US20190072452A1 - Valve manifold - Google Patents
Valve manifold Download PDFInfo
- Publication number
- US20190072452A1 US20190072452A1 US16/020,208 US201816020208A US2019072452A1 US 20190072452 A1 US20190072452 A1 US 20190072452A1 US 201816020208 A US201816020208 A US 201816020208A US 2019072452 A1 US2019072452 A1 US 2019072452A1
- Authority
- US
- United States
- Prior art keywords
- valve
- exhaust
- pilot valve
- recited
- pressure
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000012360 testing method Methods 0.000 claims description 63
- 238000002955 isolation Methods 0.000 claims description 35
- 238000012544 monitoring process Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 claims 13
- 230000003213 activating effect Effects 0.000 claims 1
- 230000001052 transient effect Effects 0.000 claims 1
- 239000012530 fluid Substances 0.000 abstract description 16
- 238000001514 detection method Methods 0.000 description 13
- 230000001276 controlling effect Effects 0.000 description 6
- 238000007789 sealing Methods 0.000 description 6
- 238000013022 venting Methods 0.000 description 4
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 238000004088 simulation Methods 0.000 description 3
- 230000001143 conditioned effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012163 sequencing technique Methods 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
- 238000012956 testing procedure Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/28—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds
- G01M3/2853—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for pipe joints or seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
- F16K1/12—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with streamlined valve member around which the fluid flows when the valve is opened
- F16K1/126—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with streamlined valve member around which the fluid flows when the valve is opened actuated by fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K27/00—Construction of housing; Use of materials therefor
- F16K27/003—Housing formed from a plurality of the same valve elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
- F16K31/122—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a piston
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K31/00—Actuating devices; Operating means; Releasing devices
- F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
- F16K31/122—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a piston
- F16K31/1225—Actuating devices; Operating means; Releasing devices actuated by fluid the fluid acting on a piston with a plurality of pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K37/00—Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
- F16K37/0066—Hydraulic or pneumatic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K37/00—Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
- F16K37/0075—For recording or indicating the functioning of a valve in combination with test equipment
- F16K37/0091—For recording or indicating the functioning of a valve in combination with test equipment by measuring fluid parameters
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/28—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds
- G01M3/2876—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for valves
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/32—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
- G01M3/3236—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators by monitoring the interior space of the containers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87169—Supply and exhaust
- Y10T137/87193—Pilot-actuated
- Y10T137/87201—Common to plural valve motor chambers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87169—Supply and exhaust
- Y10T137/87193—Pilot-actuated
- Y10T137/87209—Electric
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87169—Supply and exhaust
- Y10T137/87217—Motor
- Y10T137/87225—Fluid motor
Definitions
- the present invention relates to valves for controlling fluid flow, and, in particular, a control valve assembly having valves integrated with a valve manifold for compactly controlling fluid coupled devices.
- leak detection systems are an assembly of separate components housed in portable test units. Using a myriad of valves and pneumatic lines a component to be tested is attached to the test unit and independent valves are sequenced to route pressurized fluid, customarily air, to the component, which is then isolated. The leakage rate at the component is then measured and a part accepted or rejected based thereon.
- the multiple valves and lines may be integrated into a portable test stand for on-site testing. Nonetheless, the pneumatic system is expansive and cumbersome, with each element posing the potential for associated malfunction and leaks. Further, automation of a testing protocol is difficult because of the independent relationship of the components. Where varying test pressures are required for other components, the system must be retrofitted for each such use.
- the leak detection apparatus as disclosed in U.S. Pat. No. 5,898,105 to Owens references a manually operated systems wherein the testing procedures is controlled by plural manual valves and associated conduit occasioning the aforementioned problems and limitations.
- the hydrostatic testing apparatus as disclosed in U.S. Pat. No. 3,577,768 to Aprill provides a portable unit comprised of a plurality of independent valves and associated lines for conducting testing on equipment and fluid lines. The valves are manually sequenced for isolating test components from a single pressure source.
- U.S. Pat. No. 5,440,918 to Oster also discloses a testing apparatus wherein a plurality of conventional valving and measuring components are individually fluidly connected.
- U.S. Pat. No. 5,540,083 to Sato et al. discloses remotely controlled electromagnetically operated valves for measuring leakage in vessels and parts. Separate valve and hydraulic lines are required.
- the leak detector includes a valve block having internal porting selectively controlled by four identical and unique pneumatic poppet valves for pressurizing the test part, isolating the test part for determining leakage rates with pressure and flow sensors communicating with the porting, and exhausting the test line upon completion of the leakage test.
- the poppet valves engage valve seats incorporated within the porting.
- the poppet valves are actuated by pilot valve pressure acting on a pilot piston to effect closure of the valve.
- the sensors interface with a microprocessor for comparing measurements with the test protocol and indicate pass or fail performance. Upon removal of the pilot valve pressure, the resident pressure in the porting shifts the valve to the open position.
- the leak detector includes plural inlets for accommodating variable pressure protocols. The leak detector thus eliminates the need for external fluid connections and conduits between the various detector components, eliminates the need for two-way valving actuation, and provides for connection with external test units with a single, easy to install, pneumatic line.
- the poppet valves may be disposed in sets in a valve manifold to simulate conventional valve functionalities with a plurality of fluidic devices.
- a pair of the pitot valves operates in controlled phased opposition to apply and vent pressure to a one way actuator.
- a second set of oppositely configured valve are used for conventional operation of dual controlled devices such as two way actuators.
- FIG. 1 is a perspective view of a leak detection valve assembly and control module in accordance with an embodiment of the invention
- FIG. 2 is a schematic drawing of a leak detection system incorporating the valve assembly of FIG. 1 ;
- FIG. 3 is a top view of the valve assembly
- FIG. 4 is a front view of the valve assembly
- FIG. 5 is a vertical cross sectional view taken along line 5 - 5 in FIG. 3 ;
- FIG. 6 is a vertical cross sectional view taken along line 6 - 6 in FIG. 4 ;
- FIG. 7 is a horizontal cross sectional view taken along line 7 - 7 in FIG. 4 ;
- FIG. 8 is a horizontal cross sectional view taken along line 8 - 8 in FIG. 4 ;
- FIG. 9 is a fragmentary cross sectional view of a unique poppet valve assembly
- FIG. 10 is a schematic diagram of the leak detection system
- FIG. 11 is a truth table for the leak detection system
- FIG. 12 is a schematic diagram for the control system for the leak detection system
- FIG. 13 is a perspective view of another embodiment of a valve assembly for a leak detection system
- FIG. 14 is a perspective view of a valve manifold assembly in accordance with another embodiment of the invention.
- FIG. 15 is a top view of the valve manifold assembly shown in FIG. 14 ;
- FIG. 16 is a front view of the valve manifold assembly shown in FIG. 14 ;
- FIG. 17 is a left end view of the valve manifold assembly shown in FIG. 14 ;
- FIG. 18 is a cross sectional view of the valve manifold assembly shown in FIG. 14 , with the control module removed and including cross sectional view of valve sets taken along lines A-A and B-B in FIG. 16 and a schematic view of the control system for the valve sets for three way and four way valve functionality;
- FIG. 19 is a fragmentary cross sectional view taken along line 19 - 19 in FIG. 18 ;
- FIG. 20 is a cross sectional view of a valve manifold according another embodiment of the invention illustrating a two way valve functionality.
- FIGS. 1 and 2 illustrate a leak detection system 10 for determining the pressure integrity of components when subjected to pressure conditions during a test period.
- the leak detection system 10 comprises a valve assembly 12 and a control module 14 operatively coupled with a flow sensor 16 and pressure sensor 18 .
- the leak detector 10 is operative for testing the fluid integrity of test parts to determine is leakage standards are being achieved.
- valve assembly 12 is fluidly connected with a low pressure source 20 along line 22 , a high pressure source 24 along line 26 , a test unit 28 for testing such parts along line 30 , and an exhaust 32 along line 34 .
- Supplemental valves may be disposed in the lines for controlling flow therethrough.
- the control module 14 comprises a pilot valve assembly 36 including pilot valves 40 , 42 , 44 , and 46 fluidly connected with a high pressure valve unit 50 , a low pressure valve unit 52 , an exhaust valve unit 54 and an isolation valve unit 56 along lines 60 , 62 , 64 and 66 , respectively.
- the pressure sensor 18 is coupled with the isolation valve unit 56 by line 68 .
- the flow sensor 16 is connected with the valve units at manifold line 70 and with test part line 30 along line 72 .
- the pilot valves are connected to pilot pressure 74 by manifold line 76 .
- the lines and attendant fittings will vary in accordance with the parts undergoing testing and the test conditions.
- the valve assembly 12 comprises a valve block 40 housing via ports to be described below a low pressure valve unit 80 , a high pressure valve unit 82 , an exhaust valve unit 84 and an isolation valve unit 86 .
- the low pressure valve unit 80 is fluidly connected with line 28 and low pressure source 20 by a low pressure inlet port 90 intersecting with a vertical cross port 92 .
- the high pressure valve unit 82 is fluidly connected with line 26 and high pressure source 24 by a high pressure inlet port 94 intersecting with a vertical cross port 96 .
- the isolation valve unit 86 is fluidly connected with the line 30 by the isolation port 98 and vertical port 99 .
- the exhaust valve unit 84 is fluidly connected with line 32 by exhaust port 100 .
- the ports 90 , 94 and 100 are disposed on the front face 102 of the valve block 12 .
- the isolation port 98 is disposed on the rear face 104 of the valve block 12 .
- the ports 100 and 98 are located laterally in a central vertical plane.
- the ports 90 and 94 are symmetrically disposed on opposite sides of the exhaust port 100 and therebelow.
- the ports 100 , 94 and 90 lie in a common horizontal plane.
- Each of the ports is provided with an outer threaded bore for connection to the associated lines with an appropriate fitting for the fluid application.
- valve unit 110 including a poppet 112 having a valve stem 113 supported by sealing disk 114 for reciprocation between a raised vent position as illustrated and a lowered sealed position in counterbore 115 .
- the poppet 112 includes a cylindrical valve body 116 carrying O-ring 117 that engages the annular valve seat 118 of counterbore 115 formed coaxially with a vertical port 120 .
- the outer rim of the sealing disk 114 is supported at the base of a secondary counterbore vertically above bore 115 .
- the secondary counterbore outwardly terminates at an internally threaded end.
- a vent cap 124 includes a cylindrical sleeve 125 threadedly received in the threaded bore and a circular base 126 having a threaded center hole 128 .
- An actuating piston 129 including O-ring 130 is axially slidably carried at the interior surface of the sleeve of the vent cap 124 for movement between a raised position engaging the base 128 and a lowered position engaging the top of the valve stem 113 for moving the poppet 112 to the sealed condition.
- Angularly disposed vent holes 131 are formed in the sleeve 125 for venting the piston.
- An air line connected with the pilot pressure line is connected at the center hole 128 for connection with the pilot pressure control system.
- a counterbore 138 is formed in the bottom surface of the valve block 40 coaxially therewith.
- a circular sealing blank 140 is retained at a step in the counterbore 138 by a split retaining ring 142 retained in a corresponding annular groove thus defining a pressure chamber 144 .
- a C-shaped distribution channel or port 150 extends from the chamber 144 upwardly and intersects the counterbores 115 of valve units 110 .
- a pair of vertical ports 160 communicate upstream of the isolation valve unit 84 for connecting one line of the flow sensor 16 and the pressure sensor 18 .
- a pair of vertical ports 162 communicates on the other side of the isolation valve units 84 with the distribution port 150 . Accordingly, the flow sensor 16 in a conventional manner measures pressure transients on the part under leakage test while the pressure sensor 18 measures pressure conditions on both sides of the isolation valve.
- the valve unit is operationally connected to an independent test unit whereat parts to be leak tested may be deployed.
- the test protocol may specify a high pressure test for a defined test period or a low pressure test for a defined test period. Test parts are deemed successful if the leakage under pressure as determined by the flow sensor 16 is below a predetermined threshold.
- the control system 14 is effective for establishing the appropriate protocol.
- the control system 14 comprises the pilot valve system 250 , a microprocessor 254 coupled with a control panel 255 for defining and conducting the test protocol, test result indicator lights 256 a display screen 257 , for denoting passing or failing of the test connected to a suitable power supply 258 .
- the microprocessor 254 contains the protocols for the various parts, preferably programmed through an external computer port 260 .
- the desired protocol is accessed at control panel 255 through menu button 264 , start button 266 and scroll buttons 268 .
- the operation of the leak detector is illustrated in the truth table of FIG. 11 and taken in conjunction with the schematic of FIG. 2 .
- the control system initialized and the test protocol selected. Thereafter, the test is initiated by actuating the start button 266 .
- the high and low pressure lines are pressurized with the accompanying pilot valves 40 , 42 in the normally open positions with the solenoids deenergized. This applies pilot pressure to the associated poppets to close and seal the high pressure and low pressure valve units 50 , 52 .
- the normally closed exhaust pilot is deenergized and the exhaust valve 54 is in the open position.
- the normally closed isolation pilot is deenergized and the isolation valve unit 56 is in the open position.
- the high pressure pilot 40 is energized, venting the high pressure poppet whereby inlet high pressure air raises the high pressure valve unit 50 to the open position.
- the exhaust solenoid is energized admitting pilot pressure to the exhaust poppet piston chamber and shifting the exhaust valve unit 54 to the closed position and air flowing past the high pressure poppet pressurizes the exhaust chamber 144 through the distribution channel and past the isolation valve unit 56 to pressurize the test part with high pressure air.
- the isolation pilot is energized applying pilot pressure to the isolation piston chamber and closing the isolation poppet.
- the flow sensor 16 monitors pressure transients and through the microprocessor interface denotes pass or fail conditions at the indicator lights.
- the isolation pilot solenoid Upon completion of the test, the isolation pilot solenoid is deenergized pressurizing the high pressure piston and sealing the high pressure valve seat, thereby ceasing inlet flow. Concurrently, the isolation and exhaust pilot solenoids are deenergized allowing exhaust chamber and part pressure to shift the exhaust and isolation valves to the open position for completion of the test. In the event of excessive pressure lost at the test part, a light biasing spring may be provided at the isolation poppet to ensure movement to the open position.
- the exhaust poppet is closed and the low pressure valving sequenced in similar fashion to the high pressure test detailed above. More particularly, a part to be tested in mounted in the test fixture, the control system initialized and the test protocol selected. Thereafter, the test is initiated by actuating the start button 266 .
- the high and low pressure lines are pressurized with the accompanying pilot valves in the normally open positions with the solenoids deenergized. This applies pilot pressure to the associated poppets to close and seal the later.
- the normally closed exhaust pilot is deenergized and the exhaust poppet is in the open position.
- the normally closed isolation pilot is denergized and the isolation poppet is in the open position.
- the low pressure pilot 42 is energized, venting the low pressure valve whereby inlet low pressure air raises the low pressure valve unit 52 to the open position.
- the exhaust pilot is energized admitting pilot pressure to the exhaust poppet piston chamber and shifting the exhaust valve unit 54 to the closed position and air flowing past the low pressure poppet pressurizes the exhaust chamber through the distribution channel 150 and past the isolation poppet to pressurize the test part with high pressure air.
- the isolation pilot solenoid is energized applying pilot pressure to the isolation piston chamber and closing the isolation poppet.
- the flow sensor monitors pressure transients and through the microprocessor interface denotes pass or fail conditions at the indicator.
- the isolation pilot Upon completion of the test, the isolation pilot is deenergized pressurizing the low pressure piston and sealing the low pressure valve seat, thereby ceasing inlet flow. Concurrently, the isolation and exhaust pilot solenoids are deenergized allow exhaust chamber and part pressure to shift the exhaust and isolation poppets to the open position for completion of the test.
- the valve 280 comprises an extruded metallic valve body 282 having four valve assemblies 284 , as described above.
- the valve assemblies are controlled by solenoids 286 carried on a top horizontal surface.
- the valve body 280 has an isolation port 288 in the illustrated rear wall thereof, and high and low pressure ports, and an exhaust port in the front wall thereof, which are not shown and function as above described.
- the control lines for the valve assemblies 284 are routed through a distribution bracket 290 .
- the interior pressure sensors are coupled at pin connector 292 on the top surface of the valve body 280 for operative connection to associated instrumentation.
- the valving is incorporated into a control valve manifold 300 .
- the manifold 300 includes an extruded lower valve body 302 carrying on a top surface a plurality of longitudinally spaced control modules 304 for operatively controlling conventional fluidic devices, not shown, coupled at a longitudinal series of associated outlet ports 306 exiting at a longitudinal side wall of the valve body.
- An inlet port 310 and an exhaust port 312 extend longitudinally through the valve body 302 in parallel spaced relationship for interconnection with the valving as described in greater detail below.
- the ports 310 and 312 terminate at internally threaded ends. At the remote end, the ports are suitably sealed with a stop member, such as a threaded plug (not shown), or coupled with a succeeding manifold.
- the inlet port 310 is coupled with a supply line for supplying inlet fluid under pressure for control by the valving and controlled operation of the associated fluidic devices.
- the exhaust port 312 is coupled with an exhaust line for routing to an appropriate location the exhaust fluid.
- a pair of upwardly opening laterally spaced longitudinal channels 320 are formed in the top surface of the valve body 302 .
- Solenoids 322 are carried in the channels 320 and operatively associated with the control modules 304 for controlling pilot pressure to the valving at pilot lines 324 .
- the modules 304 are connected to a suitable power source via multiple-pin socket connector 326 carried on the front lateral side wall of the valve body 302 .
- the valve modules 304 control the flow between the ports 310 , 312 and the operative outlet ports 306 of the manifold 300 . If certain of the ports are not required for an application, the outlet ports may be plugged or capped, and additionally the associated control module deleted. Any ports associated with the inactive outlet ports are also deleted or plugged.
- valve body may be tailored to the devices to be controlled and may be coupled in series or parallel with other valving manifolds.
- the manifold in controlled formats may be advantageously employed to replicate the functionality of various conventional valving configurations, such as two-way, three-way, four-way, five-way valves. In such configurations, the manifold operates with lower control pressures within a substantially smaller envelope.
- each control module 304 is associated with a pair of laterally spaced valves 340 , 342 in Valve A and valves 344 and 346 in Valve B.
- the valves are operatively disposed in the valve body 302 as referenced in FIG. 9 above.
- the inlet valves 340 , 344 are disposed in upwardly opening vertical bores in the valve body normal to the inlet port 310 .
- Each valve includes a slidably stem supported inlet valve member 360 downwardly moveable by a floating piston 362 from a raised position communicating with the inlet port 310 and a closed position engaging an annular valve seat downstream of the inlet port.
- the exhaust valves 342 , 346 are disposed in upwardly opening vertical bodes in the valve body normal to the exhaust port 312 .
- Each valve includes a slidably stem supported outlet valve member 370 downwardly moveable by a floating piston 372 from a lowered position engaging an annular valve seat upstream of the exhaust port 312 and a raised position communicating with the exhaust port.
- An exhaust plenum chamber 380 is formed in the valve body 302 below the exhaust valve seat and in the open position communicates with the exhaust port.
- the exhaust plenum chamber 380 is sealed by a circular cover member 382 and sealed as described with reference to the prior embodiment.
- a cross passage 384 is formed at the outer periphery of the exhaust plenum chamber and established a fluid path extending serially from the outlet port 306 to the cross passage to the exhaust plenum chamber 380 to the exhaust port.
- Each piston is carried in a valve cap threadedly connected in a bore extending from the top surface of the valve body coaxial with the exhaust valve seat.
- the valve caps are fluidly connected with branch pilot lines 323 above the piston.
- the exhaust valve 370 is connected at the branch pilot line with a normally open solenoid valve 400 connected with the main pilot line 402 .
- the inlet valve 360 is connected at the branch pilot line with a normally closed solenoid valve 404 connected with the main pilot line.
- the outlet port 306 is formed in the side of the valve body 302 and intersects the inlet valve bore above the inlet valve seat.
- the device port is fluidly connected by line to one side of a single acting actuator 410 , including return spring biased piston 411 , by lines 412 and 414 .
- the inlet valve member 360 is moved upwardly to an open position by inlet pressure on the lower surface thereby shifting the piston to a raised position, establishing a fluid path through outlet port 306 and lines 412 , 414 and extending actuator piston 411 .
- the outlet valve member is shifted by the piston to the closed position sealing flow to the outlet port.
- the solenoid valves are reversed, whereby the inlet valve member 360 is closed, the outlet pilot pressure removed allowing pressure conditions in the plenum 380 to move the exhaust valve member 370 to the open position and venting the actuator to the exhaust port 312 thereby retracting the actuator piston under the spring biasing.
- Valve B is operatively coupled with Valve A.
- Valve B has a normally open inlet solenoid valve 420 and a normally closed exhaust solenoid valve 422 .
- Valve A is coupled with one end of a double acting actuator 430 , including piston 431 , by lines 412 , 432 .
- Valve B is couple at the outlet port with the other end of the actuator 430 by line 434 .
- Valve A In operation, the extension of actuator is controlled by Valve A as above described, and Valve B is in the exhaust mode.
- Valve B To retract the actuator piston 431 , Valve A is conditioned for exhaust and Valve B is conditioned for pressure, thereby shifting the piston 431 to the retracted position.
- a valve 500 includes a valve body 502 carrying a valve assembly 504 as described above.
- the inlet valve member 506 is moved by piston 508 under pilot conditions controlled by normally open solenoid valve 510 between a lower closed position engaging the inlet valve seat and the illustrated raised open position.
- the valve permits fluid flow from supply line 520 to inlet port 522 past valve member 506 to outlet port 524 to a pressure dependent device 526 .
- the solenoid valve 510 the pilot pressure is applied to the piston to closed the valve member and block flow therethrough.
- the inlet pressure shifts the valve member to the open condition.
- valve members may be independently controlled and sequenced to a desired actuation schedule.
- the normal crossover time between valve positions may be eliminated by concurrent actuation of the solenoids. Should staged actuation be desired, time sequencing may be used.
- the valve ports may be integrated with other flow control.
- Each such simulation provides the compact size afforded by the valves directly place in the manifold bodies, and the low pilot pressures required by the valves, as well as the valve opening pressures afforded by resident pressurization.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fluid-Driven Valves (AREA)
- Examining Or Testing Airtightness (AREA)
- Valve Housings (AREA)
Abstract
A valve manifold includes a valve body carrying pairs of laterally spaced piston actuated valves controlled by control modules operative to selectively pressurize and exhaust an outlet port connected to a fluid device and configured in groupings permitting varying valve functionalities.
Description
- This is a continuation of U.S. patent application Ser. No. 15/226,380 filed on Aug. 2, 2016, which will issue as U.S. Pat. No. 10,018,529 and will grant on Jul. 10, 2018, which is a continuation of U.S. application Ser. No. 14/257,193 filed on Apr. 21, 2014, which is now U.S. Pat. No. 9,404,603 granted on Aug. 2, 2016, which is a continuation of U.S. application Ser. No. 13/425,820 filed on Mar. 21, 2012, now U.S. Pat. No. 8,714,196 granted on May 6, 2014, which is a continuation of U.S. application Ser. No. 12/131,092 filed on Jun. 1, 2008, now U.S. Pat. No. 8,177,188 granted on May 15, 2012, which is a divisional of U.S. application Ser. No. 10/223,236 filed on Aug. 19, 2002, now U.S. Pat. No. 7,490,625 granted on Feb. 17, 2009, which is a continuation-in-part of U.S. application Ser. No. 09/840,688, filed on Apr. 23, 2001, now U.S. Pat. No. 6,435,010 granted on Aug. 20, 2002.
- The present invention relates to valves for controlling fluid flow, and, in particular, a control valve assembly having valves integrated with a valve manifold for compactly controlling fluid coupled devices.
- Manufacturers of hydraulic, pneumatic, and containment equipment customarily test the fluid integrity of their components to ensure safe operation in the field. Standards are generally prescribed for leakage rates at test pressures and times correlated to the desired component specifications.
- Currently, leak detection systems are an assembly of separate components housed in portable test units. Using a myriad of valves and pneumatic lines a component to be tested is attached to the test unit and independent valves are sequenced to route pressurized fluid, customarily air, to the component, which is then isolated. The leakage rate at the component is then measured and a part accepted or rejected based thereon. The multiple valves and lines may be integrated into a portable test stand for on-site testing. Nonetheless, the pneumatic system is expansive and cumbersome, with each element posing the potential for associated malfunction and leaks. Further, automation of a testing protocol is difficult because of the independent relationship of the components. Where varying test pressures are required for other components, the system must be retrofitted for each such use.
- For example, the leak detection apparatus as disclosed in U.S. Pat. No. 5,898,105 to Owens references a manually operated systems wherein the testing procedures is controlled by plural manual valves and associated conduit occasioning the aforementioned problems and limitations.
- Similarly, the hydrostatic testing apparatus as disclosed in U.S. Pat. No. 3,577,768 to Aprill provides a portable unit comprised of a plurality of independent valves and associated lines for conducting testing on equipment and fluid lines. The valves are manually sequenced for isolating test components from a single pressure source. U.S. Pat. No. 5,440,918 to Oster also discloses a testing apparatus wherein a plurality of conventional valving and measuring components are individually fluidly connected.
- Remotely controlled leak detection systems, such as disclosed in U.S. Pat. No. 5,557,965 to Fiechtner, have been proposed for monitoring underground liquid supplies. Such systems, however, also rely on an assembly of separate lines and valves. A similar system is disclosed in U.S. Pat. No. 5,046,519 to Stenstrom et al. U.S. Pat. No. 5,072,621 to Hasselmann.
- U.S. Pat. No. 5,540,083 to Sato et al. discloses remotely controlled electromagnetically operated valves for measuring leakage in vessels and parts. Separate valve and hydraulic lines are required.
- In an effort to overcome the foregoing limitations, it would be desirable to provide a portable leakage detection system for testing the fluid integrity of fluid systems and components that include integrated valving and porting within a compact envelope for automatically controlling a variable testing protocol. The leak detector includes a valve block having internal porting selectively controlled by four identical and unique pneumatic poppet valves for pressurizing the test part, isolating the test part for determining leakage rates with pressure and flow sensors communicating with the porting, and exhausting the test line upon completion of the leakage test. The poppet valves engage valve seats incorporated within the porting. The poppet valves are actuated by pilot valve pressure acting on a pilot piston to effect closure of the valve. The sensors interface with a microprocessor for comparing measurements with the test protocol and indicate pass or fail performance. Upon removal of the pilot valve pressure, the resident pressure in the porting shifts the valve to the open position. The leak detector includes plural inlets for accommodating variable pressure protocols. The leak detector thus eliminates the need for external fluid connections and conduits between the various detector components, eliminates the need for two-way valving actuation, and provides for connection with external test units with a single, easy to install, pneumatic line.
- In another aspect of the invention, the poppet valves may be disposed in sets in a valve manifold to simulate conventional valve functionalities with a plurality of fluidic devices. For three way valve functionality, a pair of the pitot valves operates in controlled phased opposition to apply and vent pressure to a one way actuator. For four way valve functionality, a second set of oppositely configured valve are used for conventional operation of dual controlled devices such as two way actuators.
- The above and other objects and advantages of the present invention will become apparent upon reading the following detailed description taken in conjunction with the accompanying drawings in which:
-
FIG. 1 is a perspective view of a leak detection valve assembly and control module in accordance with an embodiment of the invention; -
FIG. 2 is a schematic drawing of a leak detection system incorporating the valve assembly ofFIG. 1 ; -
FIG. 3 is a top view of the valve assembly; -
FIG. 4 is a front view of the valve assembly; -
FIG. 5 is a vertical cross sectional view taken along line 5-5 inFIG. 3 ; -
FIG. 6 is a vertical cross sectional view taken along line 6-6 inFIG. 4 ; -
FIG. 7 is a horizontal cross sectional view taken along line 7-7 inFIG. 4 ; -
FIG. 8 is a horizontal cross sectional view taken along line 8-8 inFIG. 4 ; -
FIG. 9 is a fragmentary cross sectional view of a unique poppet valve assembly; -
FIG. 10 is a schematic diagram of the leak detection system; -
FIG. 11 is a truth table for the leak detection system; -
FIG. 12 is a schematic diagram for the control system for the leak detection system; -
FIG. 13 is a perspective view of another embodiment of a valve assembly for a leak detection system; -
FIG. 14 is a perspective view of a valve manifold assembly in accordance with another embodiment of the invention; -
FIG. 15 is a top view of the valve manifold assembly shown inFIG. 14 ; -
FIG. 16 is a front view of the valve manifold assembly shown inFIG. 14 ; -
FIG. 17 is a left end view of the valve manifold assembly shown inFIG. 14 ; -
FIG. 18 is a cross sectional view of the valve manifold assembly shown inFIG. 14 , with the control module removed and including cross sectional view of valve sets taken along lines A-A and B-B inFIG. 16 and a schematic view of the control system for the valve sets for three way and four way valve functionality; -
FIG. 19 is a fragmentary cross sectional view taken along line 19-19 inFIG. 18 ; and -
FIG. 20 is a cross sectional view of a valve manifold according another embodiment of the invention illustrating a two way valve functionality. - Referring to the drawings for the purpose of describing the preferred embodiment and not for limiting same,
FIGS. 1 and 2 illustrate aleak detection system 10 for determining the pressure integrity of components when subjected to pressure conditions during a test period. Theleak detection system 10 comprises avalve assembly 12 and acontrol module 14 operatively coupled with aflow sensor 16 andpressure sensor 18. As hereinafter described in detail, theleak detector 10 is operative for testing the fluid integrity of test parts to determine is leakage standards are being achieved. - Referring additionally to
FIG. 10 , thevalve assembly 12 is fluidly connected with alow pressure source 20 alongline 22, ahigh pressure source 24 alongline 26, atest unit 28 for testing such parts alongline 30, and anexhaust 32 alongline 34. Supplemental valves may be disposed in the lines for controlling flow therethrough. - The
control module 14 comprises apilot valve assembly 36 includingpilot valves pressure valve unit 50, a lowpressure valve unit 52, anexhaust valve unit 54 and anisolation valve unit 56 alonglines pressure sensor 18 is coupled with theisolation valve unit 56 byline 68. Theflow sensor 16 is connected with the valve units atmanifold line 70 and withtest part line 30 alongline 72. The pilot valves are connected to pilotpressure 74 bymanifold line 76. The lines and attendant fittings will vary in accordance with the parts undergoing testing and the test conditions. - Referring to
FIGS. 3 through 8 , thevalve assembly 12 comprises avalve block 40 housing via ports to be described below a lowpressure valve unit 80, a highpressure valve unit 82, anexhaust valve unit 84 and anisolation valve unit 86. - As shown in
FIGS. 5 and 8 , the lowpressure valve unit 80 is fluidly connected withline 28 andlow pressure source 20 by a lowpressure inlet port 90 intersecting with avertical cross port 92. The highpressure valve unit 82 is fluidly connected withline 26 andhigh pressure source 24 by a highpressure inlet port 94 intersecting with avertical cross port 96. As shown inFIG. 6 , theisolation valve unit 86 is fluidly connected with theline 30 by theisolation port 98 andvertical port 99. Theexhaust valve unit 84 is fluidly connected withline 32 byexhaust port 100. As shown inFIG. 4 , theports front face 102 of thevalve block 12. Theisolation port 98 is disposed on therear face 104 of thevalve block 12. Theports ports exhaust port 100 and therebelow. Theports - All of the valve units have a common architecture as representatively shown in
FIG. 9 . Therein, avalve unit 110 including apoppet 112 having avalve stem 113 supported by sealingdisk 114 for reciprocation between a raised vent position as illustrated and a lowered sealed position incounterbore 115. Thepoppet 112 includes acylindrical valve body 116 carrying O-ring 117 that engages theannular valve seat 118 ofcounterbore 115 formed coaxially with avertical port 120. The outer rim of thesealing disk 114 is supported at the base of a secondary counterbore vertically abovebore 115. The secondary counterbore outwardly terminates at an internally threaded end. Avent cap 124 includes acylindrical sleeve 125 threadedly received in the threaded bore and acircular base 126 having a threadedcenter hole 128. Anactuating piston 129 including O-ring 130 is axially slidably carried at the interior surface of the sleeve of thevent cap 124 for movement between a raised position engaging thebase 128 and a lowered position engaging the top of thevalve stem 113 for moving thepoppet 112 to the sealed condition. Angularly disposed vent holes 131 are formed in thesleeve 125 for venting the piston. An air line connected with the pilot pressure line is connected at thecenter hole 128 for connection with the pilot pressure control system. - In typical operation, when pilot pressure is applied in the chamber above the
piston 129, thepiston 129 is forced downwardly thereby shifting thepoppet 112 to the sealed position. When the pilot pressure is removed and theport 120 is pressurized, thepoppet 112 and thepiston 129 are driven to the raised, open position. Assist springs may be deployed, particularly in the isolation valve, for providing additional biasing to the open condition. - As shown in
FIGS. 5 through 8 , with respect to theexhaust port 100 andvalve unit 84, acounterbore 138 is formed in the bottom surface of thevalve block 40 coaxially therewith. A circular sealing blank 140 is retained at a step in thecounterbore 138 by asplit retaining ring 142 retained in a corresponding annular groove thus defining apressure chamber 144. A C-shaped distribution channel orport 150 extends from thechamber 144 upwardly and intersects thecounterbores 115 ofvalve units 110. - Accordingly, when either of the pressure valve units is pressurized from its source and the pilot control to the piston is interrupted, the air flow in the
ports distribution port 150 andchamber 144 resulting in pressure communication therebetween. Referring toFIGS. 3, 7 and 8 , a pair ofvertical ports 160 communicate upstream of theisolation valve unit 84 for connecting one line of theflow sensor 16 and thepressure sensor 18. A pair ofvertical ports 162 communicates on the other side of theisolation valve units 84 with thedistribution port 150. Accordingly, theflow sensor 16 in a conventional manner measures pressure transients on the part under leakage test while thepressure sensor 18 measures pressure conditions on both sides of the isolation valve. - The valve unit is operationally connected to an independent test unit whereat parts to be leak tested may be deployed. The test protocol may specify a high pressure test for a defined test period or a low pressure test for a defined test period. Test parts are deemed successful if the leakage under pressure as determined by the
flow sensor 16 is below a predetermined threshold. Thecontrol system 14 is effective for establishing the appropriate protocol. - Referring to
FIG. 12 , thecontrol system 14 comprises thepilot valve system 250, amicroprocessor 254 coupled with acontrol panel 255 for defining and conducting the test protocol, test result indicator lights 256 adisplay screen 257, for denoting passing or failing of the test connected to asuitable power supply 258. Themicroprocessor 254 contains the protocols for the various parts, preferably programmed through anexternal computer port 260. The desired protocol is accessed atcontrol panel 255 throughmenu button 264,start button 266 andscroll buttons 268. - The operation of the leak detector is illustrated in the truth table of
FIG. 11 and taken in conjunction with the schematic ofFIG. 2 . - A part to be tested in mounted in the test fixture, the control system initialized and the test protocol selected. Thereafter, the test is initiated by actuating the
start button 266. As a first condition, the high and low pressure lines are pressurized with the accompanyingpilot valves 40, 42 in the normally open positions with the solenoids deenergized. This applies pilot pressure to the associated poppets to close and seal the high pressure and lowpressure valve units exhaust valve 54 is in the open position. The normally closed isolation pilot is deenergized and theisolation valve unit 56 is in the open position. - Thereafter the
high pressure pilot 40 is energized, venting the high pressure poppet whereby inlet high pressure air raises the highpressure valve unit 50 to the open position. Concurrently, the exhaust solenoid is energized admitting pilot pressure to the exhaust poppet piston chamber and shifting theexhaust valve unit 54 to the closed position and air flowing past the high pressure poppet pressurizes theexhaust chamber 144 through the distribution channel and past theisolation valve unit 56 to pressurize the test part with high pressure air. Thereafter, the isolation pilot is energized applying pilot pressure to the isolation piston chamber and closing the isolation poppet. Thereafter, theflow sensor 16 monitors pressure transients and through the microprocessor interface denotes pass or fail conditions at the indicator lights. - Upon completion of the test, the isolation pilot solenoid is deenergized pressurizing the high pressure piston and sealing the high pressure valve seat, thereby ceasing inlet flow. Concurrently, the isolation and exhaust pilot solenoids are deenergized allowing exhaust chamber and part pressure to shift the exhaust and isolation valves to the open position for completion of the test. In the event of excessive pressure lost at the test part, a light biasing spring may be provided at the isolation poppet to ensure movement to the open position.
- For testing under low pressure conditions, the exhaust poppet is closed and the low pressure valving sequenced in similar fashion to the high pressure test detailed above. More particularly, a part to be tested in mounted in the test fixture, the control system initialized and the test protocol selected. Thereafter, the test is initiated by actuating the
start button 266. As a first condition, the high and low pressure lines are pressurized with the accompanying pilot valves in the normally open positions with the solenoids deenergized. This applies pilot pressure to the associated poppets to close and seal the later. Correspondingly, the normally closed exhaust pilot is deenergized and the exhaust poppet is in the open position. The normally closed isolation pilot is denergized and the isolation poppet is in the open position. - Thereafter the low pressure pilot 42 is energized, venting the low pressure valve whereby inlet low pressure air raises the low
pressure valve unit 52 to the open position. Concurrently, the exhaust pilot is energized admitting pilot pressure to the exhaust poppet piston chamber and shifting theexhaust valve unit 54 to the closed position and air flowing past the low pressure poppet pressurizes the exhaust chamber through thedistribution channel 150 and past the isolation poppet to pressurize the test part with high pressure air. Thereafter, the isolation pilot solenoid is energized applying pilot pressure to the isolation piston chamber and closing the isolation poppet. Thereafter, the flow sensor monitors pressure transients and through the microprocessor interface denotes pass or fail conditions at the indicator. Upon completion of the test, the isolation pilot is deenergized pressurizing the low pressure piston and sealing the low pressure valve seat, thereby ceasing inlet flow. Concurrently, the isolation and exhaust pilot solenoids are deenergized allow exhaust chamber and part pressure to shift the exhaust and isolation poppets to the open position for completion of the test. - Referring to
FIG. 13 , a fully integrated package is illustrated for aleak detection valve 280 as described above. Thevalve 280 comprises an extrudedmetallic valve body 282 having fourvalve assemblies 284, as described above. The valve assemblies are controlled bysolenoids 286 carried on a top horizontal surface. Thevalve body 280 has anisolation port 288 in the illustrated rear wall thereof, and high and low pressure ports, and an exhaust port in the front wall thereof, which are not shown and function as above described. The control lines for thevalve assemblies 284 are routed through adistribution bracket 290. The interior pressure sensors are coupled atpin connector 292 on the top surface of thevalve body 280 for operative connection to associated instrumentation. - Referring to
FIGS. 14 through 17 , in another embodiment of the invention the valving is incorporated into acontrol valve manifold 300. The manifold 300 includes an extrudedlower valve body 302 carrying on a top surface a plurality of longitudinally spacedcontrol modules 304 for operatively controlling conventional fluidic devices, not shown, coupled at a longitudinal series of associatedoutlet ports 306 exiting at a longitudinal side wall of the valve body. Aninlet port 310 and anexhaust port 312 extend longitudinally through thevalve body 302 in parallel spaced relationship for interconnection with the valving as described in greater detail below. - The
ports inlet port 310 is coupled with a supply line for supplying inlet fluid under pressure for control by the valving and controlled operation of the associated fluidic devices. Theexhaust port 312 is coupled with an exhaust line for routing to an appropriate location the exhaust fluid. - A pair of upwardly opening laterally spaced
longitudinal channels 320 are formed in the top surface of thevalve body 302.Solenoids 322 are carried in thechannels 320 and operatively associated with thecontrol modules 304 for controlling pilot pressure to the valving atpilot lines 324. Themodules 304 are connected to a suitable power source via multiple-pin socket connector 326 carried on the front lateral side wall of thevalve body 302. Thevalve modules 304 control the flow between theports operative outlet ports 306 of themanifold 300. If certain of the ports are not required for an application, the outlet ports may be plugged or capped, and additionally the associated control module deleted. Any ports associated with the inactive outlet ports are also deleted or plugged. - It will also be apparent that the length of the valve body may be tailored to the devices to be controlled and may be coupled in series or parallel with other valving manifolds.
- The manifold in controlled formats may be advantageously employed to replicate the functionality of various conventional valving configurations, such as two-way, three-way, four-way, five-way valves. In such configurations, the manifold operates with lower control pressures within a substantially smaller envelope.
- More particularly, as shown in
FIG. 1-8 , eachcontrol module 304 is associated with a pair of laterally spacedvalves valves valve body 302 as referenced inFIG. 9 above. - The
inlet valves inlet port 310. Each valve includes a slidably stem supportedinlet valve member 360 downwardly moveable by a floatingpiston 362 from a raised position communicating with theinlet port 310 and a closed position engaging an annular valve seat downstream of the inlet port. - The
exhaust valves exhaust port 312. Each valve includes a slidably stem supportedoutlet valve member 370 downwardly moveable by a floatingpiston 372 from a lowered position engaging an annular valve seat upstream of theexhaust port 312 and a raised position communicating with the exhaust port. - An
exhaust plenum chamber 380 is formed in thevalve body 302 below the exhaust valve seat and in the open position communicates with the exhaust port. Theexhaust plenum chamber 380 is sealed by acircular cover member 382 and sealed as described with reference to the prior embodiment. Referring toFIG. 19 , across passage 384 is formed at the outer periphery of the exhaust plenum chamber and established a fluid path extending serially from theoutlet port 306 to the cross passage to theexhaust plenum chamber 380 to the exhaust port. - Each piston is carried in a valve cap threadedly connected in a bore extending from the top surface of the valve body coaxial with the exhaust valve seat. The valve caps are fluidly connected with
branch pilot lines 323 above the piston. - Referring to Valve A in
FIG. 18 illustrating a three way valve functionality, theexhaust valve 370 is connected at the branch pilot line with a normallyopen solenoid valve 400 connected with themain pilot line 402. Theinlet valve 360 is connected at the branch pilot line with a normally closedsolenoid valve 404 connected with the main pilot line. - The
outlet port 306 is formed in the side of thevalve body 302 and intersects the inlet valve bore above the inlet valve seat. The device port is fluidly connected by line to one side of asingle acting actuator 410, including return springbiased piston 411, bylines - In operation, the
inlet valve member 360 is moved upwardly to an open position by inlet pressure on the lower surface thereby shifting the piston to a raised position, establishing a fluid path throughoutlet port 306 andlines actuator piston 411. The outlet valve member is shifted by the piston to the closed position sealing flow to the outlet port. To retract the piston, the solenoid valves are reversed, whereby theinlet valve member 360 is closed, the outlet pilot pressure removed allowing pressure conditions in theplenum 380 to move theexhaust valve member 370 to the open position and venting the actuator to theexhaust port 312 thereby retracting the actuator piston under the spring biasing. - For four way simulation according to the invention, Valve B is operatively coupled with Valve A. Valve B has a normally open
inlet solenoid valve 420 and a normally closedexhaust solenoid valve 422. Valve A is coupled with one end of adouble acting actuator 430, includingpiston 431, bylines actuator 430 byline 434. - In operation, the extension of actuator is controlled by Valve A as above described, and Valve B is in the exhaust mode. To retract the
actuator piston 431, Valve A is conditioned for exhaust and Valve B is conditioned for pressure, thereby shifting thepiston 431 to the retracted position. - Referring to
FIG. 20 , the valve manifold of the present invention may also provide two way valve functionality. Therein, avalve 500 includes avalve body 502 carrying avalve assembly 504 as described above. Theinlet valve member 506 is moved bypiston 508 under pilot conditions controlled by normallyopen solenoid valve 510 between a lower closed position engaging the inlet valve seat and the illustrated raised open position. In the open position with the solenoid valve vented, the valve permits fluid flow fromsupply line 520 toinlet port 522past valve member 506 tooutlet port 524 to a pressuredependent device 526. Upon reversal of thesolenoid valve 510, the pilot pressure is applied to the piston to closed the valve member and block flow therethrough. At the next actuation, the inlet pressure shifts the valve member to the open condition. - With the above constructions, it will be appreciated that the individual valve members may be independently controlled and sequenced to a desired actuation schedule. In particular for spool valve simulation, the normal crossover time between valve positions may be eliminated by concurrent actuation of the solenoids. Should staged actuation be desired, time sequencing may be used. Further the valve ports may be integrated with other flow control. Each such simulation provides the compact size afforded by the valves directly place in the manifold bodies, and the low pilot pressures required by the valves, as well as the valve opening pressures afforded by resident pressurization.
- Having thus described a presently preferred embodiment of the present invention, it will now be appreciated that the objects of the invention have been fully achieved, and it will be understood by those skilled in the art that many changes in construction and widely differing embodiments and applications of the invention will suggest themselves without departing from the sprit and scope of the present invention. The disclosures and description herein are intended to be illustrative and are not in any sense limiting of the invention, which is defined solely in accordance with the following claims.
Claims (14)
1-8. (canceled)
9. A method of detecting a leak in a test part comprising the steps of:
pressurizing a high pressure line and a low pressure line with a high pressure pilot valve and a low pressure pilot valve, respectively, to close a high pressure valve and a low pressure valve, respectively;
deenergizing an exhaust pilot valve and an isolation pilot valve to open an exhaust valve and an isolation valve, respectively;
energizing one of the high pressure pilot valve and the low pressure pilot valve to open the high pressure valve and the low pressure valve, respectively;
energizing the exhaust pilot valve to open the exhaust valve; and
pressurizing a test part with high pressure air to detect a leak.
10. The method as recited in claim 9 wherein the step of deenergizing the exhaust pilot valve and the step of deenergizing the isolation pilot valve occur concurrently.
12. The method as recited in claim 9 wherein the step of energizing the one of the high pressure pilot valve and the low pressure pilot valve and the step of energizing the exhaust pilot valve occur concurrently.
13. The method as recited in claim 9 including monitoring pressure transients to determine if the test part leaks based on the pressure transient.
14. The method as recited in claim 9 including indicating if the test part has the leak.
15. The method as recited in claim 9 including denoting a pass condition or a fail condition of the test part.
16. The method as recited in claim 15 including denoting a pass condition or a fail condition with an indicator light.
17. The method as recited in claim 9 including mounting a test part in a test fixture.
18. The method as recited in claim 9 including initializing a control system and selecting a test protocol.
19. The method as recited in claim 9 including activating a start button to initiate a test.
20. The method as recited in claim 9 including opening the isolation valve with a spring.
21. The method as recited in claim 9 wherein the high pressure pilot valve and the lower pressure pilot valve are normally open.
22. The method as recited in claim 9 wherein the exhaust pilot valve and the isolation pilot valve are normally closed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16/020,208 US20190072452A1 (en) | 2001-04-23 | 2018-06-27 | Valve manifold |
Applications Claiming Priority (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/840,688 US6435010B1 (en) | 2001-04-23 | 2001-04-23 | Leak detection system |
US10/223,236 US7490625B1 (en) | 2001-04-23 | 2002-08-19 | Pilot valve manifold |
US12/131,092 US8177188B1 (en) | 2001-04-23 | 2008-06-01 | Valve manifold |
US13/425,820 US8714196B2 (en) | 2001-04-23 | 2012-03-21 | Valve Manifold |
US14/257,193 US9404603B2 (en) | 2001-04-23 | 2014-04-21 | Valve manifold |
US15/226,380 US10018529B2 (en) | 2001-04-23 | 2016-08-02 | Valve manifold |
US16/020,208 US20190072452A1 (en) | 2001-04-23 | 2018-06-27 | Valve manifold |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15/226,380 Continuation US10018529B2 (en) | 2001-04-23 | 2016-08-02 | Valve manifold |
Publications (1)
Publication Number | Publication Date |
---|---|
US20190072452A1 true US20190072452A1 (en) | 2019-03-07 |
Family
ID=40349224
Family Applications (6)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/223,236 Expired - Lifetime US7490625B1 (en) | 2001-04-23 | 2002-08-19 | Pilot valve manifold |
US12/131,092 Expired - Fee Related US8177188B1 (en) | 2001-04-23 | 2008-06-01 | Valve manifold |
US13/425,820 Expired - Fee Related US8714196B2 (en) | 2001-04-23 | 2012-03-21 | Valve Manifold |
US14/257,193 Expired - Fee Related US9404603B2 (en) | 2001-04-23 | 2014-04-21 | Valve manifold |
US15/226,380 Expired - Lifetime US10018529B2 (en) | 2001-04-23 | 2016-08-02 | Valve manifold |
US16/020,208 Abandoned US20190072452A1 (en) | 2001-04-23 | 2018-06-27 | Valve manifold |
Family Applications Before (5)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/223,236 Expired - Lifetime US7490625B1 (en) | 2001-04-23 | 2002-08-19 | Pilot valve manifold |
US12/131,092 Expired - Fee Related US8177188B1 (en) | 2001-04-23 | 2008-06-01 | Valve manifold |
US13/425,820 Expired - Fee Related US8714196B2 (en) | 2001-04-23 | 2012-03-21 | Valve Manifold |
US14/257,193 Expired - Fee Related US9404603B2 (en) | 2001-04-23 | 2014-04-21 | Valve manifold |
US15/226,380 Expired - Lifetime US10018529B2 (en) | 2001-04-23 | 2016-08-02 | Valve manifold |
Country Status (1)
Country | Link |
---|---|
US (6) | US7490625B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111779918A (en) * | 2020-07-10 | 2020-10-16 | 浙江汇之秋科技发展有限公司 | Pipeline plugging device and method for detecting sealing performance of STD series check valves by using same |
US20230003318A1 (en) * | 2019-12-02 | 2023-01-05 | Imi Hydronic Engineering International Sa | A valve for adjusting a fluid flow and methods for use in connection with such a valve |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7490625B1 (en) | 2001-04-23 | 2009-02-17 | John Leslie Johnson | Pilot valve manifold |
DE112008002518B4 (en) | 2007-09-13 | 2023-10-05 | James G. Johnson | Double acting directional fluid flow valve |
WO2013158534A1 (en) * | 2012-04-16 | 2013-10-24 | Ronald Alan Gatten | Pneumatically powered pole saw |
US9510517B2 (en) | 2007-11-09 | 2016-12-06 | Ronald Alan Gatten | Pneumatically powered pole saw |
US8784545B2 (en) | 2011-04-12 | 2014-07-22 | Mathena, Inc. | Shale-gas separating and cleanout system |
US8291934B2 (en) * | 2010-01-20 | 2012-10-23 | Eaton Corporation | Proportional valve assembly |
US9353586B2 (en) | 2012-05-11 | 2016-05-31 | Mathena, Inc. | Control panel, and digital display units and sensors therefor |
DE202012010469U1 (en) * | 2012-10-30 | 2012-11-15 | Bürkert Werke GmbH | Device for indicating the position of a valve spindle |
USD714174S1 (en) * | 2013-05-03 | 2014-09-30 | Mathena, Inc. | Portion of digital gauge |
USD714175S1 (en) * | 2013-05-03 | 2014-09-30 | Mathena, Inc. | Portion of digital gauge |
US10613553B2 (en) * | 2013-07-09 | 2020-04-07 | Deka Products Limited Partnership | Modular valve apparatus and system |
US9429493B2 (en) * | 2013-11-20 | 2016-08-30 | Cinetic Automation | Manifold assembly for a portable leak tester |
USD763414S1 (en) | 2013-12-10 | 2016-08-09 | Mathena, Inc. | Fluid line drive-over |
WO2015168266A1 (en) * | 2014-04-30 | 2015-11-05 | Eaton Corporation | High pressure sealed electrical connector |
CN104483070B (en) * | 2014-12-12 | 2017-10-13 | 中国一拖集团有限公司 | Tractor gearbox body oil hole leak detection valve block assembly and application method |
GB2553681B (en) | 2015-01-07 | 2019-06-26 | Homeserve Plc | Flow detection device |
GB201501935D0 (en) | 2015-02-05 | 2015-03-25 | Tooms Moore Consulting Ltd And Trow Consulting Ltd | Water flow analysis |
USD809627S1 (en) * | 2016-01-13 | 2018-02-06 | Koganei Corporation | Solenoid valve manifold |
DE102016002532A1 (en) * | 2016-02-29 | 2017-08-31 | Harburg-Freudenberger Maschinenbau Gmbh | tire-curing |
USD800591S1 (en) * | 2016-03-31 | 2017-10-24 | Homeserve Plc | Flowmeter |
CN106704661B (en) * | 2016-05-31 | 2020-05-15 | 北京中星时代科技有限公司 | Valve body and intelligent regulation multifunctional integrated valve |
DE102016110904B4 (en) * | 2016-06-14 | 2025-05-15 | Bürkert Werke GmbH & Co. KG | Valve assembly |
USD838614S1 (en) * | 2016-11-07 | 2019-01-22 | Endress+Hauser Flowtec Ag | Measuring apparatus |
USD828195S1 (en) * | 2016-11-07 | 2018-09-11 | Endress+Hauser Flowtec Ag | Measuring apparatus |
USD828197S1 (en) * | 2016-11-07 | 2018-09-11 | Endress+Hauser Flowtec Ag | Measuring apparatus |
USD838615S1 (en) * | 2016-11-07 | 2019-01-22 | Endress+Hauser Flowtec Ag | Measuring apparatus |
USD828196S1 (en) * | 2016-11-07 | 2018-09-11 | Endress+Hauser Flowtec Ag | Measuring apparatus |
USD838616S1 (en) * | 2016-11-07 | 2019-01-22 | Endress+Hauser Flowtec Ag | Measuring apparatus |
CN107514320B (en) * | 2017-07-10 | 2019-05-24 | 北京控制工程研究所 | A kind of micromass culture modular structure based on high pressure frontier technology |
CN107727334A (en) * | 2017-10-19 | 2018-02-23 | 劳福厚 | A kind of cylinder air-tightness detection device |
CN108426682B (en) * | 2018-03-16 | 2020-06-05 | 天津英创汇智汽车技术有限公司 | Suction valve airtightness measuring device and measuring method thereof |
CN110961933A (en) * | 2018-09-29 | 2020-04-07 | 台山市旺春达环保科技有限公司 | Filter core assembling production line |
CN109596284B (en) * | 2018-12-29 | 2020-07-17 | 株洲金城燃气发展有限公司 | Pipeline joint gas leakage detection device |
CN109612657B (en) * | 2018-12-29 | 2020-05-26 | 黄晓亮 | A steam pipeline leak detection device |
US11346460B2 (en) | 2019-02-05 | 2022-05-31 | Swagelok Company | Integrated actuator manifold for multiple valve assembly |
JP6889891B1 (en) * | 2021-02-18 | 2021-06-18 | 京浜ハイフロー販売株式会社 | Leak detection valve and leak detection device |
Family Cites Families (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1224221A (en) * | 1916-03-31 | 1917-05-01 | Harry Schwanebeck | Automatic atmosphere-valve. |
US2522927A (en) | 1948-03-19 | 1950-09-19 | Florence Pipe Foundry & Machin | Pipe testing machine |
US3008487A (en) * | 1959-09-08 | 1961-11-14 | Fegel Albert | Fluid control valve |
US3331237A (en) | 1964-12-07 | 1967-07-18 | Jered Ind Inc | Pneumatic leak test panel |
US3878865A (en) * | 1967-04-28 | 1975-04-22 | Kurt Friebe | Programmable pneumatic control system |
US3577768A (en) | 1969-09-02 | 1971-05-04 | A & L Battery & Electric Servi | Hydrostatic testing apparatus |
USRE29481E (en) * | 1971-02-01 | 1977-11-29 | Fluid Devices, Ltd. | Multi-way directional fluid flow control valve arrangement |
US3872712A (en) | 1971-11-18 | 1975-03-25 | Cross Co | Dynamic air flow comparator system |
IT980603B (en) * | 1972-04-17 | 1974-10-10 | Hydromatik Gmbh | SEAT TYPE TWO-WAY VALVE |
US4172582A (en) * | 1977-04-21 | 1979-10-30 | Rexnord Inc. | Reverse differential holding valve |
US4111226A (en) * | 1977-08-01 | 1978-09-05 | Ross Operating Valve Co. | Multiple function four poppet valve system |
US4188976A (en) * | 1978-02-15 | 1980-02-19 | Austin George K Jr | Multiple dental handpiece control system |
EP0045141B1 (en) * | 1980-07-24 | 1984-11-21 | British Nuclear Fuels PLC | Globe valve with insert seat |
US4587619A (en) | 1981-12-14 | 1986-05-06 | Scans Associates, Inc. | Method and apparatus for electronic leak testing |
JPS58180877A (en) * | 1982-02-12 | 1983-10-22 | Toyooki Kogyo Co Ltd | Directional control valve gear |
CH658895A5 (en) * | 1982-05-19 | 1986-12-15 | Von Roll Hydraulik | PRESSURE LIMIT VALVE FOR PRESSURED FLUID PIPES. |
US4526341A (en) * | 1983-06-15 | 1985-07-02 | Kerotest Manufacturing Corp. | Pneumatic shut-off valve |
DE3336345A1 (en) * | 1983-10-06 | 1985-04-18 | Gebr. Eickhoff Maschinenfabrik U. Eisengiesserei Mbh, 4630 Bochum | HIGH PRESSURE BALL VALVE |
US4637419A (en) * | 1984-07-09 | 1987-01-20 | Vetco Offshore, Inc. | Subsea control pod valve assembly |
US4639196A (en) * | 1986-02-12 | 1987-01-27 | Ingersoll-Rand Company | Fluid control valve |
US4763690A (en) * | 1986-07-29 | 1988-08-16 | Harsco Corporation | Leak-proof valve for gas cylinders |
DE3808962A1 (en) * | 1988-03-17 | 1989-09-28 | Rexroth Mannesmann Gmbh | PRESSURE LIMIT VALVE |
DE3905054C1 (en) | 1989-02-18 | 1990-04-19 | Danfoss A/S, Nordborg, Dk | |
US5072621A (en) | 1990-06-25 | 1991-12-17 | Hasselmann Detlev E M | Pipeline leak detector apparatus and method |
US5295391A (en) | 1992-02-11 | 1994-03-22 | Nde Environmental Corporation | Method and apparatus for detecting leaks in the ullage of a liquid storage tank |
US5295392A (en) | 1992-03-26 | 1994-03-22 | Tech Team, Inc. | Pipe testing equipment |
US5546789A (en) | 1992-08-03 | 1996-08-20 | Intertech Development Company | Leakage detection system |
US5412978A (en) * | 1993-06-22 | 1995-05-09 | Phase 1 Instruments, Inc. | Leak detection system |
JP3344046B2 (en) | 1993-12-22 | 2002-11-11 | 豊田合成株式会社 | Leak amount detection device |
DK0754050T3 (en) * | 1994-01-14 | 2002-10-21 | Xoma Technology Ltd | Anti-gram-positive bacterial methods and materials |
US5440918A (en) | 1994-04-18 | 1995-08-15 | Oster; Earl H. | Portable piping-and-pump-system testing apparatus |
US5557965A (en) | 1994-10-20 | 1996-09-24 | Dover Corporation | Pipeline leak detector |
EP0780615B1 (en) * | 1995-12-21 | 1999-08-18 | Benkan Corporation | Vacuum exhaust valve |
DE19601856C2 (en) * | 1996-01-19 | 2000-05-25 | Siemens Ag | Steamed valve |
JP3104612B2 (en) * | 1996-03-22 | 2000-10-30 | 三菱自動車工業株式会社 | Leak tester and leak test method |
US5703281A (en) * | 1996-05-08 | 1997-12-30 | Southeastern Univ. Research Assn. | Ultra high vacuum pumping system and high sensitivity helium leak detector |
US5898105A (en) | 1996-10-21 | 1999-04-27 | Owens; Carl H. | Leak detection apparatus for tubular fluid lines with fittings |
US6142164A (en) * | 1998-03-09 | 2000-11-07 | Ultra Clean Technology Systems & Service, Inc. | Method and apparatus for removing leaking gas in an integrated gas panel system |
US7490625B1 (en) * | 2001-04-23 | 2009-02-17 | John Leslie Johnson | Pilot valve manifold |
US6435010B1 (en) * | 2001-04-23 | 2002-08-20 | John Leslie Johnson | Leak detection system |
JP3778851B2 (en) * | 2001-12-25 | 2006-05-24 | Smc株式会社 | Poppet valve with heater |
US6854705B2 (en) * | 2002-09-05 | 2005-02-15 | Cito Products, Inc. | Flow control valve that may be used for mold temperature control systems |
JP3994117B2 (en) * | 2002-11-07 | 2007-10-17 | Smc株式会社 | Poppet valve with heater |
JP4217965B2 (en) * | 2003-09-02 | 2009-02-04 | Smc株式会社 | Vacuum pressure control valve |
JP3808071B2 (en) * | 2003-12-01 | 2006-08-09 | シーケーディ株式会社 | Chemical control valve |
-
2002
- 2002-08-19 US US10/223,236 patent/US7490625B1/en not_active Expired - Lifetime
-
2008
- 2008-06-01 US US12/131,092 patent/US8177188B1/en not_active Expired - Fee Related
-
2012
- 2012-03-21 US US13/425,820 patent/US8714196B2/en not_active Expired - Fee Related
-
2014
- 2014-04-21 US US14/257,193 patent/US9404603B2/en not_active Expired - Fee Related
-
2016
- 2016-08-02 US US15/226,380 patent/US10018529B2/en not_active Expired - Lifetime
-
2018
- 2018-06-27 US US16/020,208 patent/US20190072452A1/en not_active Abandoned
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20230003318A1 (en) * | 2019-12-02 | 2023-01-05 | Imi Hydronic Engineering International Sa | A valve for adjusting a fluid flow and methods for use in connection with such a valve |
US12276355B2 (en) * | 2019-12-02 | 2025-04-15 | Imi Hydronic Engineering International Sa | Valve for adjusting a fluid flow and methods for use in connection with such a valve |
CN111779918A (en) * | 2020-07-10 | 2020-10-16 | 浙江汇之秋科技发展有限公司 | Pipeline plugging device and method for detecting sealing performance of STD series check valves by using same |
Also Published As
Publication number | Publication date |
---|---|
US20140225013A1 (en) | 2014-08-14 |
US8177188B1 (en) | 2012-05-15 |
US7490625B1 (en) | 2009-02-17 |
US9404603B2 (en) | 2016-08-02 |
US10018529B2 (en) | 2018-07-10 |
US20160341627A1 (en) | 2016-11-24 |
US20130270467A1 (en) | 2013-10-17 |
US8714196B2 (en) | 2014-05-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10018529B2 (en) | Valve manifold | |
US6435010B1 (en) | Leak detection system | |
US4903529A (en) | Valve system analyzer | |
SE9000341D0 (en) | PROCEDURE AND DEVICE FOR MONITORING THE LEAKAGA STELL IN A CONDUCTING SYSTEM FOR FLUIDUM | |
CN1064939A (en) | Be used to detect the method and apparatus of the reduction valve set pressure of operation valve control | |
US9920850B2 (en) | Adjustable pilot operated flow control valve | |
CN105606355A (en) | Large integrated water gas solenoid valve detection system | |
CA1290588C (en) | Testing device for pilot valves | |
CN112284649A (en) | Multi-pipeline pressure flow coefficient testing device and testing method | |
US4770207A (en) | Fluidic system | |
CA2153854C (en) | Test connector for automatic test device | |
US4380166A (en) | Testing apparatus for a dual pressure indicator and control unit for pasteurization equipment | |
US5801298A (en) | In-line valve seat leak flow testing apparatus | |
CN113465840A (en) | Water meter sealing performance detection system and detection method | |
CN205388531U (en) | Large -scale aqueous vapor solenoid valve detecting system that synthesizes | |
GB2346672A (en) | Valve testing apparatus and method | |
CN212409999U (en) | Instant heating component testing machine | |
CN217424683U (en) | Differential pressure method gas tightness detection valve | |
US3233447A (en) | Leak indicator system | |
CN212458870U (en) | Air pressure regulating valve detection device | |
CN110017948B (en) | Test bench for cooler detection | |
US4527770A (en) | In-service test valve | |
KR20080105326A (en) | Air tightness test system and test method thereof | |
CN201210104Y (en) | Test apparatus for gas regulator | |
CN220084281U (en) | Solenoid valve leakproofness detection device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STPP | Information on status: patent application and granting procedure in general |
Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: NOTICE OF ALLOWANCE MAILED -- APPLICATION RECEIVED IN OFFICE OF PUBLICATIONS |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO PAY ISSUE FEE |