Flow measurement with diagnostics

Information

  • Patent Grant
  • 6654697
  • Patent Number
    6,654,697
  • Date Filed
    Friday, August 27, 1999
    25 years ago
  • Date Issued
    Tuesday, November 25, 2003
    20 years ago
Abstract
A fluid flow meter diagnosing the condition of its primary element or impulse lines connecting to a differential pressure sensor. A difference circuit coupled to the differential pressure sensor has a difference output representing the sensed differential pressure minus a moving average. A calculate circuit receives the difference output and calculates a trained output of historical data obtained during an initial training time. The calculate circuit also calculates a monitor output of current data obtained during monitoring or normal operation of the fluid flow meter. A diagnostic circuit receives the trained output and the monitor put and generates a diagnostic output indicating a current condition of the primary element and impulse lines.
Description




BACKGROUND OF THE INVENTION




Fluid flow meters are used in industrial process control environments to measure fluid flow and provide flow signals for flow indicators and controllers. Inferential flow meters measure fluid flow in a pipe by measuring a pressure drop near a discontinuity within the pipe. The discontinuity (primary element) can be an orifice, a nozzle, a venturi, a pitot tube, a vortex shedding bar, a target or even a simple bend in the pipe. Flow around the discontinuity causes both a pressure drop and increased turbulence. The pressure drop is sensed by a pressure transmitter (secondary element) placed outside the pipe and connected by impulse lines or impulse passageways to the fluid in the pipe. Reliability depends on maintaining a correct calibration. Erosion or buildup of solids on the primary element can change the calibration. Impulse lines can become plugged over time, which also adversely affects calibration.




Disassembly and inspection of the impulse lines is one method used to detect and correct plugging of lines. Another known method for detecting plugging is to periodically add a “check pulse” to the measurement signal from a pressure transmitter. This check pulse causes a control system connected to the transmitter to disturb the flow. If the pressure transmitter fails to accurately sense the flow disturbance, an alarm signal is generated indicating line plugging. Another known method for detecting plugging is sensing of both static and differential pressures. If there is inadequate correlation between oscillations in the static and differential pressures, then an alarm signal is generated indicating line plugging. Still another known method for detecting line plugging is to sense static pressures and pass them through high pass and low pass filters. Noise signals obtained from the filters are compared to a threshold, and if variance in the noise is less than the threshold, then an alarm signal indicates that the line is blocked.




These known methods rely on providing static pressure sensors or disassembly of the flow meter or use of an external control system for diagnostics, increasing complexity and reducing reliability. These known methods do not provide for diagnosing the condition of the primary element. There is thus a need for a better diagnostic technology providing more predictive, less reactive maintenance for reducing cost or improving reliability.




SUMMARY OF THE INVENTION




A fluid flow meter diagnoses the condition of its primary element or impulse lines. The primary element and the impulse lines together form a differential pressure generator. This differential pressure generator generates a differential pressure that represents the flow rate. The differential pressure is coupled to a differential pressure sensor in the fluid flow meter.




A difference circuit coupled to the differential pressure sensor generates a difference output representing the sensed differential pressure minus a moving average of the sensed differential pressure.




A calculate circuit receives the difference output and calculates a trained output of historical data obtained during an initial training time. The calculate circuit also calculates a monitor output of current data obtained during monitoring or normal operation of the fluid flow meter.




A diagnostic circuit receives the trained output and the monitor output and generates a diagnostic output indicating a current condition of the pressure generator relative to an historical condition.




A flow circuit is also coupled to the sensor and generates an output indicating the flow rate.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is an illustration of a typical fluid processing environment for the diagnostic flow meter.





FIG. 2

is a pictorial illustration of an embodiment of a transmitter used in a fluid flow meter that diagnoses the condition of its impulse lines and/or primary element.





FIG. 3

is a block diagram of a fluid flow meter that diagnoses a condition of its pressure generator.





FIG. 4

is a block diagram of a fluid flow meter that diagnoses the condition of its impulse lines.





FIG. 5

is a block diagram of a fluid flow meter that diagnoses the condition of its primary element.





FIG. 6

is a flow chart of a process diagnosing the condition of impulse lines.





FIG. 7

illustrates a diagnostic fluid flow meter that has a pitot tube for a primary element.





FIG. 8

illustrates a diagnostic fluid flow meter that has an in-line pitot tube for a primary element.





FIG. 9

illustrates a diagnostic fluid flow meter that has an integral orifice plate for a primary element.





FIG. 10

illustrates a diagnostic fluid flow meter than has an orifice plate clamped between pipe flanges for a primary element.





FIG. 11

illustrates a diagnostic fluid flow meter that has a venturi for a primary element.





FIG. 12

illustrates a diagnostic fluid flow meter that has a nozzle for a primary element.





FIG. 13

illustrates a diagnostic fluid flow meter that has an orifice plate for a primary element.





FIG. 14

is a flow chart of a process of diagnosing the condition of a primary element.





FIG. 15

is a flow chart of a process of diagnosing the condition of both impulse lines and a primary element.





FIG. 16

is an illustration of a transmitter with remote seals and diagnostics.





FIG. 17

is a schematic illustration of a transmitter with diagnostic features connected to a tank to measure a time integral of flow in and out of the tank.





FIG. 18

is a graph of amplitude versus frequency versus time of a process variable signal.





FIG. 19

is a block diagram of a discrete wavelet transformation.





FIG. 20

is a graph showing signals output from a discrete wavelet transformation.





FIG. 21

is a diagram showing a simplified neural network.





FIG. 22A

is a diagram showing a neural network used to provide a residual lifetime estimate.





FIG. 22B

is a graph of residual life versus time.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




In

FIG. 1

, a typical environment for diagnostic flow measurement is illustrated at


220


. In

FIG. 1

, process variable transmitters such as flow meter


230


, level transmitters


232


,


234


on tank


236


and integral orifice flow meter


238


are shown connected to control system


240


. Process variable transmitters can be configured to monitor one or more process variables associated with fluids in a process plant such as slurries, liquids, vapors and gasses in chemical, pulp, petroleum, gas, pharmaceutical, food and other fluid processing plants. The monitored process variables can be pressure, temperature, flow, level, pH, conductivity, turbidity, density, concentration, chemical composition or other properties of fluids. Process variable transmitter includes one or more sensors that can be either internal to the transmitter or external to the transmitter, depending on the installation needs of the process plant. Process variable transmitters generate one or more transmitter outputs that represent the sensed process variable. Transmitter outputs are configured for transmission over long distances to a controller or indicator via communication busses


242


. In typical fluid processing plants, a communication buss


242


can be a 4-20 mA current loop that powers the transmitter, or a fieldbus connection, a HART protocol communication or a fiber optic connection to a controller, a control system or a readout. In transmitters powered by a 2 wire loop, power must be kept low to provide intrinsic safety in explosive atmospheres.




In

FIG. 1

, integral orifice flow meter


238


is provided with a diagnostic output which is also coupled along the communication bus


242


connected to it. Control system


240


can be programmed to display the diagnostic output for a human operator, or can be programmed to alter its operation when there is a diagnostic warning from flow meter


238


. Control system


240


controls the operation of output devices such as control valve


244


, pump motors or other controlling devices.




In

FIG. 2

, an exploded view of a typical diagnostic transmitter


82


according to the present invention is shown generally. Transmitter


82


includes a flange


83


for receiving a differential pressure, a differential pressure sensor


31


, electronics including an analog to digital converter


84


, a microprocessor system


88


, a digital to analog converter


96


, and a digital communications circuit


100


. Transmitter


82


is bolted to flange adapter


87


. Microprocessor


88


is programmed with diagnostic algorithms as explained by examples shown in

FIGS. 3

,


6


,


14


and


15


. Flange adapter


87


connects to impulse pipes which, in turn, connect to flow around a primary flow element (not shown in FIG.


2


). The arrangement of transmitter


82


of

FIG. 2

is explained in more detail in FIG.


3


.




In

FIG. 3

, a block diagram shows a first embodiment of a fluid flow meter


80


adapted to sense fluid flow


22


in pipe


24


. Fluid flow meter


80


includes a pressure generator


26


that includes a primary element


28


and impulse lines


30


that couple pressures generated in the fluid flow around the primary element


28


to a differential pressure sensor


31


in a pressure transmitter


82


. The term “pressure generator” as used in this application means a primary element (e.g., an orifice plate, a pitot tube, a nozzle, a venturi, a shedding bar, a bend in a pipe or other flow discontinuity adapted to cause a pressure drop in flow) together with impulse pipes or impulse passageways that couple the pressure drop from locations near the primary element to a location outside the flow pipe. The spectral and statistical characteristics of this pressure presented by this defined “pressure generator” at a location outside the flow pipe to a connected pressure transmitter


82


can be affected by the condition of the primary element as well as on the condition of the impulse pipes. The connected pressure transmitter


82


can be a self-contained unit, or it can be fitted with remote seals as needed to fit the application. A flange


83


on the pressure transmitter


82


(or its remote seals) couples to a flange adapter


87


on the impulse lines


30


to complete the pressure connections. Pressure transmitter


82


couples to a primary flow element


28


via impulse lines


30


to sense flow. The pressure transmitter


82


comprises a differential pressure sensor


31


adapted to couple to the impulse lines


30


via a flange arrangement. An analog to digital converter


84


couples to the pressure sensor


31


and generates a series of digital representations of the sensed pressure at


86


. A microprocessor system


88


receives the series of digital representations of pressure at


86


and has a first algorithm


90


stored therein calculating a difference between the series of digital representations


86


and a moving average of the series of digital representations. A second algorithm


92


is also stored in the microprocessor system


88


that receives the difference calculated by algorithm


90


and calculates a trained data set of historical data during a training mode and calculates a current data set during a monitoring mode and generates diagnostic data


94


as a function of the current data set relative to the historical data indicating changes in the condition of pressure generator


26


. A digital to analog converter


96


coupled to the microprocessor system


88


generates an analog transmitter output


98


indicative of the sensed flow rate. A digital communication circuit


100


receives the diagnostic data


94


from the microprocessor system


88


and generates a transmitter output


102


indicating the diagnostic data. The analog output


98


and the diagnostic data


102


can be coupled to indicators or controllers as desired.




In

FIG. 4

, a block diagram shows a further embodiment of a fluid flow meter


20


adapted to sense fluid flow


22


in pipe


24


. The fluid flow meter


20


in

FIG. 4

is similar to the fluid flow meters


80


of FIG.


3


and the same reference numerals used in

FIGS. 3

are also used in

FIG. 4

for similar elements. Fluid flow meter


20


includes a pressure generator


26


that includes a primary element


28


and impulse lines


30


that couple pressures generated in the fluid flow around the primary element


28


to a differential pressure sensor


31


in a pressure transmitter


32


. The pressure transmitter


32


can be a self-contained unit, or it can be fitted with remote seals as needed to fit the application. A flange on the pressure transmitter


32


(or its remote seals) couples to a flange adapter on the impulse lines


30


to complete the pressure connections. A flow circuit


34


in the pressure transmitter


32


couples to the sensor


31


and generates a flow rate output


36


that can couple to a controller or indicator as needed.




In

FIG. 4

, a difference circuit


42


couples to the sensor


31


and generates data at a difference output


44


representing the sensed pressure minus a moving average. A calculate circuit


46


receives the difference output


44


and calculates a trained output


48


of historical data obtained during a training mode or time interval. After training, calculate circuit


46


calculates a monitor output


50


of current data obtained during a monitoring mode or normal operation time of the fluid flow meter


20


.




In

FIG. 4

, a diagnostic circuit


52


receives the trained output


48


and the monitor output


50


and generating a diagnostic output


54


indicating a current condition of the pressure generator


26


relative to an historical condition. In

FIG. 4

, calculate circuit


46


stores the historical data in circuit


56


which includes memory.




In difference circuit


42


, the moving average is calculated according to the series in Eq. 1:










A
j

=




k
=
0

m








(

P

j
+
k


)



(

W
k

)







Eq
.




1













where A is the moving average, P is a series of sequentially sensed pressure values, and W is a numerical weight for a sensed pressure value, m is a number of previous sensed pressure values in the series. Provision can also be made in difference circuit


42


to filter out spikes and other anomalies present in the sensed pressure. In

FIG. 4

, the historical data comprises statistical data, for example, the mean (μ) and standard deviation (σ) of the difference output or other statistical measurements, and the diagnostic output


54


indicates impulse line plugging. The calculate circuit


46


switches between a training mode when it is installed and a monitoring mode when it is in use measuring flow. The calculate circuit


46


stores historical data in the training mode. The diagnostic output


54


indicates a real time condition of the pressure generator


26


.




In

FIG. 4

, statistical data, such as the mean μ and standard deviation μ, are calculated based on a relatively large number of data points or flow measurements. The corresponding sample statistical data, such as sample mean


X


and sample standard deviation s, are calculated from a relatively smaller number of data points. Typically, hundreds of data points are used to calculate statistical data such as μ and σ, while only about 10 data points are used to calculate sample statistical data such as


X


and s. The number of data points during monitoring is kept smaller in order to provide diagnostics that is real time, or completed in about 1 second. Diagnostic circuit


52


indicates line plugging if the sample standard deviation s deviates from the standard deviation a by a preset amount, for example 10%.




In

FIG. 5

, a fluid flow meter


60


is shown that diagnoses the condition of the primary element


28


. The fluid flow meter


60


in

FIG. 5

is similar to the fluid flow meter


20


of FIG.


4


and the same reference numerals used in

FIG. 4

are also used in


5


for similar elements. In


5


, the diagnostic output


62


indicates a condition of the primary element


28


, while in

FIG. 4

, the diagnostic output indicates a condition of the impulse lines


30


. In

FIG. 5

, calculate circuit


46


calculates and stores data on power spectral density (PSD) of the difference output


44


rather than statistical data which is used in FIG.


4


. The power spectral density data is preferably in the range of 0 to 100 Hertz. The center frequency of a bandpass filter can be swept across a selected range of frequencies to generate a continuous or quasi-continuous power spectral density as a function of frequency in a manner that is well known. Various known Fourier transforms can be used.




Power spectral density, Fi, can also be calculated using Welch's method of averaged periodograms for a given data set. The method uses a measurement sequence x(n) sampled at fs samples per second, where n=1, 2, . . . N. A front end filter with a filter frequency less than fs/2 is used to reduce aliasing in the spectral calculations. The data set is divided into F


k,i


as shown in Eq. 2:










F

k
,
i


=


(

1
/
M

)




&LeftBracketingBar;




n
=
1

M









x
k



(
n
)







-
j







2
π








Δ





fn




&RightBracketingBar;

2






Eq
.




2













There are F


k,i


overlapping data segments and for each segment, a periodogram is calculated where M is the number of points in the current segment. After all periodograms for all segments are evaluated, all of them are averaged to calculate the power spectrum:









Fi
=


(

1
/
L

)






k
=
1

L







F

k
,
i








Eq
.




3













Once a power spectrum is obtained for a training mode, this sequence is stored in memory, preferably EEPROM, as the baseline power spectrum for comparison to real time power spectrums. Fi is thus the power spectrum sequence and i goes from 1 to N which is the total number of points in the original data sequence. N, usually a power of 2, also sets the frequency resolution of the spectrum estimation. Therefore, Fi is also known as the signal strength at the i


th


frequency. The power spectrum typically includes a large number points at predefined frequency intervals, defining a shape of the spectral power distribution as a function of frequency.




In the detection of the primary element degradation, a relatively larger sample of the spectral density at baseline historical conditions and a relatively smaller sample of the spectral density at monitoring conditions are compared. The relatively smaller sample allows for a real time indication of problems in about 1 second. An increase in the related frequency components of the power spectrum can indicate the degradation of the primary element. Using orifice plates as primary elements, for example, changes as high as 10% are observed in spectral components when the orifice plate is degraded to a predetermined level. The amount of change can be adjusted as needed, depending on the tolerable amount of degradation and the type of primary element in use. The amount of change needed to indicate a problem is arrived at experimentally for each type of primary element arrangement. Fuzzy logic can also be used to compare the many points of the power spectrums.




In

FIG. 6

, a flow chart


120


of a method of diagnosis performed in a pressure transmitter couplable to a primary flow element via impulse lines is shown. The algorithm starts at


122


. A moving average is subtracted from differential pressure data as shown at


124


to calculate a difference. During a train mode, historical data on the calculated difference is acquired and stored at


126


as statistical data μ and μ, for example. During an operational MONITOR mode, current data on the difference is acquired and stored at


128


as statistical data


X


and s. The smaller sample of current data is compared to the larger sample of the historical data to diagnose the condition of the impulse lines. Comparisons of historical and current statistical data are made at


132


,


134


,


136


and a selected diagnostic transmitter output is generated at


138


,


140


,


142


as a function of the comparisons made at


130


,


132


,


134


,


136


respectively. After completion of any diagnostic output, the process loops back at


144


to repeat the monitor mode diagnostics, or the transmitter can be shut down until maintenance is performed. If the diagnostic process itself fails, an error indication is provided on the diagnostic output at


146


. In the method


120


of diagnosis, the historical data set comprises statistical data such as data on the mean (μ) and standard deviation (σ) of the calculated difference; the current data set comprises current sample statistical data, such as the sample average (


X


) and sample deviation (s) of the calculated difference. The sample deviation (s) is compared to the standard deviation (σ) to diagnose impulse line plugging, for example. Other known statistical measures of uncertainty, or statistical measures developed experimentally to fit this application can also be used besides mean and standard deviation. When there is an unusual flow condition where


X


is much different than μ, the diagnostics can be temporarily suspended as shown at


130


until usual flow conditions are reestablished. This helps to prevent false alarm indications.




In

FIGS. 2-5

, the transmitter generates a calibrated output and also a diagnostic output that indicates if the pressure generator is out of calibration. In

FIGS. 2-5

, the primary element can comprise a simple pitot tube or an averaging pitot tube. The averaging pitot tube


63


can be inserted through a tap


64


on a pipe as shown in FIG.


7


. An instrument manifold


66


, as shown in

FIG. 8

, can be coupled between the pressure generator


26


and a pressure transmitter


68


. The primary element


28


and impulse pipes


30


can be combined in an integral orifice as shown in FIG.


9


. An orifice plate adapted for clamping between pipe flanges is shown in FIG.


10


. The primary element can comprise a venturi as shown in

FIG. 11

or a nozzle as shown in

FIG. 12

, or an orifice as shown in

FIG. 13. A

standard arrangement of a pressure generator can be used with a transmitter that is adapted to provide the diagnostics outputs. The transmitter adapts itself to the characteristics of the pressure generator during the training mode and, has a standard of comparison stored during the training mode that is available for comparison during the monitoring or operational mode. The standard of comparison can be adjusted as needed by a technician via the digital communication bus. In each arrangement, the fluid flow meter provides a calibrated flow rate output and the diagnostic output of the transmitter indicates if the pressure generator is out of calibration.




In

FIG. 14

, a flow chart


160


of a process for diagnosing the condition of a primary element is shown. The condition of the primary element can include erosion or fouling of the primary element. The method or algorithm starts at


162


. Sensor data is taken in a training mode or time interval as shown at


164


. A power spectrum of the sensor data, minus the moving average, is calculated at


166


. The power spectrum obtained is identified as the training power spectrum at


168


and stored in non-volatile memory


170


. After completion of training, the process moves on to monitoring or normal use. A further power spectrum of current sensor data, minus the moving average, is evaluated at


172


, and the power spectrum so obtained in stored in memory


174


, that can be either RAM or nonvolatile memory. At


176


, the power spectrum Fi obtained during training is compared to the power spectrum


Fi


obtained during monitoring. If there is a significant difference between Fi and


Fi


which is indicative of a problem with the primary element, a primary element warning (PE Warning) is generated as shown at


178


. If the power spectrums Fi and


Fi


are sufficiently similar, then no primary element warning is generated. After the comparison at


176


and generation of a PE Warning, as needed, program flow moves to obtain new real time sensor data at


180


and the monitoring process moves on to a new evaluation at


172


, or the flow meter can shut down when there is a PE warning. The process


160


can loop continuously in the monitoring mode to provide real time information concerning the condition of the primary element.




In

FIG. 15

, a flow chart illustrates a process


190


which provides diagnosis of both primary element (PE) and impulse lines (IL). Program flow starts at


200


. During a training mode illustrated at


202


, sensor data, minus a moving average, is obtained and training power spectrum and training statistics are stored in nonvolatile memory as explained above. Next, impulse line diagnostics (such as those explained in process


128


in

FIG. 6

) are performed at step


204


in FIG.


15


. In

FIG. 15

, after impulse line diagnostics are performed, current impulse line statistics are compared to historical (training) impulse line statistics (as detailed in processes


130


,


132


,


134


,


136


in

FIG. 6

) at


206


. If the comparison indicates a problem with plugging of impulse lines, then an impulse line warning is generated as shown at


208


. If no problem with the impulse lines is apparent, then program flow moves on to primary element (PE) diagnostics at


210


. At process


210


, power spectral density for the current real time data is calculated (as explained above in connection with FIG.


14


). The current power spectral density is compared to the historical power spectral density at


212


, and if there is a difference large enough to indicate a problem with the primary element, then a PE Warning is generated as shown at


214


. If the differences in the power spectral densities are small, then no PE warning is generated as shown at


216


. Program flow continues on at


218


to repeat the IL and PE diagnostics, or the flow meter can be shut down if there is a PE or IL warning until maintenance is performed.




Any of the methods can be stored on a computer-readable medium as a plurality of sequences of instructions, the plurality of sequences of instructions including sequences that, when executed by a microprocessor system in a pressure transmitter cause the pressure transmitter to perform a diagnostic method relative to a primary element and impulse lines couplable to the transmitter.





FIG. 16

illustrates a transmitter


230


which includes remote seals


232


,


234


connected by flexible capillary tubes


236


,


238


that are filled with a controlled quantity of isolation fluid such as silicon oil. The isolator arrangement permits placement of the sensor and electronics of transmitter


230


to be spaced away from extremely hot process fluids which contact the remote seals. The diagnostic circuitry of transmitter


230


can also be used to detect leaking and pinching off of capillary tubes


236


,


238


using the diagnostic techniques described above to provide diagnostic output


239


.





FIG. 17

schematically illustrates a transmitter


240


which is connected to taps


248


,


250


near the bottom and top of tank


242


. Transmitter


240


provides an output


244


that represents a time integral of flow in and out of the tank


242


. Transmitter


240


includes circuitry, or alternatively software, that measures the differential pressure between the taps


248


,


250


and computes the integrated flow as a function of the sensed differential pressure and a formula stored in the transmitter relating the sensed pressure to the quantity of fluid in the tank. This formula is typically called a strapping function and the quantity of fluid which has flowed into or out of the tank can be integrated as either volumetric or mass flow, depending on the strapping function stored in transmitter


240


. The diagnostic circuitry or software in transmitter


240


operates as explained above to provide diagnostic output


252


.

FIG. 17

is a schematic illustration, and transmitter


240


can be located either near the bottom or the top of tank


242


, with a tube going to the other end of the tank, often called a “leg.” This leg can be either a wet leg filled with the fluid in the tank, or a dry leg filled with gas. Remote seals can also be used with transmitter


240


.




In one embodiment, microprocessor system


88


includes signal preprocessor which is coupled to sensor


88


through analog to digital converter


84


which isolates signal components in the sensor signal such as frequencies, amplitudes or signal characteristics which are related to a plugged impulse line


30


or degraded primary element


28


. The signal preprocessor provides an isolated signal output to a signal evaluator in microprocessor


88


. The signal preprocessor isolates a portion of the signal by filtering, performing a wavelet transform, performing a Fourier transform, use of a neural network, statistical analysis, or other signal evaluation techniques. Such preprocessing is preferably implemented in microprocessor


88


or in a specialized digital signal processor. The isolated signal output is related to a plugged or plugging impulse line


30


or degraded primary element


28


sensed by sensor


31


.




The signal components are isolated through signal processing techniques in which only desired frequencies or other signal characteristics such as amplitude are identified and an indication of their identification is provided. Depending upon the strength signals to be detected and their frequency, signal preprocessor can comprise a filter, for example a band pass filter, to generate the isolated signal output. For more sensitive isolation, advanced signal processing techniques are utilized such as a Fast Fourier transform (FFT) to obtain the spectrum of the sensor signal. In one preferred embodiment, the signal preprocessor comprises a wavelet processor which performs a wavelet analysis on the sensor signal as shown in

FIGS. 18

,


19


and


20


using a discrete wavelet transform. Wavelet analysis is well suited for analyzing signals which have transients or other non-stationary characteristics in the time domain. In contrast to Fourier transforms, wavelet analysis retains information in the time domain, i.e., when the event occurred.




Wavelet analysis is a technique for transforming a time domain signal into the frequency domain which, like a Fourier transformation, allows the frequency components to be identified. However, unlike a Fourier transformation, in a wavelet transformation the output includes information related to time. This may be expressed in the form of a three dimensional graph with time shown on one axis, frequency on a second axis and signal amplitude on a third axis. A discussion of wavelet analysis is given in


On-Line Tool Condition Monitoring System With Wavelet Fuzzy Neural Network


, by L. Xiaoli et al., 8 JOURNAL OF INTELLIGENT MANUFACTURING pgs. 271-276 (1997). In performing a continuous wavelet transformation, a portion of the sensor signal is windowed and convolved with a wavelet function. This convolution is performed by superimposing the wavelet function at the beginning of a sample, multiplying the wavelet function with the signal and then integrating the result over the sample period. The result of the integration is scaled and provides the first value for continuous wavelet transform at time equals zero. This point may be then mapped onto a three dimensional plane. The wavelet function is then shifted right (forward in time) and the multiplication and integration steps are repeated to obtain another set of data points which are mapped onto the 3-D space. This process is repeated and the wavelet is moved (convolved) through the entire signal. The wavelet function is then scaled, which changes the frequency resolution of the transformation, and the above steps are repeated.




Data from a wavelet transformation of a sensor signal from sensor


31


is shown in FIG.


18


. The data is graphed in three dimensions and forms a surface


270


. As shown in the graph of

FIG. 18

, the sensor signal includes a small signal peak at about 1 kHz at time t


1


and another peak at about 100 Hz at time t


2


. Through subsequent processing by the signal evaluator, surface


270


or portions of surface


270


are evaluated to determine impulse piping or primary element degradation.




The continuous wavelet transformation described above requires extensive computations. Therefore, in one embodiment, microprocessor


88


performs a discrete wavelet transform (DWT) which is well suited for implementation in microprocessor system. One efficient discrete wavelet transform uses the Mallat algorithm which is a two channel sub-band coder. The Mallet algorithm provides a series of separated or decomposed signals which are representative of individual frequency components of the original signal.

FIG. 19

shows an example of such a system in which an original sensor signal S is decomposed using a sub-band coder of a Mallet algorithm. The signal S has a frequency range from 0 to a maximum of f


MAX


. The signal is passed simultaneously through a first high pass filter having a frequency range from ½ f


MAX


to f


MAX


, and a low pass filter having a frequency range from 0 to ½ f


MAX


.




This process is called decomposition. The output from the high pass filter provides “level


1


” discrete wavelet transform coefficients. The level


1


coefficients represent the amplitude as a function of time of that portion of the input signal which is between ½ f


max


and f


MAX


The output from the 0-½ f


max


low pass filter is passed through subsequent high pass (¼ f


max


-¼ f


max


) and low pass (0-½ f


max


) filters, as desired, to provide additional levels (beyond “level


1


”) of discrete wavelet transform coefficients. The outputs from each low pass filter can be subjected to further decompositions offering additional levels of discrete wavelet transformation coefficients as desired. This process continues until the desired resolution is achieved or the number of remaining data samples after a decomposition yields no additional information. The resolution of the wavelet transform is chosen to be approximately the same as the sensor or the same as the minimum signal resolution required to monitor the signal. Each level of DWT coefficients is representative of signal amplitude as a function of time for a given frequency range. Coefficients for each frequency range are concatenated to form a graph such as that shown in FIG.


18


.




In some embodiments, padding is added to the signal by adding data to the sensor signal near the borders of windows used in the wavelet analysis. This padding reduces distortions in the frequency domain output. This technique can be used with a continuous wavelet transform or a discrete wavelet transform. “Padding” is defined as appending extra data on either side of the current active data window, for example, extra data points are added which extend 25% of the current window beyond either window edge. In one embodiment, the padding is generated by repeating a portion of the data in the current window so that the added data “pads” the existing signal on either side. The entire data set is then fit to a quadratic equation which is used to extrapolate the signal 25% beyond the active data window.





FIG. 20

is an example showing a signal S generated by sensor


31


and the resultant approximation signals yielded in seven decomposition levels labeled level


1


through level


7


. In this example, signal level


7


is representative of the lowest frequency DWT coefficient which can be generated. Any further decomposition yields noise. All levels, or only those levels which relate impulse piping or primary element degradation are provided.




Microprocessor


88


evaluates the isolated signal received from the signal preprocessing and in one embodiment, monitors an amplitude of a certain frequency or range of frequencies identified and provides a diagnostic output if a threshold is exceeded. Signal evaluator can also comprise more advanced decision making algorithms such as fuzzy logic, neural networks, expert systems, rule based systems, etc. Commonly assigned U.S. Patent application Ser. No. 08/623,569 describes various decision making systems which can be implemented in signal evaluator


154


and is incorporated herein by reference.




Microprocessor


88


performs diagnostics related to the impulse piping or primary element using information derived from the differential pressure sensor


31


. The following describes a number, of embodiments for realizing a diagnostic circuit. The diagnostic circuit can provide a residual lifetime estimate, an indication of a failure, an indication of an intending failure or a calibration output which is used to correct for errors in the sensed process variable.




A. POLYNOMIAL CURVEFIT




In one embodiment of the present invention empirical models or polynomial curve-fitting are used to detect line plugging or primary element degradation. A polynomial-like equation which has a combination of input signals such as various statistical parameters can be used to detect primary element degradation or impulse line plugging. Constants for the equations can be stored in a memory in the transmitter or received over the communication loop


242


.




B. NEURAL NETWORKS




The signal can be analyzed using a neural network. One such neural network is a multi-layer neural network. Although a number of training algorithms can be used to develop a neural network model for different goals. One embodiment includes the known Backpropagation Network (BPN) to develop neural network modules which will capture the nonlinear relationship among a set of input and output(s).

FIG. 21

shows a typical topology *of a three-layer neural network architecture implemented in microprocessor


88


. The first layer, usually referred to as the input buffer, receives the information, and feeds them into the inner layers. The second layer, in a three-layer network, commonly known as a hidden layer, receives the information from the input layer, modified by the weights on the connections and propagates this information forward. This is illustrated in the hidden layer which is used to characterize the nonlinear properties of the system analyzed. The last layer is the output layer where the calculated outputs (estimations) are presented to the environment.





FIG. 22A

shows a schematic of a neural network which provides a residual life estimate for a primary element or impulse pipe based upon a sensor signal. The sensor signal can be either a raw sensor signal or a sensor signal which has been processed through signal processing techniques.

FIG. 22B

is a graph of residual life versus time and shows that an alarm level can be set prior to an estimated failure time. This allows the system to provide an alarm output prior to actual failure of the device.




C. THRESHOLD CIRCUITRY




This embodiment uses a set of if-then rules to reach a conclusion on the status of the impulse piping or primary element. This embodiment may be implemented easily in analog or digital circuitry. For example, with a simple rule, if the signal drops a certain amount below a historical mean, an output can be provided which indicates that an impulse line is plugged or is in the process of becoming plugged. Of course, more complex rules can be used which use multiple statistical parameters or signal components of the sensor signal to provide more accurate or different information.




D. WAVELETS




With this embodiment, one or more of the decomposition signal(s) in a wavelet analysis directly relate to line plugging and are used to diagnose the transmitter.




Although the present invention has been described with reference to preferred embodiments, workers skilled in the art will recognize that changes can be made in form and detail without departing from the spirit and scope of the invention. For example, various function blocks of the invention have been described in terms of circuitry, however, many function blocks may be implemented in other forms such as digital and analog circuits, software and their hybrids. When implemented in software, a microprocessor performs the functions and the signals comprise digital values on which the software operates. A general purpose processor programmed with instructions that cause the processor to perform the desired process elements, application specific hardware components that contain circuit wired to perform the desired elements and any combination of programming a general purpose processor and hardware components can be used. Deterministic or fuzzy logic techniques can be used as needed to make decisions in the circuitry or software. Because of the nature of complex digital circuitry, circuit elements may not be partitioned into separate blocks as shown, but components used for various functional blocks can be intermingled and shared. Likewise with software, some instructions can be shared as part of several functions and be intermingled with unrelated instructions within the scope of the invention.



Claims
  • 1. A pressure transmitter adapted to couple to a primary flow element via impulse lines to sense flow, the pressure transmitter comprising:a differential pressure sensor adapted to couple to the impulse lines to sense a pressure; an analog to digital converter coupled to the pressure sensor and generating a series of digital representations of the pressure; a microprocessor system receiving the series of digital representations of pressure and having a first algorithm stored therein to calculate a difference between the series of digital representations and a moving average of the series of digital representations, and having a second algorithm stored therein to receive the difference and calculate a trained data set of historical data during a training mode and calculating a current data set during a monitoring mode and generating diagnostic data as a function of the current data set relative to the historical data indicating changes in the condition of flow sensing; a digital to analog converter coupled to the microprocessor system generating an analog transmitter output indicative of flow; and a digital communication circuit receiving the diagnostic data from the microprocessor system and generating a transmitter output indicating the diagnostic data.
  • 2. The pressure transmitter of claim 1 wherein the microprocessor system stores the trained data set.
  • 3. The pressure transmitter of claim 1 wherein the moving average is calculated according to a series Aj=∑k=0m⁢ ⁢(Pj+k)⁢(Wk)where A is the moving average, P is a series of sensed pressure values, and W is a weight for a sensed pressure value, m is a number of previous sensed pressure values in the series, k is an integer ranging from 0 to m and j identifies a sample number.
  • 4. The pressure transmitter of claim 1 wherein the trained data set comprises statistical data.
  • 5. The pressure transmitter of claim 1 wherein the microprocessor system switches from the training mode to the monitoring mode.
  • 6. The pressure transmitter of claim 5 wherein the microprocessor system stores the trained data set in the training mode.
  • 7. The pressure transmitter of claim 1 wherein the diagnostic data indicates a real time condition of a pressure generator.
  • 8. The pressure transmitter of claim 1 wherein the diagnostic data indicates a condition of the primary flow element.
  • 9. The pressure transmitter of claim 1 wherein the diagnostic data indicates a condition of the impulse lines.
  • 10. The pressure transmitter of claim 1 wherein the analog transmitter output comprises a calibrated output, and the diagnostic data transmitter output indicates if the pressure sensor is out of calibration.
  • 11. The pressure transmitter of claim 1 wherein the trained data set of historical data comprises power spectral density of the difference.
  • 12. The pressure transmitter of claim 11 wherein the power spectral density data is in the range of 0 to 100 Hertz.
  • 13. The pressure transmitter of claim 1 wherein the pressure transmitter is adapted to couple to a pitot tube primary flow element.
  • 14. The pressure transmitter of claim 13 wherein the pitot tube is an averaging pitot tube.
  • 15. The pressure transmitter of claim 14 wherein the averaging pitot tube is insertable through a tap on a pipe.
  • 16. The pressure transmitter of claim 13 further comprising an instrument manifold coupled between the pressure generator and the pressure sensor.
  • 17. The pressure transmitter of claim 1 wherein the primary flow element and impulse lines are combined in an integral orifice.
  • 18. The pressure transmitter of claim 1 wherein the pressure transmitter is adapted to couple to a venturi primary flow element.
  • 19. The pressure transmitter of claim 1 wherein the pressure transmitter is adapted to couple to a nozzle primary flow element.
  • 20. The pressure transmitter of claim 1 wherein the pressure transmitter is adapted to couple to an orifice primary flow element adapted for clamping between pipe flanges.
  • 21. A pressure transmitter adapted to couple to a primary flow element via impulse lines to sense flow, the pressure transmitter comprising:a differential pressure sensor adapted to couple to the impulse lines to sense a pressure; a flow circuit coupled to the sensor to generate a flow output; a difference circuit coupled to the sensor to generate a difference output representing the sensed pressure minus a moving average; a calculate circuit to receive the difference output, calculate a trained output of historical data obtained during training, and calculate a monitor output of current data obtained during monitoring; and a diagnostic circuit to receive the trained output and the monitor output and generate a diagnostic output indicating a current condition of flow sensing relative to an historical condition of flow sensing.
  • 22. The pressure transmitter of claim 21 wherein the differential pressure sensor includes remote seals.
  • 23. The pressure transmitter of claim 21 wherein the flow output is a time integral of flow indicating a quantity of fluid in a tank.
  • 24. The pressure transmitter of claim 23 further including a wet leg.
  • 25. The pressure transmitter of claim 23 further including a dry leg.
  • 26. The pressure transmitter of claim 21 wherein the calculate circuit stores the historical data.
  • 27. The pressure transmitter of claim 21 wherein the moving average is calculated according to the series Aj=∑k=0m⁢ ⁢(Pj+k)⁢(Wk)where A is the moving average, P is a series of sensed pressure values, and W is a weight for a sensed pressure value, m is a number of previous sensed pressure values in the series, k is an integer ranging from 0 to m and j identifies a sample number.
  • 28. The pressure transmitter of claim 21 wherein the historical data comprises statistical data.
  • 29. The pressure transmitter of claim 21 wherein the calculate circuit switches between a training mode and a monitoring mode.
  • 30. The pressure transmitter of claim 29 wherein the calculate circuit stores historical data in the monitoring mode.
  • 31. The pressure transmitter of claim 21 wherein the diagnostic output comprises a real time indication of the condition of a pressure generator.
  • 32. The pressure transmitter of claim 21 wherein the diagnostic circuit indicates a condition of the primary element.
  • 33. The pressure transmitter of claim 21 wherein the diagnostic circuit indicates a condition of the impulse lines.
  • 34. The pressure transmitter of claim 21 wherein the flow output comprises a calibrated output and the diagnostic circuit indicates if the pressure sensor is out of calibration.
  • 35. The pressure transmitter of claim 21 wherein the historical data comprises power spectral density of the difference output.
  • 36. The pressure transmitter of claim 35 wherein the power spectral density data is in the range of 0 to 100 Hertz.
  • 37. The pressure transmitter of claim 21 wherein the diagnostic circuit implements a diagnostic algorithm selected from the group of algorithms consisting of neural networks, fuzzy logic, wavelets and Fourier transforms.
  • 38. A fluid flow meter adapted to sense fluid flow, comprising,a pressure generator having a primary element and impulse lines couplable to the fluid flow; a differential pressure sensor coupled to the impulse lines to sense a pressure; a flow circuit coupled to the sensor to generate a flow output; a difference circuit coupled to the sensor to generate a difference output representing the sensed pressure minus a moving average of the sensed pressure; a calculate circuit to receive the difference output and calculate a trained output of historical data obtained during training and calculating a monitor output of current data obtained during monitoring; and a diagnostic circuit to receive the trained output and the monitor output and generate a diagnostic output indicating a current condition of the pressure generator relative to an historical condition.
  • 39. The fluid flow meter of claim 38 wherein the calculate circuit stores the historical data.
  • 40. The fluid flow meter of claim 38 wherein the moving average is calculated according to the series Aj=∑k=0m⁢ ⁢(Pj+k)⁢(Wk)where A is the moving average, P is a series of sensed pressure values, and W is a weight for a sensed pressure value, m is a number of previous sensed pressure values in the series, k is an integer ranging from 0 to m and j identifies a sample number.
  • 41. The fluid flow meter of claim 38 wherein the historical data comprises statistical data.
  • 42. The fluid flow meter of claim 38 wherein the calculate circuit switches between a training mode and a monitoring mode.
  • 43. The fluid flow meter of claim 42 wherein the calculate circuit stores the historical data in the training mode.
  • 44. The fluid flow meter of claim 38 wherein the diagnostic output indicates a real time condition of the pressure generator.
  • 45. The fluid flow meter of claim 44 wherein the diagnostic output indicates a condition of the primary element.
  • 46. The fluid flow meter of claim 44 wherein the diagnostic output indicates a condition of the impulse lines.
  • 47. The fluid flow meter of claim 38 wherein the flow output comprises a calibrated output and the diagnostic output indicates if the pressure generator is out of calibration.
  • 48. The fluid flow meter of claim 38 wherein the historical data comprises power spectral density of the difference output.
  • 49. The fluid flow meter of claim 48 wherein the power spectral density data is in the range of 0 to 100 Hertz.
  • 50. The fluid flow meter of claim 38 wherein the primary element comprises a pitot tube.
  • 51. The fluid flow meter of claim 50 wherein the pitot tube is an averaging pitot tube.
  • 52. The fluid flow meter of claim 51 wherein the averaging pitot tube is inserted through a tap on a pipe.
  • 53. The fluid flow meter of claim 50 further comprising an instrument manifold coupled between the pressure generator and the pressure sensor.
  • 54. The fluid flow meter of claim 38 wherein the primary element and impulse lines are combined in an integral orifice.
  • 55. The fluid flow meter of claim 38 wherein the primary element comprises a venturi.
  • 56. The fluid flow meter of claim 38 wherein the primary element comprises a nozzle.
  • 57. The fluid flow meter of claim 38 wherein the primary element comprises an orifice plate adapted for clamping between pipe flanges.
  • 58. The flow meter of claim 38 wherein the diagnostic current implements a diagnostic algorithm selected from the group of algorithms consisting of neural networks, fuzzy logic, wavelets and Fourier transforms.
  • 59. A diagnostic method performed in a pressure transmitter coupled to a primary flow element via impulse lines, the method comprising:calculating a difference between a pressure sensed by the pressure transmitter and a moving average of the sensed pressure; acquiring and storing an historical data set of the calculated difference during a train mode of the pressure transmitter; acquiring and storing a current data set of the calculated difference during a monitoring mode of the pressure transmitter; comparing the current data set to the historical data set to diagnose the condition of the primary flow element and impulse lines; and generating output of the pressure transmitter indicating the condition of the primary flow element and impulse lines.
  • 60. The method of diagnosis of claim 59 wherein the historical data set comprises statistical data on the calculated difference.
  • 61. The method of diagnosis of claim 60 wherein the current data set comprises current data on a sample average (X) and a sample standard deviation (s) of the calculated difference.
  • 62. The method of diagnosis of claim 61 wherein the sample average (X) is compared to a mean (μ) to diagnose erosion of the primary flow element.
  • 63. The method of diagnosis of claim 62 wherein the sample deviation (s) is compared to the standard deviation (σ) to diagnose impulse line plugging.
  • 64. The method of diagnosis of claim 59 wherein the historical data set comprises data on the power spectral density of the calculated difference.
  • 65. The method of diagnosis of claim 64 wherein the current data set comprises data on the power spectral density of the calculated difference.
  • 66. The method of diagnosis of claim 59 wherein the comparing includes performing a diagnostic algorithm selected from the group of algorithms consisting of neural networks, fuzzy logic, wavelets and Fourier transforms.
  • 67. A computer-readable medium having stored thereon instructions executable by a microprocessor system in a pressure transmitter to cause the pressure transmitter to perform a diagnostic operation relative to a primary element and impulse lines couplable to the transmitter, the instructions comprising:calculating a difference between a pressure sensed by the pressure transmitter and a moving average of the sensed pressure; acquiring and storing an historical data set of the calculated difference during a train mode of the pressure transmitter; acquiring and storing a current data set of the calculated difference during a monitoring mode of the pressure transmitter; comparing the current data set to the historical data set to diagnose the condition of the primary element and impulse lines; and generating an output of the pressure transmitter indicating the condition of the primary element and impulse lines.
  • 68. A pressure transmitter adapted to couple to a primary flow element via impulse lines to sense flow, the pressure transmitter comprising:a differential pressure sensor adapted to couple to the impulse lines to sense a pressure; a flow circuit coupled to the sensor and generating a flow output; differencing means coupled to the sensor for generating a difference output representing the sensed pressure minus a moving average of the sensed pressure; calculating means receiving the difference output for calculating a trained output of historical data obtained during training and for calculating a monitor output of current data obtained during monitoring; and diagnosing means receiving the trained output and the monitor output and generating a diagnostic output for diagnosing a current condition of flow sensing relative to an historical condition of flow sensing.
Parent Case Info

This is a Continuation-In-Part of U.S. application Ser. No. 09/257,896, filed Feb. 25, 1999 which is a Continuation-In-Part of U.S. application Ser. No. 08/623,569, filed Mar. 28, 1996.

US Referenced Citations (214)
Number Name Date Kind
3096434 King Jul 1963 A
3404264 Kugler Oct 1968 A
3468164 Sutherland Sep 1969 A
3590370 Fleischer Jun 1971 A
3688190 Blum Aug 1972 A
3691842 Akeley Sep 1972 A
3701280 Stroman Oct 1972 A
3849637 Caruso et al. Nov 1974 A
3855858 Cushing Dec 1974 A
3952759 Ottenstein Apr 1976 A
3973184 Raber Aug 1976 A
RE29383 Gallatin et al. Sep 1977 E
4058975 Gilbert et al. Nov 1977 A
4099413 Ohte et al. Jul 1978 A
4102199 Talpouras Jul 1978 A
4122719 Carlson et al. Oct 1978 A
4249164 Tivy Feb 1981 A
4250490 Dahlke Feb 1981 A
4279013 Cameron et al. Jul 1981 A
4337516 Murphy et al. Jun 1982 A
4399824 Davidson Aug 1983 A
4417312 Cronin et al. Nov 1983 A
4517468 Kemper et al. May 1985 A
4530234 Cullick et al. Jul 1985 A
4571689 Hildebrand et al. Feb 1986 A
4630265 Sexton Dec 1986 A
4635214 Kasai et al. Jan 1987 A
4642782 Kemper et al. Feb 1987 A
4644479 Kemper et al. Feb 1987 A
4649515 Thompson et al. Mar 1987 A
4686638 Furuse Aug 1987 A
4707796 Calabro et al. Nov 1987 A
4736367 Wroblewski et al. Apr 1988 A
4736763 Britton et al. Apr 1988 A
4777585 Kokawa et al. Oct 1988 A
4818994 Orth et al. Apr 1989 A
4831564 Suga May 1989 A
4841286 Kummer Jun 1989 A
4853693 Eaton-Williams Aug 1989 A
4873655 Kondraske Oct 1989 A
4907167 Skeirik Mar 1990 A
4924418 Backman et al. May 1990 A
4934196 Romano Jun 1990 A
4939753 Olson Jul 1990 A
4964125 Kim Oct 1990 A
4988990 Warrior Jan 1991 A
4992965 Holter et al. Feb 1991 A
5005142 Lipchak et al. Apr 1991 A
5043862 Takahashi et al. Aug 1991 A
5053815 Wendell Oct 1991 A
5067099 McCown et al. Nov 1991 A
5081598 Bellows et al. Jan 1992 A
5089984 Struger et al. Feb 1992 A
5098197 Shepard et al. Mar 1992 A
5099436 McCown et al. Mar 1992 A
5103409 Shimizu et al. Apr 1992 A
5111531 Grayson et al. May 1992 A
5121467 Skeirik Jun 1992 A
5122794 Warrior Jun 1992 A
5122976 Bellows et al. Jun 1992 A
5130936 Sheppard et al. Jul 1992 A
5134574 Beaverstock et al. Jul 1992 A
5137370 McCullock et al. Aug 1992 A
5142612 Skeirik Aug 1992 A
5143452 Maxedon et al. Sep 1992 A
5148378 Shibayama et al. Sep 1992 A
5167009 Skeirik Nov 1992 A
5175678 Frerichs et al. Dec 1992 A
5193143 Kaemmerer et al. Mar 1993 A
5197114 Skeirik Mar 1993 A
5197328 Fitzgerald Mar 1993 A
5212765 Skeirik May 1993 A
5214582 Gray May 1993 A
5216226 Miyoshi Jun 1993 A
5224203 Skeirik Jun 1993 A
5228780 Shepard et al. Jul 1993 A
5235527 Ogawa et al. Aug 1993 A
5265031 Malczewski Nov 1993 A
5265222 Nishiya et al. Nov 1993 A
5269311 Kirchner et al. Dec 1993 A
5274572 O'Neill et al. Dec 1993 A
5282131 Rudd et al. Jan 1994 A
5282261 Skeirik Jan 1994 A
5293585 Morita Mar 1994 A
5303181 Stockton Apr 1994 A
5305230 Matsumoto et al. Apr 1994 A
5311421 Nomura et al. May 1994 A
5317520 Castle May 1994 A
5327357 Feinstein et al. Jul 1994 A
5333240 Matsumoto et al. Jul 1994 A
5347843 Orr et al. Sep 1994 A
5349541 Alexandro, Jr. et al. Sep 1994 A
5357449 Oh Oct 1994 A
5361628 Marko et al. Nov 1994 A
5365423 Chand Nov 1994 A
5367612 Bozich et al. Nov 1994 A
5384699 Levy et al. Jan 1995 A
5386373 Keller et al. Jan 1995 A
5388465 Okaniwa et al. Feb 1995 A
5394341 Kepner Feb 1995 A
5394543 Hill et al. Feb 1995 A
5404064 Mermelstein et al. Apr 1995 A
5408406 Mathur et al. Apr 1995 A
5408586 Skeirik Apr 1995 A
5414645 Hirano May 1995 A
5419197 Ogi et al. May 1995 A
5430642 Nakajima et al. Jul 1995 A
5434774 Seberger Jul 1995 A
5440478 Fisher et al. Aug 1995 A
5442639 Crowder et al. Aug 1995 A
5467355 Umeda et al. Nov 1995 A
5469070 Koluvek Nov 1995 A
5469156 Kogura Nov 1995 A
5469735 Watanabe Nov 1995 A
5469749 Shimada et al. Nov 1995 A
5481199 Anderson et al. Jan 1996 A
5481200 Voegele et al. Jan 1996 A
5483387 Bauhahn et al. Jan 1996 A
5485753 Burns et al. Jan 1996 A
5486996 Samad et al. Jan 1996 A
5488697 Kaemmerer et al. Jan 1996 A
5489831 Harris Feb 1996 A
5495769 Borden et al. Mar 1996 A
5510779 Maltby et al. Apr 1996 A
5511004 Dubost et al. Apr 1996 A
5548528 Keeler et al. Aug 1996 A
5560246 Bottinger et al. Oct 1996 A
5561599 Lu Oct 1996 A
5570300 Henry et al. Oct 1996 A
5572420 Lu Nov 1996 A
5573032 Lenz et al. Nov 1996 A
5591922 Segeral et al. Jan 1997 A
5598521 Kilgore et al. Jan 1997 A
5600148 Cole et al. Feb 1997 A
5608650 McClendon et al. Mar 1997 A
5623605 Keshav et al. Apr 1997 A
5629870 Farag et al. May 1997 A
5637802 Frick et al. Jun 1997 A
5640491 Bhat et al. Jun 1997 A
5654869 Ohi et al. Aug 1997 A
5661668 Yemini et al. Aug 1997 A
5665899 Willcox Sep 1997 A
5669713 Schwartz et al. Sep 1997 A
5671335 Davis et al. Sep 1997 A
5675504 Serodes et al. Oct 1997 A
5675724 Beal et al. Oct 1997 A
5680109 Lowe et al. Oct 1997 A
5682317 Keeler et al. Oct 1997 A
5700090 Eryurek Dec 1997 A
5703575 Kirkpatrick Dec 1997 A
5704011 Hansen et al. Dec 1997 A
5705978 Frick et al. Jan 1998 A
5708211 Jepson et al. Jan 1998 A
5708585 Kushion Jan 1998 A
5710370 Shanahan et al. Jan 1998 A
5713668 Lunghofer et al. Feb 1998 A
5719378 Jackson, Jr. et al. Feb 1998 A
5741074 Wang et al. Apr 1998 A
5742845 Wagner Apr 1998 A
5746511 Eryurek et al. May 1998 A
5752008 Bowling May 1998 A
5764891 Warrior Jun 1998 A
5781878 Mizoguchi et al. Jul 1998 A
5801689 Huntsman Sep 1998 A
5805442 Crater et al. Sep 1998 A
5817950 Wiklund et al. Oct 1998 A
5828567 Eryurek et al. Oct 1998 A
5829876 Schwartz et al. Nov 1998 A
5848383 Yuuns Dec 1998 A
5859964 Wang et al. Jan 1999 A
5876122 Eryurek Mar 1999 A
5880376 Sai et al. Mar 1999 A
5887978 Lunghofer et al. Mar 1999 A
5908990 Cummings Jun 1999 A
5923557 Eidson Jul 1999 A
5924086 Mathur et al. Jul 1999 A
5926778 Pöppel Jul 1999 A
5936514 Anderson et al. Aug 1999 A
5940290 Dixon Aug 1999 A
5956663 Eryurek et al. Sep 1999 A
5970430 Burns et al. Oct 1999 A
6014902 Lewis et al. Jan 2000 A
6016523 Zimmerman et al. Jan 2000 A
6016706 Yamamoto et al. Jan 2000 A
6017143 Eryurek et al. Jan 2000 A
6023399 Kogure Feb 2000 A
6038579 Sekine Mar 2000 A
6045260 Schwartz et al. Apr 2000 A
6047220 Eryurek et al. Apr 2000 A
6047222 Burns et al. Apr 2000 A
6052655 Kobayashi et al. Apr 2000 A
6061603 Papadopoulos et al. May 2000 A
6119047 Eryurek et al. Sep 2000 A
6119529 Di Marco et al. Sep 2000 A
6139180 Usher et al. Oct 2000 A
6182501 Furuse et al. Feb 2001 B1
6192281 Brown et al. Feb 2001 B1
6195591 Nixon et al. Feb 2001 B1
6199018 Quist et al. Mar 2001 B1
6236948 Eck et al. May 2001 B1
6263487 Stripf et al. Jul 2001 B1
6298377 Hartikainen et al. Oct 2001 B1
6307483 Westfield Oct 2001 B1
6317701 Pyotsia et al. Nov 2001 B1
6327914 Dutton Dec 2001 B1
6347252 Behr et al. Feb 2002 B1
6360277 Ruckley et al. Mar 2002 B1
6370448 Eryurek Apr 2002 B1
6377859 Brown et al. Apr 2002 B1
6397114 Eryurek et al. May 2002 B1
6405099 Nagai et al. Jun 2002 B1
6425038 Sprecher Jul 2002 B1
6473656 Langels et al. Oct 2002 B1
20020013629 Nixon et al. Jan 2002 A1
Foreign Referenced Citations (78)
Number Date Country
32 13 866 Oct 1983 DE
35 40 204 Sep 1986 DE
40 08 560 Sep 1990 DE
43 43 747 Jun 1994 DE
44 33 593 Jun 1995 DE
195 02 499 Aug 1996 DE
296 00 609 Mar 1997 DE
197 04 694 Aug 1997 DE
19930660 Jul 1999 DE
199 05 071 Aug 2000 DE
299 17 651 Dec 2000 DE
100 36 971 Feb 2002 DE
0 122 622 Oct 1984 EP
0 413 814 Feb 1991 EP
0 487 419 May 1992 EP
0 594 227 Apr 1994 EP
0 624 847 Nov 1994 EP
0 644 470 Mar 1995 EP
0 825 506 Jul 1997 EP
0 827 096 Sep 1997 EP
0 838 768 Sep 1997 EP
0 807 804 Nov 1997 EP
1058093 May 1999 EP
1 022 626 Jul 2000 EP
2 302 514 Sep 1976 FR
2 334 827 Jul 1977 FR
928704 Jun 1963 GB
1 534 280 Nov 1978 GB
1 534 288 Nov 1978 GB
2 310 346 Aug 1997 GB
2 347 232 Jan 2000 GB
2342453 Apr 2000 GB
58-129316 Aug 1983 JP
59-116811 Jul 1984 JP
59163520 Sep 1984 JP
59-211196 Nov 1984 JP
59-211896 Nov 1984 JP
60000507 Jan 1985 JP
60-76619 May 1985 JP
60-131495 Jul 1985 JP
60174915 Sep 1985 JP
62-30915 Feb 1987 JP
64-1914 Jan 1989 JP
64001914 Jan 1989 JP
64-72699 Mar 1989 JP
2-5105 Jan 1990 JP
5-122768 May 1993 JP
06242192 Sep 1994 JP
7-63586 Mar 1995 JP
07234988 Sep 1995 JP
8-54923 Feb 1996 JP
08102241 Apr 1996 JP
8-136386 May 1996 JP
8-166309 Jun 1996 JP
08247076 Sep 1996 JP
08313466 Nov 1996 JP
2712625 Oct 1997 JP
2712701 Oct 1997 JP
2753592 Mar 1998 JP
07225530 May 1998 JP
10-232170 Sep 1998 JP
11083575 Mar 1999 JP
WO 9425933 Nov 1994 WO
WO 9611389 Apr 1996 WO
WO 9612993 May 1996 WO
WO 9639617 Dec 1996 WO
WO 9721157 Jun 1997 WO
WO 9725603 Jul 1997 WO
WO 9806024 Feb 1998 WO
WO 9813677 Apr 1998 WO
WO 9820469 May 1998 WO
WO 9839718 Sep 1998 WO
WO 9919782 Oct 1998 WO
WO 0055700 Mar 2000 WO
WO 0041050 Jul 2000 WO
WO 0070531 Nov 2000 WO
WO 0177766 Oct 2001 WO
WO 0227418 Apr 2002 WO
Non-Patent Literature Citations (144)
Entry
International Search Report for International Application No. PCT/US 02/14934, filed May 8, 2002, Search Report dated Apr. 28, 2002.
International Search Report for International Application No. PCT/US 02/14560, filed May 8, 2002, Search Report dated Sep. 3, 2002.
“Sensor and Device Diagnostics for Predictive and Proactive Maintenance”, by B. Boynton, A Paper Presented at the Electric Power Research Institute—Fossil Plant Maintenance Conference in Baltimore, Maryland, Jul. 29-Aug. 1, 1996, pp. 50-1—50-6.
“Smart Field Devices Provide New Process Data, Increase System Flexibility,” by Mark Boland, I&CS, Nov. 1994, pp. 45-51.
“Wavelet Analysis of Vibration, Part I: Theory,” by D.E. Newland, Journal of Vibration and Acoustics, vol. 116, Oct. 1994, pp. 409-416.
“Wavelet Analysis of Vibration, Part 2: Wavelet Maps,” by D.E. Newland, Journal of Vibration and Acoustics, vol. 116, Oct. 1994, p. 417-425.
“Field-based Architecture is Based on Open Systems, Improves Plant Performance”, by P. Cleaveland, I&CS, Aug. 1996, pp. 73-74.
“Fuzzy Logic and Neural Network Applications to Fault Diagnosis”, by P. Frank et al., International Journal of Approximate Reasoning, (1997), pp. 68-88.
“A Fault-Tolerant Interface for Self-Validating Sensors”, by M.P. Henry, Colloquium, pp. 3/1-3/2 (Nov. 1990).
“The Implications of Digital Communications on Sensor Validation”, by M. Henry et al., Report No. QUEL 1912/92, (1992).
“Keynote Paper: Hardware Compilation-A New Technique for Rapid Prototyping of Digital Systems-Applied to Sensor Validation”, by M.P. Henry, Control Eng. Practice, vol. 3, No. 7., pp. 907-924, (1995).
“Neural Networks for Sensor Validation and Plant Monitoring,” by B. Upadhyaya, International Fast Reactor Safety Meeting, Aug. 12-16, 1990, pp. 2-10.
“Intelligent Behaviour for Self-Validating Sensors”, by M.P. Henry, Advances in Measurement, pp. 1-7, (May 1990).
“Integration of Multiple Signal Validation Modules for Sensor Monitoring,”by B. Upadhyaya et al., Department of Nuclear Engineering, Jul. 8, 1990, pp. 1-6.
“An Integrated Architecture For Signal Validation in Power Plants,” by B.R. Upadhyaya et al., Third IEEE International Symposium on Intelligent Control, Aug. 24-26, 1988, pp. 1-6.
“Neural Networks for Sensor Validation and Plantwide Monitoring,” by E. Eryurek, 1992.
“Programmable Hardware Architecture for Sensor Validation”, by M.P. Henry et al., Control Eng. Practice, vol. 4, No. 10., pp. 1339-1354, (1996).
“Applications of Neural Computing Paradigms for Signal Validation,” by B.R. Upadhyaya et al., Department of Nuclear Science, vol. 37, No. 2, by E. Eryurek et al. Apr. 1990, pp. 1040-1047.
“Sensor Validation for Power Plants Using Adaptive Backpropagation Neural Network,” IEEE Transactions on Nuclear Science, vol. 37, No. 2, by E. Eryurek et al. Apr. 1990, pp. 1040-1047.
A Standard Interface for Self-Validating Sensors, by M.P. Henry et al., Report No. QUEL 1884/91, (1991).
“Development and Application of Neural Network Algorithms For Process Diagnostics,” by B.R. Upadhyaya et al., Proceedings of the 29th Conference on Decision and Control, 1990, pp. 3277-3282.
“Fuzzy Logic and Artificial Neural Networks for Nuclear Power Plant Applications,” by R.C. Berkan et al., Proceedings of the American Power Conference.
Parallel, Fault-Tolerant Control and Diagnostics System for Feedwater Regulation in PWRS, by E. Eryurek et al., Proceedings of the American Power Conference.
“Signal Processing, Data Handling and Communications: The Case for Measurement Validation”, by M.P. Henry, Department of Engineering Science, Oxford University.
“Software-Based Fault-Tolerant Control Design for Improved Power Plant Operation,” IEEE/IFAC Joint Symposium on Computer-Aided Control System Design, Mar. 7-9, 1994 pp. 585-590.
“Using Artificial Neural Networks to Identify Nuclear Power Plant States,” by Israel E. Alguindigue et al., pp. 1-4.
“Taking Full Advantage of Smart Transmitter Technology Now,” by G. Orrison, Control Engineering, vol. 42, No. 1, Jan. 1995.
“Automated Generation of Nonlinear System Characterization for Sensor Failure Detection,” by B.R. Upadhyaya et al., ISA, 1989 pp. 269-274.
“Application of Neural Networks for Sensor Validation and Plant Monitoring,” by B. Upadhyaya et al., Nuclear Technology, vol. 97, No. 2, Feb. 1992 pp. 170-176.
“Detecting Blockage in Process Connections of Differential Pressure Transmitters”, by E. Taya et al., SICE, 1995, pp. 1605-1608.
09/169,873, Oct. 12, 1998, Eryurek et al.
09/175,832, Oct. 19, 1998, Eryurek et al.
09/257,896, Feb. 25, 1999, Eryurek et al.
09/303,869, May 3, 1999, Eryurek et al.
09/335,212, Jun. 17, 1999, Kirkpatrick et al.
09/360,473, Jul. 23, 1999, Eryurek et al.
09/369,530, Aug. 6, 1999, Eryurek et al.
09/384,876, Aug. 27, 1999, Eryurek et al.
09/406,263, Sep. 24, 1999, Kirkpatrick et al.
09/409,098, Sep. 30, 1999, Eryurek et al.
09/409,114, Sep. 30, 1999, Eryurek et al.
09/565,604, May 4, 2000, Eruyrek et al.
09/576,450, May 23, 2000, Wehrs.
09/606,259, Jun. 29, 2000, Eryurek.
09/616,118, Jul. 14, 2000, Eryurek et al.
09/627,543, Jul. 28, 2000, Eryurek et al.
“A TCP/IP Tuturial” by, Socolofsky et al., Spider Systems Limited, Jan. 1991 pp. 1-23.
“Approval Standards For Explosionproof Electrical Equipment General Requirements”, Factory Mutual Research, Cl. No. 3615, Mar. 1989, pp. 1-34.
“Approval Standard Intrinsically Safe Apparatus and Associated Apparatus For Use In Class I, II, and III, Division 1 Hazardous (Classified) Locations”, Factory Mutual Research, Cl. No. 3610, Oct. 1988, pp. 1-70.
“Automation On-Line” by, Phillips et al., Plant Services, Jul. 1997, pp. 41-45.
“Climb to New Heights by Controlling your PLCs Over the Internet” by, Phillips et al., Intech, Aug. 1998, pp. 50-51.
“CompProcessor For Piezoresistive Sensors” MCA Technologies Inc. (MCA7707), pp. 1-8.
“Ethernet emerges as viable, inexpensive fieldbus”, Paul G. Schreier, Personal Engineering, Dec. 1997, p. 23-29.
“Ethernet Rules Closed-loop System” by, Eidson et al., Intech, Jun. 1998, pp. 39-42.
“Fieldbus Standard for Use in Industrial Control System Part 2: Physical Layer Specification and Service Definition”, ISA-S50.02-1002, pp. 1-93.
“Fieldbus Standard for Use in Industrial Control Systems Part 3: Data Link Service Definition”, ISA-S50.02-1997, Part 3, Aug. 1997, pp. 1-159.
Fieldbus Standard for Use in Industrial Control Systems Part 4: Data Link Protocol Specification, ISA-S50.02-1997, Part 4, Aug. 1997, pp. 1-148.
“Fieldbus Support For Process Analysis” by, Blevins et al., Fisher-Rosemoung Systems, Inc., 1995, pp. 121-128.
“Fieldbus Technical Overview Understanding Foundation™ fieldbus technology”, Fisher-Rosemount, 1998, pp. 1-23.
“Hypertext Transfer Protocol—HTTP/1.0” by, Berners-Lee, et al., MIT/LCS, May 1996, pp. 1-54.
“Infranets, Intranets, and the Internet” by, Pradip Madan, Echelon Corp, Sensors, Mar. 1997, pp. 46-50.
“Internet Technology Adoption into Automation” by, Fondl e al., Automation Business, pp. 1-5.
“Internet Protocol Darpa Internet Program Protocol Specification” by, Information Sciences Institute, University of Southern California, RFC 791, Sep. 1981, pp. 1-43.
“Introduction to Emit”, emWare, Inc., 1997, pp. 1-22.
“Introduction to the Internet Protocols” by, Charles L. Hedrick, Computer Science Facilities Group, Rutgers University, Oct. 3, 1988, pp. 1-97.
“Is There A Future For Ethernet in Industrial Control?”, Miclot et al., Plant Engineering, Oct. 1988, pp. 44-46, 48, 50.
LFM/SIMA Internet Remote Diagnostics Research Project Summary Report, Stanford University, Jan. 23, 1997, pp. 1-6.
“Managing Devices with the Web” by, Howard et al., Byte, Sep. 1997, pp. 45-64.
“Modular Microkernel Links GUI And Browser For Embedded Web Devices” by, Tom Williams, pp. 1-2.
“PC Software Gets Its Edge From Windows, Components, and the Internet”, Wayne Labs, I&CS, Mar. 1997, pp. 23-32.
Proceedings Sensor Expo, Aneheim, California, Produced by Expocon Managemnet Associates, Inc., Apr. 1996, pp. 9-21.
Proceedings Sensor Expo, Boston, Massachuttes, Produced by Expocon Management Associates, Inc., May 1997, pp. 1-416.
“Smart Sensor Network of the Future” by, Jay Warrior, Sensors, Mar. 1997, pp. 40-45.
“The Embedded Web Site” by, John R. Hines, IEEE Spectrum, Sep. 1996, p. 23.
“Transmission Control Protocol: Darpa Internet Program Protocol Specification” Information Sciences Institute, Sep. 1981, pp. 1-78.
“Advanced Engine Diagnostics Using Universal Process Modeling”, by P. O'Sullivan et al., Presented at the 1996 SAE Conference on Future Transportion Technology, pp. 1-9.
“On-Line Statistical Process Control for a Glass Tank Ingredient Scale,” by R.A. Weisman, IFAC real Time Programming, 1985, pp. 29-38.
“The Performance of Control Charts for Monitoring Process Variation,” by C. Lowry et al., Commun. Statis.—Simula., 1995, pp. 409-437.
“A Knowledge-Based Approach for Detection and Diagnosis of Out-of-Control Events in Manufacturing Processes,” by P. Love et al., IEEE, 1989, pp. 736-741.
“Advanced Engine Diagnostics Using Universal Process Modeling”, by P. O'Sullivan, Presented at the 1996 SAE Conference on Future Transportation Technology, pp. 1-9.
“Smart Temperature Measurement in the '90”, by T. Kerlin et al., C&I, (1990).
“In Situ Calibration of Nuclear Plant Platinum Resistance Thermometers Using Johnson Noise Methods,” EPRI, Jun. 1983.
“Johnson Noise Thermometer for High Radiation and High-Temperature Environments,” by L. Oakes et al., Fifth Symposium on Space Nuclear Power Systems, Jan. 1988, pp. 2-23.
“Development of a Resistance Thermometer For Use Up to 1600 °C”, by M.J. de Groot et al., CAL Lab, Jul./Aug. 1996, pp. 38-41.
“Survey, Applications, And Prospects of Johnson Noise Thermometry,” by T. Blalock et al., Electrical Engineering Department, 1981 pp. 2-11.
“Noise Thermometry for Industrial and Metrological Applications at KFA Julich,” by H. Brixy et al., 7th International Symposium on Temperature, 1992.
“Johnson Noise Power Thermometer and its Application in Process Temperature Measurement,” by T.V. Blalock et al., American Institute of Physics 1982, pp. 1249-1259.
“Tuned-Circuit Johnson Noise Thermometry,” by Michael Roberts et al., 7th Symposium on Space Nuclear Power Systems, Jan. 1990.
“Tuned-Circuit Johnson Noise Thermometry,” by Michael Roberts et al., 7th Symposium on Space Nuclear Power Systems, Jan. 1990.
“Development of a Long-Life, High-Reliability Remotely Operated Johnson Noise Thermometer,” by R.L. Shepard et al., ISA, 1991, pp. 77-84.
“Application of Johnson Noise Thermometry to Space Nuclear Reactors,” by M.J. Roberts et al., Presented at the 6th Symposium on Space Nuclear Power Systems, Jan. 9-12, 1989.
“A Decade of Progress in High Temperature Johnson Noise Thermometry,” by T.V. Blalock et al., American Institute of Physics, 1982 pp. 1219-1223.
“Detection of Hot Spots in Thin Metal Films Using an Ultra Sensitive Dual Channel Noise Measurement System,” by G.H. Massiha et al., Energy and Information Technologies in the Southeast, vol. 3 of 3, Apr. 1989, pp. 1310-1314.
“A New Method of Johnson Noise Thermometry”, by C.J. Borkowski et al., Rev. Sci. Instrum., vol. 45, No. 2, (Feb. 1974) pp. 151-162.
“In-Situ Response Time Testing of Thermocouples”, ISA, by H.M. Hashemian et al., Paper No. 89-0056, pp. 587-593, (1989).
“Measurement of the Temperature Fluctuation in a Resistor Generating 1/F Fluctuation,” by S. Hashiguchi, Japanese Journal of Applied Physics, vol. 22, No. 5, Part 2, May 1983, pp. L284-L286.
“Check of Semiconductor Thermal Resistance Elements by the Method of Noise Thermometry”, by A. B. Kisilevskii et al., Measurement Techniques, vol. 25, No. 3, Mar. 1982, New York, USA, pp. 244-246.
“Thermocouple Continuity Checker,” IBM Technical Disclosure Bulletin, vol. 20, No. 5, pp. 1954 (Oct. 1977).
“A Self-Validating Thermocouple,” Janice C-Y et al., IEEEE Transactions on Control Systems Technology, vol. 5, No. 2, pp. 239-253 (Mar. 1997).
Instrument Engineers' Handbook, Chapter IV entitled “Temperature Measurements,” by T.J. Claggett, pp. 266-333 (1982).
“emWare's Releases EMIT 3.0, Allowing Manufacturers to Internet and Network Enable Devices Royalty Free,” 3 pages, PR Newswire (Nov. 4, 1998).
Warrior, J., “The IEEE P1451.1 Object Model Network Independent Interfaces for Sensors and Actuators,” pp. 1-14, Rosemount Inc. (1997).
Warrior, J., “The Collision Between the Web and Plant Floor Automation,” 6th. WWW Conference Workshop on Embedded Web Technology, Santa Clara, CA (Apr. 7, 1997).
Microsoft Presss Computer Dictionary, 3rd Edition, p. 124.
“Internal Statistical Quality Control for Quality Monitoring Instruments”, by P. Girling et al., ISA, 15 pgs., 1999.
Web Pages from www.triant.com (3 pgs.).
“Statistical Process Control (Practice Guide Series Book)”, Instrument Society of America, 1995, pp. 1-58 and 169-204.
“Time-Frequency Analysis of Transient Pressure Signals for a Mechanical Heart Valve Cavitation Study,” ASAIO Journal, by Alex A. Yu et al., vol. 44, No. 5, pp. M475-M479, (Sep.-Oct. 1998).
“Transient Pressure Signals in Mechanical Heart Valve Caviation,” by Z.J. Wu et al., pp. M555-M561 (undated).
“Caviation in Pumps, Pipes, and Valves,” Process Engineering, by Dr. Ronald Young, pp. 47 and 49 (Jan. 1990).
“Quantification of Heart Valve Cavitation Based on High Fidelity Pressure Measurements,” Advances in Bioengineering 1994, by Laura A. Garrison et al., Bed-vol. 28, pp. 297-298 (Nov. 6-11, 1994).
“Monitoring and Diagnosis of Cavitation in Pumps and Valves Using the Wigner Distribution,” Hydroaccoustic Facilities, Instrumentation, and Experimental Techniques, NCA-vol. 10, pp. 31-36 (1991).
“Developing Predictive Models for Cavitation Erosion,” Codes and Standards in A Global Environment, PVP-vol. 259, pp. 189-192 (1993).
“Notification of Transmittal of the International Search Report or the Declaration”, Nov. 7, 2002, (PCT/US02/06606).
“Notification of Transmittal of the International Search Report or the Declaration”, Jan. 3, 2003, (PCT/US02/30465).
“Self-Diagnosing Intelligent Motors: A Key Enabler for Next Generation, Manufacturing System,” by Fred M. Discenzo et al., pp. 3/1-3/4 (1999).
“Notification of Transmittal of the International Search Report or the Declaration” for PCT/US01/40791.
“Notification of Transmittal of the International Search Report or the Declaration” for PCT/US01/40782.
“Improving Dynamic Performance of Temperature Sensors With Fuzzy Control Techniques,” by Wang Lei et al., pp. 872-873 (1992).
“Microsoft Press Computer Dictionary” 2nd Edition, 1994, Microsoft Press, p. 156.
09/855,179, May 14, 2001, Eryurek et al.
09/852,102, May 9, 2001, Eryurek et al.
09/576,719, May 23, 2000, Coursolle et al.
09/799,824, Mar. 5, 2001, Rome et al.
“A Microcomputer-Based Instrument for Applications in Platinum Resistance Thermomety,” by H. Rosemary Taylor and Hector A. Navarro, Journal of Physics E. Scientific Instrument, vol. 16, No. 11, pp. 1100-1104 (1983).
“Experience in Using Estelle for the Specification and Verification of a Fieldbus Protocol: FIP,” by Barretto et al., Computer Networking, pp. 295-304 (1990).
“Computer Simulation of H1 Field Bus Transmission,” by Utsumi et al., Advances in Instrumentation and Control, vol. 46, Part 2, pp. 1815-1827 (1991).
“Progress in Fieldbus Developments for Measuring and Control Application,” by A. Schwaier, Sensor and Acuators, pp. 115-119 (1991).
“Ein Emulationssystem zur Leistungsanalyse von Feldbussystemen, Teil 1,” by R. Hoyer, pp. 335-336 (1991).
“Simulatore Integrato: Controllo su bus di campo,” by Barabino et al., Automazione e Strumentazione, pp. 85-91 (Oct. 1993).
“Ein Modulares, verteiltes Diagnose-Expertensystem für die Fehlerdiagnose in lokalen Netzen,” by Jürgen M. Schröder, pp. 557-565 (1990).
“Fault Diagnosis of Fieldbus Systems,” by Jürgen Quade, pp. 577-581 (Oct. 1992).
“Ziele und Anwendungen von Feldbussystem,” by T. Pfeifer et al., pp. 549-557 (Oct. 1987).
“PROFIBUS-Infrastrukturmaβnahmen,” by Tilo Pfeifer et al., pp. 416-419 (Aug. 1991).
“Simulation des Zeitverhaltens von Feldbussystemen,” by O. Schnelle, pp. 440-442 (1991).
“Modélisation et simulation d'un bus de terrain: FIP,” by Song et al, pp. 5-9 (undated).
“Feldbusnetz für Automatisierungssysteme mit intelligenten Funktionseinheiten,” by W. Kriesel et al., pp. 486-489 (1987).
“Bus de campo para la inteconexión del proceso con sistemas digitales de control,” Tecnologia, pp. 141-147 (1990).
“Dezentrale Installation mit Echtzeit-Feldbus,” Netzwerke, Jg. Nr.3 v. 14.3, 4 pp. (1990).
“Process Measurement and Analysis,” by Liptak et al., Instrument Engineers' Handbook, Third Edition, pp. 528-530, (1995).
IEEE Transactions on Magnetics, vol. 34, No. 5, Sep. 1998, “Optical Design of the Coils of an Electromagnetic Flow Meter,” pp. 2563-2566.
IEEE Transactions on Magnetics, vol. 30, No. 2, Mar. 1994, “Magnetic Fluid Flow Meter for Gases,” pp. 936-938.
IEEE Instrumentation and Measurement, “New approach to a main error estimation for primary transducer of electromagnetic flow meter,” pp. 1093-1097.
“Additional Information From Flowmeters via Signal Analysis,” by J.E. Amadi-Echendu and E.H. Higham, pp. 187-193.
Continuation in Parts (2)
Number Date Country
Parent 09/257896 Feb 1999 US
Child 09/383828 US
Parent 08/623569 Mar 1996 US
Child 09/257896 US