EP2778425B1 - Double entry radial fan for an extractor hood - Google Patents

Double entry radial fan for an extractor hood Download PDF

Info

Publication number
EP2778425B1
EP2778425B1 EP14156132.4A EP14156132A EP2778425B1 EP 2778425 B1 EP2778425 B1 EP 2778425B1 EP 14156132 A EP14156132 A EP 14156132A EP 2778425 B1 EP2778425 B1 EP 2778425B1
Authority
EP
European Patent Office
Prior art keywords
fan
motor
housing
double entry
radial fan
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.)
Active
Application number
EP14156132.4A
Other languages
German (de)
French (fr)
Other versions
EP2778425A1 (en
Inventor
Robert Blaz
Ilhan GÜCLÜ
Christoph Häusig
Eugen Maurer
Gert Meinhardt
Daniel Metz
Peter Schlotmann
Thomas Wilde
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BSH Hausgeraete GmbH
Original Assignee
BSH Hausgeraete GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BSH Hausgeraete GmbH filed Critical BSH Hausgeraete GmbH
Priority to PL14156132T priority Critical patent/PL2778425T3/en
Publication of EP2778425A1 publication Critical patent/EP2778425A1/en
Application granted granted Critical
Publication of EP2778425B1 publication Critical patent/EP2778425B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08Centrifugal pumps
    • F04D17/16Centrifugal pumps for displacing without appreciable compression
    • F04D17/162Double suction pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
    • F04D25/0613Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator
    • 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
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226Fan casings
    • F04D29/424Double entry casings
    • 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
    • F04D29/62Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/626Mounting or removal of fans

Definitions

  • the present invention relates to a double-flow radial fan for an extractor hood.
  • the radial fan includes a spiral housing, a fan, a blower motor and an engine mount.
  • the fan is accommodated in the housing.
  • the blower motor drives the fan wheel.
  • the fan motor is supported within the fan by means of the engine mount.
  • US 2004/0253098 A1 describes a ventilation unit for a heating system, a ventilation system and an air conditioning system, which has a housing in which a radial fan is arranged, which is driven by an electric motor.
  • An object of the present invention is to allow the simplest possible installation of a double-flow radial fan for a cooker hood.
  • a double-flow radial blower for an extractor hood having a spiral housing, a fan wheel, a blower motor, and an engine mount.
  • the spiral housing has two detachably connected housing halves, each comprising an air outlet.
  • the fan is accommodated in the housing.
  • the blower motor drives the fan wheel.
  • the engine mount supports the blower motor inside the fan.
  • the engine mount supports the blower motor only on one half of the housing, with the engine mount flanged to an edge defining an air inlet thereof.
  • the radial fan thus formed is easy to install: First, the fan motor is connected to the engine mount. After this, the engine mount together with the blower motor is attached to a first housing half, wherein the engine mount is flanged to the edge. Thereafter, the fan is rotatably connected to the fan motor. Subsequently, a second housing half of the housing is releasably connected to the first housing half.
  • the spiral housing has a tangential air outlet.
  • the fan delivers air from the two axial air inlets to the tangential air outlet.
  • the axial air inlets are opposite.
  • the air inlets may be formed circular, wherein a central axis thereof coincides with the axis of rotation of the fan motor. "Axial”, “radial”, “tangential” and “circumferentially” herein refers to an axis of rotation of the fan motor.
  • At least one screw is provided for flanging the engine mount to the rim.
  • the at least one screw can connect a support arm of the engine mount with the edge.
  • exactly three screws can be provided, wherein a respective screw connects a respective support arm with the edge.
  • the at least one screw can be screwed directly into the material of the housing half. "Direct" means that no other material, in particular no bush, is provided between the thread of the screw and the housing half.
  • the fastening points in the circumferential direction are spaced differently far from each other.
  • the attachment points are therefore arranged on a circular line. This results in the asymmetrical arrangement of the attachment points in a simple manner. Accordingly, then support arms of the engine mount can be designed asymmetrically.
  • the edge for the flanging of the engine mount on at least one mounting aid is at least one mounting aid.
  • the mounting aid may be in the form of geometries corresponding to the engine mount.
  • the mounting aid is provided in the form of a semicircular web which is adapted to receive one end of a support arm of the engine mount. Accordingly, the web and the end of the support arm form corresponding geometries which are engaged with each other so as to facilitate the positioning of the engine mount. For example, by the interaction of the end of the support arm and the web, an unintentional rotation of the engine mount about the axis of rotation can be prevented.
  • the web may be formed as a stiffening rib stiffening the edge.
  • a shaft of the fan motor is screwed by means of a threaded portion thereof with the fan wheel.
  • the fan may be bolted to the shaft in the opposite direction to the direction of rotation of the shaft for driving the fan during operation of the radial fan.
  • the thread is tightened during operation of the radial fan increasingly or a release can be safely avoided.
  • the threaded bush for example, can be extrusion-coated with the material forming the fan wheel or positively or non-positively connected.
  • a shaft of the fan motor has a centering section, which engages in a corresponding centering section of the fan motor.
  • the two housing halves are releasably connected together along a rotational axis of the fan motor.
  • the fan wheel can also be easily inserted between two housing halves.
  • At least one clip is provided for releasably connecting the two housing halves.
  • a connection by means of a snap mechanism is also possible instead of the clip.
  • a snap mechanism for example, an elastic hook may be provided, which is first deformed elastically when connecting the housing halves and hereafter snapped behind a catch, wherein the hook is arranged on one housing half and the detent on the other housing half.
  • the housing halves have at least one pair of centering geometries corresponding to one another.
  • the one half of the housing may have a pin and the other half of the housing a hole corresponding to the pin.
  • the pin may also be conical and / or chamfered to facilitate insertion into the hole.
  • the pair of corresponding Zentriergeometrien groove and have.
  • an edge of a housing half comprise a circumferential groove, while the other housing half comprises a circumferential spring.
  • the engine mounting is designed in the form of a bearing plate which has a first holder for a bearing of a shaft of a rotor of the fan motor, a second holder for a stator of the fan motor and a plurality Has support arms, which are each flanged at their ends to the edge.
  • the engine mount thus has a dual function: on the one hand, it holds the engine within the fan and on the other hand, it forms the support of the stator and rotor to each other.
  • the support arms, the first holder and the second holder may be integrally formed with each other.
  • the engine mount may be made as a diecast part, in particular made of aluminum.
  • an extractor hood is provided with the above-described double-flow radial fan.
  • a method for mounting a double-flow radial blower in particular the radial blower described above, is provided. This includes the steps of: connecting a fan motor to an engine mount, attaching the engine mount to a first housing half of a housing, flanging the engine mount to an edge defining an air inlet of the first housing half, connecting a fan wheel to the blower motor and connecting a second housing half thereof Housing with the first housing half.
  • the radial fan 2 comprises a spiral-shaped housing 3, which is composed of a first and a second housing half 4, 5.
  • the first housing half 4 has an air inlet 6 and the second housing half 5 has an air inlet 7.
  • the air inlets 6, 7 are directly opposite.
  • the air inlets 6, 7 are each formed circular and have the same central axis 11.
  • the central axis 11 is coaxial with a rotation axis 12 of an in FIG. 1 shown fan 13 arranged. Consequently, the air inlets 6, 7 are axially oriented.
  • the air inlets 6, 7 are each bounded by a radial edge 14. In FIG. 2 only one edge 14 is shown. The other edge is in FIG. 2 covered.
  • the edge 14 forms an end face of a cylinder with a spiral base on which the shape of the housing 3 is based.
  • the edges 14 are connected to each other via an axial circumferential surface 15.
  • the lateral surface 15 is composed of a first jacket section 16, which is assigned to the first housing half 4, and a second jacket section 17, which is assigned to the second housing half 5.
  • the shell sections 16, 17 and thus the two housing halves 4, 5 can by means of a tongue and groove joint 21 in the axial direction (relative to the central axis 11 and the axis of rotation 12) engage with each other.
  • the tongue and groove connection 21 may be secured by brackets.
  • Such a bracket 22 is exemplified in FIG Fig. 6 shown.
  • the bracket 22 engages at its opposite ends 40 in the first and second housing half 4, 5.
  • the brackets 22 can also be solved again, so that a detachable connection of the two housing halves 4, 5 is achieved with each other.
  • the edge 14 is formed with attachment points 24 in the form of screw holes. These are arranged directly adjacent to the air inlet 6.
  • the air inlet 7 does not have the attachment points 24, since no attachment takes place on this.
  • the fastening points 24 are spaced apart from one another in the circumferential direction 25 (relative to the center axis 11 or the rotation axis 12), so that they are symmetrical with respect to any radials 26.
  • Each of the attachment points 24 is surrounded by a semicircular stiffening rib 27 which is open towards the air inlet 6.
  • the stiffening rib 27 serves as an assembly aid for a in FIG. 1 shown engine mount 31st
  • the engine mount 31 comprises a first holder 32 in the form of a bearing cup for holding a hidden and therefore provided with a dashed line with reference numerals Bearing 33.
  • a shaft 34 of a rotor 35 is mounted in the bearing 33.
  • the rotor 35 is part of a blower motor 36 in the form of an electronically commutated motor.
  • FIG. 4 shows in a section the attachment of the shaft 34 of the blower motor 36 to a bell 45 of the fan wheel 13.
  • the shaft 34 has at its end 46 a threaded portion 47, to which a centering 51 connects directly.
  • the centering portion 51 corresponds to a centering portion 52 of the fan wheel 13.
  • a bush 53 may be used, in which the threaded portion 47 of the shaft 34 is screwed.
  • the centering portion 52 may also be on the socket 53rd be educated.
  • the screwing of the fan 13 takes place in a direction opposite to the direction of rotation 57 of the fan 13 (s. Fig. 1 ) during operation of the radial fan 2 instead.
  • the connection between the bushing 53 and the bell 45 of the fan wheel 13 can be achieved by molding the bushing 53 or a non-positive and / or positive connection.
  • FIG. Fig. 7 shows a perspective view of an assembly of the two housing halves 4 and 5 according to a step 704th
  • FIG. 5 it is shown that in addition to the tongue and groove connection 21, a further pair of corresponding Zentriergeometrien in the form of a pin 55, which cooperates with a hole 56 may be provided.
  • the hole 56 is arranged on the housing half 4 and the pin 55 on the housing half 5 and can be axially brought into engagement with each other.
  • the hole 56 is shown in dashed lines, the in FIG. 5 is covered.
  • the pin 55 may be formed chamfered to the housing half 4 or rounded to facilitate insertion into the hole 56.

Description

Die vorliegende Erfindung betrifft ein doppelflutiges Radialgebläse für eine Dunstabzugshaube.The present invention relates to a double-flow radial fan for an extractor hood.

Beispielsweise ist aus der DE 90 16 767 U1 ein doppelflutiges Radialgebläse für eine Dunstabzugshaube bekannt. Das Radialgebläse umfasst ein spiralförmiges Gehäuse, ein Lüfterrad, einen Gebläsemotor und eine Motoraufhängung. Das Lüfterrad ist in dem Gehäuse aufgenommen. Der Gebläsemotor treibt das Lüfterrad an. Der Gebläsemotor ist innerhalb des Lüfterrads mittels der Motoraufhängung gehaltert.For example, is from the DE 90 16 767 U1 a double-flow centrifugal fan for a cooker hood known. The radial fan includes a spiral housing, a fan, a blower motor and an engine mount. The fan is accommodated in the housing. The blower motor drives the fan wheel. The fan motor is supported within the fan by means of the engine mount.

US 2004/0253098 A1 beschreibt eine Lüftungseinheit für ein Heizungssystem, ein Lüftungssystem und ein Klimasystem, welches ein Gehäuse aufweist, in dem ein Radialgebläse angeordnet ist, das mit einem Elektromotor angetrieben wird. US 2004/0253098 A1 describes a ventilation unit for a heating system, a ventilation system and an air conditioning system, which has a housing in which a radial fan is arranged, which is driven by an electric motor.

Eine Aufgabe der vorliegenden Erfindung besteht darin, eine möglichst einfache Montage eines doppelflutigen Radialgebläses für eine Dunstabzugshaube zu ermöglichen.An object of the present invention is to allow the simplest possible installation of a double-flow radial fan for a cooker hood.

Demgemäß wird ein doppelflutiges Radialgebläse für eine Dunstabzugshaube mit einem spiralförmigen Gehäuse, einem Lüfterrad, einem Gebläsemotor und einer Motoraufhängung bereitgestellt. Das spiralförmige Gehäuse weist zwei lösbar miteinander verbundene Gehäusehälften auf, die jeweils einen Luftauslass umfassen. Das Lüfterrad ist in dem Gehäuse aufgenommen. Der Gebläsemotor treibt das Lüfterrad an. Die Motoraufhängung haltert den Gebläsemotor innerhalb des Lüfterrads. Die Motoraufhängung haltert den Gebläsemotor ausschließlich an einer Gehäusehälfte, wobei die Motoraufhängung an einem einen Lufteinlass derselben begrenzenden Rand angeflanscht ist.Accordingly, there is provided a double-flow radial blower for an extractor hood having a spiral housing, a fan wheel, a blower motor, and an engine mount. The spiral housing has two detachably connected housing halves, each comprising an air outlet. The fan is accommodated in the housing. The blower motor drives the fan wheel. The engine mount supports the blower motor inside the fan. The engine mount supports the blower motor only on one half of the housing, with the engine mount flanged to an edge defining an air inlet thereof.

Das so ausgebildete Radialgebläse lässt sich einfach montieren: Zunächst wird der Gebläsemotor mit der Motoraufhängung verbunden. Hiernach wird die Motoraufhängung samt Gebläsemotor an einer ersten Gehäusehälfte befestigt, wobei die Motoraufhängung an dem Rand angeflanscht wird. Hiernach wird das Lüfterrad drehfest mit dem Gebläsemotor verbunden. Anschließend wird eine zweite Gehäusehälfte des Gehäuses mit der ersten Gehäusehälfte lösbar verbunden.The radial fan thus formed is easy to install: First, the fan motor is connected to the engine mount. After this, the engine mount together with the blower motor is attached to a first housing half, wherein the engine mount is flanged to the edge. Thereafter, the fan is rotatably connected to the fan motor. Subsequently, a second housing half of the housing is releasably connected to the first housing half.

Das spiralförmige Gehäuse weist einen tangentialen Luftauslass auf. Das Lüfterrad fördert Luft von den beiden axialen Lufteinlässen zu dem tangentialen Luftauslass. Die axialen Lufteinlässe liegen sich gegenüber. Die Lufteinlässe können kreisrund ausgebildet sein, wobei eine Mittelachse derselben mit der Drehachse des Gebläsemotors zusammenfällt. "Axial", "radial", "tangential" und "in Umfangsrichtung" bezieht sich vorliegend auf eine Drehachse des Gebläsemotors.The spiral housing has a tangential air outlet. The fan delivers air from the two axial air inlets to the tangential air outlet. The axial air inlets are opposite. The air inlets may be formed circular, wherein a central axis thereof coincides with the axis of rotation of the fan motor. "Axial", "radial", "tangential" and "circumferentially" herein refers to an axis of rotation of the fan motor.

Der Gebläsemotor kann als elektronisch kommutierter Elektromotor ausgebildet sein, welcher auch als bürstenloser Gleichstrommotor (BLDC) oder EC-Motor bezeichnet wird. Der Gebläsemotor umfasst einen Stator und einen Rotor. Der Rotor kann als Innenläufer ausgebildet sein. Der Rotor umfasst vorzugsweise eine Welle, welche das Lüfterrad antreibt.The blower motor can be designed as an electronically commutated electric motor, which is also referred to as a brushless DC motor (BLDC) or EC motor. The blower motor comprises a stator and a rotor. The rotor can be designed as an internal rotor. The rotor preferably comprises a shaft which drives the fan wheel.

"Ausschließlich an einer Gehäusehälfte" meint, dass die Motoraufhängung an keinem anderen Teil, insbesondere nicht an der anderen Gehäusehälfte gehaltert ist."Only on one half of the housing" means that the engine mount is not supported on any other part, in particular not on the other half of the housing.

Gemäß einer Ausführungsform ist für das Anflanschen der Motoraufhängung an dem Rand zumindest eine Schraube vorgesehen. Die zumindest eine Schraube kann einen Tragarm der Motoraufhängung mit dem Rand verbinden. Gemäß einer Ausführungsform können genau drei Schrauben vorgesehen sein, wobei eine jeweilige Schraube einen jeweiligen Tragarm mit dem Rand verbindet. Die zumindest eine Schraube kann direkt in das Material der Gehäusehälfte eingeschraubt sein. "Direkt" meint, dass kein anderes Material, insbesondere keine Buchse, zwischen dem Gewinde der Schraube und der Gehäusehälfte vorgesehen ist.According to one embodiment, at least one screw is provided for flanging the engine mount to the rim. The at least one screw can connect a support arm of the engine mount with the edge. According to one embodiment, exactly three screws can be provided, wherein a respective screw connects a respective support arm with the edge. The at least one screw can be screwed directly into the material of the housing half. "Direct" means that no other material, in particular no bush, is provided between the thread of the screw and the housing half.

Ferner sind Befestigungsstellen für das Anflanschen der Motoraufhängung an dem Rand asymmetrisch angeordnet. Die Motoraufhängung kann somit in nur einer vorbestimmten Orientierung an den Befestigungsstellen angeflanscht werden. Somit kann diese nicht versehentlich in falscher Orientierung montiert werden. Mit "asymmetrisch" ist gemeint, dass sich keine Symmetrieachse durch die Drehachse des Gebläsemotors finden lässt, bezüglich derer die Befestigungsstellen zueinander symmetrisch sind.Furthermore, attachment points for the flanging of the engine mount are arranged asymmetrically at the edge. The engine mount can thus be flanged in only one predetermined orientation at the attachment points. Thus, this can not be accidentally mounted in the wrong orientation. By "asymmetrical" is meant that no axis of symmetry can be found through the axis of rotation of the fan motor, with respect to which the attachment points are symmetrical to each other.

Gemäß einer weiteren Ausführungsform sind die Befestigungsstellen in Umfangsrichtung unterschiedlich weit voneinander beabstandet. Die Befestigungsstellen sind also auf einer Kreislinie angeordnet. Dadurch ergibt sich die asymmetrische Anordnung der Befestigungsstellen auf einfache Weise. Entsprechend können dann auch Tragarme der Motoraufhängung asymmetrisch ausgebildet sein.According to a further embodiment, the fastening points in the circumferential direction are spaced differently far from each other. The attachment points are therefore arranged on a circular line. This results in the asymmetrical arrangement of the attachment points in a simple manner. Accordingly, then support arms of the engine mount can be designed asymmetrically.

Gemäß einer weiteren Ausführungsform weist der Rand für das Anflanschen der Motoraufhängung zumindest eine Montagehilfe auf. Dadurch kann die Motoraufhängung einfach an dem Rand montiert werden. Beispielsweise kann die Montagehilfe in Form von mit der Motoraufhängung korrespondierenden Geometrien ausgebildet sein.According to a further embodiment, the edge for the flanging of the engine mount on at least one mounting aid. This allows the engine mount to be easily mounted on the edge. For example, the mounting aid may be in the form of geometries corresponding to the engine mount.

Gemäß einer weiteren Ausführungsform ist die Montagehilfe in Form eines halbkreisförmigen Stegs vorgesehen, welcher dazu ausgebildet ist, ein Ende eines Tragarms der Motoraufhängung aufzunehmen. Entsprechend bilden der Steg und das Ende des Tragarms korrespondierende Geometrien, welche miteinander in Eingriff gebracht werden, um so die Positionierung bzw. die Montage der Motoraufhängung zu erleichtern. Beispielsweise kann durch das Zusammenwirken des Endes des Tragarms und des Stegs ein ungewolltes Verdrehen der Motoraufhängung um die Drehachse verhindert werden. Beispielsweise kann der Steg als eine den Rand versteifende Versteifungsrippe ausgebildet sein.According to a further embodiment, the mounting aid is provided in the form of a semicircular web which is adapted to receive one end of a support arm of the engine mount. Accordingly, the web and the end of the support arm form corresponding geometries which are engaged with each other so as to facilitate the positioning of the engine mount. For example, by the interaction of the end of the support arm and the web, an unintentional rotation of the engine mount about the axis of rotation can be prevented. For example, the web may be formed as a stiffening rib stiffening the edge.

Gemäß einer weiteren Ausführungsform umgibt der Steg ein Schraubenloch für die zumindest eine Schraube. Beispielsweise kann das Schraubenloch auf der Sehne des Halbkreises angeordnet sein, welchen der Steg beschreibt.According to a further embodiment, the web surrounds a screw hole for the at least one screw. For example, the screw hole can be arranged on the chord of the semicircle which the web describes.

Gemäß einer weiteren Ausführungsform ist eine Welle des Gebläsemotors mittels eines Gewindeabschnitts derselben mit dem Lüfterrad verschraubt. Insbesondere kann das Lüfterrad mit der Welle gegensinnig zur Drehrichtung der Welle zum Antreiben des Lüfterrads im Betrieb des Radialgebläses verschraubt sein. Somit zieht sich das Gewinde im Betrieb des Radialgebläses zunehmend fest bzw. ein Lösen kann so sicher vermieden werden. In das Lüfterrad kann eine Gewindebuchse eingesetzt sein, in welche der Gewindeabschnitt eingeschraubt ist. Die Gewindebuchse kann beispielsweise mit dem das Lüfterrad bildenden Material umspritzt oder form- oder kraftschlüssig verbunden sein.According to a further embodiment, a shaft of the fan motor is screwed by means of a threaded portion thereof with the fan wheel. In particular, the fan may be bolted to the shaft in the opposite direction to the direction of rotation of the shaft for driving the fan during operation of the radial fan. Thus, the thread is tightened during operation of the radial fan increasingly or a release can be safely avoided. In the fan may be inserted a threaded bush into which the threaded portion is screwed. The threaded bush, for example, can be extrusion-coated with the material forming the fan wheel or positively or non-positively connected.

Gemäß einer weiteren Ausführungsform weist eine Welle des Gebläsemotors einen Zentrierabschnitt auf, welcher in einen korrespondierenden Zentrierabschnitt des Lüftermotors eingreift. Somit zentriert sich das Lüfterrad automatisch mit dem Aufschieben desselben auf die Welle.According to a further embodiment, a shaft of the fan motor has a centering section, which engages in a corresponding centering section of the fan motor. Thus, the fan wheel centered automatically with the sliding of the same on the shaft.

Gemäß einer weiteren Ausführungsform ist der Gewindeabschnitt an einem Ende der Welle angeordnet. Der Zentrierabschnitt schließt sich bevorzugt direkt an den Gewindeabschnitt an. Dadurch kann das Zentrieren und Aufschrauben in einem Schritt stattfinden.According to a further embodiment, the threaded portion is arranged at one end of the shaft. The centering section preferably connects directly to the threaded section. As a result, the centering and screwing can take place in one step.

Gemäß einer weiteren Ausführungsform sind die zwei Gehäusehälften entlang einer Drehachse des Gebläsemotors miteinander lösbar verbunden. Dadurch, dass zwei separate Gehäusehälften vorgesehen sind, können diese jeweils in einem einfachen Werkzeug beispielsweise durch Spritzgießen hergestellt werden. Aufgrund der lösbaren Verbindung der Gehäusehälften können diese zu Wartungszwecken voneinander getrennt werden, um so einen Zugriff auf das Lüfterrad freizugeben. Auch das Lüfterrad lässt sich einfach zwischen zwei Gehäusehälften einbringen.According to a further embodiment, the two housing halves are releasably connected together along a rotational axis of the fan motor. The fact that two separate housing halves are provided, they can each be made in a simple tool, for example by injection molding. Due to the detachable connection of the housing halves they can be separated from each other for maintenance purposes, so as to release access to the fan. The fan wheel can also be easily inserted between two housing halves.

Gemäß einer weiteren Ausführungsform ist für das lösbare Verbinden der zwei Gehäusehälften zumindest eine Klammer vorgesehen. Allerdings ist auch anstelle der Klammer eine Verbindung mittels eines Schnappmechanismusses möglich. Als Schnappmechanismus kann beispielsweise ein elastischer Haken vorgesehen sein, welcher beim Verbinden der Gehäusehälften zunächst elastisch verformt wird und hiernach hinter eine Rast schnappt, wobei der Haken an der einen Gehäusehälfte und die Rast an der anderen Gehäusehälfte angeordnet ist.According to a further embodiment, at least one clip is provided for releasably connecting the two housing halves. However, a connection by means of a snap mechanism is also possible instead of the clip. As a snap mechanism, for example, an elastic hook may be provided, which is first deformed elastically when connecting the housing halves and hereafter snapped behind a catch, wherein the hook is arranged on one housing half and the detent on the other housing half.

Gemäß einer weiteren Ausführungsform weisen die Gehäusehälften zumindest ein Paar miteinander korrespondierender Zentriergeometrien auf. Beispielsweise kann die eine Gehäusehälfte einen Zapfen und die andere Gehäusehälfte ein mit dem Zapfen korrespondierendes Loch aufweisen. Durch Ineinanderschieben von Zapfen und Loch werden die Gehäusehälften zueinander zentriert. Der Zapfen kann auch konisch und/oder mit einer Fase ausgebildet sein, um ein Einführen in das Loch zu erleichtern. Weiterhin kann das Paar korrespondierender Zentriergeometrien Nut und Feder aufweisen. So kann beispielsweise ein Rand der einen Gehäusehälfte eine umlaufende Nut umfassen, während die andere Gehäusehälfte eine umlaufende Feder umfasst. Durch axiales Ineinanderschieben werden Nut und Feder miteinander in Eingriff gebracht.According to a further embodiment, the housing halves have at least one pair of centering geometries corresponding to one another. For example, the one half of the housing may have a pin and the other half of the housing a hole corresponding to the pin. By telescoping pin and hole the housing halves are centered to each other. The pin may also be conical and / or chamfered to facilitate insertion into the hole. Furthermore, the pair of corresponding Zentriergeometrien groove and have. Thus, for example, an edge of a housing half comprise a circumferential groove, while the other housing half comprises a circumferential spring. By axial telescoping tongue and groove are brought into engagement.

Gemäß einer weiteren Ausführungsform ist die Motoraufhängung in Form eines Lagerschilds ausgebildet, welcher eine erste Halterung für ein Lager einer Welle eines Rotors des Gebläsemotors, eine zweite Halterung für einen Stator des Gebläsemotors und mehrere Tragarme aufweist, welche jeweils an ihren Enden an dem Rand angeflanscht sind. Beispielsweise können genau drei Tragarme vorgesehen sein. Die Motoraufhängung weist somit eine Doppelfunktion auf: Einerseits haltert sie den Motor innerhalb des Lüfterrads und andererseits bildet sie die Halterung von Stator und Rotor zueinander aus. Die Tragarme, die erste Halterung und die zweite Halterung können einstückig miteinander gebildet sein. Beispielsweise kann die Motoraufhängung als Druckgussteil insbesondere aus Aluminium hergestellt sein.According to a further embodiment, the engine mounting is designed in the form of a bearing plate which has a first holder for a bearing of a shaft of a rotor of the fan motor, a second holder for a stator of the fan motor and a plurality Has support arms, which are each flanged at their ends to the edge. For example, exactly three support arms can be provided. The engine mount thus has a dual function: on the one hand, it holds the engine within the fan and on the other hand, it forms the support of the stator and rotor to each other. The support arms, the first holder and the second holder may be integrally formed with each other. For example, the engine mount may be made as a diecast part, in particular made of aluminum.

Weiterhin wird eine Dunstabzugshaube mit dem vorstehend beschriebenen doppelflutigen Radialgebläse bereitgestellt.Furthermore, an extractor hood is provided with the above-described double-flow radial fan.

Ferner wird ein Verfahren zur Montage eines doppelflutigen Radialgebläses, insbesondere des vorstehend beschriebenen Radialgebläses, bereitgestellt. Dieses umfasst folgende Schritte: Verbinden eines Gebläsemotors mit einer Motoraufhängung, Befestigen der Motoraufhängung an einer ersten Gehäusehälfte eines Gehäuses, wobei die Motoraufhängung an einem einen Lufteinlass der ersten Gehäusehälfte begrenzenden Rand angeflanscht wird, drehfestes Verbinden eines Lüfterrads mit dem Gebläsemotor und Verbinden einer zweiten Gehäusehälfte des Gehäuses mit der ersten Gehäusehälfte.Furthermore, a method for mounting a double-flow radial blower, in particular the radial blower described above, is provided. This includes the steps of: connecting a fan motor to an engine mount, attaching the engine mount to a first housing half of a housing, flanging the engine mount to an edge defining an air inlet of the first housing half, connecting a fan wheel to the blower motor and connecting a second housing half thereof Housing with the first housing half.

Somit ergibt sich ein einfaches Montageverfahren. Die Reihenfolge der vorstehenden bezeichneten Schritte kann variiert werden.This results in a simple assembly process. The order of the above-mentioned designated steps can be varied.

Weitere mögliche Implementierungen der Erfindung umfassen auch nicht explizit genannte Kombinationen von zuvor oder im Folgenden bezüglich der Ausführungsbeispiele schriebenen Merkmale oder Ausführungsformen des doppelflutigen Radialgebläses, der Dunstabzugshaube oder des Verfahrens. Dabei wird der Fachmann auch Einzelaspekte als Verbesserungen oder Ergänzungen zu der jeweiligen Grundform der Erfindung hinzufügen oder abändern.Further possible implementations of the invention also include not explicitly mentioned combinations of features or embodiments of the double-flow radial blower, the extractor hood or of the method described above or below with regard to the exemplary embodiments. The skilled person will also add or modify individual aspects as improvements or additions to the respective basic form of the invention.

Weitere vorteilhafte Ausgestaltungen und Aspekte der Erfindung sind Gegenstand der Unteransprüche sowie der im Folgenden beschriebenen Ausführungsbeispiele der Erfindung. Im Weiteren wird die Erfindung anhand von bevorzugten Ausführungsformen unter Bezugnahme auf die beigelegten Figuren näher erläutert.Further advantageous embodiments and aspects of the invention are the subject of the dependent claims and the embodiments of the invention described below. Furthermore, the invention will be explained in more detail by means of preferred embodiments with reference to the attached figures.

Es zeigt dabei:

  • Fig. 1: in einer perspektivischen Ansicht ausschnittsweise eine Dunstabzugshaube gemäß einer Ausführungsform;
  • Fig. 2: in einer perspektivischen Ansicht ein Gehäuse der Dunstabzugshaube aus Fig. 1;
  • Fig. 3: eine vergrößerte Ansicht aus Fig. 1;
  • Fig. 4: in einem Schnitt die Befestigung einer Welle an einem Lüfterrad aus Fig. 1;
  • Fig. 5: das Radialgebläse aus Fig. 1 bei der Montage;
  • Fig. 6: ausschnittsweise die Gehäusehälften aus Fig. 5 in einem miteinander verbundenen Zustand; und
  • Fig. 7: ein Ablaufdiagramm einer Montage des Radialgebläses aus Fig. 1.
It shows:
  • Fig. 1 in a perspective view of a partial extractor hood according to an embodiment;
  • Fig. 2 : In a perspective view of a housing of the hood Fig. 1 ;
  • Fig. 3 : an enlarged view Fig. 1 ;
  • Fig. 4 : in a section, the attachment of a shaft on a fan Fig. 1 ;
  • Fig. 5 : the radial fan off Fig. 1 during installation;
  • Fig. 6 : Partially out of the housing halves Fig. 5 in an interconnected state; and
  • Fig. 7 a flow diagram of a mounting of the radial fan from Fig. 1 ,

In den Figuren bezeichnen gleiche Bezugszeichen gleiche oder funktionsgleiche Komponenten, soweit nichts anderes angegeben ist.In the figures, the same reference numerals designate the same or functionally identical components, unless stated otherwise.

Figur 1 zeigt in einer perspektivischen Ansicht ausschnittsweise eine Dunstabzugshaube 1 mit einem doppelflutigen Radialgebläse 2. FIG. 1 shows in a perspective view a detail of an extractor hood 1 with a double-flow radial fan. 2

Das Radialgebläse 2 umfasst ein spiralförmiges Gehäuse 3, welches sich aus einer ersten und einer zweiten Gehäusehälfte 4, 5 zusammensetzt.The radial fan 2 comprises a spiral-shaped housing 3, which is composed of a first and a second housing half 4, 5.

Figur 2 zeigt in einer perspektivischen Ansicht das Gehäuse 3 aus Figur 1 ohne die weiteren in Figur 1 gezeigten Komponenten. FIG. 2 shows in a perspective view of the housing 3 from FIG. 1 without the others in FIG. 1 shown components.

In Figur 2 ist weiter zu erkennen, dass die erste Gehäusehälfte 4 einen Lufteinlass 6 und die zweite Gehäusehälfte 5 einen Lufteinlass 7 aufweist. Die Lufteinlässe 6, 7 liegen sich direkt gegenüber. Die Lufteinlässe 6, 7 sind jeweils kreisrund ausgebildet und weisen dieselbe Mittelachse 11 auf. Die Mittelachse 11 ist koaxial mit einer Drehachse 12 eines in Figur 1 gezeigten Lüfterrads 13 angeordnet. Mithin sind die Lufteinlässe 6, 7 axial orientiert. Die Lufteinlässe 6, 7 werden jeweils von einem radialen Rand 14 begrenzt. In Figur 2 ist lediglich ein Rand 14 gezeigt. Der andere Rand ist in Figur 2 verdeckt. Der Rand 14 bildet eine Stirnseite eines Zylinders mit spiralförmiger Grundfläche, auf welchem die Form des Gehäuses 3 basiert. Die Ränder 14 sind über eine axiale Mantelfläche 15 miteinander verbunden. Die Mantelfläche 15 setzt sich aus einem ersten Mantelabschnitt 16, welcher der ersten Gehäusehälfte 4 zugeordnet ist, und einem zweiten Mantelabschnitt 17 zusammen, welcher der zweiten Gehäusehälfte 5 zugeordnet ist. Die Mantelabschnitte 16, 17 und damit die beiden Gehäusehälften 4, 5 können mittels einer Nut- und Federverbindung 21 in axialer Richtung (bezogen auf die Mittelachse 11 bzw. die Drehachse 12) miteinander in Eingriff stehen. Die Nut-Feder-Verbindung 21 kann durch Klammern gesichert sein. Eine solche Klammer 22 ist beispielhaft in Fig. 6 gezeigt. Die Klammer 22 greift an ihren gegenüberliegenden Enden 40 in die erste und zweite Gehäusehälfte 4, 5. Die Klammern 22 können auch wieder gelöst werden, so dass eine lösbare Verbindung der beiden Gehäusehälften 4, 5 miteinander erzielt wird.In FIG. 2 It can also be seen that the first housing half 4 has an air inlet 6 and the second housing half 5 has an air inlet 7. The air inlets 6, 7 are directly opposite. The air inlets 6, 7 are each formed circular and have the same central axis 11. The central axis 11 is coaxial with a rotation axis 12 of an in FIG. 1 shown fan 13 arranged. Consequently, the air inlets 6, 7 are axially oriented. The air inlets 6, 7 are each bounded by a radial edge 14. In FIG. 2 only one edge 14 is shown. The other edge is in FIG. 2 covered. The edge 14 forms an end face of a cylinder with a spiral base on which the shape of the housing 3 is based. The edges 14 are connected to each other via an axial circumferential surface 15. The lateral surface 15 is composed of a first jacket section 16, which is assigned to the first housing half 4, and a second jacket section 17, which is assigned to the second housing half 5. The shell sections 16, 17 and thus the two housing halves 4, 5 can by means of a tongue and groove joint 21 in the axial direction (relative to the central axis 11 and the axis of rotation 12) engage with each other. The tongue and groove connection 21 may be secured by brackets. Such a bracket 22 is exemplified in FIG Fig. 6 shown. The bracket 22 engages at its opposite ends 40 in the first and second housing half 4, 5. The brackets 22 can also be solved again, so that a detachable connection of the two housing halves 4, 5 is achieved with each other.

Nun zurückkehrend zu Figur 2 ist dort weiter gezeigt, dass das Gehäuse 3 einen radialen Luftauslass 23 aufweist. Das in Figur 1 gezeigte Lüfterrad 13 fördert Luft von den axialen Lufteinlässen 6, 7 zu dem Luftauslass 23, wobei die Luft umgelenkt und mit einer Druckdifferenz beaufschlagt wird.Now returning to FIG. 2 is further shown that the housing 3 has a radial air outlet 23. This in FIG. 1 shown impeller 13 conveys air from the axial air inlets 6, 7 to the air outlet 23, wherein the air is deflected and subjected to a pressure difference.

Der Rand 14 ist mit Befestigungsstellen 24 in Form von Schraubenlöchern gebildet. Diese sind direkt angrenzend an den Lufteinlass 6 angeordnet. Der Lufteinlass 7 weist die Befestigungsstellen 24 nicht auf, da keine Befestigung an diesem stattfindet. Die Befestigungsstellen 24 sind in Umfangsrichtung 25 (bezogen auf die Mittelachse 11 bzw. die Drehachse 12) unterschiedlich weit voneinander beabstandet, so dass sie bezüglich keiner Radialen 26 symmetrisch sind.The edge 14 is formed with attachment points 24 in the form of screw holes. These are arranged directly adjacent to the air inlet 6. The air inlet 7 does not have the attachment points 24, since no attachment takes place on this. The fastening points 24 are spaced apart from one another in the circumferential direction 25 (relative to the center axis 11 or the rotation axis 12), so that they are symmetrical with respect to any radials 26.

Jede der Befestigungsstellen 24 ist von einer halbkreisförmigen Versteifungsrippe 27 umgeben, welche zu dem Lufteinlass 6 hin offen ausgebildet ist. Die Versteifungsrippe 27 dient als Montagehilfe für eine in Figur 1 gezeigte Motoraufhängung 31.Each of the attachment points 24 is surrounded by a semicircular stiffening rib 27 which is open towards the air inlet 6. The stiffening rib 27 serves as an assembly aid for a in FIG. 1 shown engine mount 31st

Die Motoraufhängung 31 umfasst eine erste Halterung 32 in Form eines Lagertopfes zur Halterung eines verdeckten und daher mit gestrichelter Bezugszeichenlinie versehenen Lagers 33. In dem Lager 33 ist eine Welle 34 eines Rotors 35 gelagert. Der Rotor 35 ist Bestandteil eines Gebläsemotors 36 in Form eines elektronisch kommutierten Motors.The engine mount 31 comprises a first holder 32 in the form of a bearing cup for holding a hidden and therefore provided with a dashed line with reference numerals Bearing 33. In the bearing 33, a shaft 34 of a rotor 35 is mounted. The rotor 35 is part of a blower motor 36 in the form of an electronically commutated motor.

Die Motoraufhängung 31 umfasst ferner eine zweite Halterung 37, welche einen Stator 41 des Gebläsemotors 36 drehfest hält. Der Rotor 35 ist als Innenläufer ausgebildet.The engine mount 31 further includes a second bracket 37 which rotatably holds a stator 41 of the fan motor 36. The rotor 35 is designed as an internal rotor.

Die Motoraufhängung 31 umfasst ferner genau drei Tragarme 42, welche jeweils über ein Loch und eine entsprechende Schraube 43 an den Befestigungsstellen 24 (siehe Figur 2) angeflanscht sind. Die Motoraufhängung 31 ist somit ausschließlich an der Gehäusehälfte 4 befestigt. Die Tragarme 42 krümmen sich nach innen in das Lüfterrad 13 hinein, so dass der Gebläsemotor 36, insbesondere der Rotor 35 und der Stator 41, in axialer Richtung, also entlang der Drehachse 12 innerhalb des Lüfterrads 13 angeordnet ist. Außerdem ist der Gebläsemotor 36 konzentrisch innerhalb des Lufteinlasses 6 angeordnet. Die Motoraufhängung 31, insbesondere die erste Halterung 32, die zweite Halterung 37 und die Tragarme 42, ist einstückig beispielsweise in Form eines Aluminiumdruckgussteils gebildet.The engine mount 31 further comprises exactly three support arms 42, each having a hole and a corresponding screw 43 at the attachment points 24 (see FIG. 2 ) are flanged. The engine mount 31 is thus fastened exclusively to the housing half 4. The support arms 42 curve inwardly into the fan 13, so that the fan motor 36, in particular the rotor 35 and the stator 41, in the axial direction, ie along the axis of rotation 12 is disposed within the fan 13. In addition, the blower motor 36 is disposed concentrically within the air inlet 6. The engine mount 31, in particular the first holder 32, the second holder 37 and the support arms 42, is integrally formed, for example, in the form of an aluminum die-cast part.

Ein Ende 40 eines jeweiligen Tragearms 42 greift bei einer Montage der Motoraufhängung 31 axial in eine jeweilige Montagehilfe 27 axial ein. Ein versehentliches Drehen der Motoraufhängung in Umfangsrichtung 25 ist damit verhindert. Außerdem bewirkt die asymmetrische Anordnung der Befestigungsstellen 24, dass die Motoraufhängung 31 in nur genau einer Orientierung bezüglich des Gehäuses 3 montiert werden kann. Denn nur in der gewünschten Positionierung decken sich Schraubenlöcher 44 (gestrichelt in Figur 1, weil verdeckt) der Tragearme 42 mit den Schraubenlöchern 24 in dem Rand 14. Sodann können die Schrauben 43 durch die beiden Schraubenlöcher 44 und 24 geschraubt werden. Dies ist auch in Figur 3 zu erkennen, welche eine vergrößerte Ansicht aus Figur 1 zeigt.An end 40 of a respective support arm 42 axially engages in a mounting of the engine mount 31 axially into a respective mounting aid 27 axially. Accidental rotation of the engine mount in the circumferential direction 25 is prevented. In addition, the asymmetrical arrangement of the attachment points 24 causes the engine mount 31 to be mounted in only one orientation relative to the housing 3. Because only in the desired positioning screw holes cover 44 (dashed in FIG. 1 because hidden) of the support arms 42 with the screw holes 24 in the edge 14. Then, the screws 43 can be screwed through the two screw holes 44 and 24. This is also in FIG. 3 to recognize which is an enlarged view FIG. 1 shows.

Figur 4 zeigt in einem Schnitt die Befestigung der Welle 34 des Gebläsemotors 36 an einer Glocke 45 des Lüfterrads 13. Die Welle 34 weist an ihrem Ende 46 einen Gewindeabschnitt 47 auf, an welchen sich direkt ein Zentrierabschnitt 51 anschließt. Der Zentrierabschnitt 51 korrespondiert mit einem Zentrierabschnitt 52 des Lüfterrads 13. In das Lüfterrad 13 kann eine Buchse 53 eingesetzt sein, in welche der Gewindeabschnitt 47 der Welle 34 eingeschraubt ist. Der Zentrierabschnitt 52 kann ebenfalls an der Buchse 53 ausgebildet sein. Somit ergibt sich automatisch eine Zentrierung des Lüfterrads 13 bezüglich der Welle 34 beim Aufschieben des Zentrierabschnitts 52 auf den Zentrierabschnitt 51 beim Einschrauben des Gewindeabschnitts 47. Das Aufschrauben des Lüfterrads 13 findet in einer Richtung entgegen der Drehrichtung 57 des Lüfterrads 13 (s. Fig. 1) im Betrieb des Radialgebläses 2 statt. Die Verbindung zwischen der Buchse 53 und der Glocke 45 des Lüfterrads 13 kann durch Umspritzen der Buchse 53 oder eine kraft- und/oder formschlüssige Verbindung erzielt werden. FIG. 4 shows in a section the attachment of the shaft 34 of the blower motor 36 to a bell 45 of the fan wheel 13. The shaft 34 has at its end 46 a threaded portion 47, to which a centering 51 connects directly. The centering portion 51 corresponds to a centering portion 52 of the fan wheel 13. In the fan 13, a bush 53 may be used, in which the threaded portion 47 of the shaft 34 is screwed. The centering portion 52 may also be on the socket 53rd be educated. Thus, automatically centering of the fan 13 with respect to the shaft 34 when sliding the centering 52 on the centering 51 when screwing the threaded portion 47. The screwing of the fan 13 takes place in a direction opposite to the direction of rotation 57 of the fan 13 (s. Fig. 1 ) during operation of the radial fan 2 instead. The connection between the bushing 53 and the bell 45 of the fan wheel 13 can be achieved by molding the bushing 53 or a non-positive and / or positive connection.

Zu Beginn einer Montage des Radialgebläses 2 wird der Gebläsemotor 36 an der Motoraufhängung 31 in einem Schritt 701 (s. Fig. 7) montiert, wobei insbesondere der Rotor 35 in dem Lager 33 gelagert und der Stator 41 an der zweiten Halterung 37 befestigt wird. Hiernach wird die Motoraufhängung 31 in einem Schritt 702 an dem Rand 14 der Gehäusehälfte 4 mittels der Schrauben 43 angeflanscht. Die Welle 34 des Gebläsemotors 36 wird in einem Schritt 703 mit dem Lüfterrad 13 auf die im Zusammenhang mit Figur 4 beschriebene Weise verbunden. Figur 5 zeigt in einer perspektivischen Ansicht ein Zusammenfügen der beiden Gehäusehälften 4 und 5 gemäß einem Schritt 704.At the beginning of assembly of the radial fan 2, the blower motor 36 is attached to the engine mount 31 in a step 701 (see FIG. Fig. 7 ), wherein in particular the rotor 35 is mounted in the bearing 33 and the stator 41 is attached to the second holder 37. After that, the engine mount 31 is flanged at the edge 14 of the housing half 4 by means of the screws 43 in a step 702. The shaft 34 of the blower motor 36 is in a step 703 with the fan 13 on in connection with FIG. 4 connected manner described. FIG. 5 shows a perspective view of an assembly of the two housing halves 4 and 5 according to a step 704th

In Figur 5 ist insbesondere gezeigt, dass neben der Nut-Feder-Verbindung 21 ein weiteres Paar korrespondierender Zentriergeometrien in Form eines Zapfens 55, welcher mit einem Loch 56 zusammenwirkt, vorgesehen sein können. Dabei ist beispielsweise das Loch 56 an der Gehäusehälfte 4 und der Zapfen 55 an der Gehäusehälfte 5 angeordnet und können axial miteinander in Eingriff gebracht werden. Das Loch 56 ist gestrichelt dargestellt, das in Figur 5 verdeckt ist. Der Zapfen 55 kann zur Gehäusehälfte 4 hin angefast oder gerundet ausgebildet sein, um ein Einführen in das Loch 56 zu erleichtern.In FIG. 5 In particular, it is shown that in addition to the tongue and groove connection 21, a further pair of corresponding Zentriergeometrien in the form of a pin 55, which cooperates with a hole 56 may be provided. In this case, for example, the hole 56 is arranged on the housing half 4 and the pin 55 on the housing half 5 and can be axially brought into engagement with each other. The hole 56 is shown in dashed lines, the in FIG. 5 is covered. The pin 55 may be formed chamfered to the housing half 4 or rounded to facilitate insertion into the hole 56.

Durch axiales Verbinden der beiden Gehäusehälften 4, 5 durch ein axiales in Eingriffbringen der Nut-Feder-Verbindung 21 sowie der Zapfen-Loch-Verbindung 55, 56 und abschließendes Verklammern der beiden Gehäusehälften 4, 5 mittels der Klammern 22 miteinander, wird das Lüfterrad 13 sowie der Gebläsemotor 36 im Inneren des Gehäuses 3 positioniert.By axial connection of the two housing halves 4, 5 by an axial in engaging the tongue and groove joint 21 and the pin-hole connection 55, 56 and final clamping of the two housing halves 4, 5 by means of the brackets 22 with each other, the fan 13 and the blower motor 36 is positioned inside the housing 3.

Obwohl die Erfindung vorliegend anhand bevorzugter Ausführungsbeispiele beschrieben wurde, ist sie hierauf nicht beschränkt, sondern vielfältig modifizierbar.
Verwendete Bezugszeichen:

1
Dunstabzugshaube
2
Radialgebläse
3
Gehäuse
4
Gehäusehälfte
5
Gehäusehälfte
6
Lufteinlass
7
Lufteinlass
11
Mittelachse
12
Drehachse
13
Lüfterrad
14
Rand
15
Mantelfläche
16
Mantelabschnitt
17
Mantelabschnitt
21
Nut-Feder-Verbindung
22
Klammer
23
Luftauslass
24
Befestigungsstelle
25
Umfangsrichtung
26
Radiale
27
Rippe
31
Motoraufhängung
32
erste Halterung
33
Lager
34
Welle
35
Rotor
36
Gebläsemotor
37
zweite Halterung
40
Ende
41
Stator
42
Tragarm
43
Schraube
44
Schraubenloch
45
Glocke
46
Ende
47
Gewindeabschnitt
51
Zentrierabschnitt
52
Zentrierabschnitt
53
Buchse
55
Zapfen
56
Loch
57
Drehrichtung
Although the invention has been described herein with reference to preferred embodiments, it is not limited thereto, but variously modifiable.
Used reference signs:
1
Hood
2
centrifugal blower
3
casing
4
housing half
5
housing half
6
air intake
7
air intake
11
central axis
12
axis of rotation
13
fan
14
edge
15
lateral surface
16
shell section
17
shell section
21
Tongue and groove
22
clip
23
air outlet
24
fastening point
25
circumferentially
26
radial
27
rib
31
engine Mounts
32
first bracket
33
camp
34
wave
35
rotor
36
blower motor
37
second bracket
40
The End
41
stator
42
Beam
43
screw
44
screw hole
45
Bell jar
46
The End
47
threaded portion
51
centering
52
centering
53
Rifle
55
spigot
56
hole
57
direction of rotation

Claims (14)

  1. Double entry radial fan (2) for an extractor hood (1), with a spiral-shaped housing (3), which has two housing halves (4, 5) connected to one another in a detachable manner, which each comprise an air inlet (6, 7), a fan wheel (13), which is accommodated in the housing (3), a fan motor (36), which drives the fan wheel (13), and a motor suspension (31), which retains the fan motor (36) within the fan wheel (13), wherein the motor suspension (31) retains the fan motor (36) exclusively on one housing half (4) and is flanged on an edge (14) delimiting an air inlet (6) of the same, characterised in that the fastening points (24) for the flanging of the motor suspension (31) on the edge (14) are arranged asymmetrically.
  2. Double entry radial fan according to claim 1, characterised in that there is provision for at least one screw (43) for the flanging of motor suspension (31) on the edge (14).
  3. Double entry radial fan according to claim 1, characterised in that the fastening points (24) are spaced apart from each other at differing distances in the circumferential direction (25).
  4. Double entry radial fan according to one of claims 1 - 3, characterised in that the edge (14) for the flanging of the motor suspension (31) has at least one assembly aid (27).
  5. Double entry radial fan according to claim 4, characterised in that the assembly aid (27) is provided in the form of a semicircular projection, which is embodied to accommodate an end (40) of a support arm (42) of the motor suspension (31).
  6. Double entry radial fan according to claim 5, characterised in that the projection (27) surrounds a screw hole (24) for the at least one screw (43).
  7. Double entry radial fan according to one of claims 1 - 6, characterised in that a shaft (34) of the fan motor (36) is screwed to the fan wheel (13) by means of a threaded section (47) of the fan motor (36).
  8. Double entry radial fan according to one of claims 1 - 7, characterised in that a shaft (34) of the fan motor (36) has a centring section (51), which engages into a corresponding centring section (52) of the fan wheel (13).
  9. Double entry radial fan according to claim 8, characterised in that the threaded section (47) is arranged on an end (46) of the shaft (34) and the centring section (51) attaches thereto.
  10. Double entry radial fan according to one of claims 1 - 9, characterised in that the two housing halves (4, 5) are connected to one another in a detachable manner along an axis of rotation (12) of the fan motor (36).
  11. Double entry radial fan according to claim 10, characterised in that at least one clamp (22) is provided for the detachable connection of the two housing halves (4, 5).
  12. Double entry radial fan according to one of claims 1 - 11, characterised in that the two housing halves (4, 5) have at least one pair of centring geometries (21, 55, 56) corresponding to one another.
  13. Extractor hood (1) with a double entry radial fan according to one of claims 1 - 12.
  14. Method for the assembly of a double entry radial fan (2) according to one of claims 1 - 12, having the steps:
    Connection (701) of a fan motor (36) to a motor suspension (31),
    Fastening (702) of the motor suspension (31) to a first housing half (4) of a housing (3), wherein the motor suspension (31) is flanged on an edge (14) delimiting an air inlet (6) of the first housing half (4) and fastening points (24) for the flanging of the motor suspension (31) on the edge are arranged asymmetrically,
    Rotationally-fixed connection (703) of a fan wheel (13) to the fan motor (36), and
    Connection (704) of a second housing half (5) of the housing (3) to the first housing half (4).
EP14156132.4A 2013-03-11 2014-02-21 Double entry radial fan for an extractor hood Active EP2778425B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL14156132T PL2778425T3 (en) 2013-03-11 2014-02-21 Double entry radial fan for an extractor hood

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102013204085.7A DE102013204085A1 (en) 2013-03-11 2013-03-11 Double-flow radial fan for an extractor hood

Publications (2)

Publication Number Publication Date
EP2778425A1 EP2778425A1 (en) 2014-09-17
EP2778425B1 true EP2778425B1 (en) 2016-10-19

Family

ID=50159079

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14156132.4A Active EP2778425B1 (en) 2013-03-11 2014-02-21 Double entry radial fan for an extractor hood

Country Status (3)

Country Link
EP (1) EP2778425B1 (en)
DE (1) DE102013204085A1 (en)
PL (1) PL2778425T3 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105257582A (en) * 2015-11-23 2016-01-20 上海林内有限公司 Wind guiding motor supports and fan volute
ITUA20162311A1 (en) * 2016-04-05 2017-10-05 Elica Spa Hob with integrated hood.
DE102017112983A1 (en) * 2017-06-13 2018-12-13 Ebm-Papst Mulfingen Gmbh & Co. Kg Blower housing part with bearing support and blower
CN107449003B (en) * 2017-08-09 2023-08-22 佛山市南方丽特克能净科技有限公司 Fume separation and purification fan device
CN108443189A (en) * 2018-05-27 2018-08-24 东莞市兴东电子有限公司 A kind of low noise type blower
DE102019109401A1 (en) * 2019-04-10 2020-10-15 Miele & Cie. Kg Fan device for sucking in and diverting vapors below a hob, method for operating the fan device and hob

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3390832A (en) * 1967-03-27 1968-07-02 Gen Electric Heavy motor mounting for direct blower assembly
GB1168383A (en) * 1968-04-08 1969-10-22 Torin Corp Air Blower and method of assembly thereof
GB2234012A (en) * 1989-07-14 1991-01-23 Ibm Dc motor driven centrifugal fan
DE9016767U1 (en) 1990-12-12 1991-02-28 Ebm Elektrobau Mulfingen Gmbh & Co, 7119 Mulfingen, De
DE19841762C2 (en) * 1998-09-11 2002-07-18 Ebm Werke Gmbh & Co Kg Blower housing and radial blower
DE19950245C1 (en) * 1999-10-19 2001-05-10 Ebm Werke Gmbh & Co Kg Radial fan
US7108478B2 (en) * 2003-06-13 2006-09-19 American Standard International Inc. Blower housing and cabinet with improved blower inlet airflow distribution
ITMI20090048U1 (en) * 2009-02-19 2010-08-20 Faber Spa SAFETY IMPELLER FOR FANS
EP2365224B1 (en) * 2010-03-11 2018-04-04 Elica S.p.A. Radial conveyor for suction hoods

Also Published As

Publication number Publication date
DE102013204085A1 (en) 2014-09-11
PL2778425T3 (en) 2017-04-28
EP2778425A1 (en) 2014-09-17

Similar Documents

Publication Publication Date Title
EP2778425B1 (en) Double entry radial fan for an extractor hood
DE102013105524B4 (en) centrifugal fan
EP1895166B1 (en) Flow director for a fan
DE102012004617A1 (en) Axial
DE102014207461A1 (en) Arrangement of components of a fluid energy machine, joining method
EP2268902B1 (en) Strut for an intermediate turbine housing and intermediate turbine housing
EP2467606B1 (en) Vibrational decoupling of a driving motor
DE4222264C2 (en) Cooling device for a motor vehicle
EP2971792B1 (en) Housing for a radial fan of an extractor hood
EP2072827B1 (en) Canned motor pump
EP2778428A2 (en) Mounting arrangement for a radial fan for a suction hood
DE10109621B4 (en) Serial fan
DE102010053055A1 (en) Device for fastening fan to drive shaft of motor vehicle, has holding lugs spaced in circumferential direction and passing through three openings, which are formed through lugs of fan to obtain bayonet-fastening
WO2017000990A1 (en) Pump housing having a fastening structure
DE3804217A1 (en) AXIAL FAN
EP2778429B1 (en) Engine mount for a radial fan of a vapour extractor
DE102004005028A1 (en) Mounting arrangement, drive device, fan cowl and heat exchanger assembly
EP2971788B1 (en) Bearing shield for a blower motor of a radial fan of a range hood
EP1617086B1 (en) Support strut for protection grid and fabricating method thereof
DE10203406A1 (en) Electric motor and series
EP2963264B1 (en) Modular control valve
DE102006045797B4 (en) Pump and assembly process
EP2103472B1 (en) Attachment device, in particular for one or more fan
DE102009037920A1 (en) Motor vehicle air conditioning system has outer housing, inner housing arranged within outer housing and turbo machine driven by motor, where turbo machine is arranged within inner housing
EP4083435A1 (en) Fan housing and radial fan

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20140221

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: BSH HAUSGERAETE GMBH

R17P Request for examination filed (corrected)

Effective date: 20150317

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160530

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 838603

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161115

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502014001727

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20161019

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170119

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170120

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170220

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170228

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170219

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502014001727

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170119

26N No opposition filed

Effective date: 20170720

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170228

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170228

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20171031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170228

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20170228

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20140221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20161019

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 838603

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161019

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PL

Payment date: 20230208

Year of fee payment: 10

Ref country code: IT

Payment date: 20230228

Year of fee payment: 10

Ref country code: DE

Payment date: 20230228

Year of fee payment: 10