EP2904277B1 - Flow rectifier for an axial fan - Google Patents

Flow rectifier for an axial fan Download PDF

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Publication number
EP2904277B1
EP2904277B1 EP13765661.7A EP13765661A EP2904277B1 EP 2904277 B1 EP2904277 B1 EP 2904277B1 EP 13765661 A EP13765661 A EP 13765661A EP 2904277 B1 EP2904277 B1 EP 2904277B1
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EP
European Patent Office
Prior art keywords
air guide
ring
air
guide blades
rings
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EP13765661.7A
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German (de)
French (fr)
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EP2904277A2 (en
Inventor
Thomas Heli
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Ebm Papst Mulfingen GmbH and Co KG
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Ebm Papst Mulfingen GmbH and Co KG
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • F04D29/544Blade shapes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/64Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps

Definitions

  • the present invention relates to a flow straightener for an axial fan according to claim 1.
  • Such a flow straightener is an air guide element which is arranged with its air guide vanes directly behind an axial fan in order to redirect the air set in flow by the axial fan impeller into a flow which is as axial and uniform as possible.
  • Such an air guide element is often also referred to as a "guide vane”.
  • Axial fans are used, for example, in evaporators in cold rooms, where the cold air is distributed through the axial fan into the cold room via the heat exchanger.
  • the cold air is transported as far into the room as possible in order to also cool the chilled goods at a location further away.
  • This requires an axial fan that provides the highest possible volume flow with a large throw.
  • Throw distance is understood to mean a distance up to which a limit speed of the air flow is maintained. Due to the swirling outflow of an axial fan, this throw distance is limited.
  • a downstream flow straightener which converts the twist back into a uniform axial flow, the throw distance can be significantly increased. It is important that the flow straightener has a has the lowest possible flow resistance, so that there is only an insignificant drop in pressure in the amount of air flowing through it.
  • a flow straightener of the type mentioned, which basically meets the above requirements, is from DE 44 04 262 A1 known.
  • a reduction in swirl of the flow medium is achieved in particular in that the air guide vanes, viewed in the circumferential direction, each run curved to the axial direction between an inflow-side vane edge and an outflow-side vane edge.
  • one of the blade edges specifically the edge on the front side of the stator blade, has a variable height in the radial direction. It is straight and runs inclined to the center axis of the impeller. Any effect associated with this embodiment is not described.
  • U.S. 2005/0186070 A1 discloses a fan assembly having an impeller mounted on the rotor of a motor.
  • the impeller is of a casing surrounded, wherein the housing comprises a arranged downstream of the impeller flow straightener.
  • the blades of the flow straightener have a constant height in the radial direction.
  • the present invention is based on the object of creating a flow straightener of the type mentioned at the outset, with which the disadvantages mentioned above can be overcome with a high volume flow and large throw distance.
  • the blade edge of the air guide blade which has the height changing in the radial direction, has a curvature.
  • the inflow angle of the vanes can be selected in such a way that it essentially corresponds to the outflow angle of the axial fan, and the outflow angle of the vanes can be such be chosen that the blade in this area is designed parallel to an air conveying direction running in the direction of the longitudinal axis.
  • the respective inflow angles of the air guide vanes can all be the same size in the different rings, or alternatively vary from ring to ring, in particular depending on the outflow profile of the flow medium emerging from the fan.
  • the rectifier according to the invention By choosing a corresponding number of rings with air guide vanes, the number of air guide vanes themselves and, alternatively or additionally, also preferably by an effective height of the blading, i.e. the arrangement of the air guide vanes, of the rectifier according to the invention, it can be achieved that the rectifier according to the invention also has a function as protection against accidental contact.
  • An additional protective grille can therefore be dispensed with because the openings between the rim walls and the air guide vanes can be designed so small or, in particular, the axial length of the rectifier can be designed so large that it is not possible to reach through with the hand or individual fingers to the rotating impeller is. This ensures a safe distance from a rotating impeller of the axial fan.
  • the number of air guide vanes decreases from the outer rims to the inner rims in order in this way to be able to realize an approximately equal distance between the respective vanes of a row in each rim and thus to achieve the lowest possible flow resistance.
  • the flow straightener according to the invention can be constructed in one piece, preferably as an injection-molded part made of plastic, in a manner that is not very complex in terms of production technology. It can advantageously be designed in such a way that it can subsequently be releasably mounted on a wall ring or on a protective or support grid of an already existing fan.
  • the fastening can be designed in such a way that the flow straightener can be removed from the fan in just a few movements and easily cleaned, for example in a dishwasher.
  • One of the blade edges in particular the edge on the rear side of the air guide blade, has a variable height in the radial direction.
  • the blade end directed in the outflow direction has an edge which does not run straight but which—particularly to minimize noise—is provided with a radius.
  • a third ring can be drawn in concentrically between two blade rings, which forms a transition between the two rings by being reduced in its axial length and thus adjoining the curved blade end.
  • Each second bladed ring can thus have a reduced axial length compared to the other rings arranged next to it.
  • a flow straightener 1 according to the invention is intended to be used in combination with an axial fan 2 .
  • This can be done in particular where optimal air distribution in a cold room is crucial in complex cooling applications, where the entire refrigerated goods must be evenly circulated with circulated air.
  • the advantage of using a flow straightener 1 according to the invention in a cooling room consists in particular in the fact that it can provide a strong, bundled air flow with a large throw distance in cooperation with the axial fan 2 .
  • the axial fan 2 can be designed in particular as a so-called wall ring fan and can comprise a wall ring 2a with a support grid 2b, in which a fan unit 2c is held.
  • the fan unit 2c has a motor, in particular an external rotor motor, the rotor of which is integrated directly into an axial impeller in a preferred embodiment.
  • the support grid 3 of the axial fan 2 used to hold the fan unit 2c can be designed with a wide mesh, since it does not have to fulfill the function of protection against accidental contact, because this is taken over by the flow straightener 1 .
  • a flow straightener 1 according to the invention has - this show next Figures 1 and 2 also Figures 3 to 5 -
  • Each ring 4a, 4b, 4c, 4d, 4e is delimited radially on the inside and outside by a cylindrical outer surface. Only in 3 In this regard, an inner lateral surface of the middle ring 4d is given the reference number 5 and the outer lateral surface of the middle ring 4d lying opposite it is given the reference number 6.
  • each ring 4a, 4b, 4c, 4d, 4e there is a plurality of circumferentially distributed around a longitudinal axis XX of the flow straightener 1 and arranged essentially radially, each between the lateral surfaces 5, 6 of the rings 4a, 4b, 4c, 4d , 4e running air guide vanes 7.
  • the air guide vanes 7 run at the same time - for this purpose, the rim 4c shown in section in 3 referred - each starting from an inflow-side blade edge 7a and ending in an outflow-side blade edge 7b, viewed in the circumferential direction, curved relative to the axis direction XX.
  • the inflow angle ⁇ Z of the air to the air guide vane 7 is how 6 1, defined as the acute angle between a tangent T Z applied to the leading blade edge 7a and the longitudinal axis XX. It can preferably be in the range of 20° ⁇ ⁇ Z ⁇ 80°.
  • the outflow angle ⁇ A is defined in the same way with a tangent T A applied to the outflow-side blade edge 7b and preferably has the value of 0°.
  • the inflow angle ⁇ Z can be the same on all air guide vanes 7 in a ring 4a, 4b, 4c, 4d, 4e, but differ from the respective inflow angle ⁇ Z of the air on the air guide vanes 7 in another ring 4a, 4b, 4c , 4d, 4e differ.
  • the inflow angle ⁇ Z can be varied depending on the outflow profile of the air emerging from the axial fan 2 from ring 4a, 4b, 4c, 4d, 4e to ring 4a, 4b, 4c, 4d, 4e.
  • the respective inflow angle ⁇ Z of the air is the same on all air guide vanes 7 .
  • a flow straightener 1 according to the invention can also be designed with a very stable honeycomb structure, the strength of which is additionally increased if--as shown and in particular in FIG 4 denoted by reference symbols - the inflow-side blade edges 7a and the outflow-side blade edges 7b of the air guide vanes 7 are arranged in adjacent rings 4a, 4b, 4c, 4d, 4e with a circumferential offset V relative to one another.
  • the respective distances A, in which the air guide vanes 7 are arranged in relation to one another can preferably each be of the same size. In 4 in this regard, the distance A between two adjacent edges 7a on the inflow side is specified as such an example.
  • the number of air guide vanes 7 themselves and alternatively or additionally also preferably by the total height H of the blading (cf. Figures 6 and 7 ), by which the axial length L of the flow straightener 1 according to the invention is significantly influenced, it can be achieved that the flow straightener 1 according to the invention also assumes a function as protection against accidental contact.
  • Another preferred feature of the flow straightener 1 according to the invention is that in the radial sequence of the rings 4a, 4b, 4c, 4d, 4e with the air guide vanes 7, the rings 4a, 4b, 4c, 4d, 4e each have different, in particular two, alternating heights have H1, H2. Between two rows of blades (rings 4a, 4c, 4e) with a peripherally greater height H1 of the blades, which decreases radially inward over the width of the rings 4a, 4c, 4e, a ring (rings 4b, 4d) is drawn in concentrically, the peripheral is reduced in its height H2, whereby the blade height over the rim width B then increases again radially inwards.
  • the total axial length L of the flow straightener 1 according to the invention is reduced in an optimal manner.
  • the course of the radial curvature R2 of the outflow-side blade edges 7b of the air guide vanes 7, through which the variable height in the radial direction is preferably set on each blade, can run in mirror image in adjacent rings 4a, 4b, 4c, 4d, 4e.
  • a bulging of the contour caused by the curvature R2 of the blade edge 7a is present radially outwards, follows in the adjacent ring 4d, which is delimited radially on the outside by the wall with the smaller height H2 and radially on the inside by a wall with a greater height H1, a bulging caused by the curvature R2 of the contour of the Blade edge 7a - in relation to the wall between the rims 4c, 4d mirror-inverted to the curvature R2 in the adjacent rim 4c - radially inwards.
  • this structural design can counteract back-turbulence of the flowing air, since this is guided up to the greater height H1, forming a laminar boundary layer on the air guide vanes 7.
  • the base body 3 of a flow straightener 1 according to the invention can preferably be designed in one piece and preferably as an injection molded part made of plastic, but a multi-part design, optionally also made of a metallic material, is also within the scope of the invention.
  • the base body 3 fasteners 8, 9 for releasable attachment to the axial fan 2, in particular z.
  • B latching means 8 for connection to the wall ring 2a associated with this fan 2 and/or fastening openings 9 for the passage of screws 10 serving for screwing to the fan 2.
  • a connecting or covering section 11 for the axial fan 2 can also be provided on a flow straightener 1 according to the invention, as illustrated, which also determines the axial length in an increasing manner and is therefore to be designed with as short a length as possible.
  • the total height H of the blading can optimally be in a range from 25 mm to 100 mm, which preferably corresponds to a size in the range from 5 percent to 40 percent of the size of the outside diameter of the axial fan wheel.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

Die vorliegende Erfindung betrifft einen Strömungsgleichrichter für einen Axiallüfter nach Anspruch 1.The present invention relates to a flow straightener for an axial fan according to claim 1.

Ein derartiger Strömungsgleichrichter ist ein Luftleitelement, das mit seinen Luftleitschaufeln unmittelbar hinter einem Axiallüfter angeordnet wird, um die von dem Axiallüfter-Laufrad in Strömung versetzte Luft in eine möglichst axiale und gleichmäßige Strömung umzuleiten. Ein solches Luftleitelement wird häufig auch als "Nachleitrad" bezeichnet.Such a flow straightener is an air guide element which is arranged with its air guide vanes directly behind an axial fan in order to redirect the air set in flow by the axial fan impeller into a flow which is as axial and uniform as possible. Such an air guide element is often also referred to as a "guide vane".

Axiallüfter werden u. a. bei Verdampfern in Kühlräumen eingesetzt, wo über den Wärmetauscher die kalte Luft durch den Axiallüfter in den Kühlraum verteilt wird. Bei großen Kühlräumen ist es wichtig, dass die kalte Luft möglichst weit in den Raum hinein transportiert wird, um auch das Kühlgut an einem weiter entfernten Ort zu kühlen. Dazu ist ein Axiallüfter erforderlich, der einen möglichst hohen Volumenstrom mit einer großen Wurfweite bereitstellt. Unter Wurfweite wird dabei eine Entfernung verstanden, bis zu der eine Grenzgeschwindigkeit der Luftströmung eingehalten wird. Bedingt durch die drallbehaftete Abströmung eines Axiallüfters ist diese Wurfweite begrenzt. Mit Hilfe eines nachgeschalteten Strömungsgleichrichters, der den Drall in eine gleichmäßige axiale Strömung zurückwandelt, kann die Wurfweite deutlich gesteigert werden. Wichtig ist dabei, dass der Strömungsgleichrichter einen möglichst geringen Strömungswiderstand aufweist, so dass darin nur ein unwesentlicher Druckabfall in der ihn durchströmenden Luftmenge auftritt.Axial fans are used, for example, in evaporators in cold rooms, where the cold air is distributed through the axial fan into the cold room via the heat exchanger. In the case of large cold rooms, it is important that the cold air is transported as far into the room as possible in order to also cool the chilled goods at a location further away. This requires an axial fan that provides the highest possible volume flow with a large throw. Throw distance is understood to mean a distance up to which a limit speed of the air flow is maintained. Due to the swirling outflow of an axial fan, this throw distance is limited. With the help of a downstream flow straightener, which converts the twist back into a uniform axial flow, the throw distance can be significantly increased. It is important that the flow straightener has a has the lowest possible flow resistance, so that there is only an insignificant drop in pressure in the amount of air flowing through it.

Ein Strömungsgleichrichter der eingangs genannten Art, welcher die vorstehend genannten Forderungen grundsätzlich erfüllt, ist aus der DE 44 04 262 A1 bekannt. Eine Drallminderung des Strömungsmittels wird dabei insbesondere dadurch erreicht, dass die Luftleitschaufeln in Umfangsrichtung gesehen jeweils zwischen einer anströmseitigen Schaufelkante und einer abströmseitigen Schaufelkante gekrümmt zur Achsrichtung verlaufen. In einer speziellen Ausführung ist dabei auch vorgesehen, dass eine der Schaufelkanten, und zwar die Kante auf der Leitradschaufelvorderseite, eine in radialer Richtung veränderliche Höhe aufweist. Sie ist gerade ausgebildet und verläuft zur Laufradmittelachse geneigt. Eine eventuell mit dieser Ausführung verbundene Wirkung ist nicht beschrieben.A flow straightener of the type mentioned, which basically meets the above requirements, is from DE 44 04 262 A1 known. A reduction in swirl of the flow medium is achieved in particular in that the air guide vanes, viewed in the circumferential direction, each run curved to the axial direction between an inflow-side vane edge and an outflow-side vane edge. In a special embodiment, it is also provided that one of the blade edges, specifically the edge on the front side of the stator blade, has a variable height in the radial direction. It is straight and runs inclined to the center axis of the impeller. Any effect associated with this embodiment is not described.

Nachteilig ist an diesem bekannten Strömungsgleichrichter, dass sich eine tatsächlich gleichmäßige axiale Strömung erst in einem erheblichen Abstand vom Lüfter bzw. vom Austritt aus dem Leitrad einstellt. So ist, wie die in der DE 44 04 262 A1 enthaltene Fig. 1 veranschaulicht, ein Winkel zwischen der Luftströmung und der Lüfterachse in einem peripher gelegenen Optimalbereich der radialen Länge der Luftleitschaufeln des Strömungsgleichrichters zwar nahezu Null, jedoch wächst dieser Winkel radial auswärts und insbesondere radial einwärts relativ schnell an. Dies führt zu einem divergierenden Luftstrom. Bei vorgegebenen Durchmessern der zylindrischen Mantelflächen der Wände, die radial innen und außen den Kranz der Luftleitschaufeln begrenzen, gibt es jeweils nur eine unter dem Gesichtspunkt einer Vergleichmäßigung der Strömung des Fluids optimale Schaufellänge, welche gemäß der DE 44 04 262 A1 durch aufwändige aerodynamische Messungen mit einer Conradsonde ermittelt wurde. Darüber hinaus ist bei dem Einsatz des bekannten Strömungsgleichrichters eine Kombination mit einem Schutzgitter erforderlich, um einen Berührungsschutz zu gewährleisten.The disadvantage of this known flow straightener is that an actually uniform axial flow only sets in at a considerable distance from the fan or from the exit from the guide wheel. So is like the in the DE 44 04 262 A1 included 1 As illustrated, an angle between the air flow and the fan axis is almost zero in a peripheral optimum range of the radial length of the air guide vanes of the flow straightener, but this angle increases relatively rapidly radially outwards and in particular radially inwards. This results in a divergent airflow. With given diameters of the cylindrical lateral surfaces of the walls, which delimit the ring of the air guide vanes radially inside and outside, there is only one vane length that is optimal from the point of view of equalizing the flow of the fluid, which according to the DE 44 04 262 A1 was determined by complex aerodynamic measurements with a Conrad probe. In addition, when using the known flow straightener, a combination with a protective grid is required in order to ensure protection against accidental contact.

Des Weiteren offenbart US 2005/0186070 A1 eine Ventilatoranordnung mit einem auf dem Rotor eines Motors angeordneten Laufrad. Das Laufrad ist von einem Gehäuse umgeben, wobei das Gehäuse einen in Strömungsrichtung hinter dem Laufrad angeordneten Strömungsgleichrichter umfasst. Die Schaufeln des Strömungsgleichrichters weisen in radialer Richtung eine konstante Höhe auf.Furthermore disclosed U.S. 2005/0186070 A1 discloses a fan assembly having an impeller mounted on the rotor of a motor. The impeller is of a casing surrounded, wherein the housing comprises a arranged downstream of the impeller flow straightener. The blades of the flow straightener have a constant height in the radial direction.

Der vorliegenden Erfindung liegt die Aufgabe zu Grunde, einen Strömungsgleichrichter der eingangs genannten Art zu schaffen, mit dem bei hohem Volumenstrom und großer Wurfweite die vorstehend genannten Nachteile überwunden werden können.The present invention is based on the object of creating a flow straightener of the type mentioned at the outset, with which the disadvantages mentioned above can be overcome with a high volume flow and large throw distance.

Die Schaufelkante der Luftleitschaufel, welche die sich in radialer Richtung verändernde Höhe aufweist, weist eine Krümmung auf.The blade edge of the air guide blade, which has the height changing in the radial direction, has a curvature.

Durch die vorhandene radiale Segmentierung des Querschnitts des Strömungsgleichrichters wird vorteilhafterweise erreicht, dass bei gleichbleibend hohem Volumenstrom ein Drall des strömenden Gases in der Abströmung eines Axiallüfters effektiver unterbunden wird. Ein gleichmäßiges Strömungsbild stellt sich im Vergleich mit dem bekannten Stand der Technik in geringerer Entfernung vom Strömungsgleichrichter ein, und die Wurfweite vergrößert sich. Eine signifikante Divergenz des aus dem erfindungsgemäßen Strömungsgleichrichter austretenden Luftstroms kann dabei wirksam durch eine erhöhte Anzahl von Schaufelkränzen unterbunden werden. Bei sich ändernden Abmessungen, z. B. der Innen- und Außendurchmesser eines Axialflügelrades des Lüfters und damit der Schaufellänge, aus denen in der Folge auch entsprechende Änderungen der Dimensionen des Strömungsgleichrichters resultieren, müssen keine aufwändigen Messungen und/oder Optimierungsrechnungen durchgeführt werden, da Schaufelkränze mit jeweils gleicher radialer Breite und bekannter Effizienz nebeneinander gereiht werden können.Due to the existing radial segmentation of the cross section of the flow straightener, it is advantageously achieved that a swirl of the flowing gas in the outflow of an axial fan is prevented more effectively with a consistently high volume flow. In comparison with the known state of the art, a uniform flow pattern occurs at a smaller distance from the flow straightener, and the throw distance increases. A significant divergence of the air flow emerging from the flow straightener according to the invention can be effectively prevented by an increased number of blade rings. If the dimensions change, e.g. B. the inner and outer diameter of an axial impeller of the fan and thus the blade length, which subsequently result in corresponding changes in the dimensions of the flow straightener, no complex measurements and / or optimization calculations have to be carried out, since blade rings with the same radial width and known efficiency can be lined up next to each other.

Bei der Krümmung zur Achsrichtung, welche die Luftleitschaufeln in Umfangsrichtung gesehen jeweils zwischen ihrer anströmseitigen Schaufelkante und ihrer abströmseitigen Schaufelkante aufweisen, kann der Zuströmwinkel der Schaufeln dabei derart gewählt sein, dass er im Wesentlichen dem Abströmwinkel des Axiallüfters entspricht, und der Abströmwinkel der Schaufeln kann derart gewählt sein, dass die Schaufel in diesem Bereich parallel zu einer in Richtung der Längsachse verlaufenden Luftförderrichtung ausgeführt ist. Die jeweiligen Zuströmwinkel der Luftleitschaufeln können in den verschiedenen Kränzen alle gleich groß sein, oder alternativ von Kranz zu Kranz variieren, und zwar insbesondere in Abhängigkeit vom Abströmprofil des aus dem Lüfter austretenden Strömungsmittels.With the curvature to the axial direction, which the air guide vanes each have between their inflow-side vane edge and their outflow-side vane edge, viewed in the circumferential direction, the inflow angle of the vanes can be selected in such a way that it essentially corresponds to the outflow angle of the axial fan, and the outflow angle of the vanes can be such be chosen that the blade in this area is designed parallel to an air conveying direction running in the direction of the longitudinal axis. The respective inflow angles of the air guide vanes can all be the same size in the different rings, or alternatively vary from ring to ring, in particular depending on the outflow profile of the flow medium emerging from the fan.

Durch eine Wahl einer entsprechenden Anzahl von Kränzen mit Luftleitschaufeln, der Anzahl der Luftleitschaufeln selbst sowie alternativ oder zusätzlich auch vorzugsweise durch eine effektive Höhe der Beschaufelung, also der Anordnung der Luftleitschaufeln, des erfindungsgemäßen Gleichrichters, kann erreicht werden, dass der erfindungsgemäße Gleichrichter auch eine Funktion als Berührungsschutz übernimmt. Auf ein zusätzliches Schutzgitter kann somit verzichtet werden, weil die zwischen den Kranzwandungen und den Luftleitschaufeln vorhandenen Öffnungen so klein oder insbesondere die axiale Länge des Gleichrichters so groß gestaltet werden kann, dass ein Durchgreifen mit der Hand oder mit einzelnen Fingern bis zum drehenden Laufrad nicht möglich ist. So ist ein sicherer Abstand zu einem sich drehenden Laufrad des Axiallüfters gewährleistet.By choosing a corresponding number of rings with air guide vanes, the number of air guide vanes themselves and, alternatively or additionally, also preferably by an effective height of the blading, i.e. the arrangement of the air guide vanes, of the rectifier according to the invention, it can be achieved that the rectifier according to the invention also has a function as protection against accidental contact. An additional protective grille can therefore be dispensed with because the openings between the rim walls and the air guide vanes can be designed so small or, in particular, the axial length of the rectifier can be designed so large that it is not possible to reach through with the hand or individual fingers to the rotating impeller is. This ensures a safe distance from a rotating impeller of the axial fan.

Die Anzahl der Luftleitschaufeln nimmt dabei erfindungsgemäß von den äußeren Kränzen zu den inneren Kränzen hin ab, um auf diese Weise in jedem Kranz einen annähernd gleichen Abstand zwischen den jeweiligen Schaufeln einer Reihe realisieren zu können und so einen möglichst geringen Strömungswiderstand zu erreichen.According to the invention, the number of air guide vanes decreases from the outer rims to the inner rims in order in this way to be able to realize an approximately equal distance between the respective vanes of a row in each rim and thus to achieve the lowest possible flow resistance.

Der erfindungsgemäße Strömungsgleichrichter kann in fertigungstechnisch wenig aufwändiger Weise einteilig, vorzugsweise als Spritzgießteil aus Kunststoff, aufgebaut sein. Er kann dabei mit Vorteil derart gestaltet sein, dass er nachträglich auf einen Wandring oder auf ein Schutz- bzw. Traggitter eines bereits vorhandenen Lüfters lösbar montiert werden kann. Dabei kann die Befestigung derart gestaltet sein, dass der Strömungsgleichrichter mit nur wenigen Handgriffen von dem Lüfter abgenommen und problemlos - beispielsweise in einer Spülmaschine - gereinigt werden kann.The flow straightener according to the invention can be constructed in one piece, preferably as an injection-molded part made of plastic, in a manner that is not very complex in terms of production technology. It can advantageously be designed in such a way that it can subsequently be releasably mounted on a wall ring or on a protective or support grid of an already existing fan. The fastening can be designed in such a way that the flow straightener can be removed from the fan in just a few movements and easily cleaned, for example in a dishwasher.

Durch eine geeignete Materialwahl und eine entsprechende Dimensionierung der axialen Länge des erfindungsgemäßen Strömungsgleichrichters ist es auch möglich, eine große Robustheit in Bezug auf von außen wirkende mechanische Belastungen zu gewährleisten. So ist bei einem Einsatz des erfindungsgemäßen Strömungsgleichrichters in Kombination mit einem Verdampferlüfter eine gewaltsame Entfernung von gebildetem Eis von der Oberfläche, beispielsweise mit einem Schraubendreher, möglich, ohne dass die Gleichrichterstruktur beschädigt wird. Auch können insbesondere die einschlägigen Festigkeitsanforderungen gemäß dem sogenannten Ball-Impact-Test (z. B. nach UL 2218) der Underwriters Laboratories erfüllt werden. Konkret wird bei diesem Test eine genormte Stahlkugel mit ca. 50 mm Durchmesser aus verschiedenen Höhen (unterschiedliche Schärfegrade z. B. 0,38m, 1,2m ...) im freien Fall auf den Strömungsgleichrichter fallen gelassen. Dabei muss dieser den Aufprall so überleben, dass die Berührschutzfunktion gegenüber drehenden und elektrischen Teilen noch voll gegeben ist.Through a suitable choice of material and a corresponding dimensioning of the axial length of the flow straightener according to the invention, it is also possible to ensure a high degree of robustness with regard to mechanical loads acting from the outside. Thus, when using the flow straightener according to the invention in combination with an evaporator fan, ice that has formed can be forcibly removed from the surface, for example with a screwdriver, without damaging the straightener structure. In particular, the relevant strength requirements according to the so-called ball impact test (e.g. according to UL 2218) of the Underwriters Laboratories can also be met. Specifically, in this test, a standardized steel ball with a diameter of approx. 50 mm is dropped from different heights (different degrees of sharpness, e.g. 0.38m, 1.2m ...) in free fall onto the flow straightener. It must survive the impact in such a way that the contact protection function against rotating and electrical parts is still fully available.

Eine der Schaufelkanten, und zwar insbesondere die Kante auf der Luftleitschaufelrückseite, weist eine in radialer Richtung veränderliche Höhe auf.One of the blade edges, in particular the edge on the rear side of the air guide blade, has a variable height in the radial direction.

Dabei weist das in Abströmrichtung gerichtete Schaufelende eine Kante auf, die nicht gerade verläuft, sondern die - insbesondere, zur Geräuschminimierung - mit einem Radius versehen ist.In this case, the blade end directed in the outflow direction has an edge which does not run straight but which—particularly to minimize noise—is provided with a radius.

Zwischen zwei Schaufelkränzen kann jeweils konzentrisch ein dritter Kranz eingezogen sein, der einen Übergang zwischen den beiden Kränzen bildet, indem er in seiner axialen Länge reduziert ist und so an das gekrümmte Schaufelende anschließt. Jeder zweite Schaufelkranz-Ring kann somit eine gegenüber den anderen, neben ihm angeordneten Kränzen reduzierte axiale Länge aufweisen.A third ring can be drawn in concentrically between two blade rings, which forms a transition between the two rings by being reduced in its axial length and thus adjoining the curved blade end. Each second bladed ring can thus have a reduced axial length compared to the other rings arranged next to it.

Vorteilhafte Ausführungen der Erfindung sind in den Unteransprüchen enthalten und werden an Hand der in den beiliegenden Zeichnungen dargestellten Ausführungsbeispiele näher erläutert. Es zeigen:

Fig. 1
in perspektivischer Explosionsdarstellung, eine bevorzugte Ausführung eines erfindungsgemäßen Strömungsgleichrichters zusammen mit einem Axiallüfter,
Fig. 2
den in Fig. 1 dargestellten erfindungsgemäßen Strömungsgleichrichter im Montagezustand an dem Axiallüfter,
Fig. 3
eine gegenüber Fig. 1 und 2 vergrößerte und teilgeschnittene perspektivische Ansicht des erfindungsgemäßen Strömungsgleichrichters,
Fig. 4
eine Frontansicht des erfindungsgemäßen Strömungsgleichrichters,
Fig. 5
die Ausführung des erfindungsgemäßen Strömungsgleichrichters gemäß Fig. 4 in einer teilgeschnittenen Längsdarstellung,
Fig. 6 und 7
die in Fig. 5 mit VI und VII bezeichneten Einzelheiten des erfindungsgemäßen Strömungsgleichrichters in einer stark vergrößerten Darstellung.
Advantageous embodiments of the invention are contained in the subclaims and are explained in more detail with reference to the exemplary embodiments illustrated in the accompanying drawings. Show it:
1
in a perspective exploded view, a preferred embodiment of a flow straightener according to the invention together with an axial fan,
2
the in 1 illustrated flow rectifier according to the invention in the assembled state on the axial fan,
3
one opposite Figures 1 and 2 enlarged and partially sectioned perspective view of the flow straightener according to the invention,
4
a front view of the flow straightener according to the invention,
figure 5
the design of the flow straightener according to the invention 4 in a partially sectioned longitudinal view,
Figures 6 and 7
in the figure 5 with VI and VII designated details of the flow straightener according to the invention in a greatly enlarged view.

In den Figuren der Zeichnung sind gleiche Teile bzw. funktionsgleiche Teile auch mit den gleichen Bezugszeichen gekennzeichnet. Sofern bestimmte, beschriebene und/oder aus den Zeichnungen entnehmbare Merkmale des erfindungsgemäßen Strömungsgleichrichters oder seiner Bestandteile nur im Zusammenhang mit dem Ausführungsbeispiel erwähnt sind, sind diese aber auch gemäß der Erfindung unabhängig von diesem Ausführungsbeispiel als Einzelmerkmal oder aber auch in Kombination mit anderen Merkmalen des Ausführungsbeispiels von Bedeutung und können als zur Erfindung gehörig beansprucht werden.In the figures of the drawing, the same parts or parts with the same function are also identified by the same reference symbols. If certain features of the flow straightener according to the invention or its components that are described and/or can be taken from the drawings are only mentioned in connection with the exemplary embodiment, these are also independent of this exemplary embodiment according to the invention as an individual feature or in combination with other features of the exemplary embodiment of importance and can be claimed as pertaining to the invention.

Wie zunächst aus Fig. 1 und 2 hervorgeht, ist ein erfindungsgemäßer Strömungsgleichrichter 1 dazu bestimmt, in Kombination mit einem Axiallüfter 2 zur Anwendung zu kommen. Dies kann insbesondere dort geschehen, wo bei komplexen Kühlanwendungen eine optimale Luftverteilung in einem Kühlraum entscheidend ist, wobei das gesamte Kühlgut gleichmäßig mit umgewälzter Luft umströmt werden muss. Der Vorteil des Einsatzes eines erfindungsgemäßen Strömungsgleichrichters 1 in einem Kühlraum besteht dabei insbesondere darin, dass durch ihn im Zusammenwirken mit dem Axialüfter 2 ein starker, gebündelter Luftstrom mit großer Wurfweite bereitgestellt werden kann.How first off Figures 1 and 2 shows, a flow straightener 1 according to the invention is intended to be used in combination with an axial fan 2 . This can be done in particular where optimal air distribution in a cold room is crucial in complex cooling applications, where the entire refrigerated goods must be evenly circulated with circulated air. The advantage of using a flow straightener 1 according to the invention in a cooling room consists in particular in the fact that it can provide a strong, bundled air flow with a large throw distance in cooperation with the axial fan 2 .

Der Axiallüfter 2 kann - wie dargestellt - insbesondere als ein sogenannter Wandringventilator ausgebildet sein und einen Wandring 2a mit einem Traggitter 2b umfassen, in welchem eine Ventilatoreinheit 2c gehalten ist. Die Ventilatoreinheit 2c weist dabei einen Motor auf, insbesondere einen Außenläufermotor, dessen Rotor in bevorzugter Ausführung direkt in ein Axialflügelrad integriert ist. Das zur Halterung der Ventilatoreinheit 2c dienende Traggitter 3 des Axiallüfters 2 kann weitmaschig ausgeführt sein, da es nicht die Funktion eines Berührungsschutzes erfüllen muss, weil diese vom Strömungsgleichrichter 1 übernommen wird.As shown, the axial fan 2 can be designed in particular as a so-called wall ring fan and can comprise a wall ring 2a with a support grid 2b, in which a fan unit 2c is held. The fan unit 2c has a motor, in particular an external rotor motor, the rotor of which is integrated directly into an axial impeller in a preferred embodiment. The support grid 3 of the axial fan 2 used to hold the fan unit 2c can be designed with a wide mesh, since it does not have to fulfill the function of protection against accidental contact, because this is taken over by the flow straightener 1 .

Ein erfindungsgemäßer Strömungsgleichrichter 1 weist - dies zeigen neben Fig. 1 und 2 auch Fig. 3 bis 5 - einen Grundkörper 3 auf, der mindestens zwei, bevorzugt aber mehrere - in der dargestellten Ausführung sind es fünf - Kränze 4a, 4b, 4c, 4d, 4e umfasst. Jeder Kranz 4a, 4b, 4c, 4d, 4e ist jeweils von einer zylindrischen Mantelfläche radial innen und außen begrenzt. Nur in Fig. 3 sind diesbezüglich exemplarisch eine innere Mantelfläche des mittleren Kranzes 4d mit dem Bezugszeichen 5 und die ihr gegenüber liegende äußere Mantelfläche des mittleren Kranzes 4d mit dem Bezugszeichen 6 bezeichnet.A flow straightener 1 according to the invention has - this show next Figures 1 and 2 also Figures 3 to 5 - A base body 3, which comprises at least two, but preferably several - in the illustrated embodiment there are five - wreaths 4a, 4b, 4c, 4d, 4e. Each ring 4a, 4b, 4c, 4d, 4e is delimited radially on the inside and outside by a cylindrical outer surface. Only in 3 In this regard, an inner lateral surface of the middle ring 4d is given the reference number 5 and the outer lateral surface of the middle ring 4d lying opposite it is given the reference number 6.

In jedem Kranz 4a, 4b, 4c, 4d, 4e befindet sich eine Mehrzahl von in Umfangsrichtung um eine Längsachse X-X des Strömungsgleichrichters 1 herum verteilt und im Wesentlichen radial angeordneten, jeweils zwischen den Mantelflächen 5, 6 der Kränze 4a, 4b, 4c, 4d, 4e verlaufenden Luftleitschaufeln 7. Die Luftleitschaufeln 7 verlaufen dabei gleichzeitig - hierzu wird insbesondere exemplarisch auf den geschnitten dargestellten Kranz 4c in Fig. 3 verwiesen - jeweils von einer anströmseitigen Schaufelkante 7a ausgehend und in einer abströmseitigen Schaufelkante 7b endend in Umfangsrichtung gesehen gekrümmt zur Achsrichtung X-X. Durch die Krümmung R1 zur Achsrichtung X-X, welche beispielsweise durch einen Kreisbogen bestimmt sein kann, wird insbesondere bewirkt, dass ein Zuströmwinkel µZ der Luft zu der Luftleitschaufel 7 an der anströmseitigen Schaufelkante 7a derart groß ist, dass er im Wesentlichen einem Abströmwinkel µA der mit Drall behafteten Luft aus dem Axiallüfter 2 entspricht, während der Abstömwinkel µA der Luft von den Luftleitschaufeln 7 an der abströmseitigen Schaufelkante 7b derart gewählt ist, dass die Luftleitschaufel 7 in diesem Bereich parallel zu einer in Richtung der Längsachse X-X verlaufenden Luftförderrichtung verläuft. Dieses Merkmal ist auch Fig. 6 in besonders anschaulicher Weise zu entnehmen.In each ring 4a, 4b, 4c, 4d, 4e there is a plurality of circumferentially distributed around a longitudinal axis XX of the flow straightener 1 and arranged essentially radially, each between the lateral surfaces 5, 6 of the rings 4a, 4b, 4c, 4d , 4e running air guide vanes 7. The air guide vanes 7 run at the same time - for this purpose, the rim 4c shown in section in 3 referred - each starting from an inflow-side blade edge 7a and ending in an outflow-side blade edge 7b, viewed in the circumferential direction, curved relative to the axis direction XX. through the Curvature R1 to the axis direction XX, which can be determined, for example, by an arc of a circle, has the effect, in particular, that an inflow angle µ Z of the air to the air guide vane 7 at the inflow-side vane edge 7a is so large that it essentially corresponds to an outflow angle µ A of the twist tainted air from the axial fan 2, while the deflection angle µ A of the air from the air guide vanes 7 at the outflow-side blade edge 7b is selected in such a way that the air guide vane 7 in this area runs parallel to an air conveying direction running in the direction of the longitudinal axis XX. This feature is also 6 in a particularly clear way.

Der Zuströmwinkel µZ der Luft zu der Luftleitschaufel 7 ist dabei, wie Fig. 6 veranschaulicht, definiert als der spitze Winkel zwischen einer an die anströmseitige Schaufelkante 7a angelegten Tangente TZ und der Längsachse X-X. Er kann bevorzugt im Bereich 20° ≤ µZ ≤ 80° liegen. Der Abströmwinkel µA ist in gleicher Weise mit einer an die abströmseitige Schaufelkante 7b angelegten Tangente TA definiert und hat vorzugsweise den Wert von 0°. Der Zuströmwinkel µZ kann insbesondere an allen in einem Kranz 4a, 4b, 4c, 4d, 4e liegenden Luftleitschaufeln 7 gleich groß sein, sich jedoch von dem jeweiligen Zuströmwinkel µZ der Luft an den Luftleitschaufeln 7 in einem anderen Kranz 4a, 4b, 4c, 4d, 4e unterscheiden. Hierbei können die Zuströmwinkel µZ in Abhängigkeit vom Abströmprofil der aus dem Axiallüfter 2 austretenden Luft von Kranz 4a, 4b, 4c, 4d, 4e zu Kranz 4a, 4b, 4c, 4d, 4e variiert werden.The inflow angle μ Z of the air to the air guide vane 7 is how 6 1, defined as the acute angle between a tangent T Z applied to the leading blade edge 7a and the longitudinal axis XX. It can preferably be in the range of 20°≦ μZ ≦80°. The outflow angle μ A is defined in the same way with a tangent T A applied to the outflow-side blade edge 7b and preferably has the value of 0°. The inflow angle μ Z can be the same on all air guide vanes 7 in a ring 4a, 4b, 4c, 4d, 4e, but differ from the respective inflow angle μ Z of the air on the air guide vanes 7 in another ring 4a, 4b, 4c , 4d, 4e differ. Here, the inflow angle μ Z can be varied depending on the outflow profile of the air emerging from the axial fan 2 from ring 4a, 4b, 4c, 4d, 4e to ring 4a, 4b, 4c, 4d, 4e.

In dem dargestellten Ausführungsbeispiel des erfindungsgemäßen Strömungsgleichrichters 1 ist der jeweilige Zuströmwinkel µZ der Luft an allen Luftleitschaufeln 7 gleich groß. Durch Wahl der entsprechenden Anzahl der jeweils eine gleiche Breite B aufweisenden Kränze 4a, 4b, 4c, 4d, 4e mit Luftleitschaufeln 7 (siehe Fig. 4) und der Anzahl der Luftleitschaufeln 7, die von Kranz 4a, 4b, 4c, 4d, 4e zu Kranz 4a, 4b, 4c, 4d, 4e von außen nach innen abnimmt, wird erreicht, dass alle Luftleitschaufeln 7 und Räume, in denen die Luftleitschaufeln 7 sich jeweils befinden bzw. die gegenseitigen Abstände der Luftleitschaufeln 7 voneinander, nahezu uniform und mit gleicher Größe ausgebildet sind, und daher auch im Hinblick auf die angestrebten Wirkungen der Drallminderung und Vergrößerung der Wurfweite in gleicher Weise zur Effizienzsteigerung beitragen.In the illustrated embodiment of the flow straightener 1 according to the invention, the respective inflow angle μ Z of the air is the same on all air guide vanes 7 . By choosing the appropriate number of rings 4a, 4b, 4c, 4d, 4e, each having the same width B, with air guide vanes 7 (see 4 ) and the number of air guide vanes 7, which decreases from ring 4a, 4b, 4c, 4d, 4e to ring 4a, 4b, 4c, 4d, 4e from the outside inwards, it is achieved that all air guide vanes 7 and spaces in which the Air guide vanes 7 are each located or the mutual distances of the air guide vanes 7 from each other, are formed almost uniformly and with the same size, and therefore also with regard to the desired Effects of reducing the twist and increasing the throwing distance contribute in the same way to increasing efficiency.

Ein erfindungsgemäßer Strömungsgleichrichter 1 kann auf diese Weise auch mit einer sehr stabilen Wabenstruktur ausgeführt werden, deren Festigkeit zusätzlich noch dadurch erhöht wird, wenn - wie dargestellt und insbesondere in Fig. 4 mit Bezugszeichen gekennzeichnet - die anströmseitigen Schaufelkanten 7a und die abströmseitigen Schaufelkanten 7b der Luftleitschaufeln 7 in jeweils nebeneinander liegenden Kränzen 4a, 4b, 4c, 4d, 4e mit umfangsgemäßem Versatz V zueinander angeordnet sind. Dabei können die jeweiligen Abstände A, in denen die Luftleitschaufeln 7 zueinander angeordnet sind, vorzugsweise jeweils gleich groß sein. In Fig. 4 ist diesbezüglich exemplarisch als solcher Abstand A derjenige zwischen zwei nebeneinander liegenden anströmseitigen Kanten 7a angegeben.In this way, a flow straightener 1 according to the invention can also be designed with a very stable honeycomb structure, the strength of which is additionally increased if--as shown and in particular in FIG 4 denoted by reference symbols - the inflow-side blade edges 7a and the outflow-side blade edges 7b of the air guide vanes 7 are arranged in adjacent rings 4a, 4b, 4c, 4d, 4e with a circumferential offset V relative to one another. The respective distances A, in which the air guide vanes 7 are arranged in relation to one another, can preferably each be of the same size. In 4 in this regard, the distance A between two adjacent edges 7a on the inflow side is specified as such an example.

Durch eine Wahl einer entsprechenden Anzahl von Kränzen 4a, 4b, 4c, 4d, 4e mit Luftleitschaufeln 7, der Anzahl der Luftleitschaufeln 7 selbst sowie alternativ oder zusätzlich auch vorzugsweise durch die Gesamthöhe H der Beschaufelung (vgl. Fig. 6 und 7), durch die die axiale Länge L des erfindungsgemäßen Strömungsgleichrichters 1 wesentlich beeinflusst wird, kann erreicht werden, dass der erfindungsgemäße Strömungsgleichrichter 1 auch eine Funktion als Berührungsschutz übernimmt.By choosing a corresponding number of rings 4a, 4b, 4c, 4d, 4e with air guide vanes 7, the number of air guide vanes 7 themselves and alternatively or additionally also preferably by the total height H of the blading (cf. Figures 6 and 7 ), by which the axial length L of the flow straightener 1 according to the invention is significantly influenced, it can be achieved that the flow straightener 1 according to the invention also assumes a function as protection against accidental contact.

Zur Verbesserung des Ablöseverhaltens der Luft von den Schaufeln 7 - und damit verbunden zur Geräuschminderung - ist in der dargestellten Ausführung vorgesehen, dass die abströmseitigen Schaufelkanten 7b eine in radialer Richtung veränderliche Höhe, insbesondere eine sich stetig verändernde Höhe, aufweisen. Dabei ist vorgesehen, dass die abströmseitigen Schaufelkanten 7b der Luftleitschaufeln 7 zur Einstellung der in radialer Richtung veränderlichen Höhe eine Krümmung R2 aufweisen, die ebenfalls - wie auch die Schaufelkrümmung R1 in umfangsgemäßer Richtung - bevorzugt durch einen Kreisbogen beschrieben werden kann.In order to improve the detachment behavior of the air from the blades 7—and associated noise reduction—the illustrated embodiment provides that the outflow-side blade edges 7b have a variable height in the radial direction, in particular a constantly changing height. It is provided that the outflow-side blade edges 7b of the air guide vanes 7 have a curvature R2 for setting the variable height in the radial direction, which likewise—like the blade curvature R1 in the circumferential direction—can preferably be described by an arc of a circle.

Ein weiteres bevorzugtes Merkmal des erfindungsgemäßen Strömungsgleichrichters 1 ist, dass in der radialen Folge der Kränze 4a, 4b, 4c, 4d, 4e mit den Luftleitschaufeln 7 die Kränze 4a, 4b, 4c, 4d, 4e jeweils unterschiedliche, insbesondere zwei, jeweils alternierende Höhen H1, H2 aufweisen. Zwischen jeweils zwei Schaufelreihen (Kränze 4a, 4c, 4e) mit peripher größerer Höhe H1 der Schaufeln, welche über die Breite der Kränze 4a, 4c, 4e radial einwärts abnimmt, ist jeweils konzentrisch ein Ring (Kränze 4b, 4d) eingezogen, der peripher in seiner Höhe H2 reduziert ist, wobei die Schaufelhöhe über die Kranzbreite B dann radial einwärts wieder zunimmt. Dadurch wird die Ablösung von den Luftleitschaufeln 7 verbessert und der Strömungswiderstand bei insgesamt gleichbleibender, z. B. aus Gründen des Berührungsschutzes gewählter, axialer Gesamtlänge L des erfindungsgemäßen Strömungsgleichrichters 1 in optimaler Weise verringert. Der Verlauf der radialen Krümmung R2 der abströmseitigen Schaufelkanten 7b der Luftleitschaufeln 7, durch welche die in radialer Richtung veränderliche Höhe an vorzugsweise jeder Schaufel eingestellt wird, kann dabei in jeweils nebeneinander liegenden Kränzen 4a, 4b, 4c, 4d, 4e spiegelbildlich verlaufen.Another preferred feature of the flow straightener 1 according to the invention is that in the radial sequence of the rings 4a, 4b, 4c, 4d, 4e with the air guide vanes 7, the rings 4a, 4b, 4c, 4d, 4e each have different, in particular two, alternating heights have H1, H2. Between two rows of blades (rings 4a, 4c, 4e) with a peripherally greater height H1 of the blades, which decreases radially inward over the width of the rings 4a, 4c, 4e, a ring (rings 4b, 4d) is drawn in concentrically, the peripheral is reduced in its height H2, whereby the blade height over the rim width B then increases again radially inwards. This improves the detachment from the air guide vanes 7 and the flow resistance with an overall constant z. B. for reasons of protection against accidental contact, the total axial length L of the flow straightener 1 according to the invention is reduced in an optimal manner. The course of the radial curvature R2 of the outflow-side blade edges 7b of the air guide vanes 7, through which the variable height in the radial direction is preferably set on each blade, can run in mirror image in adjacent rings 4a, 4b, 4c, 4d, 4e.

Das heißt, wenn beispielsweise - wie insbesondere durch Fig. 3 veranschaulicht wird - in einem Kranz 4c, der radial außen von einer Wand mit größerer Höhe H1 (äußere Mantelfläche 6) und radial innen von einer Wand mit geringerer Höhe H2 (innere Mantelfläche 5) begrenzt wird, eine durch die Krümmung R2 bewirkte Ausbauchung der Kontur der Schaufelkante 7a radial nach außen vorliegt, folgt in dem daneben liegenden Kranz 4d, der radial außen von der Wand mit der geringeren Höhe H2 und radial innen von einer Wand mit größerer Höhe H1 begrenzt wird, eine durch die Krümmung R2 bewirkte Ausbauchung der Kontur der Schaufelkante 7a - in Bezug auf die Wand zwischen den Kränzen 4c, 4d spiegelbildlich zur Krümmung R2 im daneben liegenden Kranz 4c - radial nach innen. Bei verringertem Materialeinsatz für den erfindungsgemäßen Strömungsgleichrichter 1 aufgrund der reduzierten Höhe H2 kann durch diese konstruktive Ausgestaltung einer Rückverwirbelung der strömenden Luft entgegengewirkt werden, da diese bis zu der größeren Höhe H1 unter Ausbildung einer laminaren Grenzschicht an den Luftleitschaufeln 7 geführt wird.That is, if, for example - as in particular by 3 is illustrated - in a ring 4c, which is delimited radially on the outside by a wall with a greater height H1 (outer lateral surface 6) and radially on the inside by a wall with a lower height H2 (inner lateral surface 5), a bulging of the contour caused by the curvature R2 of the blade edge 7a is present radially outwards, follows in the adjacent ring 4d, which is delimited radially on the outside by the wall with the smaller height H2 and radially on the inside by a wall with a greater height H1, a bulging caused by the curvature R2 of the contour of the Blade edge 7a - in relation to the wall between the rims 4c, 4d mirror-inverted to the curvature R2 in the adjacent rim 4c - radially inwards. With reduced use of material for the flow straightener 1 according to the invention due to the reduced height H2, this structural design can counteract back-turbulence of the flowing air, since this is guided up to the greater height H1, forming a laminar boundary layer on the air guide vanes 7.

Die Erfindung ist nicht auf das dargestellte und beschriebene Ausführungsbeispiel beschränkt, sondern umfasst auch alle im Sinne der Erfindung gleichwirkenden Ausführungen. Wie als bevorzugt dargestellt, kann der Grundkörper 3 eines erfindungsgemäßen Strömungsgleichrichters 1 bevorzugt einteilig und vorzugsweise als Spritzgießteil aus Kunststoff ausgeführt sein, jedoch liegt auch eine mehrteilige Ausführung, gegebenenfalls auch aus einem metallischen Material, im Rahmen der Erfindung.The invention is not limited to the exemplary embodiment shown and described, but also includes all embodiments that have the same effect within the meaning of the invention. As shown as preferred, the base body 3 of a flow straightener 1 according to the invention can preferably be designed in one piece and preferably as an injection molded part made of plastic, but a multi-part design, optionally also made of a metallic material, is also within the scope of the invention.

Des Weiteren kann der Fachmann zweckmäßige ergänzende technische Maßnahmen vorsehen, ohne dass der Rahmen der Erfindung verlassen wird. So können am Grundkörper 3 Befestigungsmittel 8, 9 zur lösbaren Befestigung an dem Axiallüfter 2, insbesondere z. B. Rastmittel 8 zur Verbindung mit dem diesem Lüfter 2 zugehörigen Wandring 2a und/oder Befestigungsöffnungen 9 zum Durchtritt von zur Verschraubung mit dem Lüfter 2 dienenden Schrauben 10, vorhanden sein. Auch ein die axiale Länge vergrößernd mitbestimmender, und daher möglichst mit geringer Länge auszuführender Verbindungs- bzw. Abdeckabschnitt 11 für den Axiallüfter 2 kann - wie dargestellt - an einem erfindungsgemäßen Strömungsgleichrichter 1 vorgesehen sein.Furthermore, the person skilled in the art can provide appropriate supplementary technical measures without departing from the scope of the invention. So the base body 3 fasteners 8, 9 for releasable attachment to the axial fan 2, in particular z. B. latching means 8 for connection to the wall ring 2a associated with this fan 2 and/or fastening openings 9 for the passage of screws 10 serving for screwing to the fan 2. A connecting or covering section 11 for the axial fan 2 can also be provided on a flow straightener 1 according to the invention, as illustrated, which also determines the axial length in an increasing manner and is therefore to be designed with as short a length as possible.

Die Gesamthöhe H der Beschaufelung kann optimalerweise in einem Bereich von 25 mm bis 100 mm liegen, was dabei vorzugsweise einer Größe im Bereich 5 Prozent bis 40 Prozent der Größe des Außendurchmessers des Axiallüfterrades entspricht.The total height H of the blading can optimally be in a range from 25 mm to 100 mm, which preferably corresponds to a size in the range from 5 percent to 40 percent of the size of the outside diameter of the axial fan wheel.

BezugszeichenReference sign

11
Strömungsgleichrichterflow straightener
22
Axiallüfteraxial fan
2a2a
Wandring von 2wall ring of 2
2b2 B
Traggitter von 2Support grid from 2
2c2c
Ventilatoreinheit von 2Fan unit from 2
33
Grundkörper von 1body of 1
4a4a
erster Kranz mit 7 in 2first wreath with 7 in 2
4b4b
zweiter Kranz mit 7 in 2second wreath with 7 in 2
4c4c
dritter Kranz mit 7 in 2third wreath with 7 in 2
4d4d
vierter Kranz mit 7 in 2fourth wreath with 7 in 2
4e4e
fünfter Kranz mit 7 in 2fifth wreath with 7 in 2
55
innere Mantelfläche von 4a, 4b, 4c, 4d, 4einner lateral surface of 4a, 4b, 4c, 4d, 4e
66
äußere Mantelfläche von 4a, 4b, 4c, 4d, 4eouter lateral surface of 4a, 4b, 4c, 4d, 4e
77
Luftleitschaufelair guide vane
7a7a
anströmseitige Schaufelkante von 7upstream blade edge of 7
7b7b
abströmseitige Schaufelkante von 7downstream blade edge of 7
88th
Rastmittel an 1 für 2Latch means on 1 for 2
99
Durchtrittsöffnung von 1 für 10Passage opening of 1 for 10
1010
Schraube zur Verbindung von 1 und 2Screw connecting 1 and 2
AA
gegenseitiger Abstand von 7 bzw. 7a (Fig. 4)mutual distance of 7 or 7a ( 4 )
BB
Breite von 4a, 4b, 4c, 4d, 4e (Fig. 4)width of 4a, 4b, 4c, 4d, 4e ( 4 )
HH
Gesamthöhe der Beschaufelung mit 7 (Fig. 6, 7)Overall height of blading with 7 ( Figures 6, 7 )
H1H1
größere Höhe von 7 (Fig. 3)greater height of 7 ( 3 )
H2H2
kleinere Höhe von 7 (Fig. 3)smaller height of 7 ( 3 )
LL
axiale Länge von 1 (Fig. 3, 5)axial length of 1 ( 3 , 5 )
R1R1
umfangsgemäße Krümmung von 7 in Richtung X-X (Fig. 3, 6)circumferential curvature of 7 in direction XX ( 3 , 6 )
R2R2
radiale Krümmung von 7b in Richtung X-X (Fig. 3, 7)radial curvature of 7b towards XX ( 3 , 7 )
TZTZ
Tangente an 7aTangent to 7a
TATA
Tangente an 7bTangent to 7b
VV
umfangsgemäßer Versatz von 7 gegeneinander (Fig. 4)circumferential offset of 7 to each other ( 4 )
X-XX-X
Längsachse von 1longitudinal axis of 1
µZµZ
Zuströmwinkel der Luft an 7 (zwischen TZ und X-X)Airflow angle at 7 (between T Z and XX)
µAµA
Abströmwinkel der Luft von 7 (zwischen TA und X-X)Air flow angle of 7 (between T A and XX)

Claims (13)

  1. Flow rectifier (1) for an axial fan (2), having a base body (3), which comprises a ring that is delimited radially inside and outside, in each case, by cylindrical curved surface areas (5, 6), said ring (4a, 4b, 4c, 4d, 4e) having a plurality of air guide blades (7), which are distributed in a circumferential direction about a longitudinal axis (X-X), and which are disposed in an essentially radial manner such that they extend between the curved surface areas (5, 6), wherein, when viewed in a circumferential direction, the air guide blades (7) extend with a curvature (R1) relative to the axial direction (X-X), in each case extending between an inflow-side blade edge (7a) and an outflow-side blade edge (7b), characterized in that two or more rings (4a, 4b, 4c, 4d, 4e) are provided in the base body (3), said rings having a plurality of air guide blades (7), which are distributed in a circumferential direction about the longitudinal axis (X-X), and which are disposed in an essentially radial manner such that they extend between the curved surface areas (5, 6), wherein two or more rings (4a, 4b, 4c, 4d, 4e) are provided in the base body (3), said rings having a plurality of in air guide blades (7), which are distributed in a circumferential direction about the longitudinal axis (X-X), and which are disposed in an essentially radial manner such that they extend between the curved surface areas (5, 6), wherein at least the outflow-side blade edge (7b) of the air guide blades (7) has a height that can be changed in a radial direction, wherein the outflow-side blade edge (7b) of the air guide blade (7), which has an adjustable height in the radial direction, has a curvature (R2), characterized in that the number of air guide blades (7) disposed within a ring (4a, 4b, 4c, 4d, 4e) decrease from ring (4a, 4b, 4c, 4d, 4e) to ring (4a, 4b, 4c, 4d, 4e) moving radially inward, so that almost the same spacing (A) between the respective air guide blades (7) exists in each ring (4a, 4b, 4c, 4d, 4e).
  2. Flow rectifier (1) according to Claim 1, characterized in that the blade edge (7a, 7b) has an adjustable height in the radial direction.
  3. Flow rectifier (1) according to one of the preceding claims, characterized in that the blade edge (7b) of the air guide blade (7), which has an adjustable height in the radial direction, has a circular arc-shaped curvature.
  4. Flow rectifier (1) according to one of the preceding claims, characterized in that, in the case of the curvature (R1) relative to the axial direction (XX), which each of the air guide blades (7) has, viewed in a circumferential direction, between the inflow-side blade edge (7a) thereof and the outflow-side blade edge (7b), the inflow angle (µZ) of the air to the air guide blade (7) is selected in such a way that said angle essentially corresponds to an outflow angle (µA) of the air out of the axial fan (2), on which the base body (3) is mounted, and in that the outflow angle (µA) of the air from the air guide blades (7) is selected in such a way that, in this region, the air guide blade (7) is designed such that it extends parallel to an air flow direction, which extends in the direction of the longitudinal axis (X-X).
  5. Flow rectifier (1) according to one of the preceding claims, characterized in that the respective inflow angle (µz) of the air is identical at all air guide blades (7).
  6. Flow rectifier (1) according to one of Claims 1 through 4, characterized in that the respective inflow angle (µz) of the air is identical at all of the air guide blades (7) that are located in a ring (4a, 4b, 4c, 4d, 4e), however said angle may differ from the respective inflow angle (µz) of the air at the air guide blades (7) in another ring (4a, 4b, 4c, 4d, 4e).
  7. Flow rectifier (1) according to Claim 6, characterized in that the respective inflow angle (µZ) of the air at the air guide blades (7) varies from ring (4a, 4b, 4c, 4d, 4e) to ring (4a, 4b, 4c, 4d, 4e) as a function of the outflow profile of the air leaving the axial fan (2).
  8. Flow rectifier (1) according to one of the preceding claims, characterized in that the base body (3) is designed one-part, and in particular designed as an injection-molded component, in particular made from plastic.
  9. Flow rectifier (1) according to one of the preceding claims, characterized in that in all of the rings (4a, 4b, 4c, 4d, 4e), openings between the air guide blades (7) are designed such that they are small enough and/or in particular, an axial height (H) of the assembly of the air guide blades (7) is designed such that it is large enough that it is not possible to reach a hand or an individual finger through to the rotating impeller.
  10. Flow rectifier (1) according to one of the preceding claims, characterized in that fasteners (8, 9) are provided on the base body (3) for releasable attachment to the axial fan (2), in particular a catch means (8) for connection to a wall ring (2a) associated with the axial fan (2) and/or mounting openings (9), through which screws (10) serving as the screw connection to the fan (2) may pass.
  11. Flow rectifier (1) according to one of the preceding claims, characterized in that in the radial sequence of the rings (4a, 4b, 4c, 4d, 4e) with the air guide blades (7), these rings (4a, 4b, 4c, 4d, 4e) each have different heights (H1, H2), in particular two heights (H1, H2), which each alternate from ring (4a, 4b, 4c, 4d, 4e) to ring (4a, 4b, 4c, 4d, 4e).
  12. Flow rectifier (1) according to Claim 11, characterized in that the respective course of the radial curvature (R2) of the blade edges (7b), using the height, which is adjustable height in the radial direction, may be adjusted, in particular on each blade (7), is designed such that the radial curvatures in adjacently located rings (4a, 4b, 4c, 4d, 4e) are a mirror image of one another.
  13. Flow rectifier (1) according to one of the preceding claims, characterized in that, in the radial sequence of the rings (4a, 4b, 4c, 4d, 4e), the inflowside blade edges (7a) and the outflow-side blade edges (7b) of the air guide blades (7) in the respective, adjacently located rings (4a, 4b, 4c, 4d, 4e) are disposed having a circumferential offset (V) relative to one another.
EP13765661.7A 2012-10-08 2013-08-27 Flow rectifier for an axial fan Active EP2904277B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012109542.6A DE102012109542A1 (en) 2012-10-08 2012-10-08 "Flow straightener for an axial fan"
PCT/EP2013/067691 WO2014056657A2 (en) 2012-10-08 2013-08-27 Flow rectifier for an axial fan

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EP2904277A2 EP2904277A2 (en) 2015-08-12
EP2904277B1 true EP2904277B1 (en) 2023-06-14

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CN (1) CN104685220B (en)
DE (1) DE102012109542A1 (en)
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US10094394B2 (en) 2018-10-09
WO2014056657A3 (en) 2014-10-02
DE102012109542A1 (en) 2014-04-10
CN104685220B (en) 2017-10-20
WO2014056657A2 (en) 2014-04-17
CN104685220A (en) 2015-06-03
EP2904277A2 (en) 2015-08-12
US20150330411A1 (en) 2015-11-19
WO2014056657A4 (en) 2014-11-13

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