Design Models of Trommels for Resource Recovery Processing
Transcription
Design Models of Trommels for Resource Recovery Processing
DESIGN MODELS OF TROMMELS FOR RESOURCE RECOVERY PROCESSING HARVEY ALTER Chamber of Commerce of the United States Washington, D.C. JEROME GAVIS Department of Geography and Environmental Engineering Baltimore, Maryland MARC L. RENARD National Center for Resource Recovery, Inc. Washington, D.C. terial riding on the barrel ABSTRACT surface d The design of a trommel requires knowledge of the number of impingements necessary to achieve a desired efficiency of separation of undersized ma E(xo,xm) = size of a spherical particle = efficiency of separation of particles in the size range terial from a feed stream and of the radius, length, Xo EO;; x <,xm inclination angle, and rotational speed necessary to f provide the required number of impingements for a = fraction of a barrel revolution per particle impingement specified mass feedrate. Expressions for predicting the number of impingements required are derived, f(x) based on expressions for the probability of passage of a particle through a hole, and for the particle size distribution according to number, The dynamics F(xo,xm) of particle motion in the trommel are described and = size distribution of particles = according to number " , fract on of articles in the � � feed in the SIze , Xo EO;;x EO;;xm used to derive equations for predicting the dimen- g = gravitational constant sions of the trommel and the rotational speed, Ex- h = vertical height 'to which a amples are given to show how the equations may be particle rides on the barrel applied. = trommel per impingement NOTATION Meaning a Dimensions (mass length, time) a round hole, short side of a rectangular hole = size of the long side of a rec tangular trommel hole b = n = number of impingements = mass feedrate needed to achieve a desired efficiency of a square hole, diameter of A = length of the trommel L M = size of a trommel hole - side p = Probability that a particle passes through a hole per L impingement p L = probability that a particle passes through a hole in n impingements thickness of the layer of ma- 361 L/t" L distance a particle moves longitudinally in the Symbol L L L L M/t P(X) P(xo, xm) = = Q = R = t = x = Xg = = {3 = = = Pb = = r = probability that a particle of size x passes through a hole in n impingements INTRODUCTION probability that particles in the size range Xo <:x <:xm pass through a large number of holes ratio of hole area to screen area, percent open area inside radius of the trommel L time of flight during a particle trajectory t size of a particle in a feed with a nonuniform size distribution L geometric mean size of particles with a log-normal size distribution angle above the horizontal diameter to which a particle rides • angle of inclination of the trommel angle of impingement rela tive to the vertical diameter of the barrel angle of impingement rela tive to the normal to the barrel surface at the point of impingement density of material in the layer riding on the barrel surface MIL 3 logarithmic standard devia tion of sizes of particles with a log-normal size dis tribution residence time of particles in the trommel THE SIZE SEPARATION PROCESS t =a derived factor, listed in Table 1 =a derived factor, listed in Table 1 w = angular rotational velocity of the trommel Rotary screening is growing in acceptance as a separation method in the' processing of municipal solid waste (MSW) for resource recovery. The use of rotary screens, commonly called "trommels," in solid waste processing can be traced at least as far back as 1928 [1] . In fact, a proposal to use a trom mel for such purposes was reported as early as 1924 [2]. More recently, trommels have been in corporated in various places in the processing streams of resource recovery plants in Monroe County, New York [3], Ames, Iowa [4], New Orleans, L)Usiana [5], Baltimore, County, Mary land [6], and Bridgeport, Connecticut [7], in North America, and in several plants in Europe [8]. Trommels have been used in minerals processing for more than four centuries. Because their use in resource recovery processing is recent, there is an almost complete lack of reported methods of de sign and scaling factors for applications in resource recovery processing. Recognizing this lack, several investigators initiated experimental programs in order to obtain empirical design and scaling criteria for particular resource recovery applica tions [9-11]. None of the published reports, however, leads to an understanding of the screening mechanism, nor provides methods by which trommels can be de signed and scaled for resource recovery and other applications. The purpose of this paper is to present a quanti tative description of trommel screening and to pro vide at least an approximate method for the design and scaling of trommels that will be generally ap plicable in resource recovery (and other) processing. Lft Once the maximum dimension of the under sized material has been decided and the screen hole size fIxed, it is necessary to determine the number of times the material to be screened must impinge on the screen surface in order to achieve the desired separation. The design is established when the dimen sions and rotational speed of the trommel that will provide the required number of impingements are specifIed. The determination of the number of impinge ments needed is a problem in probability; the num ber is a function of the cumulative probability that the desired number fraction of undersized material passes the screen. When a spherical particle of diam- 362 eter d impinges on a square hole of side a(a > d), the probability that it will pass through the hole is p = d I- a 2 (1) Q an equation originally given by Gaudin [12]. This equation also describes the probability that the par ticle will pass through a circular hole of diameter a. The factor Q is the ratio of the hole area to the total screen surface area. As Gaudin pointed out, this is a lower limit on the probability, since reflec tion from the edges of the hole is ignored. Equa tion (1) is strictly correct for particles impinging normal to the screen surface, although there is only a small change for small deviations from normal impingement [12] . When the hole is rectangular, the probability becomes [12] p = l_d a 1- � Q (2) A where a and A are the rectangular dimensions of the hole. The cumulative probability that a particle will pass through a hole after n impingements is p = n � p (1 - p) j= 1 i-I = I- (1 - p) n (3) In the absence of particle-to-particle interaction, this is also the cumulative probability that a large number of uniformly sized particles will pass through a large number of holes after n impinge ments. If the particles are not uniform in size, the probability that particles of size x 1 will pass after n impingements is 1-(1- p) n f (xd (4) where f(;c 1 ) is the number fraction of particles of size XI, i.e., the size distribution function of the particles evaluated at X I. The probability for all particles equal to or greater than a minimum size Xo and equal to or less than a maximum size xm is the integral n xm dx (5) P (xo,xm) = J f (x) 1- (1- p) Xo an equation first given by Sucher [13] . Sucher has also given an alternative form for Eq. (5), suggesting that the probability of particles passing at the nth impingement is a function of the composition of the material after the nth impinge ment rather than of the material approaching the nth impingement from the (n - I) st impingement. Then 363 It is not evident, a priori, whiCh of these equations better describes reality. Real particles, of course, are not spherical. One means of broadening the derivation to include non spherical particles is to alter the distribution func tion, f (x), to reflect an equivalent spherical size dis tribution by inclusion of suitable shape factors for particles in each size range. An alternative is to ob tain an overall shape factor empirically for given types of feed materials by comparison of the equa tions with experimentally determined probabilities. The action of a trommel is to cause the feed material to impinge n times on the screen surface as it passes through; Eq. (6) expresses the cumula tive probability that particles ranging in size be tween Xo and Xm wil l be screened out during their sojourn in the trommel. The total fraction of par ticles in this size range in the feed is which is the cumulative size distribution between Xo and Xm. The efficiency of the trommel is then E (xo,xm) = P (xo, xm)/F (xo, xm) (8) In words, the efficiency is expressed as the ratio of the number fraction of undersized material removed to the number fraction of undersized material in the feed. It is important to note that the efficiency is expressed in terms of number fractions rather than weight fractions, which are usually measured. Because Eq. (5-8) allow the efficiency to be cal culated as a function of n, when the size distribu tion,! (x), is known, the number of impingements necessary to achieve a desired fractional separation of undersized material from the feed can be deter mined. Because the increase in probability resulting from reflection of particles from the edges of the holes has been neglected, the number of impinge ments needed to attain a specified effic.iency may be somewhat lower than the calculated number in practice. This is offset, however, by the decrease in probability resulting from particle-to-particle in teraction, e.g., adhesion or deflection by collision, or from blinding of holes. Because such interactions increase as feedrate increases, the number of im pingements needed to achieve a specified efficiency must increase as feed rate increases. The difficulty, if not impossibili ty, of modeling the effects of reflection from the hole edges and particle-to-particle interactions for the complex mixture of sizes and shapes of the materials that are processed in resource recovery facilities pre vents a priori modification of the equations to account for them. The calculation of the necessary number of impingements by means of Eq. (5-8) should, therefore, be viewed as a starting point to which correction factors, obtained empirically for different types of feed streams, may be applied in order to obtain more accurate estimates. At this point, the equations describe any screen ing action, whether in a trommel or other kind of screen. THE RIDING ANGLE The angle above the horizontal diameter at which a particle of mass m will fly from the sur face is a function of the angUlar velocity, w, and the radius of the trommel, R. Figure 1 a shows that as long as the particle remains on the surface, the centrifugal force, w2R m, is equal to the sum of the normal force, T, exerted by the surface and the normal component of the gravitational force, mg sin a. When T= 0, the particle will leave the sur face. The condition for this is w2R g THE DYNAMICS OF TROMMEL ACTION = sma • (9) The angul'ar velocity needed to reach the vertical, The rotational motion of the barrel and its in a = 1T/2 (90 de g.), is the critical angular velocity clination relative to the horizontal provide the above which the particle will ride on the surface means by which material fed to the trommel is without falling. Thus, sin a is the square of the made to impinge on the screen surface. The num fraction of the critical angular velocity for which ber of impingements a mass of particles experiences the particle will ride to angle a before leaving the during its residence in the trommel is a function of surface. the trommel dimensions, its rotational speed, and Actually, because the .barrel is inclined with re angle of inclination. spect to the horizontal, it is necessary to multiply In classical applications in minerals processing, the denominator of the left side of Eq. (9) by the trommels are rotated at angular velocities at which cosine of the inclination angle, �. Because � is seldom the material within them rides less than 1T/9 seldom more than 1T/36 (5 deg. ), however, cos� � 1 (20 deg.) above the horizontal diameter before fall and may be neglected. ing back and impinging on the material riding be low [14]. Observation of trommels used in resource THE FLIGHT TRAJECTORY recovery processing, however, indicates that they The point-by-point description of the actual are rotated at higher angUlar velocities so that ma trajectory is of little interest. What are needed are terial rides higher above the horizontal diameter. the relationship between the point of landing at the Then, when the component of the gravitational bottom of the barrel and the angle a, and the time force normal to the surface becomes equal to the interval, t, during which the particle is in flight. centrifugal force, the particle leaves the surface, For the case where the particle lands at the low rising at first because it still has vertical momentum, est point of the barrel, at the vertical diameter, the but then arcing and dropping to the bottom of the vertical distance from where the particl e leaves the barrel. * While there does not appear to be any surface to where it strikes the bottom of the barrel, documentation of the reasons for such a mode of as il lustrated in Fig. 1 b, is given by operation, it is evident that this causes break-up of gt2 - wRt cosa (10) (R + h) R (1 + sina) aggregated masses of particles, increases mixing, and helps prevent blinding of screen holes. In fact, if, as before, the small inclination of the barrel from "lifters" are incorporated in many resource recov the horizontal is neglected. From this ery processing trommels in order to enhance "flight" 112 2 2 wt = sina cos a + [sin a cos a + 2 sina (1 + sina)] of particles from the surface. The quantitative de (11) scription of the mechanism of trommel. action lead ing to design and scale-up criteria described below The first term on the right is the time to reach the is based on this mode of operation. Ufters, how apogee of the trajectory and the second is the time ever. are not considered_ to fall from the apogee to the bottom of the barrel. Having a horizontal velocity, wR sin a, the particle travels the horizontal distance R cos a during this The operation in minerals processing may be described as time. When R cos a is set equal to wRt sin a, the a "slumping mode" and in resource recovery as a "cascad ing mode." result, after simplification, is = * 364 =i mljl h '" I I '1"'-Trajectory R R o. I I b. I I I ;' -. Trajectory -WI( I "7 , I I I 8 c. lEGENDS FOR . FIGURES FLIGHT TRAJECTORIES IN A TROMMEl a. Forces Acting on a Particle Causing It to Ride on the Barrel to Angle Ck b. The Trajectory for Impingement at the Vertical Diam eter, 6 =0 c. The Trajectory for Impingement at Angle 6 from the Vertical FIG. 1 PARTICLE cos3 a = [sin' a cos' a + 2 sin a {1 + sina)pl2 sin a (12) wt=sinacosa+ [sin'acos'a + 2 sina(coso +sina) f2 (13) Equation (12) is transformed to Because of Eq. (9) and the fact that sin' a + cos2 a = 1, Eq. (12) may be solved for sin a, to yield cos3 eX + sin 0 = [sin' a cos2 a sin a = 0.5, or a =n/6 (30 deg.). 11' sin a (cos 0 + sin a)] sin a (14) + 2 There is no a priori reason that the particle must This has the solution land at the vertical diameter. It is simple to show that, if the particle is to land at an angle 0 from the sin 0 = -cos 3a; cos 0 = sin 3a; 0 = 3a - n/2 (15) vertical, as illustrated in Fig. lc, Eq. (11) becomes 365 TABLE 1 TROMMEL DESIGN PARAMETERS - f 3.141 0.758 2.42 0.5972 3.279 0.712 2.38 0.5630 3.340 0.677 2.31 sin a 0.08687T (15.6°) 0.6428 o n a - 0.5495 0.06877T (12.4 °) 3.355 0.663 2.27 0.5000 0.06057T (10.9°) 3.366 0.609 2.12 0.05287T (9.5°) 3.3l3 0.552 1.92 3.193 0.491 1.68 3.014 0.427 1.41 0.4488 0.1487T (26.7°) 0.3961 0.1297T (23.3°) 0.3421 The first three columns of Table 1 list values of 0: and sin 0: for several values of {j. Because the particle (in the event it does not pass through a hole) has a horizontal velocity, wR sin 0:, as well as a vertical velocity, given by the product of g and the radical term on the right side oJ Eq. (1 4), it impinges on the surface at an angle, 1/, whose cotangent is the ratio of the vertical to horizontal velocities. Thus, after simplification 112 1 os {j 2 ) + � cot 1/ = . (3 sin2 0: (16) sm 0: sm0: The angles 1/ are given in column 4 of Table 1 for the listed values of 0: and {j. The angles 1/ and {j are equal at 0.0711 7r (12.8 deg.) when 0: = 0.1 901T (34. 3 deg. ). That is, the particle impinges normal to the surface, and w2 R (17) = 0. 563 g I an angle (3, as shown in fig. 2, the particle has a horizontal component of velocity wR cos 0: sin (3. During the time the particle is in flight it moves a horizontal distance wRt cos 0: sin (3 and a distance parallel to the inclined axis wRt cos 0: tan (3, where t is given by Eq. (1 4) and tan (3 and sin (3 have been approximated by (3, since (3 is a small angle in practice. In addition, the particle advances along the barrel a distance eqUivalent to the product of total distance the particle falls vertically and sin (3. Neg lecting cos (3, as before, the particle advances a dis tance R(3 (cos 0: + cos {j). The total horizontal displacement per impinge ment is then n THE N UMBER OF IMPIN GEMENTS REALIZED • Q = R(3 (wt cos 0: + cos 0: + cos {j) (18) which may be written Q (3R = <I> = (wt cos 0: + cos 0: + cos {j) (1 9) Values of <I> corresponding to the values of {j and 0: given in columns 2 and 3 of Table 1, are listed in column 5 of Table 1 . * The length, L, of the trom mel needed to produce n impingements is Because the vertical velocity of a particle as it leaves the barrel surface is actually a velocity per pendicular to the barrel axis which is inclined at 366 THE FEEDRATE Equations wRt coso (9) and (20) do not completely de termine the design of a trommel. They provide only sinfJ two relationships, given the hole size, among the W� COSOI onll four design parameters w, R, L, and (3. In particular, they contain no dependence on feedrate. At a cross-section of the barrel near its entrance, material riding on the barrel in a layer of thickness b along the angular section (8 + rr/2 + a) occupies a FIG. 2 PARTICLE MOVEMENT ALONG THE INCLINED BARREL SHOWING VELOCITIES AND DISTANCES L = nQ = cross-sectional area bR (8 + rr/2 + a). Material in flight occupies a cross-sectional area equivalent to (20) cI>n(3R the material that rode on the barrel during the time During each revolution of the barrel, the particle of flight, t , or bRwt . The material is moving longi rests against the surface during the angular displace tudinally along the barrel at a velocity (w/2rr)Q/f ment (8 + rr/2 + a). During the time the particle is The product of the cross-sectional area occupied by in flight, the angular displacement of the barrel is the material and its velocity along the barrel near the wt. Thus, the barrel makes the fraction of a revo entrance is the volumetric feedrate. When multiplied by the density of the material in the layer, Pb *, this gives the mass feedrate,M After substitution from lution (21) Eqs. by where t is given by Eq. (13), per impingement of the particle on its surface. The reciprocal of [ is the 'It = (sina)1I2 (wt cosa + sina + cos 8) [, corresponding to the values of 8 and a given in columns 1 and 3, are listed in column 6 of Table 1. 7 of Table 1 for corresponding values of 8 and a. to the rotational frequency w/2rr. nlU� n[ [ R J g sin a Equation (23) provides another relationship among the variables if Pb is known and b is speci fied. Although allowing b to increase permits larger (22) feedrates at a fixed R, doing so may decrease effici It has been assumed in the derivation of these ency by allowing increased particle-to-particle inter equations that the center of mass of a particle action, hole blinding, etc. rides on the surface of the barrel at the radial dis tance, R, from the axis. The center of mass of a real particle of finite size must actually ride at a distan'ce smaller than R from the axis. Moreover, if material rides several particles thick on th� surface, the dis· is, of course, no way to account for the dynamics of each particle. As an approximation R, in the as 8 decreases. The gain from larger 8, however, may be offset by the lower efficiency caused by the mately averages about which the real values may resulting departure from normal impingement when be expected to scatter. O. 0> 0.0711 rr (12.8 deg.). Experimental investiga- Horizontal trommels are used but or internal scrolls forming an Archimedes * screw to "pump" the material through. Obviously, Eq. (18) 8 decreases for a given R and (3. Alternatively, larger radius is needed at rlXed (3 at a given feedrate lated from the equations, will, then, be approxi = than the average dimension of the feed material Because 'It decreases as 8 decreases, M decreases riding on the barrel surface. The quantities calcu f3 not evident, a priori, that magnitudes of b greater as less one-half the average thickness of the material A special case is mine the depth of material, b, that produces the lead to more optimal designs. equations, may be taken to be the trommel radius with lifters It is necessary to resort to experimental observa tion on different types of feed materials to deter greatest observed efficiency at the smallest R. It is tances will be different for different particles. There * (24) (3 because (3 is small. Values of 'It are listed in' column mel is the ratio of the number of revolutions, nt, = 2rrn[ = ( w/2rr) (23) with t given by Eq. (13), and with sin (3 replaced by The residence time, T, of a particle in the trom T (20) and Simplification, M is expressed where number of impingements per revolution. Values of 1I2 (9) and does not hold in such cases. Presumably other rela Possibly Pb equals the bulk density of the feed, measured in the usual way. Howaver, this is not certain and Pb will have to be measured experimentally by observation of the feed ena of the rotating trommel. tions can b e developed to describe the movement. 367 tion is needed to ascertain the best values of {) to be used with different types of feed materials. It is reasonable, in the meantime, to specify normal im pingement, with {) = 0.071 rr (12.8 deg.) and Q = 0.190 rr (34.3 deg.). TO DESIGN A TROMMEL The purpose of a trommel is to separate under sized material in the size range Xo .;; x .;; xm with an efficiency E(xo, xm) from material fed to the trommel at a mass rate,M In order to design a . trommel to do so, it is necessary to specify the hole shape and size, the fractional area of holes, the rotational speed, radius,length, and angle of in clination. Common practice in resource recovery processing specifies circular holes (in order to minimize re.ten tion of textile and plastic material) and an angle of inclination of rr/36 (5 deg.). The hole size is deter mined by the dimension xm. The fractional area of holes should be as close to unity as possible con sistent with the structural strength of the barrel. Its speCification is a function of structural design and is not considered further here. Otherwise, the de sign is determined by Eq. (8) with Eqs. (7) and (5) or (6), Eqs. (9), (20), and (23). Equation (8), with Eqs. (7) and (5) or (6), allows calculation of the number of impingements neces sary to attain the required efficiency. Equations (9), (20), and (23), with sin Q = 0.5630, <I> = 3.34, and '11 = 2.31 then determine w, R, and L for the design feedrate and necessary number of impinge ments. This requires knowledge of the density Pb and specification of the depth of material,b,riding the trommel barrel surface. Until the results of ex periment and practice indicate otherwise, b may be taken equivalent to the mean size of the feed ma terial. N UMBER O F IMPINGEMENTS REQUIRED RAWMSW Raw MSW is most often characterized according to mass of material in different size ranges. Winkler and Wilson. [15] , however, have given number histo grams for raw MSW from Cambridge, Massachusetts, and Middlebury, Vermont, in different maximum particle dimension ranges. While distribution accord ing to maximum dimension does not account for particle shape, the distribution functions derived from the histograms can be used at least for illus trative purposes. The histograms for MSW from both cities may be fit by the log-normal distribution f (x) = 1 ...[2irri X 0 ln 2 (25) ..j2oln The geometric mean size Xg = 6.0 in. (152 mm) and the standard deviation 0ln = 0.56 for Cambridge, Massachusetts, MSW. The number fraction of minus 4.75 in. (120 mm) material in MSW from that city is given when Eq. (25) is inserted into Eq. (7). 2 4.75 F(O, 4.75) = 0.713 � exp o - 1.26 Qn dx 6.�0 (26) The probabilities, given by either Eq. (5) or (6), add Eq. (1), with the insertion of Eq. (25), are 4.75 P(O, 4.75) = 0.713 o 1 - 1 - 1 exp x - 2 x 1.26 Qn 6.00 x Q I+ 4.75 2 n (27) dx 4.7S P(0, 4.75 = 0.713 o APPLICATION x 1 -exp - 1.26 Qn 6.00 x x 1-1-Q 1+ 4.75 As examples of how the ideas developed may be applied in resource recovery processing, Eqs. (5-8) will be used to ascertain the number of impinge ments needed to separate undersized material from raw MSW through 4.75 in. (120 mm) round holes, and the number of impingements needed to separate metal cans from a solid waste stream through holes of the same size. Then Eqs. (9), (20), and (23) will be used to illustrate the calculation of rotational speed, radius, and length, for a typical feedrate. exp - X , QnXg 2 -n 2 (28) dx Integration of Eqs. (27) or (28) with different values of n gives P(O, 4.75) as a function of n. Division by F (O, 4.75) gives the efficiency of separation,E (0, 4.75), as a function of n. The integrals have been solved numerically by means of Simpson's approximation method. Fig ure 3, where n has been plotted as a function of Eon a log-normal grid,illustrates the results. Curves 368 A, B, and C show n as a function of E (0, 4.75), determined for the probability calculated from Eq. (27) with Q = 1 ,0.5, and 0.3 respectively. Curve D shows n as a function of E(O, 4.75) for the probability calculated from Eq. (28) with Q = 0.5. The most striking feature of the curves is that they each consist of two straight lines of different slope that are connected by a transition curve. In this regard, they are similar to experimentally de termined curves of efficiency as a function of siev ing time on flat screens described by Whitby [16] . The number of impingements necessary to achieve a given efficiency is approximately inversely pro portional to Q, as a comparison of curves A, B, and C show. The number of impingements at a given efficiency for probabilities calculated from Eq. (28) are slightly lower than those for probabilities calcu lated from Eq. (27) along the lower parts of the curves, but differ negligibly along the upper parts of the curves, as curves B and D illustrate. If the upper integration limits of Eqs. (26) and (27) or (28) are decreased, the integrations give the probabilities of separating < 4.75 in. (1 20 mm) material in a trommel with 4.75 in. (1 20 mm) holes. Curve E of Fig. (3) is a plot of n against E (0, 4.5) with Q = 0.75, while Curve F is a plot of n against E (0, 4.25) with Q= 1 .' Remarkably, the efficiency is log-normally distributed with respect to number of impingements up to very high separation effici encies. Moreover, the number of impingements needed to achieve a given efficiency is very much smalle�, especially at high efficiencies, than when undersized material up to the hole size is to be' separated. N UMBER OF IMPINGEMENTS REQUIRED 100 U) ... z '" :::E '" to Z Cl. :::E 10 0.1 'l'o 80 9095 99 EFFICIENCY FIG. 3 NUMBER OF IMPINGEMENTS NECESSARY TO ACHIEVE SPECIFIED EFFICIENCIES FOR REMOVAL OF UNDERSIZE MATERIAL RAW MSW IN A TROM· MEL W ITH 4.75 IN. (120 MM) HOLES A, B, C. Removal of Minus 4.75 in. (Minus 120 mm) Material, with Probabilities Calculated According to Eq. (27). for Q = 1,0.5, and 0.3 Respectively D. Removal of Minus 4.75 in. (Minus 120 mm) Material, with Probabilities Calculated According to Eq. (28) for Q 0. 5 = E. Removal of Minus 4.5 in. (Minus 114 mm) Material, with Probabilities Calculated According to Eq. (27) for Q = 0.75 F. Removal of Minus 4.25 in. (Minus 108 mm) Material, with Probabilities Calculated According to Eq. (27) for Q = 1 in. (1 20 mm). The distribution has the form CANS If recovery of food and beverage cans is an ob jective, a trommel may be an effective means of separating them from raw MSW. If interference by other materials is ignored emphasis may be placed on efficiency of separation of cans if the equations are written for distributions relative to cans alone. For simplicity, only undamaged cans of one size will be considered, 2.5 x 4 in. (64 x 1 02 rom ). The probability of passage of a can through a hole is dependent upon the orientation at which it impinges. All orientations occur with equal proba bility, however. Therefore, the cans present them selves as particles uniformly distributed with re spect to a longest dimension that ranges between that of its diameter and that of its diagonal, 4.75 10 20 40 60 1.0 x [( ) = 1 -== 0.444 (29) = 4.75 _ 2.5 -x-m -x-o � The number fraction F (2.5,4.75) is easily shown to be unity. The probabilities are either 4.75 P (2.5, 4.75)= 0.444 or P(2.5,4.75)= 0.444 2.5 1 -1-Q 1 - X n 4.75 4.75 2.5 2 1 - 1 - Q 1+ � 4 5 2 -n dx dx (31 ) Here, the efficiencies, E (2.5, 4.75), are equal num erically to the probabilities. Figure 4 illustrates the results of numerical in tegration of Eqs. (30) and (31 ). The curves are 369 is taken to be 5 Ib/ft3 (80 kg/m3), Eq. (23) with 'It = 2.31 and {3 = 1T/36 (5 deg.), gives R = 5.1 ft (1.5 m). The reqUired rotation speed is 18 rev/min, according to Eq. (9) with sin a: = 0.563.· If 70 percent efficiency of removal of minus 4.75 in. (minus 120 mm) material by a trommel with Q = 0.5 is specified, curve B of Fig. (3) shows that n = 63. Then, Eq. (20) with <I> = 3.34, gives L = 94 ft (28.5 m). If Q were 0.75, interpolation between curves A and B of Fig. 3 would give n = 45 for which the length would be 67 ft (20.4m). Even smaller lengths would be specified if removal of minus 4.5 in. (minus 114 mm) material through 4.75 in. (120 mm) holes were required. Thus, for 70 percent of efficiency of removal of such material by a trommel with Q = 0.75 curve E of Fig. 3 shows that n = 30, for which L = 45 ft (13.7 m). Curve A of Fig. 4 shows that for Q = 0.5 and n = 63 the efficiency of removal of cans is 67 per cent, while interpolation between curves A and B of that figure shows that for Q = 0.75 and n = 30 the efficiency of removal of cans is about 60 per cent. similar to those of Fig. (3). Curves A, B. C are for probabilities calculated according to Eq. (30 for Q = 1,0.5,0.3 respectively. The curve for proba bility calculated according to Eq. (31) for Q = 0.5 is undistinguishable from curve B. 100 (/) fZ '" ::E '" (!) z - 11. ::E - 10 0.1 1.0 10 20 40 60 80 9095 99 WHAT HAS B E EN ACCOMPLISHED % EFFICIENCY WHAT NEEDS TO BE DONE FIG. 4 NUMBER OF IMPINGEMENTS NECESSARY T O The development presented provides means for ACHIEVE SPECIFIED EFFICIENCIES FOR REMOVAL calculating: OF 2.5 X 4 IN. (64 X 1 00 MM) CANS FROM RAW MSW a. The number of impingements necessary to IN A TROMMEL separate undersized material from the feed to the A, B. C. Removal with Probabilities Calculated According to Eq. (30), Through 4.75 in. (1 20 mm) Holes, for Q = 1 , trommel, in any size range up to the hole diameter, 0.5, and 0.3 Respectively as a function of separation efficiency. The latter is D. Removal with Probabilities Calculated According to defined as the ratio of the fraction of undersized Eq. (30) through 5 in. (1 27 mm) Holes for Q 1 particles separated to that in the feed. In order to calculate the fraction it is necessary to know the Curve 0 illustrates how the number of impinge ments needed for a prescribed efficiency is marked distribution of particle size according to number in ly decreased when holes larger than the can diagonal the feed. There is little to distinguish between the are used. It was calculated for 5 in. (127 mm) holes two methods of calculating probabilities of passage through the holes. from the probabilities of Eq. (30) for Q = 1 with b. The radius of the trommel necessary to pro the term (1 - 1/4.75) replaced by (1 - 1/5.00) in cess material at a specified feedrate, if the thickness the integral. Thus, a small increase in hole size re and density of the material riding the barrel surface duces the number of impingements necessary to attain any efficiency, especially at high efficiencies. are known and the angle of inclination is specified. c. The length of the trommel needed to achieve The efficiency is log-normally distributed with re the number of impingements calculated. spect to number of impingements up to 0.99. This provides the complete design for specific applications e�cept for structural factors. There TROMMEl DESIGN are, however, lacks in information about materials If, for example, the trommel is to process 60 tons/hr (55 t/h) of raw MSW and if an average den At this value of a, Ii = 11 or the particles impinge normal sity for material riding the barrel surface at a depth t o the screen surface which is the maximum size hal .. , equal to the geometric mean size, 6 in. (152 mm), hence most probable and average value for d. = * 370 in resource recovery processing that introduce un certainty: a. Size distributions of raw MSW and of other process streams have usually been reported accord ing to weight fraction, but not according to num ber fraction. b. Shape factors for the irregularly shaped ma terials fed to trommels in resource recovery pro cessing are not known. c. Densities of the materials that ride on the barrel surface have not been reported. In addition, several important parameters in �e derived design equations are imperfectly specified: a. Because particle shape factors are unknown, reflection from the hole edges has been omitted from the derivation of efficiencies. b. While normal impingement has been suggested for use in design, optimal efficiency may occur at other impingement angles. c. The thickness of the material layer riding the barrel surface that leads to the optimal design for a given effici�ncy of separation and feedrate may not be equivalent to a mean dimension of the feed ma terial. There is need for better characterization of feed materials with respect to size distribution according to number and to shape factor, and for experimen tal programs in which optimal impingement angles and thicknesses of materials riding the surface are investigated for different feed materials. It is hoped that the results presented here are suffiCiently pro vocative to inspire needed investigation. They are but a first step toward a rational method for the design of trommels for size separation in resource recovery processmg. • ACKNOWLEDGMENTS The beginnings of this work were encouraged by support from Contract 68-03-2632 from the U.S. Environmental Protection Agency, Office of Re search and Development, Mr. Carlton Wiles, Project Officer. The work was supported, in part, through Indus- trial Research Participation Grant SPI-7907391 from the National Science Foundation. REFERENCES Anon., "A W estminster W onder," My Magazine (July 1 924), reprinted, Solid Wastes, Vol. 66, 1976, pp. 536-539. [1] [2] Anon., "The Govan Refuse Plant," Engineering, Vol. 126, 1928, pp. 577, 641, 710. [3] Carlson, D., Spencer, D., and Christensen, H., "Monroe County Resource Recovery Project," Proc. Fifth Mineral Waste Utilization Symp., 1976, pp. 196-203. [4] Funk, H. D. and Russell, S. H., "Energy and Ma terials Recovery System," Proc. F ifth Mineral Waste Utilization Symp., 1 976, pp. 133-140. 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