EP3203084B1 - Fan wheel and blower unit - Google Patents
Fan wheel and blower unit Download PDFInfo
- Publication number
- EP3203084B1 EP3203084B1 EP16153807.9A EP16153807A EP3203084B1 EP 3203084 B1 EP3203084 B1 EP 3203084B1 EP 16153807 A EP16153807 A EP 16153807A EP 3203084 B1 EP3203084 B1 EP 3203084B1
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- EP
- European Patent Office
- Prior art keywords
- fan wheel
- carrier means
- rotation
- axis
- disc
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
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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
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
- F04D25/082—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation the unit having provision for cooling the motor
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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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
- F04D29/282—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
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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
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/5806—Cooling the drive system
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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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
Definitions
- the invention relates to a fan wheel for conveying a gaseous fluid, with a plurality of blades, which are arranged in a predeterminable angular division in an annular space volume around an axis of rotation and which are each fixed to carrier means with their axial, mutually opposite end regions, a first carrier means being a disk-shaped circular blank is formed coaxially to the axis of rotation and comprises a hub arrangement and wherein a second carrier means is designed as a ring coaxial to the axis of rotation and a spaced from the first carrier means is arranged a coaxial to the axis of rotation support plate which forms an annular gap with the first carrier means, the support disc of at least an inlet opening is penetrated, which enables a radially outward fluid flow in the annular gap.
- the invention further relates to a blower arrangement.
- an impeller with an inflow stabilizer which balances the fluid flow with a channel diffuser and is used in a centrifugal type rotary compressor.
- slots are formed in the side walls of flow separating vanes of a diffuser, which open into cavities within the vanes, the plurality of cavities communicating with a common one, closed by means of the openings in the diffuser wall trained distributors are connected and the fluid connections between the plurality of passages in the diffuser and the surrounding common distributor increases the operating range of the compressor, since pressure surges in one or more passages are quickly compensated for.
- the DE 33 10 376 A discloses a radial fan with a spiral housing and a fan wheel rotatably mounted in the spiral housing, a lateral inflow opening being provided in the spiral housing, an air gap or intermediate space being present between the inner wall of the spiral housing opposite the inflow opening and the fan wheel, the air gap or intermediate space being radial Direction is sealed in the radial end region of the fan wheel.
- a fan wheel for conveying a gaseous fluid which has a plurality of blades, which are arranged at a constant angular division about an axis of rotation, at least one blade having an edge region and an inner region and a bead extending therebetween along a course curve and / or the edge region of a first Blade area and the inner region are determined by a second blade area, which are arranged and / or configured in a geometrically different manner.
- the DE 10 2008 048 433 A1 discloses a radial fan with a closed fan wheel arranged in a housing, which can be connected via a hub to an output shaft of a motor, a first guide vane ring being arranged on one side of the fan wheel and a second guide vane ring being arranged on the side of the fan wheel facing away from it, wherein the second guide vane ring has a radial offset from the first guide vane ring towards the hub.
- a fan wheel can be designed as a radial fan wheel, in particular with backward-curved blades, or also as a drum impeller, as can be seen, for example, in US Pat DE 1 628 336 A is known.
- the drum impeller consists of a large number of narrow lamellae, which form the blades of the wheel and which are fastened between two end rings, the radius of which is substantially larger than the width of the lamellae, so that a drum-shaped construction is formed which is suitably connected to a Hub is connected, for example with the help of a circular plate which is attached to the fins at the center.
- the object of the invention is to provide a fan wheel with improved aerodynamics and improved strength properties, and a blower arrangement with an enlarged range of uses.
- a space volume of the annular gap delimited by the first support means and by the support disk has an axial extent along the axis of rotation that is considerably smaller than the axial extent of the annular space volume that is determined by the two support means and in which the blades are arranged are.
- the axial extent of the annular gap along the axis of rotation is particularly preferably less than 20 percent, in particular less than 10 percent, of the axial extent of the annular space volume. This ensures that a fluid flow that flows through the annular gap in the radial direction toward the outside when the fan wheel rotates about the axis of rotation is considerably less than a fluid flow that flows through the annular space volume in the radial direction to the outside.
- a mass flow of a main fluid flow through the annular space volume is at least 5 times, in particular at least 10 times larger than the mass flow of a secondary fluid flow through the annular gap.
- the fluid flow through the annular gap can be used to dissipate heat from a drive motor which is used to drive the fan wheel.
- the support disk is connected to the hub arrangement. This ensures an advantageous introduction of force and torque from the hub arrangement to the support disk, which ensures an advantageous flow of force in the fan wheel.
- the connection of the support disk to the hub arrangement simplifies the centering of the support disk required for an advantageous concentricity of the fan wheel.
- the support disk is connected directly to the first carrier means.
- the support disk and the first support means form a stable composite which, with a suitable design of the support disk and the first support means, leads to a considerable increase in the stability of the fan wheel, without the need for a considerably larger amount of material.
- the first carrier means which is typically formed as a stamped sheet-metal blank, in view of the connection to the support disk with a reduced one Material thickness is executed and the, preferably designed as a stamped sheet metal blank, has a material thickness which is similar to the material thickness of the first carrier means, in particular is identical to the material path of the first carrier means.
- the support disk and the first carrier are integrally connected to one another, for example by welding, in particular reader welding, and / or gluing.
- projections in particular beads, are formed on the support disk and / or on the first support means, each in the axial direction in the annular gap, which are fixed to an opposite surface of the support disk or the first support means.
- projections which can already be formed during the manufacture of the support disk, which is typically designed as stamped sheet-metal blanks, or the first carrier means, in addition to a stabilizing effect for the respective component (first carrier center, support disk), an inexpensive and precise spacing of the two components from one another is also possible .
- the projections are preferably geometrically adapted with a front side facing the respectively opposite surface to a geometry of the opposite surface, which can preferably be flat. In this way, a large-area support of the projections on the opposite component is ensured, so that the desired stable bond between the support disk and the first carrier can be created.
- the projections are designed in the radial direction Show main extension.
- the projections have a double function which, in addition to the precise spacing and stable connection of the support disk and the first carrier means, also comprises a guiding action for the fluid flowing through the annular gap.
- the projections are arranged on radial lines which extend outward from the axis of rotation in the radial direction.
- the projections assume an offset and / or an acute angle with the radial lines or are at least partially curved.
- the support disk is preferably penetrated by a plurality of inlet openings arranged at the same angular division from the axis of rotation, in particular congruently, between which radial spokes extend from the hub arrangement to a radially outer ring region of the support disk.
- the task of the inlet openings is to allow an axial inflow of fluid into the annular gap when the fan wheel rotates.
- the inlet openings are congruent, that is to say geometrically congruent, and are arranged at the same angular division with respect to the axis of rotation.
- the inlet openings are each delimited in the circumferential direction by radial spokes, which are preferably web-shaped and in particular extend along radial lines that extend radially outward from the axis of rotation. It can further be provided that the inlet openings are bordered by a radially inner, circular segment-shaped edge and / or by a radially outer, circular segment-shaped edge. It is expedient if guide projections, in particular beads, of the first carrier means extend along the radial spokes up to the radially outer ring region, in particular up to a maximum diameter of the radially outer ring region. This ensures a fluid guide function for the fluid flow in the annular gap.
- the fluid is always guided in an aerodynamically favorable manner with its flow movement starting from the inlet opening, which is formed in a radially inner region of the support disk, up to the radial exit from the annular gap with the aid of the respective guide projection.
- support projections in particular beads, which are arranged on the first support means and / or on the support disk and are arranged between adjacent guide projections and extend in the radial direction over the radially outer ring region and are fixed on an opposite surface of the support disk or the first support means are.
- These support projections serve as additional guide means for the fluid flow in the annular gap and also contribute to the formation of a stable combination of the support disk and the first carrier means.
- the support disk has, in a radially outer area, an at least partially circular projection that extends in an axial direction opposite to the annular gap.
- the task of the at least partially circular projection is to stabilize the support disk.
- the arrangement of the radial circumferential projection in the radially outer region of the support disk enables an advantageous combination between the desired stabilizing effect and the smallest possible Impairment of the fluid flow in the annular gap can be achieved.
- a projection is formed on the blades in a radially outer region, the longest edge of which makes an acute angle with the axis of rotation.
- the purpose of this projection on the blade is to stabilize the radially outer region of the blade, which is exposed to the greatest fluid forces when the fan wheel is used in a blower arrangement.
- this projection can also be used to advantageously influence the fluid flow through the annular space volume, this fluid flow, the production of which is the main task of the fan wheel, being considerably greater than the fluid flow through the annular gap.
- the longest edge of the projection on the blade is aligned parallel to a connecting line between an outer edge of the first carrier means designed as a disc-shaped circular blank and an inner edge of the second carrier means designed as a ring.
- a blower arrangement with a drive motor which has a drive shaft which is rotatably mounted on a motor housing comprises, as well as solved with a fan wheel according to any one of the preceding claims, wherein the fan wheel with the hub assembly is rotationally fixed to the drive shaft such that the support disc is arranged adjacent to the motor housing, so that when the fan wheel rotates about the axis of rotation, a fluid flow from the motor housing is effected in the direction of the support disc.
- the fan wheel is provided to provide a main fluid flow and a secondary fluid flow when rotating about the axis of rotation, the secondary fluid flow being able to be used, for example, to support heat dissipation from the drive motor.
- Fan wheel 1 shown in different views, is provided for conveying a gaseous fluid, in particular air, and can be used, for example, in an oven, not shown, where it is set in rotation by a drive motor, not shown, about a rotation axis 2 in order to circulate the Air volume located in the oven.
- the fan wheel 1 has, for example, a first carrier means designed as a disk-shaped circular blank 3 coaxial with the axis of rotation 2 and a second carrier means designed as a ring 4 coaxial with the axis of rotation 2, which are spaced along the axis of rotation 2 and arranged coaxially to one another.
- the ring 4 is designed with respect to the axis of rotation 2 as a rotating body with a J-shaped profile and forms an inflow nozzle for a main fluid flow which, when the fan wheel 1 rotates about the axis of rotation 2 in the radial direction outwards between the two carrier means 3 and 4 is promoted.
- a plurality of blades 5 arranged in predeterminable, in particular constant, angular pitch, the largest surface 6 of which extends between the round blank 3 and the ring 4.
- the largest surface 6 is flat and is arranged in a plane, not shown, which is delimited by the axis of rotation 2 and a radial line 7 extending transversely to the axis of rotation 2 in the radial direction.
- a projection 8 is formed on the largest surface 6, the longest edge 9 of which forms an acute angle 10 with the axis of rotation 2, as is the case here in the representation of the Figure 3 is indicated.
- each blade 5 has a tab 15, 16, which is oriented transversely to the largest surface 6 and with which the blade 5 is flat, both on an axial end region 11 facing the round plate 3 and on an axial end region 12 facing the ring 4. in particular cohesively, is fixed to the circular blank 3 or the ring 4.
- the longest edge 9 of the projection 8 is aligned at least substantially parallel to a connecting line 17 between a circular outer edge 18 of the round blank 3 and a circular inner edge 19 of the ring 4.
- the circular disc 3 is assigned a support disk 20 which is formed coaxially to the axis of rotation 2 and which forms an annular gap 21 with the circular disc 3.
- the support disk 20 is designed as a rotating body with respect to the axis of rotation 2 and is provided with a plurality of inlet openings 22, which are arranged, for example, in the same angular division to the axis of rotation 2. It can be provided that all inlet openings 22 have an identical cross-sectional geometry and are therefore congruent.
- the inlet openings 22 are arranged on the support disk 20 such that radial spokes 23 are formed between the inlet openings 22, which limit the inlet openings 22 in the circumferential direction and which connect an annular inner region 24 of the support disk 20 to an annular outer region 25 of the support disk 20.
- the inner region of the support disk is connected in a force-transmitting manner to a hub arrangement 26, which in turn is connected to the circular blank 3 in a force-transmitting manner.
- the hub arrangement 26 is designed as a shaft coupling, for example rotationally fixed attachment of the fan wheel 1 is set up on a drive shaft, not shown.
- a plurality of projections 27 and 28 facing the support disk 20 are formed on the round blank 3, which can be a stamped sheet-metal blank, which are implemented, for example, in the manner of beads.
- the projections 27 are guide projections which extend in the radial direction over almost the entire diameter of the round blank 3 and which are arranged such that they rest on the radial spokes 23 and the adjoining outer region 25 of the support disk 20.
- the projections 28 are designed as support projections which, for example, rest only on the outer region 25 of the support disk 20.
- Both the guide projections 27 and the support projections 28 have end faces 29 facing the support disk 20, which lie flat against a surface 30 of the support disk 20 facing the round blank 3 and are fixed there, for example, in a materially integral manner, in particular by gluing or welding.
- the guide projections 27 and the support projections 28 thus determine the distance 31 between the round blank 3 and the support disk 20 and thus also the volume of the annular gap 21.
- the distance 31 is selected to be considerably smaller than a distance 34 between the round blank 3 and the ring 4.
- both the guide projections 27 and the support projections 28 are aligned with a respective main extension along radial lines (not shown in more detail) which, starting from the axis of rotation 2, extend in the radial direction to the outside.
- the support disk 20 has in a radially outer region a circular circumferential projection 32 which extends axially in a direction away from the round blank 3 and which is provided as an exemplary triangular shaped bead for stabilizing the support disk 20.
- a concave depression is formed by the projection 32 when the rear side 33 of the fan wheel 1 is viewed, while the surface 30 of the support disk 20 facing the circular disc 3, with the exception of the projection 32, is of a flat design.
- the hub arrangement 26 enables the fan wheel 1 to be fixed in a rotationally fixed manner on a drive shaft, not shown, of a motor, in particular an electric motor.
- the fan wheel 1 is preferably arranged on the drive shaft such that the support disk 20 faces the motor, while the ring 4 faces away from the motor.
- a (secondary) fluid flow can be brought about through the annular gap 21, this (secondary) fluid flow, for example, heated air from the surroundings of the engine and can thus help cool the engine.
Description
Die Erfindung betrifft ein Ventilatorrad zur Förderung eines gasförmigen Fluids, mit mehreren Schaufeln, die in vorgebbarer Winkelteilung in einem ringförmigen Raumvolumen um eine Rotationsachse angeordnet sind und die mit ihren axialen, einander entgegengesetzten Endbereichen jeweils an Trägermitteln festgelegt sind, wobei ein erstes Trägermittel als scheibenförmige Ronde koaxial zur Rotationsachse ausgebildet ist und eine Nabenanordnung umfasst und wobei ein zweites Trägermittel als Ring koaxial zur Rotationsachse ausgebildet ist und wobei beabstandet zum ersten Trägermittel eine koaxial zur Rotationsachse ausgebildete Stützscheibe angeordnet ist, die mit dem ersten Trägermittel einen Ringspalt ausbildet, wobei die Stützscheibe von wenigstens einer Einlassöffnung durchsetzt ist, die einen radial nach außen gerichteten Fluidstrom im Ringspalt ermöglicht. Ferner betrifft die Erfindung eine Gebläseanordnung.The invention relates to a fan wheel for conveying a gaseous fluid, with a plurality of blades, which are arranged in a predeterminable angular division in an annular space volume around an axis of rotation and which are each fixed to carrier means with their axial, mutually opposite end regions, a first carrier means being a disk-shaped circular blank is formed coaxially to the axis of rotation and comprises a hub arrangement and wherein a second carrier means is designed as a ring coaxial to the axis of rotation and a spaced from the first carrier means is arranged a coaxial to the axis of rotation support plate which forms an annular gap with the first carrier means, the support disc of at least an inlet opening is penetrated, which enables a radially outward fluid flow in the annular gap. The invention further relates to a blower arrangement.
Aus der
Die
Aus der
Die
Ein Ventilatorrad kann als Radiallüfterrad, insbesondere mit rückwärtsgekrümmten Schaufeln, oder auch als Trommellaufrad ausgeführt sein, wie dies beispielsweise aus der
Die Aufgabe der Erfindung besteht darin, ein Ventilatorrad mit verbesserter Aerodynamik und verbesserten Festigkeitseigenschafen sowie eine Gebläseanordnung mit vergrößertem Einsatzspektrum bereitzustellen.The object of the invention is to provide a fan wheel with improved aerodynamics and improved strength properties, and a blower arrangement with an enlarged range of uses.
Diese Aufgabe wird gemäß einem ersten Erfindungsaspekt für ein Ventilatorrad der eingangs genannten Art mit den Merkmalen des Anspruchs 1 gelöst..This object is achieved according to a first aspect of the invention for a fan wheel of the type mentioned at the outset with the features of
Vorzugsweise ist vorgesehen, dass ein vom ersten Trägermittel und von der Stützscheibe begrenztes Raumvolumen des Ringspalts längs der Rotationsachse eine axiale Erstreckung aufweist, die erheblich kleiner als die axiale Erstreckung des ringförmigen Raumvolumens ist, das von den beiden Trägermitteln bestimmt wird und in dem die Schaufeln angeordnet sind. Besonders bevorzugt beträgt die axiale Erstreckung des Ringspalts längs der Rotationsachse weniger als 20 Prozent, insbesondere weniger als 10 Prozent, der axialen Erstreckung des ringförmigen Raumvolumens. Hierdurch wird gewährleistet, dass ein Fluidstrom, der bei einer Rotation des Ventilatorrads um die Rotationsachse den Ringspalt in radialer Richtung nach außen durchströmt, erheblich geringer ist als ein Fluidstrom, der das ringförmige Raumvolumen in radialer Richtung nach außen durchströmt. Beispielhaft ist davon auszugehen, dass ein Massenstrom eines Hauptfluidstroms durch das ringförmige Raumvolumen wenigstens 5-fach, insbesondere wenigstens 10-fach größer als Massenstrom eines Nebenfluidstroms durch den Ringspalt ist. Exemplarisch kann der Fluidstrom durch den Ringspalt für eine Wärmeabfuhr von einem Antriebsmotor genutzt werden, der zum Antrieb des Ventilatorrads eingesetzt wird.It is preferably provided that a space volume of the annular gap delimited by the first support means and by the support disk has an axial extent along the axis of rotation that is considerably smaller than the axial extent of the annular space volume that is determined by the two support means and in which the blades are arranged are. The axial extent of the annular gap along the axis of rotation is particularly preferably less than 20 percent, in particular less than 10 percent, of the axial extent of the annular space volume. This ensures that a fluid flow that flows through the annular gap in the radial direction toward the outside when the fan wheel rotates about the axis of rotation is considerably less than a fluid flow that flows through the annular space volume in the radial direction to the outside. As an example, it can be assumed that a mass flow of a main fluid flow through the annular space volume is at least 5 times, in particular at least 10 times larger than the mass flow of a secondary fluid flow through the annular gap. As an example, the fluid flow through the annular gap can be used to dissipate heat from a drive motor which is used to drive the fan wheel.
Zweckmäßig ist es, wenn die Stützscheibe mit der Nabenanordnung verbunden ist. Hierdurch wird eine vorteilhafte Kraft- und Drehmomenteinleitung von der Nabenanordnung auf die Stützscheibe gewährleistet, womit ein vorteilhafter Kraftfluss im Ventilatorrad sichergestellt wird. Darüber hinaus wird durch die Verbindung der Stützscheibe mit der Nabenanordnung die für einen vorteilhaften Rundlauf des Ventilatorrads erforderliche Zentrierung der Stützscheibe vereinfacht.It is expedient if the support disk is connected to the hub arrangement. This ensures an advantageous introduction of force and torque from the hub arrangement to the support disk, which ensures an advantageous flow of force in the fan wheel. In addition, the connection of the support disk to the hub arrangement simplifies the centering of the support disk required for an advantageous concentricity of the fan wheel.
Vorteilhaft ist es, wenn die Stützscheibe unmittelbar mit dem ersten Trägermittel verbunden ist. Durch diese Maßnahme bilden die Stützscheibe und das erste Trägermittel einen stabilen Verbund, der bei geeigneter Gestaltung von Stützscheibe und erstem Trägermittel zu einer erheblichen Steigerung der Stabilität des Ventilatorrads führt, ohne dass hierfür ein erheblich größerer Materialeinsatz erforderlich wäre. Dies gilt insbesondere dann, wenn das typischerweise als stanzgeprägter Blechzuschnitt ausgebildete erste Trägermittel angesichts der Verbindung mit der Stützscheibe mit einer reduzierten Materialstärke ausgeführt wird und die, vorzugsweise als stanzgeprägter Blechzuschnitt ausgebildete, Stützscheibe eine Materialstärke aufweist, die der Materialstärke des ersten Trägermittels ähnlich ist, insbesondere mit der Materialstrecke des ersten Trägermittels identisch ist. Vorzugsweise ist vorgesehen, dass die Stützscheibe und das erste Trägermittel stoffschlüssig miteinander verbunden sind, beispielsweise durch Schweißen, insbesondere Leserschweißen, und/oder Kleben.It is advantageous if the support disk is connected directly to the first carrier means. As a result of this measure, the support disk and the first support means form a stable composite which, with a suitable design of the support disk and the first support means, leads to a considerable increase in the stability of the fan wheel, without the need for a considerably larger amount of material. This applies in particular when the first carrier means, which is typically formed as a stamped sheet-metal blank, in view of the connection to the support disk with a reduced one Material thickness is executed and the, preferably designed as a stamped sheet metal blank, has a material thickness which is similar to the material thickness of the first carrier means, in particular is identical to the material path of the first carrier means. It is preferably provided that the support disk and the first carrier are integrally connected to one another, for example by welding, in particular reader welding, and / or gluing.
Erfindungsgemäß ist vorgesehen, dass an der Stützscheibe und/oder am ersten Trägermittel jeweils in axialer Richtung in den Ringspalt erstreckte Vorsprünge, insbesondere Sicken, ausgebildet sind, die an einer gegenüberliegenden Oberfläche der Stützscheibe oder des ersten Trägermittels festgelegt sind. Mit derartigen Vorsprüngen, die bereits bei der Herstellung der typischerweise als stanzgeprägte Blechzuschnitte ausgebildeten Stützscheibe bzw. des ersten Trägermittels ausgebildet werden können, ist neben einer Stabilisierungswirkung für die jeweilige Komponente (erstes Trägermitte, Stützscheibe) auch eine kostengünstige und präzise Beabstandung der beiden Komponenten zueinander möglich. Vorzugsweise sind die Vorsprünge geometrisch mit einer der jeweils gegenüberliegenden Oberfläche zugewandten Stirnseite auf eine Geometrie der gegenüberliegenden Oberfläche, die vorzugsweise eben ausgebildet sein kann, angepasst. Hierdurch wird eine großflächige Auflage der Vorsprünge an der jeweils gegenüberliegenden Komponente gewährleistet, so dass der angestrebte stabile Verbund zwischen Stützscheibe und erstem Trägermittel geschaffen werden kann.According to the invention, projections, in particular beads, are formed on the support disk and / or on the first support means, each in the axial direction in the annular gap, which are fixed to an opposite surface of the support disk or the first support means. With such projections, which can already be formed during the manufacture of the support disk, which is typically designed as stamped sheet-metal blanks, or the first carrier means, in addition to a stabilizing effect for the respective component (first carrier center, support disk), an inexpensive and precise spacing of the two components from one another is also possible . The projections are preferably geometrically adapted with a front side facing the respectively opposite surface to a geometry of the opposite surface, which can preferably be flat. In this way, a large-area support of the projections on the opposite component is ensured, so that the desired stable bond between the support disk and the first carrier can be created.
Bei einer vorteilhaften Weiterbildung der Erfindung ist vorgesehen, dass die Vorsprünge eine in radialer Richtung ausgebildete Haupterstreckung aufweisen. Hierdurch weisen die Vorsprünge eine Doppelfunktion auf, die neben der präzisen Beabstandung und stabilen Verbindung der Stützscheibe und des ersten Trägermittels auch eine Führungswirkung für das den Ringspalt durchströmende Fluid umfasst. Exemplarisch ist vorgesehen, dass die Vorsprünge auf Radiallinien angeordnet sind, die sich von der Rotationsachse in radialer Richtung nach außen erstrecken. Alternativ kann vorgesehen sein, dass die Vorsprünge einen Versatz und/oder einen spitzen Winkel mit den Radiallinien einnehmen oder zumindest bereichsweise gekrümmt ausgebildet sind.In an advantageous development of the invention, it is provided that the projections are designed in the radial direction Show main extension. As a result, the projections have a double function which, in addition to the precise spacing and stable connection of the support disk and the first carrier means, also comprises a guiding action for the fluid flowing through the annular gap. By way of example, it is provided that the projections are arranged on radial lines which extend outward from the axis of rotation in the radial direction. Alternatively, it can be provided that the projections assume an offset and / or an acute angle with the radial lines or are at least partially curved.
Bevorzugt ist die Stützscheibe von mehreren, in gleicher Winkelteilung zur Rotationsachse angeordneten, insbesondere kongruent ausgebildeten, Einlassöffnungen durchsetzt, zwischen denen Radialspeichen von der Nabenanordnung zu einem radial außenliegenden Ringbereich der Stützscheibe erstreckt sind. Die Aufgabe der Einlassöffnungen besteht darin, bei einer Rotation des Ventilatorrads einen axialen Zustrom von Fluid in den Ringspalt zu ermöglichen. Um einen vorteilhaften aerodynamischen Wirkungsgrad für den Fluidstrom im Ringspalt zu gewährleisten, ist insbesondere vorgesehen, dass die Einlassöffnungen kongruent, also geometrisch deckungsgleich, ausgebildet sind und hinsichtlich der Rotationsachse in gleicher Winkelteilung zueinander angeordnet sind. Die Einlassöffnungen werden in Umfangsrichtung jeweils von Radialspeichen begrenzt, die vorzugsweise stegförmig ausgebildet sind und sich insbesondere entlang von Radiallinien erstrecken, die ausgehend von der Rotationsachse in radialer Richtung nach außen verlaufen. Ferner kann vorgesehen sein, dass die Einlassöffnungen von einer radial innenliegend angeordneten, kreisabschnittsförmigen Kante und/oder von einer radial außenliegend angeordneten, kreisabschnittsförmigen Kante berandet werden. Zweckmäßig ist es, wenn Leitvorsprünge, insbesondere Sicken, des ersten Trägermittels entlang der Radialspeichen bis zum radial außenliegenden Ringbereich, insbesondere bis zu einem Maximaldurchmesser des radial außenliegenden Ringbereichs, erstreckt sind. Hierdurch wird eine Fluidleitfunktion für die Fluidströmung im Ringspalt gewährleistet. Hierbei wird das Fluid bei seiner Strömungsbewegung ausgehend von der Einlassöffnung, die in einem radial innenliegenden Bereich der Stützscheibe ausgebildet ist, bis zum radialen Austritt aus dem Ringspalt stets mit Hilfe des jeweiligen Leitvorsprungs in aerodynamisch günstiger Weise geführt.The support disk is preferably penetrated by a plurality of inlet openings arranged at the same angular division from the axis of rotation, in particular congruently, between which radial spokes extend from the hub arrangement to a radially outer ring region of the support disk. The task of the inlet openings is to allow an axial inflow of fluid into the annular gap when the fan wheel rotates. In order to ensure an advantageous aerodynamic efficiency for the fluid flow in the annular gap, it is provided in particular that the inlet openings are congruent, that is to say geometrically congruent, and are arranged at the same angular division with respect to the axis of rotation. The inlet openings are each delimited in the circumferential direction by radial spokes, which are preferably web-shaped and in particular extend along radial lines that extend radially outward from the axis of rotation. It can further be provided that the inlet openings are bordered by a radially inner, circular segment-shaped edge and / or by a radially outer, circular segment-shaped edge. It is expedient if guide projections, in particular beads, of the first carrier means extend along the radial spokes up to the radially outer ring region, in particular up to a maximum diameter of the radially outer ring region. This ensures a fluid guide function for the fluid flow in the annular gap. Here, the fluid is always guided in an aerodynamically favorable manner with its flow movement starting from the inlet opening, which is formed in a radially inner region of the support disk, up to the radial exit from the annular gap with the aid of the respective guide projection.
Bevorzugt ist vorgesehen, dass an dem ersten Trägermittel und/oder an der Stützscheibe jeweils zwischen benachbarten Leitvorsprüngen angeordnete, in radialer Richtung über den radial außenliegenden Ringbereich erstreckte Stützvorsprünge, insbesondere Sicken, ausgebildet sind, die an einer gegenüberliegenden Oberfläche der Stützscheibe oder des ersten Trägermittels festgelegt sind. Diese Stützvorsprünge dienen als zusätzliche Leitmittel für die Fluidströmung im Ringspalt und tragen auch zur Bildung eines stabilen Verbunds aus Stützscheibe und erstem Trägermittel bei.Provision is preferably made for support projections, in particular beads, which are arranged on the first support means and / or on the support disk and are arranged between adjacent guide projections and extend in the radial direction over the radially outer ring region and are fixed on an opposite surface of the support disk or the first support means are. These support projections serve as additional guide means for the fluid flow in the annular gap and also contribute to the formation of a stable combination of the support disk and the first carrier means.
In weiterer Ausgestaltung der Erfindung ist vorgesehen, dass die Stützscheibe in einem radial außenliegenden Bereich einen zumindest bereichsweise zirkular umlaufenden Vorsprung aufweist, der in einer dem Ringspalt entgegengesetzten Axialrichtung erstreckt ist. Die Aufgabe des zumindest bereichsweise zirkular umlaufenden Vorsprungs besteht in einer Stabilisierung der Stützscheibe. Durch die Anordnung des radialen umlaufenden Vorsprungs im radial außenliegenden Bereich der Stützscheibe kann eine vorteilhafte Kombination zwischen der angestrebten Stabilisierungswirkung und einer möglichst geringen Beeinträchtigung des Fluidstroms im Ringspalt erzielt werden.In a further embodiment of the invention, it is provided that the support disk has, in a radially outer area, an at least partially circular projection that extends in an axial direction opposite to the annular gap. The task of the at least partially circular projection is to stabilize the support disk. The arrangement of the radial circumferential projection in the radially outer region of the support disk enables an advantageous combination between the desired stabilizing effect and the smallest possible Impairment of the fluid flow in the annular gap can be achieved.
Bei einer vorteilhaften Weiterbildung der Erfindung ist vorgesehen, dass an den Schaufeln in einem radial außenliegenden Bereich ein Vorsprung ausgebildet ist, dessen längste Kante mit der Rotationsachse einen spitzen Winkel einnimmt. Die Aufgabe dieses Vorsprungs an der Schaufel besteht in einer Stabilisierung des radial außenliegenden Bereichs der Schaufel, der bei Verwendung des Ventilatorrads in einer Gebläseanordnung den größten Fluidkräften ausgesetzt ist. Ferner kann dieser Vorsprung auch zur vorteilhaften Beeinflussung des Fluidstroms durch das ringförmige Raumvolumen eingesetzt werden, wobei dieser Fluidstrom, dessen Erzeugung die Hauptaufgabe des Ventilatorrads ist, erheblich größer als der Fluidstrom durch den Ringspalt ist.In an advantageous development of the invention it is provided that a projection is formed on the blades in a radially outer region, the longest edge of which makes an acute angle with the axis of rotation. The purpose of this projection on the blade is to stabilize the radially outer region of the blade, which is exposed to the greatest fluid forces when the fan wheel is used in a blower arrangement. Furthermore, this projection can also be used to advantageously influence the fluid flow through the annular space volume, this fluid flow, the production of which is the main task of the fan wheel, being considerably greater than the fluid flow through the annular gap.
Vorteilhaft ist es, wenn die längste Kante des Vorsprungs an der Schaufel, insbesondere zumindest im Wesentlichen, parallel zu einer Verbindungslinie zwischen einer Außenkante des als scheibenförmige Ronde ausgebildeten ersten Trägermittels und einer Innenkante des als Ring ausgebildeten zweiten Trägermittels ausgerichtet ist. Hierdurch kann der Fluidstrom, der bei einer Rotation des Ventilatorrads das ringförmige Raumvolumen zwischen den beiden Trägermitteln durchsetzt und in radialer Richtung nach außen abströmt, in Richtung des radial außenliegenden, kreisringförmigen Austrittsspalts des Ringspalts gelenkt werden und damit den Fluidaustritt aus dem Ringspalt begünstigen.It is advantageous if the longest edge of the projection on the blade, in particular at least substantially, is aligned parallel to a connecting line between an outer edge of the first carrier means designed as a disc-shaped circular blank and an inner edge of the second carrier means designed as a ring. As a result, the fluid flow which, when the fan wheel rotates, passes through the annular space between the two carrier means and flows outward in the radial direction can be directed in the direction of the radially outer, circular exit gap of the annular gap and thus favor the fluid exit from the annular gap.
Die Aufgabe der Erfindung wird gemäß einem zweiten Erfindungsaspekt durch eine Gebläseanordnung mit einem Antriebsmotor, der eine drehbar an einem Motorgehäuse gelagerte Antriebswelle umfasst, sowie mit einem Ventilatorrad nach einem der vorhergehenden Ansprüche gelöst, wobei das Ventilatorrad mit der Nabenanordnung derart drehfest an der Antriebswelle festgelegt ist, dass die Stützscheibe benachbart zum Motorgehäuse angeordnet ist, so dass bei einer Rotationsbewegung des Ventilatorrads um die Rotationsachse ein Fluidstrom vom Motorgehäuse in Richtung der Stützscheibe bewirkt wird. Beispielhaft ist das Ventilatorrad dazu vorgesehen, bei einer Rotation um die Rotationsachse einen Hauptfluidstrom sowie einen Nebenfluidstrom bereitzustellen, wobei der Nebenfluidstrom beispielsweise dazu genutzt werden kann, eine Wärmeabfuhr vom Antriebsmotor zu unterstützen.According to a second aspect of the invention, the object of the invention is achieved by a blower arrangement with a drive motor which has a drive shaft which is rotatably mounted on a motor housing comprises, as well as solved with a fan wheel according to any one of the preceding claims, wherein the fan wheel with the hub assembly is rotationally fixed to the drive shaft such that the support disc is arranged adjacent to the motor housing, so that when the fan wheel rotates about the axis of rotation, a fluid flow from the motor housing is effected in the direction of the support disc. As an example, the fan wheel is provided to provide a main fluid flow and a secondary fluid flow when rotating about the axis of rotation, the secondary fluid flow being able to be used, for example, to support heat dissipation from the drive motor.
Eine vorteilhafte Ausführungsform der Erfindung ist in der Zeichnung dargestellt. Dabei zeigt:
Figur 1- eine perspektivische Vorderansicht eines Ventilatorrads, bei dem ein erstes Trägermittel als scheibenförmige Ronde und ein zweites Trägermittel als Ring jeweils koaxial zu einer Rotationsachse ausgebildet sind, wobei dem ersten Trägermittel eine koaxial zur Rotationsachse ausgebildete Stützscheibe zugeordnet ist und wobei zwischen den Trägermitteln in radialer Richtung ausgerichtete Schaufeln angeordnet sind,
Figur 2- eine perspektivische Schnittdarstellung des Ventilatorrads gemäß der
,Figur 1 Figur 3- eine seitliche Schnittdarstellung des Ventilatorrads gemäß der
, undFigur 1 Figur 4- eine perspektivische Rückansicht des Ventilatorrads gemäß der
.Figur 1
- Figure 1
- a perspective front view of a fan wheel, in which a first carrier means as a disc-shaped blank and a second carrier means as a ring are each formed coaxially with an axis of rotation, wherein the first carrier means is assigned a support disk formed coaxially with the axis of rotation and with blades aligned in the radial direction between the carrier means are arranged
- Figure 2
- a perspective sectional view of the fan wheel according to the
Figure 1 , - Figure 3
- a side sectional view of the fan wheel according to the
Figure 1 , and - Figure 4
- a rear perspective view of the fan wheel according to the
Figure 1 .
Ein in den
Das Ventilatorrad 1 weist exemplarisch ein als scheibenförmige Ronde 3 koaxial zur Rotationsachse 2 ausgebildetes erstes Trägermittel sowie ein als Ring 4 koaxial zur Rotationsachse 2 ausgebildetes zweites Trägermittel auf, die längs der Rotationsachse 2 beabstandet und koaxial zueinander angeordnet sind. Beispielhaft ist der Ring 4 bezogen auf die Rotationsachse 2 als Rotationskörper mit einem J-förmigen Profil ausgebildet und bildet eine Einströmdüse für einen Hauptfluidstrom, der bei einer Rotation des Ventilatorrads 1 um die Rotationsachse 2 in radialer Richtung nach außen zwischen den beiden Trägermitteln 3 und 4 gefördert wird.The
Zwischen der Ronde 3 und dem Ring 4 sind bezüglich der Rotationsachse 2 mehrere in vorgebbarer, insbesondere konstanter, Winkelteilung angeordnete Schaufeln 5 vorgesehen, deren größte Oberfläche 6 sich zwischen der Ronde 3 und dem Ring 4 erstreckt. Rein exemplarisch ist vorgesehen, dass die größte Oberfläche 6 eben ausgebildet ist und in einer nicht näher dargestellten Ebene angeordnet ist, die von der Rotationsachse 2 und einer quer zur Rotationsachse 2 in radialer Richtung erstreckten Radiallinie 7 begrenzt ist. Ferner ist rein exemplarisch vorgesehen, dass an der größten Oberfläche 6 ein Vorsprung 8 ausgebildet ist, dessen längste Kante 9 einen spitzen Winkel 10 mit der Rotationsachse 2 einnimmt, wie dies in der Darstellung der
Ferner ist rein exemplarisch vorgesehen, dass die längste Kante 9 des Vorsprungs 8 zumindest im Wesentlichen parallel zu einer Verbindungslinie 17 zwischen einer kreisförmigen Außenkante 18 der Ronde 3 und einer kreisförmigen Innenkante 19 des Rings 4 ausgerichtet ist.It is also provided purely by way of example that the
Der Ronde 3 ist eine koaxial zur Rotationsachse 2 ausgebildete Stützscheibe 20 zugeordnet, die mit der Ronde 3 einen Ringspalt 21 ausbildet. Rein exemplarisch ist die Stützscheibe 20 als Rotationskörper bezüglich der Rotationsachse 2 ausgebildet und mit mehreren Einlassöffnungen 22 versehen, die beispielhaft in gleicher Winkelteilung zur Rotationsachse 2 angeordnet sind. Dabei kann vorgesehen sein, dass sämtliche Einlassöffnungen 22 eine identische Querschnittgeometrie aufweisen und somit kongruent ausgebildet sind. Die Einlassöffnungen 22 sind exemplarisch derart an der Stützscheibe 20 angeordnet, dass zwischen den Einlassöffnungen 22 jeweils Radialspeichen 23 ausgebildet sind, die die Einlassöffnungen 22 in Umfangsrichtung begrenzen und die einen kreisringförmigen Innenbereich 24 der Stützscheibe 20 mit einem kreisringförmigen Außenbereich 25 der Stützscheibe 20 verbinden. Der Innenbereich der Stützscheibe ist mit einer Nabenanordnung 26 kraftübertragend verbunden, die ihrerseits mit der Ronde 3 kraftübertragend verbunden ist. Die Nabenanordnung 26 ist beispielhaft als Wellenkupplung ausgebildet, die für eine drehfeste Anbringung des Ventilatorrads 1 auf einer nicht dargestellten Antriebswelle eingerichtet ist.The
Rein exemplarisch sind an der Ronde 3, bei der es sich um einen stanzgeprägten Blechzuschnitt handeln kann, mehrere der Stützscheibe 20 zugewandte Vorsprünge 27 und 28 ausgebildet, die beispielhaft in der Art von Sicken verwirklicht sind. Bei den Vorsprüngen 27 handelt es sich um Leitvorsprünge, die sich nahezu über den gesamten Durchmesser der Ronde 3 in radialer Richtung erstrecken und die derart angeordnet sind, dass sie auf den Radialspeichen 23 und dem sich daran anschließenden Außenbereich 25 der Stützscheibe 20 aufliegen. Hingegen sind die Vorsprünge 28 als Stützvorsprünge ausgebildet, die beispielhaft nur auf dem Außenbereich 25 der Stützscheibe 20 aufliegen. Sowohl die Leitvorsprünge 27 als auch die Stützvorsprünge 28 weisen der Stützscheibe 20 zugewandte Stirnseiten 29 auf, die an einer der Ronde 3 zugewandten Oberfläche 30 der Stützscheibe 20 flächig anliegen und dort beispielsweise stoffschlüssig, insbesondere durch Kleben oder Schweißen, festgelegt sind. Damit bestimmen die Leitvorsprünge 27 und die Stützvorsprünge 28 den Abstand 31 zwischen der Ronde 3 und der Stützscheibe 20 und damit auch das Raumvolumen des Ringspalts 21. Dabei ist der Abstand 31 erheblich kleiner als ein Abstand 34 zwischen der Ronde 3 und dem Ring 4 gewählt, so dass bei einer Rotation des Ventilatorrads 1 um die Rotationsachse 2 ein von den Schaufeln 5 hervorgerufener (Haupt-)Fluidstrom, der durch den Ring 4 in axialer Richtung eintritt und in radialer Richtung zwischen Ronde 3 und Ring 4 nach außen austritt, erheblich größer als ein (Neben-)Fluidstrom durch den Ringspalt 21 ist, der durch die Einlassöffnungen 22 in axialer Richtung eintritt und in radialer Richtung nach außen zwischen der Ronde 3 und der Stützscheibe 20 austritt.By way of example only, a plurality of
Rein exemplarisch sind sowohl die Leitvorsprünge 27 als auch die Stützvorsprünge 28 mit einer jeweiligen Haupterstreckung entlang von nicht näher dargestellten Radiallinien ausgerichtet, die ausgehend von der Rotationsachse 2 in radialer Richtung nach außen verlaufen.As a purely exemplary example, both the
Wie aus der Darstellung der
Die Nabenanordnung 26 ermöglicht eine drehfeste Festlegung des Ventilatorrads 1 an einer nicht dargestellten Antriebswelle eines Motors, insbesondere eines Elektromotors. Vorzugsweise wird das Ventilatorrad 1 derart auf der Antriebswelle angeordnet, dass die Stützscheibe 20 dem Motor zugewandte ist, während der Ring 4 den Motor abgewandt ist. Hierdurch kann bei einer Rotation des Ventilatorrads 1 um die Rotationsachse 2 zusätzlich zu dem (Haupt-)Fluidstrom durch den Ring 4 ein (Neben-)Fluidstrom durch den Ringspalt 21 bewirkt werden, wobei dieser (Neben-)Fluidstrom beispielsweise erwärmte Luft aus der Umgebung des Motors abführen kann und dort damit zur Kühlung des Motors beiträgt.The
Claims (12)
- Fan wheel for conveying a gaseous fluid, having a plurality of blades (5) which are arranged in a predeterminable angular division in an annular spatial volume about an axis of rotation (2) and which are each fixed with their axial, mutually opposite end regions (11, 12) to carrier means (3, 4), wherein a first carrier means (3) is constructed as a disc-shaped circular blank which is coaxial with the axis of rotation (2) and comprises a hub arrangement (26) and wherein a second carrier means (4) is constructed as a ring which is coaxial with the axis of rotation (2), wherein a support disc (20) is arranged at a distance from the first carrier means (3), which support disc (20) is coaxial with the axis of rotation (2) and forms an annular gap (21) with the first carrier means (3), and wherein the support disc (20) is penetrated by at least one inlet opening (22) which allows a radially outwardly directed fluid flow in the annular gap (21), characterised in that projections (27, 28) extending in the axial direction into the annular gap (21) are formed on the supporting disc (20) and/or on the first carrier means (3) respectively, which are fixed to an opposite surface (30) of the supporting disc (20) or of the first carrier means (3).
- Fan wheel according to claim 1, characterized in that the supporting disk (20) is connected to the hub assembly (26) .
- Fan wheel according to claim 1 or 2, characterized in that the supporting disk (20) is directly connected to the first carrier means (3).
- Fan wheel according to claim 1, 2 or 3, characterized in that the projections (27, 28) are formed as beads.
- Fan wheel according to claim 1, 2, 3 or 4, characterized in that the projections (27, 28) have a main extension in the radial direction.
- Fan wheel according to one of the preceding claims, characterised in that the supporting disc (20) is penetrated by a plurality of inlet openings (22), which are arranged at the same angular pitch relative to the axis of rotation (2) and are in particular congruently formed, between which radial spokes (23) extend from the hub arrangement (26) to a radially outer annular region (25) of the supporting disc (20) .
- Fan wheel according to claim 6, characterised in that guide projections (27), in particular beads, of the first support means (3) are extended along the radial spokes (23) up to the radially outer annular region (25), in particular up to a maximum diameter of the annular region (25).
- Fan wheel according to claim 7, characterised in that supporting projections (28), in particular beads, are formed on the first carrier means (3) and/or on the supporting disk (20), each arranged between adjacent guide projections (27) and extending in the radial direction over the radially outer annular region (25), said supporting projections (28) being fixed to an opposite surface (30) of the supporting disk (20) or of the first carrier means (3).
- Fan wheel according to one of the preceding claims, characterised in that the supporting disc (20) has, in a radially outer region, a projection (32) which is circularly circumferential at least in regions and which extends in an axial direction opposite to the annular gap (21).
- Fan wheel according to one of the preceding claims, characterized in that a projection (8) is formed on each of the blades (5) in a radially outer region, the longest edge (9) of which projection (8) makes an acute angle (10) with the axis of rotation (2).
- Fan wheel according to claim 10, characterised in that the longest edge (9) of the projection (8) on the blade (5) is aligned, in particular at least substantially, parallel to a connecting line (17) between an outer edge (18) of the first carrier means (3) formed as a disc-shaped round plate and an inner edge of the second carrier means (4) formed as a ring.
- Blower arrangement with a drive motor, which comprises a drive shaft rotatably mounted on a motor housing, and with a fan wheel (1) according to one of the preceding claims, which is fixed to the drive shaft in a rotationally fixed manner with the hub arrangement (26) in such a way that the support disc (20) is arranged adjacent to the motor housing, so that a fluid flow is effected from the motor housing in the direction of the support disc (20) during a rotational movement of the fan wheel (1) about the axis of rotation (2).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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EP16153807.9A EP3203084B1 (en) | 2016-02-02 | 2016-02-02 | Fan wheel and blower unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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EP16153807.9A EP3203084B1 (en) | 2016-02-02 | 2016-02-02 | Fan wheel and blower unit |
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Publication Number | Publication Date |
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EP3203084A1 EP3203084A1 (en) | 2017-08-09 |
EP3203084B1 true EP3203084B1 (en) | 2020-07-15 |
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EP16153807.9A Active EP3203084B1 (en) | 2016-02-02 | 2016-02-02 | Fan wheel and blower unit |
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Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DK113512B (en) | 1965-09-08 | 1969-03-31 | Nordisk Ventilator | Centrifugal fan with drum impeller. |
US3414188A (en) * | 1966-11-25 | 1968-12-03 | American Radiator & Standard | Fan having hollow blades |
DE3310376A1 (en) * | 1983-03-22 | 1984-09-27 | Ebm Elektrobau Mulfingen Gmbh & Co, 7119 Mulfingen | Radial fan with spiral housing |
DE102008048433A1 (en) * | 2008-09-23 | 2010-03-25 | Daimler Ag | Rotary axial blower, has blower wheel closely arranged in housing and connected with drive shaft of motor, and two guide vanes arranged on opposite sides of blower wheel, where one of guide vanes has radial offset to hub |
ES2659780T3 (en) * | 2013-09-10 | 2018-03-19 | Punker Gmbh | Fan turbine |
-
2016
- 2016-02-02 EP EP16153807.9A patent/EP3203084B1/en active Active
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