AU632759B2 - Diagnostic apparatus and method for fluid control valves - Google Patents
Diagnostic apparatus and method for fluid control valves Download PDFInfo
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- AU632759B2 AU632759B2 AU40188/89A AU4018889A AU632759B2 AU 632759 B2 AU632759 B2 AU 632759B2 AU 40188/89 A AU40188/89 A AU 40188/89A AU 4018889 A AU4018889 A AU 4018889A AU 632759 B2 AU632759 B2 AU 632759B2
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Description
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COMMONWEALTH OF AUSTRAL f PATENTS ACT 1952 FORM 21-56(5574)A AS Class: Int. Class Application Number: Lodged: Complete specification: Lodged: Accepted: Published: Priority: Related Art: 0 S S
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ee Name of Applicant: Address of Applicant: Actual Inventor/X: Address for Service: FISHER CONTROLS INTERNATIONAL, INC.
8000 Maryland Avenue, Clayton, Missouri 63105, United States of America.
WILLIAM VINCENT FITZGERALD E.F. WELLINGTON CO., Patent and Trade Mark Attorneys, 457 St. Kilda Road, Melbourne, 3004, Victoria.
Complete Specification for the invention entitled: i "DIAGNOSTIC APPARATUS AND METHOD FOR FLUID CONTROL VALVES" The following statement is a full description of this. invention including the best method of performing it known to us.
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1A This invention relates to fluid control valves and more particularly to apparatus and a method for diagnostically testing and evaluating the condition of such valves, particularly pneumatically operated valves.
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0006 0 5 Background Of The Invention Reference may be made to the following U.S.
patents of interest: 4,542,649; 4,660,416; 4,690,003; 4,693,113; 4,712,071; 4,735,101.
10 Fluid control valves are used in a wide variety of applications such as oil and gas pipelines and processing lines, as well as to control water and other fluids in nuclear power generating stations. In such critical applications, substantial maintenance is 15 required, both of the periodic preventative maintenance type as well as to repair valve breakdowns in order to assure that the control valve performs properly, thereby reducing losses associated with process fluid leakage and trim damage. It has been desired therefor to provide an easy and readily available technique for diagnostically checking such fluid control valves already installed in the system so that operational problems can be detected before they become the source S 0
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of fluid process losses or, in the worse case, cause unscheduled shutdowns of the processing system.
A motor operated valve analysis and testing system is described in the above-mentioned patents for fluid control valves operated by a very specific type of electric actuator including a motor moving the valve stem through a worm gear, and a cluster of compression springs termed a "spring pack" for reacting to valve stem thrust. Spring pack movement is detected to 10 provide an indirect indication of stem load. However this first requires that a calibration be done where the stem load is measured using a load cell and the readings correlated to spring pack movement. The load cell is then removed and the spring pack reading used to measure stem load during operation. Motor current is also measured and is correlated to stem load to give an indication of the overall condition of the motor. This prior art system is time consuming and cumbersome in requiring the initial calibrations as well as requiring a significant amount of time to install and remove the load cell on each actuator to be tested.
Furthermore, many fluid control valves, such as pneumatically actuated control valves do not have a motor or spring pack so that the valve measurements 25 described earlier in connection with electrically actuated valves does not apply to such pneumatic units. Accordingly, it is desired to provide an improved technique for diagnostically testing fluid control valves, such as pneumatically operated valves in a fast and efficient manner.
Summary Of The Invention In accordance with the principles of the present invention, there is provided apparatus and a method for diagnostically testing fluid control valves, such as pneumatically actuated valves. The technique :1 it 3 21-56(5574)A includes providing a pressure sensor to sense varying pressure at the input of the valve actuator and a position sensor to sense movement of the valve plug.
The valve is then operated through a test operation cycle by supplying a controlled variable pneumatic pressure to the input of the pneumatic valve actuator.
During the test operation cycle the valve plug is moved through a desired range, normally from a fully opened position to a fully closed position and returned from the fully closed position to the fully opened position.
During the test operation cycle, the pressure j sensor provides an output signal which corresponds to varying pressure at the valve actuator input, and the 15 position sensor provides an output signal corresponding Sgee ee to movement of the valve plug. The respective output signals of air pressure at the actuator and of valve plug or valve stem position are then processed to derive data representing the variation in pressure at the valve 20 actuator input as a function of movement of the valve plug during the test operation cycle. The valve stem S"load is derived by multiplying the air pressure times the effective area of the actuator diaphragm. Since the effective area is a known quantity, no calibration cycle is required to determine valve stem load as in the prior art.
Therefore a significant advantage of the present invention is the ability to immediately plot valve stem load versus valve position and display the plot such as on a visual display and/or a printer.
Analysis of the plot of stem load versus valve plug travel provides several important pieces of information on the valve condition, namely: 1. A determination of valve packing, seal, and bearing friction. Excessive friction levels can 4 21-56(5574)A affect actuator operation. Friction values that are too low may indicate insufficient load on the packing since packing friction is normally the largest of its three constituents; 2. Determine the valve spring constant and spring adjustment to thereby check for an incorrect or damaged spring and to determine whether the spring "benchset" has been properly adjusted; 3. Determine the valve seat load by determining the pressure at which the plug contacts the seat and comparing it to the final pressure; and Determining that the valve plug is S contacting the seat on the closing stroke.
A diagnostic check of the valve actuator can also be made with the present invention. In a goes conventional pneumatic operated valve, a current to 600 ""pressure transducer is coupled to a valve positioner which supplies an operating pneumatic pressure to the valve diaphragm actuator which in turn 20 is coupled to a sliding valve stem and plug. A feedback o is provided by a valve positioner arm having one end connected to the actuator/valve stem and the other end coupled to the positioner so as to track movement of the valve stem. Normally a 4-20 mA signal controls the valve operation.
r The present invention includes providing a control signal to the I/P transducer to operate the valve over a test operation cycle, while taking measurements of the respective inputs and outputs of the I/P transducer and the valve positioner. Therefore, during i the test operation cycle wherein the valve is stroked through its test cycle, the present apparatus provides a calibration check on the valve positioner and the I/P transducer. In addition, utilizing the above input information, the present system can verify valve stroke, actual stroking time, and pneumatic supply pressure.
5 21-56(5574)A Brief Description Of The Drawings The features of this invention are set forth with particularity in the appended claims. The invention may be best understood by reference to the following description taken in conjunction with the accompanying drawings, in which like reference numerals identify like elements in the several figures and in which: Figure 1 is a schematic diagram of a fluid control valve and actuator assembly for a sliding stem valve to illustrate the moving parts that cause flow changes through the valve; Figure 2 is a schematic diagram illustrating a *'bee: fluid control valve and actuator assembly and diagnostic S 15 valve testing apparatus in accordance with the present invention; Figure 3 is a block diagram illustrating the diagnostic valve controller components and the flow of input and output information in accordance with the 20 present invention; and o C •Figures 4-8 are graphic plots derived from the diagnostic controller output information and which plots are helpful in evaluating the valve and actuator condition.
Detailed Description A very large variety of control valve and actuator combinations are commercially available. Such commercially available valve types include sliding stem, rotary ball, rotary plug, butterfly, and eccentric disk. The actuator can be spring and diaphragm, spring and piston, double acting piston, hydraulic, electrohydraulic, or electric, mounted on either a rotary or sliding stem valve. The present invention is particularly useful for fluid control valves using a pneumatically operated actuator with either diaphragms 6 21-56(5574)A 0
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or pistons as their primary source of power. For purposes of illustrating the principles of the present invention, a spring and diaphragm actuator on a sliding stem valve is described hereinafter. It is to be understood however that the principles of this invention can also be adapted for use on a rotary valve.
Figure 2 illustrates a fluid control valve and actuator assembly 10 schematically illustrated so that the force interactions can be better understood. The 10 valve and actuator assembly 10 shown in Figure 2 is known as a spring to open, flow-down, balanced construction and is one of the more common versions commercially available and used, however it is understood that the present invention can be applied equally well with other pneumatically operated versions.
Valve 10 includes diaphragm plate 12, actuator stem 14 and a valve plug/stem assembly including valve stem 16 and plug 18. A stem connector 20 connects actuator stem 14 to valve stem 16. Spring 22 normally 20 exerts sufficient pressure upwardly on diaphragm 12 to lift the valve plug and stem assembly so that the valve is in the open position.
Referring now to Figure 1, there is illustrated a simplified free body diagram of the valve 25 and actuator with schematic representations of diaphragm 12, actuator stem 14, valve stem 16, plug 18 and connector 20. The illustrated components are the moving parts that cause changes in fluid flow through the valve. The respective forces labeled and illustrated in Figure 1 adjacent to a respective directional arrow are defined in the following Table 1.
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i 7 21-56(5574)A Table 1 DEFINITION OF FORCES Force Symbol Description Fa The product of the air pressure in the actuator and the effective area of the diaphragm. The effective area changes with valve plug travel, and this change is taken into account in the system's calculations.
Fp The spring load acting against Fa, and expressed as Fp Fi-+ T(K).
Fi Initial spring pre-load with the valve wide open. This is a function *of the valve benchset, or in other 15 words, the initial spring adjustment.
T Valve plug travel with zero as the wide-open position.
K Spring constant.
Fb The actuator bearing friction force, *20 which always acts in the direction opposite to stem movement.
.o Ff Packing friction, especially important with graphite or asbestostype packing where improper packing 25 adjustment can result in relatively o..o large variations in packing friction.
FU1 The stem unbalance caused by the internal pressure acting on the unbalance area of the stem.
Fs The friction force between the seal and the I.D. of the cage. This changes as a function of the type and diameter of the seal.
FL The seat load between the plug and seat ring. This is critical in _yl 1-11-~111-- 1 -~LLI 8 21-56(5574)A FU2 determining the shut-off capabilities of the valve in question.
The pressure unbalance on the plug.
It can be in either direction depending on whether the valve is flow-up or flow-down. In any case, in a balanced design it is very 0
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A general force balance on the parts, as shown LO in Figure 1, results in the following equation: Fa Fp (Fb) (Ff) FU1 (Fs) FL FU2 (1) Applying the equation for the case where the valve is closing and ignoring the relatively small plug imbalance, yields the following: Fa Fp Fb Ff FU1 Fs FL (2) Note that Fb, Ff and Fs are all friction forces and that Ff (Packing Friction) can vary considerably. If spring force is subtracted from Fa, it yields the net force available in the actuator stem to 20 overcome the three friction forces and the pressure unbalance on the stem, and provide for sufficient seat load to limit through-leakage to acceptable levels.
Simplifying Equation 2 yields: (Fa Fp) Fn (net force) Ffr FU1 FL, (3) where Ffr Fb Ff Fs Examination of Equation 3 yields some interesting information. To successfully perform its duties, an actuator must be able to fully stroke the 'valve (usually with some velocity requirement) and load the seat to provide for proper shut-off. To fully stroke the valve, the net force available throughout the valve stroke must be slightly greater than (Ffr FU1) or the stem won't move. The difference between Fn and (Ffr FUl) together with the flow rate of the air 35 supply, determines the velocity of stem movement. In 1 i p
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i. u ;1 I--I 9 21-56(5574)A addition, the actuator must apply FL to provide a seat load sufficient to assure shut-off in the closed position. This means that even though the net force available agrees with the original actuator sizing calculations, if one of the frictional forces of FUI is too great, it would reduce the seat load and could even affect the ability of the valve to achieve full stroke. In equation form that is expressed as follows: Fn (Ffr FUl) FL (4) 10 With Fn constant, any increase in (Ffr FUl) result in a decrease in FL (seat load). Reduced seat load causes unnecessary leakage with a resultant "drop in process efficiency and possible trim damage.
In the same way, if Fn is too low even though 55.5 15 (Ffr FUI) is correct, the same problem results. Fn can be reduced if there is an insufficient air supply, or a spring that is adjusted too tightly or that has the wrong spring rate.
To avoid these problems and assure that the 20 actuator/valve assembly will properly perform, requires a verification of the forces shown in Equation 3. The apparatus and method of the present invention described hereinafter with respect to Figures 2-8 provides a valve diagnostic check-up in a very fast and reliable test 25 operation cycle. Several other useful diagnostic .o results are also obtained.
Referring now to Figure 2, there is illustrated a diagnostic controller 30 which provides a 0-30 mA signal output on channel 1 in either a programmed ramp or step change form to stroke or operate valve assembly 10 over a predetermined range and thereby provide respective sensor output signals on channels 2, 3, 4, 5, 6 to diagnostic controller 30. Information to be entered into controller 30 can be provided by keyboard 32 and the output information from controller
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can be coupled to a CRT display 34 as well as to a printer 36.
Valve assembly 10 includes valve body 38 having valve plug 18 connected to valve stem 16 and in turn connected through stem connector 20 to actuator stem 14. Actuator stem 14 is in turn connected to diaphragm plate 12 which is mounted within a spring barrel 40 by means of flexible diaphragm 42 to control the flow of fluid between the inlet and outlet ports 10 43,45 of valve body 38. Spring 22 normally biases plate 12 upwardly so that in the sliding stem valve illustrated in Figure 2, valve plug 18 is pulled up away from the valve seat so as to open the valve.
Actuation of the valve is provided by standard components including a current to pressure transducer 42 and a positioner 44 for supplying a controlled valve operating pressure at valve actuator input line 46.
Such a typical configuration includes a supply of pressurized air on pneumatic line 48 which is split and 20 fed through respective pneumatic lines through respective valves to the current to pressure (I/P) transducer as well as to valve positioner 44. Thus, input pneumatic line 50 to transducer 42 and input pneumatic line 52 to the valve positioner are each at the pneumatic supply pressure.
Normally, the signal input for controlling valve assembly 10 consists of a 4-20 mA signal on transducer input line 53 which will provide a corresponding output pressure of about 3-15 psi (0.21-1.06 kscm) on line 54 which is supplied to the controlled input of positioner 44. The output pressure of positioner 44 is supplied on line 56 to actuator pressure input line 46 in order to operate valve 10. A booster relay 58 may be provided when desired to increase the air volume. Booster relay 58 includes an A-^d
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input of supply line pressure on input line 60 to aid in proper operation of the valve actuator by positioner 44 under certain conditions. Valve positioner 44 also includes valve positioner arm 60 connected at one end to the actuator arm and at the other end within positioner 44 to provide valve position registration and thereby to insure that positioner 44 moves plug 18 the desired amount in response to changes in the input current to transducer 42.
10 Accordingly, under ordinary operations of valve assembly 10, with about a 4 mA signal input to transducer 42, the transducer provides about a 3 psi (0.21 kscm) input to positioner 44, which in turn provides a corresponding pressure on actuator input line 46 which is not sufficient to overcome spring 22 and the valve is therefore in the fully opened position. When the control current signal is raised to about 20 mA, transducer 42 provides about 15 psi (1.06 kscm) to positioner 44, which in turn provides a corresponding pressure input at line 46 to counteract spring 22 and thereby slide valve stem 16 downwardly so as to seat valve plug 18 and thereby close the valve. Obviously, various valve positions in between the fully opened and fully closed position are obtained by variations in the input 4-20 mA current signal to transducer 42.
In order to provide diagnostic evaluation of valve 10 in terms of the valve characteristics previously described, a suitable output signal from diagnostic controller 30 is provided on current signal output channel 1 to transducer 42. As an example, a 0 to 30 mA signal on channel 1 is sufficient to insure that the valve is stroked through its fully opened and fully closed positions. Less than the full range of valve operation may also be provided. Pressure sensors 70, 72, 74 and 76 are temporarily mounted to sense the c 0 0 *r 9
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li c Icc- 12 21-56(5574)A pneumatic pressure on the illustrated respective pneumatic lines and provide an electric output signal on respective input channels 2, 3, 4 and 5 to the diagnostic controller. Such pressure sensors are well known, commercially available items. If booster relay 58 is not present then sensor 74 is needed.
A position sensor 78 also is suitably temporarily removably mounted in the valve assembly to detect the linear positional movement of valve positioner arm 60 which corresponds to movement of valve **plug 18. Position sensor 78 provides a corresponding see electric output signal which is supplied to channel 6 of controller 30. Position sensor 78 is a commercially available device such as a digital linear gauge, 15 manufactured by Nititoyo Company of Japan utilizing a light source and an etched glass light sensor to provide a signal on channel 6 in response to linear movement of the valve plug.
Thus, as valve assembly 10 is stroked through S 20 its test operating cycle by means of its control current 056 signal on channel 1, a respective pressure is being sensed and the corresponding electric signals are fed to channels 2, 3, 4 and 5, and simultaneously the valve plug position and travel distance is being sensed and 25 the corresponding electric signal is supplied on channel 6. The usefulness of obtaining such pressure and valve S"plug position information can be seen with reference to the following Table 2.
Table 2 INPUT DESCRIPTIONS Channel Number Descriptions 2 Supply Pressure to the Positioner.
By monitoring this pressure, the user can verify that supply pressure is sufficient to provide full valve 13 21-56(5574)A stroke and seat load. He can also check for pressure decay during the stroke, which can slow actuator operation that is sometimes caused by restrictions in the supply pressure line.
3 Signal to the Positioner. This can be used to check proper I/P transducer calibration when compared with 10 channel 1 during valve stroke, since channel 2 is the input and channel 3 gee..is the output. At the same time, a second display can be generated showing the relationship between 15channel 3 and channel 5, permitting the user to verify positioner calibration.
4 Signal to Booster relay when present, checks booster input against lose. 20 booster output (channel 5) for proper operation.
Air-to-Diaphragm Signal. This is one of the key parameters that, when compared to channel 6 (valve position or travel), provides the force equation verification described with reference to equation 6 Valve Position or Travel. The second half of the force equation verification related to positional movement of the valve plug.
Figure 3 illustrates the components of diagnostic controller 30 which supply the 0-30 mA control signal on channel 1 to control valve assembly and receive the pressure related signals on channels 2,
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14 21-56(5574)A 3, 4, 5 and the valve travel distance information on channel 6. The pressure related signals are coupled through a bank of amplifiers 80, multiplexer 82, analog/digital converter 84 to microprocessor 86. The valve travel information on channel 6 is coupled to a counter 88 and then into microprocessor 86. A digital/ analog converter 90 converts the digital output of microprocessor 86 into the required analog control signal for channel i. Providing suitable microprocessor program instructions for controlling the acquisition of data and developing graphic output plots is well within o.0 the skills of an ordinary programmer in the art. A program for microprocessor 86 is presented in Appendix A.
15 Keypad 92 and liquid crystal display 96 are provided for inputting and outputting information to the microprocessor. Suitable disc drive and power supply components are provided.
Thus, as the valve assembly is stroked through its operating cycle, the corresponding pressure and A valve travel information on channels 2 through 6 are obtained by microprocessor 86 and can be displayed immediately, or stored for later processing and display in graphical form for suitable analysis of the valve 25 parameters. For example, the graphical plot of Figure 4 see: ee 0can be provided from information derived from channel and channel 6. Figure 4 illustrates the change in diaphragm pressure, i.e. the pressure at input line 46 as sensed by pressure sensor 76 as a function of the valve travel sensed by position sensor 78 and which I :information is supplied on channel 6 as the valve is r stroked from a fully open position near A at the lefthand side of Figure 4 to a fully closed position at the right-hand side of Figure 4 near C and then returned to a fully open position illustrated at the left-hand side r 1__1 .~111_ 15 21-56(5574)A of Figure 4 near A. Figure 4 allows the following valve parameters to be examined: Packing Seal and Bearing Friction Since friction acts in both valve operating directions, the friction valve can be determined by measuring the vertical width of the band (between the reference arrows labelled "Twice Friction"), dividing by two, and multiplying by the effective area of the diaphragm. The system will automatically calculate this quantity and compare it to normal levels stored in the diagnostic controller for the valve in question. Excessive friction levels can affect actuator operation as
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*described earlier. Friction values that are too low may .55i0 indicate insufficient load on the packing since packing friction is normally the largest of the three friction constituents.
Ge*(2) Benchset (Spring Adjustment and Spring •.oe Constant) The spring constant can be determined by computing the average slope of the curves from points A to C representing 10% to 90% of travel, and converting to force/distance units by using the effective diaphragm o area. Spring adjustment is checked by examining the loads at 10% to 90% of travel. Both the spring constant and adjustment can then be compared to normal values.
25 Seat Load Seat load is determined by measuring the pressure difference between points 1 and 2 on the curve. Point 1 is where the valve plug first ."contacts the seat, and is accompanied by a very radical change in slope. Point 2 is the maximum pressure on the diaphragm. Multiplying this pressure difference times the effective area of the diaphragm yields the seat load in force units, which can be compared to acceptable levels given valve size and service conditions.
Additional graphic plots utilizing the sensed valve parameter information can be prepared as
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X 16 21-56(5574)A illustrated in Figures 5 through 9. Figure 9 is a plot of the output pressure derived on channel 3 as a function of the input control current on channel 1 as the valve is stroked through a test operation cycle from open to close and returned to open. Figure 5 can be used to generate a deviation cycle thereby providing a complete picture of transducer 42 operation, including characteristics of linearity, hysterisis and range. The same type of calibration information for valve positioner 44 can be developed from Figure 6. Figure 6 represents the plot of information derived from valve plug movement or travel on channel 6 as a function of Sgoinput pressure on channel 3 during the valve test e operation cycle.
go 15 Figure 7 represents the valve travel informa- 0 tion on channel 6 and also the input current signal on channel 1 (either ramp, step-change or on-off) as a *000 function of time. Figure 7 allows one to verify the amount of valve travel and the stroking speed. Figure 8 is a plot of the supply pressure on channel 2 as a 60:0function of the valve distance on channel 6 during the valve test operation cycle. An evaluation of the plot of Figure 8 can be made so that the effect of supply pressure on valve stroking time can be evaluated.
o* 25 Accordingly, the valve diagnostic information provided in accordance with the present information and 0000 as illustrated for instance in Figures 4-8, enable those skilled in the art to very quickly determine where any valve problems occur and to take appropriate action to remedy such problems before they cause extensive valve damage or, in the worse case, a forced system shutdown. Extensive use of the present invention in a fluid control system as part of a preventative maintenance program should greatly reduce the expenditures associated with valve maintenance as well as improve system reliability and availability.
17 21-56(5574)A It is to be understood that the valve test operation cycle can be run from the open to the closed and again to the open position or vice versa. In addition, less than all of the test operation cycle may be run in accordance with the present invention in order to provide useful valve output diagnostic information.
As an example, in Figure 4, valuable seat load information is determined between points 1 and 2 on the illustrated curve and the valve need only be stroked in order to encompass these two points. Therefore either a partial or a full cycle may be utilized.
In addition, while the illustrated embodiment of this invention is in connection with sliding stem valves, it is to be understood that the same principles 15 apply as well to other types of valves such as rotary discs or balls. Similarly, rather than detecting the "ur. position and thereby the valve travel by detecting the movement of positioner arm 60, or of valve stem 16 or of actuator stem 14, the movement of any other part associated with the movement of valve plug 18 can be utilized. As an example, one could if desired detect linear movement of diaphragm plate 12 since the plate is integrally connected to and therefore moves integrally .with valve plug 18. Sensors 70, 72, 74, 76 can be located in diagnostic controller 30 and connected to the respective pneumatic lines through suitable air lines if desired.
v fo The foregoing detailed description has been Sgiven for clearness of understanding only, and no 30 unnecessary limitations should be understood therefrom, as modifications will be obvious to those skilled in the art, within the scope of the following claims.
The matter contained in each. of the following claims is to be read as part of the. general description of the present invention.
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Claims (7)
1. Apparatus for diagnostically testing and deter- mining the operating condition of a pneumatically operated fluid control valve, said valve having a pneumatic actuator interconnected to a valve flow control member for moving the flow control member between respective closed and open valve positions with respect to a valve seat, and a variable pneumatic pressure line connected to a valve positioner providing a variable pneumatic pressure output to the input of the pneumatic actuator for operating said valve in a test operation cycle defined by moving the flow control member along at least a portion of the movement between said respective closed and open valve positions, said apparatus comprising: 15 first transducer means operative to sense the pneumatic pressure at the input of the pneumatic actuator during said test operation cycle and provide a corresponding first output signal for flow control member movements encompassing the 20 fully closed valve position wherein said flow control member is seated on the valve seat; second transducer means operative to sense the movement of the flow control member during said test operation cycle, and provide a second output signal for flow control member movements encompassing the fully closed valve position; signal processing means responsive to said first and second output signals to provide valve diagnostic data corresponding to variations in T~rO I 19 -i ':1 the pneumatic pressure at the input to the pneumatic actuator as a function of the movement of the flow control member during a portion of said test operation cycle corresponding to flow control member movements encompassing the fully closed valve position; and output display means coupled to said signal processing means and operative to display said valve diagnostic data and thereby enable determination of valve seat load values for said valve under test; said output display means including means operative to display a substantially linear relationship in said pneumatic pressure as a function of flow control member travel during said test operation cycle and display at least two pneumatic pressure values at the end of the test operation cycle corresponding to closing of the valve as the flow control member initially contacts the valve seat and is then totally seated against the valve seat, said two pneumatic pressure valves including a pressure value at the point in flow control member travel where the pneumatic pressure abruptly changes from said linear relationship and a pressure value at the point in the flow control member travel where the maximum pneumatic pressure value is reached, and the pressure abruptly changes as the flow control membertravel direction is reversed. -r 20 5
2. A method for diagnostically testing and determin- ing the operating condition of a pneumatically operated fluid control valve having a valve actuator connected to a valve flow control member for movement between respective closed and open valve positions with respect to a valve seat, comprising the steps of: providing a pressure sensor to sense varying pressure at the input of the valve actuator; providing a position sensor to sense movement of the flow control member; providing controlled variable pneumatic pressure to the input of the valve actuator to operate the valve in a test operation cycle defined by moving the flow control member along at least a portion of the movement between said respective closed and open valve positions; obtaining a first signal from the pressure sensor corresponding to varying pressure at the valve actuator input during the test operation cycle for flow control member movements encompassing the fully closed valve position wherein said flow control member is seated on the valve seat; obtaining a second signal from the position sensor corresponding to movement of the flow control member during the test operation cycle for flow control member movements encompassing the fully closed valve position; I L.n -21- processing said first and second signals to derive vallre diagnostic data representing the variation in pressure at the valve actuator input as a function of movement of the flow control member during the test operation cycle corres- ponding to flow control member movements encomp- assing the fully closed valve position; and displaying said valve diagnostic data for enabling determination of valve seat load values for said valve under test; including the steps of displaying at least two S: pneumatic pressure values at the end of the test operation cycle corresponding to closing of the valve as the flow control member initially contacts the valve seat an' is then totally seated against the valve seat, said two pneumatic pressure values including a pressure value at the first point in flow control member travel j where the pneumatic pressure initially abruptly S20 changes in value at the end of the test operation cycle and a pressure value at the second point in the continued travel of the flow control member where the maximum pneumatic pressure value is reached and the pressure again abruptly changes as the flow control member travel direction is reversed.
3. Apparatus for diagnostically testing and deter- mining the operating condition of a pneumatically operated valve, said valve having a pneumatic actuator driving an interconnected actuator stem, valve stem, and valve plug for moving the valve plug into and out of sealing engage- ment with the valve seat corresponding to respective closed l 22 and open valve positions, and a variable pneumatic pressure line connected to a valve positioner providing a variable pneumatic pressure output to the input of the pnuematic actuator ftr operating said valve in a test operation cycle defined by moving the valve plug from a fully open position to a fully closed position and from said fully closed position to a fully open position, said apparatus comprising: first transducer means operative to sense the pneumatic pressure at the input of the pneumatic actuator during said test operation cycle and provide a corresponding first output signal *sees: second transducer means operative tc sense the 15 movement of the valve plug during said test operation cycle, and provide a second output signal (ch.6); signal processing means responsive to said first ee and second output signals to provide valve 20 diagnostic data corresponding to variations in the pneumatic pressure at the input to the :pneumatic actuator as a function of the movement of the valve plug during said test operation cycle; 25 third transducer means operative to sense the pneumatic pressure at the variable pneumatic pressure line during said test operation cycle and provide a corresponding third output signal and Ip I~ I- 23 wherein said signal processing means is res- ponsive to said second and third output signals to provide valve diagnostic data corresponding to movement of the valve plug (ch.6) as a function of variations in said variable pneumatic pressure line (ch.3) during said test operation cycle.
4. Apparatus according to claim 3, including a current to pressure transducer having a variable control current signal input (ch.l) and a variable pneumatic pressure output coupled to the variable pneumatic pressure line connected to the valve positioner; and wherein said signal processing means is res- ponsive to said variable control current signal and to said third output signal to provide valve "15 diagnostic data corresponding to variations in said variable pneumatic pressure line connected to the valve positioner (ch.3) as a function of said variable control signal (ch.l) during said test operation cycle.
5. Apparatus according to claim 4, including display •I means operative to.display said valve diagnostic data and enable determination of at least valve friction values, valve seat load values, valve positioner calibration values and current to pressure transducer calibration values for said valve under test.
6. Apparatus according to claim 1 or 3, substantial- ly as described herein'with reference to the embodiment 1 illustrated in Fig. 2 of the accompanying drawings. i 'I' I 24
7. The method according to claim 2, substantially as described herein with reference to the embodiment illustra- ted in Fig. 3 of the accompanying drawings. DATED this 28th day of October, 1992 0 0 0 0 0 00 000000 *00* 0 FISHER CONTROLS INTERNATIONAL, INC., By its Patent Attorneys, E. F. WELLINGTON CO., By: S. Wellington) .00. 0 0 0 A/RR/1523/7 11 ii
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US23660288A | 1988-08-25 | 1988-08-25 | |
US236602 | 1994-05-02 |
Publications (2)
Publication Number | Publication Date |
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AU4018889A AU4018889A (en) | 1990-03-01 |
AU632759B2 true AU632759B2 (en) | 1993-01-14 |
Family
ID=22890176
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU40188/89A Ceased AU632759B2 (en) | 1988-08-25 | 1989-08-24 | Diagnostic apparatus and method for fluid control valves |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU632759B2 (en) |
CA (1) | CA1335943C (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007020597A1 (en) * | 2007-05-02 | 2009-01-02 | Siemens Ag | Method for checking the functionality of a positioning device |
CN108730266B (en) * | 2018-07-03 | 2023-07-18 | 徐州金鼎恒立液压件有限公司 | Device and method for measuring internal leakage of hydraulic cylinder |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3098382A (en) * | 1960-03-04 | 1963-07-23 | Lockheed Aircraft Corp | Hydraulic test equipment |
US4523286A (en) * | 1981-08-07 | 1985-06-11 | Hitachi, Ltd. | Apparatus for making diagnosis of valve device in turbine system |
EP0264148A1 (en) * | 1986-10-08 | 1988-04-20 | Pumptech N.V. | Flow measurement and monitoring system for positive-displacement pumps and pumps equipped with this system |
-
1989
- 1989-08-24 CA CA000609370A patent/CA1335943C/en not_active Expired - Lifetime
- 1989-08-24 AU AU40188/89A patent/AU632759B2/en not_active Ceased
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3098382A (en) * | 1960-03-04 | 1963-07-23 | Lockheed Aircraft Corp | Hydraulic test equipment |
US4523286A (en) * | 1981-08-07 | 1985-06-11 | Hitachi, Ltd. | Apparatus for making diagnosis of valve device in turbine system |
EP0264148A1 (en) * | 1986-10-08 | 1988-04-20 | Pumptech N.V. | Flow measurement and monitoring system for positive-displacement pumps and pumps equipped with this system |
Also Published As
Publication number | Publication date |
---|---|
CA1335943C (en) | 1995-06-20 |
AU4018889A (en) | 1990-03-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK14 | Patent ceased section 143(a) (annual fees not paid) or expired |