Self-contained hydraulic ESD system

Information

  • Patent Grant
  • 6276135
  • Patent Number
    6,276,135
  • Date Filed
    Thursday, April 29, 1999
    25 years ago
  • Date Issued
    Tuesday, August 21, 2001
    23 years ago
Abstract
A hydraulic control circuit for a hydraulic actuator, including a high-low pilot valve having a sensing port for connection to a flow line. A single pressure line connects the high-low pilot to a hydraulic actuator. A second line connects the high-low pilot to a reservoir. A normally closed relief valve is connected to the single pressure line for relief of excessive pressure. A normally closed override valve is connected to the single pressure line for manual override of circuit controls. A pump is connected to the single pressure line for pressuring the single pressure line. The hydraulic control circuit has a normally open time out valve on the single pressure line, the time out valve being set to close a pre-set time interval after being manually activated, to isolate the high-low pilot, from the single pressure line to the hydraulic actuator, until the time out period has elapsed. The override valve is connected to the single pressure line between the time out valve and the hydraulic actuator. The relief valve is connected to the single pressure line between the time out valve and the hydraulic actuator. The override valve, relief valve, high-low pilot, and the pump are connected between the first line and the reservoir.
Description




FIELD OF THE INVENTION




This invention relates to hydraulic emergency shut-down systems (ESD) for actuating closure of valves.




BACKGROUND OF THE INVENTION




Several emergency shut down systems are known in the art such as the ESD sold by Erichsen, the ESD sold by Bettis of Houston, USA, the RA-Presco™-Dyne ESD sold by Barber Industries, of Edmonton, Canada, and U.S. Pat. No. 5,341,837 of Johnson. U.S. Pat. No. 4,961,560 Ellett-Two Way Latching Trip Valve. U.S. Pat. No. 5,070, 00 Johnson-Safety Valve Actuator. U.S. Pat. No. 5,213,133 Ellett-Pilot Control Valve. U.S. Pat. No. 5,291,918 Johnson-Safety Valve Actuator. U.S. Pat. No. 5,464,040 Johnson-Safety Valve Actuator. These devices typically include a pilot valve that senes pressure in a flow line. When the pressure moves out of a pre-defined range, the pilot valve signals an actuator to close a valve and shut down flow in the flow line. These devices typically have a high pressure line and a low pressure line. The high pressure line is used to actuate the actuator, while the low pressure line is controlled by the pilot valve.




SUMMARY OF THE INVENTION




The use of dual high and low pressure controls unnecessarily complicates the design of the ESD. This invention provides a novel ESD that includes a single pressure line for control functions at the pilot valve and actuator.




There is therefore provided in accordance with an aspect of the invention, a hydraulic control circuit for a hydraulic actuator, including a high-low pilot valve having a sensing port for connection to a flow line. A single pressure line connects the high-low pilot to a hydraulic actuator. A second line connects the high-low pilot to a reservoir. A normally closed relief valve is connected to the single pressure line for relief of excessive pressure. A normally closed override valve is connected to the single pressure line for manual override of circuit controls. And a pump is connected to the single pressure line for pressuring the single pressure line.




In a further aspect of the invention, the hydraulic control circuit has a normally open time out valve on the single pressure line, the time out valve being set to close a pre-set time interval after being manually activated. In a further aspect of the invention, the override valve is connected to the single pressure line between the time out valve and the hydraulic actuator. The relief valve is preferably connected to the single pressure line between the time out valve and the hydraulic actuator. The override valve, relief valve and the pump are preferably connected between the first line and the reservoir.




In addition, this invention provides a novel configuration of pilot valve and time out valve.




These and other aspects of the invention are described in the detailed description of the invention and claimed in the claims that follow.











BRIEF DESCRIPTION OF THE DRAWINGS




There will now be described preferred embodiments of the invention, with reference to the drawings, by way of illustration only and not with the intention of limiting the scope of the invention, in which like numerals denote like elements and in which:





FIG. 1

is a hydraulic schematic of a hydraulic control circuit according to the invention,





FIG. 2

is a section through a time out valve for use in the hydraulic circuit of

FIG. 1

;





FIG. 3

is a bottom view of the time out valve of

FIG. 2

;





FIG. 4

is a side view of the time out valve of

FIG. 2

;





FIG. 5

is a section through the time out valve of

FIG. 2

with the section taken at right angles to the section of

FIG. 2

; and





FIG. 6

is a detail of a drip valve for use in the time out valve of

FIG. 2

;





FIG. 7

is a section through a pilot valve for use in the hydraulic control circuit of

FIG. 1

;





FIG. 8

is a detail of a diaphragm used in the pilot valve of

FIG. 7

;





FIG. 9

is a is side view of the pilot valve of

FIG. 7

;





FIG. 10

is a section through a pilot valve similar to the one shown in

FIG. 7

but showing a modification used for high pressure lines; and





FIG. 11

is a section along the line


11





11


of FIG.


7


.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




In this patent document, a reference to “a connection”, “connected” or “connect(s)” is a reference to hydraulic connection unless the context otherwise requires.




Referring to

FIG. 1

, there is shown a hydraulic control circuit for an actuator


20


, which actuates a valve, not shown. A high-low pilot valve


10


is connected to a flow line


16


to be monitored through port


12


of valve


10


and line


14


. A single pressure line or hydraulic manifold


18


connects the high-low pilot


10


to the hydraulic actuator


20


. The single pressure line


18


has a single pressure along its length, and thus forms a single pressure circuit. A second line


22


connects the high-low pilot


10


to a reservoir


24


. A normally closed relief valve


26


is connected to the single pressure line


18


through line


28


for relief of excessive pressure and drains through line


27


and line


22


to the reservoir


24


. A normally closed override valve


30


is connected to the single pressure line through line


28


and


29


for manual override of circuit controls. The line


28


connects to the line


18


between the time out valve


44


and actuator


20


. The override valve


30


drains through line


31


and


22


to the reservoir


24


. A pump


32


is connected to the single pressure line


18


via line


34


and line


28


for pressuring the single pressure line. The pump


32


is preferably a hand pump, and is separated from the line


28


by a filter


36


and a leak tight outlet check valve


38


, both on line


34


. The pump


32


is also connected via line


40


with inlet check valve


42


to reservoir


24


.




When the pump


32


is activated, fluid moves from reservoir


24


through lines


40


,


34


and


28


into line


18


. The relief valve


26


and override valve


30


block return of fluid to reservoir


24


, and thus pressure builds up in line


18


when the pump


32


is activated. The time out valve


44


is normally open, and is set to close a pre-set time interval after being manually activated. The time out valve


44


is described in more detail in relation to

FIGS. 6-10

. A filter


46


is also provided on the single pressure line


18


, along with a fusible plug


48


.




The hydraulic control circuit works as follows. The high-low pilot


10


monitors pressure in the flow line


16


and is normally closed. When the pressure exceeds a high set point or is lower than a low set point, the pilot valve


10


opens, and hydraulic fluid drains from line


18


and


22


into reservoir


24


. Loss of pressure at the actuator


20


causes the actuator


20


to close its associated valve. If the pressure in lines


28


or


18


becomes too high itself, then relief valve


26


opens, until the pressure returns to normal. The actuator


20


can be activated manually by operation of the override valve


30


. If the temperature becomes too high, fusible plug


48


opens to allow line


18


to drain and activate the actuator


20


.




To set the actuator


20


initially, pressure must be built in line


18


. This is accomplished initially by closing time out valve


44


. High low pilot


10


is open with low line pressure being sensed. The time out valve


44


begins to count down towards opening. How it does this is described in relation to

FIGS. 6-10

. While time out valve


44


is closed, pump


32


is activated to increase the pressure in lines


18


and


28


until actuator


20


is activated. Activation of actuator


20


will lead to increase of pressure in flow line


16


, and if the line is working properly, pressure in line


16


will be in its intended operating range. Thus, when valve


44


opens, the high-low pilot


10


will have closed, thus maintaining pressure in line


18


and activating the actuator


20


with pressure in line


18


.




The pilot


10


is shown in

FIGS. 7-10

. The pilot


10


is designed to bleed down an E.S.D. hydraulic circuit when high or low pressures are sensed, such as in an Oil/Gas production or pipeline facility. The high and low set points are independently adjustable to meet predetermined levels, in accordance with the desire of the operations personnel. The pilot may be used for high only or low only or both high and low in one unit. Several springs can be chosen to provide a broad range of set points, in both high and low categories.




The time out valve


44


is shown in

FIGS. 2-6

. The time-out valve


44


is located in the pilot circuit shown in

FIG. 1

so that when start up is required and the pilot is in the bleed down position (low line pressure being sensed), the time-out valve can be closed preventing bleed down of hydraulic pressure enabling the E.S.D. system to be pressured up with hydraulic oil.




Referring to

FIG. 2

, the time-out valve


44


is formed from a body


109


, with head


102


. An O-ring


104


is provided between body


109


and head


102


. A stem


106


extends through the body


109


and head


102


, and is provided with a stem wiper


101


to keep the stem


109


clean. A piston


107


sits in a cylindrical chamber between the body


109


and head


102


. The stem


106


passes through the piston


107


. Springs


103


are positioned between the head


102


and piston


107


on spring guides


105


O-rings


108


,


120


and


118


are provided respectively between the piston


107


and body


109


, between stem


106


and head


102


and between piston


107


and stem


106


. Within the body


109


, the stem


106


sits in inner cage


116


and outer cage


111


. Lower O-ring


112


and upper O-ring


114


are provided between outer cage


111


and the body


109


. Outer cage


111


is secured in the body


109


by snap ring


113


. The stem


106


is provided with grooves


150


. An O-ring


115


is provided in the body


109


adjacent the grooves


150


in the stem


106


. An O-ring


117


is provided at the upper end of the inner cage


116


between the stem


106


and body


109


. A pin


119


is provided transversely in the piston


107


to hold the piston


107


on the stem


106


. The body


109


is provided with ports


149


and


148


. The port


148


communicates with a bore


146


which terminates in an annular groove


151


in the body


109


that extends around the stem


109


at the top of the outer cage


111


. Bore


146


is plugged on its outer end with plug


110


. The port


149


communicates with a bore


152


which terminates in an annular groove


153


in the body


109


that extends around the stem


109


at the bottom of the inner cage


116


. Bore


152


is plugged on its outer end with plug


110


.




Referring to

FIGS. 4-6

, the stem


106


is provided with handle or lever


131


which is pivotally attached to stem


106


at pivot pin


135


. The lever


131


is pivotally secured to the head


102


by lever bracket


134


and fulcrum pin


133


which passes through both the lever bracket


134


and the lever


131


. A capscrew


132


with nut


129


secures the lever bracket


134


to the head


102


, with the bracket


134


spaced from the head


109


by spacer


130


. Capscrews


136


secure the head


102


to the body


109


. Capscrews


128


secure the body


109


to a supporting block (not shown). An alignment pin


137


aligns the piston


107


with respect to the head


102


. The chamber


138


above and below the piston


107


is filled with dampening fluid. A vent plug


139


, with spring


140


and ball


141


, is provided at the top of the chamber


138


in head


102


, and communicates with the chamber


138


through bore


154


. The ball


141


is biased against the terminus of bore


154


in head


102


by spring


140


.




Referring in particular to

FIG. 6

, the piston


107


has a metering valve connecting between the portions of the chamber


138


above and below the piston


107


. The metering valve is formed from a retainer


121


, under which is placed a screen


122


and insert


123


. The insert


123


, which is hat shaped, forms a seat for an O-ring


124


. An orifice disc


125


, with an orifice in the middle, is placed against the insert


123


and


0


ring


124


. A spring


126


is placed between a shoulder


155


on the piston


107


and the orifice disc


125


. A snap ring


127


keeps a second screen


122


in place.




When the time-out valve


44


is open, oil can flow up through port


149


in body


109


through inner cage


116


, through grooves


150


in stem


106


, and through the outer cage


111


into port


148


in body


109


to the line


118


.




To close the time-out valve, the lever


131


is pushed down. This raises the stem


106


so that the grooves


150


do not connect with the inner cage


116


and outer cage


111


and the hydraulic oil cannot go through the time-out valve


44


.




When the time-out valve


44


is closed with the lever


131


pushed down (stem up), the pilot


10


is timed out of the circuit for as long as it takes for the time-out valve


44


to open again on its own.




The time-out valve


44


operation is described as follows: When the stem


106


is moved up by the lever


131


, the piston


107


moves up with the stem


106


and compresses piston springs


103


. As the piston


107


moves up in the upper bore of the body


109


, the dampening fluid


138


lifts orifice disc


125


off O-ring


124


around the insert


123


, thus allowing fluid to pass so the piston


107


can, in fact, move up. Upon releasing the lever


131


, the piston springs


103


push down on the piston


107


. The dampening fluid


138


now has to flow through the seated orifice disc


125


which delays the rate that the piston


107


and stem


106


moves downward. This delay causes the pilot


10


to be timed-out of the circuit. The duration of time-out can be determined by choosing the orifice size in the orifice disc


125


and by choosing a suitable viscosity for the dampening fluid


138


.




The pilot is designed particularly for use with the E.S.D. shown in

FIG. 1

, but it may be used with other systems requiring high and low set points. When the production/pipeline facility pressure is too high or too low due to failure of the facility, the pilot senses this condition and bleeds down E.S.D. system hydraulic pressure causing the shut down valve (not shown) to close and prevent product loss. The pilot is shown in

FIGS. 7-10

.




The base of the pilot consists of a bottom sub


221


, which contains a pressuresensing capsule, which is made up of nut


214


, upper ring


215


, lower ring


216


, gasket


217


, diaphragm


218


, scrolled support disc


219


, and piston


220


. The design and operation of the pressure sensing system is described in greater detail in U.S. Pat. No. 5,670,766 of Argus Machine Co. Ltd., of Edmonton, Canada, from whom the product may be purchased. The nut


214


is used to hold down the upper ring


215


, and the lower ring


216


, which compresses the gasket


217


, sealing off the sensed facility pressure against the diaphragm


218


. The scrolled support disc


219


transmits the diaphragm


218


movement to the piston


220


. This design differs slightly from what is described in U.S. Pat. No. 5,670,766 by having an increased piston stroke which is required to sufficiently open a high poppet


210


and low poppet


224


, to provide adequate bleed down rate of the hydraulic pressure.




Stem


230


transfers movement of the piston


220


through low base plate


201


to low pressure spring


237


and at higher pressures through high base plate


228


to high pressure spring


231


. Spool


223


is positioned approximately in an axial relationship to the stem


230


by the use of a selection of two spool spacers


206


, one above and one below the spool


223


, and necessary shims


207


and


213


, all retained snugly with a snap ring


205


. The assembly in this paragraph may be modified to use threads on the stem


230


and in the spool


223


with a lock nut instead of the snap ring


205


.




A top sub


234


is threaded into the bottom sub


221


and holds stop ring


227


down against stop ring shims


226


. The number of stop ring shims


226


is determined by how many it takes to cause the stem


230


to shoulder up against the high base plate


228


when the upward travel of the stem


230


has reached 50% of its total travel. This portion of the travel is called the low pressure travel function, and may be approximately 0.025″. Two set screws


204


are inserted through threaded holes in the bottom sub


221


into counterbored holes in the top sub


234


locking them together.




The high pressure spring


231


is situated between the stop ring


227


and the high adjuster ring


232


. The high pressure spring


231


is compressed by screwing down high adjustment knob


235


against high contact ring


233


which moves down against the high load screws


203


moving them down with the high adjuster ring


232


. High pressure spring


231


controls the high pressure travel function, namely the top 50% of the upward stem


230


travel.




The low pressure spring


237


is situated between the low base plate


201


and low adjustment


239


. Low pressure spring


237


is compressed by screwing down the low adjustment


239


. The low pressure spring


237


controls the low pressure travel function.




Low adjustment cover


238


serves to totally enclose the inner pilot assembly, as well as the low adjustment


239


, and threads onto the top sub


234


. O-rings


211


(between bottom sub


221


and a lower side of poppet block


209


),


225


(between an upper side of poppet block


209


and bottom sub


221


),


229


(between high adjustment knob


235


and bottom sub


221


), and


236


(between cover


238


and knob


235


) seal off the outer atmosphere from the inner pilot assembly. O-ring


202


only serves to hold the low base plate


201


from falling out of place off the stem


230


. An elastomeric U-cup seal


222


keeps impurities and condensed water vapor out of the lower portions of the pilot assembly.




The operating position of the high poppet


210


is adjusted by activating upper setting screws


208


and lower setting screws


212


, which thread into the poppet block


209


, before tightening block capscrews


240


. The same procedure is used to obtain the operating position of the low poppet


224


. Currently a body breather vent


242


is used to return the E.S.D. hydraulic oil, bled down by either the high poppet


210


or the low poppet


224


. Optionally, the poppet blocks


209


may be configured to port the fluid bled by the poppets


210


and


224


directly to a return line. A body drain plug


241


is provided for draining the pilot body. Pressure in from line


18


is provided to high sense side of the pilot


12


through port


251


, and to low sense side of the pilot


12


through port


250


. Activation of the poppet valves


210


and


224


cause fluid to flow through the ports


251


and


250


respectively around the spool


223


between the spool


223


and the poppet block


209


and exit the pilot


12


through outlet drain


242


, which connects to line


22


. The poppet valves


210


and


224


are of the type typically used as tire stem valves.




The high and low set points are adjusted separately, the high set point being affected by subsequent low set point changes. Adjustments of the high set point do not affect the low set point. It is therefore desirable to complete the low set point adjustments before completing the high set point adjustment. For high pressure Oil/Gas production or pipeline applications, an alternate plunger type piston


243


received by collar


244


and packed with packing seals


245


and


246


can be used instead of the diaphragm


218


, as shown in FIG.


10


.




In an embodiment of the ESD made by Argus Machine Co. Ltd. of Edmonton, Alberta, Canada, the oil reservoir


24


had a useable volume of 140 cu. in. (200 cu. in. to fill). The maximum sustained output pressure was 2,000 p.s.i. Automatic transmission fluid was used as the hydraulic fluid in line


18


down to −20° F. and aircraft hydraulic oil for below −20° F. (J-13 Univis). The general operational instructions are: To start-up system (opening gate valve with actuator


20


), lift knob on time-out valve


44


(to isolate pilot signal). Reciprocate handle of hand pump


32


until valve is open. After the time-out period has elapsed, the high-low pilot


10


takes over control of the system. When either high or low set points are sensed by the high-low pilot


10


, the hydraulic oil pressure is bled back to tank


24


causing the acuator


20


to close the gate valve. If it is desired to close the gate valve even though sensed flow line pressures are within the set points of the pilot, simply depress the knob on the over-ride valve


30


. A fusible plug


48


is incorporated into the system to automatically bleed the hydraulic oil pressure back to tank in the event of a fire or extremely high temperature.




To test the high-low pilot


10


, use an isolation valve between it and the flow line


16


.




Use a pressure gauge and a hand operated hydraulic hand pump to simulate flow line pressures and test for both high and low set points.




1. Mount the subject E.S.D. System onto the spring close actuator cylinder


20


with bracket and clamps (available from Argus Machine Co. Ltd.), and mount the pressure control pilot


10


on its own test stand adjacent to the E.S.D.




2. Connect the actuator


20


, hydraulic manifold


18


and pressure control pilot


10


, using stainless steel tubing and fittings. Use Loctite PST dope on pipe threads where applicable.




3. Remove filler cap (pressure/vacuum type) and ¾ fill the hydraulic oil reservoir with J-13 Univis aircraft hydraulic oil. Leave the filler cap off until air bleeding is done.




4. Install a temporary pressure gauge (2,000 p.s.i.) on the port, where the fire safe fusible plug


48


is normally installed, for this test. (The system relief valve is set at 1,000 p.s.i.)




5. The pressure control pilot


10


should be sensing zero pressure at this time to allow the air to be displaced from within the system.




6. Activate the lever of the time-out valve


44


& reciprocate the hand pump


32


until the spring close actuator


20


has fully opened the gate valve.




7. Wait for the time-out valve


44


to shift and bleed the pressure from the actuator


20


.




8. Allow five (5) minutes for the air bubbles to escape from the oil in the reservoir


24


.




9. Apply pressure to the pressure control pilot


10


, bringing it into the operating range between the high and low set points.




10. Pump up the system again, opening the gate valve.




11. Push down on the knob of the over-ride valve


30


and hold it down until the gate valve closes.




12. Allow five (5) minutes for the air bubbles to escape from the oil in the reservoir


24


.




13. Repeat Steps 6, 11 and 12. Install the filler cap.




14. Repeat Step 6 and check the low set point of the pressure control pilot


10


.




15. Repeat Step 6 and check the high set point of the pressure control pilot


10


.




16. Apply pressure to one side of the gate valve and check its operation, by either cycling the pressure control pilot


10


or, by setting the pilot


10


within the operating range and using the over-ride valve


30


.




17. Check the leak tight integrity of the system by installing a dial indicator (reading in 0.001″ increments) on the stem of the spring close actuator


20


when the gate valve is in the open position.




18. The stem of the dial indicator should rest on the head of the spring close actuator. Spring close actuator action, from the valve open position, should clear the dial indicator after about 0.500″ of movement.




19. The dial indicator dwell position, for the leak tight integrity test, should be about 0.100″ to 0.400″ from the fully open gate valve position. Jog the over-ride valve to obtain this position. ‘Zero’ the dial and let the system stand for one hour. The actuator stem should not shift more than 0.001″ during that time. The system temperature should be held within ±5° F. during this test.




20. To speed up the process of determining the cause of leak down, if any, temporarily install an instrument valve in the supply line from the hydraulic manifold


18


to the pilot


10


. (In an emergency a ¼″ N.P.T. pipe plug could be installed at the manifold instead.)




A person skilled in the art could make immaterial modifications to the invention described in this patent document without departing from the essence of the invention that is intended to be covered by the scope of the claims that follow.



Claims
  • 1. A hydraulic control circuit for a hydraulic actuator, the hydraulic control circuit comprising:a high-low pilot valve having a sensing port for connection to a flow line; a first line connecting the high-low pilot to a hydraulic actuator, the first line forming a single pressure circuit; a second line connecting the high-low pilot to a reservoir; a normally closed relief valve connected to the first line for relief of excessive pressure; a normally closed override valve connected to the first line for manual override of circuit controls; and a pump connected to the first line for pressuring the first line.
  • 2. The hydraulic control circuit of claim 1 further comprising a normally open time out valve on the first line, the time out valve being set to close for a pre-set time interval after being activated.
  • 3. The hydraulic control circuit of claim 1 in which the override valve is connected to the first line between the time out valve and the hydraulic actuator.
  • 4. The hydraulic control circuit of claim 1 in which the relief valve is connected to the first line between the time out valve and the hydraulic actuator.
  • 5. The hydraulic control circuit of claim 1 in which the override valve, relief valve and the pump are connected between the first line and the reservoir.
US Referenced Citations (9)
Number Name Date Kind
3800537 Denis Apr 1974
4676140 Haussler Jun 1987
4961560 Ellett Oct 1990
5070900 Johnson Dec 1991
5213133 Ellett May 1993
5291918 Johnson Mar 1994
5341837 Johnson Aug 1994
5464040 Johnson Nov 1995
5522212 Kubik Jun 1996
Non-Patent Literature Citations (8)
Entry
Abstract of U.S. Patent No. 4,921,207, issued May 1, 1990, Baker, 1 page.
Sigma Enterprises, Inc. product brochure entitled “Combination Hi/Low Bleeder Pilot”, 1997 Technical Product Bulletin, 3 pages.
Erichsen product brochure entitled “Self Contained Hydraulic Shutdown System”, at least as early as Oct. 1989, 3 pages. Inventor has seen earlier versions but does not have copies.
Bettis Actuators & Controls, product brochure entitled “PressureGuard™ Self-Contained Hydraulic Emergency Shutdown Systems”, printed Sep. 1995, 6 pages.
Barber™ Industries Ltd. product brochure entitled “RA-PRESCO-DYNE Self Contained Emergency Shut Down System For Reverse Acting Gate Valves”, Bulletin 680, printed Aug. 1991, and Operating Manual for Hydraulic Operated-Spring Opposed Valve Actuation Systems, printed Feb. 1993, 15 pages. Advertising for RA-PRESCO-DYNE system appeared in Oilweek magazine, Canada, in Sep. 1977.
Barber™ Industries Ltd. C-HL-Presco Pilot 1991+10+28, and Type C-HL-Presco Pilot, Model 5398, 14+Nov.+1991, 2 pages.
Barber™ Industries Ltd. product brochure entitled “Presco-Pilot”, 10/91, 4 pages.
“New pressure control pilot solves a pollution problem,” Jim Ellett, Oilweek, Canada, Sep. 20, 1971.