Quick connect pressure reducer/cylinder valve for self-contained breathing apparatus

Abstract

A quick pressure reducer and cylinder valve for use with an SCBA includes a cylinder valve that connects to a pressure vessel, a pressure reduction assembly for reducing the pressure of breathing air provided by the pressure vessel, a probe, and an inlet/latch assembly. The probe includes a notch and a threadless probe tip, and the inlet/latch includes a corresponding receptacle and one or more latches adapted to fit into the notch to retain the probe in the receptacle. A pushbutton switch in the receptacle is triggered by insertion of the probe tip therein, thereby providing an electrical signal. Probes of different sizes may be used to correspond to different pressure capacities, and the inlet/latch assembly may be arranged either to permit the insertion of only one probe size or may be arranged to accept different sizes but to function differently based on the size of the probe. The latches are inoperable except at or below a nominal pressure.

Claims

1. A universal cylinder valve and pressure reducer for use in a self-contained breathing apparatus, comprising: a cylinder valve that connects to a pressure vessel; a pressure reduction assembly; a first probe having a probe tip of a first size; a second probe having a probe tip of a second size, the second size being different from the first size; and an inlet/connector assembly, including: a probe tip receptacle adapted to receive the probe tip of the first probe at a first size therein and to establish a fluid connection therewith, and further adapted to alternatively receive the probe tip of the second probe at a second size therein and to establish a fluid connection therewith, and a connector adapted to retain the first probe at the first size when the first probe is inserted in the probe tip receptacle, and adapted to alternatively retain the second probe at the second size when the second probe is inserted in the probe tip receptacle.

2. The universal cylinder valve and pressure reducer of claim 1, wherein the first probe and the second probe are each mountable to the cylinder valve, and wherein the inlet/connector assembly is connected to the pressure reduction assembly.

3. The universal cylinder valve and pressure reducer of claim 2, wherein the connector is a latch.

4. The universal cylinder valve and pressure reducer of claim 3, wherein each of the first and second probes includes a notch, and wherein the latch includes a latch shoulder configured to fit into the notch of the probe that is inserted in the probe tip receptacle.

5. The universal cylinder valve and pressure reducer of claim 4, wherein each notch is disposed in a side of the respective probe, wherein each probe defines a central axis, and wherein the latch shoulder is movable in a direction transverse to the central axis of the respective probe when the probe is inserted in the probe tip receptacle.

6. The universal cylinder valve and pressure reducer of claim 2, wherein the inlet/latch assembly includes an inlet nozzle disposed in the probe tip receptacle.

7. The universal cylinder valve and pressure reducer of claim 6, wherein the first and second probes each include a hollow in the respective probe tip thereof, each hollow being adapted to receive a distal end of the inlet nozzle when the respective probe is inserted into the probe tip receptacle.

8. The universal cylinder valve and pressure reducer of claim 6, wherein the inlet/connector assembly further includes a disk coaxially arranged around the inlet nozzle.

9. The universal cylinder valve and pressure reducer of claim 8, wherein the disk is spring-loaded.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Further features, embodiments, and advantages of the present invention will become apparent from the following detailed description with reference to the drawings, wherein;

(2) FIG. 1 is a block diagram of a self-contained breathing apparatus incorporating a quick connect valve and pressure reducer, in accordance with the preferred embodiments of the present invention;

(3) FIG. 2 is a perspective view of the quick connect value and pressure reducer of FIG. 1;

(4) FIG. 3 is a side plan view of the quick connect valve and pressure reducer of FIG. 2;

(5) FIG. 4 is a top plan view of the quick connect valve and pressure reducer of FIG. 2;

(6) FIG. 5 is a front plan view of the quick connect valve and pressure reducer of FIG. 2;

(7) FIG. 6 is a perspective view of the cylinder valve of FIG. 2, shown in isolation;

(8) FIG. 7 is a top plan view of the cylinder valve of FIG. 6 with a protective cap attached;

(9) FIG. 8 is a rear plan view of the cylinder valve of FIG. 7, shown in isolation;

(10) FIG. 9 is a left side cross-sectional view of the cylinder valve of FIG. 7, taken along line 9-9;

(11) FIG. 10 is a rear cross-sectional view of the cylinder valve of FIG. 7, taken along line 10-10;

(12) FIG. 11 is a perspective view of the probe of FIG. 6, shown in isolation;

(13) FIG. 12 is a left side plan view of the probe of FIG. 11;

(14) FIG. 13 is a front plan view of the pressure reducer of FIG. 2 shown in isolation;

(15) FIG. 14 is a top plan view of the pressure reducer of FIG. 13;

(16) FIG. 15 is a front cross-sectional view of the pressure reducer of FIG. 13, taken along line 15-15;

(17) FIG. 16 is a top cross-sectional view of the pressure reducer of FIG. 13, taken along line 16-16;

(18) FIG. 17 is right side cross-sectional view of the pressure reducer of FIG. 13, taken along line 17-17;

(19) FIG. 18 is a front schematic view of the pressure reducer of FIG. 13, showing the state of the pressure reducer at initial activation;

(20) FIG. 19 is a front schematic view of the pressure reducer of FIG. 13, showing the latch pins being forced into openings in the latches;

(21) FIG. 20 is a front schematic view of the pressure reducer of FIG. 13, illustrating normal high pressure operation of the pressure reducer;

(22) FIG. 21 is a front schematic view of the pressure reducer of FIG. 13, illustrating normal low pressure operation of the pressure reducer;

(23) FIG. 22 is a front view of an alternative pressure reducer;

(24) FIG. 23 is a top cross-sectional view of the pressure reducer of FIG. 22, taken along line 23-23; and

(25) FIG. 24 is a left side cross-sectional view of the pressure reducer of FIG. 22, taken along line 24-24.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(26) Referring now to the drawings, in which like numerals represent like components throughout the several views, the preferred embodiments of the present invention are next described. The following description of the preferred embodiment(s) is merely exemplary nature and is in no way intended to limit the invention, its application, or uses.

(27) FIG. 1 is a block diagram of a self-contained breathing apparatus (SCBA) 10 carried by firefighters, other emergency services workers, and the like, that incorporates a quick connect valve and pressure reducer 20, in accordance with the preferred embodiments of the present invention. The SCBA 10 includes one or more pressure vessel 12, the quick connect valve and pressure reducer 20, a second stage pressure reduction assembly or regulator 14, a facepiece 16 and a hose assembly 18. The pressure vessel 12 is a pressurized cylinder or tank that provides a supply of breathing gas to the wearer. In one preferred form of the invention the tank 12 may be of a type that initially holds air at a pressure of about 316.4 kg/sq.cm. (4500 p.s.i.g.) or another standard capacity. The quick connect valve and pressure reducer 20 is disposed at the outlet of the tank 12 and in fluid communication therewith. The hose assembly 18 is connected between the quick connect valve and pressure reducer 20 and the facepiece 16 via the second stage regulator 14. This breathing regulator 14, which is preferably disposed on the facepiece 16 as seen schematically in FIG. 1, includes a regulator chamber (not shown) in fluid communication with the hose assembly 18. The facepiece 16 covers the wearer's nose and mouth in airtight connection, and preferably covers the wearer's eyes with a transparent shield 15 for external viewing. The second stage regulator 14 may be any one of a number of conventional or novel types, including demand type regulators or positive pressure type regulators.

(28) In addition, the SCBA preferably includes an electronics system (not shown). In its simplest embodiment, the electronics system is simply an audible alarm generator. The audible alarm generator may be triggered under certain conditions, such as described hereinbelow. However, much more complex electronics may be available, such as that described in the aforementioned U.S. patent application Ser. No. 10/744,901.

(29) FIG. 2 is a perspective view of the quick connect valve and pressure reducer 20 of FIG. 1, while FIGS. 3, 4 and 5 are side, top and front plan views, respectively, of the quick connect valve and pressure reducer 20 of FIG. 2. As shown therein, the quick connect valve and pressure reducer 20 includes a cylinder valve 22 and a pressure reducer 24. The cylinder valve 22 and pressure reducer 24 may be easily separated and connected via a quick connect mechanism described in greater detail below.

(30) FIG. 6 is a perspective view of the cylinder valve 22 of FIG. 2, shown in isolation; FIGS. 7 and 8 are top and rear plan views, respectively, of the cylinder valve 22 of FIG. 6 with a protective cap 45 attached; and FIGS. 9 and 10 are left side and rear cross-sectional views of the cylinder valve 22 of FIG. 7, taken along lines 9-9 and 10-10, respectively. As shown therein, the cylinder valve 22 includes a valve body 26, a cylinder connection 28, a CGA assembly 30, a valve assembly 32, a pressure gauge assembly 34, a bumper guard assembly 36, a safety valve assembly 38 and a probe assembly 40. As with conventional valve bodies, the valve body 26 is integrally formed and includes a plurality of bores, as shown in FIGS. 9 and 10. The cylinder connection 28 includes a drain tube 42 disposed within, and extending from, a threaded male fitting 41, which may be integrally formed with the valve body 26. The cylinder connection 28 is preferably of a conventional design and size that may be attached to the pressure vessel or tank 12 or other standard tanks by inserting the drain tube 42 into the end of the tank 12 and screwing the male fitting 41 into a corresponding female threaded female fitting in the tank 12. A packing 43 is included around the threaded fitting 41 in order to ensure a tight seal. The threaded fitting 41, drain tube 42 and packing 43 may each be of conventional design.

(31) The CGA assembly 30 includes a threaded male fitting 44, best seen in FIG. 6, a protective cap 45, best seen in FIG. 7, and a check valve (not shown). The threaded fitting 44 is preferably a standard CGA fitting that is itself screwed into the valve body 26. The protective cap 45 may be a cover loosely connected to the valve body 26 via a tether 46. In one embodiment, the cover is formed from aluminum, and the tether is formed from a rubber compound. Alternatively, however, the cover may be formed from plastic, while the tether 46 may be a metal chain. The CGA assembly 30 is preferably of conventional variety, such as that used in prior art cylinder valves 22 as the primary connection point between the valve and a conventional first stage pressure reducer. When the check valve is forced open by a stem on a corresponding threaded female fitting, a direct air path is preferably created from the air tank 12 through the outlet of the CGA assembly 30 for a purpose discussed hereinbelow.

(32) As perhaps best shown in FIG. 10, the valve assembly 32, which may likewise be of conventional construction, includes a handle 49, valve plug and assembly 50, packing washer 52, wear washer 54, nylon lock nut 56, stem valve 58, spring 60, bonnet 62 and packings 64, 66. The valve plug and assembly 50 is disposed within a bore in the valve body 26 so as to control the passage of gas through the valve body 26. The stem valve 58 is arranged to extend axially through the bonnet 62, which is threaded into the valve body 26, to the handle 49, which is connected to the stem valve 58 via the lock nut 56. The spring 60, which may be a helical compression spring, is arranged to bias the handle 49 away from the bonnet 62. Notches (not shown) are disposed radially around the bottom of the handle 49 and adapted to engage tabs (not shown) extending radially from the bonnet 62 when the handle 49 is not in use. To open or close the valve 58, the handle 49 may be manually forced toward the valve body 26 in order to disengage the tabs from the notches, this permitting the valve assembly 32 to be screwed in or out as desired. All of these components may be of conventional design and construction.

(33) As perhaps best shown in FIG. 9, the pressure gauge assembly 34 includes a pressure gauge 68, a cover 70, a back-up ring 72 and a packing 74. The pressure gauge 68, which is marked or otherwise adapted to provide a numerical or other visual indication of the magnitude of the pressure in the tank 12, is arranged in a bore in the valve body 26 that is disposed on the upstream side of the gas path from the valve plug and assembly 50. The cover 70 is a transparent plastic shield that prevents external debris and the like from damaging the gauge 68. The bumper guard assembly 36, which includes a bumper guard 76 comprising a hard rubber cover surrounding a metal core, fastened to the valve body 26 via screws 78, protects the cover 70 and gauge 68 from external physical blows, bumps and the like. The pressure gauge assembly 34 and bumper guard assembly 36 may each be of conventional construction.

(34) Also as shown in FIG. 9, the safety valve assembly 38 includes a burst disc 80, a safety body 82, and a safety cap washer 84, each of which may be of conventional design. The safety valve assembly 38 is arranged in a bore in the valve body 26 that is also disposed on the upstream side of the gas path from the valve plug and assembly 50. The safety valve assembly 38 provides an emergency release path should the pressure within the cylinder valve 22 exceed a predetermined threshold, as governed by the design of the burst disc 80 and the rest of the assembly 38.

(35) Referring again to FIG. 9, the probe assembly 40 includes a threaded female fitting 85, a probe 86 and a packing 87. The female fitting 85 is preferably formed in the valve body 26 itself, and the probe 86 includes a threaded male fitting 91 at one end which is screwed into the female fitting 85 in the valve body 26. The packing 87 helps to ensure a tight seal between the probe 86 and the valve body 26, while the threaded fittings 85, 91 facilitate the easy removal of one probe 86 from the valve body 26 and replacement with a different one. Alternatively, if a permanent connection is desired the probe 86 may be affixed in place within the valve body 26.

(36) FIG. 11 is a perspective view of the probe 86 of FIG. 6, shown in isolation, and FIG. 12 is a left side plan view of the probe 86 of FIG. 11. Disposed at the end opposite the threaded male fitting 91 is a tapered probe tip 93, whose widest point defines a tip rim 94, having a cylindrical or tapered hollow 95 disposed therein. Intermediate the probe tip 93 and the male fitting 91 are a circumferential notch 96, a shaft 97 and a hexagonal flange 98. As shown in FIG. 9, a bore 92 is disposed within the threaded end and connected in fluid communication with the cylindrical hollow 95 at the opposite end by a narrow tube 99. The hexagonal flange 98 makes it possible to use a wrench or similar tool to install or uninstall the probe 86 from the valve body 26, while the purpose of the other elements of the probe 86 will become apparent hereinbelow. The probe 86 is preferably integrally formed from a single piece of metal, such as stainless steel, and more preferably overmolded with a suitable thermoplastic such as PolyEtherEiher-Ketone (PEEK).

(37) The dimensions of the probe 86 and its various features may be varied as desired. However, changes in the dimensions or design of the probe 86 may need to be coordinated with corresponding changes in the dimensions or design of portions of the pressure reducer 24, as will become apparent below. Optionally, a set of probes 86 having different dimensions may be developed such that each differently-sized or -shaped probe 86 is intended for use only with tanks 12 of a particular capacity or pressure level. For example, a longer, narrower probe could be intended for use with a 4500 p.s.i.g.-rated tank 12, while a shorter, thicker probe 86 could be intended for use with a 2216 p.s.i.g.-rated tank 12. These dimensional changes may be coordinated by dimensional changes in particular elements of the pressure reducer 24 for a purpose more fully described hereinbelow.

(38) FIGS. 13 and 14 are front and top plan views of the pressure reducer 24 of FIG. 2, shown in isolation. The primary components of the pressure reducer 24 include a pressure reduction assembly 110, a manifold assembly 180, an inlet/latch assembly 190 and an electrical assembly 130 (best seen in FIG. 17).

(39) FIG. 15 is a front cross-sectional view of the pressure reducer 24 of FIG. 14, taken along line 15-15, and FIGS. 16 and 17 are top and right side cross-sectional views of the pressure reducer 24 of FIG. 13, taken along lines 16-16 and 17-17, respectively. The pressure reduction assembly 110 includes a housing 111, primary and secondary reducer modules 122, 123, a transfer valve assembly 124, a high pressure elbow assembly 126, pressure plugs 134, packings 135, a diffuser assembly 136 (best seen in FIG. 16), a positioner assembly 138 (best seen in FIG. 17) and a quick charge assembly 140. The housing 111 is preferably machined from a single block of suitable metal, such as an aluminum forging, and includes a variety of bores and other adaptations for the various components, as well as a plurality of connecting conduits 112, 114, 115 linking the components together.

(40) Referring again to FIG. 15, the primary and secondary reducer modules 122, 123 each comprise a collection of conventional components, including a respective piston head 150, 151, a respective hollow piston shaft 152, 153 and a respective helical compression spring 154, 155. Although not shown, one or both of the reducer modules 122, 123 may be built as an independently replaceable modular unit, which may simplify manufacture and repair. In general, the assemblies 122, 123 utilize a balanced piston design in that the respective components of the two reducer modules 122, 123 are similar, except for the strengths of the respective compression springs 154, 155. Gas may be fed to the two reducer modules 122, 123 via a central supply conduit 112. The transfer valve assembly 124 likewise includes a collection of conventional components, including a valve 160 and a valve sleeve 162. Design and construction of the pressure reducer 24 may be more straightforward if the transfer valve assembly 124 is disposed intermediate the primary and secondary reducer modules 122, 123, as shown, but other arrangements will be apparent to those of ordinary skill in the art.

(41) The quick charge assembly 140 provides an alternative means for supplying high pressure breathing gas to the central supply conduit 112 to be distributed through the pressure reducer 24 to the user. It is anticipated that such a feature would typically be used during emergency situations, where the tank 12 connected to the cylinder valve 22 is empty or malfunctioning and there is no time to replace or repair it. As perhaps best shown in FIG. 16, the quick charge assembly 140 includes a male coupling covered by a protective cap 143. The coupling 142 is oriented horizontally but at a slight forward angle relative to the primary axes of the pressure reducer 24. The quick charge assembly 140 interfaces with the central supply conduit 112 and the pressure reducer housing 111 via a check valve 144, a pair of orifice plates 146 and a seal retainer spring 148.

(42) Referring again to FIGS. 14 and 15, the manifold assembly 180, which includes an automatic transfer valve assembly 182, is fastened to the housing 111 of the pressure reduction assembly 110 via a plurality of screws 181, which may be of a socket-head type. The manifold assembly 180 is generally of conventional design and construction, adapted to fit with the pressure reducer housing 111 and its various components.

(43) Referring again to FIGS. 16 and 17, the inlet/latch assembly 190, which is attached to the font of the pressure reduction assembly 110 via a plurality of screws, primarily includes a probe tip receptacle 197, a pair of cylinder latches 192, 193, an inlet nozzle 194 and a pair of latch lock pins 204, all arranged in a housing. The probe tip receptacle 197 is a cylindrical opening adapted to receive the probe tip 93, while the proximate end of the inlet nozzle 194 is adapted to fit snugly within the cylindrical hollow 95 in the probe tip 93 when the probe tip 93 is inserted into the receptacle 197. When thus arranged, an air path is completed between the cylinder valve 22 and the pressure reducer 24. The snug fit of the inlet nozzle 194 within the probe tip 93 may be further enhanced by the inclusion of a packing 195 disposed near the end of the nozzle 194, thereby providing a seal between the cylindrical hollow 95 of the probe 86 and the nozzle 194, while the distal end of the nozzle 194 may be sealed to the pressure reduction assembly 110 with a packing 202 and lubricant.

(44) The latches 192, 193 are arranged transversely within the inlet/latch assembly 190 and include respective latch shoulders 198, 199 adapted to fit within the circumferential notch 96 in the probe 86. Springs 189 are provided to bias the two latches 192, 193 toward each other. Bearings 48, preferably formed from a self-lubricating material, are provided on the latches 192, 193. In addition, as perhaps best seen schematically in FIGS. 18-21, an opening is disposed in the body of each latch 192, 193 to accommodate one of the latch lock pins 204 as next described.

(45) The latch lock pins 204 are oriented perpendicularly relative to the latches 192, 193 and arranged to be coaxial with correspondingly-shaped and -sized openings in the latches 192, 193 when the latches 192, 193 are in their normal biased positions. However, a compression spring 206 is arranged around each latch lock pin 204 in order to bias the pins 204 away from the latches 192, 193, thereby permitting the latches 192, 193 to be moved transversely when sufficient forces are exerted thereon. The latch lock pins 204 reside in bores in the inlet/latch assembly 190 which are in fluid communication with the central supply conduit 112 via connector conduits 114, 115, thus permitting the distal ends of the latch lock pins 204 to be subjected to the same gas pressure as is supplied to the central supply conduit 112. The latch lock pins 204 are equipped with a packing 210, held in place by a packing retainer 208 and coated with a lubricant, in order to ensure a tight seal. The compression springs 206 are preferably selected and installed so as to be overcome when a relatively nominal threshold pressure, which for example may be 50 p.s.i.g., is applied to the distal ends of the pins 204. Thus, when a gas pressure of more than the threshold exists in the central supply conduit 112, the proximate ends of the pins 204 are forced into the openings in the latches 192, 193, thus preventing the latches 192, 193 from being moved. As a result, the latches 192, 193 are locked in place whenever the threshold gas pressure exists in the system, thus providing an important safety feature in the operation of the probe 86 and latches 192, 193.

(46) The inlet/latch assembly 190 is further equipped with a spring-loaded nipple disk 196 adapted to provide an additional seal between the probe tip 93 and the inlet nozzle 194. The nipple disk 196 preferably includes an integral skirt, perhaps best seen in FIG. 16, having an arcuate cress-section for a purpose described more fully hereinbelow. A compression spring 200 is arranged axially behind the nipple disk 196 in order to bias the disk 196 toward the probe tip 93. The spring 200 also has the effect of expelling the probe tip 93 from the probe tip receptacle 197 when the latches 192, 193 are pulled apart, as described hereinbelow.

(47) The shape and dimensions of the elements of the various elements of the inlet/latch assembly 190 are selected to correspond to the shape and dimensions of the probe 86. However, as described previously, it may be desirable to develop a set of probes 86 having different dimensions or shape such that each differently sized or shaped probe 86 is intended for use only with tanks 12 of a particular capacity or pressure level. In this case, changes in the size or shape of the probe 86 are preferably coordinated with corresponding changes in the arrangement of the inlet/latch assembly 190. The dimensional variations in both probes 86 and inlet/latch assemblies 190 for different tank capacities are preferably significant enough such that a probe 86 intended for use with one capacity level cannot be used in an inlet/latch assembly 190 that is intended for use with a different capacity level. For example, referring back to the exemplary probes 86 described previously, the long, narrow probe 86 may be too long to be latched between the latches 192, 193, while the short, thicker probe 86 may be too wide to fit in the probe tip receptacle 197. Such a feature prevents a tank 12 of the wrong capacity from being used accidentally. This may prevent damage to the pressure reducer 24 or injury to a user, and may further prevent a user from believing that the tank 12 being utilized in his SCBA 10 has a higher capacity than it does.

(48) Although perhaps less desirable because of the increased connection time involved, it will be apparent that the use of probes of different dimensions, corresponding to different pressure vessel capacities, may also be applied to other types of probe connectors. For example, instead of a circumferential notch retained between two spring-loaded latches, a probe (not shown) could utilize a more conventional threaded male CGA fitting from which extends a probe tip similar to those described herein, and a probe tip receptacle could be provided with a corresponding threaded female CGA fitting. Probe tips of different lengths could then be configured to extend a greater or lesser depth into the probe tip receptacle, depending on the placement of the threaded fitting relative to the probe tip. Such a configuration would permit the use of the universal pressure reducer concept described herein, but would make it more difficult to connect or disconnect the probe from the inlet/latch assembly.

(49) Referring to FIG. 17, the electrical assembly 130 includes an electrical switch 212, a switch wire 139, a retainer 128 and a cable connector assembly 131. The electrical switch 212, which is preferably a normally-off switch actuated via a small spring-loaded button located on the bottom thereof, is disposed within a recess in the inlet/latch assembly 190 such that the button on the switch 212 protrudes downward through a small aperture into the cavity in which the inlet nozzle 194, nipple disk 196 and spring 200 are disposed. The switch 212 itself is protected from the external environment by a switch cover 214, whose underside is covered with rubber, arranged to cover the recess and attached via a plurality of screws 216. The switch wire is electrically connected from the switch 212, which is grounded to the inlet/latch assembly 190, through the pressure reduction assembly 110 to the cable connector assembly 131 and from there to the SCBA electronics system. The cable connector assembly 131 is secured to the pressure reduction assembly 110 via the retainer 128 and a screw (not shown) and sealed with a sealing compound.

(50) The button on the switch 212 is positioned relative to the cavity containing the nipple disk 196 such it lies at the periphery of the path of motion taken by the nipple disk 196 as it moves back and forth along the inlet nozzle 194. Thus, when the nipple disk 196 is forced rearward by the probe tip 93, the skirt of the disk 196 makes contact with the button on the switch 212, thereby depressing the button and actuating the switch 212. Preferably, the switch 212 and nipple disk 196 are arranged such that when the probe tip 93 is fully inserted in the probe tip receptacle 197, the nipple disk 196 remains in contact with the button on the switch 212, thus keeping the switch 212 actuated. A signal indicating that the probe tip 93 is engaged in the inlet/latch assembly 190 is thus transmitted along the switch wire 129, the cable connector assembly 131 and a corresponding cable (not shown) to the SCBA electronics system. When the probe tip 93 is removed from the receptacle 197, the spring 200 forces the disk 196 back forward, releasing the switch button and deactuating the switch 212.

(51) To use the quick connect valve and pressure reducer 20, the cylinder valve 22 is first installed on a breathing air tank 12 by threading the male fitting 41 into a corresponding female fitting on the tank 12 and charging (pressurizing) the tank 12. For convenience, a plurality of loaded tanks 12 may be stored with cylinder valves 22, each with an appropriately-sized probe 86, already installed. When a tank 12 is needed, the assembled tank 12 and cylinder valve 22 may be positioned such that the probe 86 is aligned with the probe tip receptacle 197, and then the probe tip 93 may be inserted therein. As the probe tip 93 encounters the latch shoulders 198, 199, the latches 192, 193 tend to be forced outward, thereby permitting the probe tip rim 94 to pass between the latch shoulders 198, 199. Additional resistance is encountered when the probe tip 93 encounters the nipple disk 196, which is biased by the compression spring 200. When force sufficient to overcome the spring 200 is applied to the probe 86, the probe tip 93 may move deeper into the inlet/latch assembly 190 until the tip rim 94 passes the latch shoulders 198, 199, thereby permitting the shoulders 198, 199 to snap into place in the circumferential notch 96. The latches 192, 193 are held in place in that position by the force of the latch springs 189, thus capturing and retaining the probe 86 within the probe tip receptacle 197.

(52) As long as the probe tip 86 is retained in the probe tip receptacle 197 as described above, the nipple disk 196 is maintained in continuous contact with the activation button on the switch 212 of the electrical assembly 130, thereby activating it. The switch 212 thus provides the SCBA electronics system with an electrical indication that a probe 86, and implicitly an assembled air tank 12 and cylinder valve 22, are installed in the pressure reducer 24. The SCBA electronics system, whether it may be a simple audible alarm generator or a more complex electronic device, may then operate accordingly.

(53) Once the pressure reducer 24 has been connected to the cylinder valve 22, the entire assembly is ready for operation. The tank 12, quick connect valve and pressure reducer 20 and other equipment are loaded on the user's back using a backpack, harness and the like, and the facepiece 16 is placed over the user's face such that it covers the user's mouth, nose or both, in conventional fashion. The hose assembly 18 is arranged to extend comfortably between the pressure reducer 24 and the facepiece 16, without interfering with the user's natural movements. The cylinder valve 58 may be opened by manually turning the handle 49 of the valve assembly 32 as described above, thereby permitting breathing gas to flow through the cylinder valve 22 and into the inlet nozzle 194 of the pressure reducer 24.

(54) Breathing gas passes through the pressure reducer 24 as follows. FIG. 18 is a front schematic view of the pressure reducer 24 of FIG. 13, showing the state of the pressure reducer 24 at initial activation. From the inlet nozzle 194 the breathing as enters the central supply conduit 112 where it may be distributed to the primary and secondary reducer modules 122, 123. At the same time, high pressure breathing gas travels through the latch in connector conduits 114, 115 to act on the ends of the latch lock pins 204. The force thus applied is sufficient to overcome the bias applied, in the opposite direction by respective springs 206, thereby forcing the opposite ends of the pins 204 into respective openings in the latches 192, 193. FIG. 19 is a front schematic view of the pressure reducer 24 of FIG. 13, showing the latch pins 204 being forced into openings in the latches 192, 193. The latches 192, 193 are thus locked in place whenever fluid pressure sufficient, to overcome the latch pin springs 206 exists in the central supply conduit 112, thereby preventing the probe 86 from becoming accidentally disengaged from the inlet/latch assembly 190 while high-pressure gas is flowing therethrough. The latch lock pins 204 and springs 206 are preferably calibrated such that any pressure above approximately 50 p.s.i.g. is sufficient to hold the latch lock pins 204 in place in the latches 192, 193.

(55) Further operation of the pressure reducer 24 may proceed according to conventional principles. FIG. 20 is a front schematic view of the pressure reducer 24 of FIG. 13, illustrating normal high pressure operation of the pressure reducer 24. Breathing air flows through the primary reducer module 122, which delivers a constant outlet pressure of nominal 100 p.s.i.g., at which pressure the breathing gas is subsequently communicated to the second stage regulator 14 for further pressure reduction. At the high pressures initially provided by the air tank 12, the pressure in the central supply conduit 112 is very high relative to the lower pressure on the outlet side of the primary reducer module 122, and even though the lower pressure is applied to a larger surface area of the transfer valve 160 than the area to which the high pressure is applied, the transfer valve 160 normally closes during high pressure operation. Breathing gas is thus supplied to the second stage regulator 14 via the primary reducer module 122, which opens and closes during inhalation and exhalation, respectively. The user may thus breathe normally via the SCBA 10 as he carries out his normal duties in the air-poor environments in which his work or other activities may take him.

(56) FIG. 21 is a front schematic view of the pressure reducer 24 of FIG. 13, illustrating normal low pressure operation of the pressure reducer 24. As more air is drawn out of the air tank 12, the pressure of the breathing air passing into the pressure reducer 24 diminishes. However, the pressure at the outlet of the primary reducer module 122 remains constant. Thus, because the surface area of the transfer valve 160 to which the low pressure breathing air is applied is much larger than that to which the diminished high pressure breathing air is applied, the transfer valve 160 is eventually forced open. From this point on the pressure differentials keep the primary reducer module 122 closed, while breathing air flows through the secondary reducer module 123 at a constant outlet pressure. The breathing gas is subsequently communicated to the second stage regulator 14 at this constant outlet pressure, which may be greater than the constant outlet pressure provided by the primary reducer module 122, as the secondary reducer module 123 opens and closes during inhalation and exhalation respectively.

(57) It is extremely desirable, and is in fact required by NIOSH and NFPA standards, for an alarm to be generated once pressure in the tank 12 drops below a predetermined level, which is preferably of the maximum capacity. This alarm may use the audible alarm generator described previously, or may be a separate alarm. Use of the transfer valve 160 to trigger such an alarm may be easily accomplished by designing the various components of the pressure reducer 24, and particularly the transfer valve assembly 124, such that the transfer valve 160 opens at the desired pressure level. This may be accomplished using a conventional balanced piston with cylinder pressure on one side and reducer pressure on the other. When pressure in the tank 12 depletes to capacity, the transfer valve 160 shifts allowing secondary reducer pressure to flow to an alarm mechanism.

(58) The SCBA 10 may be used as described above until either the tank 12 is empty (or at least empty enough that the pressure in the system drops below the predetermined nominal pressure) or until the cylinder valve 22 is closed by turning the handle 49 as described above, thereby shutting off the flow of air from the tank 12. Once the pressure in the central supply conduit 112 drops below the threshold level described above, the compression springs 206 on the latch lock pins 204 force the pins 204 away from the openings in the latches 192, 193, thereby unlocking them. The probe 86 may then be removed from the probe tip receptacle 197 by grasping the latches 192, 193 and pulling them apart with sufficient force to overcome the latch springs 189, thereby releasing the probe 86 from the latch shoulders 198, 199. Upon its release from the latches 192, 193, the probe 86 is then ejected by the force of the compression spring 200 acting on the nipple disk 196. Once the probe 86 has been withdrawn from the pressure reducer 24, the cylinder valve 22 and tank 12 may, if desired, be replaced by a full tank 12 and valve 22 so as to permit the user to continue working with a fresh supply of air, or the components may be cleaned, stored, repaired or the like.

(59) Alternatively, the tank 12 may be recharged without removing the probe 86 from the pressure reducer 24. This may be accomplished via the CGA assembly 30 by simply connecting a supply line having a corresponding female CGA fitting to the CGA assembly. The check valve opens, and air may be forced directly into the tank 12 with the valve assembly 32 in its closed positions. Alternatively, if the valve assembly 32 is adjusted to its open position, pressurized air may be forced directly through the probe 86 into the pressure reducer 24.

(60) FIG. 22 is a front view of an alternative pressure reducer 324, and FIGS. 23 and 24 are top and left side cross-sectional views of the pressure reducer 324 of FIG. 22, taken along lines 23-23 and 24-24, respectively. The primary components of the pressure reducer 324 include the pressure reduction assembly 310, a manifold assembly 380, an inlet/latch assembly 390 and an electrical assembly (not shown). This pressure reducer 324 is modified to accept probes 86 of different dimensions, representative of pressure vessels 12 of different capacities, and to automatically set a low-pressure alarm based on the capacity. The pressure reduction assembly 310 includes a housing 311, primary and secondary reducer modules 322, 323 (shown in FIG. 23), a transfer valve assembly 361 (shown in FIG. 24) and a selector valve assembly 332. The function of the reducer modules 322, 323 is similar to the previously-described primary and secondary reducer modules 122, 123 in that they are a balanced piston design. In addition, as shown, the reducer modules 322, 323 are built as independently replaceable modular units, which may be preferred for ease of manufacture and repair; however, this is not required.

(61) The transfer valve assembly 361 includes a collection of conventional components, including a valve 360 and a valve sleeve 362. As described below, the size and pressurization of the transfer valve assembly 361 determines when a predetermined alarm will sound to alert the wearer that only of the original capacity of the pressure vessel 12 remains. The valve 360 includes two sections or stages 364, 365, wherein the second valve stage 365 has a larger cross-section than that of the first valve stage 364 for a purpose made evident below.

(62) The manifold assembly 380, which is generally similar in design and function to the previously described manifold assembly 180, is attached to the pressure reduction assembly 310 with a plurality of screws 391. The inlet/latch assembly 390, which may be attached to the front of the pressure reduction assembly 310 via a plurality of screws 391, primarily includes a probe tip receptacle 397, a pair of latches 392, 393, an inlet nozzle 394 and a nipple disk 396. Each latch 392, 393 has a respective latch shoulder 398, 399. The function and design of inlet/latch assembly 390 is likewise generally similar to that of inlet/latch assembly 190.

(63) Referring to FIG. 24, the selector valve assembly 332 includes two pushrods 350, a selector valve plate 351, a selector valve 357 and a selector valve poppet 356. When the nipple disk 396 is displaced by a probe 86 that is designed specifically for a 2216 p.s.i.g, pressure vessel, the skirt of the disk 396 makes contact with the button on a switch 312, thereby depressing the button and actuating the switch 312, as described with regard to the first pressure reducer 24. When contact is made, a signal is sent from the switch 312 to the electronic system indicating that a probe 86 of a first set of predetermined dimensions (designated, for example, for specific use with a 2216 p.s.i.g. pressure vessel 12) has been inserted. In addition, however, the disk 396 contacts and displaces the pushrods 350, which in turn moves the selector valve plate 351. This allows the selector valve 357 and selector valve poppet 356 to unseat, thus pressurizing both a first main conduit 315 and a second, wider conduit 316. As a result, air pressure is supplied to both sections or stages 364, 365 of the transfer valve 360 via both conduits 315, 316, and the transfer valve 360 does not shift until pressure in the tank 12 drops to of the 2216 p.s.i.g. capacity. Once this shift occurs, secondary reducer pressure is allowed to flow to the alarm mechanism mentioned previously.

(64) On the other hand, when a probe 86 of a second set of predetermined dimensions (designated, for example, for specific use with a 4500 p.s.i.g. pressure vessel 12) has been inserted, it also contacts and displaces the nipple disk 396, as described previously, but the displacement is not as great as with the probe 86 of the first dimensions. As a result, the disk 396 does not make contact with the switch 312 or the pushrods 350. Because the pushrods 350 do not move, the selector valve assembly 332 remains seated. Thus, the second conduit 316 is vented to atmosphere, and only the first conduit 315 and one stage 364 of the transfer valve 360 are pressurized. Therefore, pressure is only supplied to the first transfer valve section 364, which shifts once pressure in the tank 12 drops to of the 4500 p.s.i.g. capacity, which in turn allows secondary reducer pressure to flow to the alarm mechanism mentioned previously. In other words, the selector valve assembly 332 ensures that the pressure reducer 324 automatically recognizes the tank capacity and causes the proper stage or stages of the transfer valve 360 to shift, thus triggering the alarm mechanism, at of the tank capacity regardless of whether the capacity is 2216 p.s.i.g. or 4500 p.s.i.g.

(65) In addition, because the disk 396 does not make contact with the switch 312, no signal is sent to the electronics system. The absence of a signal thus indicates to the electronic system that a probe 86 corresponding to a 4500 p.s.i.g. pressure vessel 12 has been inserter. Of course, the pressure levels may be varied, and the active signal may be used to represent a higher capacity and the absence of a signal the lower capacity. However, if it is desired that an active signal (rather than the absence of a signal) is always used to indicate the capacity level of the pressure vessel 12, it will be apparent to those of ordinal skill in the art that a second switch may be included, or the switch 312 may be replaced with a more complicated switch, in order to trigger such a signal. It will also be apparent that such a scheme may be further expanded to include more than two different pressure capacities, such as a 2216 p.s.i.g. capacity, a 3000 p.s.i.g. capacity, and a 4500 p.s.i.g. capacity. Finally, it will be apparent that the switch 312 may also be used to electronically trigger operation of the transfer valve assembly 361 through the inclusion of a small motor (not shown) or the like. Such an approach may either be used to assist pneumatic control of the transfer valve assembly 361 directly, or may be used to control operation of the selector valve assembly 332, thereby controlling the transfer valve assembly 361 indirectly. The mechanical approach, however, is preferred because of its ruggedness and simplicity of operation and service.

(66) Based on the foregoing information, it is readily understood by those persons skilled in the art that the present invention is susceptible of broad utility and application. Many embodiments and adaptations of the present invention other than those specifically described herein, as well as many variations, modifications, and equivalent arrangements, will be apparent from or reasonably suggested by the present invention and the foregoing descriptions thereof, without departing from the substance or scope of the present invention. Accordingly, while the present invention has been described herein in detail in relation to its preferred embodiment, it is to be understood that this disclosure is only illustrative and exemplary of the present invention and is made merely for the purpose of providing a full and enabling disclosure of the invention. The foregoing disclosure is not intended to be construed to limit the present invention or otherwise exclude any such other embodiments, adaptations, variations, modifications or equivalent arrangements; the present invention being limited only by the claims appended hereto and the equivalents thereof. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for the purpose of limitation.