Abstract
A flotation separation apparatus for separating particles in suspensions, feeds slurry containing the particles through an inlet into a contactor where gas is fed through an inlet to mix with the slurry, for example in a downwardly plunging jet, to form a gas-liquid bubbly two-phase mixture under pressure from an outlet restriction in a throttling duct. The mixture is passed through a flow manipulator configured to induce a high energy dissipation rate, for example by way of a Shockwave formed in a diverging section of the throttling duct reducing the size of the bubbles and brining those bubbles into intimate contact with particles in the mixture which is released into a separation cell where a flow manipulating draft tube is provided to reduce turbulence in the mixture. Alternative apparatus and methods for inducing the high energy dissipation rate and for reducing turbulence in the mixture are also described and claimed.
Claims
1. Apparatus for contacting bubbles and particles in a flotation separation system, said apparatus comprising: a contactor arranged to receive under pressure a supply of feed slurry incorporating particles suspended in a liquid and a supply of gas, the contactor being arranged to mix the slurry with the gas forming a gas-liquid bubbly two-phase mixture; an outlet from the contactor configured to provide a restriction to the flow of mixture therethrough and maintain the mixture within the contactor under pressure, the outlet further being configured to induce a supersonic shockwave within the mixture passing therethrough, and configured such that when slurry and gas are fed into the contactor at feed rates and pressures determined to form said gas-liquid bubbly two-phase mixture and force the mixture through the outlet at a rate that induces said supersonic shockwave within the mixture reducing the size of the bubbles within the mixture and bringing those bubbles into intimate contact with particles in the mixture; and a separation cell including a mixture-directing device, the mixture-directing device arranged to receive mixture from the outlet and to control the release of that mixture into the separation cell, wherein the mixture impinges against adjacent surfaces of the mixture directing device to create a high shear environment for the mixture before allowing bubbles with attached particles to rise to the surface of liquid within the cell.
2. Apparatus as claimed in claim 1 wherein the contactor comprises a substantially vertical column arranged to receive the feed slurry under pressure into the top of the column.
3. Apparatus as claimed in claim 2 wherein the contactor incorporates mixing means comprising a nozzle arranged to form a downwardly plunging jet of feed slurry within the column, and a gas inlet in the vicinity of the jet so formed such that in use gas is entrained into the jet forming said gas-liquid bubbly two-phase mixture.
4. Apparatus as claimed in claim 2 wherein the outlet from the contactor is configured to form at least one throttling duct providing said restriction to the flow of mixture therethrough.
5. Apparatus as claimed in claim 4 wherein the throttling duct has a converging section leading to a throat sized to provide said restriction.
6. Apparatus for contacting bubbles and particles in a flotation separation system as claimed in claim 1, wherein the mixture from the outlet issues downwardly and the adjacent surfaces are formed by an impingement plate located substantially horizontally below the outlet.
7. Apparatus for contacting bubbles and particles in a flotation separation system as claimed in claim 6, wherein the impingement plate forms the lower end of a shroud encompassing at least the lower part of the contactor.
8. Apparatus for contacting bubbles and particles in a flotation separation system as claimed in claim 1, wherein the mixture from the outlet issues into a shroud located within the separation cell, and the adjacent surfaces comprised some of the internal surfaces of the shroud.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) FIG. 1 is a schematic side view of a flotation device showing a gas-liquid contactor, a flow restrictor and a riser pipe to direct the flow downstream of the restrictor according to the present invention;
(2) FIG. 2 is a schematic view of the flow restriction device shown in FIG. 1.
(3) FIG. 3 is a schematic side view of the apparatus shown in FIG. 1 using an alternative flow restriction device;
(4) FIG. 4 is a schematic side view of an alternative gas-liquid contactor and riser pipe according to the invention;
(5) FIG. 5(a) is an enlarged side view of the flow restriction shown in FIG. 3 and FIG. 4.
(6) FIG. 5(b) is an enlarged plan view in the plane A-A in FIG. 4 showing the disposition of the flow restrictions shown in FIG. 4 and FIG. 5(a);
(7) FIG. 6(a) is an enlarged side view of an alternative restriction at the exit from the gas-liquid contactor and directing the discharge from the restriction in the radial direction;
(8) FIG. 6(b) is an enlarged plan view of the restriction and radial flow device shown in FIG. 6(a);
(9) FIG. 7 is an enlarged schematic side view of the restriction and alternative radial flow device shown in FIG. 6(a);
(10) FIG. 8 shows a schematic side view of an alternative flow restrictor and apparatus to direct the downstream flow in a radial and then a vertically-upwards direction;
(11) FIG. 9 shows an alternative gas-liquid contactor, pressure reducing restrictor and flow distribution means;
(12) FIG. 10 shows a further alternative gas-liquid contactor and pressure-reducing means and conduit to direct the resulting gas-liquid mixture to the froth layer in a flotation column.
(13) FIG. 11 shows the recovery of particles of various sizes subjected to flotation in a device according to the invention.
DETAILED DESCRIPTION
(14) A first preferred embodiment of an intensive flotation column flotation cell according to the invention is shown in FIG. 1. The liquid feed containing the particles to be separated by flotation is prepared or conditioned with appropriate collectors and frother reagents prior to entry to the column, so that the values are hydrophobic and will be able to form strong bonds with bubbles. The feed to the column enters at the inlet 10 and flows through the pre-mixing device 11 where it mixes with air which enters at 12. In this embodiment the gas is premixed with the liquid in a plunging jet apparatus prior to introduction to a pressure reducing means. The feed liquid enters a converging section 13 forming a nozzle in which the liquid is accelerated to form a plunging jet 14 of relatively high velocity. A pressurised gas stream enters through the side arm 15, and is entrained into the high speed jet 14 to form a gas-liquid mixture in which the bubbles are typically less than 0.5 nm n in diameter, in a conduit 16. The bubbly two-phase flow travels vertically downwards to the bend 17 where it changes direction, and enters a throttling duct 18 which has the form of a converging-diverging channel. Preferably the velocity of the gas-liquid mixture in the throat of the converging-diverging channel exceeds the speed of sound, when the flow is said to be choked. The flow becomes choked when the ratio of the absolute pressure upstream of the throat to the absolute pressure downstream of the throat exceeds a critical value. When the pressure ratio is above the critical value, the flow downstream of the throat becomes supersonic, and a shock wave forms in the diverging section, which involves a large pressure rise over a very small physical distance, of the order of 3 to 5 mm. The small bubbles in the gas-liquid mixture are rendered even smaller by being forced through the shock wave, where they are brought into intimate contact with the hydrophobic particles in the suspension to form bubble-particle aggregates. The emulsion of fine bubbles and adhering particles then passes through the connecting conduit 19 to a shroud in the form of a draft tube or riser 20, before discharging into the flotation tank or column 21. The column contains liquid whose upper surface 22 is maintained at a particular level by means not shown. The bubbles disengage from the liquid and rise through the froth-liquid interface 22, carrying the hydrophobic particles into the froth 23, which discharges over a lip 24 into a launder 25 and thence out of flotation vessel through an exit conduit 26. The liquid flows downwards to the base of the cell 21, and leaves through the exit pipe 27, and a valve 28 that is used to control the level of liquid in the cell.
(15) Because the density of the gas-liquid mixture leaving the restrictive throat 18 is less than that of the contents of the column 21, which is essentially that of gas-free liquid, an upwards convective flow is established through the draft tube 20. Liquid from the column is drawn into the base of the draft tube and is brought into contact with bubbles that have been generated in the plunging jet contactor 16 and the choked flow device 18 in combination. Thus a proportion of the particles that may not have made contact with bubbles when first entering the vessel through the contacting system, or which may have detached from the froth layer 23 and fallen back into the liquid in the flotation vessel 21, will have an additional opportunity to become attached to bubbles and be carried by them into the froth layer. It has been found that if the draft tube 20 is open-ended at its upper and lower extremities, the ratio of the flowrate of recirculating liquid to that of the incoming feed liquid, which is termed the internal recycle ratio, is quite large, of order 4 to 6. Such flowrates give rise to highly energetic flows within the cell 21, and a buoyant plume rises from the upper open end of the draft tube 21 whose velocity is so high that it can be disruptive to the froth layer and lead to an increase in drop-back of particles from the froth. Accordingly it has been found to be advantageous to incorporate an entry tube 29, which restricts the internal recycle ratio to a value preferably between 2 and 3. The height/diameter ratio of the draft tube 20 and the inlet pipe 29 are each preferably in the range 2 to 5. The centreline of the horizontal conduit 19 should intersect with the axis of the draft tube 20 at a height approximately equal to 1.5 times the diameter of the conduit 19 above the lowest extremity of the said draft tube.
(16) In this embodiment preferably the plunging jet contactor is mounted so that the jet is directed vertically downwards. The cross-sectional area of the plunging jet contactor 16 in a plane normal to the axis should be such that the downward superficial velocity of the liquid is above the terminal velocity of the largest bubbles that are likely to form in the contactor, and it has been found that an appropriate velocity is in the range 0.3 to 1 m/s. It is convenient to make the cross-sectional area of the inlet and outlet of the converging-diverging throttle 18 and the transfer conduit 19, to be the same as that of the contactor 16. The cross-sectional area of the draft tube 20 should be not less than that of the contactor 16, and should preferably in the range 2 to 4 times said area. The area of the entry pipe 29 should be in the range 0.1 to 0.5 of the cross-sectional area of the draft tube 20.
(17) The area of the throat is chosen with advantage so that the gas-liquid mixture formed in the contactor 16 attains the speed of sound there. If the sonic velocity is exceeded, a shockwave forms downstream of the throat, which has an effect on the size of the bubbles in the flow. FIG. 2 shows a shock wave bubble generator according to the present invention in greater detail. In FIG. 2, the device 18 comprises a conduit 31, a converging section 32, a throat 33 in which the walls are essentially parallel, a relatively slowly diverging section 34 and a delivery conduit 19, the walls of which may conveniently be parallel. A gas-liquid mixture, preferably well-mixed so that the bubbles are already finely divided, enters the entry conduit 31. Preferably the velocity of the gas-liquid mixture in the region upstream of the throat is sub-sonic; the velocity of the gas-liquid mixture in the throat 33 reaches the speed of sound in the mixture at that point; a region of flow exists downstream of the throat 33 in which the gas-liquid mixture accelerates and reaches supersonic velocities; a shock wave 35 is produced in the slowly-diverging section 34; the flow reverts to a subsonic condition in the region immediately downstream of the shock wave and the velocity of the gas-liquid mixture is further reduced in the diverging region downstream of the shock wave. The mixture leaves the device at a convenient subsonic final velocity at the exit 36 to the conduit.
(18) The way in which small bubbles are produced in the apparatus described can be explained with reference to the changes in the pressure in the two-phase mixture. In the entry region 31 the pressure is constant in the gas and liquid phases, and is denoted the upstream pressure. When the mixture accelerates in the converging region 32, the pressure reduces according to well-known laws of fluid flow, so the bubbles in the mixture become larger. In the throat 33, at a critical value of the upstream pressure, the gas-liquid mixture reaches the speed of sound in the mixture. If the upstream pressure is sufficiently large, the fluid continues to accelerate downstream of the throat 33, and the pressure continues to fall, so that the bubbles continue to increase in volume. At a certain point in the diverging region, a shock wave 35 occurs, across which there is a catastrophic change in the flow, and the pressure rises from a small value ahead of the shock to a large value downstream. Because of the rapid pressure change, the large bubbles ahead of the shock break up in a violent fashion, to form very small bubbles, typically less than half the size of the bubbles in the flow in the entrance duct 31. It has been found that the thickness of the shock wave in the flow direction is relatively small, being in the range 3 to 5 mm typically. It will be appreciated that a purpose of this invention to bring about contact between hydrophobic particles and small bubbles. The chaotic motions that occur within the shock wave have the effect not only of breaking up the bubbles, but also of freshly creating a very large interfacial gas-liquid area in a high-energy, intensively-mixed zone within the shock wave and downstream of it. The combination of very small bubbles and high-energy mixing has the effect of bringing about instant contact between the bubbles and the hydrophobic particles.
(19) The cross-sectional area to achieve a sonic velocity in the throat shown in FIG. 2, can be calculated from an equation that has been experimentally verified (Sandhu, N., Jameson, G. J. An experimental study of choked foam flows in a converging-diverging nozzle, International Journal of Multiphase Flow (1979), 5, 39). The equation is presented here in the form:
(20)
(21) where P.sub.0 is the pressure in the conduit 31 upstream of the throat; .sub.t is the gas/liquid volume ratio in the throat 33; and .sub.3, P.sub.3 are respectively the gas/liquid volume ratio and the pressure in the discharge conduit 19. (All pressures are in units of Pascals absolute). The gas/liquid ratio in the throat .sub.t can be represented as the dimensionless liquid flowrate:
(22)
(23) where Q.sub.L is the volumetric flowrate of liquid (m.sup.3/s); .sub.L is the density of the liquid (kg/m.sup.3) and A.sub.t is the flow area in the throat 33 (m.sup.2). Thus if the downstream conditions, i.e. the pressure and the gas/liquid volume ratio in the aerated mixture entering the flotation cell, are known, it is possible to solve equation 1 to find the critical value of the upstream pressure P.sub.0 for the velocity in the throat 33 to reach the speed of sound and hence for the flow to be choked. Any increase in pressure above the critical value will lead to the formation of a shock wave downstream of the throat.
(24) It is not possible to find analytic solutions to Equation 1. However, it has been found that the following equation, which can be solved easily, is an excellent representation of Equation 1 for values of the dimensionless liquid flowrate (1/.sub.t) less than 2.5:
(25)
(26) The rate of capture of particles by flotation can be enhanced by increasing the shear rate, or rate of dissipation of energy, in the vicinity of the particles and the bubbles. The shear rate is proportional to the square root of the rate of energy dissipation. In the embodiment shown in FIG. 1, the energy dissipation rate downstream of the throat 33 is high because much of the energy stored in the pressurised feed and gas entering the throat is dissipated in the shockwave 35, which is typically 3 to 5 mm in thickness. It can be calculated for example that the energy release rate in the shockwave is of the order of 20,000 kW/cubic meter of shockwave. For particle-bubble contacting purposes however it can be advantageous to release the same amount of energy into a larger volume of liquid as in the embodiment shown in FIG. 3, which provides a longer time for the particles and bubbles to come into contact. In conventional mechanical flotation machines, the energy dissipation rate is generally in the range 2 to 3 kW of power per cubic meter of liquid in the flotation cell. Contact between bubbles and particles takes place in the volume enclosed by the impeller and stator in the cell, which is typically of the order of 5 to 10 percent of the volume of the cell. Accordingly the effective dissipation rate in mechanical cells is of the order of 50 kW per cubic meter of active volume. In flotation columns, the energy dissipation rate is much less. It is an aim of the present invention to provide an active contacting environment downstream of the flow restriction in which the energy dissipation rate is at least as high as found in mechanical flotation cells. In the embodiment shown in FIG. 3, the dissipation rate in the volume immediately downstream of the throat 33 is of the order of 100 to 150 kW/m3.
(27) The embodiment shown in FIG. 1 has the advantage that, through the use of the divergent diffuser downstream of the throat, the maximum amount of mechanical energy in the feed to the choke can be recovered, which can be an important consideration when running costs are important. However, in some cases, energy costs are outweighed by other factors, especially where it is possible to increase the recovery of valuable particles. A further embodiment is shown in FIG. 3, in which energy recovery is reduced but where the mechanical energy that is lost is used to improve the contacting between the incoming feed liquid and the liquid in the flotation column. The slowly-diverging diffuser 34 is dispensed with. The mixture of gas bubbles from the aerating contactor 11 enters through the conduit 31, and accelerates in the converging channel 32 to a throat 33 which discharges directly into a duct 19; there is no slowly-diverging diffuser 34. The short form of the constriction is denoted 37. The critical pressure for the attainment of sonic flow in the throat is predicted by equations (1) and (3) as before. If the critical pressure is exceeded, shockwaves are formed downstream of the throat, but they are not necessarily bounded by a solid wall. The flow issuing from the throat takes the form of a gas-liquid wall jet with considerable velocity, of the order of 20 m/s. The throat discharges directly into the conduit 19, in the walls of which openings 41 have been formed, through which liquid is entrained from the flotation column 21. Particles that may have escaped capture in the first pass of the feed liquid into the combined aerating contactor 11 and the restricting throat 33, have an additional opportunity to be captured by bubbles freshly entering the column through the throat 33. This embodiment is particularly favourable for the capture of ultrafine particles, because of the creation of a high-shear environment with a high gas/liquid ratio, in the mixing zone downstream of the jet issuing from the throat 33. One or more openings 41 should be provided. The openings are conveniently located equi-spaced around the circumference of the conduit 19, at a position downstream of the throat equal to 0.5 to 2 times the throat diameter. The total flow area of the openings 41 should be approximately equal to the cross-sectional area of the conduit 19.
(28) In all the embodiments disclosed here, the throat length should preferably be in the range 0 to 3 times the throat diameter.
(29) An advantage of using the converging-diverging nozzle shown in FIG. 2 and the truncated form shown in FIG. 3, is that high ratios of gas to feed liquid can be dispersed into small bubbles in such devices, especially when operated in choked conditions where shockwaves form downstream of the nozzle. In the case of a nozzle discharging into a flotation cell at essentially atmospheric pressure, for gas:liquid ratios of 0.5 to 4 at the same pressure, the pressure upstream of the choke is typically 1.7 to 4 times the downstream pressure, implying that the gas:liquid ratio within the contactor 16 is in the range 0.58 to 0.25. The gas:liquid ratio has a strong effect on bubble generation and generally, finer bubbles can be formed when the volume ratio of gas to liquid is small, because of the reduction in the rate of coalescence of bubbles subsequent to formation. High gas:liquid ratio dispersions of bubbles in the flotation slurry are highly desirable, because they lead to high values of the specific surface area of bubbles, which leads in turn to higher carrying capacity or production from the flotation device as a whole. Accordingly, in the embodiments described, it is convenient to operate with gas:liquid ratios in the flotation column between 0.5 and 4.
(30) A further embodiment is shown in FIG. 4, in which the gas-liquid contactor 16 is mounted by means not shown essentially co-axially with the flotation column 21. Suitably conditioned feed liquid is introduced through the inlet pipe at 10 which has a converging section 11 in which the liquid is accelerated to form a plunging jet 14 of relatively high velocity. A gas stream under pressure enters through a side arm 15, and is entrained into the high speed jet 14 to form a gas-liquid mixture in the contactor 16 in which the bubbles are substantially less than 1 mm in diameter. The bubbly mixture travels downwards to the lower end of the downcomer, where it passes into a discharge nozzle 37 shown in more detail in FIGS. 5(a) and 5(b). Each exit nozzle 37 communicates with the liquid inside a flotation column 21. The liquid flows downwards to the base of the cell 21, and leaves through the exit pipe 27, and a valve 28 that is used to control the level of liquid in the cell. The upper lip 24 of the vessel 21 forms an overflow weir for froth 23 which is collected in a launder 25 and is drained away through an outlet 26.
(31) In operation, the contactor 16 is filled with a dense foam that travels downwards to discharge through one or more discharge nozzles 37. The bubbles in the mixture discharged from the contactor mix with the liquid in the containing vessel 21 and disengage from it, rising to the top of the vessel to form the froth layer 23. The level of liquid in the outer vessel or container is maintained by the valve 28 or other means, at a level 22. Air is introduced through the entry port 12, at a pressure and flowrate so that the downcomer 16 fills with a dense foam that is agitated by the entering jet of liquid 14, that carries the particulate material to be collected by the bubbles. The turbulent mixing created by the kinetic energy in the plunging jet is a highly favourable environment for the capture of particles by the bubbles in the dense foam. Because of the violent and turbulent nature of the plunging jet the particles in the feed liquid are brought into intimate contact with the bubbles, thus providing a favourable environment for the collection of the hydrophobic particles by the bubbles. Because of the flow restriction brought about by the discharge nozzle 37, the pressure in the downcomer 16 is well above the ambient pressure in the containing vessel 21 at the discharge end of the nozzle 37. The small bubbles in the gas-liquid mixture are rendered even smaller by being forced through the nozzle, where they are brought into further intimate contact with the hydrophobic particles in the suspension to form bubble-particle aggregates. The pressure of the liquid feed and the air supply are such as to be able to maintain the flow of gas and liquid through the discharge nozzles 37.
(32) The gas-liquid mixture that discharges from the shortened nozzle 37, which consists only of the converging section 37 and the parallel-walled throat 33, does so at a considerable velocity, and the momentum in the flow can be utilised further, to increase the overall efficiency of the flotation system. Thus it has been found advantageous to incorporate an internal draft tube 20, which surrounds the lower end of the contactor 16. Because the average density of the gas-liquid mixture being discharged into the draft tube is lower than the density of the liquid in the vessel 21, it tends to rise in the vertical direction, and a circulating pattern is created. Liquid from the vessel is drawn into the entry tube 29 which would otherwise be passing directly out of the tailings exit pipe 28, so the incorporation of the draft tube leads to the further exposure of the particles in the recirculated liquid to the bubbles discharging from the nozzle(s) 37, thereby leading to further opportunities for capturing some particles that would otherwise pass out of the vessel
(33) In relation to the embodiment shown in FIG. 4, FIG. 5(a) shows an elevation view of a discharge nozzle 37, and FIG. 5(b) shows a plan view of an embodiment comprising three nozzles 37 equi-spaced around the periphery of the contactor 16. It will be appreciated that one or more nozzles could be used, in which case the total flow area of the throats 33 of the individual nozzles should be used in the calculation of the upstream pressure P.sub.0 in the contactor 16.
(34) FIG. 6(a) shows an alternative embodiment of the pressure restriction and dispersion means for use at the termination of the initial contactor 16. A mixture of gas bubbles and liquid slurry formed in the contactor enters a converging conduit 32 of a truncated choke 37 and passes to a throat 33 from which it leaves through a radial diffuser in the space between an upper circular disc 43 and a lower circular disc 44. The discs 43, 44 that define the radial passageway of the disperser are substantially horizontal.
(35) In the embodiment shown in FIG. 6(a), the two circular discs 43,44 may be held at a fixed distance apart, so that the flow passage between them is of constant vertical height. In this case, the velocity between the discs decreases continuously with increasing radial distance from the axis. If the velocity is sufficiently high, sonic flow conditions will exist in or downstream of the throat 33. Surprisingly, it has been found advantageous to mount the lower disc so that it is free to move in the vertical direction. Because of the changes in velocity within the space between the discs, the pressure in said space is substantially less than the pressure at the end of the radial channel, and hence, is less than the pressure in the liquid external to the radial disperser. A large force is thus induced that tends to push the two discs together. If the lower disc is free to move, it will come to a stable equilibrium at a certain distance from the upper disc. Observation suggests that in this case the speed of sound is reached in the gas-liquid mixture when it reaches the outermost region 46 of the radial passage between the discs.
(36) It is a property of the converging flow in the radial channel 45, that the suction induced in said channel decreases as the separation distance h increases. This observation gives a significant practical advantage to the case where the lower disc is free to move in the vertical direction, in that if the space between the discs becomes blocked by a large particle, the pressure in the radial channel 45 will increase and will force the lower disc 44 to move away from the upper disc 43, thereby releasing the large particle which is swept away in the flow.
(37) In another embodiment shown in FIG. 7, upper and lower discs 43 and 44 are provided that are flexible and compliant to the flow conditions. Thus they can adapt to a shape that is dictated by the pressure developed in the flow within the radial passage 45. It has been found that in such a case, the spacing between the two circular discs at the exit 46 can be very small, leading to high velocities in the gas-liquid stream leaving the periphery of the radial disperser. The small thickness of the gas-liquid mixture at the exit is conducive to the production of very small bubbles. In such an apparatus, one or both of the opposing discs can be flexible. An impingement plate 47 is provided, to absorb the stagnation pressure of the impinging liquid jet emanating from the throat 33. It is preferred that both the converging nozzle 37 and the impingement plate 47 be of a wear-resistant substantially solid material. It is preferable for the impingement plate to be restrained by a means not shown, at a fixed distance from the throat 33, and on the same vertical axis. This embodiment is particularly useful in a feed stream containing coarse particles. Because of the flexible properties of the material used for either or both of the upper and lower discs, it is not necessary for a complete disc to move in order to release a particle that may have become lodged in the radial channel 45all that is required is for one of the discs to distort locally, in the region of the particle, for the latter to be released, thereby unblocking the channel.
(38) A further embodiment is shown in FIG. 8, which depicts a restrictive throat at the lower extremity of a first contacting device 16. The mixture of fine bubbles and slurry passes through the throat 33 under pressure, and strikes the impingement plate 54 at high velocity, spreading out in the radial direction. Because of the high momentum in the jet, liquid is entrained, and the jet expands as it travels radially outwards. The draft tube 20 restricts the outwards radial motion of the jet, and a toroidal vortex 55 is formed. The average rate of shear in the toroid is very high, and an environment that is very favourable to the break-up of bubbles and the contacting of bubbles and particles exists. Remarkably, it has been found that the gas fraction in the region surrounding the vortex can be maintained at values as high as 0.65, approaching the maximum packing fraction of spheres. The high gas fraction also leads to rapid contact of bubbles and hydrophobic particles, especially for larger particles, because the distance between bubbles is smaller than the size of the particles. Flotation efficiency is further improved by the buoyancy-induced flow created in the draft tube 20, which permits some of the liquid that has previously entered through the pressure restricting throat 33, which may contain particles that have dropped out of the froth, to be recycled.
(39) FIG. 9 shows a further embodiment in which the flotation device consists of a separation vessel 21 which can be conveniently cylindrical in form, with a conical bottom 59, a froth overflow lip 24 at the upper end of the cylindrical vessel, which is surrounded by a launder 25 fitted with an outlet 26 for the removal of froth product from the device. At the lower end of the separation vessel is a conduit 27 for the discharge of tailings under the control of a valve 28. The level of liquid in the vessel is maintained at a suitable level by means not shown. Liquid feed under pressure enters the separation apparatus through a nozzle 61. The feed is a suspension in water of particles to be treated by froth flotation, which have been suitably conditioned by reagents and frothers as appropriate. At the exit of the nozzle 61, the feed forms a liquid jet which enters a first chamber 62 and mixes with air that has been introduced under pressure through an entry pipe 15. Air is entrained through the turbulent mixing action of the jet, and is dispersed into small bubbles in the liquid, which travels downwards through the first chamber 62 to a second nozzle 64. In the second nozzle 64, the bubbly flow is forced under pressure to reach a velocity that is approximately equal to the speed of sound in the mixture. Under such conditions there are abrupt changes in pressure downstream of the nozzle exit 65, such that the bubbles in the flow are broken into smaller gas fragments. It is not essential that the sonic velocity of the mixture is reached in the nozzle 64; alternatively the conditions in the second nozzle are such as to provide a positive backpressure in the first chamber 62, and reliance is placed on the shearing action of the jet that issues from the second nozzle 65 to break up the bubbles within it as it mixes with the downstream fluid.
(40) The exit stream from the second nozzle enters a second chamber 66, which is fitted with appropriately-placed ports 67, through which fluid can be drawn, to dilute the liquid content in the jet emanating from the second nozzle 64. The combined flow of gas-liquid mixture from the nozzle 64, and recirculating flow through the entry ports 67, passes downwards through the second chamber 66, to discharge through the opening 68.
(41) Surrounding the second chamber 66 and co-axial with it is a draft tube 69 that is conveniently of conical shape. The combined flow leaving the second chamber 66 contains both gas and liquid, and accordingly is of lower mean density than the liquid in the flotation vessel 21, so it rises under gravity in the annular space between the chamber 66 and the draft tube 69, filling the said annular space with a bubbly mixture. Liquid from the lower part of the separation vessel 21 is drawn through the port 70 at the lower extremity of the draft tube 69.
(42) The two-phase gas-liquid mixture rising out of the open upper end 71 of the draft tube enters the upper part of the separation vessel 21, and the gas bubbles rise upwards and separate from the liquid to form a froth layer 23. The froth rises upwards and discharges over the lip 24 into the launder 25 and out of the vessel through the exit pipe 26. The tailings, from which the floatable material has substantially been removed, pass out through the pipe 27. This embodiment is particularly appropriate for the recovery of coarse particles, because the conical draft tube 69 can be of such dimensions and placed in such a way that distance between the top of the said draft tube and the froth-liquid interface 22 can be minimised. The tapered shape of the conical draft tube permits the upward velocity of the mixture of liquid and particle-laden bubbles to diminish with height generating a quiescent flow leaving the upper exit of the draft tube 69, thereby enhancing the probability of retention of coarse particles by the bubbles.
(43) A further embodiment is shown in FIG. 10 in which pressurised aerated slurry from a first chamber discharges into a second contacting chamber as a high-speed jet, of velocity typically in the range 10 to 20 m/s. The contents of the base of the second chamber are vigorously agitated by the energy in the jet providing an environment that is particularly favourable for further reducing the size of the bubbles and for capturing hydrophobic particles in the feed. The gas fraction in the lower parts of the second chamber may be as high as 0.5 to 0.6, values that are typical of a dense liquid foam, and particularly useful for capturing coarse particles. The height of the second chamber is such that when the gas-liquid mixture nears the top, the flow is relatively quiescent. The bubbles continue to rise into the froth layer, while the waste particles are carried out of the vessel. Particles that drop back from the froth fall directly into the second chamber under gravity where they have an additional opportunity to attach to fresh rising bubbles.
(44) In the embodiment shown in FIG. 10, liquid feed under pressure enters the separation apparatus through a nozzle 81. The feed is a suspension in water of particles to be treated by froth flotation, which have been suitably conditioned by reagents and frothers as appropriate. At the exit of the nozzle 81, the feed forms a liquid jet 14 which enters a first chamber 16 and mixes with air that has been introduced under pressure through an entry pipe 15. Air is entrained through the turbulent mixing action of the jet, and is dispersed into small bubbles in the liquid, which travels downwards through the first chamber 16 to a second nozzle 83, from which it issues under pressure through the throat 84. Bubbles that have been formed in the first chamber 16 are further reduced in size by the pressure changes as they pass through the nozzle 83, and by the high-shear environment downstream of the nozzle. The exit stream from the second nozzle enters a second chamber 85, which is conveniently cylindrical in shape, and of a diameter much larger than that of the first chamber 16. The high-speed gas-liquid jet that issues from the nozzle 83 is directed downwards against an impingement plate 86 that is constructed of a high-wear material, and is deflected so as to flow radially outwards to the conical base 87 of the second chamber. In the base of the second chamber, the gas-liquid mixture is highly agitated by the energy in the incoming jet, and forms a rapidly-rotating toroidal vortex 55, in which the size of the bubbles is reduced by the high-shear conditions, which are also favourable to high rates of contact between bubbles and particles in the liquid. As the mixture rises, the general level of turbulence reduces and the flow at the top of the second chamber 85 is relatively uniform.
(45) The two-phase gas-liquid mixture rising out of the open upper end 88 of the second chamber 85 enters the upper part of the separation vessel 21, and the gas bubbles rise upwards and separate from the liquid to form a froth layer 23. The froth rises upwards and discharges over the lip 24 into the launder 25 and out of the vessel through the exit pipe 26. The tailings, from which the floatable material has substantially been removed, pass out through the pipe 27.
(46) It is advantageous to be able to control the liquid velocity rising in the riser conduit that forms the second chamber 85, especially when the particles are so large that their terminal velocity is greater than the liquid vertical velocity in the riser. In the embodiments shown in FIGS. 8 and 9, it is difficult precisely to control the velocity in the draft tube, which is a function not only of the gas fraction in the feed fluid but also the solids fraction in the feed and in the liquid external to the draft tube. In the embodiment shown in FIG. 10, the riser has a closed base, and the superficial rise velocity of the liquid across the exit plane 88 is related simply to the liquid flowrate through the throat 84 and the cross-sectional area perpendicular to the flow at 88. The feed does not contain individual particles at infinite dilution. In practice, the feed consists of a suspension of particles at a finite volume fraction, and hence the terminal velocity of individual particles is less than the terminal velocity at infinite dilution because of the phenomenon known as hindered settling. Thus it is not necessary for the vertical velocity in the riser 85 to exceed the terminal velocity of individual particles, in order for such particles to be carried upwards and out of the riser; all that is required is to maintain a velocity that exceeds the hindered settling velocity, so that the suspension forms an expanded fluidised bed. Accordingly, in the present embodiment the device should be sized to maintain the hydrophobic and hydrophilic particles in the feed in a suspended state in the second chamber 85. The hydrophobic particles attached to bubbles will rise out of the liquid and into the froth layer, while other particles will flow with the liquid down the annular gap 89 between the column 21 and the outer wall of the second chamber 85. In practice it is found that some of the coarse hydrophobic particles that are carried into the froth, subsequently disengage from bubbles and drop back into the vessel 21, as a result of bubble coalescence in the froth. In the embodiment shown in FIG. 10, the majority of such particles will fall back into the second chamber 85 where they will be captured by bubbles newly entering the system, and carried once more into the froth.
(47) The invention is described in terms applicable to the separation of minerals in which ore is finely crushed to form a slurry or suspension of particles in water, and the slurry is conditioned with collector and frother to make the mineral species that is to be recovered by flotation hydrophobic or non-wetting, while the non-wetting or hydrophilic species that are to remain in the suspension and are discharged from the flotation vessel as tailings. An example of this is the separation of fine coal particles from the surrounding gangue in a mining operation.
(48) However the invention will also apply to systems in which the particles are of an organic native and typically of biological or non-metallic origin such as algae, printing ink, dairy fat or other liquid particulate systems. The invention will also apply to systems in which all the particles are to be removed in the froth, there being no requirement to separate the components of the particles in the feed liquid on the basis of their hydrophobicity or lack thereof.
(49) A further application is in the removal of metals such as aluminium from suspensions.
EXAMPLE
(50) Samples of silica were subjected to flotation in an embodiment of the invention according to FIG. 1. The silica had a top size of 48 microns and half of the particles in the sample by mass had a particle size below 7.9 microns. Dodecylamine was used as collector at 500 gm/tonne, and methyl isobutyl carbinol at a concentration of 20 ppm was used as frother. The silica, at a concentration of 5% W/W was conditioned in a feed tank for ten minutes, before being pumped to the gas-liquid contactor. In two separate runs the volume ratios of the air flowrate to the flowrate of feed in the flotation column were 1:1 and 2:1 respectively. The pressures upstream of the choking nozzle are shown in Table 1. The overall recovery was calculated from measurements of the flowrates of the feed, the product and the tailings, and the percent solids in each flow. To correct for the presence of entrained material in the concentrate, the amount of entrainment was estimated on the assumption that the water in the froth product contained silica at the same concentration as in the tailings. Tests were conducted with a device constructed according to the present invention and also for comparison, an existing technology in the form of a conventional Jameson cell was used. The results are shown in Table 1.
(51) TABLE-US-00001 TABLE 1 Pressure Air:feed upstream of Flotation volumetric constriction, Overall True machine ratio kPa gauge recovery % recovery % This invention 1:1 90 77 74 2:1 150 93 87 Existing 1:1 54 51 technology
(52) The true recoveries were also calculated on a size-by-size basis, and the results are shown in FIG. 11.
