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The measurement of forces in chip refiners 2001

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THE MEASUREMENT OF FORCES IN CHIP REFINERS By SEYED MOHAMMAD Al I SIADAT B.Eng. (Mechanical Engineering), McMaster University, 1997 A THESIS SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF APPLIED SCIENCE In THE F A C U L T Y OF G R A D U A T E STUDIES Department of Mechanical Engineering We accept this thesis as conforming to the required standard THE UNIVERSITY OF BRITISH COLUMBIA March 2001 © S. M. Ali Siadat, 2001 In presenting this thesis in partial fulfilment of the requirements for an advanced degree at the University of British Columbia, I agree that the Library shall make it freely available for reference and study. I further agree that permission for extensive copying of this thesis for scholarly purposes may be granted by the head of my department or by his or her representatives. It is understood that copying or publication of this thesis for financial gain shall not be allowed without my written permission. The University of British Columbia Vancouver, Canada Department DE-6 (2/88) ABSTRACT The purpose of the chip refining process in the pulp and paper industry is to produce wood pulps and to enhance certain desirable properties of the fibres in the pulp suspension, by subjecting the wood material to cycles o f shear and compressive stress. This process has commonly been quantified in terms o f energy-based parameters such as specific energy and refining intensity, but such methods, although useful for establishing energy-pulp quality relationships, do not describe the underlying fundamental mechanisms o f the process. It has been suggested that a knowledge of the stress-strain history o f individual fibres can yield a deeper understanding o f the process [Page, Fundamental Research Symposium (1989)]. Wi th the long-term goal of such an understanding, the forces experienced by pulp in the refining zone are measured in a laboratory refiner operating at 700 rpm with softwood T M P at 16% consistency. This is done using a two-axis force sensor, originally designed by A . Bankes, P. W i l d and D . Ouellet. The design, in its original form, did not perform well enough to provide a reliable force measurement under the high excitation frequency of passing refiner bars, as the sensor's resonant frequency was too low. A modified design with a much higher natural frequency is presented here, along with force measurements in the refining zone for various plate clearances, and varying dilution flow rate. From these measurements, we see that both the normal and shear forces contain a component due to the ploughing action o f the corner of the bar through the floe (termed i i the comer force), a phenomenon previously only seen in the shear force [Batchelor et al. J. Pulp Pap. Sci . 23(1) (1997), Senger et al., Proceedings of the International Mechanical Pulping Conference, (2001)]. The peak normal force increased with decreasing plate clearance, while the peak shear force measured by the sensor did not exceed U N , corresponding to a maximum shear force per unit bar length of 2.2 kN/m. The equivalent tangential coefficient o f friction decreased with decreasing plate clearance, and also decreased upon the addition o f dilution water. The sensor design needs further refinement for testing at higher refiner rotational speeds, as signals acquired at high speeds are distorted by the sensor's resonant vibrations. i i i CONTENTS ABSTRACT LIST OF TABLES , LIST OF FIGURES. ACKNOWLEDGEMENT 1. INTRODUCTION. 2. REFINING THEORY. 2.1 Energy-Based Refining Theories 2.1.1 Introduction To Energy-Based Refining Theories 2.1.2 L o w Consistency Refining Theory 2.1.3 High Consistency Refining Theory 2.2 Force-Based Refining Theories. 2.2.1 Forces In L o w Consistency Refining 2.2.2 Forces In High Consistency Refining 2.3 Research Objectives 3. ORIGINAL SENSOR DESIGN 3.1 Design Details 3.2 Impact Tests & Calibration. 3.3 Refiner Tests Using Original Sensor Design 3.4 Discussion Of Preliminary Test Results. 3.4.1 Calibration 3.4.2 Dynamic Behaviour 3.4.3 Sensor Fabrication iv 4. MODIFIED SENSOR DESIGN 3 7 4.1 Design Modifications 37 4.1.1 Machining O f Housing Parts 37 4.1.2 Piezo Ceramic Elements 38 4.1.3 Insulating Material 38 4.1.4 Housing Support 39 4.1.5 Damping Mechanisms 41 4.1.6 Further Stiffening O f Sensor 41 4.2 Impact Tests & Calibration 43 4.2.1 Sensor Response To Combined Normal A n d Shear Loads 43 4.2.2 Effect O f Impact Position 48 5. REFINING TRIALS. 50 5.1 Experimental Setup 50 5.2 Refining Force Profiles 51 5.2.1 Bar Passing Events 51 5.3 Data Rejection Criteria 55 5.3.1 Sensor Vibrations 56 5.3.2 Cycl ic Fluctuations In Normal Force Wi th Each Rotation 59 5.4 Analysis & Discussion 62 5.4.1 Impact Statistics 62 5.4.2 Variation O f Shear Force Wi th Plate Clearance 63 5.4.3 Effect O f Injecting Dilution Water 65 5.4.4 Variation of \k,eq Wi th Plate Clearance & Consistency 65 v 5.4.5 Ranges O f Measured p^eq & Average Pressure 67 6. CONCLUSIONS 71 BIBLIOGRAPHY. 73 NOMENCLATURE 76 APPENDIX A: Specifications O/D2B502 Refiner Plates 79 APPENDIX B: Properties OfPiezo Ceramic Elements 80 APPENDIX C: Calibration Procedure 81 APPENDIX D: Matlab Programs 96 APPENDIX E: Estimated Length Of Bars Crossing at Any Given Time 100 v i LIST OF TABLES 1.1 Differences between chip refiners and pulp refiners 4 4.1 K-Values determined by impacting the sensor at different angles 45 4.2 Variation o f sensitivity (K-values) o f piezo elements 2 and 3 with varying impact position on the top face o f the probe. A l l K-values are in V / N , and a is the standard deviation 49 5.1 Summary of impact statistics for refining runs at 700 rpm (a is the standard deviation) 63 5.2 Values o f constants from different sources for use in Equation 2.8 (SI and S2 refer to primary and secondary stage processes, respectively) 68 v i i LIST OF FIGURES 1.1 Schematic diagram o f a chip refiner 2 3.1 Components o f the preliminary sensor design 20 3.2 Sensor installed in refiner plate for measuring forces during refiner operation 21 3.3 Impact testing o f sensor (mounted in jig) using force hammer. Impacts in the x- direction correspond to the direction of bar impacts at the leading edge during refiner operation 23 3.4 Force hammer impact in time and frequency domain 23 3.5 Response o f sensor (from piezo elements 1 & 3) to a normal impact at the probe tip ...24 3.6 Variation o f peak signal voltage from piezos 1, 2 and 3 with impact force for normal impacts 25 3.7 Average transfer functions for piezo elements 1 and 3 in response to 20 vertical impacts 27 3.8 Signals from piezo elements during refiner operation. Bar passing events cannot be distinguished as vibrations dominate the signal 30 3.9 Refining forces derived from the above signals. The fine line corresponds to the forces calculated from piezo elements 1 and 3, while the bold line uses the combination of piezo elements 2 and 3 30 3.10 The variation o f the refining forces over a period of 1 second, as derived from different piezo combinations. The periodic behaviour corresponds to the rotor plate rotation 32 3.11 Comparison o f measured with calculated values o f the normal force for impacts applied to the sensor when mounted in the plated 33 3.12 Exaggerated diagram showing how the piezo elements deform as the probe is displaced 35 4.1 Sensor housing design changes 38 4.2 Average transfer functions for piezo elements 1 and 3, with the new housing modifications and the 2 mm-wide piezo elements 40 4.3 Sensor used in conjunction with shims in order to inhibit deformation o f housing 40 v i i i 4.4 Effect o f using latex pads in conjunction with layers of mica in the shims. The time domain signal of piezo element 3 is shown in response to an impact from the force hammer 42 4.5 Transfer functions for piezo elements 1 and 3, for revised sensor design with all new modifications 42 4.6 Impacts administered at different angles by using aluminum wedges 44 4.7 A comparison of the true normal component with values calculated from Equations 4.4a and 4.5a 47 4.8 A comparison o f the true normal and shear components with those calculated from Equations 4.4b and 4.5b 47 4.9 The moving load during a bar passing event. A s the rotor bar moves across the top o f the probe, so does the centre o f pressure 48 5.1 Refining normal force (bold line) and shear force (fine line) at 700 rpm as calculated using piezo combinations 2-3 and 2-4 52 5.2 One o f the three segments of the D2B502 rotor plate (the stator plate segments are identical) 53 5.3 The normal (bold line) and shear forces (fine line) due to a typical bar impact 54 5.4 A n illustration o f problematic 30 k H z resonant vibrations o f the sensor 56 5.5 Typical force profiles of bar impacts at 2560 rpm 57 5.6(a) Sensor vibrations at approximately 2 k H z 58 5.6(b) 2 k H z vibrations grow in amplitude for five successive bar impacts, until a sixth impact from a wider bar reduces their amplitude. This record shows several successive occurrences o f this phenomenon 58 5.7 Cycl ic fluctuations in normal force with each rotation at 2560 rpm 60 5.8 Variation o f plate clearance and mean normal force through one full rotation o f the rotor plate 61 5.9 Equivalent tangential coefficient o f friction versus plate clearance 66 5.10 Plot o f the equivalent tangential coefficient of friction against average mechanical pressure for different refiners 68 ix ACKNOWLEDGEMENT The author wishes to thank the many people whose help eased the task of preparing this thesis. To Dr. D . Ouellet for the priceless guidance provided throughout my experience as a Masters' student. To J. Senger for the many helpful discussions and valuable feedback, and for generally being a pleasure to work with. To R. Nagy for the technical support to combat the seemingly endless computer problems. To Dr. P. W i l d , A . Bankes, M . Olmstead and B . Shiari for much helpful input regarding the force sensor. To P. Taylor for the meticulous fabrication of sensor parts. To T. Paterson, K . Wong, L . Brandly, B . Dutka, J. Marsden, B . M c M i l l a n , R. Penko, J. Mackenzie, G . White, Dr. R. Thiruvengadaswamy, and Dr. G . Stewart for providing help in many areas during m y time at the Pulp & Paper Centre. To the N C E Mechanical Wood Pulps Network for funding my project. A n d most of all , to my parents for ceaseless love and support throughout my time as a student (and as a human being, for that matter). x 1. INTRODUCTION Refiners are used in the pulp and paper industry to mechanically separate fibres from the wood matrix and to enhance certain pulp properties. The former o f the two actions, commonly termed mechanical pulping, is carried out in chip refiners at high consistency. Here, wood chips are fed into the refiner and fibres are peeled away from the wood structure by repeated cycles o f shear and compressive stresses. This mechanism affects the physical properties o f the individual fibres, and o f the paper ultimately made from these fibres. The most common type of refiner is the disc refiner, illustrated schematically in Figure 1.1. Pulp is fed through the inlet, and moves between the two refiner plates, one stationary and the other rotating at high speed (commonly 1800 rpm in North America, and 1500 rpm in Europe). Both plates have a bar and groove pattern, and are separated by a small gap through which the pulp flows. A s the rotor bars pass over the stator bars, agglomerates of pulp fibres are trapped repeatedly between the passing bars, and in this way receive the cyclic loading that constitutes the mechanical action o f refining. These loading events are the topic of study in this work, for they are the basic cause of the changes to the fibre structure. The nature o f the changes in the refined pulp is strongly dependent on the absolute and relative magnitudes o f these loads and the number o f loading cycles received by each fibre. These factors are influenced by the plate 1 Outlet Figure 1.1 Schematic diagram of a chip refiner. pattern, the refiner rotational speed, the pulp consistency, the plate clearance and the residence time o f pulp in the refining zone. A l l these variables come under consideration depending on the desired result. A t this point, we must make a distinction between chip refining and pulp refining. Chip refining is the production o f pulp from wood chips by refining at high consistency, whereas low consistency pulp refining is carried out to develop the properties o f fibres that have already been separated by chemically dissolving the wood substances that bind them together. 2 In chip refiners, it is desired first to break down the wood chips and free the individual fibres, and then to enhance their flexibility. The chips are first impacted at the beginning o f the refining zone with a coarse bar pattern that becomes progressively finer as we move radially outwards through the refining zone. The breaker bar section is tapered slightly to allow for a larger plate gap in this region, which narrows to a smaller gap at the intermediate bar section, and often continues to narrow all the way to the outer radius o f the refining zone. Due to the high energy mechanical action in chip refiners, large amounts o f steam are produced between the refiner plates, causing high temperatures and pressures that are not encountered in the lower consistency pulp refining process. The purpose of pulp refining is to alter the properties of the fibres, which have already been separated from the wood matrix, to a state that best serves the final product. Therefore, the breaker bar section is not required in this application, and usually there is only one type o f bar that spans the refining zone. A s a result o f the lower consistency, pulp refining is carried out at a much lower plate clearance than chip refining. The key differences between pulp and chip refiners are summarized in Table 1.1. Due to these differences (most notably in the flow of pulp), the refining action in the two processes is characterized differently. On a very basic level, however, the action o f the two types o f refiners is similar, as in both cases the wood material is repeatedly beaten by passing refiner bars. Therefore, there are some similarities in the characterization o f the different types o f refiners. 3 Chip Refiners Pulp Refiners Consistency High (20-60%) Low (3-5%) Plate diameter 36 to 68 inches (0.91 to 1.73 m) 32 to 48 inches (0.81 to 1.22 m) Speed 1500 rpm in Europe 1200 or 1800 rpm in North America (although some 1st stage refiners run at up to 2300 rpm) 600 to 900 rpm Plate Clearance 0.5 to 3 mm 0.06 to 0.2 mm Specific Energy 1.5to3.5MWh/t 80 to 250 kWh/t Pulp Flow Pulp is propelled by forces inside refiner Pulp suspension is pumped through refiner Table 1.1 Differences between chip refiners and pulp refiners. In order to predict the extent of the refining treatment received by the fibres, a number o f theories have been put forward. For the most part, these have been based on the net mechanical energy transferred to a unit mass of pulp, and the "intensity" at which this energy is applied. This approach has proven useful in developing relationships between key operating variables and the quality of the resulting pulp suspensions, and the simplicity o f some of these energy methods has facilitated their widespread use. However, when it comes to understanding the fundamental mechanisms of refining, such energy-based theories offer limited insight, because they make no attempt to describe the mechanisms by which the energy was transferred to the fibres. Refined fibres undergo a variety of structural changes due to the different modes o f loading they experience. Passing bars cut and bend fibres, and subject them to cyclically varying normal and shear stresses. Furthermore, the effects also depend on the combinations o f the modes o f loading and the relative magnitudes o f these loads. A general objective o f the work presented here is to develop a better understanding o f high consistency refining based on the forces encountered in the process. This work w i l l 4 focus on measuring the forces that are experienced between refiner bars and examining how they are affected by operating conditions. The basis o f our approach was to develop a two-axis force sensor capable o f withstanding the harsh conditions present inside an operating refiner, and to use this sensor to measure forces at various plate clearances, consistencies and rotational speeds. The refiner used in this study is a 12-inch Sprout Waldron laboratory refiner. The force sensor used was originally designed by A l a n Bankes [1], and was modified in order to improve its behaviour. The modified design is useful for tests on the laboratory refiner, operating at speeds up to 700 rpm, above which meaningful force measurements are not possible as sensor vibrations dominate the signal. This thesis begins with a review of refining theories and previous investigations regarding the refining forces. The focus then shifts to the development, testing and use o f the refiner force sensor. This is followed by an analysis of force measurements made during refiner operation. 5 2 . REFINING THEORY Characterization o f the action of refining has evolved over the years to enable producers of pulp to predict the effects o f different operating conditions. This chapter w i l l review the key theories put forward to characterize the action o f both high consistency and low consistency refining. The review w i l l focus first on energy-based theories for the two types o f processes, and then on research into forces experienced by pulp floes in refiners. This w i l l set the stage for a summary of the objectives of the work presented in this thesis. 2.1 ENERGY-BASED REFINING THEORIES 2.1.1 INTRODUCTION TO ENERGY-BASED REFINING THEORIES The most widely used parameter for characterization of the degree o f refining at both high and low consistency is the specific energy, which is defined as the energy transferred per unit mass of pulp. It is calculated from: E = — (2.1) mf where P is the net power transferred to the pulp and mf is the oven-dry fibre mass flow rate through the refiner. On its own, the specific energy is not enough to fully characterize the refining action, because o f differences in types and sizes of refiner, plate designs and operating conditions. Therefore, two trials with pulp refined to the same specific energy can exhibit very different results, as the different effects of refining on the fibres (internal and external fibrillation, fibre cutting, etc.) can occur to different extents. This is true for both high consistency [2] and low consistency processes [3]. It was therefore necessary to develop a second parameter which, when used in conjunction with the specific energy, would allow us to predict the effects o f refining by accounting for other important refining conditions. This additional parameter generally attempts to quantify the severity or intensity of the refining treatment by estimating the amount o f energy transferred to pulp with every refiner bar impact. The number o f impacts received by each fibre is directly dependent on the time it spends in the refining zone (the residence time). In low consistency refiners, pulp is pumped through by an external pumping system, and the liquid nature o f the suspension allows a simple calculation of the residence time based on geometric considerations and the flow rate o f the pulp suspension. In high consistency chip refiners, the pulp suspension behaves more like a wet solid than a liquid, and no pump is used. Therefore, the velocity of the pulp through the refiner is determined by considering the forces acting on it, such as the centrifugal force, contact forces with the refiner plates, and drag forces from the large amounts o f steam produced during the process. Because o f these key differences in the way pulp flows through low and high consistency refiners, the measures o f refining intensity differ in these two cases. They w i l l therefore be reviewed separately in the next two sections. 7 2.1.2 LOW CONSISTENCY REFINING THEORY There have been many suggestions for the form of the refining intensity parameter at low consistency. A s the name suggests, this parameter, in all its forms, describes the severity with which the energy treatment is imparted to the pulp. The definitions o f the measures of intensity discussed here are all in the form: P 1 = (2.2) constant where / is the intensity and P is the net power. The form of the constant in the denominator distinguishes the different ways of measuring the intensity. In low consistency processes, the most commonly used intensity measure is the specific edge load (SEL), defined as [4]: P P SEL = -^— = ^ - ^ - (2.3) CEL X " " » „ A c o The denominator here is known as the cutting edge length {CEL). It is the total length o f bar crossings per second in the refining zone. The values nri and nSi are the number of bars on the rotor and stator, respectively, in a radial increment i, Z,- is the length o f the refiner bar within the radial increment, and co is the rotational speed o f the refiner (revolutions per second). The SEL is therefore a measure o f the energy transferred per unit length of bar, measured in J/m. 8 This intensity measure is based on the design o f the plates in use, but neglects many parameters that are known to have an effect on the mechanical treatment. A major criticism o f the SEL theory is that it ignores parameters such as groove depth, bar and groove widths, and bar angle, although it has been suggested that some of these parameters are indirectly accounted for [5]. In response to these criticisms, extensions to the SEL theory were devised that included some of these other plate parameters. Among these were the Modified Edge Load (MEL) [6] and Specific Surface Load (SSL) [7] theories. Other theories were not limited to plate design parameters, as factors such as pulp consistency, unrefined fibre properties and plate clearance had yet to be addressed. Possibly the most comprehensive o f all intensity measures to date, in terms of accounting for all the relevant factors in the refining process, comes from Kerekes' C-factor theory [3]. This theory accounts for plate parameters, pulp properties and operating variables, and also allows for an estimation of the number of impacts received by each fibre, as wel l as the average energy associated with each impact. However, due to its more complex nature than the SEL-type theories, the C-factor theory is not as widely used in industry. 2.1.3 HIGH CONSISTENCY REFINING THEORY One o f the greatest influences in the understanding of high consistency refining came when Miles and M a y published their highly successful model of the flow o f pulp in chip refiners [8] in 1990. They followed it up a year later with extensions on the theory and experimental results to support the work [9]. Their approach consists of considering the 9 forces acting on an element of pulp in the refining zone to predict its radial velocity, which is then used to estimate the residence time. The model predicts that this element of pulp is acted on by centrifugal and frictional forces, along with the drag forces exerted by the copious amounts o f steam generated in the refiner. The equation derived for the radial velocity of the pulp, v, as it relates to the radial position in the refining zone, r, is: where CO is the refiner's rotational speed, c is the pulp consistency (fraction), \ir and are the coefficients o f friction in the radial and tangential directions respectively, r\ and are the inner and outer radii o f the refining zone, a is a constant that equals 4 for a single-disc refiner and 2 for a double-disc refiner, and S is a term related to the steam flow. The steam flows backward (i.e. counter to the flow o f pulp) near the inlet of the refining zone, and forward near the outlet, exerting no force on the pulp at the stagnation point in between. Therefore, by assuming that the effects of the backward and forward flowing steam cancel each other out, the equation is simplified by removing the steam flow term [10]. A further simplification can be made by assuming that the pulp velocity gradient is small relative to other terms in Equation 2.4, and the differential equation is then reduced to a simple algebraic equation. The residence time, %, can then be determined using: dv _ rco 2 dr v — a Vr Ecjr) II, a>( r 2 2 - r , 2 ) + S (2-4) (2.5) 10 and the number of impacts experienced by each unit of pulp, nimp, is: where Nav is the average number of bars per unit length of arc. Using this, Mi les and M a y then coined an intensity measure for the chip refining process. This is the specific energy per impact, e: F e = — (2.7) TV av Thus, as Mi les , M a y and associates have shown [8-11], a two-parameter energy-based characterization can be used to predict certain pulp property changes associated with changes in refining conditions. 2.2 FORCE-BASED REFINING THEORIES To their credit, researchers have come a long way in predicting the response o f pulp to refining by quantifying the process in terms of energy-based parameters. However, all o f these characterizations possess the common shortcoming that none can describe the exact mechanisms of the energy transfer. A variety o f structural changes are experienced by the fibres in the process, among which internal fibrillation, external fibrillation, fibre shortening and the creation o f fines are the main ones. The type of loading seen by the fibres is the direct influence for these changes, but none o f the energy based characterizations yield an understanding o f these effects. The following sections are dedicated to the research that has focused on the refining forces in order to gain a 11 complete, detailed picture of the mechanical phenomena occurring inside a refiner. The cases of high and low consistency are again taken up separately. 2.2.1 FORCES IN LOW CONSISTENCY REFINING In 1989, Page described his vision of the forces acting on an agglomerate o f pulp fibres (a floe) as it is trapped between passing bars in the refining zone [12]. He envisioned three main forces in refining: a normal component (perpendicular to the faces o f the bars) due to the compression of the floe, a shearing component (in the direction tangential to the relative motion of the bars) due to friction between the pulp and the bars, and a "ploughing" force (also known as the 'corner force') required for the bar corners to plough through the floe. Page himself did no work to measure these forces. One o f the first attempts to quantify the refining forces was described by Khlebnikov et al. at the Leningrad Institute for the Pulp and Paper Industry. They used sensors to determine the forces in a conical refiner operating at 2-3 % consistency [13]. They measured forces in two perpendicular directions on the face of a refiner bar, those directions being normal to the face o f the bar (the normal force) and tangential to the motion o f the bar (the tangential force, or shear force). They plotted the shear force profile that they measured due to individual bar passing events where floes were trapped between opposing refiner bars. The shear force was seen to rise sharply at the start of the event, then fall sharply to a much lower level where it remained essentially constant until the trailing edges o f the bars in question parted ways. 12 The sensor designs they used were based on strain gauges, and these designs were revised the following year [14] before being used by Goncharov, who then implemented their use in a disc refiner [15]. He reported similar force profiles to those o f Khlebnikov et al. In retrospect, it seems likely that the initial peak in the shear force was due to the corner force described by Page twenty years later, and the lower, constant force regime that followed it was the friction force between the pulp and the metal faces o f the refiner bars. The initial high force regime was seen to act for a greater portion of the bar passing event when the plate clearance was decreased. The overall magnitudes of the forces measured were seen to rise with increasing consistency, increasing operating speed, and decreasing plate gap. Khlebnikov et al. defined the ratio of the tangential force to the normal force as the coefficient of refining, and saw that it increased for decreasing plate clearance and for increasing speed. Goncharov reported a coefficient of refining o f approximately 0.11 for unbleached sulphite pulp at 2.5-3 % consistency refined at 720 rpm. He also quoted peak pressures at the bar surface of around 3.4 M P a for the initial high force regime. In 1981, Nordman et al. measured pressures in grooves and on bar surfaces in a disc refiner at low consistency, running at 1200 rpm [16]. They registered pressure peaks on the bar surfaces that corresponded to bar passing events, although these were somewhat more erratic in nature than those depicted by Khlebnikov et al. Nordman et al. reported peak to peak pressures o f 0.08-0.12 M P a due to bar passing events - more than 20 times lower than those reported by Goncharov. 13 In 1997, Martinez, Batchelor, Kerekes and Ouellet published work done to characterize and model the forces on pulp floes when trapped between opposing refiner bars at low speed (corresponding to approximately 1 rpm) [17,18]. Their tests were performed on a specially designed machine, called the single-bar refiner. This could compress and shear one floe o f pulp at a time in the same way as would occur between opposing refiner bars, while measuring forces in the normal and tangential directions. In this way, they could examine the effect of single bar passing events on individual floes. They used spherical nylon floes at a consistency o f 9.5% and assumed linear elastic behaviour to develop and test a force model. These tests showed evidence of a corner force component in the shear force. After this initial peak, the shear force dropped to a lower constant value. The normal force profile rose to a peak at the beginning of the bar passing event, and remained essentially constant until the trailing edges o f the passing bars parted ways. The model was later modified by Batchelor and Ouellet to consider previously dried kraft pulp fibres with collapsed lumens. It was also extended to predict the tensile forces experienced by individual fibres. According to the model, the tensile force to which a fibre is subjected depends on the location and orientation o f the fibre within the floe, as well as the size o f the trapped portion of the floe [19]. 14 2.2.2 FORCES IN HIGH CONSISTENCY REFINING In 1975, Atack et al. measured the temperature and pressure at different locations in the refining zone in a single-disc, open-discharge refiner operating at 1800 rpm and discharge consistencies of 20-50% [20]. Although they could not see the details o f bar passing events, they did see pressure "spikes" at the frequency at which bars passed over the pressure sensor. These spikes were seen to be as high as 620 kPa at times. Atack later suggested that the magnitude o f these spikes would be influenced by the size o f floes [21]. In their pressure measurements, Atack et al. also observed cyclic pressure fluctuations (approximately 28 kPa in magnitude) with each rotation o f the rotor plate, upon which the spikes were superimposed. Having correlated this cyclic variation with variations in the plate separation due to run-out in the rotor plate, they concluded that this periodic fluctuation was due to the saturated steam pressure in the refining zone. In later work, Atack et al. used high-speed photography to show that periodic variations in the amount o f pulp present at any given area o f the refining zone occur due to that same rotor run-out phenomenon [22]. In 1982, Franzen and Sweitzer studied the variation of the total axial thrust with varying motor load, specific energy and consistency [23]. They quantified the refining forces in terms o f the total axial thrust and a tangential friction force (which draws the torque from the motor) between the plates. The latter was defined as proportional to the axial thrust, 15 the constant o f proportionality being a coefficient of friction. They proceeded to claim (referring to extensive unpublished work by Fisher) that this coefficient o f friction increased with increasing consistency. The resultant tangential friction force was envisioned to act at a certain radial distance from the centre of the plates, and this distance was shown to vary depending on the operating conditions. Mi les and M a y derived the following simple equation for this coefficient o f friction for a non-pressurized refiner [8]: IP p : = — (2.8) ha>Fm(rl+r2) where ]it is the tangential coefficient of friction, P is the motor load, Fm is the total axial thrust, rj and o are the inner and outer radii o f the refining zone, respectively, CO is the rotational speed o f the refiner (rad/s) and h is the number o f rotating discs (1 or 2). Using data from a Bauer 914 m m atmospheric double-disc refiner operating at 1200 rpm, they plotted the motor load against the axial thrust for different pulp consistencies (15, 20 and 30%) and found all points to fall on the same straight line, indicating that the coefficient of friction was independent o f consistency. From the slope of the line, they calculated a value of 0.75 for Furthermore, they suggested that \it was independent o f the radial position in the refining zone. A s the tangential speed o f a refiner bar is proportional to the radial position at which the speed is measured, this implies that \it would also be independent o f refiner speed. 16 Most recently, Senger and Ouellet used the single bar refiner apparatus o f the work o f Martinez et al. and Batchelor et al. to examine the forces on T M P floes at high consistency and low speed [24]. They showed nonlinear elastic behaviour at high consistency, and presented clear evidence o f the corner force component in the shear force. A s the corner force was seen to represent a large part o f the shear force, the ratio of the shear to the normal force could no longer be considered a true coefficient o f friction, and they coined a new variable, the equivalent tangential coefficient o f friction \it,eq, as this ratio. \\,t,eq was shown to increase with increasing consistency and with increasing floe grammage, and it was seen to decrease with an increasing extent o f bar wear. 23 RESEARCH OBJECTIVES The fact that energy-based characterizations do not refer directly to the mechanisms by which refining causes structural changes in the fibres leaves us in search o f a force-based theory by which we can completely quantify and predict the effects o f refining. Such a theory has yet to be developed, and before this can happen much work needs to be done in understanding the refining forces themselves. This is not the only reason to study the refining forces. Given that the refining process is energy intensive, it becomes even more desirable to understand its underlying mechanisms, as it could help to reduce energy costs in the long run. 17 The objectives of the work presented here can be summarized as follows: - To design and implement the use o f a two-axis force sensor for a refiner operating at high consistency - To measure the normal and shear forces experienced by pulp floes during bar passing events To investigate how these forces are influenced by operating conditions. Work was begun on the first of these three objectives by A . Bankes, P. W i l d , and D . Ouellet prior to the start of the work presented as part of this Master's thesis. The original design and preliminary testing of the force sensor comprised the work done as part o f the Master's degree o f A . Bankes. This work is described in detail in his Master's thesis [1], and summarized in the next chapter. 18 3. ORIGINAL SENSOR DESIGN The work o f Bankes included the original design of the sensor, the building and testing o f a large-scale prototype, and the construction and testing of a preliminary version o f the force sensor for use inside the laboratory refiner at the U B C Pulp and Paper Centre. The reader is referred to Bankes' Master's thesis for details on the design concept and the large-scale prototype [1]. The testing of the original design was performed at U B C , and marked the beginning o f the work done as part of this thesis. The objectives for the tests described in this chapter were: to develop and implement a calibration procedure, to examine the sensor's dynamic behaviour, to examine force traces from the refiner and identify bar passing events, to bring to light any other issues involved in the design, fabrication, assembly and use of the sensor. 3.1 DESIGN DETAILS The original design o f the sensor is depicted schematically in Figure 3.1 in terms of its separate components, and the assembled item is shown in Figure 3.2. This design was devised by A . Bankes in collaboration with P. W i l d and D . Ouellet [1]. The workings o f the force sensor can be summarized as follows: The sensor's T-shaped probe is held inside the housing, completely supported by the four piezo ceramic 19 elements under preload, such that any displacement of the probe relative to the sensor housing w i l l deform the piezo elements. Figure 3.1 Components of the preliminary sensor design. According to [1], signals from two piezo elements from opposite sides of the sensor probe tip (one from the left and one from the right, as pictured in Figure 3.1) can be used to uniquely determine the magnitude and direction of the force acting on the probe tip. The calculation o f these forces is described in Section 3.2. The sensor probe tip has the same shape as a refiner bar, and was designed as such to replace a 5 mm-long section of a bar. A hole was machined in the back of a D2B502 refiner plate (see Appendix A for specifications) in which the sensor fits snugly, with the probe tip replacing the removed bar section. 20 T Probe Top Plate Figure 3.2 Sensor installed in refiner plate for measuring forces during refiner operation. The piezo ceramic material used for the elements was lead zirconate titanate (PZT), whose ferro-electric behaviour is specified in Appendix B. The piezo elements in the original design were 1 mm X 1 mm X 7 mm in size, and were clamped under preload along the 5 mm length that was in contact with the probe. An insulating layer was required to prevent conduction between the electrodes of the piezo elements and the sensor's metal parts. In the preliminary design, small sheets of paper were glued to the appropriate locations on the sensor probe and housing for this purpose. The adhesive used was a Loctite™ cyano-acrylate product. To prevent water from entering the sensor housing, it was sealed around the edges at the last step of the assembly using a silicone sealant. 21 3.2 IMPACT TESTS & CALIBRATION The response o f the refiner force sensor was characterized using a P C B 086D80 piezoelectric impact hammer. This device, used i n conjunction with an appropriate signal conditioner, gives an output signal whose voltage is proportional to the magnitude o f the force experienced at the tip of the hammer head. The impact testing setup is illustrated schematically in Figure 3.3. The force hammer reliably measures forces up to 60 N , and the impacts provide excitation up to very high frequencies (see Figure 3.4). A s a result, it is ideal for testing the sensor's response in both the time domain and the frequency domain. The original calibration method consisted o f impacting the sensor in two perpendicular directions, which corresponded to the directions of the normal (y-direction) and shear (x- direction) refining forces. However, this method cannot be used when the sensor is mounted in the refiner plate, because the neighbouring bars obstruct the hammer's path when trying to apply horizontal impacts. Therefore, the sensor was held in a vice for the calibration presented in [1], where it could easily be impacted in the two directions. It was later noted by the author o f this work that the vice did not adequately replicate the sensor's mounting conditions in the refiner plate, and so a specially designed j i g (depicted in Figure 3.3) was constructed to hold the sensor for the impact testing. The geometry o f the j ig 's contacting surface with the sensor is identical to that of the refiner plate. 22 y Figure 3.3 Impact testing of sensor (mounted in jig) using force hammer. Impacts in the x-direction correspond to the direction of bar impacts at the leading edge during refiner operation. Time (ms) n 100f 1 80 Q L I I 1 I I I I I i l 0 10 20 30 40 50 60 70 80 90 100 Frequency (kHz) Figure 3.4 Force hammer impact in time and frequency domain. 23 The sensor was struck with the hammer and the resulting piezo signals were analysed. Piezo elements emit negative signals when compressed, and positive signals when extended1. A sample impact with the corresponding sensor output signals is shown in Figure 3.5. CD 80 60 40 S | 20 X 0 so 3 > 1 ^ 2 0 -2 -4 -6 a o 1.4 1.6 1.8 2 Time (ms) 2.2 1 / I I 1 1 i 1.4 1.6 1.8 2 2.2 2.4 / 1 1 1 1 1 \j\f\^ 1.4 1.6 1.8 2 2.2 2.4 I \ 1 1 1 1 2.4 Figure 3.5 Response of sensor (from piezo elements 1 & 3) to a normal impact at the probe tip. The magnitude of the first peak of each piezo element signal was seen to be directly proportional to the peak amplitude of the force hammer signal, for impacts in both the normal and shear directions. This is expressed mathematically as: 1 The terms compression and extension, as used here, should be understood as being relative to the preloaded state. As the piezo elements are under preload, they are always under compressive stress. When the preload is applied, the piezo elements emit a signal for a brief period of time and then this signal fades to zero. Subsequently, the piezo elements emit no charge unless further relative deformation takes place. If the elements are then extended relative to the preloaded state, even though they are not experiencing a positive tensile stress, they will emit a positive signal. 24 Vi=KiNFN (3.1a) VrKiSFs (3.1b) where the subscript i denotes the piezo element number, Vt is the voltage from piezo element i, FM and Fs are the normal and shear force magnitudes, respectively, and KIN and Kis are the normal and shear calibration coefficients (in V / N ) . The former relation, as an example is illustrated graphically in Figure 3.6. Piezo Voltage vs Impact Force (y-direction) 4 i Hammer Force (N) Figure 3.6 Variation of peak signal voltage from piezos 1,2 and 3 with impact force for normal impacts. A t this point, it was assumed that the response from each piezo element to an impact at an arbitrary angle 0 to the y-direction (a combined normal and shear load) was equal to the sum of the responses to the normal component F cos& and the shear component F sinQ. This assumption of the validity of linear superposition is tested in Section 4.2. For now, the following relations are assumed to hold: FN = FcosQ (3.2a) Fs = FsinQ (3.2b) Vt =KiNFN + KiS Fs = F(KiN cosQ + KiS sinQ) (3.3) 25 where F is the magnitude o f the resultant force. It should be noted here that these calibration coefficients KJS and Km were determined by impacting the sensor in the aforementioned j ig , after which the sensor was transferred to the refiner plate and again impacted in the normal direction to see how the response compared to that in the j ig . Invariably, the values o f KJN determined from the plate and the j i g differed, sometimes by up to 20%. Due to this discrepancy, the K-values subsequently used for force calculations were not those determined directly from the j i g configuration. Instead, the value of KIN from the plate was used, and Kts was calculated using the following equation: KiN{jig) This assumes that the normal and shear calibration coefficients change proportionately when the sensor's mounting conditions change. The validity o f this assumption was difficult to verify in practice, and this represents a serious limitation o f this calibration method. A more reliable method o f determining the value o f Kts was therefore developed and w i l l be presented in Section 4.2. Using Equation 3.3, one can derive equations for the forces FN and Fs given the voltage from any two piezo elements on opposite sides of the probe tip. These w i l l be in the form: FN=CiVi+CjVJ (3.5a) Fs=DiVi+DJVj (3.5b) 26 where i and j are the numerical designations of the piezo elements on either side o f the probe, and the values o f C and D for these piezo elements can be determined using the K - values above. A detailed description o f this calibration procedure, including the determination o f all relevant constants, is given in Appendix C . The average transfer functions of piezo elements 1 and 3 are depicted in Figure 3.7 for frequencies up to 15 kHz . Transfer functions were calculated for several impacts and averaged over the range o f frequencies according to: f n . . \ Hi(f) = 20log J,(\r,(f)'r>(f)\)j (3.6) Piezo Element 1 5 Frequency (kHz) Piezo Element 3 Frequency (kHz) Figure 3.7 Average transfer functions for piezo elements 1 and 3 in response to 20 vertical impacts. 27 where Hi ( / ) is the magnitude (in dB) o f the average transfer function at frequency / a n d Vt(f) and Vh(f) are the magnitudes of the signals from piezo / and the hammer, respectively, at said frequency. We can see that the transfer function is markedly different between piezo elements 1 and 3. In both cases, the transfer function exhibits several peaks, first in the region between 1 and 3 k H z , and then above 8 k H z or so. This behaviour was unexpected, since a finite element analysis of the system, carried out by Bankes, indicated that the lowest natural frequency should be about 25 kHz . The cause o f this discrepancy was not immediately apparent, but w i l l be examined later in this chapter. 3.3 REFINER TESTS USING ORIGINAL SENSOR DESIGN The force sensor was used to measure forces in the U B C Pulp and Paper Centre's Sprout- Waldron 12-inch laboratory refiner. This refiner is non-pressurized, and is run using a 50 horsepower (35 k W ) motor. The motor load is controlled by manually varying the plate clearance. The low natural frequency quoted above for the force sensor must be compared with the frequency at which bars on the refiner's rotor plate pass over the sensor probe during refiner operation, as this is the major frequency component of the excitation force. W e calculate the bar passing frequency using the following equation: / - J l ^ (3.7) J b p 60(5 + G) 28 where Q is the refiner speed (rpm), r s is the radial position (m) o f the sensor on the refiner plate, and B and G are the bar and groove widths (m), respectively, on the rotor plate. On the D2B502 plates used here, the sum B + G is 5.4 mm, and the sensor was at a radial distance o f 14.6 cm from the axis of rotation o f the rotor plate. Thus, for a speed of 2560 rpm (full speed), fbp is 7.2 kHz , and for 1260 rpm, fi,p is 3.6 kHz . Under normal circumstances, the refiner can be run at any desired speed up to 2560 rpm using a variable frequency drive. However, the drive emits large quantities o f electrical noise which interfere with the data acquisition. This drive had to be bypassed as a result, and the refiner speed could only be varied by changing the configuration o f the pulleys over which the drive belts ran. This allowed us to run the refiner at only two speeds: 1260 rpm and 2560 rpm. Ideally the sensor should be an overdamped system with a natural frequency much higher than the frequency o f excitation, so that the sensor's natural vibration does not affect its ability to measure the refining forces. However, from the data presented in Figures 3.5 and 3.7, we can see that this sensor has a low natural frequency and is underdamped. W e could therefore expect that the sensor's vibration behaviour would dominate the signal, and prevent accurate force measurement. Indeed, this is exactly what was observed. Figure 3.8 shows a 10 ms time trace o f the individual piezo signals during refiner operation, and Figure 3.9 shows the force traces derived from those piezo signals. The signals are clearly dominated by the sensor's vibration, as can be seen in their sinusoidal 29 0 -0.1 -0.2 646 647 648 649 650 651 652 653 654 655 0 S -0.1] -0.2 646 647 648 649 650 651 652 653 654 655 0 > ^ -0.1 o N U £ -i 645 646 647 648 649 650 651 652 653 654 655 Time (ms) Figure 3.8 Signals from piezo elements during refiner operation. Bar passing events cannot distinguished as vibrations dominate the signal. be o PL, £ i - I o 6 4 2 0 -21 H r- n i r- n r _1 I L j I L. 645 646 647 648 649 650 651 652 653 654 655 Time (ms) 1 o Pi u eo U JS o- -1- - | 1 rr r n 1 1 r 645 646 647 648 649 650 651 652 653 654 655 Time (ms) Figure 3.9 Refining forces derived from the above signals. The fine line corresponds to the forces calculated from piezo elements 1 and 3, while the bold line uses the combination of piezo elements 2 and'. 30 nature. Wi th the bar passing frequency at 3.6 kHz , the time between bar passing events is 0.28 ms, and no such events can be distinguished from the trace, neither in the piezo signals nor in the force trace. A n interesting feature can be seen in Figure 3.10, where the forces are plotted for 1 second of refiner operation. The periodic variation of the force trace corresponds exactly to the refiner's rotational speed. This is due to the run-out on the rotor plate, which effectively causes a cyclic variation in the plate clearance. The pulp between the plates thus sees a periodic, varying level o f compressive strain, and this comes through in the force reading. It should be noted that the forces calculated from the combination o f piezo elements 1 and 3 differ from those calculated from combination 2 and 3, in both Figures 3.9 and 3.10. This aspect was not examined in [1] and is discussed in the following section. 31 Refining Forces Calculated from Piezo Elements 1 & 3 J i_ 100 200 300 400 500 600 700 800 900 Time (ms) J i _ 100 200 300 400 500 600 700 800 900 Time (ms) „ 2 z S -1 Refining Forces Calculated from Piezo Elements 2 & 3 0 100 200 300 400 500 600 700 800 900 Time (ms) _ i i i i _ 0 100 200 300 400 500 600 700 800 900 Time (ms) Figure 3.10 The variation of the refining forces over a period of 1 second, as derived from different piezo combinations. The periodic behaviour corresponds to the rotor plate rotation. 32 3.4 DISCUSSION OF PRELIMINARY TEST RESULTS 3.4.1 CALIBRATION The equations reported earlier for force determination proved reliable, and the calibration o f the sensor was successful (see Figure 3.11). However, some doubts remained with regard to interpreting the piezo element responses in terms o f the linear superposition assumption o f Equation 3.3. Impact testing using a large-scale model suggested that the assumption was not valid [1], and such a test had yet to be devised and carried out for the prototype. This test is described in Section 4.2. 0 10 20 30 40 50 60 70 Measured Force (from force hammer) (N) Figure 3.11 Comparison of measured with calculated values of the normal force for impacts applied to the sensor when mounted in the plated. There was also the noted shortcoming of using the mounting j i g to calibrate the sensor, when K-values differed significantly between cases where the sensor was mounted in the j i g and those where it was mounted in the refiner plate. It thus became necessary either to verify Equation 3.4, or to devise a method by which the K-value for shear forces could be determined with the sensor mounted in the plate. The latter o f the two options was selected, and this is also described in Section 4.2. 33 3.4.2 DYNAMIC BEHAVIOUR O f all the aspects of sensor behaviour that were studied in these tests, its vibration characteristics emerged as the area most in need o f improvement. The sensor's low natural frequency was the reason for the vibration problems, as explained earlier. Given that the bar passing frequency was 3.6 kHz , and higher frequency components were present in the excitation, a sensor capable of measuring forces in such an environment would need a significantly higher natural frequency than that o f this design. Ideally, an overdamped system would also be desirable. The forces experienced could not be determined with any certainty, neither qualitatively nor quantitatively, not only due to the vibrations, but also due to the fact that signals from piezo elements on vertically opposite sides of the sensor probe were not consistent with expectations. To clarify this point, consider the case shown in Figure 3.12. Assuming that the dominant factor controlling the piezo signal is the normal stress in the y- direction, as piezo element 1 is extended (relative to the preloaded state), its signal should be positive, while piezo element 2, being compressed, should give a negative signal. Therefore, we would expect piezo elements 1 and 2 to exhibit signals o f opposite sign at all times (and the same would be expected o f piezo elements 3 and 4). In reality, this was not the case (see, for example, Figure 3.8 in previous sections). 34 Bottom Plate Figure 3.12 Exaggerated diagram showing how the piezo elements deform as the probe is displaced. One possible explanation for this is that the piezo signals are not only dependent on the normal stress experienced by the elements, but also on shear stresses to a significant extent. Although such a ferro-electric material behaving ideally would not respond to shear stress, it was confirmed that the elements used here were not behaving ideally, as the polarization direction of some parts of the crystal structure were not perfectly aligned with the poling direction [1]. Another possible explanation for the discrepancy between piezo element pairs is that the sensor housing was not perfectly rigid, contrary to earlier assumptions. Relative deformation of the top and bottom plates o f the housing would not only explain this, but would also account for the discrepancy between the natural frequency predicted by the finite element model and the value observed experimentally. Subsequent testing confirmed this suspicion, as w i l l be explained in the following chapter. 3.4.3 SENSOR FABRICATION Piezo ceramic elements would often crack during sensor assembly, and imperfections in the machined finish of the sensor housing were seen as the root o f the problem. The 35 piezo elements would effectively rest on ridges left by the machining tools, and would thus bend and break when the preloading screws were tightened. The lack o f good contact between the piezo surfaces and the top and bottom plates was also suspected to reduce the stiffness o f the assembly. To compound the problem, the piezo elements' dimensions (most importantly the thickness in the y-direction) varied significantly from one element to the next. This caused further difficulties in keeping the top and bottom plates parallel during assembly, and made it hard to ensure that all piezo elements saw the same preload. A l l o f the issues explained above led to the conclusion that significant modifications to the sensor were required before a reliable refiner force measurement would be possible. The following chapter is dedicated to the necessary modifications and their effects on the sensor's behaviour. 36 4. MODIFIED SENSOR DESIGN In an effort to address the problems with sensor performance that were outlined in the previous section, several design modifications were examined. Considerable efforts were also devoted to finding the cause o f the low natural frequency of the sensor. These steps led to an improved sensor design which is presented in this chapter. Improvements to the calibration procedure were also necessary, as was the testing o f certain assumptions. The impact tests to this end and a new calibration method are also presented here. 4.1 DESIGN MODIFICATIONS 4.1.1 MACHINING OF HOUSING PARTS In order to improve the surface finish of the sensor housing, a new housing design was proposed in which the square recesses in the top and bottom plates were replaced by circular recesses. This was done after noting that the surface finish defects were largely tool marks left by the passage of the small end m i l l used to machine the square recesses. This problem is avoided with the new design, as the circular recesses can be bored directly with one pass using a large end m i l l o f the desired diameter. This change is illustrated in Figure 4.1. Wi th this modification, it also became more practical to use four screws to hold the top and bottom plates together. This would also stiffen the housing and help ensure that the top and bottom plates were parallel during sensor assembly. 37 Top Plate Top Plate Revised Sensor Housing Old Sensor Housing Bottom Plate Bottom Plate Figure 4.1 Sensor housing design changes. 4.1.2 PIEZO CERAMIC ELEMENTS To increase the stiffness of the sensor system, and thus raise the sensor's natural frequency, it was decided to use wider piezo elements. The new piezo elements were 2 mm wide (twice the original width in the x-direction according to Figure 3.1), and identical to the original elements in other dimensions. For each sensor built, careful attention was given to the selection of the piezo elements prior to sensor assembly to ensure that each piezo element's thickness (dimension along the y-axis) was within ± 0 . 0 1 m m of the others. 4.1.3 INSULATING MATERIAL Attention was also given to the selection of material used to insulate the piezo elements from the metal parts of the sensor. The different materials considered were scotch tape, mica and alumina coating. The first, a 3M™-brand scotch tape, had the advantages o f being a cheap, effective and quick solution. The tape layer provided ample insulation, but its stiffness was unknown and subject to some doubt. Layers o f mica were also considered for insulation, but were rejected, as their use required a greater amount of glue. The added thickness due to the extra glue and mica 38 layers was deemed too large, and was difficult to control precisely. This caused difficulties in ensuring that the top and bottom plates of the housing were parallel, and also lowered the stiffness o f the system. It was postulated that using a thinner, stiffer insulation layer could improve the vibration characteristics of the sensor. To this end, an alumina coating was applied to a set o f sensor parts. This coating is expected to have a higher modulus of elasticity than the tape and was about half as thick, both contributing to higher support stiffness for the probe. However, using the tape instead of the coating did not appear to reduce the first natural frequency at all , and so it was concluded that the choice between these two was not a limiting factor in the design's lowest mode of vibration. The changes described up to this point shifted the sensor's first natural frequency from 2.5 k H z to 8 k H z (see Figure 4.2). 4.1.4 HOUSING SUPPORT A s explained in section 3.4, the individual piezo element signals did not behave as expected, and we suspected that this might be due to deformation o f the sensor housing. To determine whether such deformation was taking place, shims were used to obstruct any deflection of the top and bottom plates. These shims (made from mica) were used as shown in Figure 4.3, to sandwich the sensor. A side effect i f this modification was to increase the preload on the piezo elements, which reduced the sensor's sensitivity, but not to a problematic extent. The addition o f shims alone raised the natural frequency 39 Piezo 1 Frequency (kHz) Figure 4.2 Average transfer functions for piezo elements 1 and 3, with the new housing modifications and the 2 mm-wide piezo elements. Shims Refiner Back Plate Figure 4.3 Sensor used in conjunction with shims in order to inhibit deformation of housing. of test sensors to the 12-15 k H z range. The effect of placing shims against the top plate was greater than that achieved by placing shims against the bottom plate, implying that 40 the top plate deformed more readily than the bottom plate. This explains why transfer functions o f piezo elements 2 and 3 (which are between the probe and the bottom plate) were generally better than those of 1 and 4 (which were against the top plate). Although transfer functions of piezo elements 1 and 4 were improved with the use of shims, they still did not behave as well in the frequency domain as piezo elements 2 and 3, which generally exhibited smoother transfer functions and higher natural frequencies. Therefore the piezo element combination 2-3 is preferred for force measurement. 4.1.5 DAMPING MECHANISMS Attempts were made to add a damping mechanism to the system in different ways. The void regions o f the sensor housing were filled with different combinations o f latex and silicone, but none of these attempts at internally damping the system made much difference. However, when external damping mechanisms were employed, a considerable effect was seen in the free vibration behaviour. Latex pads were added to the shims to dampen the vibrations due to the deformation o f the housing, and the effects are shown in Figure 4.4. The damping factor increased from approximately 1% to 7% upon adding the latex pads. 4.1.6 FURTHER STIFFENING OF SENSOR Finally, we tried filling the void regions in the sensor housing with epoxy, to stiffen the system even further. This last modification, in combination with all the others mentioned above, gave test sensors whose first natural frequencies were in the range 25-30 k H z (see Figure 4.5). 41 No latex pads present 0.4 ^0.2 3 2 u B 1 h "o > 2.5 3 4 Time (ms) Latex pads used as part of shims 4.5 3.5 Time (ms) 4.5 Figure 4.4 Effect of using latex pads in conjunction with layers of mica in the shims. The time domain signal of piezo element 3 is shown in response to an impact from the force hammer. Piezo 1 25 30 35 Frequency (kHz) Figure 4.5 Transfer functions for piezo elements 1 and 3, for revised sensor design with all new modifications. 42 4.2 IMPACT TESTS AND CALIBRATION Aside from the work summarized in the previous section, other aspects o f the sensor's behaviour were examined. The objectives of the tests presented in this section were: - To test the response of the sensor to combined normal and shear loads, To examine how the sensor's response changes when varying the position of impact on the probe, To develop a more reliable calibration procedure, in which all calibration coefficients are determined with the sensor mounted in the refiner plate. 4.2.1 SENSOR RESPONSE TO COMBINED NORMAL AND SHEAR LOADS When pulp floes are impacted by bars during refiner operation, the resultant force is a combination o f a normal and a shear component. Thus far, it has been assumed that the sensor's response to such a force would be the sum of its response to the pure vertical component plus the response to the pure horizontal component of the force. This was mathematically stated as: Vi =KiNFN + KiS Fs = F(KiN cosQ + KiS sinQ) (3.3) where F is the magnitude o f the resultant force and 9 is the angle that its line o f action makes with the perpendicular to the top face of the probe (i.e., the angle made with the y- direction, as defined in Figure 3.1). If the refining forces are to be calculated as such, then a confirmation of the above equation is required. 43 To this end, wedges of different geometries were constructed from aluminum and glued to the top face o f the probe, so that repeatable impacts could be applied to the sensor at precise angles (see Figure 4.6). A s the wedges were made from aluminum, their individual masses were very small (ranging from 0.02 to 0.05 g), generally below 3% of that o f the sensor probe (weighing 2 g), and so any effects of having increased the probe mass were not significant. Figure 4.6 Impacts administered at different angles by using aluminum wedges. For every angle 8 at which the probe was impacted, the piezo elements responses were seen to be proportional to the magnitude of the impact force, Vt=KmF (4.1) where K,e is the experimentally determined constant of proportionality. KfN was determined as before, by impacting the sensor vertically (0 = 0°), and i f the assumption o f linear superposition holds, then K;s could be determined from: 44 Kjq = KIN cos 9 + KJS sin 9 (4.2) or, rearranging, Kn -KiNcosQ sin 9 (4.3) If the assumption o f linear superposition is valid, the values o f K;s calculated from Equation 4.3 for different angles should all be the same. The results are summarized in Table 4.1. It should be noted that piezo element 2 cracked during the assembly o f this sensor, and so no signals from this piezo element are included in this analysis. Aside from the values in the shaded regions of the table, the K J S values calculated for different angles are close. The exception to this are those values in the shaded regions, which were inaccurate because at this particular angle, the sensor response was small (Kie changes sign in these regions) and the signal-to-noise ratio was low, hence the discrepancies in the K J S values. Angle Piezo 1 Piezo 3 Piezo 4 Kie Kis K3e K3S K49 K4S (°) (mV/N) (mV/N) (mV/N) (mV/N) (mV/N) (mV/N) 0 43.3 - -70.2 - 48.6 - 10 57.0 82.7 -42.1 155.7 28.3 -112.7 20 71.8 91.0 16 O 242.3 -S 4 -161.0 30 86.4 97.8 26.9 175.4 -18.9 -122.0 40 94.6 95.6 50.9 162.8 -31.3 -106.6 Ave K 1 S =91.8 mV/N Ave K3S = 164.6 mV/N Ave K4S =-113.7 mV/N KIN =43.3 mV/N K3N =-70.2 mV/N K4N =48.6 mV/N Table 4.1 K-Values determined by impacting the sensor at different angles Using the method outlined in Appendix C, the average K-values can be used to derive equations to calculate the normal and shear forces from a combination of two piezo elements. For the piezo combinations 1-3 and 1-4, these are: 45 FNa =12.12F, - 6 . 7 6 F 3 Fsu = 5.17F, +3.I9F3 (4.4a,b) F m 4 = 12.12F, +9.78F 4 7 ^ = 5 . 1 8 ^ - 4 . 6 1 ^ (4.5a,b) where V i , V3 and V 4 are the magnitudes o f the piezo element signals in volts. The true normal and shear forces on the sensor probe, as measured by the hammer, are: We can now compare these true forces with those calculated from the sensor signals using Equations 4.4 and 4.5. Figures 4.7 and 4.8 show the calculated forces plotted against the actual forces for 100 impacts at the different angles listed in the table above. A linear regression performed on the two sets o f data gave slopes and correlation coefficients very close to 1 for both graphs, indicating that a measure o f the forces with the assumption of linear superposition is reliable. Comparing the data to the equal-value lines in the figures, piezo combination 1-3 appears to slightly overestimate the normal force and underestimate the shear force. These deviations from the equal value lines on the graphs are explained by the fact that piezo elements 1 and 4 are in use here, and they are known to give less accurate results than piezo elements 2 and 3, as explained earlier. Another source of error was the difficulty in ensuring that the line of action o f the impact forces passed through the centre o f the probe tip. This caused more significant errors in the impacts at the larger angles, as is evident from the string of points that lie below the equal value line in Figure 4.7, which represent the data for 0 = 40°. FN = F cosQ (3.2a) Fs = FsinQ (3.2b) 46 Actual Normal Component (F cosG) (N) Figure 4.7 A comparison of the true normal component with values calculated from Equations 4.4a and 4.5a. Actual Shear Component (F sinG) (N) Figure 4.8 A comparison of the true normal and shear components with those calculated from Equations 4.4b and 4.5b. 47 The validity of the linear superposition assumption can now be used in order to calibrate the sensor in the plate, as both KJN and K , s can be determined with the sensor mounted in the refiner plate, thus solving the problem o f having to use the mounting j ig . 4.2.2 EFFECT OF IMPACTPOSITION One of the major objectives o f this work is to examine the refining forces and their variation over the duration o f a bar passing event when a floe is trapped between the sensor and a rotor bar. During such an event, a rotor bar passes over the sensor, trapping a floe at the leading edge of the probe where the forces begin to act. A s the rotor bar moves over the probe, the centre o f pressure moves away from the leading edge, right across the width of the probe's top face, to end up at the trailing edge of the probe tip. It is therefore important that the sensor response does not change significantly with the point of application of the loads, so that a meaningful force profile over the bar passing event can be acquired. Rotor b ai Sensor probe tip Figure 4.8 The moving load during a bar passing event. As the rotor bar moves across the top of the probe, so does the centre of pressure. The experiment conducted to study this aspect of the sensor behaviour consisted of dividing the top face o f the probe into a grid o f 15 squares, each 1 mm x 1 mm in size, 48 and vertically impacting the centre o f each square several times with the force hammer to determine a K-value for each piezo element in each location. The results for piezo elements 2 and 3 are shown in Table 4.2. A s one would expect, there is a small variation in the voltage of the signal per unit force o f impact along the width o f the probe (as the moment arm of the impact relative to each piezo element changes along the x-direction). There is little effect of moving the impact position along the length o f the probe (z-direction), as shown by the low standard deviations reported in the table. Thus we can conclude that K J N undergoes only small changes with varying impact position (mostly within 10% of the mean), and that the value measured in the centre o f the probe is representative o f the mean value. Similar results were seen when K-values were measured for impacts applied at 30° at different positions on the grid. The sensitivity of the sensor did not vary greatly for the different impact positions, suggesting that K J S is affected in the same way as K J N , and that neither are significantly sensitive to the point o f application of the forces in question. Piezo 2 K-Values Piezo 3 K-Values X <J(X) 1 2 3 1 0.139 0.145 0.152 0.007 2 0.140 0.148 0.149 0.005 z 3 0.142 0.151 0.152 0.005 4 0.138 0.149 0.148 0.006 5 0.143 0.152 0.153 0.006 o(z) 0.002 0.003 0.002 K2N(mean) = 0.147 V/N X 1 2 3 O(x) 1 0.095 0.084 0.079 0.008 2 0.092 0.086 0.078 0.007 z 3 0.093 0.084 0.078 0.007 4 0.095 0.088 0.077 0.009 5 0.092 0.087 0.074 0.009 a(z) 0.001 0.002 0.002 K3N(mean) = 0.085 V/N Table 4.2 Variation of sensitivity (K-values) of piezo elements 2 and 3 with varying impact position on the top face of the probe. All K-values are in V/N, and a is the standard deviation. 49 5 . REFINING TRIALS 5.1 EXPERIMENTAL SETUP Refining trials with the improved sensor were performed using the same Sprout Waldron 12-inch atmospheric discharge laboratory refiner that was used for the tests described in Chapter 3. New pulleys and drive belts were purchased to be able to run the refiner at different speeds. Trials were conducted with the refiner running at speeds of 700 rpm and 2560 rpm (full speed) using softwood T M P at an inlet consistency of 16%. For the high speed runs, the pulp was continuously fed into the refiner using a plunger-style feeder, thus maintaining a reasonably stable motor load. This method could not be used for the low speed runs, as the refiner's ability to propel pulp outwards through the refining zone is greatly reduced at lower speeds. Therefore, the pulp was fed in small quantities (about 0.3 kg at a time), and dilution water was injected intermittently via the eye o f the refiner to ensure that pulp passed through and exited the refining zone. The consistency was varied during the low speed tests by adding dilution water. Pulp samples taken from inside the refiner after adding dilution water had an average consistency of 13%. This value is, o f course, only approximate, and the technique is useful only for distinguishing between a high consistency (16% without addition o f dilution water), and a lower consistency (upon addition of dilution water). In the high-speed tests, pulp was fed at two different inlet consistencies: 25% and 12%. 50 A l l trials were performed using D2B502 plates, which gave a bar passing frequency over the sensor probe of 2 k H z for the low speed runs, and 7.4 k H z at high speed. Data acquisition was carried out on a state-of-the-art 4-channel digital oscilloscope. We sampled 3 piezo signals (from piezo elements 2,3 and 4) and one signal from a tachometer measuring the refiner's rotational speed. The sampling rate was 250 k H z for the low speed tests and 1 M H z for the high-speed tests. The objectives for these tests were: to isolate bar passing events and examine their force profiles - to observe the variation o f normal and shear forces and their relative magnitude upon changing the plate clearance, refiner speed, and consistency. 5.2 REFINING FORCE PROFILES 5.2.1 BAR PASSING EVENTS Figure 5.1 shows a 5 ms force trace representing the normal and shear forces during refiner operation at 700 rpm. In all such diagrams in this chapter, the normal force is depicted by the bold line, and the shear force by the fine line. Several interesting features are present here. The sharp spikes, occurring at approximately 0.5 ms intervals, are the force profiles o f bar passing events. The first and seventh spikes are impacts that last slightly longer than the others. This is a feature of the D2B502 plate pattern (see Figure 5.2), on which all bars have a width of 2.8 mm, except every sixth bar, which has a width o f 5.5 m m over the location o f the sensor probe. The radial position o f the probe 51 corresponds to the streak visible on the left half of the segment near the outer radius. This is a scratch left by the sensor probe. The larger width o f some o f the bars at this radial position explains why some peaks are wider in the force profile. In the case depicted in Figure 5.1, the peak magnitude o f the forces varies when we look at successive impacts. This is typical o f what was generally observed. The peak levels were seen to vary quite erratically depending on how the pulp was feeding. This was to be expected, since the magnitude of the forces depends on factors 417 418 419 420 421 422 Time (ms) Figure 5.1 Refining normal force (bold line) and shear force (fine line) at 700 rpm as calculated using piezo combinations 2-3 and 2-4. 52 Figure 5.2 One of the three segments of the D2B502 rotor plate (the stator plate segments are identical). such as the floe size, floe position relative to the bars and floe strength, all o f which can vary greatly during normal refiner operation. Forces calculated from the combination of signals from piezo elements 2 and 4 agree well with those from the combination of 2 and 3 in terms of the magnitudes o f the forces. However, as we can see from Figure 5.1, the profiles from the 2-4 combination are somewhat more adversely affected by vibrations, and so the combination 2-3 was regarded as correct, and the 2-4 combination was not used for any force data. Figure 5.3 shows a close-up of one bar impact. In general, the force profiles of individual bar impacts were quite clearly defined and were all quite similar in shape. Both the normal and shear forces rise sharply to a 53 maximum early in the impact, and then fall to a lower level that gradually drops off to zero as the impact ends. The shear force profiles measured here were similar to those shown by Senger et al. on their low-speed single bar refiner [24], but we saw important differences between the normal force profile measured in the two cases. In the work of Senger et al., the normal 78.9 79 79.1 79.2 79.3 79.4 79.5 79.6 Time (ms) Figure 5.3 The normal (bold line) and shear forces (fine line) due to a typical bar impact. force profile was essentially triangular and symmetric about the peak value, as the compressive force on the floe rose steadily to reach a maximum when the rotor and stator bars were centred over each other, then dropped steadily to zero as the bars departed each other [24]. In contrast, they also observed that the shear force profile was asymmetric, and attributed this to the action of the corner force. This force component, acting on the leading edge o f the bar, rose sharply at the start o f the impact, and dropped to zero 54 halfway through the impact, when the leading edge o f the rotor bar reached the trailing edge of the stator bar. Senger et al. observed that the corner force acted almost entirely in the tangential direction. The overall shear force during a bar crossing was thus the sum of the corner force and the friction force (proportional to the normal force), which explained the asymmetry o f the shear force profile. The profiles shown here suggest that the corner force has a component in the normal as well as in the tangential direction. The fact that the corner force has a normal component in our results and did not display one in the measurements performed by Senger [24] at low speed may be an indication that the direction o f action of the corner force is influenced by speed. Our results are not sufficient to reach a definite conclusion on this aspect, however, and a more detailed investigation of the effect of refiner speed w i l l be required. 5.3 DATA REJECTION CRITERIA To investigate how refiner operating conditions affected the forces between bars, we recorded signals representing thousands of bar impacts. Sensor vibrations and other phenomena detrimental to the force measurement were sometimes seen to affect the signals adversely. We therefore had to reject some signals when analyzing records of data, and the criteria used for rejecting such signals are described in this section. 55 5.3.1 SENSOR VIBRATIONS The sensor's vibration problems encountered in these tests can be split into two categories: Vibrations at 30 kHz , corresponding to the peaks in the transfer functions i n Figure 4.5 (resonant vibration). - Vibrations at 2 kHz , set up by bar passing events at this frequency, Although some low-magnitude 30 k H z vibrations were present in most signals, these were not often a cause of a loss of accuracy. In some cases, however, the shear force profile was significantly affected by these vibrations. Signals where the amplitude o f these vibrations exceeded 10% of the peak magnitude of the shear force were rejected. A n example o f such a signal is shown in Figure 5.4. 20 - 30 25 r 10 0 - 5 711 711.2 711.4 711.6 711.8 712 712.2 712.4 712.6 712.8 Time (ms) Figure 5.4 An illustration of problematic 30 kHz resonant vibrations of the sensor. 56 Figure 5.5 shows typical bar passing events at an operating speed o f 2560 rpm. Although bar impacts are clearly distinguishable, the true peak magnitude o f the forces is subject to some doubts, as the resonant response o f the sensor affects the measurement to a significant degree. This is particularly true for the shear force because o f its lower peak magnitude. A s a result of this problem, none of the signals we collected at high refiner rotational speed could be used for quantitative analysis. This is clearly a shortcoming o f the force sensor that needs to be addressed in subsequent design refinements. i i i i i i i i 59.3 59.4 59.5 59.6 59.7 59.8 59.9 60 Time (ms) Figure 5.5 Typical force profdes of bar impacts at 2560 rpm. In some cases during the tests at 700 rpm, the sensor was seen to vibrate at a frequency close to that o f the bar passing events. This is shown in Figures 5.6 (a) and (b), where the five consecutive 2.8 mm bars begin to excite the sensor into vibration at approximately 2 57 30 I 1 1 1 1 1 1 r 25 - 20 - 15 - _ -j Q | I j , , , i i I I I I | 1 | 378 380 382 384 386 388 390 392 394 396 Time (ms) Figure 5.6(a) Sensor vibrations at approximately 2 kHz. 50 40 ^ 30 <D O 1 20 10 0 1 1 1 lrJttl|||l|Pl i i i < i i w 475 480 485 490 495 500 Time (ms) Figure 5.6(b) 2 kHz vibrations grow in amplitude for five successive bar impacts, until a sixth impact from a wider bar reduces their amplitude. This record shows several successive occurrences of this phenomenon. 58 k H z . A s the sensor starts to vibrate in this way, the normal force reading after the bar impact dips down to a negative value, instead of reading zero normal force. This dip increases in magnitude with each bar passing, until the passing o f the sixth bar, which is wider than the previous five on the D2B502 plate pattern. The impact with this bar serves to dissipate the energy of the vibration in two ways. A s the pulp between this wider bar and the sensor probe is held against the probe for a longer time, this provides a damping mechanism. Also , the passage of the wider bar effectively breaks the periodicity of the excitation, thus temporarily counteracting the vibration (before it is set up again by the next five bars). It should be noted that these vibrations are only present in the normal force and not in the shear force, suggesting that the sensor probe is vibrating purely with linear motion along the y-axis (as defined in Figure 3.1). These vibrations sometimes become severe enough to significantly affect the force measurement, as shown in Figure 5.6(a), and so all force signals displaying vibrations whose amplitudes were over 10% of the magnitude o f the peak force were rejected. 5.3.2 CYCLIC FLUCTUATIONS IN NORMAL FORCE WITH EACH ROTATION In some o f the signals, particularly at high speed, another problem began to appear in the normal force signal. Figure 5.7 shows a part of a signal that seems to be comprised o f a low frequency cyclic variation in the normal force upon which the spikes (bar impacts) are superimposed. This cyclic variation corresponds exactly to the period of rotation o f the refiner, and again only appears in the normal force. 59 Figure 5.7 Cyclic fluctuations in normal force with each rotation at 2560 rpm. Figure 5.8 is a plot of the average normal force and the varying plate clearance over one rotation, and there is a clear relationship between the two. A s it was not possible to measure the exact plate clearance at the location of the sensor during normal refiner operation, the clearance was estimated by measuring the height o f each bar with a dial gauge when the refiner was off. Zero plate clearance was determined with the refiner in operation, by narrowing the plate gap until the highest point on the rotor plate was contacting the highest point on the stator (the sensor probe tip) once per revolution. Thus, the plate clearance setting on the refiner applies to the gap between the highest bar on the rotor and the sensor probe. The clearance associated with other bars passing over the sensor probe can be determined relative to that using the bar heights measured with the dial gauge. Although the determination o f the plate clearance using the static 60 measure o f rotor bar heights is not exactly representative of the actual plate clearance during operation, it serves here for a qualitative comparison o f the varying plate clearance and the mean normal force. The mean normal force was calculated by taking a moving average of entire revolutions of the rotor during operation, and the similarity in the shapes o f the two curves was used to align them with each other in Figure 5.8. 20 40 Bar# 60 80 100 120 140 • Plate Gap O Average Normal Force 2.0 1.8 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 o Figure 5.8 Variation of plate clearance and mean normal force through one full rotation of the rotor plate. The regions o f smaller plate gap are associated with higher normal force. This trend most l ikely occurs because of higher compressive stresses imposed on the pulp network at lower plate gaps. This phenomenon was not restricted to the high speed tests, but was more pronounced there than in the 700 rpm runs. This phenomenon was considered a problem, as the offset in the normal force could have been due to a change in the sensor preload, with the sensor housing compressed between the refiner plate segment and the back plate (see Figure 4.3). Such circumstances would 61 skew the force measurement. Pending further tests to determine whether this phenomenon was indeed problematic, signals showing such a shift in the baseline force were excluded from further analysis. 5.4 ANALYSIS AND DISCUSSION 5.4.1 IMPACT STATISTICS In order to analyze several signals, each containing hundreds o f bar impacts (those satisfactorily free o f the rejection criteria outlined in the previous section), the signals were processed using M A T L A B 5 for Windows. M A T L A B programs were used at all stages of signal analysis - for the calibrations and impact testing described earlier, as wel l as for the calculation of the refining forces from piezo signals and the subsequent analysis o f these measured forces. A l l M A T L A B programs (m-files) used in this work are included in Appendix D . To analyze the force signals from the refiner, a program was designed to isolate individual bar passing events in the signal. This program also extracted the normal and shear force profiles of the events, recorded the peak values of these forces, and calculated the equivalent tangential coefficient of friction as the ratio of these forces. The latter was calculated using two different methods; first by taking the ratio o f the peaks o f the shear and normal forces (called u, t e i7(peaks)), and second by calculating the ratio o f these forces at each point in time during the impact and then taking the average (p.,,e?(ave)) of these values. The beginning and the end of each impact were defined by the points at which the normal force rose above 1 N and fell below it, respectively. The region in between 62 was extracted from the force signal as the bar passing event. Strictly speaking, the event starts when the force rises from zero and ends when the force falls back down to zero, but a threshold value of 1 N had to be used to prevent falsely registering impacts due to noise or small vibrations in the signal. A summary o f our results is shown in table 5.1. Mean Gap (0.001") Mean Gap (mm) Peak F,m Peak Fm p.te,(peaks) Mean o r W a v e ) Mean o No. of Impacts Mean a Max Mean a Max No Dilution Water 18 8 5 3 0.46 0.21 0.13 0.08 1.61 0.69 5.24 3.63 3.56 26.14 4.17 4.43 34.96 5.19 6.65 46.42 1.00 0.68 3.86 0.99 0.90 6.32 0.96 1.01 8.52 0.92 1.19 8.32 0.59 0.19 0.29 0.09 0.23 0.06 0.18 0.04 0.55 0.20 0.36 0.11 0.27 0.09 0.20 0.06 210 1302 1873 1557 Dilution Water Added 8 5 3 0.21 0.13 0.08 4.17 4.35 38.99 7.83 6.74 37.67 13.58 11.57 55.33 0.96 1.03 10.39 1.40 1.22 9.13 2.06 1.86 10.83 0.23 0.06 0.18 0.05 0.16 0.04 0.27 0.09 0.21 0.08 0.18 0.08 2716 716 996 Table 5.1 Summary of impact statistics for refining runs at 700 rpm (a is the standard deviation). A s expected, the data shows a clear trend of increasing force with decreasing plate clearance. Lowering the plate clearance causes an increase in the axial thrust on the plates due to an increased reaction force from the pulp between the plates. This also increases the shear force and thus the power consumption. 5.4.2 VARIATION OF SHEAR FORCE WITH PLATE CLEARANCE While the peak normal force keeps increasing with decreasing plate gap, the peak shear force seems to level off at about 11 N . Noting from the force profiles that the peak shear force is reached very shortly after the start o f the impact, it seems reasonable to suggest that the peak is due mostly to the corner force. The ceiling o f approximately U N would 63 therefore correspond to the maximum shear force per unit length o f bar that can possibly be attained at this speed and range o f consistency, which is calculated at 2.2 kN/m. This suggests that there may also be a ceiling in the motor load, which can be estimated using: where co is the refiner speed (in radians per second), a is the fraction o f the refining zone area that is packed with pulp, rj and r2 are the inner and outer radii o f the refining zone, respectively, FSL is the shear force per unit length, and Lbc is the total length of rotor and stator bar edges crossing at any time during refiner operation. This equation assumes that the torque on the refiner's shaft is equal to the moment exerted by the resultant shear force (calculated based on the average shear force per unit length o f bar edge) acting at a radial distance halfway between the inner and outer radii o f the refining zone. Lbc is estimated at 2.3 m (details o f this estimate are given in Appendix E) , which is approximately half o f the total bar length of each of the plates, and a is estimated at 0.76 Equation 5.1 predicts the aforementioned ceiling in the motor load to be 44 k W for the lab refiner when operating at 700 rpm. For the Sprout-Waldron 60-inch refiner in [25], is estimated at 116 m (using to the method in Appendix E), and this leads to an upper limit in the motor load o f 19 M W for the refiner running at 1500 rpm. These values are somewhat higher than the rated capacity o f the motor in each o f the two cases, which for the laboratory refiner is 35 k W , and for the 60-inch refiner is 10 M W for (5.1) [26]. 64 a single refining zone. This estimate of the ceiling in the motor load is nevertheless expected to be higher than anything achieved under normal conditions, as the maximum shear force per unit length was used in the calculation, and this was assumed to act uniformly on all bars under load. In reality, the average shear force per unit length throughout the refining zone w i l l l ikely always be lower than this, thus drawing less power. The bar coverage fraction a also has a significant effect on this measure, and the value quoted above is a rough estimate at best. 5.4.3 EFFECT OF INJECTING DILUTION WATER The addition of dilution water at constant plate gap seems to cause an increase in the peak magnitude o f the forces, but this trend must be interpreted with caution. The refiner does not feed wel l at 700 rpm and, prior to the addition o f dilution water, relatively few impacts are registered before the pulp fills the grooves and forms a mat on the surface of the plates. The addition of dilution water washes away the pulp on the surface o f the plates, which causes a surge in the flow o f material through the refiner and, in turn, leads to an increase in both the number and the peak magnitude o f impacts measured shortly after. Thus, the effect observed here might be due to an increased capacity to feed material through the refiner, rather than an intrinsic increase in the reaction force o f the pulp mat as a result of a change in consistency. 5.4.4 VARIATION OF \iteq WITH PLATE CLEARANCE AND CONSISTENCY The equivalent tangential coefficient o f friction, \itfeq, taken as the average ratio o f the shear to the normal force, are plotted for the different test conditions in Figure 5.9. These values are close to those calculated from the peak values of the shear and normal force 65 from each impact, and qualitatively behave in the same way, although | i i^(ave) is generally slightly higher than |i,, e 9(peaks). The value o f \it,eq decreases with decreasing gap, because the shear force starts to level off at the lower plate gaps while the normal force continues to rise. Adding dilution water decreases the consistency of the pulp suspension between the plates, and this results in a lower value of \i,,eg at a given plate gap. This is consistent with a trend that has been observed by Isaksson et al. in an industrial refiner, where Effect of Plate Gap and Consistency on p ^ 0.6 0.5 1 ° - 4 9S I. t 0.3 0.2 0.1 0.0 • No Dilution A Dilution Water Added 0.00 0.10 0.20 0.30 Mean Plate Clearance (mm) 0.40 0.50 Figure 5.9 Equivalent tangential coefficient of friction vs plate clearance dilution was seen to reduce \x.t_eq [25]. A similar dependence on consistency was also observed by Senger et al. [24] for measurements carried out on a single-bar refiner at very low speeds and at consistencies ranging from 5% to 80%. However, the effect he observed in this consistency range was less pronounced than the one depicted by our results in Figure 5.9. In contrast, Miles and M a y reported that \it>eq was unaffected by 66 consistency, based on tests performed using a pilot-scale refiner at discharge consistencies in the range of 15-30% [8]. Although the differences in \it>eq for the different consistency cases are barely within the calculated standard deviation, a student's t-test showed that the differences are significant at a 99.9% confidence limit. 5.4.5 RANGES OF MEASURED \l,,eq AND A VERAGE PRESSURE For the purpose of comparing the range o f measured values of mechanical pressure (due to compressive stress on the pulp between the plates) and the equivalent tangential coefficient o f friction, a graph o f \it>eq against average mechanical pressure is plotted in Figure 5.10. This graph includes data from this work and from several other sources. The average mechanical pressure for our data was calculated as the ratio o f the average peak normal force (from Table 5.1) to the area o f the sensor probe tip (15 mm 2 ) . For all data aside from that of this work, \it,eq was calculated using Equation 2.8, 2P M = — (2.8) * hmFm(rl+r2) and the average mechanical pressure was determined from: p - = t = 4 M (5'2) where AM is the area o f the refiner plates bearing the thrust load o f the pulp between the plates. This is calculated using the bar coverage fraction, a , along with the proportion o f the total refining zone area {A^ constituted by bar surfaces, represented by the fraction X. 67 Assuming identical rotor and stator geometries in all cases, and that bar and groove widths are equal, a value of 0.50 is used for the fraction k. The values of the constants used for each of the different data sets are given in Table 5.2. INVESTIGATORS 0) n h A (rad/s) (m) (m) (%) Atack etal. (SI & S2) 189 0.376 0.533 1 75.6 Isaksson et al. S1 157 0.45 0.785 1 75.6 Isaksson et al. S2 157 0.51 0.785 1 75.6 Miles & May 126 0.355 0.457 2 16 Table 5.2 Values of constants from different sources for use in Equation 2.8 (SI and S2 refer to primary and secondary stage processes, respectively). 0.1 0.0 -I 1 1 1 1 1 1 1 0 500 1000 1500 2000 2500 3000 3500 Pressure (kPa) Figure 5.10 Plot of the equivalent tangential coefficient of friction against average mechanical pressure for different refiners. The dark shaded area represents the data from this work, where the bar coverage fraction a is expected to lie somewhere between 30% and 80%. These values were used to estimate the high and low pressure bounds for this shaded region. For the data of Miles and May a = 16% is used based on measurements made using that refiner [27]. For all other data, a is estimated at 0.76, based on an average value calculated from data published in [26]. 68 In the case of Isaksson et al., the steam thrust for the data published in [25] was calculated improperly. Corrected data was obtained from the authors [28], but an uncertainty remained, in that pressure measurements were taken at the refiner inlet and also at the inner radius of the refining zone, but nothing is known about the pressure profile in the breaker bar region between those two points. Two possibilities were considered: that the pressure increased linearly with radial position from the value measured at the inlet to the higher value at the end of the breaker bar region, and secondly that the pressure remained constant at the inlet level throughout the breaker bar region. The nature o f the true pressure profile is expected to be somewhere in between these two cases. The shaded region encompasses the range o f pressure and \itieq calculated assuming the two cases described above. In all cases, the value o f \it,eq increases as the pressure decreases. This is not a surprising result, as the calculation of \it,eq was performed using Fm in the denominator, and the calculation of the average pressure used Fm in the numerator. The only exception to this is the data from our work, which used the normal force in this same way instead o f Fm. This explains the general shape of the trend seen with increasing pressure. It should therefore be re-emphasized that the purpose of plotting this graph was to compare the ranges o f our measured values with those from other sources, and not to investigate the relationship between \it>eq and mechanical pressure. Such a relationship would have to be examined under conditions o f constant throughput and motor load, as these are known to have an effect on the variables under consideration. Furthermore, the calculated values o f pressure would be affected by the bar coverage fraction, a , which is unknown here. 69 The values used are estimates at best, and could also be affected by the mass flow rate o f pulp fed through the refiner. It is interesting to note that for all data sets, except for that of the primary stage refiner o f Isaksson et al., the curves for different refiners lie very close to each other, suggesting that they were operating in a range of conditions in which the equivalent tangential coefficient o f friction for a given pressure was similar for all o f those refiners. The difference between the first and second stage refiners from the data o f Isaksson et al. reflects the lower motor load o f the latter case, as a lower [it,eq (and hence, for a given pressure, a lower shear force) is associated with a decrease in the power consumption. The two points in the data o f Atack et al. with the lowest values of \itieq were also taken from a second stage refiner. These two points were refined at a low specific energy (unlike the third point with \it,eq=0.48, which was refined at a specific energy comparable to the first stage trials). Our trials were performed by refining softwood T M P , effectively making it a second stage process. This would explain why our points lie in the lower region relative to the others. The fact that the range values of \itfeq and pressure measured here are similar to those reported by the other sources, coupled with the fact that the values of \itieq for a given pressure are also similar, indicates that experiments carried out on the laboratory refiner can be useful for investigating the phenomena observed in larger refiners. Further testing is necessary to determine the exact nature o f the relationship between the variables i n question. 70 6. CONCLUSIONS Energy-based methods are commonly used to characterize the action o f refiners by quantifying the energy transferred to pulp fibres that pass through the refining zone. However, these methods fail to give insight into the real physical mechanisms acting in the process. In the refining zone, pulp floes experience cyclically varying loads in directions normal and tangential to the motion of the refiner bars that impact them, and it is these forces that cause the structural changes induced by refining. Therefore, an understanding o f these forces is a prerequisite to an understanding of the refining process. A two-axis force sensor was developed for use in a 12-inch laboratory refiner to measure the normal and shear forces during refiner operation. Although the sensor response presented some limitations when operating the refiner at full speed (2560 rpm), these were not a great detriment when running the refiner at 700 rpm. The magnitudes o f the normal and shear forces were seen to rise sharply at the start o f bar impacts on pulp floes, then to fall sharply again to a lower level before tapering off to zero as the bar impacts came to an end. This profile suggests that the normal force is made up o f two components, these being the compressive force on the pulp floe (the lower level regime) and the corner force required to plough through the floe (the initial peak in the force profile). The shear force on the refiner bar also contains a corner force component, along with a component due to friction between the pulp and the bar's top face. The corner force appears to be the major component in both cases. Previous work, based on measurements made at low speed in a single-bar refiner, had suggested that the corner force only affected the shear force in refining [24]. 71 While the normal force was seen to increase as the plate clearance decreased, the shear force measured by the sensor reached a maximum at approximately U N . If the corner force is the major component of the refining forces, then the forces essentially act at the leading edge of the refiner bars. This suggests an upper limit to the shear force reaction o f the pulp per unit bar length o f approximately 2.2 kN/m, for the 16% inlet consistency and 700 rpm conditions tested here. The equivalent tangential coefficient of friction was seen to decrease with decreasing plate gap, due primarily to the leveling off o f the shear force while the normal force continued to rise. Adding dilution water also lowered the equivalent tangential coefficient of friction slightly, suggesting that consistency may have an effect, although more testing needs to be done over a greater range of consistency to confirm this. Further work must be carried out to improve the vibration characteristics o f the sensor, as its resonant vibrations dominated the signals collected during refining trials at full speed. The lowest natural frequency o f the sensor must be raised and its damping characteristics enhanced in order to implement its use at speeds closer to those used industrially. 72 BIBLIOGRAPHY 1. A . Bankes, "Design and development of a mechanical wood pulp refiner force sensor", Master's Thesis, Queen's University (Jan. 2000). 2. M . I . Stationwala, K . B . Miles , A . Karnis, "The effect of first stage refining conditions on pulp properties and energy consumption", Journal of Pulp and Paper Science, 19(1) (1993). 3. R .J . Kerekes, "Characterization o f pulp refiners by a C-factor", Nordic Pulp and Paper Research Journal, 5(l):3-8 (1990). 4. W . Brecht, " A method for the comparative evaluation o f bar equipped beating devices", Tappi Journal, 50(8):40A (1967). 5. C.F. Baker, "Specific edge load theory - Applications and limitations" Pira International Refining Conference, Paper 02 (1991). 6. F.P. Meltzer, P. Sepke, "New ways to forecast the technological results o f refining", Proceedings of the International Refining Conf. & Exhibition, Atlanta (1995). 7. J. Lumiainen, "Specific surface load theory", Proceedings o f the International Refining Conf. & Exhibition, Atlanta (1995). 8. K . B . Mi les , W . D . May, "The flow of pulp in chip refiners", Journal of Pulp and Paper Science, 16(2):J63-71 (1993). 9. K . B . Mi les , W . D . May , "Predicting the performance o f chip refiners; A constitutive approach", Journal of Pulp and Paper Science, 19(6):J268-274 (1993). 10. K . B . Mi les , " A simplified method for calculating the residence time and refining intensity in a chip refiner", Paperija Puu, 73(9):852-857 (1991). 11. K . B . Mi les , A . Karnis, "The response o f mechanical and chemical pulps to refining", Tappi Journal, 74(1):157-164 (1991). 12. D . H . Page, "The beating of chemical pulps - The action and effects", In F. Bolam, editor, Fundamentals of Papermaking: Transactions o f Fundamental Research Symposium held at Cambridge, volume 1, pages 1-38. Fundamental Research Committee, British Paper and Board Makers ' Association (Sept. 1989). 73 13. A . A . Khlebnikov, V . F . Pashinski, V . N Goncharov, E . A . Smimova, "Analysis o f forces involved in the operation of a conical refiner", Bum Promst. No.22:129- 13 6 (English Translation) (1969). 14. V . N . Goncharov, E . A . Smirnova, E . V . Shemyakin, "Method for the determination of stresses between refiner blades", Bum Promst. No.27:134-138 (1970). 15. V . N . Goncharov, "Force factors in the disc refiner and their effect on the beating process", Bum Promst. No.5:12-14 (English Translation) (1971). 16. L . Nordman, J.E. Levl in , T. Makkonen, H . Jokisalo, "Conditions in an L C refiner as observed by physical measurements", Paperi Ja Puu 63(4) 169-180(1981). 17. D . M . Martinez, W.J . Batchelor, R.J . Kerekes, D . Ouellet, "Forces on fibres in low consistency refining: Normal force", Journal of Pulp and Paper Science, 23(1):J11-18 (1997). 18. W.J . Batchelor, D . M . Martinez, R.J . Kerekes, D . Ouellet, "Forces on fibres in low consistency refining: Shear force", Journal of Pulp and Paper Science, 23(1):J40- 45 (1997). 19. W.J . Batchelor, D . Ouellet, "Estimating the forces on fibres in refining", 4 t h Pira International Refining Conference, Fiuggi, Italy, Paper 2 (March, 1997). 20. D . Atack, M . I . Stationwala, "On the measurement o f temperature and pressure in the refining zone of an open discharge refiner", Transactions of the Technical Section o f the Canadian Pulp and Paper Association (3):71-76 (1975). 21. D . Atack, "Towards a theory o f refiner mechanical pulping", Appita Journal, 34(3):223-227 (1980). 22. D . Atack, M . I . Stationwala, A . Karnis, "What happens in refining" Pulp and Paper Canada, 85(12):T303-308 (1984). 23. R. Franzen, R. Sweitzer, "Refining forces in high stock concentration pulping", Appita Journal 36(2): 116-121 (1982). 24. J. Senger, D . Ouellet, "Factors affecting the shear forces in high-consistency refining", Proceedings of the International Mechanical Pulping Conference, Helsinki, Finland, In Press (2001). 25. A . J . Isaksson, A . H Horch, B . Al l i son , A . Karlstrom, L . Nilsson, "Model l ing o f mechanical thrust in T M P refiners", Proceedings o f the International Mechanical Pulping Conference, Stockholm, Sweden, pages 87-93 (1997). 74 26. D . Atack, M . I . Stationwala, A . Karnis, "Distribution A n d motion o f pulp fibres on refiner bar surface" Journal of Pulp and Paper Science, 18(4):J131-J137 (1992). 27. W . D . May , M . R . McRae, K . B . Miles , W . E . Lunan, " A n approach to the measurement o f pulp residence time in a chip refiner", Journal of Pulp and Paper Science, 14(3):J47-J53 (1988). 28. A . J . Isaksson, B . Al l i son , Personal communication of corrected tangential coefficient of friction data of reference [25]. 75 NOMENCLATURE a constant equal to 4 for a single disc-refiner and 2 for a double-disc refiner a bar coverage fraction Am area o f refiner plates experiencing thrust load (m 2) Arz total area o f refining zone (m ) B refiner bar width (m) c pulp consistency (fraction) Q normal force coefficient for piezo element /, (N/V) CEL cutting edge length (m/s) Di shear force coefficient for piezo element /, (N/V) e specific energy per impact (J/kg impact) E specific energy (J/kg) f frequency (Hz) fbp frequency of bar passing events (Hz) F magnitude o f resultant force on sensor probe tip (N) Fm mechanical thrust (N) FN normal force (N) Fs shear force (N) FSL shear force per unit length (N/m) G groove width (m) h constant equal to 1 for a single-disc refiner and 2 for a double-disc refiner H refiner bar height (m) 76 Hi average transfer function for piezo element i (dB) I refining intensity (units depend on definition o f intensity used) KIN sensitivity of piezo element / to a normal force on the sensor probe tip (V/N) Kis sensitivity of piezo element / to a shear force on the sensor probe tip (V/N) KIQ sensitivity of piezo element / to a force acting at angle 0 to the y-axis (V/N) Lbc total length of bar edges crossing Lj length o f refiner bar within radial increment i (m) X fraction of refining zone area constituted by bar surfaces mf oven-dry fibre mass flow rate through refiner (kg/s) p r radial coefficient o f friction [it tangential coefficient of friction \\,t,eq equivalent tangential coefficient of friction Nov average number o f bars per unit length o f arc on refiner plate (m"1) n number o f impacts riimp number o f impacts experienced by pulp in one pass through the refining zone riri number o f bars on rotor plate nSi number o f bars on stator plate 0 angle between the line of action of impact force and the y-axis (°) PaVe average mechanical pressure on refiner plates (Pa) P net refining power (W) n inner radius of the refining zone (m) r2 outer radius o f the refining zone (m) rs radial position of sensor on stator plate (m) 77 R regression correlation coefficient S steam flow term (s"1) SEL specific edge load (J/m) x residence time (s) v radial velocity o f pulp in the refining zone (m/s) Vh peak voltage of hammer signal (V) Vi peak voltage of signal from piezo element i (V) CO refiner rotational speed (rad/s) Q refiner rotational speed (rpm) 78 APPENDIX A SPECIFICATIONS OF D2B502 REFINER PLATES Rotor and stator plates are identical. Inner radius of refining zone, r i = 12.25 cm Outer radius of refining zone, X2 = 15.25 cm Bar width, B = 2.8 mm Bar Height, H = 3.7 mm Groove Width, G = 2.6 mm Number of bars per segment at radial position of sensor (14.6 cm) = 48 Number of segments on rotor = 3 Number of segments on stator = 3 Figure A l . A segment of the rotor plate 79 APPENDIX B PROPERTIES OF PIEZO CERAMIC ELEMENTS Property Piezo Elements in Original Design Piezo Elements in Modified Design Units Material Lead Zirconate Titanate Lead Zirconate Titanate Dimensions 1 mm x 1 mm x 7 mm 1 mm x 2 mm x 7 mm Density 7.65 7.7 g/cm 3 Curie Temperature T c 360 350 °C Electrical Dielectric Constant K 3 3 T 1750 1800 Dissipation Factor 1.6 1.5 % Piezoelectric Coupling Factor kp 0.62 0.6 — k 3 1 0.37 0.34 — k» 0.72 0.69 — Charge Constant d 3 1 -160 -175 10- I2C/N d 3 3 365 400 10 1 2C/N Voltage Constant &i -11.5 -11 10- 3Vm/N & 3 25 25.1 10' 3Vm/N Frequency Constants N P 2050 2057 Hz.m N , 1400 1359 Hz.m N , 1800 1857 Hz.m Elastic Modulus Compliance S„ E 15.5 15.4 10" 12m2/N S 3 3 E 19 18.4 10- 12m2/N 80 APPENDIX C CALIBRATION PROCEDURE This section provides details of the calibration procedures employed with the sensors used in this project. The section is split into two parts, the first explaining the original calibration method, which involved the use o f the mounting j ig , and the second explaining the revised calibration method, which involved impacting the sensor in the plate only. CI. ORIGINAL CALIBRATION METHOD This method consisted of impacting the sensor (mounted in the jig) with the force- measuring hammer along the x- and y-directions, as shown in Figure 3.3. This leads to the determination o f K-values (the sensor response in V / N ) for both normal and shear impacts in the j ig . The sensor is then installed in the refiner plate, and impacted normally (along the y-direction) thus determining the actual sensitivity to normal impacts (as this is generally different from the K-value observed with the sensor in the j ig). The K-value for shear impacts in the plate is then calculated by appropriate scaling according to Equation 3.4. Equations for calculating the forces from the piezo signals are derived from these K-values. This process is shown in detail below for the sensor used for the data in chapter 3. 81 The results of impacting the sensor in the j i g in the normal and shear directions are shown in Figures C I and C2, while Figure C3 shows the results of impacting the sensor in the normal direction while mounted in the plate. .£* -1 § -2 <u -3 -4 -5 -6 • Piezo 1 O Piezo 2 A Piezo 3 V, = 0.0509FN R2 = 0.9492 V : = -0.0419FN V, = -0.0786FN R 2 = 0.992 Magnitude of Normal Force, FN (N) Figure CI. Piezo voltage vs normal impact force (impacts applied in mounting jig). 15 if 10 DC i o > e N « c -10 -15 • Piezo 1 (V) • Piezo 2 (V) A Piezo 3 (V) V 3 =0.1783FS R 2 = 0.9921 Magnitude of Shear Force, Fs(N) Figure C2. Piezo voltage vs shear impact force (impacts applied in mounting jig). 82 es 0 > -1 e N - 2 -5 -6 • Piezo 1 (V) • Piezo 2 (V) A Piezo 3 (V) V 3 = -0.0705FN R' = 0.9935 Tto Magnitude of Normal Force, F N (N) Figure C3. Piezo voltage vs normal force (impacts applied with sensor mounted in plate). The results o f linear regressions are shown on the graphs, and the K-values are determined from the slopes of these graphs. The summarized results of the above are: KjNO'ig) = 0-0509 V / N KisQig) = 0.170 V / N KIN(plate) = 0.0570 V / N K2N(jig) = -0.0419 V / N K2S(jig) = -0.176 V / N K2N(plate) = -0.0473 V / N AjArf/'fe) = -0.0786 V / N /vjstf/g) = 0.178 V / N KiN(plate) = -0.0705 V / N K-values for shear impacts in the plate are now calculated by applying Equation C I (same as Equation 3.4) below: KiN(jig) The use of this equation marks a slight departure from the calibration method used in [1], in which the discrepancy between the K-values from the j i g and plate mounting conditions was not addressed. 83 Equation 3.4 yields: Kls(plate) = 0.190 V / N K2S(plate) = -0.199 V / N Kss(plate) = 0.160 V / N N o w we can state that: (C2a) Rearranging the above equation then gives: (FN) [Fs) \ iN ^iS (C2b) This equation thus gives the normal and shear forces calculated using any desired pair o f piezo elements. A s explained in [1] and chapter 3 of this work, pairs o f piezo elements must be chosen such that they are on opposite sides of the probe, and so only piezo pairs 1-3 and 2-3 are used for force calculations. (Fm,\ (6.96 - 8.69^VX\ S13 3.28 2.58 A F, N23 523 (-7.39 -9.3lYV2} 3.47 2.29 I V, (C3a) (C3b) These equations were used to back-calculate the forces from the piezo responses. A l l the data are shown in the following tables, with the calculated forces and their respective errors shown in the four columns on the right. 84 Table CI. Data for normal impacts applied with Fj^measured) V, v2 v3 (N) (V) (V) (V) 6.26 0.28 -0.26 -0.60 7.79 0.32 -0.34 -0.72 9.63 0.43 -0.42 -0.79 11.16 0.54 -0.50 -0.97 12.08 0.32 -0.42 -1.07 15.15 0.56 -0.58 -1.26 15.45 0.62 -0.62 -1.16 16.37 0.68 -0.64 -1.32 17.29 0.71 -0.62 -1.29 18.82 0.85 -0.72 -1.44 20.66 1.01 -0.83 -1.44 20.97 0.95 -0.86 -1.60 23.11 1.32 -0.92 -1.69 23.11 1.53 -0.94 -1.66 24.03 1.65 -1.06 -1.76 27.10 1.21 -1.12 -2.04 28.93 1.14 -1.28 -2.13 31.69 1.98 -1.36 -2.35 32.30 1.43 -1.38 -2.35 35.26 1.87 -1.41 -2.88 36.03 1.78 -1.48 -2.76 38.33 1.96 -1.61 -2.88 39.09 2.09 -1.83 -3.07 39.86 2.12 -1.76 -3.13 45.22 2.15 -1.80 -3.57 46.75 2.21 -1.92 -3.57 47.52 2.28 -1.95 -3.76 48.28 2.62 -2.16 -3.88 49.82 2.62 -2.23 -4.01 52.88 2.84 -2.19 -4.26 54.41 2.49 -2.11 -4.44 55.18 3.03 -2.31 -4.32 57.48 3.06 -2.42 -4.76 sensor in mounting jig. Fhll3 Error(13) FN23 Error(23) (N) (%) (N) (%) 7.12 13.66 7.52 20.14 8.53 9.44 9.27 18.87 9.83 2.10 10.42 8.22 12.22 9.50 12.75 14.18 11.50 4.80 13.04 7.94 14.80 2.27 15.94 5.25 14.41 6.78 15.42 0.25 16.18 1.16 16.99 3.75 16.14 6.68 16.58 4.12 18.47 1.86 18.73 0.51 19.56 5.33 19.54 5.45 20.48 2.31 21.22 1.21 23.90 3.38 22.56 2.41 25.08 8.53 22.43 2.97 26.73 11.25 24.18 0.60 26.12 3.61 27.26 0.59 26.44 8.60 29.29 1.21 34.19 7.89 31.90 0.65 30.37 5.98 32.06 0.74 38.03 7.85 37.23 5.58 36.29 0.74 36.60 1.60 38.69 0.94 38.69 0.95 41.19 5.35 42.05 7.57 41.95 5.24 42.17 5.81 45.97 1.65 46.48 2.78 46.40 0.75 47.40 1.39 48.46 1.99 49.38 3.91 51.94 7.58 52.08 7.86 53.03 6.45 53.78 7.97 56.72 7.27 55.79 5.50 55.96 2.85 56.98 4.72 58.57 6.15 57.25 3.75 62.59 8.90 62.15 8.14 Mean = 5.42 Mean = 5.05 85 Table C2. Data for normal impacts applied with Fs(measured) v, v2 v3 (N) (V) (V) (V) 1.8689 0.3688 -0.4512 0.37 2.1752 0.4 -0.4512 0.4013 2.3284 0.4313 -0.4825 0.4325 4.0135 0.7125 -0.8263 0.7763 4.3199 0.6813 -0.8263 0.7763 4.3199 0.7438 -0.8575 0.8388 4.7794 0.9375 -0.92 0.8388 5.6985 1.1938 -1.1075 1.0888 7.0772 0.9812 -1.2637 1.3075 8.1495 1.6062 -1.2637 1.37 8.3027 1.4 -1.4825 1.5575 9.2218 1.4187 -1.7012 1.745 9.6814 1.5875 -1.6387 1.745 11.5196 1.9 -1.9512 2.0888 11.826 2.9312 -2.0137 2.1513 12.4387 2.0875 -2.0137 2.2138 13.6642 2.8687 -2.4512 2.5888 14.1238 2.275 -2.295 2.5263 15.0429 2.1312 -2.295 2.62 15.8088 2.6187 -2.5137 2.8388 16.0662 2.7125 -2.92 2.995 16.4216 2.3187 -2.6075 2.87 17.0343 2.4687 -2.7637 3.0888 17.1875 2.9437 -2.5762 2.9013 20.9681 3.4 -3.3575 3.6825 22.1936 3.5875 -3.67 3.995 23.4191 3.9625 -3.92 4.3075 27.0956 4.525 -4.545 4.87 28.6275 4.5875 -4.545 4.995 32.3039 4.9625 -5.3325 5.1825 34.4975 6.6188 -6.4625 7.1312 35.2635 6.15 -6.4938 6.6625 35.3676 5.4625 -5.995 5.745 36.0294 6.6188 -6.9063 7.1312 37.5613 7.0875 -7.1313 7.6 40.625 7.4 -7.4438 8.0687 43.6887 7.0875 -7.275 7.2875 47.5184 8.025 -8.3688 8.5375 48.2843 8.65 -8.6813 8.85 53.6456 8.8063 -8.9938 9.1625 55.1775 9.5875 -10.0875 9.9437 55.4534 9.275 -9.775 9.475 57.4755 10.3687 -10.8688 10.5688 62.0711 10.3687 -10.7125 10.9 63.1127 11.15 -11.9625 11.2625 64.6446 10.3687 -10.8688 11.2125 69.2402 11.3062 -12.1188 11.9938 69.2402 11.3062 -12.1188 11.9938 sensor in mounting jig. Fsis Error(li) Error(23) (N) (%) (N) (%) 2.16 15.80 2.41 29.11 2.35 7.91 2.48 14.23 2.53 8.68 2.66 14.44 4.34 8.13 4.64 15.73 4.24 1.91 4.64 7.53 4.60 6.57 4.90 13.34 5.24 9.62 5.11 6.99 6.72 18.01 6.34 11.19 6.59 6.86 7.38 4.27 8.80 8.02 7.52 7.70 8.61 3.71 8.71 4.92 9.16 0.72 9.90 7.35 9.71 0.29 9.68 0.01 11.62 0.88 11.55 0.30 15.16 28.23 11.91 0.74 12.56 0.96 12.06 3.07 16.09 17.74 14.43 5.63 13.98 1.02 13.75 2.65 13.75 8.60 13.96 7.18 15.91 0.66 15.22 3.70 16.62 3.47 16.99 5.76 15.01 8.60 15.62 4.88 16.07 5.68 16.66 2.18 17.14 0.27 15.58 9.33 20.65 1.50 20.08 4.22 22.07 0.54 21.88 1.40 24.11 2.95 23.47 0.20 27.41 1.15 26.92 0.64 27.93 2.42 27.21 4.95 29.65 8.22 30.37 5.98 40.11 16.26 38.76 12.34 37.36 5.95 37.79 7.17 32.74 7.43 33.96 3.98 40.11 11.32 40.30 11.84 42.86 14.09 42.15 12.22 45.09 10.99 44.31 9.06 42.05 3.75 41.93 4.02 48.35 1.75 48.59 2.26 51.21 6.05 50.39 4.36 52.52 2.09 52.19 2.71 57.10 3.49 57.77 4.71 54.87 1.06 55.62 0.30 61.28 6.61 61.92 7.73 62.13 0.10 62.13 0.10 65.63 3.99 67.30 6.64 62.94 2.64 63.39 1.94 68.03 1.75 69.52 0.40 68.03 1.75 69.52 0.40 Mean = 6.05 Mean = 6.08 86 Table C3. Data for normal impacts applied with Fnfmeasured) v, v2 Vj (N) (V) (V) (V) 4.93 0.22 -0.31 -0.50 7.38 0.38 -0.37 -0.63 8.46 0.44 -0.39 -0.63 8.76 0.41 -0.54 -0.78 9.94 0.51 -0.37 -0.66 12.44 0.59 -0.54 -0.88 12.59 0.59 -0.67 -1.00 13.66 0.84 -0.78 -0.78 13.66 0.75 -0.66 -0.91 14.28 0.69 -0.58 -1.03 16.12 0.75 -0.68 -1.13 16.68 0.75 -0.78 -1.22 17.60 0.78 -0.82 -1.28 18.52 0.91 -0.78 -1.34 20.97 1.33 -1.05 -1.50 21.48 1.06 -1.09 -1.75 22.81 1.25 -1.09 -1.53 24.03 1.22 -1.07 -1.72 24.64 1.72 -1.22 -1.69 25.26 1.34 -1.15 -1.75 28.63 1.32 -1.37 -2.00 29.85 1.69 -1.39 -2.16 32.61 1.48 -1.48 -2.47 33.73 1.75 -1.57 -2.56 35.26 1.81 -1.70 -2.48 37.56 2.06 -1.75 -2.63 40.63 2.25 -2.00 -2.91 47.52 2.69 -2.25 -3.38 48.28 2.79 -2.33 -3.28 50.58 3.12 -2.45 -3.75 51.35 3.08 -2.47 -3.69 59.01 3.29 -2.75 -4.03 62.84 3.48 -2.93 -4.30 62.84 3.48 -2.94 -4.30 63.60 3.87 -2.99 -4.44 64.37 4.26 -3.08 -4.40 65.13 3.78 -3.12 -4.75 sensor mounted in plate. Fm3 Error FN23 Error (N) (%) (N) (%) 5.87 18.96 6.96 41.19 8.04 8.91 8.59 16.29 8.48 0.24 8.74 3.32 9.62 9.76 11.23 28.13 9.27 6.73 8.88 10.68 11.74 5.64 12.11 2.60 12.82 1.83 14.28 13.40 12.66 7.33 13.04 4.58 13.10 4.16 13.31 2.61 13.75 3.71 13.85 2.99 15.00 6.94 15.52 3.71 15.81 5.20 17.11 2.59 16.56 5.88 17.99 2.22 17.99 2.87 18.27 1.31 22.29 6.31 21.69 3.43 22.60 5.24 24.31 13.21 22.01 3.51 22.33 2.10 23.42 2.55 23.87 0.66 26.69 8.30 24.75 0.44 24.56 2.76 24.81 1.76 26.57 7.20 28.71 0.30 30.48 2.11 30.33 1.59 31.75 2.62 33.88 3.91 34.45 2.12 35.48 5.19 34.12 3.23 35.57 0.86 37.17 1.05 37.39 0.46 40.97 0.85 41.90 3.13 48.03 1.08 48.05 1.12 47.86 0.88 47.67 1.27 54.30 7.36 53.02 4.82 53.45 4.09 52.56 2.36 57.86 1.95 57.80 2.04 61.51 2.11 61.66 1.88 61.59 1.99 61.73 1.77 65.50 2.98 63.41 0.30 67.89 5.46 63.69 1.05 67.55 3.71 67.25 3.25 Mean =3.93 Mean =3.14 The mean percentage errors in all cases are quite low, and the graph o f Figure C4 shows a good agreement between the force measured by the impact hammer, and that calculated using the magnitudes of the piezo signals. These two facts suggest that the calibration procedure here is reliable. 87 Measured Force (from force hammer) (N) Figure C4. Calculated force vs. Measured force for normal impacts with sensor mounted in plate. C2. NEW CALIBRATION METHOD A s explained in section 3.4, the original calibration was modified, as it did not account for the change in the sensor's response to impacts in the shear direction when it was transferred from the j i g to the plate. It was seen, time and time again, that the response o f the sensor was extremely sensitive to the mounting conditions. This became an even more significant issue when the use of shims was employed to stiffen the sensor housing, as there was no way to ensure that the preload on the piezo ceramic elements in the j i g was the same as that in the plate. 88 It was therefore decided that calibration had to be performed with the sensor installed in the plate, to ensure that mounting conditions did not change between the time o f calibration and refining trials. This section provides the impact data and details o f the calibration for the sensor used for the data in section 4.2, where the calibration method is outlined. The sensor was impacted at various angles (as described in section 4.2), and K-values (KJQ) were determined for different angles, 0, to the normal direction (as shown in Figure 4.6). KIN was determined as before, by impacting the sensor in the normal direction. Kis was then determined using: cose sin0 This was done for all angles, 0, at which the sensor was impacted, and the mean value o f Kis found in this way was taken as the true Kis- Table C4 shows all the impact data (magnitude o f impact force F from force hammer, and piezo voltages Vj, V3 and V4), along with the true normal and shear forces associated with each impact (F cos0 and F sin0, respectively), and the back-calculated normal and shear components from the piezo signals. Figures C5 through C9 are graphs of the impact data, with linear regressions from which the K-values were determined. These K - values are summarized in Table C5 , which is identical to Table 4.1. 89 Table C4. Data for impacts administered at different angles. e F V, v2 Vs F cosQ FsinQ Fmi Fsi3 Ff/N Fsu o (N) (V) (V) (V) (N) (N) (N) (N) (N) (N) 0 9.19 0.41 -0.56 0.47 9.19 0.00 8.73 0.31 9.47 -0.04 0 11.80 0.52 -0.77 0.58 11.80 0.00 11.42 0.22 11.97 -0.03 0 15.01 0.67 -0.94 0.72 15.01 0.00 14.48 0.48 15.19 0.16 0 15.47 0.67 -1.02 0.76 15.47 0.00 15.01 0.23 15.62 -0.05 0 17.16 0.75 -1.09 0.83 17.16 0.00 16.48 0.39 17.16 0.08 0 17.46 0.77 -1.14 0.83 17.46 0.00 16.99 0.32 17.35 0.16 0 22.06 0.97 -1.45 1.04 22.06 0.00 21.56 0.37 21.87 0.25 0 22.37 0.97 -1.53 1.08 22.37 0.00 22.09 0.12 22.30 0.04 0 22.98 1.02 -1.63 1.13 22.98 0.00 23.29 0.07 23.31 0.07 0 24.51 1.06 -1.67 1.19 24.51 0.00 24.18 0.16 24.47 0.04 0 25.12 1.09 -1.73 1.21 25.12 0.00 24.98 0.12 25.14 0.07 0 26.96 1.13 -1.94 1.32 26.96 0.00 26.73 -0.36 26.54 -0.26 0 28.80 1.23 -2.06 1.41 28.80 0.00 28.90 -0.20 28.75 -0.11 0 29.41 1.30 -2.09 1.44 29.41 0.00 29.87 0.03 29.80 0.08 0 31.25 1.33 -2.22 1.58 31.25 0.00 31.10 -0.21 31.50 -0.38 0 33.70 1.47 -2.56 1.58 33.70 0.00 35.12 -0.58 33.21 0.35 0 35.54 1.52 -2.53 1.74 35.54 0.00 35.48 -0.24 35.39 -0.17 10 6.59 0.39 -0.25 0.17 6.49 1.14 6.46 1.24 6.45 1.25 10 7.20 0.43 -0.29 0.19 7.09 1.25 7.14 1.26 6.98 1.34 10 9.65 0.56 -0.35 0.23 9.50 1.68 9.11 1.76 9.04 1.80 10 10.72 0.62 -0.39 0.27 10.56 1.86 10.16 1.94 10.10 1.98 10 11.64 0.66 -0.41 0.28 11.47 2.02 10.74 2.08 10.70 2.10 10 12.56 0.73 -0.43 0.28 12.37 2.18 11.74 2.42 11.61 2.49 10 14.09 0.80 -0.59 0.40 13.88 2.45 13.63 2.25 13.56 2.29 10 15.32 0.88 -0.56 0.36 15.09 2.66 14.37 2.75 14.12 2.88 10 20.53 1.19 -0.75 0.50 20.22 3.56 19.46 3.75 19.28 3.85 10 20.53 1.16 -0.88 0.63 20.22 3.56 19.93 3.19 20.13 3.11 10 22.06 1.25 -0.91 0.64 21.72 3.83 21.28 3.57 21.41 3.52 10 24.20 1.39 -0.98 0.69 23.84 4.20 23.51 4.05 23.58 4.03 10 25.74 1.47 -1.05 0.73 25.34 4.47 24.88 4.25 24.99 4.22 10 27.57 1.63 -0.98 0.69 27.15 4.79 26.35 5.26 26.42 5.25 10 27.57 1.53 -1.34 0.78 27.15 4.79 27.64 3.63 26.20 4.33 10 27.88 1.64 -1.17 0.83 27.46 4.84 27.81 4.74 27.98 4.68 10 29.87 1.69 -1.47 0.86 29.42 5.19 30.38 4.04 28.86 4.78 10 32.78 1.86 -1.38 0.97 32.28 5.69 31.83 5.23 32.01 5.17 10 32.78 1.83 -1.48 1.05 32.28 5.69 32.19 4.72 32.40 4.64 20 4.29 0.30 0.07 -0.03 4.03 1.47 3.19 1.79 3.36 1.71 20 4.37 0.29 0.06 -0.03 4.10 1.49 3.13 1.71 3.24 1.66 20 5.13 0.32 0.08 -0.04 4.82 1.76 3.28 1.90 3.47 1.81 20 5.36 0.37 0.09 -0.04 5.04 1.83 3.89 2.21 4.14 2.09 20 9.50 0.65 0.14 -0.08 8.92 3.25 6.95 3.83 7.17 3.74 20 10.11 0.68 0.16 -0.08 9.50 3.46 7.18 4.02 7.48 3.89 20 11.18 0.73 0.19 -0.10 10.51 3.82 7.53 4.38 7.87 4.23 20 13.17 0.89 0.22 -0.11 12.38 4.51 9.33 5.33 9.73 5.15 20 14.71 1.03 0.24 -0.14 13.82 5.03 10.90 6.09 11.15 5.98 20 17.46 1.17 0.31 -0.16 16.41 5.97 12.05 7.04 12.62 6.78 20 19.00 1.29 0.34 -0.17 17.85 6.50 13.32 7.75 13.94 7.47 20 23.59 1.62 0.41 -0.21 22.17 8.07 16.82 9.66 17.48 9.36 20 23.59 1.68 0.43 -0.22 22.17 8.07 17.51 10.08 18.26 9.74 20 24.51 1.79 0.40 -0.26 23.03 8.38 18.95 10.52 19.12 10.46 20 25.74 1.86 0.45 -0.24 24.18 8.80 19.44 11.04 20.15 10.72 20 28.34 2.06 0.38 -0.27 26.63 9.69 22.43 11.87 22.40 11.91 20 29.41 2.10 0.55 -0.29 27.64 10.06 21.72 12.59 22.63 12.18 30 5.90 0.49 0.11 -0.08 5.11 2.95 5.17 2.87 5.08 2.91 30 6.28 0.54 0.13 -0.09 5.44 3.14 5.72 3.22 5.73 3.22 30 7.81 0.65 0.14 -0.11 6.77 3.91 6.91 3.82 6.78 3.89 90 e F V, v, V, (°) (N) (V) (V) (V) 30 7.97 0.67 0.15 -0.12 30 8.73 0.73 0.16 -0.12 30 9.11 0.78 0.20 -0.13 30 11.80 1.00 0.24 -0.21 30 15.78 1.33 0.36 -0.29 30 15.78 1.34 0.38 -0.30 30 16.54 1.45 0.33 -0.27 30 17.46 1.52 0.40 -0.33 30 17.62 1.55 0.39 -0.33 30 18.84 1.66 0.47 -0.36 30 19.30 1.67 0.46 -0.36 30 20.83 1.80 0.63 -0.42 30 22.37 1.91 0.64 -0.43 30 24.51 2.09 0.77 -0.49 30 25.43 2.22 0.69 -0.48 30 25.74 2.19 0.83 -0.52 30 31.56 2.78 0.95 -0.61 40 6.20 0.52 0.20 -0.14 40 6.28 0.51 0.19 -0.14 40 7.35 0.61 0.27 -0.17 40 7.51 0.61 0.29 -0.17 40 7.51 0.65 0.26 -0.18 40 10.26 0.89 0.34 -0.28 40 14.09 1.24 0.50 -0.38 40 17.00 1.55 0.83 -0.52 40 17.16 1.58 0.83 -0.50 40 19.61 1.80 0.95 -0.59 40 22.98 2.08 1.01 -0.63 40 23.90 2.19 1.26 -0.77 40 24.51 2.22 1.32 -0.80 40 25.74 2.39 1.39 -0.83 40 25.74 2.33 1.34 -0.83 40 30.94 3.04 1.45 -0.91 40 32.48 3.04 1.64 -1.00 40 34.62 3.32 1.78 -1.09 40 36.00 3.54 2.00 -1.20 40 39.06 3.94 2.16 -1.33 FcosQ FsinQ (N) (N) 6.90 3.98 7.56 4.37 7.89 4.56 10.22 5.90 13.66 7.89 13.66 7.89 14.33 8.27 15.12 8.73 15.26 8.81 16.32 9.42 16.72 9.65 18.04 10.42 19.37 11.18 21.23 12.25 22.02 12.71 22.29 12.87 27.33 15.78 4.75 3.99 4.81 4.04 5.63 4.73 5.75 4.82 5.75 4.82 7.86 6.60 10.80 9.06 13.03 10.93 13.14 11.03 15.02 12.60 17.60 14.77 18.31 15.36 18.78 15.75 19.71 16.54 19.71 16.54 23.70 19.89 24.88 20.87 26.52 22.25 27.58 23.14 29.92 25.11 FN13 Fsn (N) (N) 7.07 3.95 7.71 4.26 8.06 4.63 10.51 5.93 13.65 8.02 13.71 8.16 15.37 8.57 15.67 9.11 16.13 9.23 16.91 10.06 17.14 10.12 17.55 11.28 18.77 11.90 20.20 13.27 22.24 13.66 20.91 13.95 27.27 17.42 4.92 3.31 4.95 3.24 5.56 3.99 5.51 4.08 6.11 4.16 8.41 5.68 11.63 7.99 13.13 10.65 13.47 10.79 15.39 12.34 18.40 13.98 18.08 15.36 18.02 15.69 19.58 16.79 19.22 16.35 27.02 20.33 25.74 20.93 28.18 22.84 29.46 24.69 33.11 27.25 Fm4 FSH (N) (N) 6.94 4.01 7.59 4.32 8.08 4.63 10.04 6.16 13.22 8.23 13.35 8.34 14.98 8.77 15.19 9.35 15.57 9.51 16.53 ' 10.25 16.72 10.33 17.68 11.24 18.95 11.83 20.61 13.09 22.18 13.71 21.44 13.72 27.72 17.23 4.93 3.31 4.86 3.29 5.71 3.93 5.78 3.95 6.13 4.16 7.99 5.89 11.33 8.14 13.71 10.39 14.20 10.46 16.01 12.06 19.11 13.66 19.10 14.89 19.14 15.18 20.88 16.20 20.19 15.91 27.95 19.91 27.03 20.34 29.53 22.23 31.18 23.90 34.73 26.52 91 0° (Normal direction) Force (N) Figure C5. Impacts applied in the normal direction. 10° R = 0.9464 Force (N) Figure C6. Impacts applied at 10° to the normal direction. 92 es a .3° 1 e N • Piezo 1 • Piezo 3 A Piezo 4 20° V, =0.0718F IT = 0.9958 V 3 = 0.0169F = 0.9591 -1 J " * <S0 V 4 = -0.0094F Force (N) = 0.9834 Figure C7. Impacts applied at 20° to the normal direction. 30° es a .3° 1 s« o • Piezo 1 • Piezo 3 A Piezo 4 V, = 0.0864F Rz = 0.9984 0.0269F R =0.9118 R' = 0.975 Force(N) Figure C8. Impacts applied at 30° to the normal direction. 93 40° 05 e Sf 53 o N ii • Piezo 1 • Piezo 3 A Piezo 4 V4 = -0.0313F Force (N) R = 0.9783 4B Figure C9. Impacts applied at 40° to the normal direction. Angle Piezo 1 Piezo 3 Piezo 4 Kie Kis K39 K 3 S K»e K 4 S (°) (mV/N) (mV/N) (mV/N) (mV/N) (mV/N) (mV/N) 0 43.3 - -70.2 - 48.6 - 10 57.0 82.7 -42.1 155.7 28.3 -112.7 20 71.8 91.0 16.9 242.3 -9.4 -161.0 30 86.4 97.8 26.9 175.4 -18.9 -122.0 40 94.6 95.6 50.9 162.8 -31.3 -106.6 Ave K 1 S =91.8 mV/N Ave K 3 S =164.6 mV/N Ave Kis =-113.7 mV/N KIN =43.3 mV/N K 3 N =-70.2 mV/N K 4 N =48.6 mV/N Table C5. K-Values determined by impacting the sensor at different angles A s a validation o f the calibration procedure, the following two graphs (Figures 4.7 and 4.8) show plots of the measured forces from the force hammer signal against the calculated forces from the piezo signals. The graphs show more scatter than Figure C4, which is the equivalent graph for the old calibration method. This is because of the difficulty in administering angled impacts in such a way that the line of action o f the 94 applied force passed through the center of the probe tip. Regardless, the agreement was judged to be sufficiently good for a reliable determination of the forces. 0 5 10 15 20 25 30 35 40 Actual Normal Component (F cosq) (N) Figure CIO. (Same as Figure 4.7) Comparison of calculated and measured normal forces. Actual Shear Component (F sinq) (N) Figure C l l . (Same as Figure 4.8) Comparison of calculated and measured shear forces. 95 APPENDIX D MATLAB PROGRAMS DL CALIBRATION "Cal ibn .nf c l e a r load c : \ l e c r o y \ c a l i b n \ s c l 0 0 0 . d a t load c:\lecroy\calibn\sc2000.dat load c:\lecroy\calibn\sc3000.dat load c:\lecroy\calibn\sc4000.dat % Piezo 1 s i g n a l % Piezo 2 s i g n a l % Piezo 3 s i g n a l % Hammer s i g n a l c l e a r sclOOO sc2000 sc3000 sc4000; cl(1)=max(scl000) c2(1)=min(sc2000) c3(l)=min(sc3000) h(l)=max(sc4000) ; % Maximum piezo 1 voltage % Minimum piezo 2 voltage % Minimum piezo 3 voltage % Maximum hammer voltage load c : \ l e c r o y \ c a l i b n \ s c l 0 0 1 . d a t load c:\lecroy\calibn\sc2001.dat load c:\lecroy\calibn\sc3001.dat load c:\lecroy\calibn\sc4001.dat cl(2)=max(scl001) c2(2)=min(sc2001) c3(2)=min(sc3001) h(2)=max(sc4001) ; % Maximum piezo 1 voltage % Minimum pi e z o 2 voltage % Minimum pi e z o 3 voltage % Maximum hammer voltage c l e a r sclOOl sc2001 sc3001 sc4001; % The program proceeds i n t h i s way u n t i l a l l relevant impacts are processed. The % ve c t o r s c l , c2, c3 and h are then exported t o Microsoft Excel f o r the l i n e a r % r e g r e s s i o n , k-value determination and d e r i v a t i o n of fo r c e equations. D2. TRANSFER FUNCTIONS T F . r r T c l e a r w=hanning(50002); % Define Hanning window load d : \ l e c r o y\calibn\scl000.dat load d:\lecroy\calibn\sc4000.dat tfn=tfe(sc4000,sclOOO,65536,10000000,w) , t f l ( l , : ) = a b s ( t f n ( l : 7 5 0 ) ' ) ; c l e a r sclOOO sc4000; % Piezo s i g n a l % Hammer s i g n a l % C a l c u l a t e t r a n s f e r f u n c t i o n % C a l c u l a t e magnitude of t r a n s f e r f u n c t i o n load d : \ l e c r o y \calibn\scl001.dat load d:\lecroy\calibn\sc4001.dat 96 tfn=tfe(sc4001,scl001,65536,10000000,w); t f l ( 2 , : ) = a b s ( t f n ( l : 7 5 0 ) ' ) ; c l e a r sclOOl sc4001; % The program proceeds i n t h i s way u n t i l a l l relevant impacts are processed, and the % average t r a n s f e r f u n c t i o n i s then c a l c u l a t e d as follows ( u s u a l l y f o r 10 impacts): t f a v l = s u m ( t f 1 ) / l l ; % C a l c u l a t e average t r a n s f e r f u n c t i o n t f d b l = 2 0 * l o g l 0 ( t f a v l ) ; % Convert t o d e c i b e l s f=(0:65535)*10000000/65536; % Define frequency s c a l e fr=f(1:750); figure(1) p l o t ( f r , t f d b l ) ; g r i d on; hold on; t i t l e ( ' A v e r a g e Transfer Function f o r Piezo 1' ) ; x l a b e l ( ' f r e q (Hz)'); y l a b e l ( ' T F (dB) ') ; D3. REFINER FORCE SIGNAL ANALYSIS "Getstats.m" % This program loads p i e z o s i g n a l s , c a l c u l a t e s the shear and normal fo r c e s , r e g i s t e r s the % beginning and end of a l l impacts, and computes the d e s i r e d s t a t i s t i c s such as peak % fo r c e s , c o e f f i c i e n t of f r i c t i o n (as a v r a t i o and p e a k r a t i o ) , and impact d u r a t i o n . % These are then saved as column vectors that are extracted and compiled f o r se v e r a l % s i g n a l s by the program named "Compilestats.m". c l e a r load d:\lecroy\d4ref\scl003.dat load d:\lecroy\d4ref\sc2003.dat V2=scl003; % Piezo 2 Voltage V3=sc2003; % Piezo 3 Voltage c l e a r scl003 sc2003; Fn=-4.40*V2-10.67*V3; Fs=-1.68*V2+2.52*V3; c l e a r V2 V3; % FORCE PROFILE ANALYSIS peakcount=2; % Peak Counter (set at 2 t o s t a r t with because (peakcount-1) % as used below would otherwise give a negative index. avrange=2; % Number of p o i n t s e i t h e r s i d e of point ' i ' used f o r mean value thresh=1.0; % Threshold force value (1 N) f o r recognizing impacts impstart(1)=-150; % Avoids mishandling the f i r s t impact impfinish(l)=-150; buffer=100; % Number of points neglected a f t e r an impact (to help % prevent r e g i s t e r i n g v i b r a t i o n s as impacts) impswitch=l; % Noise Compensation by mean c a l c u l a t i o n f o r i=l:avrange meanFn(i)=Fn(i); meanFs (i) =Fs (i) ,- end f o r i=length(Fn)-avrange:length(Fn) 97 meanFn(i)=Fn(i) ; meanFs(i)=Fs(i); end f o r i=l+avrange:length(Fn)-avrange-1 meanFn(i)=mean(Fn(i-avrange:i+avrange)); meanFs(i)=mean(Fs(i-avrange:i+avrange)); end c l e a r Fn Fs; % F i n d l o c a t i o n of s t a r t and end of impacts f o r i=2:length(meanFn) i f (meanFn(i-l)<thresh) & (meanFn(i)>=thresh) & (i-impstart(peakcount- l)>buffer) impstart(peakcount)=i; impswitch=i; e l s e i f (meanFn(i-1)>thresh) & (meanFn(i)<=thresh) & (impswitch-impstart(peakcount- l)>buffer) & impstart(length(impstart))>0 impfinish(peakcount)=i; peakcount=peakcount+l ; end end end IMPSTART=impstart/250; % Convert i n d i c e s to time (ms) IMPFINISH=impfinish/250; t=(0:4e-3:1000.004); % Compute Impact S t a t i s t i c s f o r j=2:peakcount-l flocsizeindex(j)=IMPFINISH(j)-IMPSTART(j); F n p r o f i l e ( 1 : i m p f i n i s h ( j ) - i m p s t a r t ( j ) + 1 , j ) = m e a n F n ( i m p s t a r t ( j ) : i m p f i n i s h ( j ) ) ' ; F s p r o f i l e ( 1 : i m p f i n i s h ( j ) - i m p s t a r t ( j ) + 1 , j ) = m e a n F s ( i m p s t a r t ( j ) : i m p f i n i s h ( j ) ) ' ; maxFn(j)=max(Fnprofile( :, j ) ) ; maxFs (j ) =max(Fsprofile (:, j ) ) ,- peakratio(j)=maxFs(j)/maxFn(j); a v r a t i o ( j ) = m e a n ( F s p r o f i l e ( 1 : i m p f i n i s h ( j ) - i m p s t a r t ( j ) + 1 , j ) . / F n p r o f i l e ( 1 : i m p f i n i s h ( j ) - i m p s t a r t ( j ) + 1 , j ) ) ; end % Save a l l s t a t s 'Impact* Fn Fs R(pk) R(av) Floe Size Index(ms) impstart i m p f i n i s h 1 [ ( 3 : j ) ' maxFn(3:j)'maxFs(3:j)'peakratio(3:j)' a v r a t i o ( 3 : j ) ' f l o c s i z e i n d e x ( 3 : j ) ' IMPSTART(3:j)' IMPFINISH(3:j)'] stats003=[(3:j)' maxFn(3:j) ' maxFs(3:j)'pkratio(3:j) ' a v r a t i o ( 3 : j ) ' f l o c s i z e i n d e x ( 3 : j ) ' IMPSTART(3:j)' IMPFINISH(3:j)']; meanfnO 03 =meanFn; save d:\research\data\d4ref\stats003; save d:\research\data\d4ref\meanfn003; D4. COMPILA TION OF IMP A CT ST A TISTICS "Compilestats.m" % T h i s program provides a p l o t of the s i g n a l showing the s t a r t and end of impacts % as recognized by "Getstats.m", and outputs a l l the impact data a s s o c i a t e d with % the s i g n a l i n question. This data i s then exported t o Microsoft Excel manually. c l e a r load d:\research\data\d4ref\stats003 98 t=(0:l/1000:50000/1000) ; % P l o t of f o r c e s and s t a r t X f i n i s h p o i n t s f o r the purpose of checking how w e l l % impacts were recognised by the previous program. % The green l i n e s s i g n i f y the s t a r t of the extracted impacts and the red l i n e s % s i g n i f y the end of the impacts. f i g u r e d ) c l f ; h o l d on; plot(t,meanFn,'b',t,meanFs,' r' ) ; f o r j=2:peakcount-l plot([IMPSTART(j) IMPSTART(j)] , [-2 50] , ' g-', [IMPFINISH(j) IMPFINISH(j)] , [-2 50], ' r - end xlabel('Time (ms)'); y l a b e l (' Force (N) 1 ) ,- t i t l e ( ' I m p a c t s at 700RPM, Dec 4, sc*016b'); % D i s p l a y v e c t o r s containing stored v a r i a b l e s 'maxFn' maxFn' 'maxFs' maxFs1 ' p k r a t i o 1 p k r a t i o ' 'avratio' a v r a t i o 1 'impdur' f l o c s i z e i n d e x ' 1 n=' 1 eng th (maxFn) 99 APPENDIX E ESTIMA TED LENGTH OF BARS CROSSING A TANY GIVEN TIME This quantity was estimated in chapter 6 to estimate the total shear force acting on the rotor plate. Assuming equal bar and groove widths, the surfaces of the bars constitute approximately half of the total area of the refining zone. That is: A = 4 r ( E 1 ) where Ab is the total area o f bar surfaces and An is the area of the refining zone. The total bar length is then given by the total bar area divided by the bar width, B, and the total length o f bars crossing is estimated to be half o f the total bar length. Therefore: 2 2 bc AB AB where r/ and r2 are the inner and outer radii o f the refining zone, respectively, and LbC is the total length o f bars crossing at any given time. For the Sprout-Waldron 12-inch laboratory refiner with the D2B502 plates, rj is 12.25 cm, r2 is 15.25 cm, and B is 2.8 mm, giving a value o f 2.3 m for LbC- For the Sprout- Waldron T W I N 60 refiner in [25], ri is 45 cm and r2 is 78.5 cm, and B is assumed to be 2.8 mm, giving a value o f 116 m for Lbc- 100


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