referring initially to fig1 of the drawings , a combination suppressant storage and nozzle unit generally designated 10 is illustrated in vertical cross - section . tubular nozzle structure broadly designated 12 is preferably a conventional reducing long elbow 14 which may have a small diameter circular end 16 of a diameter for example of 4 inches i . d . and a large circular end 18 of approximately 6 inches i . d . welded onto the large end 18 of elbow 14 is a conventional end cap 20 having a cylindrical side wall 22 and a dome - shaped end wall 24 . flange structure broadly designated 26 is provided at the small end of reducer 14 and may take the form of a flange 28 welded to small diameter end 16 in circumscribing relationship thereto . the internal cylindrical diameter of flange 28 concentric with the axis of end 16 is of stepped configuration presenting grooves of increasing diameter as the outer face 30 of the flange is approached . the first , innermost step 32 of flange 28 meets with an outer large diameter step 34 . an annular stepped ring 36 is configured to be received within the stepped opening of flange 28 and thereby has an inner shoulder 38 of dimensions to be complementally received within step 32 . the major portion 40 of ring 36 is likewise complementally received within the step 34 of flange 28 . means for removably securing the ring 36 to flange 28 takes the form of a series of threaded studs 42 which extend through ring 36 and are threaded into flange 28 . a bulged rupture disc 44 is clamped in the flange structure 26 between ring 36 and the flange 28 . disc 44 has a concavo - convex central rupture section 46 with the convex surface thereof facing outwardly . a transversely l - shaped lip portion 48 received between ring 36 and flange 28 and is clamped against step 32 with the outer upturned extremity of the section 48 extending toward outer step 34 in order to assure a fluid tight seal when the disc 48 is secured in place within flange structure 26 . preferably , disc 44 is fabricated of relatively thin metal material such as stainless steel of uniform thickness so that controlled bursting thereof is assured . in order to enhance full opening of disc 44 upon command , the concavo - convex section 46 may be scored with a cross pattern 50 thus causing the disc to open in four leaves providing a substantially unimpeded flow relief passage through the end 16 of nozzle structure 12 . opening of disc 44 upon command is preferably accomplished by a provision of initiator or detonator assembly broadly designated 52 . a tubular boss 54 welded to elbow reducer 14 and communicating with the interior thereof mounts an elongated initiator support tube 56 . it is noteworthy in this respect that the inner extremity of boss 54 is oblique and surfaced such that it is smoothly complemental with the interior rounded surface 58 of elbow reducer 14 . the outer end of boss 54 is internally stepped as at 60 for receipt of the complementally flanged outer end 62 of the detonator support tube 56 which is telescoped therein . the internally stepped surface 60 of boss 54 is threaded for receipt of an annular stop nut 64 . the innermost end 66 of detonator support tube 56 terminates adjacent rupture disc 54 as depicted in fig1 and preferably is disposed substantially at the point of engagement of the innermost face of ring 36 with the inner step 32 of flange 28 . a small rupture disc 68 silver soldered to the innermost end 66 of support tube 56 serves to hermetically seal the interior of storage nozzle unit 10 and prevent outflow of suppressant through the assembly 52 . an electrically actuated initiator or detonator 70 is positioned within tube 56 adjacent disc 68 and has leads 72 which lie within tube 56 and exit from boss 54 through the fitting 74 threaded into the flanged part of tube 56 . although not depicted , it is understood that the nozzle structure 12 is desirably provided with a nipple fitting on the side wall 14 having a removable threaded cap thereon allowing filling of the interior of the structure 12 with a suitable liquid suppressant such as halon 1301 under pressure . the fitting also serves to permit the introduction of compressed gaseous nitrogen which by virtue of the difference of density thereof as compared with that of halon 1301 causes the nitrogen to be contained at the top of the unit 10 in overlying relationship to the suppressant . the halon is normally held under an applied pressure of compressed gaseous nitrogen at a pressure of about 360 psi whereby the suppressant is maintained at its vapor pressure of about 200 psi . furthermore , the halon 1301 if contained within unit 10 under a nitrogen pressure of about 360 psi will be about 90 % in liquid form and about 10 % in gaseous form between the liquid level and the layer of nitrogen . if desired , a pressure gauge may be provided on the side wall 14 of nozzle structure 12 in communication with the interior of the reducer 14 in order to permit observation of the pressure within the unit 10 at any desired time . in the use of unit 10 , an explosion protection system will normally include a device for sensing an incipient explosion . this may take the form of a pressure rise detector , an infrared detector , or other suitable means to indicate the onset of an explosion . most frequently , systems rely upon pressure detectors for this purpose because of the reliability of such detectors and the fact that they are well adapted to effect closing of a switch upon shifting of a pressure sensitive diaphragm which activates an electrical circuit for electrical triggering of the detonator 70 . the unit 10 is disposed such that discharge of suppressant therefrom will impinge directly on the area to be protected from an explosion . thus , if it is desired for the suppressant to be dispersed other than vertically or horizontally as shown in fig1 a suitable deflector may be provided in association with flange structure 26 to divert the suppressant in any desired direction after delivery thereof from the unit 12 . deflectors of various sizes and shapes may be used ; e . g ., a curved fan shaped deflector may advantageously be used in certain applications . if the deflector is tubular in construction , it should be of dimensions which do not cause upstream turbulent outflow of suppressant from the nozzle structure 10 . when an electrical command signal is sent to the detonator 70 from the pressure sensitive detector or the like , actuation of the detonator opens disc 68 causing the shock wave to directly impinge on the concave face of rupture disc 44 thereby causing the latter to open fully in the form of four individual petals . instantaneous release of the pressurized suppressant such as halon 1301 allows delivery of the suppressant from the interior of unit 12 as the suppressant flows outwardly through opening 16 and ring 36 . because the reducer 14 is filled with suppressant , or at least there are no parts of the reducing elbow filled with suppressant which do not decrease in diameter as the small circular end 16 thereof is approached , the liquid suppressant is maintained in liquid form throughout the time of discharge and there is no tendency for such liquid as the pressure is released thereon to vaporize and form bubbles in the liquid causing turbulent , choked two - phase flow . although the interior cylindrical surface 76 of ring 36 in a preferred embodiment does not decrease in diameter as the outer extremity of the ring is approached , such construction could be provided if desired . it has been found though that the length of passage 76 is of such short dimension axially thereof that the outrush of suppressant is so great that there is no opportunity for the liquid to vaporize and to form two - phase turbulent flow which would interfere with release of the suppressant and thereby decrease its delivery time . improved suppressant delivery rates have been accomplished using the constantly reducing diameter elbow 14 of the present invention as compared with the 90 ° elbow previously employed . in an exemplary system , as previously indicated , sensing of a 1 / 4 pound pressure rise can readily be accomplished within 5 milliseconds and in many instances at times of the order of 2 milliseconds . a 1 millisecond time loss is normally encountered in the electronic control panel where a check must be carried out to make certain that the detector has sensed a condition calling for discharge of suppressant . once the command signal has been sent to the detonator , there is a finite period of time involved in firing of the initiator . generally , this time loss is of the order of three milliseconds . accordingly , 5 to 6 milliseconds elapse in detection of pressure rise or other indication of an impending explosion and activation of the detonator . the next elapsed time is the most critical because as previously pointed out , the pressure rise curve of an explosion is somewhat parabolic in shape . thus , the longer the time period after initiation of the event , the closer the pressure rise comes to the time where it increases exponentially . accordingly , the faster suppressant can be delivered to the site to be protected , the more likely that effective protection can be afforded . using a conventional long radius 90 ° elbow of uniform internal diameter throughout its length of 3 . 063 inches , and a longitudinal dimension of about 9 inches ( measured along the centerline of the passage through the elbow ), tests showed that the time required to effect discharge of halon from a 1 . 8 liter storage container ( 6 pounds of halon 1301 ) was at least about 120 milliseconds . a 7 liter storage bottle ( containing about 24 pounds of halon 1301 ) required at least about 190 milliseconds for the contents of the containment vessel to be expelled . in view of this data , an average expulsion time of about 180 milliseconds can be routinely used in planning explosion protection installations and advising users of the potential of the system . when a reducing elbow was used as depicted in fig1 having a 4 inch outlet and a maximum diameter of 6 inches overall , the discharge time for the halon suppressant was found to be no more than about 45 milliseconds . the reduction in discharge time was therefore much greater than could be attributed simply to the dimensional differences between the 3 inch diameter discharge orifice of the conventional long radius 90 ° elbow tested as compared with the 4 inch diameter of orifice 16 of the 4 - 6 inch reducing elbow 14 . these studies led to the understanding that it is desirable to maintain the ratio of the length of the centerline of the passage for discharge of a liquid suppressant such as halon 1301 under pressurized containment calculated on the basis of the length of the passage that is of uniform cross - sectional area , with respect to the diameter of the final orifice through which the suppressant is delivered . this l / d ratio should be maintained at a value no greater than 1 and preferably less than 0 . 5 . in the instance of the 90 ° uniform internal diameter elbow compared with the reducing elbow discharge nozzle of this invention , the l / d ratio ( 9 / 3 = 3 ) is far greater than 1 . on the other hand , using a 4 - 6 inch reducing elbow , and 11 / 2 inch thick flange as depicted in fig1 wherein the length of the passage 76 of equal diameter throughout its length presented by the flange 26 is no more than about 11 / 2 inches , the l / d ratio is 1 . 5 / 4 = 0 . 37 . for economy , it is desirable to use steel reducing elbows commercially available on the market . the 4 - 6 inch reducing elbow of the preceding test is a unit that can be purchased on the open market . other reducing elbows of different sizes are also readily available . the use of reducing elbow 14 permits ready variation of the amount of suppressant that may be contained for release to a particular area to be protected . for example , in fig3 the modified suppressant storage and nozzle unit 110 has a reducing elbow 114 , flange structure 126 , an initiator within assembly 152 , and a rupture disc which are identical to the same components as illustrated in fig1 . in this instance though , a length of conventional 6 inch pipe 176 is welded between the largest end 118 of elbow 114 and the end cap 120 which is identical to cap 20 . it can be appreciated that pipe section 176 can be of any desired length depending upon the volume of suppressant required for a particular application . of primary importance though is the fact that there are no internal surfaces within the unit 110 that increase in cross - sectional diameter , and then decrease before discharge of the suppressant through the final outlet orifice . the internal diameter stays the same , or then uniformly decreases as the discharge opening is approached to assure that there is no tendency for the suppressant to vaporize when the rupture disc opens thereby exposing the confined suppressant to the lower atmospheric pressure . in fig4 a suppressant storage and nozzle unit 210 represents a further modification of the invention . the nozzle structure 212 is identical to nozzle structure 12 . however , a stepped adapter 278 ( sometimes referred to as a type of eccentric reducer ) is welded to the upper large end 218 of elbow 214 in order to increase the suppressant storage capacity of the system . in the case where a 4 - 6 inch reducing elbow 214 is employed , the adapter 278 may be a 6 - 10 inch eccentric reducer . the small diameter end 280 of adapter 278 is of a dimension to complementally fit with the end 218 of reducing elbow 214 while the upper large diameter end 282 of adapter 278 is of particular dimensions to provide the necessary volume of suppressant . again , adapter 278 is a conventional item used to reduce from one diameter of cylindrical pipe to another . a conventional end cap 220 as illustrated in fig4 may be welded direct to the large end 282 of adapter 278 , or if desired , and optionally , a pipe section 276 may be interposed between end 282 of adapter 278 and the cap 220 . as with unit 110 , wherein the length of intermediate pipe section 176 may be of any desired length , the length of pipe section 276 may be varied at will to change the volume of contained suppressant . the stepped or eccentric reducing adapter 278 has interior walls which provide a smooth uninterrupted transition from the larger diameter of end 282 leading toward the small diameter end 280 . in all instances , the interior , intermediate cross - sectional diameter of the midsection 284 of adapter 278 decreases uniformly between the large end 282 and the small end 280 . fig5 and 7 illustrate other suppressant storage and nozzle units that embody the principles of the present invention . in the embodiment of fig5 and 6 , suppressant storage and nozzle unit 310 is a 4 - 6 inch unstepped concentric pipe reducer 314 which has flange structure 326 on the small end 316 of the pipe concentric mounting a rupture disc 344 , all of which are of identical construction to that of flange 26 . the only difference in constructional details is the length and disposition of boss 354 forming a part of initiator housing 352 . the boss 354 corresponds to boss 54 of unit 10 . tube 356 forming a part of initiator housing 352 is of somewhat different length than tube 56 . here again though , the boss 354 welded to the side wall of the pipe concentric 314 at an angle such that the tube 356 carried thereby does not significantly impede free flow of liquid suppressant from the concentric through the orifice defined by flange 326 upon opening of rupture disc 344 . the end cap 324 is the same as end cap 24 , and again a conventional 6 inch pipe section 376 may be interposed between end cap 324 and the large end 318 of concentric reducer 314 . unit 410 illustrated in fig7 and 8 is the same as embodiment 310 except that the nozzle structure 412 is made up of an unstepped eccentric pipe reducer 414 as a replacement for the concentric reducer 314 . otherwise , the components are the same as those of unit 310 . although the units 10 - 410 inclusive are especially adapted for containment and controlled discharge of a liquid suppressant such a halon 1301 , a particularly important feature of the units is the fact that if desired , a solid powdered composition may be used as a suppressant medium in lieu of a liquid . useful powder suppression agents in this respect include boric acid , monoammonium phosphate and sodium bicarbonate . disposition of the initiator 70 in close proximity to the rupture disc 44 causes the shock wave produced thereby upon actuation of the detonator to impinge directly on the concave face of the disc to effect instantaneous full opening thereof without dissipation of the energy produced by the detonation . although detonator 70 would not have to be located as close to rupture disc 44 as illustrated in unit 10 of fig1 where nozzle structure 12 is used in a liquid suppressant application , the construction as depicted is preferred because it makes the unit universally usable for both liquids and powders without modification . the improved high rate discharge nozzle structure of this invention also has utility for explosion protection systems which function as isolation devices . for example , if a grinding machine has a dust duct leading to an outside dust collector such as a bag house , an explosion in the collector unit can have catastrophic consequences inside of the building where the grinding machine is located . this can be especially dangerous to workers around the grinding machine . although bag houses are generally equipped with explosion relief vents , when an explosion does occur , it is possible that the gaseous combustion products generated , even though substantially vented from the bag house through the relief openings in the collector house , will be at a high enough pressure level to cause gasses and even the flame front itself to back flow through the duct work connecting the grinding machine or machines to the dust collector unit . this can result in an explosion inside the grinding machine . in order to preclude such event from happening , a protection system can be installed in the duct work leading from a grinding machine or other source of dust , to the remotely located dust collector . the protection system included a pressure detector or a light activated component , a controller and a suppressant storage and release assembly . if the detector senses an untoward condition in the duct work , the controller sends an electrical command to the detonator to open the rupture disc serving to contain a liquid or powder suppressant in a containment vessel of a type as depicted in one of the previously described vessels . release of the suppressant in the dust duct serves to stop the reverse flow of hot gasses toward the source of the dust and to suppress any advancing flame front which could cause an explosion at the grinding machine or the like . here again , unimpeded flow of suppressant from the containment vessel is imperative in the shortest possible time period .
a suppressant delivery and release nozzle structure is disclosed for an explosion protection system . the nozzle is a reducing elbow , concentric or eccentric mounting a rupture disc at its small end . a selectively actuatable detonator housed in the nozzle adjacent the disc permits substantially instantaneous opening of the disc upon command for release and delivery of suppressant to a zone to be protected from an explosion hazard . the configuration of the nozzle assures unimpeded discharge of suppressant from the system in a minimum of time without significant two - phase flow . the nozzle is equally adaptable for liquid or powdered suppressant compositions .