Separating unit having an impaction surface
11400400 · 2022-08-02
Assignee
Inventors
Cpc classification
B05B14/44
PERFORMING OPERATIONS; TRANSPORTING
B01D45/16
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
B05B16/40
PERFORMING OPERATIONS; TRANSPORTING
B05B14/43
PERFORMING OPERATIONS; TRANSPORTING
B01D45/06
PERFORMING OPERATIONS; TRANSPORTING
International classification
B01D45/00
PERFORMING OPERATIONS; TRANSPORTING
B01D45/08
PERFORMING OPERATIONS; TRANSPORTING
B05B14/43
PERFORMING OPERATIONS; TRANSPORTING
B01D45/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A separating stage for inertial separation of components contained in a fluid flowing through, in particular paint particles and/or paint agglomerates includes at least one separating segment, which has at least one acceleration section for the fluid on the inlet side, in which the fluid is accelerated in a through-flow direction, and a first impaction surface for components contained in the fluid is downstream of the acceleration section. A separating unit having at least one separating stage, a kit, a transport cart, a coating facility, and a method for producing a separating unit are also provided.
Claims
1. Separating unit having at least one separating stage for inertial separation of components contained in a fluid flowing through the separating unit, comprising a separating segment which has at least one acceleration section having an inlet and, downstream of the inlet in a through-flow direction, the separating segment having a first impaction surface for components contained in the fluid downstream of the acceleration section, wherein the first impaction surface has a baffle region and a curved portion downstream of the baffle region in the through-flow direction arranged to deflect a direction of the fluid by at least 180° with respect to the through-flow direction of the fluid in the acceleration section, a second impaction surface downstream of the first impaction surface in the through-flow direction, wherein the second impaction section includes a curved portion formed by a rear side of a boundary wall of the acceleration section, wherein an end edge of the curved portion of the first impaction surface is oriented toward the second impaction surface, wherein the acceleration section is designed as a nozzle having a free flow cross-section that tapers downwardly in the through-flow direction, and wherein the at least one separating stage is arranged in a housing wherein multiple separating stages are arranged fluidically so they can have flow through them in parallel and/or in series.
2. Separating unit as claimed in claim 1, wherein a guide element is arranged in front of or in a free flow cross section of the acceleration section.
3. Separating unit as claimed in claim 2, wherein the guide element extends parallel to an incident flow surface of the separating stage, and/or the guide element is arranged in a plane of symmetry of the free flow cross section, and/or in that the guide element has a two-dimensional cross section.
4. Separating unit as claimed in claim 1, wherein the housing has an opening on its incident flow side, the opening having an upper edge and a lower edge, wherein the upper edge and the lower edge have different heights.
5. Separating unit as claimed in claim 4, wherein a height of the lower edge is higher than a height of the upper edge.
6. Separating unit as claimed in claim 1, wherein at least one filter stage is arranged downstream of the separating stage.
7. Separating unit as claimed in claim 6, wherein the at least one filter stage has a folded filter bellows, the fold edges of which are oriented transversely to an extension of the acceleration section extending in parallel to a z-axis.
8. Separating unit as claimed in claim 1, wherein the separating stage and one or more filter stages are arranged in a common housing.
9. Separating unit as claimed in claim 1, wherein a bottom part and/or cover part has a negative contour in the form of a cross section of the at least one separating stage as a holder for the at least one separating stare.
10. Separating unit as claimed in claim 9, wherein the negative contour is formed as interrupted openings in the bottom part and/or cover part.
11. Separating unit as claimed in claim 1, wherein the separating stages are formed from a kit of components, the kit comprising blanks made of at least one of cardboard, corrugated cardboard, fiber molded parts, and deep-drawn parts made of plastic.
12. Separating unit as claimed in claim 11, wherein the blanks have predefined buckle lines and/or fold lines.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further advantages result from the following description of the drawings. Exemplary embodiments of the invention are illustrated in the drawings. The drawings, the description, and the claims contain numerous features in combination. A person skilled in the art will expediently also consider the features individually and combined them to form further meaningful combinations.
(2) In the exemplary figures:
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DETAILED DESCRIPTION
(33) Components that are the same or have the same function are identified in the figures with the same reference signs. The figures only show examples and are not to be understood as restrictive.
(34) Directional terminology used hereinafter with terms such as “left”, “right”, “top”, “bottom”, “in front”, “behind”, “after” and the like is used only for better comprehension of the figures and is not to represent a restriction of the generality in any case. The components and elements shown, and their design and use can vary in terms of the considerations of a person skilled in the art and can be adapted to the respective applications.
(35)
(36) The separating stage 100 has an incident flow surface 10 and an acceleration section 12, for example, a nozzle, on the inlet side, followed by a first impaction surface 13 having fluid flow deflection on a first curved portion 15. The incident flow surface 10 forms a cross-sectional area in front of the acceleration section 12.
(37) A coordinate cross x, y is indicated for orientation. The x-axis corresponds to a longitudinal axis, which is preferably a main through-flow direction of the acceleration section 12. In this example, the y-axis corresponds to a transverse axis, along which the incident flow surface 10 and a free flow cross section are arranged at the entry of the fluid into the acceleration section 12. The z-axis is oriented perpendicular to the image plane and in this example corresponds to a vertical axis of the separating stage 100. In this exemplary embodiment, the separating stage 100 is formed by a single separating segment.
(38) A person skilled in the art understands that the y-axis would form the vertical axis and the z-axis the transverse axis if the separating stage 100 were rotated, for example, by 90° about the x-axis.
(39) The cross-sectional area is to be understood as the cross-sectional area of the separating segment perpendicular to a main through-flow direction.
(40) The main through-flow direction is to be understood as an imaginary straight connection between inlet side and outlet side of the separating stage. The flow enters the separating stage at the inlet side and exits again at the outlet side, which is opposite to the inlet side in this example, independently of whether one or more reversals of direction take place in the interior of the separating stage 100.
(41) The incident flow surface 10 merges into the wall of the acceleration section 12. The acceleration section 12 is oriented having its open end 16 toward a baffle region 14 of the first impaction surface 13 which is arranged at a distance transversely thereto. The curved portion 15 of the first impaction surface 13 follows a second impaction surface 18 with opposing fluid flow deflection on a further portion 22 curved in the opposite direction to the first. The fluid flow is indicated by straight and rounded thick arrows.
(42) The fluid, for example, a mixture of air and paint particles and paint agglomerates from a painting facility, is incident on the incident flow surface 10, which has a width B0, and enters the acceleration section 12 of the separating stage 100 in a through-flow direction 102 in the direction of the x-axis. For simplification, it is ignored here that the part of the fluid which is incident on the incident flow surface 10 experiences a deflection into the acceleration section 12 due to the rounded profile of the acceleration section 12 at the entry of the fluid into the acceleration section 12. At the narrowest point of the acceleration section 12, it has a width B1 in the direction of the y-axis.
(43) The distance from the end 16 of the acceleration section 12 to the opposite baffle region 14 of the impaction surface 13 is identified by L1. In this example, the acceleration section 12 also has the width B1 at the end 16. If the width of the acceleration section 12 were to widen again towards the end 16, the distance L1 would be determined from the narrowest point having the width B1, specifically from the end of the region having the narrowest width B1 which is closest to the end 16 of the acceleration section 12.
(44) The incoming fluid flow is divided symmetrically to the longitudinal direction of the acceleration section 12 in the transverse direction on both sides into two partial flows flowing away from each other and deflected outward from the end 16 of the acceleration section 12. The portion 15 of the first impaction surface 13 curved uniformly having a radius R1 follows on both sides on the baffle region 14, which is flat in this example. The region of the first impaction surface 13 opposite to the acceleration section 12 is flat.
(45) The end edge 21 of the curved portion 15 is oriented toward a second impaction surface 18, which has a curved portion 22. The second impaction surface 18 is advantageously formed by the outside of the acceleration section 12. The distance between the end edge 21 and the baffle region 14 is referred to as the depth L2 of the first impaction surface 13.
(46) The incoming fluid is accelerated in the acceleration section 12 and deflected after the baffle region 14 on the left side of the figure clockwise in accordance with the curvature of the curved portion 15 and counterclockwise on the opposing right side. The deflection is at least 45°, preferably greater than 180°, here 270°, with respect to the through-flow direction 102. The deflection by greater than 180° increases the probability of a wall contact for the particles in the fluid flow, so that the separation efficiency is increased.
(47) The fluid flow is further deflected at the second impaction surface 18, which is arranged having an entry region transverse to the first curved portion 15. The curved portion 22 of the second impaction surface 18 is curved in the opposite direction to the first curved portion 15 of the first impaction surface 13. The fluid flow is deflected further there counterclockwise on the left side in the figure and clockwise on the right side of the figure, so that the fluid flow flows into the boundary section 12 opposite to the original through-flow direction 102 at the beginning of the impaction surface 18 and is finally deflected further in the direction of the x-axis at a boundary wall 20. The two partial flows leave the separating stage 100 in the original through-flow direction 102.
(48) Particles from the fluid can easily be deposited on the curved portions 15, 22 due to the deflection of the centrifugal forces prevailing on the curved portions 15, 22. After the first deflection on the first impaction surface 13, particles that are located far from this surface in the fluid flow necessarily come into the vicinity of the second impaction surface 18 during the second deflection on the second impaction surface 18 and can easily be deposited there and thus removed from the fluid flow.
(49) The distance L1 between the acceleration section 12 and the impaction surface 13 arranged behind it is at least half of the width B2 in the narrowest cross-section of the acceleration section 12. A shorter distance L1 results in an increased pressure loss and the structure would be rapidly clogged by deposited paint. The ratio of the width B2 to the depth L2 of the first impaction surface 13 is between 1:2 and 3:1. A ratio of greater than 1.5:1, in particular approximately 2:1, has proven to be particularly advantageous for the flow guiding.
(50) The mean inflow velocity in the narrowest cross section of the acceleration section 12 is preferably 5 m/s to 20 m/s. If the highest possible degrees of separation are to be achieved, velocities of approximately 15 m/s have proven to be advantageous. On the other hand, if a coarse separation is to take place with the lowest possible pressure loss, velocities of approximately 10 m/s have proven to be advantageous.
(51) It is advantageous if a clear width B1 of the acceleration section 12 of the separating stage 100 is at least 20 mm at the narrowest point in order to prevent clogging of the acceleration section 12 due to adhering particles, for example paint deposits from painting facilities. For paints that form particularly voluminous agglomerates during the deposition, which is typical, for example, for water-based base coats, the clear width B1 is preferably at least 40 mm.
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(58) On overflowed inner radii R2 having rounded end edge 24 or in front of the relatively sharp-edged end edge 21 of overflowed walls, the collection niches 30, 32 open opposite to the overflow direction prevent particles already deposited on the wall surface from being entrained, in particular paint particles or agglomerates.
(59) The separating stages 100 and separating units formed therefrom can be adapted for different applications, in particular defined by a required degree of separation, volume flow to be treated, and process conditions, by selecting individual separating stages 100 from an assortment of suitable separating stages and arranging them in suitable sequence in succession.
(60) A required separation efficiency can be achieved with the lowest possible pressure loss via the separating unit 100. The highest possible storage capacity can also be achieved in order to achieve a long service life for the separating units. The separating unit 100 can have dimensions that are easy to handle and, particularly when loaded, can also have a weight that is still easy to handle.
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(63) For a respective separating segment of the first separating stage 100 of a separating unit, the ratio of the free inflow area, ie the narrowest cross section in the acceleration section 12, to the total cross-sectional area in front of the acceleration section 12 is in the range of 1:4 to 1:10. A ratio in the range of 1:6 to 1:8 has proven to be advantageous. The cross-sectional area is to be understood as the cross-sectional area of the respective separating segment of the separating stage 100 perpendicular to a main through-flow direction. The entire cross-sectional area of the separating segments is also referred to as the incident flow surface 10.
(64) The separating stage 100 is constructed from a bottom part 122, a cover part 124, which is preferably of identical construction, and multiple components 110, 112, which are to form wall parts for the flow direction, namely the incident flow surface 10 having slotted acceleration sections 12 and first impaction surfaces 13. The component 110 also provides the second impaction surfaces 18 in the assembled state.
(65) Bottom part 122 and cover part 124 have a negative contour, predetermined, for example, by depressions, holding nubs, and the like, in the form of the horizontal cross section of the separating stage 100 to have flow through it. The components 110, 112 are inserted into these negative contours.
(66) Bottom part 122 and cover part 124 can be provided as a flat blank, for example, made of corrugated cardboard, having corresponding cutouts, or preferably as a three-dimensionally shaped component. Bottom part 122 and cover part 124 are particularly preferably provided as fiber molded parts or deep-drawn parts, in which the negative contour is designed in the form of depressions tapering downward and/or protrusions having trapezoidal cross-section, so that insertion bevels are available for easier insertion of the components 110, 112.
(67) The components 110, 112 of the wall parts preferably consist of or comprises flat blanks 300 as seen in
(68) This design is suitable for rather coarse separating structures, which offer moderate separation efficiency and a very high storage volume with low pressure loss. Therefore, this separating stage 100 is primarily intended as a first separating stage 102 for coarse separation. Depending on the process, in particular depending on the paint, however, it can also be sufficient as the only separating stage 100. In CFD simulations and tests of such separating stages 100, a separation efficiency in the range of 60% to 96% could be achieved with differential pressures of the unloaded separating stage 100 between 100 Pa and 300 Pa.
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(70) The guide element 160 extends in a plane of symmetry of the free flow cross section at the entry of the fluid into the acceleration section 12 from the bottom part 122 to the cover part 124 along the z-axis. In this example, the guide element 160 has an extension which is parallel to the z-axis.
(71) In this example, the guide element 160 is formed tapering to a point against the direction of flow, for example having a V-shaped cross section. The guide element 160 can be used to minimize noise during the flow through the separating unit 200.
(72) The guide element 160 can be provided detachably from the separating unit 200 and can be removed from the separating unit 200 if necessary.
(73) The guide element 160 can influence the through flow in such a way that a noise development can be reduced or substantially suppressed.
(74) By way of suitable positioning and/or shaping of the guide element 160, it can induce swirling of the inflowing fluid, for example, inflowing air, and/or a reflection of the sound generated after the acceleration section 12.
(75) In an alternative example, the cross section of the region of the baffle region 14 opposite to the acceleration section 12 can be pointed (see, for example,
(76) The guide element 160 can be provided as a one-piece additional element, which can be added or left out if needed during the construction of the separating unit 106.
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(78) The wall part shown can be brought into its shape by curving or buckling and inserted with its tabs on its narrow sides into the openings of the negative contour.
(79) An advantageous method for producing a separating stage 100 are separating unit 200 having at least one separating stage 100 according to the invention provides that the kit 109 is provided from components.
(80) The components are in particular blanks made of cardboard and/or corrugated cardboard and/or fiber molded parts and/or deep-drawn parts made of plastic.
(81) Components are taken from the kit and shaped to form at least one incident flow surface, at least one acceleration section, and at least one impaction surface.
(82) The shaped components are inserted into a corresponding negative form of bottom part 122 and/or cover part 124. The assembly made up of the at least one incident flow surface, the at least one acceleration section, and the at least one impaction surface having bottom part 122 and cover part 124 is inserted into a housing.
(83) At least one filter stage, in particular a depth filter, can optionally be inserted into the housing downstream of the at least one separating stage in the through-flow direction.
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(85) The separating stage 100 is constructed from one or more, three-dimensionally shaped components 130, 132, 134 formed as sheets and forms a relatively fine separating stage 106. The sheets are three-dimensionally shaped, but free of undercuts.
(86) The separating structure can be produced by arranging multiple components 130, 132, 134 in succession or by folding one or more such components 130, 132, 134 or by a combination of folding and arranging these components 130, 132, 134 in succession.
(87) The components 130, 132, 134 formed as sheets are preferably fiber molded parts or deep-drawn parts. The component 130 contains the incident flow surface 10 and accelerator sections 12 as well as partition walls between the acceleration sections 12, the component 132 contains the first impaction surfaces 13, and the component 134 contains a support structure for the component 132.
(88) This design of the separating stage 106 is suitable for rather fine separating structures having increased separation efficiency and less storage volume.
(89) For this purpose, the geometric structure of the separating stage 100 comprises a plurality of acceleration sections 12, which are arranged in parallel and are designed as incoming flow nozzles, having first impaction surfaces 13 which are arranged relatively close behind and have comparatively small radii of curvature. In CFD simulations of such separating stages 100, the separation efficiency at differential pressures between 300 Pa and 400 Pa over the unloaded separating stage was in the range from 93 to 99%.
(90) A set of components 130, 132, 134 can be designed such that several different separating stages 100 can alternatively be produced therefrom. The components 130, 132, 134 are preferably blanks made of cardboard or corrugated cardboard and/or fiber molded parts and/or deep-drawn parts made of plastic. Due to the production process, fiber molded parts or deep-drawn parts are formed without undercuts and therefore can be stacked well. All components can therefore be transported in a space-saving manner.
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(92) The separating stage 100 is distinguished in that impaction surfaces having incident flow due to parallel acceleration sections 12 designed as incoming flow nozzles are arranged spatially in succession. To represent the structures arranged in succession, multiple identical components 130, 132, 134 are used here, which only have to be used rotated by 180° around the x-axis, the longitudinal axis here, for the rear part of the structure. The components 130, 132, 134 are preferably fiber molded parts.
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(94) In the first separating stage 100, 108, the incoming flow takes place through six acceleration sections 12 having flow through them in parallel in the first component 130 and the first impaction surfaces 13 (component 132) behind them are arranged offset in succession. The second separating stage 100, 106 consists of or comprises geometrically identical contours, but only has three acceleration structures 12 which have flow through them in the component 130 in the rear region of the exploded view. The first and second separating stages 108, 106 are constructed from a total of 10 components 130, 132, 134: However, it is advantageous that only three different components 130, 132, 134 are used for this purpose. The second separating stage 106 has a higher separation efficiency since it has flow through it at twice the flow velocities as the first separating stage 106. Both separating stages 108, 106 are arranged in a common outer box as housing 150.
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(96) The separating unit 200 is constructed from two separating stages 104, 106 and a post-filter stage in the form of a depth filter 140. The first separating stage 104 is constructed in accordance with the exemplary embodiment in
(97) Both separating stages 104, 106 and depth filter 140 are arranged in a common outer box as housing 150
(98) In general, separating units 200 are preferred in the exemplary embodiments, the external dimensions of which do not exceed width×height×depth (corresponds to the edge length measured in the flow direction 102 (
(99) The filter stage 140 in the form of a depth filter can advantageously have a folded filter bellows 142.
(100) The separating unit 200 is provided for treating an air volume flow of 500 m.sup.3/h to 2000 m.sup.3/h, in particular 1300 m.sup.3/h to 1800 m.sup.3/h.
(101) At an incident flow velocity of the separating unit 200 (with respect to the total cross-sectional area) of 1.6 m/s, the pressure loss for the through flow of the unloaded separating unit is in the range of 200 Pa to 800 Pa, preferably at most 600 Pa.
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(103) The filter stage 140 has a folded filter bellows 142, the fold edges 144 of which are oriented in the direction of the y-axis and thus transversely to the extension 11 of the acceleration sections extending in the direction of the z-axis and which extend in the direction of the z-axis. This allows the fluid that emerges from the second separating stage 106 to flow through the filter stage 140 evenly. If the separating unit 200 were tilted around the x-axis, for example, it is advantageous to maintain the relative orientation of the fold edges 144 of the filter stage 140 transverse to the extension 11 of the acceleration section 12.
(104) The filter edges 144 are angular in this example. Optionally, the filter edges 144 can also be designed differently, for example V-shaped or U-shaped.
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(106) In this exemplary embodiment, the separating stage 100 comprises, for example, only a single separating segment. The separating stage 100 furthermore has a guide element 160 in front of the free flow cross section at the entry of the fluid into the acceleration section.
(107) The filter stage 140 has a folded filter bellows 142, the fold edges 144 of which are oriented in the direction of the y-axis and thus transversely to the extension 11 of the acceleration section extending in the direction of the z-axis. If the separating unit 200 were tilted around the x-axis, for example, it is advantageous to maintain the relative orientation of the fold edges 144 of the filter stage 140 transverse to the extension 11 of the acceleration section 12.
(108) The guide element 160 extends in a plane of symmetry of the free flow cross section at the entry of the fluid into the acceleration section from the bottom part 122 to the cover pan 124 along the vertical axis z. The guide element 160 has an extension in this example which is parallel to the z-axis.
(109) In this example, the guide element 160 is formed tapering to a point against the direction of flow, for example having a V-shaped cross section. The guide element 160 can be used to minimize noise during the flow through the separating unit 200.
(110) The guide element 160 can be provided detachably from the separating unit 200 and can be removed from the separating unit 200 if necessary.
(111) The guide element 160 can influence the through flow in such a way that a noise development can be reduced or substantially suppressed.
(112) By way of suitable positioning and/or shaping of the guide element 160, it can induce swirling of the inflowing fluid, for example, inflowing air, and/or a reflection of the sound generated after the acceleration section 12.
(113) In an alternative example, the cross section of the region of the baffle region 14 opposite to the acceleration section 12 can be pointed (see, for example,
(114) The guide element 160 can be provided as a one-piece additional element, which can be added or left out if needed during the construction of the separating unit 106.
(115) The two stages 100, 140 can optionally be arranged in a single housing or in two separate housings.
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(118) The coating facility 400 is used, for example, for painting vehicle bodies 500. The vehicle body 500 is arranged on a work platform and is sprayed with paint while it is moved in the transport direction 410, which extends perpendicular to the plane of the drawing in the figure. The air flow having paint residues flows downward in the coating facility 400 and flows through the transport carts 300 arranged on both sides. It is obvious that a plurality of transport carts 300 having separating units 200 can have the paint-laden air flow through them in parallel, wherein the plurality of transport carts 300 can also be arranged on only one side of the coating facility 400. The transport carts 300 form a fluid-conducting connection to an exhaust air duct. The paint-laden air flows through the separating units 200 of the transport carts 300 and reaches its outlet and enters the exhaust air duct in a purified state. The purified exhaust air can again be used for the painting process and can be circulated or can be exhausted from the painting facility 400. The movable transport carts 300 can be exchanged during operation in the coating facility 400.