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    A direct approach of modeling batch grinding in

     ball mills using population balance principles and

    impact energy distribution

    Amlan Datta, Raj K. Rajamani* Department of Metallurgical Engineering, University of Utah, 135 South 1460 East Rm 412, Salt Lake City,

    UT 84112 0114, USA

    Received 29 May 2000; received in revised form 5 February 2001; accepted 3 April 2001

    Abstract

    The design and scale-up of ball mills are important issues in the mineral processing industry.

    Incomplete knowledge about the mechanics of charge motion often forces researchers to rely on

     phenomenological modeling to formulate scale-up procedures. These models predict the behavior of 

    large industrial-scale mills using the data obtained in small laboratory-scale mills. However, the

    differences in charge motion in plant-scale and lab-scale mills introduce significant inaccuracies in

    the predictions. In this article, a batch-grinding model using the impact energy distribution of the mill

    is explained. The distribution of impact energy is obtained from the simulation of the charge motion

    using the discrete element method. The model is also verified with experimental data, and the

    strengths and the weaknesses of the model in its current form have been identified. It is anticipated

    that a model, which uses information about impact-energy distribution will overcome some of the

    difficulties faced by the phenomenological models.   D  2002 Elsevier Science B.V. All rights

    reserved.

     Keywords: batch grinding models; ball mill scale-up; impact-energy distribution; discrete element method

    0301-7516/02/$ - see front matter  D  2002 Elsevier Science B.V. All rights reserved.

    PII: S 0 3 0 1 - 7 5 1 6 ( 0 1 ) 0 0 0 4 4 - 8

    * Corresponding author. Tel.: +1-801-581-6386; fax: +1-801-581-4937.

     E-mail address: [email protected] (R.K. Rajamani).

    www.elsevier.com/locate/ijminpro

    Int. J. Miner. Process. 64 (2002) 181–200

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    1. Introduction

    Comminution is a process step for a wide range of industries including cement,

    ceramics, pharmaceutics, paper, pigments, and minerals. Many industrial surveys haveestablished that a significant portion of the total cost of metal production is expended in

    comminution processes. The grinding operation in a ball mill is a capital- and energy-

    intensive process. Hence, a marginal improvement in the efficiency of mill operation will

     be of immense economic benefit to the industry.

    A typical scale-up procedure for designing large industrial-scale mills consists of 

    several steps (Herbst and Fuerstenau, 1980). First, laboratory experiments in smaller size

    mills are conducted under identical operating conditions to obtain the breakage properties

    of a particular ore. Then, these properties are scaled to larger mills using suitable

    mathematical models. In the end, the mill dimensions are computed from the feed and

    the estimated product size distributions. However, the fundamental drawback to this

    approach is that the motion of the charge in a small mill and that in a large mill are

    significantly different. The large mill runs at a much lower absolute speed than the small

    mill, even though the percent critical mill speed value is the same. For example, at 60%

    critical speed, the charge is very clearly divided into cascading and cataracting zones in the

    case of a large mill, while for the same speed only a cataracting zone exists in a small mill.

    Moreover, the laboratory-scale mill uses a ball size distribution with a smaller top ball size,

    which also alters the breakage regime in these two mills.

    The earliest scale-up model for prediction and design of the performance of an

    industrial-scale ball mill was formulated by Bond (1952, 1960), a procedure that evolvedfrom the classical energy-size reduction principle (Austin, 1973). Several criticisms of 

    Bond’s model are found in the literature (Austin et al., 1984; Gumtz and Fuerstenau,

    1970). First of all, the entire size distribution of feed and product is characterized by a

    single parameter called 80% passing size. Secondly, all the grinding sub-processes are

    lumped in a single work index term, and also, the information about ball size distribution

    and lifter design is absent in the scale-up procedure.

    Some of the deficiencies of Bond’s scale-up procedure were overcome in a grinding

    model developed using the population balance principles (Herbst, 1979). The evolution of 

    size distribution in the mill is described by the following equation:

    d½ Hmiðt Þ

    dt   ¼ S i Hmiðt Þ þ

    Xi1 j ¼1

    bij S  j  Hm j ðt Þ ð1Þ

    where   mi   is the mass fraction of a particular size class   i,   S i   is the selection function or 

    fractional breakage rate of size class  i,  bij  is the breakage distribution function of the size

    class, and   H   is the mass hold-up of the mill. This phenomenological model has the

    required kinetic parameters, which is an improvement over the Bond model.

    In scale-up procedures utilizing the population balance model (PBM), the selection and

     breakage functions are determined in a small laboratory mill. The laboratory experiments

    are done with nearly identical feed materials and operating conditions. Then, these para-meters are scaled for bigger industrial mills. It has been shown experimentally that the

     breakage function does not depend upon the grinding environment and can be normalized

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    with respect to the size (Broadbent and Callcott, 1956; Herbst and Fuerstenau, 1980;

    Herbst et al., 1981). So the size-normalized values obtained for a particular ore in a la-

     boratory-scale mill can be used for an industrial mill.

    Herbst and Rajamani (1982) applied the specific selection function hypothesis (Herbst and Fuerstenau, 1973; Herbst et al., 1973) for scaling up the selection function. The

    selection function is proportional to the mass-specific power input to the mill. The constant 

    of proportionality is known as the ‘‘specific selection function’’.

    Therefore, knowing the required mill capacity and the power consumption, one can

    calculate the selection function of the industrial mill. However, the variation of grinding

    regimes as influenced by the mill diameter, the ball sizes, and the lifter configuration was

    not included in the model.

    Austin et al. (1984) proposed a more elaborate model where each individual design

    and operating parameter including mill diameter, rotational speed, ball size distribution,

    and powder filling were accounted for while computing the selection functions for the

    industrial mill. However, this method requires calculation of several empirical parame-

    ters.

    The problem with all the methodologies is that the mill is treated as a black box. In

    other words, instead of incorporating the mode of energy expenditure in the mill, PBM

    links the feed and the product size distribution via a series of model parameters. The effect 

    of ball size distribution on grinding has not been clearly interpreted. Breakage regime and

    the mixing efficiency are dependent on the mill size, ball size distribution, lifter 

    configurations, and other parameters.

    The model envisaged here is an approach wherein the numerous collisions occurringin the mill are modeled first, and the results are coupled with breakage of particles as

    they are caught in these collisions. As a result, one obtains the evolution of size dis-

    tribution in the mill. It is anticipated that this technique eventually will lead to a pro-

    cedure where the capacity of a mill can be directly estimated without any intermediate

    scale-up procedure.

    2. Grinding model based on impact energy

    Previously, several researchers have proposed the concept of energy-based breakagerate and breakage distribution functions and have attempted to derive these functions from

    the collision patterns inside a mill (Narayanan, 1987; Cho, 1987; Hofler and Herbst, 1990;

    King and Bourgeois, 1993; Morrell and Man, 1997). Some of these models did not have

    adequate information about impact patterns in the mill, and in other cases, the models were

    too complex and required a considerable amount of parameter estimation. In order to

    reduce the difficulties encountered in the previous efforts, a simple and direct model is

    formulated here that requires minimal parameter estimation.

    In practice, all the operating parameters, such as ball size distribution, absolute value of 

    mill speed, and lifter configurations, differ between small and large mills. These

     parameters directly affect charge motion and, hence, the distribution of collision energy.Therefore, the collision energy distribution is the most fundamental phenomenon that 

    should be the basis of any grinding model of a ball mill. During the tumbling action in a

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     ball mill, it is assumed that each collision nips a certain amount of material of a particular 

    size class and breaks some material in that class. The broken material is redistributed in the

    lower sizes, and this distribution depends on the energy of that collision. The breakage due

    to the tumbling action, as shown in Fig. 1, is assumed to be equivalent to subjecting

    Fig. 1. Grinding phenomenon in a ball mill as interpreted in terms of collision energy and frequency.

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    individual layers of particles to a series of impacts of various energy levels at an identical

    rate. Thus, the grinding action is idealized as each of the ball-to-ball collisions capturing a

    specific mass of particles. It is assumed that collisions of energy  ek   are generated in the

    tumbling charge at a rate of  kk  collisions per second and that each collision of energy  ek nips  m  j,k  grams of particles in size interval  j . The breakage function based on the energy,

    bij,k , is defined as the fraction of that  m  j,k  grams of broken particle from size  j   that reports

    to a smaller size i. For all size classes of particles and all collisions associated with various

    levels of energy, a population balance equation for a batch grinding mill can be written as:

    d M iðt Þ

    dt   ¼

    X N k ¼1

    kk mi;k  M iðt Þ

     H   þ

    X N k ¼1

    Xi1 j ¼1

    kk m j ;k bij ;k  M  j ðt Þ

     H   :   ð2Þ

    The term M i(t )/  H  in Eq. (2) represents the instantaneous mass fraction of size class  i  in

    the mill. This term acts as an ‘‘effectiveness factor’’ for the collision. It implies that the

    total number of collisions of an energy level is distributed to all the size classes in

     proportion to their instantaneous mass fraction. This idea is indirectly in accordance with

    the principle of first-order breakage kinetics. The model equation incorporates three input 

    terms: the impact energy spectra, broken mass in the particle bed at a given impact energy,

    and the energy-based breakage function. The first one is obtained from the simulation of 

     ball charge motion, and the other two are experimentally determined from drop-ball tests.

    The implicit assumptions of the model are the following.

    (1) Breakage of particles due to abrasion is negligible. Impact is the only mode of 

    energy transfer from the grinding media to the particles. In other words, shearing of  particles during ball-to-ball or ball-to-wall collision is absent.

    (2) Each collision takes part in grinding. This means each collision nips some material

    regardless of the location of the collision. This is a valid assumption, if the fractional mill

    filling of the media interstices is more than 1.0.

    (3) The content of the mill is perfectly mixed, i.e., the size distribution of the particle

     bed caught between two colliding balls is the same as the prevailing distribution in the

    entire mill. This assumption is valid for dry grinding where internal classification is not as

     prevalent as in wet grinding.

    (4) There is no progressive damage leading to breakage due to low-energy impacts, i.e.,

     breakage due to repeated collisions at low energy is not accounted for in the model.(5) The linearity assumption is also implied here, i.e., the broken-mass and breakage

    functions remain the same as the size distribution changes in the mill. It has been

    established by earlier research (Schonert, 1979) that the breakage characteristics of a

     particle depend upon the size distribution of particles around it. Nevertheless, this

    assumption simplifies the effort needed to conduct the drop-ball experiments. The

    alternative is to conduct drop-ball tests for all possible grinding environments, which

    would be too time-consuming.

    (6) In deriving both the breakage parameters by drop-ball tests, it is assumed that the

     particle bed that is nipped between two colliding bodies is made up of four layers of 

    material. There is a significant difference in the breakage characteristics when a single particle, a monolayer, and a multilayer of particles are stressed in a collision. Therefore,

    this assumption implies an average grinding environment in the mill.

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    3. Obtaining impact energy spectra by the discrete element method

    The impact energy spectrum is obtained from numerical simulation of the ball charge

    motion, which is based upon the discrete element method (DEM) (Cundall and Strack,1979). This technique computes the finite displacement and rotation of bodies isolated by

    a distinct and undeformable boundary, as these bodies undergo collision and translation. It 

    is a suitable choice for a ball mill, where the balls and the mill shell are treated as distinct 

    elements.

    There are a few studies on the measurement impact forces in the ball mass that have

     been reported in the literature (Dunn and Martin, 1978; Rolf and Vongluekiet, 1984;

    Vermeulen et al., 1984; Yashima et al., 1988; Van Nierop and Moys, 1996). However, it is

    very difficult to develop suitable instrumentation to measure the impact energy distribution

    in the harsh environment that prevails inside a mill. Therefore, numerical simulation of the

     ball charge motion appears to be a better tool for this purpose. Morrell (1992) modeled the

    cascading ball charge as a series of concentric ball layers, each one slipping against the

    adjacent layer of balls. However, this approach does not predict the impact distributions.

    Powell and Nurick (1996a,b), on the other hand, modeled the trajectory of one ball carried

    upward and released by the lifter, which gives only the impact energy due to cataracting

    motion. The most suitable simulation is the DEM simulation (Mishra and Rajamani, 1992,

    1994; Rajamani et al., 2000; Kano et al., 1997; Cleary, 1998), which accounts for the

    geometry of the lifters and which allows individual balls to take their own free trajectory

    depending on their position in the mill.

    In the two-dimensional discrete element simulation scheme, a ball is represented as adisc with a mass equal to that of the sphere, and the circular mill shell including the lifters

    is represented by a series of straight lines (walls). The DEM models the ball-to-ball

    collision with a linear spring and dashpot. The spring provides the repulsive force and the

    dashpot dissipates a portion of the relative kinetic energy. During collision, the balls are

    allowed a virtual overlap  D x, and the normal   v n  and tangential   v t   relative velocities de-

    termine the collision forces. The normal force is given by:

     F n ¼ k nD x þ C nv n   ð3Þ

    where k n is the normal spring constant and  C n is the normal damping coefficient. The ballsrebounding after collision follow a free-flight trajectory as per Newton’s law until the next 

    collision. Likewise, a pair of spring and dashpot is used in the tangential direction.

    The two quantities of interest within the scope of the current work are the mill power 

    draft and the impact energy distribution. At each collision, a fraction of the supplied

    energy is consumed, which is modeled by the dashpot. Thus, the addition of the product of 

    normal and shear force on the dashpot and respective overlap (subscripts n and s denote

    normal and shear direction, respectively) gives the energy lost at that contact, which is

    given by:

     E  ¼X

    Xk 

    jC nAv nA

    2Dt 

    þ

    C sAv sA2Dt k

      ð4Þ

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    where the energy loss term is summed up over all the collisions (k ) and for all the time

    steps (t ). The energy associated with each of the collisions is summed over a few

    revolution of the mill, which leads to the impact energy distribution and power draft.

    Lacking any measurement technique for recording energy in individual collision inside themill, we rely on the accuracy of the simulation’s power draft prediction. A detailed

    investigation of the capability of the DEM simulation for predicting the power draft of ball

    mills of different sizes is reported elsewhere (Datta et al., 1999). The agreement between

    the measured and predicted power draft implies that the impact energy distribution

    computed with this simulation scheme is a reasonable approximation of the true spectrum

     prevailing in the mill.

    4. Experimental work 

    A drop-ball apparatus was used in this work to determine experimentally the broken-

    mass (mi,k ) and the energy-based breakage function (bij,k ). The apparatus used in this work 

    is similar to the ultra-fast load cell (Hofler and Herbst, 1990; Bourgeois et al. 1992). The

    key factors in this method are the drop-ball diameter, particle bed configuration, and anvil

    geometry. A certain amount of material corresponding to four layers of particle bed was

     placed on top of the anvil in a thin paper cup. Then, a ball of desired size was dropped on

    that bed from a desired height. After breakage, the broken mass was size analyzed for the

    distribution of progeny particles. For each collision energy, the breakage functions were

    determined by averaging the results from 40 to 50 test samples. Hence, experimental error was minimized to a large extent. Broken-mass data was obtained from about 5 to 10 test 

    samples for each collision energy. Small sieves of diameter 7.6 cm (3 in.) were used in size

    analysis to minimize material loss when handling the small amounts of sample.

    Batch grinding tests were performed in three mills (diameters 25.4, 38.1, and 90.0 cm)

    using limestone as feed material. In addition, the data of Siddique (1977) on the same

    25.4-cm mill were also examined. In all these experiments, the power draft was calculated

    from experimentally measured torque on the drive shaft. Table 1 shows the operating

    conditions maintained in these experiments.

    Limestone from two different sources, referred to as limestone-A and limestone-B, was

    used. Breakage parameters were obtained separately for these two types of material. Twoexploratory batch-grinding tests were conducted using both materials under the conditions

    reported by Siddique (1977) in the 25.4-cm diameter mill. The mill product size

    distributions over various grinding times obtained from Limestone-A were close to those

    reported by Siddique. Hence, the breakage parameter from that particular limestone was

    used while examining Siddique’s data.

    5. Results and discussions

    The charge motion of the experimental mills was simulated by the DEM simulationcode using the parameters presented in Table 1. As seen in Table 1, the predicted mill

     powers are in good agreement with the measured mill power data. The computed impact 

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    Table 1

    Experimental conditions and mill power draft of batch grinding tests

    D L (cm) Feed size (mm) Ballload (%)

    % Critical

    mill speed

    Lifter configurations Ball size distribution

    (size in cm wt.%)

    25.4 29.2 2.36 1.7 35 65 8, Rectangular (1.9 0.5 cm) Monosize (5.08 – 100%)

    38.1 29.2 2.36 1.7 35 65 10, Rectangular (2.5 0.9 cm) Monosize (5.08 –100%) 90.0 14.0 9.5 6.35 20 40 8, Square (4.0 4.0 cm) Monosize (5.08 – 100%) 25.4 29.2(Siddique, 1977)

    1.7 naturalfeed

    50 60 8, Rectangular (1.9 0.5 cm) Multisize (3.81 – 53%, 2.51.91–12%, and 1.27–5%

    38.1 29.2(Siddique, 1977)

    1.7 naturalfeed

    50 60 10, Rectangular (2.5 0.9 cm) Multisize (3.81– 53%, 2.51.91–12%, and 1.27–5%

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    energy distributions are presented in Fig. 2. Generally, the total number of impacts in the

    25.4-cm mill is less than that in the other two mills. Further, the maximum energy of 

    impact in this mill is only 0.475 J. The impacts in mid- and high-energy intervals are

    greater in number inside the 90.0-cm mill than in the 38.1-cm mill. Moreover, in the lower energy range, the numbers of collisions are very close for the 90- and 38.1-cm mills. Even

    though the 90.0-cm mill exhibits only a cascading charge, compared with the 38.1-cm

    mill, which exhibits both cascading and cataracting charge, the number of low-energy

    collisions is the same in both the mills. In recording the impact spectrum from simulation,

    an energy interval of 0.01 J was used to increase the accuracy of predictions made with the

    impact-energy-based population balance model.

    First, to parameterize the model, a study of the breakage behavior of limestone-A and

    limestone-B was undertaken. The general trend of variation of broken mass with impact 

    energy is shown in Figs. 3 and 4. The broken mass is defined as the amount of material

     passing through the bottom screen, which brackets the monosize feed material. The bro-

    ken-mass versus impact-energy data was fitted with a logarithmic function for inter-

     polation purposes. In the lower energy range, the broken mass increases sharply with

    impact energy, which is not the case at higher energy. At the same level of impact energy,

    the broken mass of particles of bigger size is more than that of smaller particles, and this is

    attributed to the greater density of internal flaws in bigger particles. However, this trend is

    reversed in extremely low-energy collisions, as evident in Fig. 4. At such low impact 

    Fig. 2. Impact energy distribution in ball mill of different diameter. Conditions are described in Table 1.

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    force, the applied stress does not exceed the critical fracture stress considering the high

    cross-sectional area of the bigger particle. The critical stress of a large particle is lower 

    than that of a small particle due to the higher density of internal flaws.

    The general trends of the breakage distribution function are presented in Figs. 5 and 6

    for the two limestones. They exhibit a finer distribution with the increase in the energy of 

    the impact. It was established by earlier research (Hofler and Herbst, 1990) that high-

    energy impacts are low in efficiency. A significant portion of the energy of impact iswasted in the collision between the anvil and the drop-ball, as well as in displacing the

     particles in the bed. Therefore, as we increase the impact energy, the fineness of the

     product increases steeply in the beginning. As shown in Figs. 5 and 6, the extent of 

    fineness diminishes in the higher energy range.

    It has been often found that the breakage functions used in the population balance

    models are normalizable with respect to the parent size interval (Herbst et al., 1973;

    Siddique, 1977). The normalized size is defined as the ratio of the bottom size of each

    interval to that of the parent size class. This particular behavior of broken particle

    fragments is extremely convenient for modeling breakage phenomena, since a progeny

    distribution obtained from one size class of particle is applicable for other size classes also.In the drop-ball tests reported here, two different size classes exhibit the same progeny

    distribution, as shown in Fig. 7, for identical impact energy when plotted against the

    Fig. 3. Variation of broken mass with particle size and impact energy. Material = limestone-A; drop-balldiameter = 5.08 cm; particle bed configuration = four layers.

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    Fig. 4. Variation of broken mass with particle size and impact energy. Material = limestone-B; drop-balldiameter = 5.08 cm.; particle bed configuration = four layers.

    Fig. 5. Breakage functions for different impact energies. Material = limestone-A, 2.36 1.7 mm (four layers);drop-ball diameter = 5.08 cm.

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    normalized size. However, several previous research initiatives (Austin et al., 1984; Cho,

    1987) demonstrated that an abnormal nature of the progeny distribution was evident in

    Fig. 6. Breakage functions for different impact energies. Material = limestone-B, 9.5 6.35 mm (four layers);drop-ball diameter = 5.08 cm.

    Fig. 7. Breakage function normalized with respect to parent size. Material = limestone-A; particle bed

    configuration = four layers; drop-ball diameter = 5.08 cm.

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    some grinding experiments using coarser mill feed. Thus, it is anticipated that there is a

    dependence of the breakage distribution function on feed size and ball size distribution.

    Tavares (1997) also confirmed the dependence of breakage distribution on particle size, by

    single-particle breakage experiments. Likewise, as seen in Fig. 8, the coarse particleexhibited a non-normalizable breakage function. The size distribution of progenies is

    coarser for the first two size intervals compared to the smaller particle sizes for the same

    energy input. Therefore, whenever large particles were used as the feed material, two

    different sets of breakage functions were used for the large and small size classes in the

    computation of the mill product size distribution.

    While the model is formulated in precise detail regarding the collision energy and the

    size of particles nipped in a specified collision, in the actual milling operation inevitably

    the situation is much different. Hence, a multiplication factor of 0.8 was found necessary

    in the appearance and disappearance terms in the right-hand side of Eq. (2), particularly for 

    the predictions for the 38.1- and 90.0-cm mills. This possibly indicates that the efficiency

    of grinding reduces when there is greater amount of fine material in the mill. However, it is

    difficult to quantify this effect and incorporate it explicitly in the model. Nevertheless, this

    simple correction parameter gave reasonably good predictions of all the experimental

    results.

    Fig. 8. Breakage function normalized with respect to size. Material = limestone-B; particle bed-configuration

    = four layers; drop-ball diameter = 5.08 cm.

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    The logarithmic functions shown as solid lines in Figs. 3 and 4 between the amount of 

     broken mass and impact energy were used for interpolation. Broken-mass values of size

    classes at which drop-ball tests were not conducted were calculated by interpolation. The

    energy-dependent broken-mass values were determined only for the first five size intervalsdue to the difficulty in executing a drop-ball test for extremely fine sizes of particles.

    Therefore, the mill product size distribution was also predicted for the first five size classes

    only. Some dependence of broken mass on the drop-ball diameter was observed in this

    study. Therefore, for the grinding experiments with multisize balls in the charge, a

    combined broken-mass data in proportion to the mass fraction of balls of different size was

    used for prediction. This technique was previously used by Austin et al. (1976) to modify

    the selection function in the PBM equation in proportion to mass fractions of media sizes.

    The breakage function data for the complete range of energy values were also

    determined by interpolation, since it was not possible to do drop-ball tests for extremely

    low values of impact energy; the required data were obtained by extrapolating the

    available values. Breakage functions were determined from the parent size class and

    applied to other sizes assuming that they are normalizable with respect to size. There was

    no variation of breakage function due to the size of drop-ball; hence, the breakage function

    obtained from the top-size of the ball charge was used as input for grinding simulations

    with multisize ball charge.

    The predicted results are in good agreement with the measured data for 25.4- and 38.1-

    cm mills (Figs. 9 and 10), and the model is able to predict the size distribution with

    reasonable accuracy even for longer grinding times. The predicted values of median size

    (d 50

    ) and the 80% passing size (d 80

    ) shown in Figs. 11 and 12 are quite close for thesegrinding cases. However, the predicted results for the 90-cm mill shown in Fig. 13 were in

    general not as good as the other two mills. The high particle-to-ball diameter ratio in this

    Fig. 9. Predicted and measured product size distributions: 25.4-cm mill, 35% ball load, 55 rpm speed, 100%

    5.08-cm balls.

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    mill is the reason for the poor prediction. The anomalous nature of the breakage of coarse

     particles is well documented in the literature (Austin et al., 1984). When the ball diameter 

    is relatively larger compared to the particle size, then the particles fill up high individual

    interstitial volumes. Hence, the chance of breakage due to abrasion is greater. Never-theless, in its current state the model is quite useful to estimate the mill performance in

    terms of the median size (d 50), as shown in Fig. 14.

    Fig. 10. Predicted and measured product size distributions: 38.1-cm mill, 35% ball load, 41 rpm speed, 100%

    5.08-cm regular steel balls.

    Fig. 11. Predicted and measured d 50 and d 80 of the mill product: 25.4-cm mill, 35% ball load, 55 rpm speed, 100%

    5.08-cm balls.

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    The model was also tested on grinding experiments where multi-size feed and balls

    constituted the mill charge. The operating conditions are listed in the last two rows of 

    Table 1. A natural feed of   10 mesh (1.7 mm) was charged in the mill in both tests. The

     ball charge was made up of a mixture of 3.81-, 2.54-, 1.91-, and 1.27-cm diameter balls.The predictions are shown in Figs. 15 and 16. Although the grinding media was made up

    of four size classes of ball, breakage data for only 3.81- and 2.54-cm balls were available.

    Hence, the mass of balls in the 1.91- and 1.27-cm diameter classes was equally distributed

    Fig. 12. Predicted and measured  d 50  and  d 80  of the mill products: 38.1-cm mill, 35% ball load, 41 rpm speed,

    100% 5.08-cm regular steel balls.

    Fig. 13. Predicted and measured product size distributions: 90.0-cm mill, 20% ball load, 18 rpm speed, 5.08-cm

     balls (100%).

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    into the 3.81- and 2.54-cm classes while simulating the charge motion of these two mills.

    Even with this approximation, the predictions were close to the measured product size

    distribution.

    It is anticipated that, with further modification in the simulation and prediction scheme,

    the model will become more accurate in the estimation of mill product size distributions.For example, the probability of a collision nipping some particles has been assumed to be

    equal irrespective of the location. This assumption will certainly introduce an error in the

    Fig. 14. Predicted and measured  d 50 of the mill product: 90-cm mill, 20% ball load, 18 rpm speed, 100% 5.08-cm

     balls.

    Fig. 15. Predicted and measured product size distributions: 25.4-cm diameter mill, 50% ball load, 55-rpm mill

    speed, 3.81-cm top-size ball.

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     prediction and lead to overestimation of the fineness of the product size distribution.

    Further work will divide the collisions in terms of their spatial distribution and a

     probability factor incorporated in the model. Furthermore, the nipped particle bed was

    assumed to be made up of four layers of material. More realistically, the particle bed

     between two colliding balls will be composed of something in between a monolayer and

    several layers of material. In order to avoid this shortcoming of the model, the distance

    traveled by two balls in the mill during the course of a collision should be taken into

    account. This distance will be a fairly good indication of the number of layers of material

    caught in the collisions. However, the complexity of the prediction scheme will increase if 

    these modifications are incorporated.

    6. Conclusion

    A direct simulation approach for the modeling of the evolution of particle size in a

    tumbling mill is described. This approach treats the grinding process as a multitude of 

    collisions of various energy values in which a bed of particles is caught and broken. The

     breakage process in a collision is idealized as a bed of four layers of particles being nipped

    in an impact of a specified energy. Schemes for the calculation of impact energy and

    measurement of breakage process in a collision are described. Such an idealization ob-

    viously implies severely restrictive assumptions. Despite the assumptions, the model pre-

    dictions are satisfactory, which suggests that this approach is worth further development.

    For example, all of the collisions are taken as normal collision forces that nip a bed of 

     particles, whereas, in reality, numerous collisions occur in oblique directions. This resultsin shearing of the particle bed, and shearing in turn produces finer fragments. A shear cell

    apparatus may be useful for characterizing this type of breakage of the particle bed. With

    Fig. 16. Predicted and measured product size distributions: 38.1-cm diameter mill, 50% ball load, 43 rpm mill

    speed, 3.81-cm top-size ball.

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    these suggested modifications in the mill charge simulation as well as the experimental

    technique, it is anticipated that the model predictions will be improved further.

    Acknowledgements

    This research has been supported under Grant Number G1115149 from the United

    States Department of Interior, administered by the US Bureau of Mines through the

    Generic Mineral Technology Center of Comminution.

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