 118 and through any subsequent processing apparatus placed in the flow path 108, as indicated at 108C, such as the second oxygen getting device 122, the NOx scavenging device 124, the heat transfer device 126, a filter or some other processing or conditioning device such as, for example, a NH 3 scavenger, as may be desired, to 10 further condition the gas mixture or alter the flow characteristics thereof. The gas mixture then exits the second set of openings 106, as indicated at 108D, at a reduced velocity. In some embodiments, it may be desirable to reduce the velocity of the gas mixture such that it exits the second set of openings 106 at a subsonic velocity. 15 Additional components may be utilized within the flow path to control the velocity of the gas mixture. For example, as shown in FIG. 1, the flow path 108 may include one or more bends or channels to redirect the flow of the gas mixture and reduce the velocity thereof. Additionally, baffles or other similar devices may be placed in the flow path 108 to control flow characteristics of the gas mixture. 20 Additional diffusers may also be utilized including, for example, at or adjacent the second set of openings 106 to further reduce the velocity of the gas mixture exiting the housing 102. As the gas mixture exits the second set of openings 106, the gas mixture contains a volume of inert gas, such as nitrogen, configured to displace the oxygen 25 contained with the air of a substantially enclosed environment. The gas mixture also includes an amount of oxygen-depleted air, which was initially drawn from the substantially enclosed environment, such that the overall level of oxygen available to support combustion is substantially reduced and, desirably, prevents further combustion of any fire which may be occurring within the environment serviced by the 30 fire suppression apparatus 100. Referring now to FIGS. 5 and 6, FIG. 5 shows a perspective of a defined environment 150 in which a fire suppression apparatus 100 of the present invention may be utilized, while FIG. 6 shows a schematic of a fire suppression system 152 16 which may incorporate one or more of the fire suppression apparatuses 100 and may be used to service the above-stated environment 150. One or more of the fire suppression apparatuses 100 may be strategically located within the environment 150 to draw in air from .the environment 150 and 5 distribute a gas mixture, such as described hereinabove, back to the environment 150. The number of the apparatuses 100 utilized and their specific location within the environment 150 may depend, for example, on the size of the environment 150 (e.g., the volume of air contained thereby), the intended use of the environment 150 (e.g., human-occupied, clean room, etc.), and/or the type of fire expected to be 10 encountered within the environment 150. The fire suppression system 152 may include one or more sensors 154 such as, for example, smoke sensors, heat sensors, or sensors which are configured to detect the presence of a particular type of gas. The system may also include one or more actuators 156 which may be manually triggered by an occupant of the 15 environment 150 upon the occurrence of a fire. The sensors 154 and actuators 156 may be operably coupled with a control unit 158, which may include, for example, a dedicated control unit or a computer programmed to receive input from or otherwise monitor the status of the sensors 154 and actuators 156 and, upon the occurrence of a predetermined event, actuate the gas-generating device 110 (FIGS. 1 and 2) and 20 initiate the operation of the fire suppression apparatuses 100. Thus, for example, upon the detection of smoke by a sensor 154, or upon the manual triggering of one of the actuators 156, an appropriate signal may be relayed to the control unit 158. The control unit 158 may then generate an appropriate signal which is relayed to the fire suppression apparatuses 100, thereby igniting the ignition 25 device 132 (FIG. 2). As set forth above, the igniting device causes the propellant 114 (FIG. 2) to ignite and combust, generating gas and, ultimately, resulting in a gas mixture being distributed within the environment 150. The fire suppression system 152 may be configured to relay such signals through an appropriate transmission path 160 which may include, for example, conductors configured for either analog or digital 30 transmission of such signals, or a wireless transmission path between the various devices. The fire suppression system 152 may further include an alarm 162 which may also be actuated by the control unit 158. Such an alarm 162 may include a device configured to provide a visual indicator, an auditory indicator, or both to any occupants of the environment 150.

17 Referring now to FIGS. 7A and 7B, another embodiment of a fire suppression apparatus 100' is shown. The fire suppression apparatus 100' is constructed similarly to that which is shown and described with respect to FIGS. 1 and 2, except that the apparatus is configured and located so as to be substantially integrated with a 5 structure 170 associated with the environment being serviced or protected thereby. Thus, the structure 170 may be integral with the housing 102' of the fire suppression apparatus 100' wherein a first opening 104' (or set of openings) is formed within a wall or panel 172 of the of the structure 170, a second opening 106' (or set of openings) is formed within the wall 172 of the structure 170, and a flow path 108' is defined 10 between the first and second openings 104' and 106'. Various processing devices may be placed in the flow path 108' including, for example, oxygen-getting devices, NOx scavengers, filters and/or heat transfer devices such as described above. Additionally, various flow control devices such as diffusers, baffles or redirected flow paths may be incorporated into the fire 15 suppression apparatus 100' to control the flow of the gas mixture which ultimately exits the second opening 106'. The structure 170 into which the fire suppression apparatus 100' is integrated may include a room of a building or the cabin of a land, sea or air vehicle such as, for example, an automobile, a train car, a plane or some other vehicle. For example, the 20 structure 170 may include an automobile and the wall or panel 172 may include a portion of the dashboard or a side panel associated with a door. Thus, the fire suppression apparatus 100' may be located in various strategic locations in numerous types of environments. Referring briefly to FIG. 8, a partial cross-sectional view of a fire suppression 25 apparatus 100" is shown in accordance with another embodiment of the present invention. The fire suppression apparatus 100" is similar to those described above but is configured to be portable such that it may be actuated and quickly disposed within a selected environment. Thus, for example, a manually deployed actuator 180 may be configured to actuate any igniting device associated with the gas-generating device 30 110". In operation, a user may deploy the actuator 180 by, for example, pulling a safety pin 182 and pressing a button or other mechanical device 184, thereby actuating an igniting device and combusting propellant contained within the gas generating device 110". A timer or other delay mechanism may also be incorporated with the actuator so that actuation of the associated igniting device and combustion of 18 the propellant contained within the gas-generating device 110" does not occur for a predetermined length of time. Such a delay mechanism may allow users to actuate the fire suppression apparatus 100" and then distance themselves therefrom so as to avoid contact with the apparatus 100" in cases where the heat of the apparatus 100" 5 or gases generated thereby may pose a threat when a user is in extremely close proximity therewith. Thus, in operation, a user may be able to deploy the actuator 180, dispose of the fire suppression apparatus 100" in an identified environment (e.g., in a room of a building, the cabin of an automobile or other vehicle, etc.) and, if necessary, remove 10 themselves from the fire suppression apparatus 100" to a remote location prior to the ignition and operation thereof. While the invention may be susceptible to various modifications and alternative forms, specific embodiments have been shown by way of example in the drawings and have been described in detail herein. However, it should be understood that the 15 invention is not intended to be limited to the particular forms disclosed. Rather, the invention includes all modifications, equivalents, and alternatives falling within the spirit and scope of the invention as defined by the following appended claims.

Claims (17)

1. A fire suppression apparatus comprising: a structure having a first inlet opening therein, a second outlet opening therein 5 and a flow path providing fluid communication between the first inlet opening and the second outlet opening; a gas-generating device located and configured to provide a flow of a first gas through a nozzle of the gas-generating device, the nozzle extending into and at least partially surrounded by a portion of the flow path, and to direct the flow of the first gas 10 out of the nozzle into the flow path downstream from the nozzle such that the flow of the first gas draws a volume of a second gas through the first inlet opening and into the flow path upstream from the nozzle; a diffuser in the flow path downstream of the nozzle, the diffuser located and configured to effect mixing of the first gas with the volume of the second gas drawn 15 into the flow path to form a gas mixture and to expand the gas mixture to reduce the velocity and the temperature of the gas mixture; and a heat transfer device disposed in the flow path between the diffuser and the first inlet opening and configured to allow at least the second gas therepast. 20

2. The fire suppression apparatus of claim 1, wherein the heat transfer device is thermally coupled with the nozzle of the gas-generating device.

3. The fire suppression apparatus of any one of claims 1 or 2, wherein the heat transfer device includes a plurality of thermally conductive fins. 25

4. The fire suppression apparatus of claim 3, wherein the plurality of thermally conductive fins is coupled with the nozzle of the gas-generating device.

5. The fire suppression apparatus of any one of claims 1 through 4, further 30 comprising an oxygen reducing device positioned within the flow path and configured to reduce a level of oxygen in the volume of the second gas as the second gas flows through the oxygen reducing device. -enaneo 20

6. The fire suppression apparatus of claim 5, wherein the oxygen reducing device includes an oxygen reactive material comprising at least one of iron, nickel, copper, zirconium and titanium. 5

7. The fire suppression apparatus of any one of claims 1 through 6, further comprising at least one additional heat transfer device disposed in the flow path.

8. The fire suppression apparatus of any one of claims 1 through 7, wherein the nozzle is configured to accelerate the flow of the first gas to a substantially sonic 10 velocity or greater.

9. The fire suppression apparatus of any one of claims 1 through 8, wherein the gas-generating device further includes a solid propellant composition configured to generate the first gas upon combustion thereof. 15

10. The fire suppression apparatus of claim 9, wherein the solid propellant composition is configured to generate a volume of at least one of N 2 , H 2 0 and CO 2 as the first gas. ?0

11. The fire suppression apparatus of any one of claims 9 or 10, further comprising an igniting device configured to ignite the solid propellant composition.

12. The fire suppression apparatus of any one of claims 1 through 11, further comprising an NOx scavenger disposed within the flow path. 25

13. The fire suppression apparatus of any one of claims 1 through 12, further comprising an NH 3 scavenger disposed within the flow path.

14. The fire suppression apparatus of any one of claims 1 through 13, further 30 comprising a filter disposed within the flow path.

15. A fire suppression system comprising: at least one fire suppression apparatus comprising: 21 a structure having a first inlet opening therein, a second outlet opening therein and a flow path providing fluid communication between the first inlet opening and the second outlet opening; a gas-generating device located and configured to provide a flow of a first gas 5 through a nozzle of the gas-generating device, the nozzle extending into and at least partially surrounded by a portion of the flow path, and to direct the flow of the first gas out of the nozzle into the flow path downstream from the nozzle such that the flow of the first gas draws a volume of a second gas through the first inlet opening and into the flow path upstream from the nozzle; 10 a diffuser in the flow path downstream from the nozzle, the diffuser located and configured to effect mixing of the first gas with the volume of the second gas drawn into the flow path to form a gas mixture and to expand the gas mixture to reduce the velocity and the temperature of the gas mixture; a heat transfer device disposed in the flow path between the diffuser and the 15 first inlet opening and configured to allow at least the second gas therepast; and a controller configured to generate a signal and transmit the signal to the at least one fire suppression apparatus upon occurrence of a specified event, wherein the gas-generating device is configured to provide the flow of the first gas upon receipt of the signal from the controller. 20

16. A fire suppression apparatus substantially as hereinbefore described with reference to the accompanying drawings.

17. A fire suppression system substantially as hereinbefore described with 25 reference to the accompanying drawings. .fwva