EP3775571B1 - Fan and inflow grille for a fan - Google Patents
Fan and inflow grille for a fan Download PDFInfo
- Publication number
- EP3775571B1 EP3775571B1 EP19715390.1A EP19715390A EP3775571B1 EP 3775571 B1 EP3775571 B1 EP 3775571B1 EP 19715390 A EP19715390 A EP 19715390A EP 3775571 B1 EP3775571 B1 EP 3775571B1
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- EP
- European Patent Office
- Prior art keywords
- webs
- inflow
- fan
- grille
- region
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/70—Suction grids; Strainers; Dust separation; Cleaning
- F04D29/701—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps
- F04D29/703—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps specially for fans, e.g. fan guards
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2210/00—Working fluids
- F05D2210/10—Kind or type
- F05D2210/12—Kind or type gaseous, i.e. compressible
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
Definitions
- the present invention relates to a fan (axial, radial or diagonal fan) with an impeller and a guide device in the flow path in front of the impeller, preferably in front of the inlet area of an inlet nozzle, wherein the guide device is designed as an inflow grille with flat webs and wherein the webs form a plurality of grid-cell-like flow channels. Furthermore, the invention relates to a special guide device which is designed in the sense of an inflow grille with flat webs.
- a generic fan with inflow-side guide vane is, for example, made of WO 03/054395 A1 or from WO 2015/124237 A1 known.
- the guide device provided there serves primarily to even out the flow, and in particular to reduce noise.
- the known guide device generates a pre-swirl in the direction of rotation of the impeller. It is important to note that acoustic improvements are regularly accompanied by losses in air performance and efficiency.
- the guide device provided there is also very complex to manufacture.
- guide vanes are already known from practice, which serve to improve efficiency and/or air performance.
- these guide vanes have acoustic disadvantages and are complicated to construct and install in the respective fan products. They are usually installed in front of fan impellers in a cylindrical installation space with a diameter approximately the same as the fan impeller and therefore do not have a significantly larger flow area than the fan. As a result, the air speeds in the area of these guide vanes are relatively high, which in particular causes the acoustic disadvantages.
- the invention is based on the following technical problem.
- the present invention is therefore based on the task of designing and developing a fan in such a way that noise is reduced in the event of a disturbed inflow.
- the fan should be compact and have only extremely low pressure losses.
- a guide device in particular an inflow grille or guide grille, should be specified which meets the above requirements and which can be manufactured using plastic injection molding with economical tooling. It should be dimensionally stable and be able to advantageously take on the function of an upstream contact protection grille.
- the webs extend predominantly between preferably two branches or between one branch in each edge area. Preferably three webs meet at each branch.
- the underlying independent claims are the basic idea of providing an inflow grille or inlet grille in front of the inlet nozzle of a fan in order to reduce the noise generated when the fan is operating in the event of a disruption to the inflow.
- the inflow grille is defined by flat webs, whereby the webs are arranged in such a way that grid-cell-like flow channels are created.
- advantageous geometries can be realized, for example in that the flow channels have a honeycomb-like cross-section.
- honeycomb-like is to be understood in the broadest sense, so that it also includes polygons, for example grid cells with a square, five-sided or hexagonal or polygonal cross-section.
- the inflow grille has a basket-like contour, whereby the contour can refer to both the outer and the inner envelope surface of the inflow grille.
- An inflow grille of the type mentioned above is suitable for the radial inflow in the area close to the nozzle plate.
- the flow channels have a beneficial effect on low pressure losses.
- the basket-like outer contour is also advantageous for demoldability in the context of an injection molding technique that is used primarily for plastic parts.
- compact grilles with the corresponding properties can be produced.
- the basket-like outer contour is particularly advantageous if it is continuous and curved.
- the grid webs should be as thin as possible, for example in the range of 0.25 mm to 1 mm web thickness. In the direction of flow they should have a depth of at least 5 mm (hence the term "flat web” chosen in the claims).
- the grid bars form a non-structured grid in which honeycomb-like grid cells are combined with one another.
- the grid cells can be polygonal and combined with one another or with one another. This allows minimal obstruction by grid bars to be achieved, particularly when a certain maximum grid width is necessary due to the required noise reduction or taking into account contact protection aspects, which leads to low pressure and efficiency losses.
- the inlet grille advantageously extends over the entire area up to the imaginary extension of the fan axis, so it has no or no particularly large opening in the inner area.
- a central opening is not necessary, and can even be avoided, provided the inlet grille also provides protection against contact. It has also been found that a central opening is detrimental to minimizing noise and improving the stability of the grille.
- the special design of the inflow grille is particularly advantageous, not only in terms of the grid-like flow channels, but also in terms of the continuous and curved outer contour.
- Honeycomb elements with 4, 5 or 6 corners allow unstructured grilles to be created, with variable grille widths being possible across the entire inflow grille, depending on requirements.
- the inlet grille according to the invention is intended for use in an axial, radial or diagonal fan and is constructed in accordance with the above statements.
- Fig.1 shows an embodiment of an inflow grille 1 in a perspective view from the front, ie seen from the inflow side.
- the inflow grille 1 is similar to the illustration in Fig. 17 advantageously mounted in front of the inlet nozzle 2 of a fan so that its axis roughly coincides with the rotation axis of the fan.
- the air first flows through the inlet grille 1 into the inlet nozzle 2 before it experiences a total pressure increase as it flows through an impeller 3 of the fan, which is driven by a motor 4.
- the inlet grille 1 evens out the incoming air, thereby reducing the noise generated in the impeller.
- the inlet grille 1 consists of a large number of webs 5 which define grille cells 6.
- the grille cells 6 are flowed through when the fan is operating, i.e. they form flow channels.
- the incoming air has a lower speed in an area in front of an inlet nozzle 2 than inside an inlet nozzle 2, since the area flowed through by the air mass flow conveyed by the fan is larger in an area in front of an inlet nozzle 2 than in an inlet nozzle 2.
- the inlet grille 1 is used in such an area of relatively low flow speeds, i.e. the flow speed at the inlet grille 1 is lower than the flow speed in the inlet nozzle 2. This keeps flow losses and noise generation at the inlet grille 1 to a minimum.
- the inflow in an area in front of an inlet nozzle 2 is not flat or not predominantly parallel to the axis, it is of great advantage not to make the contour of the inflow grille 1 completely flat.
- the contour can be described by the outer envelope surface 7 and/or the inner envelope surface 8 ( Fig. 2 ) of the inflow grille 1.
- These envelope surfaces 7, 8 are defined by the totality of the inflow and outflow end faces 7a and 8a of the webs 5 (see Fig. 1a ), supplemented by imaginary continuous or curvature-continuous completions in the area of the flow channels 6.
- Fig. 1a shows a detailed, enlarged view of a section of the inlet grille 1 from Fig.1 .
- the webs 5 have a significant depth t (9) in the direction of flow, advantageously around 6-20 mm. For this reason, the webs 5 are also referred to as "flat" webs.
- a grid cell 6 is also characterized by a cell width w (12), for example defined by the radius of the largest in-sphere of the cell 6.
- a small grid width w (12) is advantageous, for example a value of w (12) of no more than two to three times the web depth t (12) for the majority of the cells 6 of an inflow grid 1.
- the inflow grid 1 in the embodiment according to Fig.1 also represents a contact protection device which, in accordance with regulations and standards, must comply with requirements for the cell width w (12) depending on the cell shape and the distance of the cell 6 from a rotating part of the fan. This additionally limits the size of the cell width w (12) upwards.
- the web lengths I are determined based on the neutral fibers 13, advantageously on the outer or inner envelope surface 7 or 8).
- An "unstructured" grid structure with honeycomb-like cells 6 as in the exemplary embodiment can be very advantageous for the required total web length under the described conditions for the maximum grid width w (12).
- the inlet grille 1 is according to Fig.1 shown in a perspective view from the downstream side.
- the inlet grille 1 has fastening areas 18 on the outside, which serve to attach the inlet grille 1 to the inlet nozzle 2 or the nozzle plate 32 ( Fig. 17 ) to be attached.
- fastening areas 18 There are various options for designing the fastening areas 18. Possible fastenings are screws, rivets, snap hooks, bayonet locks, gluing, snapping, Velcro or others. In the example, a screw hole is provided on each of the four fastening areas 18.
- the basket-like contour of the inner envelope surface 8 of the inflow grille 1 is clearly visible.
- This contour extends along the outer circumference for a certain distance, preferably more than 10 mm or more than 8% of the outer diameter D (20) ( Fig.5 ), approximately parallel to the imaginary central axis, approximately on a cylinder jacket (cylinder jacket-like region 34).
- the cells 19 of the outer row are located in this cylinder jacket-like region 34, two adjacent cells of which are separated from one another by a web 35 of the outer row.
- the cells 19 of the outer row have a rather elongated shape.
- the cell widths w (in-sphere radii, for the cells 19 of the outer row essentially determined by the distance between two adjacent webs 35 of the outer row) of these cells are rather smaller than the in-sphere radii of the other cells 6.
- the contour is flat or flat, approximately orthogonal to the axis (flat region 33).
- the transition from the flat region 33 to the cylinder jacket-like region 34 takes place via a short transition region 24, which is curved in the exemplary embodiment.
- the outer envelope surface 7 and the inner envelope surface 8 run approximately parallel. The division of the regions 33, 34, 24 can be carried out based on the outer and/or inner envelope surface 7 or 8.
- the inlet grille 1 is according to Fig.1 and 2 in axial plan view from the front (seen from the inflow side).
- Such an inflow grille 1 is advantageously manufactured using plastic injection molding. It is also advantageous to view the grille from Fig.3 also to be chosen as the demolding direction for an injection molding tool in order to keep the tool complexity low.
- one tool part then moves relative to the inflow grille 1 towards the viewer, advantageously the nozzle side of the tool, and another tool part moves away from the viewer.
- the injection molding tool advantageously has no further slides for the sake of ease of manufacture.
- the webs can also advantageously have a curvature in order to optimally guide the flow.
- a web 29 is marked, which is an axially aligned web, i.e. it is aligned parallel to the axis (viewing and slide direction), which makes it easier to demold it.
- Axially aligned webs 29 are advantageously provided with a demolding slope.
- a suitable, more elastic material is selected, small undercuts can be created and still demolded in the axial direction with a simple open-close tool. This makes it easy and economical to create a contour that is particularly optimized in terms of flow.
- the cells in the area near the axis are smaller than those in the area away from the axis.
- the cell size or cell width w (12, see Fig.2 ) is optimized in each case with regard to the requirements regarding compliance the contact protection regulations and with regard to the acoustic improvements or flow equalization to be achieved.
- the distribution of the cells is optimized using a special algorithm.
- a wide variety of cell contours occur (when viewed on one of the envelope surfaces 7 or 8), in particular, but not exclusively, regular and irregular 4-6 corners.
- each cell when viewed on an envelope surface 7 or 8) describes a range of points which are those that are closest to an imaginary central point (on the envelope surface) compared to the imaginary central points of all other cells.
- the structure of the grid 1 is therefore also characterized by the fact that in the majority of branching areas 15 exactly 3 webs 5 meet, in far fewer branching areas 4 webs 5 meet. Furthermore, there are no relatively small cells at the edge with a flow area of less than 50% with respect to the flow area of one of their neighboring cells, which are caused by an effect of "cutting through outer cells with the edge".
- the inlet grille 1 is made of Fig. 1 to 3 shown in axial plan view from behind (seen from the downstream side).
- the webs 35 of the outer row which are aligned in the axial direction, have a free end 14. This allows them to be demolded by a tool slide which moves in the direction of the downstream side (towards the viewer) when opened.
- the fact that the ends 14 of the outer webs 35 are not connected is disadvantageous in terms of strength and dimensional stability, but can be compensated for by using a high-quality material or by using large wall thicknesses d (10).
- the segments can have slight differences from one another, for example in the area of the fastening provisions, if their number does not correspond to the number of segments. corresponds, or in an inner area close to the axis, in which segmentation may be more difficult under certain circumstances.
- segmentation can be used advantageously to assemble inlet grilles 1 from several injection-molded segments, e.g. by clipping, locking, screwing, gluing, by fastening to the nozzle plate, or the like.
- segmentation can be used advantageously to assemble inlet grilles 1 from several injection-molded segments, e.g. by clipping, locking, screwing, gluing, by fastening to the nozzle plate, or the like.
- the central part can, however, be of a simple design, in particular even or flat.
- Fig.5 shows the inlet grille 1 according to the Fig. 1 to 4 in a side view and in section on a plane through the axis.
- the course of the basket-like contour of the inflow-side and outflow-side envelope surfaces 7 and 8 is clearly visible.
- the outer envelope surface 7 has an outer diameter D (20), which is also referred to as the diameter D (20) of the inflow grille 1, whereby the diameter of the fastening areas 18 is not taken into account here.
- the outer envelope surface 7 and inner envelope surface 8 run approximately parallel to one another in the exemplary embodiment.
- the distance between the envelope surfaces 7 and 8 is advantageously 6 mm to 18 mm or is approximately 3%-10% of the diameter D (20) of the inflow grille 1.
- the contour runs approximately parallel to the axis for a distance (cylinder jacket-like part 34).
- the transition region 24 has a small extension in the radial direction of less than 12.5% of the outer diameter D (20).
- the flat region 33 has a diameter DE (21) which is advantageously relatively large and has at least 75% of the value of the outer diameter D (20).
- the inflow grille 1 has an axial height H (22), with the cylinder jacket-like region on the outer envelope surface 7 has an axial extension of HZ(23). HZ (23) is advantageously larger than 6% of the diameter D (20).
- the basket-like contour of the inflow grille 1 or its envelope surfaces 7, 8 is well adapted in terms of flow conditions.
- air is expected to flow in more in a radial direction from the nozzle plate 32, which, due to the cylinder jacket-like shape of the grille 1 in this area 34, can pass through it approximately transversely to the envelope surfaces 7, 8 over a short path and thus with low flow losses.
- an axial inflow is expected, which then also flows through the grille 1 over a short path transversely to the envelope surfaces 7, 8.
- the compactly designed transition area 24 with a small extension enables a low installation height H (22) to be achieved, which is advantageous for a small space requirement of the inflow grille 1.
- the axial installation height H (22) is advantageously no greater than 25% of D (20).
- the targeted alignment of the webs can be clearly seen, which do not always run exactly perpendicular to the envelope surfaces, but are sometimes significantly different from this and optimally adapted to the exact inflow direction.
- the webs 5 are not curved in the flow direction. However, this is certainly conceivable in other embodiments.
- the outer ends 14 are open, i.e. not connected to one another (except at the fastening areas 18).
- Fig.6 shows another embodiment of an inflow grille 1 in a perspective view from the front (from the inflow side).
- the outer ends 14 of the webs 35 of the outer row are connected via an outer connecting ring 25.
- This increases the dimensional stability of the outer webs 35, which can be advantageous with regard to compliance with the requirements for contact protection, especially when softer or more elastic materials are used.
- the outer connecting ring 25 can also be advantageous for the filling behavior of an injection molding tool.
- the connecting ring 25 is connected to the webs 35 by means of a connection 27. This connection is designed as an extension area the outer webs 35 are designed in the form of a curve with a large curve radius > 3 mm.
- the fastening areas 18 are integrated into the connecting ring 25.
- the connecting ring 25 lies in a plane that represents the screw-on plane toward the nozzle 2 or the nozzle plate 32.
- the connecting ring 25 can run away from the fastening areas 35 and axially offset from the screw-on plane. This creates space between the nozzle 2 or the nozzle plate 32 and the connecting ring 25 when assembled. The presence of such space can be necessary for existing screw heads with which, for example, the nozzle 2 and the nozzle plate 32 can be screwed together, or in order to be able to position pressure extraction devices.
- the connecting ring runs axially offset from the screw-on plane in areas, some or all of the webs 35 of the outer row can protrude beyond this toward the nozzle 2 or the nozzle plate 32, or end at the connecting web 25 when viewed in the axial direction. Additional webs can also be attached in the area between the connecting web and the screw-on plane.
- the connecting ring 25 is interrupted in some areas and thus individual outer ribs 35 with open outer ends 14 are present. These outer ribs 35 with open outer ends 14 can also be shortened so that the outer ends 14 are at a distance from the screw-on plane. This can also serve to create space for screw heads, pressure tapping devices or the like between the screw-on plane and the inflow grille 1 in the assembled state.
- FIG.7 the inlet grille 1 is according to Fig.6 in axial plan view from behind (seen from the downstream side).
- the connecting ring 25 is located radially completely outside all webs 5, with the exception of the axially aligned webs 35 of the outer row with their connections 27 to the connecting ring 25.
- This is particularly advantageous for the demoldability of the grid 1 from a simple open-close injection molding tool. Examples are shown in Fig.7 four identical cells 26 of the grid 1, which is made up of four identical segments. Since the number of different cells is greatly reduced by such segmentation, the effort involved in the construction of the grille 1 and especially the associated injection molding tool.
- Fig.8 shows an inflow grille 1 in a perspective view from the front (from the inflow side).
- the cells 6 and the webs 5 are neither arranged in a honeycomb-like manner nor unstructured, but rather radially extending webs 5 are formed that run over the circumference.
- Four radially extending webs 5 meet in the central axis area at a central branching point 16.
- the number of webs 5 that meet per branching area 15 is mainly 4.
- the inflow grille 1 has a basket-like contour of the outer envelope surface 7. In this embodiment, no transition area is formed between the flat area 33 and the cylinder jacket-like area 34, but rather a "bend" that separates or connects these two areas.
- the webs 5a and 5b shown as examples have a large undercut area 17 with respect to a demolding direction parallel to the axis. Due to this large undercut area, demolding from a simple open-close injection molding tool parallel to the axis direction is not conceivable. Demolding is conceivable with slides that demold radially outwards in a star shape, which form the part of the grid 1 corresponding to the cylinder jacket-like part 34.
- Fig.9 the inlet grille 1 is according to Fig.8 shown in perspective view from behind (seen from the downstream side).
- the basket-like contour of the inner envelope surface 8 is clearly visible.
- Fig.10 the inlet grille 1 is in accordance with Fig.8 and 9 shown in axial plan view from the front (seen from the inflow side).
- Four identical cells 26 of the four-segmentation are shown as examples.
- the inlet grille 1 is in accordance with Fig. 8 to 10 shown in a side view and in section on a plane through the axis.
- the diameter D (20) of the grille 1 and the diameter DE (21) of the flat or level area 33 correspond, since no transition area is formed.
- the axial height H (22) of the grille 1 is slightly greater than the axial height HZ (23) of the cylindrical part, since the fastening areas 18 protrude axially to the right (towards the screw-on plane) beyond the grille. This means that in the assembled state, away from the fastening areas, there is a small distance between the nozzle 2 or the nozzle plate 32 and the grille 1 or the webs 35 of the outer row.
- This distance provides space, for example, for screw heads of screws that connect the nozzle 2 and the nozzle plate 32, or space for pressure tapping devices in the radius of the inlet nozzle 2.
- a similar design, according to which space is created between at least some outer grid webs 35 or also an outer connecting ring 25 and the nozzle 2 or the nozzle plate 32, is also possible for embodiments with unstructured grids similar to the Fig.1 until 7 and 12 until 16 conceivable. It is also conceivable in embodiments with unstructured grids that no transition areas are formed between the cylinder jacket-shaped area 34 and the flat or level area 33 of the inflow grid, but rather that they meet at a bend.
- FIG. 12 another embodiment of an inflow grille 1 according to the invention is shown in a side view and in section on a plane through the axis.
- the webs 5 in the exemplary embodiment are partially curved when viewed in section. This allows an even better adaptation of the grille 1 or the webs 5 to the inflow.
- advantages in terms of demoldability can be achieved with fixed, flow-favorable surface angles of the webs 5 on the inflow side (outer envelope surface 7).
- curved webs 5 a targeted, low-loss deflection of the inflow can be achieved if required. Any curvature (direction, amount) is conceivable.
- Curved webs 5 can also be axially aligned webs at the same time. For example, webs 35 of the outer row in particular can also be curved and axially aligned in this way.
- Fig. 13 shows a further embodiment of an inflow grille 1 according to the invention in a perspective view from the front (from the inflow side).
- the grille 1 is constructed in an unstructured manner, so that in the majority of cases 3 webs 5 meet at the branching areas 15.
- An outer connecting ring 25 is formed, via which the webs 35 of the outer row are connected to one another.
- the connections 27 of the outer webs 35 to the connecting ring 27 are designed as rounded areas with relatively large rounding radii in extension of the webs themselves.
- the connections 27 advantageously extend in the radial direction over a large part of the radial extent of the connecting ring 25 (over more than half of this area).
- Four fastening areas 18 are integrated into the course of the connecting ring 25.
- outer webs 35b which are located approximately centrally on the fastening areas 18 in the circumferential direction, are reduced in external diameter in order to gain access to the screw connection of the inflow grille to the fastening areas 18.
- These outer webs 35b, which are reduced in external diameter, are advantageously extended inwards in diameter in order to have the necessary stability and the necessary cross-section for the injection molding process (see also the web 35b of the outer row in the area of a fastening area 18 in Fig. 16 ).
- central injection area 28 is formed.
- the liquid plastic is injected centrally into this injection area 28 and is then distributed over this disk-like area into the webs 5.
- the innermost webs 5 have an inner end 31 at which they are connected to the central injection area 28.
- Fig. 14 the inlet grille 1 is according to Fig. 13 shown in an axial plan view from the front (seen from the inflow side).
- This embodiment is designed to be completely free of undercuts with regard to demoulding in the axial direction. This makes tool production significantly easier and guarantees a reliable injection moulding process with short cycle times.
- Two webs 5a and 5b are shown as an example, the position of which is coordinated with one another in such a way that they do not overlap one another, seen in this axial plan view. To achieve this, A close interaction of the course of the envelope surfaces 7 and 8, the choice of the web depths t (9), the position and the alignment of the webs must be observed, taking into account compliance with the contact protection regulations.
- axially aligned webs 29 prevents two axially non-aligned webs 30 from meeting at a branching area 15, the wall normal vectors of which, aligned in the same cell 6, have x components (axis-parallel components) with different signs.
- two axially non-aligned webs 30 often meet one axially aligned web 29, or three axially aligned webs 29.
- Other combinations occur less frequently.
- Axially aligned webs 29 are advantageously designed with draft angles in order to facilitate their demolding from an injection mold. In an injection mold, both sides of an axially aligned web are formed by the same tool part. The property "axially aligned" applies strictly speaking to a middle surface between the two sides of an axially aligned web 29.
- all webs 5 are designed as axially aligned webs 29.
- the tool can be designed in such a way that in the corresponding inner cells 6 with exclusively or predominantly axially aligned webs 29, no tool parting line runs diagonally through the cells, but the complete contour of the cells can be introduced into a tool part. This further facilitates tool production. Due to the axial inflow In the inner area close to the axis, this can be easily achieved without any major loss of efficiency or acoustics.
- the embodiment according to Figure 14 is made up of 12 identical segments, whereby the 12-fold rotational symmetry is locally interrupted by only 4 fastening areas 18.
- the number of different cells 6 is significantly reduced by segmentation with a high number of segments.
- the inflow grille 1 has a total of 312 cells 6, but due to the segmentation there are only 26 differently designed cells 6.
- Embodiments with 8 segments are also particularly advantageous.
- segmentation can also be used to produce an inflow grille 1 according to the invention in several parts, in particular in the case of larger outer diameters.
- Fig. 15 shows the embodiment according to Fig. 13 and 14 in a side view.
- the connection areas 27 of the outer webs 35 to the outer connecting ring 25 can be clearly seen.
- the connection area 27, which is designed here as a rounded area, can also be designed in a different way, for example as a chamfer.
- Fig. 16 is the embodiment according to Fig. 13 to 15 shown in a side view and in section on a plane through the axis.
- the exemplary webs 5a and 5b do not overlap when viewed in the axial direction.
- the connecting ring 25 does not overlap the web 5a when viewed in the axial direction. All of this is advantageous for a simple design of the injection molding tool, since undercuts between the webs 5a and 5b and the connecting ring 25 are avoided with regard to demolding parallel to the axial direction.
- the webs 35b of the outer row which are located in the area of the fastening areas 18, are adapted to the screws with which the inlet grille 1 is screwed to an inlet nozzle 2 or to a nozzle plate 32, and their outer diameter is reduced for better accessibility.
- these webs 35b are also at least slightly offset inwards in diameter.
- the central injection area 28 can be clearly seen in the section.
- the liquid plastic injected centrally in this area can be distributed well over the inner ends 31 onto the webs 5.
- the inner ends 31 are advantageously rounded with the central injection area 28 or provided with a chamfer.
- Fig. 17 shows an example of a fan with an inlet grille 1, a nozzle 2 which is attached to a nozzle plate 32, and a fan impeller 3 which is driven by a schematically shown motor.
- the air first flows through the inlet grille 1 into the inlet nozzle 2 before it experiences a total pressure increase as it flows through the rotating impeller 3 of the fan. Turbulence in the inflow causes increased noise in the fan.
- An inlet grille 1 according to the invention evens out the inflow and thus reduces the noise.
- the inlet grille 1 also takes on the function of a suction-side contact guard. The pressure loss which occurs when the air flows through the grille 1 is minimized by the advantageous design according to the invention.
- a diagonal fan 3 is shown in the exemplary embodiment.
- the inlet grille 1 can just as easily be used with a radial or axial fan.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Description
Die vorliegende Erfindung betrifft einen Ventilator (Axial-, Radial- oder Diagonalventilator) mit einem Laufrad und einer Vorleiteinrichtung im Strömungspfad vor dem Laufrad, vorzugsweise vor dem Einlaufbereich einer Einlaufdüse, wobei die Vorleiteinrichtung als Einströmgitter mitflächigen Stegen ausgeführt ist und wobei die Stege eine Vielzahl von gitterzellenartigen Strömungskanälen bilden. Des Weiteren betrifft die Erfindung eine besondere Vorleiteinrichtung, die im Sinne eines Einströmgitters mit flächigen Stegen ausgeführt ist.The present invention relates to a fan (axial, radial or diagonal fan) with an impeller and a guide device in the flow path in front of the impeller, preferably in front of the inlet area of an inlet nozzle, wherein the guide device is designed as an inflow grille with flat webs and wherein the webs form a plurality of grid-cell-like flow channels. Furthermore, the invention relates to a special guide device which is designed in the sense of an inflow grille with flat webs.
Ein gattungsbildender Ventilator mit zuströmseitiger Vorleiteinrichtung ist beispielsweise aus
Aus der Praxis sind auch bereits sogenannte Vorleiträder bekannt, die zur Begünstigung des Wirkungsgrads und/oder der Luftleistung dienen. Diese Vorleiträder bedingen jedoch akustische Nachteile und sind kompliziert im Aufbau sowie im Einbau in die jeweiligen Ventilatorprodukte. Sie werden regelmäßig vor Ventilatorlaufräder in einen zylindrischen Bauraum mit Durchmesser etwa des Ventilatorlaufrades eingebaut und haben somit, im Vergleich zum Ventilator, keine signifikativ größere Durchströmungsfläche. Dadurch sind die Luftgeschwindigkeiten im Bereich dieser Vorleiträder relativ hoch, was insbesondere die akustischen Nachteile bewirkt.So-called guide vanes are already known from practice, which serve to improve efficiency and/or air performance. However, these guide vanes have acoustic disadvantages and are complicated to construct and install in the respective fan products. They are usually installed in front of fan impellers in a cylindrical installation space with a diameter approximately the same as the fan impeller and therefore do not have a significantly larger flow area than the fan. As a result, the air speeds in the area of these guide vanes are relatively high, which in particular causes the acoustic disadvantages.
Grundsätzlich liegt der Erfindung das folgende technische Problem zugrunde.Basically, the invention is based on the following technical problem.
Ventilatoren reagieren auf gestörte Zuströmung häufig mit erhöhtem Lärm. In vielen Ventilatoranwendungen, beispielsweise bei der kontrollierten Wohnraumbelüftung (KWL), entstehen aus den regelmäßigen Kompaktheitsanforderungen zwangsweise gestörte Zuströmbedingungen. Der entstehende Lärm, der oft große tonale Anteile hat, ist regelmäßig niederfrequent. Insbesondere bei Lüftungsgeräten ist eine Lärmreduktion dieses niederfrequenten Lärms unabdingbar.Fans often react to disturbed air flow with increased noise. In many fan applications, for example in controlled residential ventilation (KWL), the regular compactness requirements inevitably result in disturbed inflow conditions. The resulting noise, which often has a large tonal component, is usually low-frequency. Noise reduction of this low-frequency noise is essential, particularly in ventilation devices.
Es ist auch bereits bekannt, den Lärm mit sogenannten Strömungsgleichrichtern bei gestörter Zuströmung maßgeblich zu reduzieren. Jedoch verursachen solche Strömungsgleichrichter nicht unerhebliche Druckverluste und benötigen obendrein großen Bauraum. Der vorliegenden Erfindung liegt daher die Aufgabe zugrunde, einen Ventilator derart auszugestalten und weiterzubilden, dass bei gestörter Zuströmung eine Schallreduktion stattfindet. Der Ventilator soll kompakt bauen und nur äußerst geringe Druckverluste haben. Außerdem soll eine Vorleiteinrichtung, insbesondere ein Einströmgitter bzw. Vorleitgitter angegeben werden, welches den voranstehenden Anforderungen genügt und welches mit wirtschaftlichem Werkzeugaufwand in Kunststoff-Spritzguss herstellbar ist. Es soll formstabil sein und vorteilhaft die Funktion eines anströmseitigen Berührschutzgitters übernehmen können.It is also already known to significantly reduce noise with so-called flow straighteners in the event of a disturbed inflow. However, such flow straighteners cause not inconsiderable pressure losses and also require a large amount of installation space. The present invention is therefore based on the task of designing and developing a fan in such a way that noise is reduced in the event of a disturbed inflow. The fan should be compact and have only extremely low pressure losses. In addition, a guide device, in particular an inflow grille or guide grille, should be specified which meets the above requirements and which can be manufactured using plastic injection molding with economical tooling. It should be dimensionally stable and be able to advantageously take on the function of an upstream contact protection grille.
Voranstehende Aufgabe ist in Bezug auf einen erfindungsgemäßen Ventilator durch alternative Merkmalskombinationen gemäß den Merkmalen der nebengeordneten Ansprüche 1 und 3 gelöst. In Bezug auf das erfindungsgemäße Einströmgitter ist die voranstehende Aufgabe durch die Merkmale des Anspruchs 10 gelöst, der auf die den Ventilator betreffenden Ansprüche Bezug nimmt.The above object is achieved with respect to a fan according to the invention by alternative feature combinations according to the features of the
Im Rahmen einer ersten Variante gemäß Anspruch 1 erstrecken sich die Stege ganz überwiegend zwischen vorzugsweise zwei Verzweigungen oder zwischen je einer Verzweigung in einem Randbereich. Je Verzweigung treffen sich vorzugsweise drei Stege. Mit diesen Merkmalen sind ganz besondere gitterzellenartige Strömungskanäle gebildet, die geeignet sind, bei gestörter Zuströmung den Lärm zu reduzieren.In a first variant according to
Der weiter nebengeordnete Anspruch 3 beansprucht eine weitere Alternative, wonach das Einströmgitter eine korbartige Kontur hat, wobei diese Ausgestaltung auf die äußere und/oder innere Hüllfläche des Einströmgitters bezogen ist.The further
Gleiches gilt für die Ausgestaltung des Einströmgitters selbst, welches mit dem weiter nebengeordneten Anspruch 10 unter Rückbezug auf die den Ventilator betreffenden Ansprüche definiert ist.The same applies to the design of the inlet grille itself, which is defined in the
Den nebengeordneten Ansprüchen liegt die grundsätzliche Idee zugrunde, ein Einströmgitter oder Zuströmgitter vor der Einlaufdüse eines Ventilators vorzusehen, um bei gestörter Zuströmung den beim Betrieb des Ventilators entstehenden Lärm zu reduzieren. Das Einströmgitter ist durch flächige Stege definiert, wobei die Stege derart zueinander angeordnet sind, dass gitterzellenartige Strömungskanäle entstehen. Durch die geschickte Kombination der Stege, die Verzweigungen und Knotenpunkte bilden, lassen sich vorteilhafte Geometrien realisieren, beispielsweise dahingehend, dass die Strömungskanäle einen wabenartigen Querschnitt haben. Der Begriff "wabenartig" ist im weitesten Sinne zu verstehen, so dass darunter auch Vielecke zu subsummieren sind, beispielsweise Gitterzellen mit 4-eckigem, 5-eckigem oder 6-eckigem bzw. mehreckigem Querschnitt.The underlying independent claims are the basic idea of providing an inflow grille or inlet grille in front of the inlet nozzle of a fan in order to reduce the noise generated when the fan is operating in the event of a disruption to the inflow. The inflow grille is defined by flat webs, whereby the webs are arranged in such a way that grid-cell-like flow channels are created. By cleverly combining the webs, which form branches and nodes, advantageous geometries can be realized, for example in that the flow channels have a honeycomb-like cross-section. The term "honeycomb-like" is to be understood in the broadest sense, so that it also includes polygons, for example grid cells with a square, five-sided or hexagonal or polygonal cross-section.
Entsprechend den zuvor erörterten gitterzellenartigen Strömungskanälen ist es von weiterem Vorteil, dass das Einströmgitter eine korbartige Kontur hat, wobei sich die Kontur sowohl auf die äußere als auch auf die innere Hüllfläche des Einströmgitters beziehen kann.According to the previously discussed grid cell-like flow channels, it is further advantageous that the inflow grille has a basket-like contour, whereby the contour can refer to both the outer and the inner envelope surface of the inflow grille.
Ein Einströmgitter der zuvor genannten Art wird der radialen Zuströmung im Bereich nahe der Düsenplatte gerecht. Die Strömungskanäle wirken sich vorteilhaft auf niedrige Druckverluste aus. Die korbartige Außenkontur ist obendrein vorteilhaft für die Entformbarkeit im Rahmen einer vor allem bei Kunststoffteilen anzuwendenden Spritzgießtechnik. Außerdem lassen sich kompakte Gitter mit den entsprechenden Eigenschaften herstellen.An inflow grille of the type mentioned above is suitable for the radial inflow in the area close to the nozzle plate. The flow channels have a beneficial effect on low pressure losses. The basket-like outer contour is also advantageous for demoldability in the context of an injection molding technique that is used primarily for plastic parts. In addition, compact grilles with the corresponding properties can be produced.
Ganz besonders vorteilhaft ist die korbartige Außenkontur, wenn diese stetig und gekrümmt ist. Die Gitterstege sollen möglichst dünn ausgeführt sein, beispielsweise im Bereich von 0,25 mm bis 1 mm Stegdicke. In Durchströmrichtung sollten sie eine Tiefe von mindestens 5 mm haben (daher der in den Ansprüchen gewählte Begriff "flächiger Steg").The basket-like outer contour is particularly advantageous if it is continuous and curved. The grid webs should be as thin as possible, for example in the range of 0.25 mm to 1 mm web thickness. In the direction of flow they should have a depth of at least 5 mm (hence the term "flat web" chosen in the claims).
Weiter vorteilhaft bilden die Gitterstege ein nicht strukturiertes Gitter, bei dem wabenartige Gitterzellen miteinander kombiniert sind. Wie bereits zuvor ausgeführt, können die Gitterzellen mehreckig und dabei miteinander bzw. untereinander kombiniert sein. Es lässt sich so eine minimale Versperrung durch Gitterstege erreichen, insbesondere dann, wenn eine gewisse maximale Gitterweite aufgrund der benötigten Lärmreduktion oder unter Berücksichtigung von Berührschutzaspekten nötig ist, was zu niedrigen Druck- und Wirkungsgradverlusten führt.Another advantage is that the grid bars form a non-structured grid in which honeycomb-like grid cells are combined with one another. As already mentioned, the grid cells can be polygonal and combined with one another or with one another. This allows minimal obstruction by grid bars to be achieved, particularly when a certain maximum grid width is necessary due to the required noise reduction or taking into account contact protection aspects, which leads to low pressure and efficiency losses.
Das Einströmgitter erstreckt sich in weiter vorteilhafter Weise über den gesamten Bereich bis zur gedachten Verlängerung der Ventilatorachse, weist also im inneren Bereich keine oder keine besonders große Öffnung auf. Eine solche mittige Öffnung ist im Lichte der erfindungsgemäßen Lehre nicht nötig, ja sogar zu vermeiden, sofern das Einströmgitter zusätzlich einen Berührschutz erfüllt. Außerdem hat man herausgefunden, dass eine mittige Öffnung einer Geräuschminimierung und Stabilität des Gitters entgegensteht.The inlet grille advantageously extends over the entire area up to the imaginary extension of the fan axis, so it has no or no particularly large opening in the inner area. In light of the teaching of the invention, such a central opening is not necessary, and can even be avoided, provided the inlet grille also provides protection against contact. It has also been found that a central opening is detrimental to minimizing noise and improving the stability of the grille.
Von besonderem Vorteil ist jedenfalls die besondere Ausgestaltung des Einströmgitters, nicht nur in Bezug auf die gitterzellenartigen Strömungskanäle, auch in Bezug auf die stetige und gekrümmte Außenkontur. Durch Wabenelemente mit 4, 5 oder 6 Ecken lassen sich unstrukturierte Gitter realisieren, wobei variable Gitterweiten über das gesamte Einströmgitter hinweg realisierbar sind, je nach Bedarf.The special design of the inflow grille is particularly advantageous, not only in terms of the grid-like flow channels, but also in terms of the continuous and curved outer contour. Honeycomb elements with 4, 5 or 6 corners allow unstructured grilles to be created, with variable grille widths being possible across the entire inflow grille, depending on requirements.
Das erfindungsgemäße Einströmgitter dient zur Anwendung in einem Axial-, Radial- oder Diagonalventilator und ist entsprechend den voranstehenden Ausführungen konstruiert.The inlet grille according to the invention is intended for use in an axial, radial or diagonal fan and is constructed in accordance with the above statements.
Es gibt nun verschiedene Möglichkeiten, die Lehre der vorliegenden Erfindung in vorteilhafter Weise auszugestalten und weiterzubilden. Dazu ist einerseits auf die dem Anspruch 1 nachgeordneten Ansprüche und andererseits auf die nachfolgende Erläuterung bevorzugter Ausführungsbeispiele eines erfindungsgemäßen Einströmgitters anhand der Zeichnung zu verweisen. In Verbindung mit der Erläuterung der bevorzugten Ausführungsbeispiele der Erfindung anhand der Zeichnung werden auch im Allgemeinen bevorzugte Ausgestaltungen und Weiterbildungen der Lehre erläutert. In der Zeichnung zeigen
- Fig. 1
- in perspektivischer Ansicht von der Zuströmseite aus gesehen ein Ausführungsbeispiel eines erfindungsgemäßen Einströmgitters,
- Fig. 1a
- in perspektivischer Ansicht eine schematische Detaildarstellung einer aus Stegen aufgebauten Zelle gemäß
Fig. 1 , wobei charakteristische Abmessungen der Stege und Zellen gekennzeichnet sind, - Fig. 2
- in perspektivischer Ansicht von der Abströmseite aus gesehen, das Einströmgitter aus
Fig. 1 , - Fig. 3
- in axialer Draufsicht, von der Zuströmseite aus gesehen, das Einströmgitter aus
Fig. 1 und2 , - Fig. 4
- in axialer Draufsicht, von der Abströmseite aus gesehen, das Einströmgitter aus
Fig. 1 bis 3 , - Fig. 5
- in einer Seitenansicht und im Schnitt an einer Ebene durch die Achse das Einströmgitter gemäß
Fig. 1 bis 4 , wobei charakteristische Abmessungen des Einströmgitters eingezeichnet sind, - Fig. 6
- in perspektivischer Ansicht von der Zuströmseite aus gesehen ein weiteres Ausführungsbeispiel eines erfindungsgemäßen Einströmgitters,
- Fig. 7
- in axialer Draufsicht, von der Abströmseite aus gesehen, das Einströmgitter aus
Fig. 6 , - Fig. 8
- in perspektivischer Ansicht von der Zuströmseite aus gesehen ein weiteres Ausführungsbeispiel eines Einströmgitters,
- Fig. 9
- in perspektivischer Ansicht von der Abströmseite aus gesehen, das Einströmgitter aus
Fig. 8 , - Fig. 10
- in axialer Draufsicht, von der Zuströmseite aus gesehen, das Einströmgitter aus
Fig. 8 und 9 , - Fig. 11
- in einer Seitenansicht und im Schnitt an einer Ebene durch die Achse das Einströmgitter gemäß
Fig. 8 , wobei charakteristische Abmessungen des Einströmgitters eingezeichnet sind,bis 10 - Fig. 12
- in einer Seitenansicht und im Schnitt an einer Ebene durch die Achse ein weiteres Beispiel eines erfindungsgemäßen Einströmgitters mit gekrümmten Stegen,
- Fig. 13
- in perspektivischer Ansicht von der Zuströmseite aus gesehen ein weiteres Ausführungsbeispiel eines erfindungsgemäßen Einströmgitters mit einem zentralen, geschlossenen Anspritzbereich,
- Fig. 14
- in axialer Draufsicht, von der Zuströmseite aus gesehen, das Einströmgitter aus
Fig. 13 , - Fig. 15
- in einer Seitenansicht das Einströmgitter gemäß
Fig. 13 ,und 14 - Fig. 16
- in einer Seitenansicht und im Schnitt an einer Ebene durch die Achse das Einströmgitter gemäß
Fig. 13 ,bis 15 - Fig. 17
- in perspektivischer, schematischer Ansicht von der Zuströmseite aus gesehen und geschnitten an einer Ebene durch die Achse einen Ventilator mit Motor, Laufrad, Einlaufdüse, einer Düsenplatte und dem Einströmgitter gemäß
Fig. 13 .bis 16
- Fig.1
- in perspective view from the inflow side an embodiment of an inflow grille according to the invention,
- Fig. 1a
- in perspective view a schematic detailed representation of a cell constructed from webs according to
Fig.1 , where characteristic dimensions of the webs and cells are marked, - Fig. 2
- in perspective view from the downstream side, the inlet grille made of
Fig.1 , - Fig.3
- in axial plan view, seen from the inflow side, the inflow grille made of
Fig.1 and2 , - Fig.4
- in axial plan view, seen from the downstream side, the inlet grille made of
Fig. 1 to 3 , - Fig.5
- in a side view and in section on a plane through the axis the inlet grille according to
Fig. 1 to 4 , where characteristic dimensions of the inlet grille are shown, - Fig.6
- in perspective view from the inflow side, another embodiment of an inflow grille according to the invention,
- Fig.7
- in axial plan view, seen from the downstream side, the inlet grille made of
Fig.6 , - Fig.8
- in perspective view from the inflow side another embodiment of an inflow grille,
- Fig.9
- in perspective view from the downstream side, the inlet grille made of
Fig.8 , - Fig.10
- in axial plan view, seen from the inflow side, the inflow grille made of
Fig.8 and9 , - Fig. 11
- in a side view and in section on a plane through the axis the inlet grille according to
Fig. 8 to 10 , where characteristic dimensions of the inlet grille are shown, - Fig. 12
- in a side view and in section on a plane through the axis another example of an inflow grille according to the invention with curved webs,
- Fig. 13
- in perspective view from the inflow side, another embodiment of an inflow grille according to the invention with a central, closed injection area,
- Fig. 14
- in axial plan view, seen from the inflow side, the inflow grille made of
Fig. 13 , - Fig. 15
- in a side view the inlet grille according to
Fig. 13 and 14 , - Fig. 16
- in a side view and in section on a plane through the axis the inlet grille according to
Fig. 13 to 15 , - Fig. 17
- in perspective, schematic view seen from the inflow side and cut on a plane through the axis, a fan with motor, impeller, inlet nozzle, a nozzle plate and the inflow grille according to
Fig. 13 to 16 .
Das Einströmgitter 1 besteht aus einer Vielzahl an Stegen 5, welche Gitterzellen 6 definieren. Die Gitterzellen 6 werden im Betrieb des Ventilators durchströmt, das heißt sie bilden Strömungskanäle. Die zuströmende Luft weist in einem Bereich vor einer Einlaufdüse 2 niedrigere Geschwindigkeit auf als im Inneren einer Einlaufdüse 2, da die durchströmte Fläche für den vom Ventilator geförderten Luftmassenstrom in einem Bereich vor einer Einlaufdüse 2 größer ist als in einer Einlaufdüse 2. Das Einströmgitter 1 wird in einem solchen Bereich eher niedriger Strömungsgeschwindigkeiten eingesetzt, d.h. die Durchströmgeschwindigkeit beim Einströmgitters 1 ist niedriger als die Durchströmgeschwindigkeit in der Einlaufdüse 2. Dadurch werden Strömungsverluste und Lärmentstehung am Einströmgitter 1 gering gehalten.The
Da allerdings die Zuströmung in einem Bereich vor einer Einlaufdüse 2 nicht eben bzw. nicht überwiegend parallel zur Achse ist, ist es von großem Vorteil, auch die Kontur des Einströmgitters 1 nicht komplett eben auszuführen. Die Kontur kann etwa beschrieben werden durch die äußere Hüllfläche 7 und/oder die innere Hüllfläche 8 (
Für einen niedrigen Druck- und Wirkungsgradverlust ist eine möglichst niedrige Versperrung der durchströmten Fläche durch die Gitterstege 5 vorteilhaft. Dies kann durch dünne Stege (Stegdicke d (10) vorteilhaft überwiegend <= 2 mm [<=1 mm]) erreicht werden und/oder durch eine Minimierung der Gesamtsteglänge (Summe aller Steglängen I (11) eines Einströmgitters (1). Die Steglängen I werden anhand der neutralen Fasern 13 bestimmt, vorteilhaft auf der äußeren oder inneren Hüllfläche 7 bzw. 8). Eine "unstrukturierte" Gitterstruktur mit wabenartigen Zellen 6 wie im Ausführungsbeispiel kann unter den beschriebenen Bedingungen an die maximale Gitterweite w (12) sehr vorteilhaft für die benötigte Gesamtsteglänge sein.For a low pressure and efficiency loss, it is advantageous to block the flow area as little as possible by the
In
In der Ansicht gemäß
In
Die Befestigungsbereiche 18 sind im Zusammenspiel mit den Gitterstegen 5 derart gestaltet, dass ihre Entformung aus einem Spritzgießwerkzeug hinterschnittfrei in einer Schieberrichtung parallel zur Achse (entspricht der Blickrichtung in dieser Darstellung) möglich ist. Man kann erkennen, dass die Gitterstege 5 teilweise nicht parallel zur Mittelachse (=Blickrichtung) ausgerichtet sind, sondern vielmehr in ihrer Ausrichtung optimal an die Zuströmverhältnisse angepasst sind. Die Stege können vorteilhaft auch eine Krümmung aufweisen, um die Strömung optimal zu leiten. Beispielhaft ist ein Steg 29 markiert, welcher ein axial fluchtender Steg ist, d.h. er ist parallel zur Achse (Blick- und Schieberrichtung) ausgerichtet, was dessen Entformung erleichtert. Axial fluchtende Stege 29 werden vorteilhaft mit einer Entformschräge versehen. Es gibt allerdings auch axial nicht fluchtende Stege 30, 30a, da alle Stege 5 möglichst optimal an die Strömungsrichtungen angepasst sind. Die beiden radial äußersten Reihen an Gitterstegen 5, die etwa in Umfangsrichtung verlaufen, verlaufen im Übergangsbereich 24 der Hüllflächen 7 oder 8 und sind so aufeinander abgestimmt, dass nur geringe oder keine Hinterschneidungsbereiche entstehen, d.h. sie verdecken sich, in Achsrichtung gesehen, nicht oder nur geringfügig. Im dargestellten Ausführungsbeispiel besteht beispielhaft ein geringer Hinterschneidungsbereich 17 im Zusammenspiel des Steges 5a der radial äußersten Reihe an Stegen 5 und des Steges 5b der zweiten Reihe an Stegen 5, da diese beiden Stege in Blickrichtung einen geringen Überdeckungsbereich aufweisen. Bei Wahl eines geeigneten eher elastischen Werkstoffes können geringe Hinterschneidungen realisiert und dennoch mit einem einfachen Auf-Zu-Werkzeug in Achsrichtung entformt werden. Dadurch lässt sich eine strömungstechnisch besonders optimierte Kontur einfach und wirtschaftlich realisieren. Weiterhin besteht ein geringfügiger Hinterschneidungsbereich im Verzweigungsbereich 15 zwischen den beiden axial nicht fluchtenden Stegen 30 und 30a, da die x-Komponente derer Flächennormalenvektoren ein unterschiedliches Vorzeichen aufweist. Auch diese geringfügige Hinterschneidung kann bei Wahl eines geeigneten Werkstoffes mit einem einfachen Auf-Zu-Werkzeug entformt werden.The
In diesem Ausführungsbeispiel sind die Zellen im achsnahen Bereich kleiner als diejenigen in einem achsfernen Bereich. Die Zellgröße bzw. Zellweite w (12, siehe
Gemäß
Das Einströmgitter 1 im Ausführungsbeispiel ist aus vier identischen Segmenten bestehend ausgeführt. Dies stellt einen erheblichen Vorteil vor allem bei der Konstruktion des Bauteiles und des für die Fertigung benötigten Werkzeugs dar, da die Zahl der unterschiedlich gestalteten Gitterzellen 6 dadurch um den Faktor 4 (Faktor=Zahl der Segmente) reduziert ist. Das Strömungsbild ist infolge dieser Segmentierung unabhängig von der Ausrichtung (Quadrant) des Einströmgitters 1 bei der Montage. Es ist auch eine andere Zahl an Segmenten möglich. Die Segmente können geringfügige Unterschiede voneinander aufweisen, beispielsweise im Bereich der Befestigungsvorkehrungen, falls deren Zahl nicht der Segmentzahl entspricht, oder in einem achsnahen Innenbereich, in dem sich eine Segmentierung unter Umständen schwieriger gestalten kann. Insbesondere bei großen Außendurchmessern kann eine Segmentierung vorteilhaft dazu genutzt werden, dass Einströmgitter 1 aus mehreren spritzgegossenen Segmenten zusammengefügt werden, z.B. durch Klipsen, Einrasten, Schrauben, Kleben, über die Befestigung an der Düsenplatte, oder dergleichen. Bei diesem mehrteiligen Ansatz ist es auch denkbar, neben den eigentlichen identischen Segmenten ein separates, unterschiedliches, zentrales Teil zu realisieren, das dann allerdings ein eigenes Spritzgießwerkzeug erfordert. Das zentrale Teil kann jedoch einfach gestaltet sein, insbesondere eben bzw. flach.The
Im gezeigten Ausführungsbeispiel befindet sich im Zentrum, auf der Achse, ein zentraler Verzweigungspunkt 16 von 4 (=Zahl der Segmente im Ausführungsbeispiel) Stegen 5.In the embodiment shown, there is a central branching
Die korbartige Kontur des Einströmgitters 1 bzw. deren Hüllflächen 7, 8 ist hinsichtlich der Strömungsverhältnisse gut angepasst. Im zylindermantelartigen Bereich 34 ist eine eher in radialer Richtung von der Düsenplatte 32 her einströmende Luft zu erwarten, die infolge der zylindermantelartigen Form des Gitters 1 in diesem Bereich 34 dieses etwa quer zu den Hüllflächen 7, 8 auf kurzem Wege und somit mit geringen Strömungsverlusten passieren kann. Im flachen bzw. ebenen Bereich 33 ist eher eine axiale Zuströmung zu erwarten, die dann ebenfalls quer zu den Hüllflächen 7,8 das Gitter 1 auf kurzem Wege durchströmt. Durch den kompakt gestalteten, eine geringe Erstreckung aufweisenden Übergangsbereich 24 kann eine geringe Bauhöhe H (22) erreicht werden, was vorteilhaft für einen niedrigen Platzbedarf des Einströmgitters 1 ist. Vorteilhaft ist die axiale Bauhöhe H (22) nicht größer als 25% von D (20).The basket-like contour of the
Weiterhin ist gut die gezielte Ausrichtung der Stege zu erkennen, die nicht immer genau senkrecht zu den Hüllflächen verlaufen, sondern davon teilweise deutlich abweichend der genauen Zuströmrichtung optimal angepasst ist. Im Ausführungsbeispiel sind die Stege 5 in Durchströmrichtung nicht gekrümmt. Dies ist bei anderen Ausführungsformen aber durchaus denkbar. Bei den radial äußeren Stegen 35 sind die äußeren Enden 14 offen, das heißt nicht miteinander verbunden (außer an den Befestigungsbereichen 18).Furthermore, the targeted alignment of the webs can be clearly seen, which do not always run exactly perpendicular to the envelope surfaces, but are sometimes significantly different from this and optimally adapted to the exact inflow direction. In the exemplary embodiment, the
Im Ausführungsbeispiel liegt der Verbindungsring 25 in einer Ebene, die die Anschraubebene hin zur Düse 2 bzw. zur Düsenplatte 32 darstellt. Bei anderen vorteilhaften Ausführungsformen kann der Verbindungsring 25 abseits der Befestigungsbereiche 35 axial versetzt zur Anschraubebene verlaufen. Dadurch entsteht im montierten Zustand Platz zwischen der Düse 2 bzw. der Düsenplatte 32 und dem Verbindungsring 25. Das Vorhandensein eines solchen Platzes kann nötig sein für vorhandene Schraubenköpfe, mit welchen beispielsweise die Düse 2 und die Düsenplatte 32 verschraubt sein können, oder um Druckentnahmeeinrichtungen platzieren zu können. Verläuft der Verbindungsring in Bereichen axial versetzt zur Anschraubebene, können einige oder alle Stege 35 der äußeren Reihe über diesen hin zur Düse 2 bzw. zur Düsenplatte 32 hinausstehen, oder in Axialrichtung gesehen am Verbindungssteg 25 enden. Es können im Bereich zwischen Verbindungssteg und Anschraubebene auch weitere Stege angebracht sein. Bei anderen Ausführungsformen ist es auch denkbar, dass der Verbindungsring 25 bereichsweise unterbrochen ist und somit einzelne äußere Rippen 35 mit offenen äußeren Enden 14 vorhanden sind. Diese äußeren Rippen 35 mit offenen äußeren Enden 14 können auch verkürzt sein, sodass die äußeren Enden 14 mit Abstand zur Anschraubebene liegen. Auch dies kann dazu dienen, im montierten Zustand Platz für Schraubenköpfe, Druckentnahmeeinrichtungen oder ähnlichem zwischen Anschraubebene und Einströmgitter 1 zu schaffen.In the exemplary embodiment, the connecting
In
Die beispielhaft gezeigten Stege 5a und 5b weisen einen großen Hinterschneidungsbereich 17 bezüglich einer Entformrichtung parallel zur Achse auf. Aufgrund dieses großen Hinterschneidungsbereiches ist eine Entformung aus einem einfachen Auf-Zu-Spritzgießwerkzeug parallel zur Achsrichtung nicht denkbar. Eine Entformung ist mit sternförmig radial nach außen entformenden Schiebern denkbar, die den zum zylindermantelartigen Teil 34 korrespondierenden Teil des Gitters 1 ausbilden.The
In
In
In
In
Bei der Ausführungsform gemäß
In
Um Hinterschneidungsbereiche nahe von Verzweigungsbereichen 15 zu vermeiden, wird es unter Verwendung von axial fluchtenden Stegen 29 vermieden, dass sich an einem Verzweigungsbereichen 15 zwei axial nicht fluchtende Stege 30 treffen, deren in dieselbe Zelle 6 ausgerichteten Wandnormalenvektoren x-Komponenten (achsparallele Komponenten) mit unterschiedlichen Vorzeichen haben. Infolgedessen treffen bei einem Verzweigungsbereich 15 im Ausführungsbeispiel häufig 2 axial nicht fluchtende Stege 30 auf einen axial fluchtenden Steg 29, oder drei axial fluchtende Stege 29. Andere Kombinationen treten seltener auf. Axial fluchtende Stege 29 werden vorteilhaft mit Entformungsschrägen ausgeführt, um deren Entformung aus einem Spritzgießwerkzeug zu erleichtern. In einem Spritzgießwergzeug werden beide Seiten eines axial fluchtenden Steges von demselben Werkzeugteil ausgebildet. Die Eigenschaft "axial fluchtend" trifft genau genommen auf eine mittlere Fläche zwischen den beiden Seiten eines axial fluchtenden Steges 29 zu.In order to avoid undercut areas close to branching
Um ein komplett hinterschneidungsfreies Gitter zu gestalten, müssen unter Umständen Einschränkungen bei Akustik und Wirkungsgrad hingenommen werden. Je nach Gegebenheiten kann es auch sinnvoll sein, geringfügige Hinterschneidungen zu akzeptieren, die dann dennoch mit einem einfachen Werkzeug entformt werden können (Zwangsentformung, Drehbewegung von Werkzeugteilen, Abbildung von Bauteilkonturbereichen auf Auswerfern o.ä.).In order to design a grille that is completely free of undercuts, it may be necessary to accept limitations in terms of acoustics and efficiency. Depending on the circumstances, it may also make sense to accept minor undercuts that can then still be demolded using a simple tool (forced demolding, rotary movement of tool parts, mapping of component contour areas on ejectors, etc.).
Im Ausführungsbeispiel sind in einem radial inneren Bereich, etwa ab einem bestimmten Grenzradius, alle Stege 5 als axial fluchtende Stege 29 ausgebildet. Infolgedessen kann das Werkzeug so gestaltet werden, dass bei den entsprechenden inneren Zellen 6 mit ausschließlich oder überwiegend axial fluchtenden Stegen 29 keine Werkzeugtrennlinie schräg durch die Zellen verläuft, sondern die vollständige Kontur der Zellen in ein Werkzeugteil eingebracht werden kann. Dies erleichtert die Werkzeugherstellung weiter. Aufgrund der axialen Zuströmung im inneren, achsnahen Bereich ist dies ohne größere Wirkungsgrad- oder Akustikeinbußen gut realisierbar.In the exemplary embodiment, in a radially inner area, approximately from a certain limit radius, all
Die Ausführungsform gemäß
Bei der Ausbildung von vier Befestigungsbereichen 18 ist vorteilhaft die Zahl der Segmente ein Vielfaches von 4. Eine Segmentierung kann auch genutzt werden, um ein erfindungsgemäßes Einströmgitter 1, insbesondere bei größeren Außendurchmessern, mehrteilig herzustellen.When forming four
In
Der zentrale Anspritzbereich 28 ist im Schnitt gut zu erkennen. Im Spritzgießprozess kann sich der zentral an diesem Bereich eingespritzte flüssige Kunststoff über die inneren Enden 31 auf die Stege 5 gut verteilen. Die inneren Enden 31 sind dabei vorteilhaft mit dem zentralen Anspritzbereich 28 verrundet bzw. mit einer Fase versehen.The
Hinsichtlich weiterer vorteilhafter Ausgestaltungen der erfindungsgemäßen Lehre wird zur Vermeidung von Wiederholungen auf den allgemeinen Teil der Beschreibung sowie auf die beigefügten Ansprüche verwiesen.With regard to further advantageous embodiments of the teaching according to the invention, reference is made to the general part of the description and to the appended claims in order to avoid repetition.
Schließlich sei ausdrücklich darauf hingewiesen, dass die voranstehend beschriebenen Ausführungsbeispiele der erfindungsgemäßen Lehre lediglich zur Erörterung der beanspruchten Lehre dienen, diese jedoch nicht auf die Ausführungsbeispiele einschränken. Die Erfindung wird durch die beigefügten Ansprüche begrenzt.Finally, it should be expressly pointed out that the exemplary embodiments of the teaching according to the invention described above serve only to explain the claimed teaching, but do not restrict it to the exemplary embodiments. The invention is limited by the appended claims.
- 11
- EinströmgitterInflow grille
- 22
- EinlaufdüseInlet nozzle
- 33
- VentilatorlaufradFan impeller
- 44
- MotorMotor
- 5, 5a, 5b5, 5a, 5b
- Stegweb
- 66
- Gitterzelle, StrömungskanalGrid cell, flow channel
- 77
- äußere, zuströmseitige Hüllflächeouter, inflow-side envelope
- 7a7a
- äußere, zuströmseitige Stirnfläche der Stegeouter, inflow-side face of the webs
- 88
- innere Hüllflächeinner envelope
- 8a8a
- innere, ausströmseitige Stirnfläche der Stegeinner, outflow-side face of the webs
- 99
- Stegtiefe tBridge depth t
- 1010
- Stegdicke dWeb thickness d
- 1111
- Steglänge IBridge length I
- 1212
- Zellweite w, InkugelradiusCell width w, insphere radius
- 1313
- neutrale Faser eines Stegesneutral fiber of a bridge
- 1414
- äußeres Ende eines Steges, Randbereichouter end of a web, edge area
- 1515
- Verzweigungsbereich von StegenBranching area of webs
- 1616
- zentraler Verzweigungspunkt von Stegencentral branching point of bridges
- 1717
- HinterschneidungsbereichUndercut area
- 1818
- BefestigungsbereichMounting area
- 1919
- Zelle der äußeren ReiheCell of the outer row
- 2020
- Durchmesser D des GittersDiameter D of the grid
- 2121
- Durchmesser DE des flachen bzw. ebenen GitterteilesDiameter DE of the flat or level grid part
- 2222
- axiale Höhe H des Gittersaxial height H of the grid
- 2323
- axiale Höhe HZ des zylindermantelartigen Teilsaxial height HZ of the cylinder jacket-like part
- 2424
- Übergangsbereich der HüllflächeTransition area of the envelope
- 2525
- äußerer Verbindungsringouter connecting ring
- 2626
- identische Zellen einer Segmentierungidentical cells of a segmentation
- 2727
- Anbindung des VerbindungsringsConnection of the connecting ring
- 2828
- Geschlossener, zentraler AnspritzbereichClosed, central injection area
- 2929
- axial fluchtender Stegaxially aligned web
- 30,30a30,30a
- axial nicht fluchtender Stegaxially non-aligned web
- 3131
- inneres Ende eines Steges (Randbereich)inner end of a web (edge area)
- 3232
- DüsenplatteNozzle plate
- 3333
- flacher bzw. ebener Bereich des Einströmgittersflat or level area of the inlet grille
- 3434
- Zylindermantelartiger Bereich des EinströmgittersCylinder shell-like area of the inflow grille
- 3535
- Steg der äußeren ReiheBridge of the outer row
- 35b35b
-
Steg der äußeren Reihe im Bereich eines Befestigungsbereichs 18Web of the outer row in the area of a
fastening area 18
Claims (10)
- Axial, radial or diagonal fan, having an impeller and a preliminary guide device in the flow path in front of the inlet region of an inlet nozzle, wherein the preliminary guide device is in the form of an inflow grid (1) with planar webs (5), wherein the webs (5) form a large number of cells (6) with grid-cell-like flow channels, wherein the cells (6) at least partially have a honeycomb-like cross-section, wherein the cells (6) as a result of different cell contours are formed by regular and/or irregular squares and/or pentagons and/or hexagons,
characterised in that the webs comprise axially aligned webs and axially non-aligned webs, wherein in at least one branch region two axially non-aligned webs meet on at least one axially aligned web. - Fan (axial, radial or diagonal fan) according to claim 1, characterised in that the cells (6) in the region close to the axis are smaller than those in the region remote from the axis.
- Axial, radial or diagonal fan having an impeller and a preliminary guide device in the flow path in front of the impeller, preferably in front of the inlet region of an inlet nozzle, wherein the preliminary guide device is in the form of an inflow grid (1) having planar webs (5), wherein the webs (5) form a large number of grid-cell-like flow channels (6), and wherein the inflow grid has a basket-like contour (outer and/or inner enveloping surface) which has a cylinder-covering-like outer region (34) and a planar region (33) close to the axis,
characterised in that the webs comprise axially aligned webs and axially non-aligned webs, wherein in at least one branch region two axially non-aligned webs meet on at least one axially aligned web. - Fan according to claims 1 to 3, characterised in that a region free from webs (5) is formed at the centre of the inflow grid (1), that is to say, without flow channels (6).
- Fan according to any one of claims 1 to 4, characterised in that the webs (5) have a web thickness in the range from 0.25 mm to 2 mm.
- Fan according to any one of claims 1 to 5, characterised in that a region close to the axis of the contour extends in a level or very planar manner, substantially orthogonally with respect to the centre axis.
- Fan according to any one of claims 1 to 6, characterised in that an outer edge region of the inner contour extends substantially parallel with the centre axis, approximately on a notional cylinder covering.
- Fan according to any one of claims 1 to 7, characterised in that the inflow grid (1) has in an outer edge region securing means which are preferably integral with some of the webs (5) and which are used for positive-locking and/or non-positive-locking securing on the inlet nozzle (2) or the nozzle plate (32) of the fan.
- Fan according to any one of claims 1 to 8, characterised in that there is formed on the edge region of the inflow grid (1) a stabilisation ring which preferably comprises securing means which are used for positive-locking and/or non-positive-locking securing on the inlet nozzle (2) or the nozzle plate (32) of the fan.
- Inflow grid having features according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SI201930866T SI3775571T1 (en) | 2018-04-09 | 2019-02-15 | Fan and inflow grille for a fan |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102018205300.6A DE102018205300A1 (en) | 2018-04-09 | 2018-04-09 | Fan and inflow grille for a fan |
| PCT/DE2019/200013 WO2019196992A1 (en) | 2018-04-09 | 2019-02-15 | Fan and inflow grille for a fan |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP3775571A1 EP3775571A1 (en) | 2021-02-17 |
| EP3775571B1 true EP3775571B1 (en) | 2024-09-25 |
Family
ID=66041085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19715390.1A Active EP3775571B1 (en) | 2018-04-09 | 2019-02-15 | Fan and inflow grille for a fan |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US11703065B2 (en) |
| EP (1) | EP3775571B1 (en) |
| JP (2) | JP2021519885A (en) |
| KR (1) | KR102795830B1 (en) |
| CN (1) | CN112262261B (en) |
| DE (1) | DE102018205300A1 (en) |
| ES (1) | ES3001091T3 (en) |
| SI (1) | SI3775571T1 (en) |
| WO (1) | WO2019196992A1 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207795691U (en) * | 2018-01-13 | 2018-08-31 | 广东美的环境电器制造有限公司 | A kind of axial flow blower ducting assembly |
| CN110985444B (en) * | 2020-01-06 | 2022-04-19 | 北京航天奥祥通风科技股份有限公司 | Fan and fan assembly |
| KR102350103B1 (en) * | 2020-03-19 | 2022-01-11 | 케이비오토텍 주식회사 | Blower for vehicle seat |
| JP7629303B2 (en) * | 2021-01-06 | 2025-02-13 | 株式会社マキタ | Blower |
| EP4042861B1 (en) * | 2021-02-12 | 2023-12-20 | Andreas Stihl AG & Co. KG | Protection device for a suction or blowing channel of a working device and working device with a protective device |
| CN217421645U (en) * | 2022-03-03 | 2022-09-13 | 阳光电源股份有限公司 | Cowl and fan device |
| EP4245999A1 (en) * | 2022-03-18 | 2023-09-20 | Mann+Hummel Life Sciences & Environment Holding Singapore Pte. Ltd. | Flow grid and ambient air purification device |
| WO2023234927A1 (en) * | 2022-05-31 | 2023-12-07 | Itt Goulds Pumps, Inc. | Pump casing |
| CN219101727U (en) | 2022-12-21 | 2023-05-30 | 台达电子工业股份有限公司 | diversion grille |
| CN116447754A (en) * | 2023-04-13 | 2023-07-18 | 海信(山东)厨卫有限公司 | Gas water heater |
| DE102023134471A1 (en) * | 2023-12-08 | 2025-06-12 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Flow guide device and fan with a flow guide device |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102015112148A1 (en) * | 2014-07-31 | 2016-02-04 | Gentherm Incorporated | Fan inlet interface and cover |
| WO2016116871A1 (en) * | 2015-01-22 | 2016-07-28 | Elica S.P.A. | Suction grid for an air guide of a domestic hood, air guide having such grid and domestic hood having such air guide. |
Family Cites Families (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5088886A (en) * | 1990-08-28 | 1992-02-18 | Sinko Kogyo Co., Ltd. | Inlet air flow conditioning for centrifugal fans |
| DE10162919A1 (en) | 2001-12-20 | 2003-07-03 | Bsh Bosch Siemens Hausgeraete | fan device |
| US7089963B2 (en) * | 2002-11-26 | 2006-08-15 | David Meheen | Flow laminarizing device |
| US7104753B2 (en) * | 2004-07-13 | 2006-09-12 | Dreison International, Inc. | Motor fan guard |
| GB0613012D0 (en) * | 2006-06-30 | 2006-08-09 | Qinetiq Ltd | Axial flow impeller |
| CN201246347Y (en) * | 2008-09-01 | 2009-05-27 | 麦克·梵得雅德 | Fan casing |
| DE202009017511U1 (en) * | 2009-12-22 | 2011-05-05 | Ebm-Pabst Mulfingen Gmbh & Co. Kg | Fan unit for filter fan |
| RU2431062C1 (en) | 2010-03-15 | 2011-10-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Axial fan |
| DE102011015784A1 (en) * | 2010-08-12 | 2012-02-16 | Ziehl-Abegg Ag | fan |
| EP2778432B1 (en) * | 2013-03-15 | 2015-10-14 | ebm-papst Mulfingen GmbH & Co. KG | Ventilator assembly with flow rectifier |
| US10337526B2 (en) * | 2015-05-11 | 2019-07-02 | Chervon (Hk) Limited | Blower |
| US9835176B2 (en) * | 2013-04-05 | 2017-12-05 | Acoustiflo Llc | Fan inlet air handling apparatus and methods |
| DE102014102370A1 (en) * | 2014-02-24 | 2015-08-27 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Flow straightener and fan arrangement with flow straightener |
| CN204942101U (en) * | 2014-10-07 | 2016-01-06 | 日本电产株式会社 | Fan |
| DE202014105284U1 (en) * | 2014-11-04 | 2014-12-08 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Protective grille with improved efficiency and noise behavior |
| DE102015115308A1 (en) * | 2015-09-10 | 2017-03-16 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Flow guide for arrangement on a fan |
| CN205173078U (en) * | 2015-11-19 | 2016-04-20 | 广东美的环境电器制造有限公司 | A box fan rear net and box fan |
| FR3044028B1 (en) * | 2015-11-25 | 2017-11-17 | Pellenc Sa | ELECTROPORTATIVE BLOWER WITH REDUCED REACTION TORQUE. |
| JP6616709B2 (en) * | 2016-02-23 | 2019-12-04 | 株式会社やまびこ | Portable power work machine |
| DE102016115616A1 (en) * | 2016-08-23 | 2018-03-01 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Flow straightener of a fan |
| JP6687120B2 (en) * | 2016-09-30 | 2020-04-22 | 工機ホールディングス株式会社 | Blower |
| US20180135874A1 (en) * | 2016-11-16 | 2018-05-17 | Long Chang | Fan Guard for Electric Fan with Cooling Assembly |
| DE102017209291A1 (en) * | 2017-06-01 | 2018-12-06 | Ziehl-Abegg Se | Fan and guide grille for a fan |
| US10309423B2 (en) * | 2017-06-02 | 2019-06-04 | International Business Machines Corporation | Mechanically actuated safety compliant fan finger guard structures and methods |
| CN109538504B (en) * | 2017-09-21 | 2021-03-16 | 日本电产株式会社 | Tandem axial flow fan |
| US10837453B2 (en) * | 2018-09-21 | 2020-11-17 | Quanta Computer Inc. | Fan module with lockable lens |
| US11560843B2 (en) * | 2020-02-25 | 2023-01-24 | General Electric Company | Frame for a heat engine |
-
2018
- 2018-04-09 DE DE102018205300.6A patent/DE102018205300A1/en active Pending
-
2019
- 2019-02-15 WO PCT/DE2019/200013 patent/WO2019196992A1/en not_active Ceased
- 2019-02-15 CN CN201980038538.2A patent/CN112262261B/en active Active
- 2019-02-15 EP EP19715390.1A patent/EP3775571B1/en active Active
- 2019-02-15 JP JP2020553571A patent/JP2021519885A/en active Pending
- 2019-02-15 SI SI201930866T patent/SI3775571T1/en unknown
- 2019-02-15 ES ES19715390T patent/ES3001091T3/en active Active
- 2019-02-15 KR KR1020207032305A patent/KR102795830B1/en active Active
- 2019-02-15 US US17/046,451 patent/US11703065B2/en active Active
-
2023
- 2023-09-27 JP JP2023164145A patent/JP2023169380A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102015112148A1 (en) * | 2014-07-31 | 2016-02-04 | Gentherm Incorporated | Fan inlet interface and cover |
| WO2016116871A1 (en) * | 2015-01-22 | 2016-07-28 | Elica S.P.A. | Suction grid for an air guide of a domestic hood, air guide having such grid and domestic hood having such air guide. |
Also Published As
| Publication number | Publication date |
|---|---|
| SI3775571T1 (en) | 2025-03-31 |
| ES3001091T3 (en) | 2025-03-04 |
| KR20200141079A (en) | 2020-12-17 |
| KR102795830B1 (en) | 2025-04-16 |
| BR112020020491A2 (en) | 2021-01-12 |
| EP3775571A1 (en) | 2021-02-17 |
| JP2021519885A (en) | 2021-08-12 |
| US20210164495A1 (en) | 2021-06-03 |
| CN112262261A (en) | 2021-01-22 |
| DE102018205300A1 (en) | 2019-10-10 |
| WO2019196992A1 (en) | 2019-10-17 |
| JP2023169380A (en) | 2023-11-29 |
| CN112262261B (en) | 2024-01-02 |
| US11703065B2 (en) | 2023-07-18 |
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