METHOD AND SYSTEM FOR DETECTING PLATE CLASHING IN DISC REFINERS

Abstract: A method and system for the detection of plate clash­ ing in disc refiners and provided herein. The signal from either an acoustic or vibration monitor (12) is processed through a filter (14) which isolates those frequencies at which a significant increase in signal level is known to occur during a clash or are generated in association with imminent or actual plate clashing. The signal level of the filtered data is compared with a threshold level (19) at which protective action must be taken. Protection can be automatically initiated by the plate clash detection system; alternatively, it can be done manually by an operator, using the detection system as a warning device.

Description: METHOD AND SYSTEM FOR DETECTING PIRATE CLASHING IN DISC REFINERS This invention relates to a method and means for the detection of plate clashing in disc refiners. Such refiners are'used for processing a material, e.g., a pulp suspension or a mixture of wood chips, water and chemicals. A disc refiner includes two discs at least one being rotatable relative to the other and forming between them a nairow, slot-shaped chamber. Each disc is an assembly of wedge-shaped segments bolted or otherwise secured to the surface of a circular plate holder; the number of segments per disc is specific to the refiner type. The discs are so arranged that they are displaceable toward and away from one another for adjustment of the size of the chamber and the resulting pressure exerted on the material beLng refined. Under load, the refining pressure forces the material in the chamber into the form of a pad which prevents destructive contact between the two refiner plates. Should the pulp pad break down, du-e either to process or to machine disturbances or machine failure, plate contact can occur until the pad reforms, the operator releases the plate pressure, or the attendant change in motor load causes the load protection circuits automatically to open the plates. The degree of damage incurred by the plates during the contact period (dependent npon the contact pressure and the period's duration detenines whether they thell have to be replaced with a new set. Plate replacement is often necessary. The capacity of refining units is rapidly increasing and the cost of plate replacement is closely following this same trend. Downtime on a single unit is giving rise to both larger process disturbances and production losses. At the present tine, no effective means exists tor anticipating an imminent clash, or for early detection once it occurs, that is suitable for industrial application. A refiner operator can, with careful attention hear the sound of metal-to-metal contact during a clash. His effectiveness, however, varies according to the resident environmental noise and the type of refiner casing. Often, the operator is not near enough to the refiner to hear the emitted souJs and, if they are heard, it is difficult to initiate preventative action before plate damage occurs. General purpose electronic equipment is available for sound and vibration analysis. Two categories of equipment which are available include on-line real-time signature analyzers, and machine protection systems. Neither of these systems has, as yet, been used for plate clash protection, and both have serious drawback-s that limit their applicability in this area. On-line signature analyzers are used for the characterization of input signals. They suffer from both high cost and complexity. Plate clashing develops rapidly; signature analyzers do not permit input data to be analyzed quickly enough to allow preventative action to be taken before destructive plate damage occurs. There is no facility for the automatic detection of the relevant phenomena nor for preventative action. Machine protection systems do not have the selectivity required for singling out clash data in an accurate and consistent manner. Thus, the pecularities of the monitored signal, during periods of plate clash, are not readily identifiable with such equipment. Peak detection, upon which machine protection systems depend, is highly err,atic due to the nature of the clash phenomena. Consequently, an object of a broad aspect of the present invention is to provide a consistent and reliable means for the early detection of the plate clash phenomena so that preventive action can then be taken to minimize plate damage and reduce process upsets. The present inventio. is predicated on the use of the energy level in either the vibration or the acoustic signal from a refining unit to warn of plate clashing. Consequently, by a broad aspect of this invention, a refiner plate clash detection system is provided, comprising (a) means for receiving a first signal generated in association with imminent or actual plate clashing, having at least one distinct frequency related to the clash, (b) filter means having a passband matched to said at least one distinct frequency of said first signal through which said at least one frequency is passed, and (c) means for generating an alarm signal when the amplitude of the filtered first signal has exceeded a predetermined level. By one variant thereof, the clash detecting system further includes means fur maintaining the alarm signal on until manually reset by an operator. By another aspect of this invention, a refiner plate clash detection system is provided comprising: (a) means for receiving a first signal generated upon plate clashing having at least one distinct frequency related to the clash, (b) filter means having a passband matched to pass the distinct frequency of said first signal to provide a filtered output signal, (c) means for smoothing the filtered signal (d) means for establishing a threshold level, (e) comparator means for receiving said filtered signal and for comparing it with the threshold level, and for providing an output signal of predetermined form, upon said first signal exceeding said threshold level, and (f) means for receiving said output signal and for generating an alarm operation signal in response thereto. By one variant, the system further includes signal smoothing means connected to the output of the filter means for receiving said first signal and for providing a varying D.C. voltage output signal to the comparator related to the average aqXitude of said first signal, the means for providing a threshold signal comprising adjustable D.C. voltage supply means. By one variation thereof, the signal smoothing means comprises an RIilto-DC voltage converter. By another variation the means for receiving the output signal includes a circuit including a bistable flip flop operated in one state in response to said output signal , for generating an alarm signal. By yet another variation, the system includes resetting means for restoring said flip flop to its other state and thus shutting of said alarm signal. By another variant, the system includes a vibration sensor mounted on said refiner for sensing vibration and for generating said first signal in response thereto. By a further variant, the system includes an accelerometer mounted on said refiner for sensing axial vibration and for generating said first signal in response thereto. By yet another variant, the system includes a microphone for generating said first signal. By a further variant, the centre frequency of the passband of the filter is determined by the formula f0 =n wherein f0 is the center frequency of said passband, n = the number of segments at a given radius, per single disc and R R = the sum of the rotational rates of the two discs enclosing the giver. refining volume. By yet another variant, the system includes a relay operated by said alarm operation signal for automatically opening the refiner plates for reducing the refining pressure or for shuttling off the power to the motor turning the refiner plates when the alarm means indicates a clash. By a further aspect of this invention a method is provided for detecting plate clashing in disc refiners which comprises: determining the frequency at which a significant increase in signal level occurs during a plate clash; monitoring the acoustic or vibration frequencies of the disc refiner; continuously determining the signal level of the acoustic or vibration frequencies; continuously comparing that signal level with a predetermined threshold signal prior to a plate clash and automatically signalling when the signal level exceeds the threshold level. By a variant thereof, the frequency is determilled by the formula fO = n C R wherein fO = a clash frequency, n = the member of segments, at a given radius, per single disc and 2 R = the sum of the rotation rates of two adjacent discs enclosing the given refining volume. The basis of broad aspects of the present invention was bhe discovery of the inter-relationship between the power spectral densities of the vibration and acoustic signals, and a clash of refiner plates. During a clash, the power in certain frequency bands increases significantly over that observed under normal running conditions. The frequency bands over which the most interesting changes occur stretch from just above D.C. to 2.5 KEIz for an acoustic signal and to 7 KIIz for a vibration signal. The vibration signal can be derived from a commercially available accelerometer placed strategically for monitoring vibrations, preferably in the axial direction of the refiner, or located or imbedded in the refiner casing, while the acoustic source can be a microphone in proximity to the unit. Indeed, there may he evidence that the distinct signal frequencies related to a clash occur just prior to a clash. In the use of the broad concepts of this invention, a maximum emergy threshold is established over a chosen frequency band for each signal type (vibration or acoustic) which is only exceeded during plate clashing. By monitoring the translated voltage or current output level of the vibrational or acoustic sensors in the selected band, the plate clash alarm is initiated when the respective threshold level is crossed. The width of the frequency band is a tradeoff between the need to monitor all frequencies at which significant changes in power level occur (for stability and repeatability of the alarm) and the need to keep the band narrow substantially to eliminate frequencies wliich have no role (for noise elimination, sensitivity and reliability). The threshold level is esbablished taking into consideration the necessity of detecting all plate clashes and, at the same time, minimizing false alarms. The basis for the discovery upon which broad aspects of the present invcntion is based was originally derived from the observed operation of a Sprout-Waldron, 12,000 horsepower, Tvin-50 refiner. However, it is equally applicable to other refining units having discs which rotate relative to each other. The increase in signal power during the period of a plate clash was noted from an analysis of the acoustic and vibration data. However, a superiority of the vibration signal over the acoustic one in the power analysis was found to exist. Because of the greater stability of the power level in the vibiation signal during normal refiner operation, and its more rapid increase on the occurrence of a clash, the use of a vibration monitor as the signal source is preferred, although the invention is not restricted thereto. To provide effective plate clash protection, en appropriate frequency band over which the sensor signal voltage can be measured must be specified. Ideally, the selected band should be independent of the refiner type and should bu predetermillel such that no adjustment is required at the mill site. As a band suitable for all refiner types may not exist, it is preferable to be able to specify it by its relationship to certain characteristics of the refiner to be protected. It has not been possible to locate a single frequency band that is known to be suitable for use with all disc refiners tested. However, for all refiners tested, certain major modes of vibration have been noted and, for most, it haJ been possible to relate these to the plate configuration and the disc rotation rate. During plate clash, most refiners eMlibit pronounced peaks in vibration energy at frequencies given by either the passing rate of the disc segments, f0, or its harmonicas. These frequencies are of particular importance for this application due to their relative frequency stability, and their peaking effect during a clash. For a given refining volume, the frequency of Vibration fO is defined by: f0 = (the number of segments, at a given radius, per single disc) (the sum of the rotation rates of the two discs enclosing the given refining volume) (1) assuming that the number of segments per disc is identical. For these refiners, the required frequency during plate clash ing is selected on the basis of the exhibited modes of vibration during clasliing, with Equation (1) scrving as the basis for the frequency search. Frequency selection for all other refiners is done experimcntally, with a thorough analysis of the respective vibration signal. In the accompanying drawings: Figure 1 is a block diagram of an embodiment of the plate clash detector system of one aspect of this invention; Figure 2 is a graph of a typical output signal amplitude of a vibration sensor against frequency; and Figure 3 is a more detailed block diagram of an aspect of this invention. Description of Figure 1 As seen in Figure 1, a signal source 11, which may be the output of a sensor which is a vibration monitor 12, e.g. an accelerometer or tlse output of a microphone located adjacent to the discs is fed to a filter 14 (e.g. preferably a 4 pole Butterworth filter) which has a center frequency c and a bandwidth W. The filtered signal 15 is smoothed in smoothing circuit 16. The signal 17 of the smoothed filtered signal is compared with a predetermined threshold level 18 from alarm signal threshold circuit 19. If the signal level 17 equals or exceeds the threshold level 18, an alarm monitor circuit 20 is activated, and an alarm signal 21 is provided. Description of Figure 2 Figure 2 shows the amplitude vs. frequency of typical output signals from a vibration monitor during plate clashing. The signal is generally of low amplitude across the lower portions of the audio frequency band and in the absence of clashing, would be at the approximate low amplitude across the entire band. However, upon clashing of the plates, it has been found that relatively very hl amplitude signals occur at specific frequencies (which will be discussed in more detail below). In the present example of Figure 2, there is clearly a welldefined peak at 360 Hertz (as well as at 120 Hertz). Operation of Embodiment of Figure 1 In use, the signal from either a vibration or acoustic sensor which forms the vibration monitor is passed through a filter having centre frequency c and bandwidth W, both fe and W being matched to the frequency of the signals produced upon clashing of the discs. The centre frequency of the filter for the signal spectrum shown in Figure 2 should thus be at 360 Hertz. After filtering, the signal is smoothed (for example, by converting the RMS level to a D.C. voltage level) which signal is then compared with a predetermined threshold signal (i.e. a D.C. threshold voltage). If the threshold level is exceeded, some form of alarm is activated or protective action is taken, as desired. The system can be implemented using hard-wired circuitry (analog or digital), an appropriately programmed digital computer, or a hybrid of each. There are various electrical circuits that can achieve the objects described above. In one particular embodiment shown in block diagram in Figure 1, the input signal is provided by a commercially available accelerometer which is mounted to monitor axial vibrations on the refiner easing, powered by a constant current source of conventional construction. This input signal is then filtered by a filter, with one or more passband frequencies set such that the vibrational frequencies within the desired monitoring bank are passed unattenuated. A gain stage raises the signal level to an appropriate value, for ease of detection, and this signal is RMS-to-DC converted to obtain a smoothed varying D.C. signal level. The D.C. signal is applied to a comparator with a referee D.C. threshold signal, which triggers downstream alarm circuits when the threshold level is exceded. A visible and audible alarm can be provided to alert the refiner operator. Additionally, a relay is preferably provided which can be used either automatically to open the refiner plates or to reduce the refining pressure, when a clash is identified. The audible alarm and protection relay, once triggered, should be reset by the operator, while the visible alarm turns ON and OFF with the alarm condition. Description of Figure 3 A more detailed block diagram of an aspect of this invention is shown in Figure 3. An input signal from the vibration monitor, which can be either an accelerometer, microphone, etc. as noted earlier is applied to input terminal 25. The bandwidth of the accelerometer should extend at least between 1 and 7,u00 Hertz, which includes all of the frequencies of interest in the present case. The specific translation bandwidth of the circuit is preferably defined by a bandpass filter. This can be implemented by using a series of a J)air of filters, the first being a low pass filter 26 connected to tile input of a high pass filter 27, wi tii the input terminal 25 connected to tile input of low pass filter 26. Of course, filters connected in parallel can be used to pass diferent frequencies of the signal related to the clash. Preferably, the high frequency band-end of tiie low pass filter is variable, as is the low frequency band end of high pass filter 27. By varying the band-ends, a passlealld can be produced which has a frequency width sufficient to encompass the peaking vibrational signal produced during a clash, and having a centre frequency at the midpoint of the peaking: signal. The output of high pass filter 27 is connected to the input of an amplifier 25, the output of which is applied to the input of an RMS-to-DC converter 29. The output of the RMS-to-DC converter 29 is connected to one input of comparator 30, the other input of which is connected to nn adjustable D.C. voltage source, e.g., the tap on potentiometer 31 which is connected between ground and a source of potential +V. It is also preferred that the output of the RMS-to-DC converter 29 should be connected to the input of a voltmeter 32 through a switch 33. The voltmeter 32 is also connected to the tap of potentiometer 31 through an amplifier 34 and switch 33. The output of comparator 30 is connected to one of the inputs of a bistable flip flop 35, the other input of which is connected through a reset switch 36 to a source of potential +V. The output of flip flop 35 is connected to a relay 37 which has its contact connected to an alarm terminal 38 for operatioll thereof. In operation, the normal signal outputs of the sensor, which are at low level as shown in ligure 2, are applied to terminal 25 of the plate clash monitor. The signals are filtered in low pass and high pass filters 2G and 27, and are normally at low amplitude voltage level. Howevcr, in the case of a plate clash, a relative high level signal at the frequency of the bandpass of the combination of filters 26 and 27 is generated, and passes therethrough. The signal at this frequency is amplified in amplifier 28, and applied to RMS-to-DC converter 29. In converter 29 the signal is effectively smoothed, and a relatively constant, or relatively slowly varying D.C. signal is applied to comparator 30. The other input of comparator 30 has a preset threshold D.C. signal applied thereto. Once the output signal of cons-er- ter 29 exceeds the aforenoted threshold signal, an output signal is produced from comparator 30 and is applied to the input of flip flop 35. With the polarity of the input signals from comparator 30 being proper, flip flop 35 operates and remains stable in the operated state. An output signal thus results and is applied to relay 37, which itself operates and remains on. Wit its contacts closed, an alarm connected to tcrminal 38 is thus operated and remains operated. Once an operator has become alerted, and wishes to shut-off the alarm, he manually closes reset switch 76, which resets flip flop 35 into its original state. The output signal of flip flop is thus removed, (unless further clashing of the plates is encountered), and thus relay 37 is released, shutting off the alarm. One relatively simple way of setting the alarm threshold level is to place switch 33 in position by which meter 32 monitors the D.C. output signal of converter 29. The highest level D.C. signal is monitored during the non-clashing periods. In addition, the minimum high amplitude signal level is noted during a clashing period. Switch 33 is then switched into position at the output of amplifier 34. Amplifier 34, being a nullity gain buffer amplifier, does not change the level of the D.C. voltage signal which is input to the comparator and is read on meter 32. potentiometer 31 is then adjusted to a level intermediate the highest level normal D.C. output signal from converter 29 and the lowest level signal present during clashing. Of course other ways of setting the threshold can be utilized if desired. It will be understood by a person slcilled in the art that numerous variations and additions to the circuit noted above can be provided. For example, while comparator 30 has been dexeribed as being in analog forum, it can be strobed and its output signal be of pulse form, Flip flop 95 can operate in synchronization therewith, and operate an audible alarm with its output pulses directly. Other means can be used to locle up a relay (either electromagnetic or solidstate) whereby a constaiit alarm wliich niust be manually reset i S operated. The accelerometer may be that sold by Unholtz-Dickie as Model 8805 accelerometer with magnetie base. The filter may be a series of a low pass filter and a high pass fi 1 ter to define the passband; the low pass filter may be that sold fly Frequency Devices as Model 744PB-3, a four pole Butterworth low pass filter. The high pass filter may be that sold by Frequency Devices as Model No. 774BT-3, a four pole Butterworth resistive tuneable highpass filter. The RMS-to-DC converter may be that sold by Analog Devices as Model No. 441J. A series of trials have been cai-:'ied out to eluci date the range of application of the described sensor. Both the distinctiveness of the clash phenomena as well as the possibilities for frequency band selection were examined, for various refiner types. The lack Of a good sensor for measuring plate separation makes it difficult to quarantee when plate clashing actually occurs. Consequently, the described frequency phenomena was related to plate clashing in three ways: (a) experienced refiner operators were used to help identify a clash occurrence; (b) linear velocity displacement transducers, LVDT's, were used to monitor plate movement; (c) forced clashes were initiated without chips, where the only possible contact between tile plates was metal-tometal. SPROUT-WALDHON TWIN - 50 (6o Hertz Supply) - Eight clashes were studied. The accelerometer was located on the refiner casing, measuring vibration in either the axial or radial direction. Along with the vibration signal, the motor load, the chip-belt speed and a measure of plate movement from an LVDT were recorded. It was found that: (i) At a frequency of 360 Hz, there was a pronounced increase in the amplitude of the vibration during a clash. (ii) The total energy in tile signal (the integral over frequency of the vibration spectrum) did not vary significantly during a clash (iii) Using Equation (1), the nmniber of plate segments (12) multiplied by the rotation speed (30 Hz) located the dominant vibration mode, 360 Hz. (iv) Better clash detection resulted with the accelerometer measuring vibration in the axial direction. SPROUT-WALDRON TWIN-50 (50 Hertz Supply) - Results are similar to those obtained with this refiner operating from a 60 Hz supply, excepting the location of the dominant vibration mode. The dominant frequency was 300 Hz, equal to the product of rotation speed (25 Hz) and the member of plate segments (12). SPROUT-WALDRON 42-1A - Two clashes were analyzed, with the accelerometer measuring radial vibration. It was found that: (i) The first clash gave rise to three large peaks at 720, 1440 and 2160 Hz, respectively. (ii) The second clash showed a dominant peak at 2160 Hz. (iii) The energy peaks were located at frequencies that are integral multiples of 360 Hz, the product of rotation speed and tie number of plate segments. SPROUT-WALDRON 42-1R - Three separate trials were conducted on this refiner, with the following results: (i) A peak at 360 Hz was always present during clashing. (ii) The total energy in tlie vibration signal could diminish during a clash; nevertheless, the amplitude of the vibration at 360 Hz still increased. (iii) The rotatioii speed (30 rotations per second) multiplied by the number of segments (12) located the 360 Hz mode. SPROUT-WALDRON 361-CP (Pressurized) - To clashes ere observed, with the sensor measuring axial vibration. A distinct peak at 610 and 625 Hz was noted for each, respectively. It was also noted that: (i) There was a slight shift in frequency between the clashing and non-clashing con;itions, likely caused by a small change in the speed of rotation of the induction motor. (ii) The noted frequencies could not be related to the rotation speed of the disc and the number of segments, using Equation (1). However, it is believed that this is due to rotational speed changes of the disc due to the clash. BAUER 400 - This is a double-disc refiner driven by to induction motors. The nominal speed of disc rotation is 1200 RPM and each refining plate is made up of six segments. It was found that: (i) With both discs rotating, a major energy peak was located between 215 and 240 Hz, during a clash. The latter frequency was equivalent to the product of the number of segments per plate (6) and the sum of the rota-tion frequency of each of the two counter-rotating discs (40 Hz). (ii) There was a slight shift in the peaking frequency and this was related to variations in the rotation speed of the induction motors during clashing. (iii) For certain clashes, the second harmonic (480 Hz) of the characteristic frequency appeared as the main mode of vibration. For others, the characteristic frequency, the second harmonic, or both, could be present. (iv) With only one disc rotating, a major peak was found around 100 IIz, during clashing. This was lower than the expected frequency of 120 Hz and it is thought tiiat this may be due to variations in the rotational speed of the disc. BAUER 412 - Vibrations were measured in the axial direction. A peak in energy is found at 480 Hz, which is the sceolti harmonic of the frequency calculated using @ Equation (1). DEFIBRATOR RPL50 - Each di se plate on this refiner has three different sections. The outer one has 12 segments, the middle section has eight and the inner section has four, The middle section on the stationary disc can be moved slightly in the axial direction. Tests were made with the sensor monitoring axial vibration. It was found tiat: (i) There was a large peak at 960 llz, surrounded by peaks of smaller amplitude, 50 liz apart. (ii) A vibration peak also occurred at 480 Hz, suggest- ing that the middle section of the discs, made up of eight segments, were contactillg. Using Equation (1), the base frequency calculated was 240 Hz for 8 sections and 50 Hz rotation. DEFIBRATOR RPL50 (Pressurized) - The dise configuration is the same as that described previously. With the sensor measuring vibration, in the axial direction, a series of peaks were again evident, with the one at 720 Hz particularly outstanding at the beginning of the clash. The prior peaks are again 30 Ilz apart. This suggests that the olter part of the dise, with 12 segments, was clashing. The results of these varioios tests, together wi @th tlic expected peaks calculated using Equation (1), are listed in Table 1. TABLE 1: Summary of Test Results; Refiner Clashing. DISC NO. OF SEGMENTS PER ROTATION ROTATING DISC, AT f OBSERVED FEFINER TYPE RPM/RPS DISCS GIVEN RADIUS Hz PEAKS(Hz) Sprout-Waldron Twin-50 1800/30 1 (per 12 360 360 (60 Hz) volume) Sprout-Waldron Twin-50 1500/25 1 (per 12 300 300 (50 Hz) volume) Sprout-Waldron 720 42-1A 1800/30 1 . 12 360 1440 2160 Sprout-Waldron 42-1B 1800/30 1 12 360 360 Sprout-Waldron 616 361-CP 1800/30 1 9 270 630 Bauer 215 400 1200/20 2 6 240 240 Bauer 412 1200/20 2 6 240 480 Defibrator (Open- 1800/30 1 . 4-Inner 120 Discharge) 8 - Middle 240 960 12-Outer 360 Defibrator 4-In er 120 (Pressurized) 1800/30 1 8-Middle. 240 720 12 Outer 360 vibration measurements in the axial direction were generally found to give better results than those in the radial. Except for some preliminary trials, tlic sensor was always located as close as possible to the refining chamber, wherein the alarm frequencies originate. In the case of the Sprout-Waidron Twin-50, sensor position is more crucial as there are two refining chambers to monitor; identification of the clashing disc-set is important in those situations where clashing can be prevented by the adjustment of either the chip feed rate or the dilution water flow. It may be advantageous to use two vibration sensors, one to monitor each refining chamber, to identify the clashing Sec. In summary, teste have been carried out on fourteen refiners, of nine different tyres. Clashing has been initiated by either reducing the chip feed or by forcing the plates closer together. In all cases, the vibration signal exhibits a very large increase in amplitude at specific frequencies, at the time of plate clash. With one exception, the Sprout Waldron 361-CP, observed frequencies were equal to either a fundamental frequency, fO, or its harmonics. The Sprout Waldron Twin-50, as well as the 42-1B, show high vibration energy at the fundamental frequency, fO. All other refiners tested, excepting the Sprout-Waldron 361-CP, have a major vibration mode at the second harmonic of the fundamental frequency. The Bauer 400 peaks at the expected fundamental frequency. The second harmonic, however, is often the dominallt one. The ease and reliability of vibration measurement makes the use of an accelerometer very desirable. It was noted that there were very distinct changes in the frequency spectrum of the vibration signal at the time of plate clashing. It was observed that the total energy in the vibration signal, over the total frequency range analyzed (0 to 5 300 Hz), tended either to increase or to remain constant during plate clashing. There were instances, nonetheless, where this total energy was reduced. In all cases, however, the energy level at the characteristic frequency, fo, or its harmonics always increased during clashing. From the foregoing description, one skilled in tìhe art e?n easily ascertain the essential chllacteristics of this invention, and without departing from the spirit and scope thereof, can make various changes and modifications of the invention to adapt it to various usages and conditions. Consequently, such changes and modifications arc properly, equitably, and "intended" to be, within the full range of equivalence of the following claims.

Claims: CL The embcdiments of the invention in which an exclusive prcpcrty or privilege is claimed are defined as follows: 1. A refiner plate clash detection system comprising: (a) means for re receiving a first signal generated upon plate clashing having at least one distinct frequency related to the clash, (b) filter means having a passband matched to pass said distinct frequency of said signal to provide a filtered output signal, (c) means for smoothing said filtered signal, (d) means for establishing a threshold level, (e) comparator means for receiving said filtered signal and for comparing it with said threshold level and for providing an output signal of predetermined form, upon said first signal exceeding said threshold level, and (f) means for re receiving said output signal and for generating an alarm operation signal in response thereto. 2. A refiner plate clash detection system as defined in claim 1, further including signal sroothing means oonnected to the output of the filter means for re receiving said first signal and for providing a varying D.C. voltage output signal to the comparator related to the average amplitude of said first signal; the means for establishing a threshold level comprising ar:justable D.C. voltage supply means for providing a D.C. threshold signal. 3. A refiner plate clash detecting system as defined in claim 2, in which the signal smoothing means comprises an R@ S-to-DC voltage converter. 4. A refiner plate clash detecting system as defined in claim 3, in which the means for receiving the output signal includes a circuiit including a bistable flip flop operated in one state in response to said output signal, for generating an alarm signal. n = the number of segments at a given radius, per single disc and #R=the sum of the rotational rates of the two discs enclosing the given refining volume. 12. The system of claims 2, 4 or 9 including a relay operated by said alarm operation signal for automatically opening the refiner plates, for reducing the refining pressure or for shutting off the power to the motor turning the refiner plates lhen the alarm means indicates a clash. 13. A method of detecting plate clashing in disc refiners which coMprises: determining the frequency at which a significant increase in signal level occurs during a plate clash; monitoring the acoustic or vibration frequencies of the disc refiner; continuously determining the signal level of the acoustic or vibration frequencies; continuously coMparing that signal level with a predetermined threshold signal prior to a plate clash; and automatically signalling when the signal level exceeds the threshold level. 14. The method of claim 13 wherein the frequency is determined by the formula fo = n#R wherein fo = a clash frequency n = the number of segments, at a given radius, per single disc and #R= the sum of the rotation rates of two adjacent discs enclosing the given refining volume.

Inventors: BUTLER, DONALD JAMES, ROGERS, JAMES HUBERT
Applicants: PRICE (NFLD.) PULP & PAPER LIMITED, PULP AND PAPER RESEARCH INSTITUTE OF CANADA
Application year: 1979
Main classification: G08B21
IPC codes: D21D1, G01H1