Powder coating system for coating workpieces with coating powder
10751744 ยท 2020-08-25
Assignee
Inventors
Cpc classification
B05B16/60
PERFORMING OPERATIONS; TRANSPORTING
Y02P70/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16L45/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L25/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B05B14/43
PERFORMING OPERATIONS; TRANSPORTING
F16L43/003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B05B14/48
PERFORMING OPERATIONS; TRANSPORTING
International classification
F16L25/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B05B14/43
PERFORMING OPERATIONS; TRANSPORTING
F16L43/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L45/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B05B14/48
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The powder coating system according to the invention for coating workpieces with coating powder has a coating cubicle (3) and a cyclone separator (5), the coating cubicle (3) being connected to the cyclone separator (5) via a residual powder pipe (4). The cyclone separator (5) comprises in its inlet region an outlet tube (23) in which there is disposed a guide apparatus (50) that has multiple blades (51). These are designed so that the air vortex (28) impinging on the blades (51) can be deflected into a vertical air stream (30).
Claims
1. A powder coating system for coating workpieces with coating powder, wherein a coating cubicle and a cyclone separator are provided, the coating cubicle is connected to an inlet of an inlet tract of the cyclone separator via a residual powder pipe, an outlet tube is provided in the outlet tract of the cyclone separator, in which a guide apparatus is disposed in the outlet tube, the guide apparatus has multiple blades which are designed such that the air vortex impinging on the blades can be deflected at least partially into an eddy-free air stream, and a guide blade having an edge with a plurality of spaced apart projections is provided in the inlet tract of the cyclone separator.
2. The powder coating system according to claim 1, wherein the blades are disposed radially to the longitudinal axis (LA) of the guide apparatus.
3. The powder coating system according to claim 1, wherein the blades are curved in the inlet region.
4. The powder coating system according to claim 1, wherein at least some of the blades in the inlet region and the longitudinal axis (LA) of the guide apparatus each form an angle () between 40 and 70.
5. The powder coating system according to claim 1, wherein the blades in the outlet region are designed to be rectilinear.
6. The powder coating system according to claim 1, wherein at least some of the blades in the outlet region have a surface which is aligned parallel to the longitudinal axis (LA).
7. The powder coating system according to claim 1, wherein the guide apparatus tapers on its downstream side.
8. The powder coating system according to claim 1, wherein the guide apparatus has a holder by means of which it can be disposed in the outlet tube.
9. The powder coating system according to claim 1, wherein the guide apparatus tapers on its upstream side.
10. The powder coating system according to claim 1, wherein the guide blade is disposed tangentially to the powder-air stream entering the cyclone separator.
11. The powder coating system according to claim 1, wherein a residual powder pipe each is disposed along the longitudinal sides of the coating cubicle, a collecting tube is provided, which extends transversely to the residual powder pipes and into which the residual powder pipes open, the collecting tube has a cross section which widens substantially continuously over the length of the collecting tube.
12. The powder coating system according to claim 1, wherein the residual powder pipe has at least one bend to deflect the powder-air stream in another direction the bend has a short, curved outer wall and a long, curved outer wall, wherein the long, curved outer wall has a bulge.
13. The powder coating system according to claim 12, wherein the bend has an inner curve which is part of the short outer wall, the bend has an outer curve which is part of the long outer wall, the long outer wall has a straight section tangentially followed by the outer curve.
14. The powder coating system according to claim 1, wherein the edge of the guide blade is configured as a serrated edge.
15. The powder coating system according to claim 1, wherein the guide blade curves in a direction of flow through the inlet tract, and wherein the edge is a downstream edge of the guide blade.
16. The powder coating system according to claim 1, wherein the inlet tract defines a main flow path for a powder-air stream, the guide blade extending within the inlet tract tangentially to the main flow path, and the edge of the guide blade is spaced from an interior wall forming a portion of the inlet tract to permit flow of the powder-air stream thereacross.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the following the invention will be explained by means of several exemplary embodiments with reference to several figures.
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EMBODIMENTS OF THE INVENTION
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(20) The outlet tube 23 may, for example, have a length of 800 to 1100 mm and a diameter of 480 to 900 mm. The length of the outlet tube 23 depends, inter alia, on the height of the cyclone separator 5. Through a series of experiments it has been found that there is a relationship between the degree of separation of the outlet tube 23 and the separation in the main stream. With increasing length of the outlet tube 23, the degree of separation does indeed increase in the outlet tube 23, the separation in the main stream, however, is thereby adversely affected.
(21) The outlet tube 23 is preferably disposed so that its longitudinal axis extends parallel to the longitudinal axis of the cyclone separator 5. In addition, it is generally advantageous if the longitudinal axis of the outlet tube 23 coincides with the longitudinal axis of the cyclone separator 5, so that the outlet tube 23 is disposed centrally in the cyclone separator 5 and in the outlet tract 5.3 of the cyclone separator 5, respectively.
(22) The guide apparatus 50 preferably protrudes from the bottom of the outlet tube 23 at least 100 mm. As a result, the air vortex 28 has the opportunity to apply itself to the blades 51. This prevents the air vortex 28 from being negatively influenced by the secondary stream 31. If the guide apparatus 50 did not protrude from the outlet tube 23, the secondary stream 31 could influence the stream angle of the air vortex 28 in such a way that shock losses occur. The shock losses would arise if the stream does not hit the blade 51 under the blade angle E.
(23) The guide apparatus 50 is disposed for the most part or entirely in the outlet tube 23. A possible installation position of the guide apparatus 50 is shown in
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(25) The guide apparatus 50 also has a number of guide blades 51, which are here also referred to as blades in short. These can be attached to the outside of the core 55.
(26) Instead, it is also possible to attach the guide blades 51 to the outlet tube 23. Some or all of the guide blades 51 can also be attached both to the core 55 and to the outlet tube 23. The guide blades 51 can be attached by welding, for example.
(27) When the guide apparatus 50 is pushed into the outlet tube 23, it is advantageous if between the guide blades 51 and the outlet tube 23 there are no or minimal air gaps.
(28) The entire guide apparatus or parts thereof can be made of steel, aluminum or conductive plastic, for example. Welding, casting or rapid manufacturing, such as sintering or 3D printing, are conceivable, for example, as the manufacturing method.
(29) The guide blades 51 are preferably disposed equidistant from one another.
(30) Below, the shape of the guide blades 51 will be explained with reference to a blade. Preferably, all blades 51 have the same shape. In the lower region 51.3 the blade 51 has a flat surface which is slightly inclined relative to the horizontal plane. Preferably, together with the horizontal it forms an angle between 20 and 50, even better between 30 and 37. The angle is also referred to as the angle of inflow. With reference to the longitudinal axis LA of the guide apparatus 50, this means that the guide blade 51 and the longitudinal axis LA form an angle (=90) between 40 and 70 and even better between 53 and 60. This inclined surface 51.3 is followed by a curvature in the central region 51.2 a. In the upper Region 51.1, the guide blade 51 has a flat, vertical surface 51.1.
(31) At its lower end the curved surface 51.2 can tangentially transition into the planar surface 51.3, and/or at its upper end it can transition into the vertical surface 51.1. In this way, edges are avoided at the transitions of the surfaces 51.1 to 51.2 and 51.2 to 51.3, so that there the risk of powder deposition is reduced.
(32) In a further embodiment of the guide blade 51, the flat surface is absent in the lower region 51.3. Instead, the guide blade is already curved at the lower end and then transitions at the top into the flat, vertical surface 51.1.
(33) In another embodiment of the guide blade 51, both flat surfaces are missing. Instead, the guide blade is already curved at the lower end and the curvature extends to the upper end of the guide blade. There, the guide blade is curved so that the tangent of the curvature is substantially vertical.
(34) The guide blades 51 are preferably disposed radially on the lateral surface of the core 55, i.e. rectilinearly starting from the center of the core 55. In one embodiment of the guide apparatus 16 blades are provided. Preferably, the number of blades is between 10 and 25.
(35) The purpose of the guide blades 51 is to dissolve the rising air vortex 28 (see
(36) When the air streams past the blades 51, vortex shedding may occur in the outlet region 50.2 of the blades 51. However, these are not relevant here.
(37) Before the upwardly rising air vortex 28 reaches the guide apparatus 50, it has a kinetic energy composed of a vertical (translational) portion and a rotational portion. By means of the guide apparatus 50, this rotational component of the kinetic energy is now converted into an additional translational kinetic energy. Thus, the rotational portion of the kinetic energy is not destroyed or converted into heat energy, but as mentioned, into an additional translational kinetic energy. This has the advantage, among other things, that the energy efficiency of the cyclone separator and thus also of the entire powder coating system increases.
(38) In principle, the longitudinal axis of the cyclone separator 5 does not have to be vertically aligned, as shown in
(39) Instead of the guide apparatus 50, another embodiment of the guide apparatus can also be disposed in the outlet tube 23. Below, various possible embodiments of the guide apparatus will be described.
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(41) Instead of installing the guide apparatus 60 at a fixed height in the outlet tube 23, it can also be adjustable in height. The holder 63 may be designed as a threaded rod with nut from which then the guide apparatus 60 is suspended. The position of the guide apparatus 60 in the outlet tube 23 can be adjusted manually via the nut. Alternatively, the holder 63 may have a tongue and groove system with lock to be able to adjust the position of the guide apparatus 60.
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(45) The individual components of a guide apparatus can also be used in one of the other guide apparatuses. For example, the cone 84 of the guide apparatus 80 may also be used at the bottom of the guide apparatus 50. The components of the guide apparatuses can be combined with each other in any way.
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(47) The pipe 4 comprises a pipe adapter 41, which serves to connect a pipe with a round cross section, which may be, for example, the collecting tube 130 according to
(48) The bend 42 may include a maintenance door 45. Instead of integrating the maintenance door 45 in the bend, the maintenance door 45 may also be provided in the pipe 43. By means of the maintenance door 45 the inside of the pipe may be checked for dirt after a color change and the pipe may be cleaned, if necessary. The maintenance door is shown open in
(49) The components just described, pipe adapter 41, bends 42 and 44 and pipe sections 43 may be made in series and have standard dimensions. They can be produced in stock and serve as standard components. Using these, freely selectable pipe runs can then be formed. The pipe run illustrated in
(50) The components 41-44 of the pipe 4 may be made of sheet metal.
(51) A first possible embodiment of the bend 42 is shown in
(52) The wall 42.1 is shorter than the wall 42.2 and is therefore also referred to as a short outer wall 42.1, whereas the wall 42.2 is also referred to as a long outer wall 42.2 of the bend 42.
(53) The curvature of the wall 42.1 may have a constant radius R1 over the entire curvature, but this is not mandatory. In principle, the wall 42.1 can be more or less arbitrarily concavely curved. Advantageously, however, the curvature in the region 42.12 is not so great thatseen from a fluidic point of viewit forms a corner, because otherwise powder could be deposited there.
(54) Curvature is also understood to mean a shape formed by a polygon, which essentially corresponds to the desired curved run. Thus, the curvature can be generated both by a circular arc and by a polygon. For example, a quarter circle can also be formed by a polygon with 4 to 8 corners. Principally, the above applies to all curvatures present in the bend. The number of corners of the polygon should be chosen so large that in the polygon no too pointed corners or too sharp edges arise because otherwise there could be a stall and powder could deposit there. This also applies, mutatis mutandis, to the inner curve and the outer curve of the bend, which can be formed for example by circular arcs, elliptical sections, arc segments or polygons.
(55) The curvature of the opposite wall 42.2 may have a radius R2 in a first region 42.22 of the curvature and a radius R3 in a second region 42.23 of the curvature. In the two regions 42.22 and 42.23, the two curvatures are in opposite directions. Thus, the course of the curvature in the wall 42.2 is first concave and then convex. But it is also possible to make the curvature in the wall 42.2 so that it is first convex and then concave. The entire curvature of the wall 42.2 is designed so that a bulge 42.24 results in the wall 42.2. By the bulge 42.24 the pipe cross section is increased. This ensures that the powder flowing through the bend 42 does not deposit on the wall 42.2 or can even sinter there. In
(56) If the radius R3 of the concave curvature in the region 42.23 is chosen so large to be close to a straight line, then the region 42.23 can also be formed rectilinearly. In this case, the wall in the region 42.23 is formed by an oblique surface, which merges tangentially into the convex curvature in the region 42.22.
(57) The powder-air mixture can flow through the opening 42.3 into the bend 42 and exit the bend through the opening 42.4. In this case, the arrow 20 indicates the direction of flow of the powder-air mixture. The powder-air mixture can flow through the bend 42 also in the opposite direction. In this case, the arrow 20 indicates the direction of flow of the powder-air mixture. In
(58) A second possible mounting position of the bend 44 is indicated by the dashed line and the reference numeral 44, with the bulge of the bend being located at the side. Thus, one and the same bend can be installed in the residual powder pipe 4 in two different ways.
(59) If the powder-air stream flows through the opening 42.3 into the bend 42 according to the arrow 20, the powder particles hit the wall 42.2 of the bend in the region of the bulge 42.24. The bulge 42.24 thus serves as a bounce surface for the powder particles. The powder particles are slowed without friction. Since no appreciable friction arises, it is prevented that the particles can sinter there. As a result of the permanent air stream the particles are subsequently transported from there to the outlet opening of the bend. The bounce surface preferably has a width between D/2 and D, wherein D is the width of the opening 42.3 of the bend 42.
(60) As mentioned, however, the flow through the bend 42 can also be in the opposite direction. The powder-air stream then flows according to the arrow 20 through the opening 42.4 into the bend 42. In the region PF, some of the powder particles hit the wall 42.2 of the bend perpendicularly, which thus serves as a bounce surface for these powder particles. The powder particles are slowed there without any friction and thus prevented from being able to sinter there. As a result of the permanent air stream, the particles are subsequently transported from there to the outlet opening of the bend, which in this case is the opening 42.3. The bounce surface PF in this case is that surface of the bend 42 which the powder particles impinge perpendicularly or approximately perpendicularly. The bounce surface PF preferably has a width between D/2 and D, wherein D is the width of the opening 42.4 of the bend 42.
(61) If the powder-air mixture flows into the bend 42 in the direction 20, a larger proportion of the powder hits a surface of the outer wall 42.2 aligned perpendicular to the direction of flow compared to the case where the powder-air mixture flows into the bend 42 in the direction 20. Thus, the bounce surface PF at the direction of flow 20 is greater than in the direction 20. Thus, the risk of sintering in the flow in the direction 20 is even smaller than in the flow in the direction 20.
(62) The pressure losses are in both cases of similar magnitude, regardless of whether the air stream flows through the bend 42 coming from the direction 20 or 20.
(63) In previously known bends, the long outer wall 42.2 has a radius R4 and extends as shown in dashed lines in
(64) The bend 42 shown in
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(68) The fan-shaped end 16 of the guide blade 14 is located on the downstream side of the guide blade. The advantage is that this can result in no or almost no deposits at this transition in the cyclone separator, because the shedding surface is reduced to a minimum.
(69) The foregoing description of the exemplary embodiments according to the present invention is for illustrative purposes only. Within the scope of the invention various changes and modifications are possible. Thus, for example, the cyclone separator 5 shown in
(70) The guide blades 51 may also have serrations or may be fan-shaped in the outlet region 51.1. The outlet region 51.1 can be designed in a similar manner as are the fan-shaped ends 16 of the guide blade 14.
(71) The powder coating system for coating of workpieces with coating powder can be provided with a coating cubicle 3, a cyclone separator 5 and a filter 9, the coating cubicle 3 being connected to the cyclone separator 5 via a residual powder pipe 4. However, it is also possible that the coating cubicle 3 is connected to the filter 9 via the residual powder pipe 4.
LIST OF REFERENCE NUMERALS
(72) 1 Powder coating system 2 Spray guns 3 Coating cubicle 4 Residual powder pipe 5 Cyclone separator 5.1 Inlet tract 5.2 Separation tract 5.3 Outlet tract 6 Pipe 7 Fan 9 Post-filter 10 Powder center 11 Workpiece 12 Pipe 13 Suction tube 14 Guide blade 15 Lid of the cyclone separator 16 Fan-shaped ends 20 Powder-air mixture or powder-air stream 21 Inlet 22 Outlet 23 Outlet tube 24 Outer wall of the cyclone separator 25 Powder outlet 26 Supporting structure 27 Transport direction of the powder 28 Air vortex 29 Sieve 30 Vertical or substantially eddy-free air stream 31 Secondary stream 32 Manual coating booth 33 Waste container 41 Pipe adapter 41.1 Round cross section 41.2 Quadrangular cross section 42 Bend 42.1 Wall of the bend 42.11 Region of the wall 42.1 42.12 Region of the wall 42.1 42.2 Wall of the bend 42.21 Region of the wall 42.2 42.22 Region of the wall 42.2 42.23 Region of the wall 42.2 42.24 Bulge 43 Straight tube 44 Bend 45 Maintenance door 50 Guide apparatus 50.1 Inlet region 50.2 Outlet region 51 Blade 51.1 Rectilinear region 51.2 Curvature 51.3 Rectilinear region 52 Cone or truncated cone 55 Cylindrical core 60 Guide apparatus 60.1 Inlet region 60.2 Outlet region 61 Blade 61.1 Rectilinear region 61.2 Curvature 61.3 Rectilinear region 62 Cone 63 Holder 65 Cylindrical core 70 Guide apparatus 70.1 Inlet region 70.2 Outlet region 71 Blade 71.1 Rectilinear region 71.2 Curvature 71.3 Rectilinear region 72 Cone 73 Holder 75 Cylindrical core 80 Guide apparatus 80.1 Inlet region 80.2 Outlet region 81 Blade 81.1 Rectilinear region 81.2 Curvature 81.3 Rectilinear region 82 Cone 83 Holder 84 Cone 85 Cylindrical core 90 Guide apparatus 90.1 Inlet region 90.2 Outlet region 91 Blade 91.1 Rectilinear region 91.2 Curvature 91.3 Rectilinear region 92 Cone 93 Holder 94 Shell 95 Cylindrical core 130 Collecting tube 131 Inlet 132 Inlet 133 Outlet 134 Inspection lid 135 Collecting tube D1 Diameter D2 Diameter D3 Diameter X1 Distance R1 Radius R2 Radius R3 Radius R4 Radius L1 Reference axis L2 Reference axis LA Longitudinal axis of the guide apparatus PL1 Projection line 1 PL2 Projection line 2 PF Bounce surface Angle of curvature Angle Angle in the inlet region of the blade