refer now to fig1 which is an overall drawing of the preferred embodiment of the invention . the device comprises a container 1 which contains a composition of inert gases 2 . in the form of the preferred embodiment the invention shall provide inert gas composition labeled ig - 541 by the united states environmental protection agency significant new alternatives program ( snap ), which comprises a blend of 52 % by volume nitrogen , 40 % by volume argon and 8 % by volume carbon dioxide . the container 1 contains this blend , with the subtraction of nitrogen in the preferred embodiment ; such that the container 1 is correspondingly 52 % smaller by volume than a typical ig - 541 container designed to protect identical enclosed volumes . a solid propellent gas generator 3 is operably attached to the container 1 . the solid propellent gas generator 3 contains special solid propellent 4 designed to generate nitrogen gas 5 when the burning of the propellent 4 is initiated by an electric squib 6 designed to initiate the propellent 4 . in the preferred embodiment the propellent 4 comprises a mixture of sodium azide and sulphur that is universally used in automotive airbag gas inflators and common to those experienced in the art . this composition generates almost pure nitrogen gas in a very inexpensive configuration . upon initiation and firing of the electric squib 6 ( either by automatic or manual initiation of an electric circuit upon detection of a fire in a compartment , and familiar to those experienced in the art ), the propellent 4 rapidly burns to generate nitrogen gas 5 which is directed to the container 1 by means of suitable plumbing 7 . in the preferred embodiment the exhaust part of the gas generator 3 contains a rupture disk 8 designed to prevent passage of the inert gas composition 2 from the container 1 into the solid propellent gas generator 3 , yet rupture upon generation of the higher pressures due to nitrogen gas 5 generated from the initiated solid propellent gas generator 3 to facilitate the release of nitrogen gas 5 from the initiated solid propellent gas generator 3 . in the preferred embodiment an optional dip tube 9 is enclosed in the container 1 and operably attached to the plumbing 7 to facilitate release of the nitrogen gas 5 into the lower portion of the internal volume of the container 1 . this is designed to promote mixing with the inert composition 2 enclosed in the container 1 . a discharge valve 10 facilitates containment of the high pressure inert gas composition 2 and nitrogen gas 5 . upon discharge of the nitrogen gas 5 from the solid propellent gas generator 3 into the lower portion of the container 1 , the discharge valve 10 releases the blended nitrogen gas 5 and the inert gas composition 2 out of the container 1 . the discharge valve 10 can be configured to contain a rupture disk designed to rupture at a pressure above the normal storage pressure of the inert gas composition 2 due to the addition of the nitrogen gas 5 from the solid propellent gas generator 3 to facilitate the release of the nitrogen gas 5 and the inert gas composition 2 . the blend of nitrogen gas 5 and the inert gas composition 2 moves through a conduit 11 or transport plumbing which is operably connected to the container 1 at the discharge valve 10 and an enclosed compartment 12 where it is released through a discharge nozzle 13 . thus , the blend of nitrogen gas 5 and said inert gas composition 2 is released into the enclosed compartment 12 in which a fire is located , effectively extinguishing the fire upon discharge of the nitrogen gas 5 and the inert gas composition 2 into the compartment 12 . the solid propellent gas generator 3 must be sized to generate the appropriate quantity of nitrogen gas 5 to blend with the inert gas composition 2 of argon and carbon dioxide to create a nitrogen , argon and carbon dioxide blend ratio of 52 %: 40 %: 8 % respectively in the preferred embodiment . the following example will illustrate the substantial volume savings achieved by using the nitrogen stored in solid form in the solid propellent gas generator 3 and supplied to the argon and carbon dioxide in the inert gas composition 2 stored as pressurized gas in the container 1 . a standard container size for storing ig - 541 is 3 . 8 cubic feet , stored at 2175 pounds per square inch pressure , which will generate 435 cubic feet of inert gas composition upon release into an enclosed atmosphere of approximately 925 . 5 cubic feet -- the estimated enclosure size in which such an amount of extinguishant will provide proper protection and safely extinguish fires . the weight of this inert gas composition is approximately 38 . 87 pounds mass in this container . accounting for molecular weights of the different inert gases in the composition , nitrogen accounts for approximately 44 . 83 percent of the composition weight ( or 17 . 43 pounds mass ), argon accounts for approximately 44 . 33 percent of the composition weight , and carbon dioxide accounts for approximately 10 . 84 percent of the composition weight . since the representative volumes of the inert gases are proportional to their relative concentrations , if nitrogen is removed from the composition , the container volume can be reduced by approximately 52 percent . 17 . 43 pounds of nitrogen must then be added to the remaining argon / carbon dioxide mixture that now requires only 1 . 82 cubic feet to store . a standard solid propellent gas generator blend of sodium azide and sulphur ( similar to those used in current automotive airbags ) can generate an almost completely pure nitrogen gas . for this blend , about 80 . 3 percent by weight of sodium azide and about 19 . 7 percent by weight sulphur is needed ( u . s . pat . no . 3 , 741 , 585 ). by balancing the chemical reaction , a total of 51 . 89 grams of nitrogen will be produced for every 100 grams of sodium azide / sulphur blend . the density of sulphur is approximately 2 . 07 grams per cubic centimeter , and the density of sodium azide is approximately 1 . 846 grams per cubic centimeter , so an estimated average density of the blend , adjusted for the proportion by weight of each ingredient , is approximately 1 . 89 grams per cubic centimeter . to generate the 17 . 43 pounds mass of nitrogen required from the generator , a total of 33 . 59 pounds mass of the gas generator propellent blend is required . using the estimated density of the blend and converting units , a gas generator of 0 . 29 cubic feet in volume is needed to supply the necessary mass of nitrogen . this is substantially less than the 1 . 98 cubic feet of nitrogen needed in compressed gas form . when the gas generator volume is added to the argon / carbon dioxide compressed gas mixture volume , a total volume of 2 . 11 cubic feet is required , which is a 44 . 5 percent reduction in required storage volume over a conventional compressed ig - 541 inert gas blend system to provide the same level of protection . the sodium azide nitrogen gas generator system was chosen as the preferred embodiment due to its low cost and wide availability , while retaining the substantial portion of system size reduction available using this technique . other variations may exist from the preferred embodiment . these include , but are not limited to , the use of other propellent blends that have been recently discovered that produce higher quantities of nitrogen gas per a given mass or volume of a propellent , but current experimentation and limited availability and cost limits their use at this time . in addition , the carbon dioxide component of the inert gas blend can also be generated by a propellent gas generator in a similar fashion and in addition to the nitrogen gas generator to further reduce overall system size . a particular blend of cupric oxalate , potassium perchlorate and other reactants , as detailed in u . s . pat . no . 3 , 806 , 461 , example 1 , can generate the necessary 4 . 21 pounds mass of carbon dioxide necessary for the system in example 1 of this disclosure detailed above in a carbon dioxide gas generator of 0 . 077 cubic feet , as opposed to the 0 . 304 cubic feet required for carbon dioxide in compressed gas state . the total space savings of utilizing both the carbon dioxide and nitrogen gas generators in concert with an argon compressed gas tank for the application expressed in example 1 above is a 50 . 5 percent reduction in required volume . this extra reduction in required volume may be offset by the increased complexity and expense of a carbon dioxide gas generator . in the present state of the art requiring argon , which is a noble gas and generally unreactive and nonexistent in a compound state , it is assumed that the argon must remain in compressed gas state unless cryogenically cooled , and the space savings approaches a limit of 60 percent due to the 40 percent requirement of argon in the blend . however , the door remains open for other carbon dioxide and nitrogen generating propellent blends which may become acceptable and thus further reduce the required space for such a system . these space savings will be greatly magnified in more common systems that protect much larger volumes of enclosed spaces in actual practice . other inert gas blends that provide fire protection capability can also be created using this approach , including one previously approved blend that uses 50 percent by volume argon and 50 percent by volume nitrogen . various techniques exist in the art for initiating the gas generators and controlling and distributing the flow of the inert gases which can be incorporated into the invention disclosed above , including multiple distribution channels and discharge outlets . there is thus described a novel compact , affordable inert gas fire extinguishing system which meets all of its stated objectives and which overcomes the disadvantages of existing techniques . the foregoing description of the preferred embodiment of the invention has been presented for the purposes of illustration and description . it is not intended to be exhaustive or limit the invention to the precise form disclosed . many modifications and variations are possible in light of the above teaching . it is intended that the scope of the invention not be limited by this detailed description , but should include such modifications and variations within the scope of the claims appended hereto .
a compact , affordable fire extinguishing system utilizes a combination of compressed inert gas tanks and solid propellent gas generators to provide a blend of inert gases to extinguish fires in an enclosure . the compressed inert gas tanks may contain gases such as argon or carbon dioxide or a combination thereof . the solid propellent gas generators may generate upon initiation either nitrogen or carbon dioxide or a combination thereof . the inert gases from both sources are blended into a composition that will extinguish fires at concentrations that will allow human occupancy during discharge . such a system can be constructed at a substantially smaller size than conventional compressed gas systems , due to the greater density of the inert gases in the propellent form in storage , which allows greater utility and affordability where installation space is limited or retrofit is desired into prior fire protection systems .