EP2122182B1 - Ventilator wheel, system and transmission line - Google Patents

Ventilator wheel, system and transmission line Download PDF

Info

Publication number
EP2122182B1
EP2122182B1 EP08707176.7A EP08707176A EP2122182B1 EP 2122182 B1 EP2122182 B1 EP 2122182B1 EP 08707176 A EP08707176 A EP 08707176A EP 2122182 B1 EP2122182 B1 EP 2122182B1
Authority
EP
European Patent Office
Prior art keywords
fan
air
guide ring
fan blades
axial
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
EP08707176.7A
Other languages
German (de)
French (fr)
Other versions
EP2122182A2 (en
Inventor
Steffen Leonhard
Steffen Saar
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.)
SEW Eurodrive GmbH and Co KG
Original Assignee
SEW Eurodrive GmbH and Co KG
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 SEW Eurodrive GmbH and Co KG filed Critical SEW Eurodrive GmbH and Co KG
Priority to PL08707176T priority Critical patent/PL2122182T3/en
Priority to EP17000355.2A priority patent/EP3214316B1/en
Publication of EP2122182A2 publication Critical patent/EP2122182A2/en
Application granted granted Critical
Publication of EP2122182B1 publication Critical patent/EP2122182B1/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
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/288Part of the wheel having an ejecting effect, e.g. being bladeless diffuser
    • 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
    • F04D29/70Suction grids; Strainers; Dust separation; Cleaning
    • F04D29/701Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps
    • F04D29/703Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps specially for fans, e.g. fan guards

Definitions

  • the invention relates to a fan, a system and a transmission series.
  • the DE 1 253 402 B discloses a noise reduction device on multi-bladed radial fans for ventilating electrical machines.
  • the fan blades are arranged irregularly according to a method described in more detail in the document, so that there are no adjacent pairs of fan blades which enclose the same angle.
  • a fan is known at the central hub fan blades are arranged at regular intervals.
  • the fan blades have a different curvature, so that their ends have irregular intervals.
  • a suction nozzle and an impeller for a fan with regularly arranged wings is known.
  • the suction nozzle has an elliptical cross section in a plane in which the axis of rotation of the fan is located.
  • the impeller is sheathed and has a similar elliptical cross-section as the suction nozzle.
  • the impeller is dimensioned such that after assembly of the fan, the sheath covers the stationary suction and rotates around it.
  • the fan has an inverted shell surrounding a hollow stump.
  • the hollow stump is connected to the shell by a set of oblique airfoils, the axial extent of the airfoils corresponding to the axial extent of the shell.
  • the fans consist of a radially outwardly open fan wheel, wherein a radially outwardly open annular air outlet opening is formed, which extends over the outer edges of the blades and rotates with the fan.
  • WO 97/09535 A discloses a radial impeller with regularly arranged fan blades, wherein the fan blades open in the radial direction are mounted between a front and a rear plate.
  • the fan blades are configured to extend radially farther outward on one of the two plates than on the other plate.
  • a fan which has a plurality of unevenly spaced fan blades, wherein the center of gravity of the fan wheel is located in the axis of rotation.
  • an axial fan in which the fan blades are arranged radially between a hub and a circumferential ring, wherein each adjacent fan blades have different distances from one another.
  • the invention is therefore the object of developing a fan, so that the environmental impact is reduced.
  • the object is achieved in the fan according to the features indicated in claim 1, in the system according to the features specified in claim 9 and in the transmission series according to the features indicated in claim 12.
  • a first fan blade has a first angular distance to a first circumferentially adjacent fan blade and the first fan blade has a second angular distance to a second fan blade adjacent in the opposite direction, wherein the first angular distance is smaller than the second angular distance
  • the sequence in the circumferential direction of the angular intervals of a respective wing to the next adjacent in the circumferential direction Fan blades at least two different types of angular distance values.
  • the fan blades are not necessarily arranged regularly.
  • the advantage here is that the fan blades produce periodic excitations whose main frequency component is lower than would be the case if all angular distances were equal. In particular, the frequency component is at most half that of a regular arrangement of the fan blades.
  • each air duct is limited by at least fan blades, an air guide ring and / or a base body, wherein the cross section of the air channel has a minimum in the course from inside to outside.
  • air ducts are formed with a nozzle effect. These nozzles advantageously cause a directed flow of cooling air.
  • the minimum of the cross section of the air duct is effected by a minimum of the distance between the base body and the air guide ring, in particular by a minimum of the distance between the sectional figures of the body with an axial plane on the one hand and the air guide ring with the axial plane on the other.
  • the fan wheel advantageously comprises a main body, fan blades and an air guide ring, wherein the base body has a frustoconical region and form at least two fan blades, a segment of the frusto-conical region and a segment of the air guide a radially extending air channel whose cross-section has a minimum in the radial course.
  • the advantage here is that the fan is easily manufacturable, since the geometric properties of the air duct, in particular the nozzle shape, with the boundary surfaces of air guide ring and body is easy to manufacture and controllable.
  • the main body of the fan is occupied in addition to its holding function with a Heilleitmaschine. As a result, parts can be saved.
  • the cross section of the air guide ring is convex on its inner side and concave on its outer side, in particular shaped such that the wall thickness is substantially constant.
  • the consistency of the wall thickness depends on the manufacturing tolerances of the production technology and on the speeds at which the fan is used.
  • the outer shape of the air guide thus follows substantially the inner shape of the air guide ring, and it is an advantageous form of the air guide at formed at the same time low material usage. The advantage here is that for the air guide little material must be used, so that its moment of inertia is minimized.
  • the base body has a frustoconical region and the air guide ring is concentrically inscribed in a mathematical cone such that the air guide touches the mathematical cone in a first and a second axial region and in a third axial region between air guide ring and the mathematical cone a minimum distance is provided, wherein the third axial region is arranged between the first axial region and the second axial region, and at least two fan blades, a segment of the frusto-conical region and a segment of the air guide ring form an outwardly extending air channel.
  • the advantage here is that the constructional and manufacturing technology easy to handle geometric shapes, a nozzle-like air duct is available.
  • each air channel is characterized by a geometric size
  • the sequence of the geometric size of the air ducts is an irregular sequence in one revolution of the fan.
  • the geometric size of each air duct is the angle between the limiting fan blades or the angle of a limiting fan blade a fan-fixed reference direction.
  • the geometric size of each air duct is the angular position of the center of gravity or the center plane of the air duct or the angle of an excellent direction of the air duct to a fan-fixed reference direction.
  • the center of gravity formed by all the fan blades is in the center of the fan.
  • the maximum axial extent of the fan blades is greater than the maximum axial extent of the air guide ring.
  • the maximum axial extent of the fan blades is more than twice as large as the maximum axial extent of the air guide ring.
  • the advantage here is that a radial or laterally oblique discharge of the cooling air is made possible.
  • the fan is used in various transmissions or in general systems with fan.
  • the maximum radial extent of the fan blades is greater than the minimum radial extent of the air guide ring.
  • the advantage here is that large air outlets are formed, can be conducted through the cooling air to the housing to be cooled.
  • the fan blades on the suction side are axially retracted up to a radius, in particular by more than one third of the maximum axial extent of the fan blades.
  • the advantage here is that at a small distance from the fan, a fan cover can be placed, wherein at the intake ports or air inlets generated by the fan blades noise can be reduced.
  • each fan blade on a plane of symmetry in which preferably the axis of rotation of the fan is.
  • a rotationally invariable fan wheel is formed in a simple manner, and cooling air always flows in the same direction through the air channels.
  • the radial extent of the base body is smaller than the outer diameter of the fan wheel, in particular at least fifteen percent smaller than the inner diameter of the air guide ring.
  • the air ducts each form an air outlet, which comprises a radially aligned and an axially aligned portion.
  • the fan on different transmissions, especially directly in front of a housing wall or on a Kegelradtopf operable.
  • a fan with a fan with fan blades and a fan cover is included, wherein the fan as described above according to the invention asuge distinct and wherein the fan cover surrounds the fan at least partially and the fan cover a Area having axial air inlets, wherein the fan blades in a first portion of the range with axial air inlets have a constant distance from the fan cover and in a second portion of the range with axial air inlets, the distance of the fan blades of the fan cover is greater than the constant distance in the first portion is, in particular, more than twice as large.
  • the fan blades extend radially beyond the region with axial air inlets.
  • the cooling air is particularly advantageous sucked.
  • the fan wheel is arranged on a shaft of the transmission, in particular of the driving shaft.
  • a separate motor for the drive of the fan is dispensable.
  • a fan wherein the fan as described above according to the invention asuge masculin and that the fan in a first variant on the driving shaft of a bevel gear is mounted and that the fan wheel is mounted in a second variant on the driving shaft of a spur gear.
  • air is preferably radially passable through air ducts and, in the second variant, air is directed through the air ducts at an angle to the radial direction and at an angle to the axial direction, in particular in an axial plane of the fan wheel obliquely to the axis of the fan wheel.
  • a housing wall of the transmission partially covers the air outlet of the air ducts in the first variant, in particular the axially oriented partial region of the air outlet.
  • FIG. 1 shows a fan for a fan of a transmission.
  • the fan wheel comprises at least one main body 10 with a hub 13, fan blades 11 and an air guide ring 12.
  • the fan is intended for mounting on a shaft of a gearbox.
  • the hub 13 is placed on the shaft for frictional connection with the same.
  • the fan wheel is driven by the shaft.
  • the shaft thus drives the fan blades 11, thereby producing an approximately radially or obliquely outwardly directed air flow.
  • This direction of the air flow is independent of the direction of rotation of the fan wheel, since each fan blade 11 has a plane of symmetry in which the axis of rotation of the fan wheel is located.
  • the main body 10, the air guide ring 12 and two adjacent fan blades 11 form air channels, is passed through the air flow.
  • FIG. 2 shows the back of the fan FIG. 1 , A support ring 20 of the main body 10 and the support edges 21 of each fan 11 are in a common plane.
  • the plane described is aligned parallel to the housing wall of the transmission and arranged at a small distance to this.
  • the fan with body, fan blades and guide ring is preferably made in one piece, in particular as a casting of aluminum or plastic, wherein in the case of use of plastic particularly preferably the plastic to avoid electrostatic charge is formed electrically conductive.
  • the fan is made of steel.
  • FIG. 3 shows a top view of the front of the fan after FIG. 1 ,
  • the fan blades 11 are mounted, wherein the fan blades 11 each have a plane of symmetry, which contains the axis of rotation of the fan.
  • the fan blades 11 are thus substantially, that is, apart from inclinations of the surfaces of the fan blades 11, perpendicular to an annular, truncated cone-shaped portion 35 of the body 10th
  • Each fan blade 11 is arranged with respect to a fan-fixed reference direction 36 each at an angle w1.
  • the fan blades 11 are irregularly arranged: In particular, the difference amounts of each two angles w1 can not be represented as an integer multiple of a basic amount. Thus, resonance excitations are reduced by the fan blades 11, in particular, the frequency of the resonance excitations is reduced.
  • the fan is mounted on a gear shaft and the number of fan blades and the number of teeth of the gear shaft of the gear shaft have no common divider.
  • the number of fan blades and the number of teeth of each gear of the transmission has no common divider.
  • the fan wheel on a mirror symmetry plane, in which preferably the axis of rotation of the fan wheel is included.
  • the outer diameter of the main body 10 in FIG. 3 is much smaller than the outer diameter of the fan selected.
  • the outer diameter of the base body 10 is two-thirds of the outer diameter of the fan and thus of the air guide ring 12, and more preferably, the outer diameter of the base body 10 relative to the inner diameter of the air guide ring 12 is reduced by ten to twenty percent.
  • favorable flow conditions for the fan can be achieved.
  • the air guide ring 12 is composed of a first guide ring 33 and a second guide ring 34, which are each designed to be annular and frusto-conical.
  • the opening angle of the second guide ring 34 is selected larger than the opening angle of the first guide ring 33.
  • a first fan blade 31, a second fan blade 32, a segment 30 of the frusto-conical region 35 of the base body 10 and a segment 37 of the air guide ring 12 enclosed by the two fan blades 31, 32 form an air channel through which air flows during operation.
  • Each of these air ducts formed in this way has an opening angle or angular distance w2, ie the angle between the delimiting fan blades 31, 32, ie between two nearest neighbors, and an angle w3 of the center plane of the air duct with respect to a reference direction 36.
  • the opening angle w2 results thus in each case from the difference of the angle w1 to the limiting fan blades 31, 32.
  • the angle w3 differs in the example according to the FIG. 3 from the angles w1 to the limiting fan blades 31, 32 each by a constant, that is independent of the number of fan blades, amount.
  • the sequence of opening angles w2 and the sequence of angles w3 defines an irregular sequence of numbers.
  • FIG. 4 shows a sectional view taken along in FIG FIG. 4 with AA designated axial plane.
  • the fan blades 11 have approximately rectangular recesses 40, so that the fan blades 11 in operation at a first area in the FIG. 4 from the top to be mounted fan cover at a shorter distance than in a second area.
  • This second area contains air inlets for the air supply to the fan wheel, and by the recess 40 periodic vibration excitations at the air inlets are avoided by a Vorbeistich the fan blades 10 in close proximity.
  • the main body 10 comprises at least one hub 13 for non-positive connection of the impeller on a shaft and a frusto-conical portion 35.
  • This frusto-conical portion 35 forms with the first guide ring 33 and the second guide ring 34 a nozzle-shaped air passage, wherein the nozzle-like constriction is approximately at the minimum Distance m is formed by air guide ring 12 and body 12.
  • This minimum distance m causes a minimum cross-section of the air channel delimited by a segment of the air guide ring 12, a segment of the frusto-conical region 35 and two adjacent fan blades 11, this cross section being assumed to be approximately at the same position as the minimum distance.
  • the exact position of the minimum cross section with respect to the minimum distance depends on the specific configuration of the cross section of the air guide ring 12 and the frusto-conical region.
  • the air guide ring 12 is formed at least from a first guide ring 33 and a second guide ring 34, wherein the opening angle of the frusto-conical first guide ring 33 is smaller than the opening angle of the frusto-conical second guide ring 34.
  • First guide ring 33 and second guide ring 34 are connected along a concentric ring.
  • the design of the opening angle of the guide rings 33, 34 is such that the air guide ring 12 can be inscribed in a conical surface 42, wherein the conical surface 42 touches the air guide ring 12 at two concentric cutting circles 43, 44, the conical surface 42 but not the interior of the air guide ring 12 cuts.
  • the air guide ring 12 thus has an axial cross section, whose outer contour is concave.
  • a convex surface is formed on the inner side of the air guide ring 12 facing the shaft, where convex the property that the connecting line of two points on the inside of the air guide ring 12 always runs at least partially inside the air guide ring 12.
  • the inner contour of the cross section of the air guide ring 12 is thus curved with opposite signs as the outer contour of the cross section of the frusto-conical portion 35, in particular its radial outlet. Both contours are thus convex, with the convexities facing each other.
  • first guide ring 33 and second guide ring 34 results in a constriction and a minimum distance m, which causes a nozzle effect in the associated air duct.
  • the inside of the air guide ring is convex, but not described by two connected truncated cones, but by, for example, a parabolic or a circular arc-shaped cross-sectional contour. Even in these cases, a resulting cross-sectional constriction causes a nozzle effect with which an air flow can be conducted.
  • the air guide ring 12 does not extend axially over the entire length of the fan, in particular the fan blades 11. Rather, the second guide ring 34 terminates at an axial distance from the plane defined by the support ring 20. In this way, a radial opening 41 is formed for the air ducts through which - in the assembled state - air in the radial direction along the housing wall of the transmission can be conducted.
  • FIG. 5 shows a gear 50 with mounted fan 57.
  • a fan cover 51 surrounds the fan. For illustration is in FIG. 5 only one half of the fan cowl 51 is shown.
  • the hub 13 of the fan wheel sits on an intermediate part 54 and is non-positively connected thereto, wherein the intermediate part 54 in turn is arranged on a shaft 53 of the transmission and is at least positively connected thereto.
  • the shaft 53 is the driving shaft of the transmission 50.
  • the fan cover 51 has an annular area with air inlets 55, through which the fan draws air.
  • the axial orientation of the fan blades 11 causes, regardless of the direction of rotation is sucked in the same axial direction.
  • the suction side of the fan is clearly defined as the side through which the air flows.
  • the air ducts have an opening through which air therefore exits independently of the direction of rotation. Thus, an air outlet is formed.
  • the diameter of the area with air inlets 55 is equal to the inner diameter of the first guide ring 33.
  • the fan blades 11 strip past the air inlets 55 during a rotational movement.
  • the fan blades 11 each have a recess 40, so that only a portion of the area of the air inlets 55 is swept by the fan blades 11 at a small distance, while another, radially further inboard portion is covered at a greater distance.
  • the radial extent of the radially further inner subregion is greater than the radial extent of the radially outer subregion.
  • FIG. 6 shows the fan FIG. 5 in a side view.
  • the fan wheel is mounted above a bevel gear pot 61.
  • a gap 60 is provided between the fan cover 51 and the first guide ring 33.
  • the recess 40 of the fan blades 11 in the axial direction is about twice as long as the axial extent of the gap 60th
  • the provided along the radial boundary edge 22 of the fan blades 11 withdrawal of the second guide ring 34 allows mounting of the fan on a shaft which protrudes from a side wall of the transmission 50.
  • the fan is mounted directly in front of this side wall, and the moving of the fan blades 11 air flows radially outwards and thus along the housing wall.
  • the housing wall covers a portion of the air outlet of the air ducts, namely that portion which is axially aligned, the surface normal is thus arranged parallel to the shaft axis.
  • a series is formed in whose variants, such components that form the fan, in particular the fan, are uniformly used.
  • the variety of parts of the series is reduced.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

Die Erfindung betrifft einen Lüfterrad, ein System und eine Getriebebaureihe.The invention relates to a fan, a system and a transmission series.

Die DE 1 253 402 B offenbart eine Einrichtung zur Geräuschminderung an vielschaufligen Radiallüftern zum Belüften elektrischer Maschinen. Die Lüfterschaufeln sind nach einer in der Druckschrift näher beschriebenen Methode unregelmäßig angeordnet, so dass es keine benachbarten Paare von Lüfterschaufeln gibt, welche den gleichen Winkel einschließen.The DE 1 253 402 B discloses a noise reduction device on multi-bladed radial fans for ventilating electrical machines. The fan blades are arranged irregularly according to a method described in more detail in the document, so that there are no adjacent pairs of fan blades which enclose the same angle.

Aus der WO 91/02165 A ist ein Lüfter bekannt, an dessen zentraler Nabe Lüfterschaufeln im regelmäßigen Abstand angeordnet sind. Die Lüfterschaufeln weisen eine unterschiedliche Krümmung auf, so dass deren Ende unregelmäßige Abstände aufweisen.From the WO 91/02165 A a fan is known at the central hub fan blades are arranged at regular intervals. The fan blades have a different curvature, so that their ends have irregular intervals.

Aus der US 5 478 201 A ist eine Ansaugdüse und ein Flügelrad für einen Lüfter mit regelmäßig angeordneten Flügeln bekannt. Die Ansaugdüse hat einen elliptischen Querschnitt in einer Ebene, in der die Rotationsachse des Lüfters liegt. Das Flügelrad ist ummantelt und hat einen ähnlichen elliptischen Querschnitt wie die Ansaugdüse. Das Flügelrad ist derart dimensioniert, dass nach Zusammensetzen des Lüfters die Ummantelung die stationäre Ansaugdüse überdeckt und um sie rotiert.From the US 5,478,201 A a suction nozzle and an impeller for a fan with regularly arranged wings is known. The suction nozzle has an elliptical cross section in a plane in which the axis of rotation of the fan is located. The impeller is sheathed and has a similar elliptical cross-section as the suction nozzle. The impeller is dimensioned such that after assembly of the fan, the sheath covers the stationary suction and rotates around it.

Aus der GB 2 090 338 A ist ein Lüfterrad mit regelmäßig angeordneten Lüfterflügeln bekannt. Das Lüfterrad weist eine invertierte Schale auf, die einen hohlen Stumpf umgibt. Der hohle Stumpf ist mit der Schale durch einen Satz von schrägen Schaufelblättern verbunden, wobei die axiale Ausdehnung der Schaufelblätter der axialen Ausdehnung der Schale entspricht.From the GB 2 090 338 A is a fan with regularly arranged fan blades known. The fan has an inverted shell surrounding a hollow stump. The hollow stump is connected to the shell by a set of oblique airfoils, the axial extent of the airfoils corresponding to the axial extent of the shell.

Aus der US 1 447 915 A un der US 1 447 916 A sind Lüfter mit regelmäßig angeordneten Schaufelblättern bekannt. Die Lüfter bestehen aus einem radial nach außen offenen Lüfterrad, wobei eine radial nach außen offene ringförmige Luftaustrittsöffnung ausgebildet ist, die sich über die Außenränder der Schaufelblätter erstreckt und die mit dem Lüfterrad rotiert.From the US 1 447 915 A and the US 1 447 916 A Fans with regularly arranged blades are known. The fans consist of a radially outwardly open fan wheel, wherein a radially outwardly open annular air outlet opening is formed, which extends over the outer edges of the blades and rotates with the fan.

Aus der WO 97/09535 A ist ein radiales Lüfterrad mit regelmäßig angeordneten Lüfterflügeln offenbart, wobei die in radialer Richtung offenen Lüfterflügel zwischen einer vorderen und einer hinteren Platte montiert sind. Die Lüfterflügel sind so ausgebildet, dass sie sich an einer der beiden Platten radial weiter nach außen erstrecken als an der anderen Platte.From the WO 97/09535 A discloses a radial impeller with regularly arranged fan blades, wherein the fan blades open in the radial direction are mounted between a front and a rear plate. The fan blades are configured to extend radially farther outward on one of the two plates than on the other plate.

Aus der US 3,285,502 ist ein Lüfterrad bekannt, das mehrere ungleichmäßig voneinander beabstandete Lüfterflügel aufweist, wobei der Schwerpunkt des Lüfterrades in der Drehachse liegt.From the US 3,285,502 a fan is known which has a plurality of unevenly spaced fan blades, wherein the center of gravity of the fan wheel is located in the axis of rotation.

Aus der EP 0 757 181 A2 ist ein Axiallüfter bekannt, bei dem die Lüfterflügel radial zwischen einer Nabe und einem umlaufenden Ring angeordnet sind, wobei jeweils benachbarte Lüfterflügel unterschiedliche Abstände zueinander besitzen.From the EP 0 757 181 A2 an axial fan is known, in which the fan blades are arranged radially between a hub and a circumferential ring, wherein each adjacent fan blades have different distances from one another.

Der Erfindung liegt daher die Aufgabe zugrunde, einen Lüfter weiterzubilden, so dass die Umweltbelastung vermindert ist.The invention is therefore the object of developing a fan, so that the environmental impact is reduced.

Erfindungsgemäß wird die Aufgabe bei dem Lüfterrad nach den in Anspruch 1 angegebenen Merkmalen, bei dem System nach den in Anspruch 9 angegebenen Merkmalen und bei der Getriebebaureihe nach den in Anspruch 12 angegebenen Merkmalen gelöst.According to the invention the object is achieved in the fan according to the features indicated in claim 1, in the system according to the features specified in claim 9 and in the transmission series according to the features indicated in claim 12.

Wichtige Merkmale der Erfindung eines Lüfterrads sind, dass ein erster Lüfterflügel zu einem ersten in Umfangsrichtung benachbarten Lüfterflügel einen ersten Winkelabstand aufweist und der erste Lüfterflügel zu einem zweiten in entgegengesetzter Richtung benachbarten Lüfterflügel einen zweiten Winkelabstand aufweist, wobei der erste Winkelabstand kleiner als der zweite Winkelabstand ist. Alternativ umfasst die Abfolge in Umfangsrichtung der Winkelabstände von einem jeweiligen Flügel zum in Umfangsrichtung nächstbenachbarten Lüfterflügel mindestens zwei verschiedene Sorten von Winkelabstandswerten. Somit ist eine einfache Ausgestaltung angegeben, bei der die Lüfterflügel nicht notwendig regelmäßig angeordnet sind. Von Vorteil ist dabei, dass die Lüfterflügel periodische Anregungen erzeugen, deren hauptsächlicher Frequenzanteil niedriger liegt, als dies der Fall wäre, wenn alle Winkelabstände gleich groß wären. Insbesondere liegt der Frequenzanteil höchstens bei der Hälfte derjenigen zu einer regelmäßigen Anordnung der Lüfterflügel.Important features of the invention of a fan wheel are that a first fan blade has a first angular distance to a first circumferentially adjacent fan blade and the first fan blade has a second angular distance to a second fan blade adjacent in the opposite direction, wherein the first angular distance is smaller than the second angular distance , Alternatively, the sequence in the circumferential direction of the angular intervals of a respective wing to the next adjacent in the circumferential direction Fan blades at least two different types of angular distance values. Thus, a simple embodiment is specified in which the fan blades are not necessarily arranged regularly. The advantage here is that the fan blades produce periodic excitations whose main frequency component is lower than would be the case if all angular distances were equal. In particular, the frequency component is at most half that of a regular arrangement of the fan blades.

Bei einer vorteilhaften Ausgestaltung ist jeder Luftkanal begrenzt durch zumindest Lüfterflügel, einen Luftleitring und/oder einen Grundkörper, wobei der Querschnitt des Luftkanals im Verlauf von innen nach außen ein Minimum aufweist. Somit sind Luftkanale mit Düsenwirkung ausgebildet. Diese Düsen bewirken vorteilhaft ein gerichtetes Strömen der Kühlluft.In an advantageous embodiment, each air duct is limited by at least fan blades, an air guide ring and / or a base body, wherein the cross section of the air channel has a minimum in the course from inside to outside. Thus, air ducts are formed with a nozzle effect. These nozzles advantageously cause a directed flow of cooling air.

Bei einer vorteilhaften Weiterbildung ist das Minimum des Querschnitts des Luftkanals durch ein Minimum des Abstandes zwischen dem Grundkörper und dem Luftleitring bewirkt, insbesondere durch ein Minimum des Abstandes zwischen den Schnittfiguren des Grundkörpers mit einer Axialebene einerseits und des Luftleitrings mit der Axialebene andererseits. Vorteilhaft umfasst das Lüfterrad einen Grundkörper, Lüfterflügel und einen Luftleitring, wobei der Grundkörper einen kegelstumpfförmigen Bereich aufweist und zumindest jeweils zwei Lüfterflügel, ein Segments des kegelstumpfförmigen Bereichs und ein Segment des Luftleitrings einen radial verlaufenden Luftkanal bilden, dessen Querschnitt im radialen Verlauf ein Minimum aufweist. Von Vorteil ist dabei, dass das Lüfterrad einfach fertigbar ist, da die geometrischen Eigenschaften des Luftkanals, insbesondere die Düsenform, mit den Begrenzungsflächen von Luftleitring und Grundkörper einfach herstellbar und kontrollierbar ist. Zudem ist der Grundkörper des Lüfterrads zusätzlich zu seiner Haltefunktion mit einer Luftleitfunktion belegt. Hierdurch sind Teile einsparbar.In an advantageous development, the minimum of the cross section of the air duct is effected by a minimum of the distance between the base body and the air guide ring, in particular by a minimum of the distance between the sectional figures of the body with an axial plane on the one hand and the air guide ring with the axial plane on the other. The fan wheel advantageously comprises a main body, fan blades and an air guide ring, wherein the base body has a frustoconical region and form at least two fan blades, a segment of the frusto-conical region and a segment of the air guide a radially extending air channel whose cross-section has a minimum in the radial course. The advantage here is that the fan is easily manufacturable, since the geometric properties of the air duct, in particular the nozzle shape, with the boundary surfaces of air guide ring and body is easy to manufacture and controllable. In addition, the main body of the fan is occupied in addition to its holding function with a Luftleitfunktion. As a result, parts can be saved.

Bei einer vorteilhaften Ausgestaltung ist der Querschnitt des Luftleitrings an seiner Innenseite konvex geformt und an seiner Außenseite konkav geformt, insbesondere derart geformt, dass die Wandstärke im Wesentlichen konstant ist. Die Konstanz der Wandstärke hängt hierbei von den Fertigungstoleranzen der Fertigungstechnik und von den Drehzahlen ab, bei denen der Lüfter eingesetzt wird. Die Außenform des Luftleitring folgt somit im Wesentlichen der Innenform des Luftleitrings, und es ist eine vorteilhafte Form des Luftleitrings bei gleichzeitig geringem Materialeinsatz ausgebildet. Von Vorteil ist dabei, dass für den Luftleitring wenig Material eingesetzt werden muss, so dass sein Massenträgheitsmoment möglichst gering ist.In an advantageous embodiment, the cross section of the air guide ring is convex on its inner side and concave on its outer side, in particular shaped such that the wall thickness is substantially constant. The consistency of the wall thickness depends on the manufacturing tolerances of the production technology and on the speeds at which the fan is used. The outer shape of the air guide thus follows substantially the inner shape of the air guide ring, and it is an advantageous form of the air guide at formed at the same time low material usage. The advantage here is that for the air guide little material must be used, so that its moment of inertia is minimized.

Bei einer vorteilhaften Weiterbildung weist der Grundkörper einen kegelstumpfförmigen Bereich auf und der Luftleitring ist in einen mathematischen Kegel konzentrisch derart einbeschreibbar, dass der Luftleitring den mathematischen Kegel in einem ersten und einem zweiten axialen Bereich berührt und in einem dritten axialen Bereich zwischen Luftleitring und dem mathematischen Kegel ein Mindestabstand vorgesehen ist, wobei der dritte axiale Bereich zwischen dem ersten axialen Bereich und dem zweiten axialen Bereich angeordnet ist, und zumindest jeweils zwei Lüfterflügel, ein Segment des kegelstumpfförmigen Bereichs und ein Segment des Luftleitrings einen nach außen verlaufenden Luftkanal bilden. Von Vorteil ist dabei, dass die mit konstruktionstechnisch und fertigungstechnisch einfach handhabbaren geometrischen Formen ein düsenartiger Luftkanal bereitstellbar ist.In an advantageous development, the base body has a frustoconical region and the air guide ring is concentrically inscribed in a mathematical cone such that the air guide touches the mathematical cone in a first and a second axial region and in a third axial region between air guide ring and the mathematical cone a minimum distance is provided, wherein the third axial region is arranged between the first axial region and the second axial region, and at least two fan blades, a segment of the frusto-conical region and a segment of the air guide ring form an outwardly extending air channel. The advantage here is that the constructional and manufacturing technology easy to handle geometric shapes, a nozzle-like air duct is available.

Bei einer vorteilhaften Weiterbildung sind mindestens zwei verschiedenartige Luftkanäle an einem Lüfterrad gebildet. Vorzugsweise ist jeder Luftkanal durch eine geometrische Größe beschreibbar, und die Abfolge der geometrischen Größe der Luftkanäle stellt bei einer Umdrehung des Lüfters eine unregelmäßige Folge dar. Besonders vorzugsweise ist die geometrische Größe jedes Luftkanals der Winkel zwischen den begrenzenden Lüfterflügeln oder der Winkel eines begrenzenden Lüfterflügels zu einer lüfterfesten Referenzrichtung. Alternativ ist die geometrische Größe jedes Luftkanals die Winkelposition des Schwerpunkts oder der Mittenebene des Luftkanals oder der Winkel einer ausgezeichneten Richtung des Luftkanals zu einer lüfterfesten Referenzrichtung. Somit sind einfache geometrische Kenngrößen angegeben, die zur Ausbildung eines erfindungsgemäßen Lüfterrads heranziehbar sind.In an advantageous development, at least two different types of air ducts are formed on a fan. Preferably, each air channel is characterized by a geometric size, and the sequence of the geometric size of the air ducts is an irregular sequence in one revolution of the fan. More preferably, the geometric size of each air duct is the angle between the limiting fan blades or the angle of a limiting fan blade a fan-fixed reference direction. Alternatively, the geometric size of each air duct is the angular position of the center of gravity or the center plane of the air duct or the angle of an excellent direction of the air duct to a fan-fixed reference direction. Thus, simple geometric characteristics are given, which are heranziehbar to form a fan according to the invention.

Bei einer vorteilhaften Weiterbildung liegt der von allen Lüfterflügeln gebildete Schwerpunkt im Zentrum des Lüfters. Von Vorteil ist dabei, dass bei verminderter Geräuschbelastung Zusatzbelastungen der Lager und des Materials durch Unwucht vermieden werden.In an advantageous development, the center of gravity formed by all the fan blades is in the center of the fan. The advantage here is that with reduced noise pollution additional loads on the bearings and the material can be avoided by imbalance.

Bei einer vorteilhaften Weiterbildung ist die maximale axiale Ausdehnung der Lüfterflügel größer als die maximale axiale Ausdehnung des Luftleitrings.In an advantageous development, the maximum axial extent of the fan blades is greater than the maximum axial extent of the air guide ring.

Bei einer vorteilhaften Weiterbildung ist die maximale axiale Ausdehnung der Lüfterflügel mehr als doppelt so groß wie die maximale axiale Ausdehnung des Luftleitrings. Von Vorteil ist dabei, dass ein radiales oder seitlich schräges Abströmen der Kühlluft ermöglicht ist. Somit ist das Lüfterrad bei verschiedenen Getrieben oder allgemein Systemen mit Lüfter einsetzbar.In an advantageous development, the maximum axial extent of the fan blades is more than twice as large as the maximum axial extent of the air guide ring. The advantage here is that a radial or laterally oblique discharge of the cooling air is made possible. Thus, the fan is used in various transmissions or in general systems with fan.

Bei einer vorteilhaften Weiterbildung ist die maximale radiale Ausdehnung der Lüfterflügel größer als die minimale radiale Ausdehnung des Luftleitrings. Von Vorteil ist dabei, dass große Luftaustritte ausgebildet sind, durch die Kühlluft auf das zu kühlende Gehäuse leitbar ist.In an advantageous development, the maximum radial extent of the fan blades is greater than the minimum radial extent of the air guide ring. The advantage here is that large air outlets are formed, can be conducted through the cooling air to the housing to be cooled.

Bei einer vorteilhaften Weiterbildung sind die Lüfterflügel auf der Ansaugseite bis zu einem Radius axial zurückgenommen, insbesondere um mehr als ein Drittel der maximalen axialen Ausdrehung der Lüfterflügel. Von Vorteil ist dabei, dass in geringem Abstand zum Lüfterrad eine Lüfterhaube aufsetzbar ist, wobei an den Ansaugöffnungen oder Lufteinlässen von den Lüfterflügeln erzeugte Geräusche verminderbar sind.In an advantageous development, the fan blades on the suction side are axially retracted up to a radius, in particular by more than one third of the maximum axial extent of the fan blades. The advantage here is that at a small distance from the fan, a fan cover can be placed, wherein at the intake ports or air inlets generated by the fan blades noise can be reduced.

Bei einer vorteilhaften Weiterbildung weist jeder Lüfterflügel eine Symmetrieebene auf, in der vorzugsweise die Drehachse des Lüfterrads liegt. Somit ist auf einfache Weise ein drehsinninvariantes Lüfterrad ausgebildet, und es strömt Kühlluft immer in der gleichen Richtung durch die Luftkanäle.In an advantageous development, each fan blade on a plane of symmetry, in which preferably the axis of rotation of the fan is. Thus, a rotationally invariable fan wheel is formed in a simple manner, and cooling air always flows in the same direction through the air channels.

Bei einer vorteilhaften Weiterbildung ist die radiale Ausdehnung des Grundkörpers kleiner als der Außendurchmesser des Lüfterrads, insbesondere wenigstens fünfzehn Prozent kleiner als der Innendurchmesser des Luftleitrings. Somit sind vorteilhafte geometrische Verhältnisse ausgebildet, bei denen die Kühlluft besonders effektiv strömen kann.In an advantageous development, the radial extent of the base body is smaller than the outer diameter of the fan wheel, in particular at least fifteen percent smaller than the inner diameter of the air guide ring. Thus, advantageous geometric conditions are formed, in which the cooling air can flow particularly effective.

Bei einer vorteilhaften Weiterbildung bilden die Luftkanäle jeweils einen Luftaustritt, der einen radial ausgerichteten und einen axial ausgerichteten Teilbereich umfasst. Somit ist das Lüfterrad an verschiedenen Getrieben, insbesondere direkt vor einer Gehäusewand oder an einem Kegelradtopf, betreibbar.In an advantageous development, the air ducts each form an air outlet, which comprises a radially aligned and an axially aligned portion. Thus, the fan on different transmissions, especially directly in front of a housing wall or on a Kegelradtopf operable.

Wichtige Merkmale der Erfindung eines Systems, insbesondere eines Getriebes, sind, dass ein Lüfter mit einem Lüfterrad mit Lüfterflügeln und einer Lüfterhaube umfasst ist, wobei das Lüfterrad wie bereits oben beschrieben erfindungsgemäß asugebildet ist und wobei die Lüfterhaube das Lüfterrad zumindest teilweise umgibt und die Lüfterhaube einen Bereich mit axialen Lufteinlässen aufweist, wobei die Lüfterflügel in einem ersten Teilbereich des Bereichs mit axialen Lufteinlässen einen konstanten Abstand von der Lüfterhaube aufweisen und in einem zweiten Teilbereich des Bereichs mit axialen Lufteinlässen der Abstand der Lüfterflügel von der Lüfterhaube größer als der konstante Abstand im ersten Teilbereich ist, insbesondere mehr als doppelt so groß. Somit sind besonders vorteilhafte Strömungsverhältnisse erreicht, und die Geräuschentwicklung an einer Lüfterhaube durch vorbeistreifende Lüfterflügel ist vermindert.Important features of the invention of a system, in particular a transmission, are that a fan with a fan with fan blades and a fan cover is included, wherein the fan as described above according to the invention asugebildet and wherein the fan cover surrounds the fan at least partially and the fan cover a Area having axial air inlets, wherein the fan blades in a first portion of the range with axial air inlets have a constant distance from the fan cover and in a second portion of the range with axial air inlets, the distance of the fan blades of the fan cover is greater than the constant distance in the first portion is, in particular, more than twice as large. Thus, particularly advantageous flow conditions are achieved, and the noise on a fan cover by passing fan blades is reduced.

Bei einer vorteilhaften Weiterbildung erstrecken sich die Lüfterflügel radial über den Bereich mit axialen Lufteinlässen hinaus. Somit ist die Kühlluft besonders vorteilhaft ansaugbar.In an advantageous development, the fan blades extend radially beyond the region with axial air inlets. Thus, the cooling air is particularly advantageous sucked.

Bei einer vorteilhaften Weiterbildung ist das Lüfterrad auf einer Welle des Getriebes, insbesondere der eintreibenden Welle, angeordnet. Somit ist ein separater Motor für den Antrieb des Lüfterrads verzichtbar.In an advantageous development, the fan wheel is arranged on a shaft of the transmission, in particular of the driving shaft. Thus, a separate motor for the drive of the fan is dispensable.

Wichtige Merkmale der Erfindung einer Getriebebaureihe mit Varianten, die jeweils einen Lüfter mit Lüfterrad und mindestens eine Getriebestufe umfassen, sind, dass ein Lüfterrad wobei das Lüfterrad wie bereits oben beschrieben erfindungsgemäß asugebildet ist und dass das Lüfterrad in einer ersten Variante auf der eintreibenden Welle einer Kegelradstufe montiert ist und dass das Lüfterrad in einer zweiten Variante auf der eintreibenden Welle eines Stirnradstufe montiert ist. Vorzugsweise ist in der ersten Variante Luft durch Luftkanäle radial leitbar und in der zweiten Variante Luft durch die Luftkanäle in einem Winkel zur radialen Richtung und in einem Winkel zur axialen Richtung, insbesondere in einer Axialebene des Lüfterrads schräg zur Achse des Lüfterrads. Von Vorteil ist dabei, dass die Teilevielfalt in einer Getriebebaureihe reduziert ist, und dass die Variationsmöglichkeiten für die Lüftermontage erhöht ist.Important features of the invention of a transmission series with variants, each comprising a fan with fan and at least one gear stage are that a fan wherein the fan as described above according to the invention asugebildet and that the fan in a first variant on the driving shaft of a bevel gear is mounted and that the fan wheel is mounted in a second variant on the driving shaft of a spur gear. In the first variant, air is preferably radially passable through air ducts and, in the second variant, air is directed through the air ducts at an angle to the radial direction and at an angle to the axial direction, in particular in an axial plane of the fan wheel obliquely to the axis of the fan wheel. The advantage here is that the variety of parts is reduced in a transmission series, and that the possible variations for the fan assembly is increased.

Bei einer vorteilhaften Weiterbildung deckt in der ersten Variante eine Gehäusewand des Getriebes den Luftaustritt der Luftkanäle teilweise ab, insbesondere den axial orientierten Teilbereich des Luftaustritts. Somit ist vorteilhaft die Kühlluft in radialer Richtung um das Getriebegehäuse herum leitbar. Es wird somit eine gute Kühlleistung bewirkt.In an advantageous development, a housing wall of the transmission partially covers the air outlet of the air ducts in the first variant, in particular the axially oriented partial region of the air outlet. Thus, advantageously, the cooling air in the radial direction can be conducted around the transmission housing. It is thus causes a good cooling performance.

Weitere Vorteile ergeben sich aus den Unteransprüchen.Further advantages emerge from the subclaims.

Die Erfindung wird nun anhand von Abbildungen näher erläutert:
Es zeigt

  • Figur 1 eine Ansicht eines Lüfterrads von vorn,
  • Figur 2 eine Ansicht des Lüfterrads aus Figur 1 von hinten,
  • Figur 3 eine Draufsicht auf die Vorderseite des Lüfterrads aus Figur 1,
  • Figur 4 den Schnitt des Lüfterrads entlang einer in Figur 3 mit A-A bezeichneten Axialebene,
  • Figur 5 eine Ansicht eines Getriebes mit montiertem Lüfter
  • Figur 6 eine Seitenansicht des Getriebes aus Figur 5 mit aufgeschnittener Lüfterhaube und aufgeschnittenem Lüfterrad.
The invention will now be explained in more detail with reference to figures:
It shows
  • FIG. 1 a view of a fan from the front,
  • FIG. 2 a view of the fan from FIG. 1 from behind,
  • FIG. 3 a plan view of the front of the fan from FIG. 1 .
  • FIG. 4 the section of the fan along an in FIG. 3 Axial plane labeled AA,
  • FIG. 5 a view of a gearbox with mounted fan
  • FIG. 6 a side view of the transmission FIG. 5 with cut fan cover and cut fan wheel.

Figur 1 zeigt ein Lüfterrad für einen Lüfter eines Getriebes. Das Lüfterrad umfasst zumindest einen Grundkörper 10 mit einer Nabe 13, Lüfterflügel 11 und einen Luftleitring 12. FIG. 1 shows a fan for a fan of a transmission. The fan wheel comprises at least one main body 10 with a hub 13, fan blades 11 and an air guide ring 12.

Das Lüfterrad ist zur Montage auf einer Welle eines Getriebes vorgesehen. Hierzu wird die Nabe 13 auf die Welle gesteckt zur kraftschlüssigen Verbindung mit derselben.The fan is intended for mounting on a shaft of a gearbox. For this purpose, the hub 13 is placed on the shaft for frictional connection with the same.

Das Lüfterrad wird durch die Welle angetrieben. Die Welle treibt somit die Lüfterflügel 11 an, wodurch eine in etwa radial oder schräg nach außen gerichtete Luftströmung erzeugt wird. Diese Richtung der Luftströmung ist unabhängig vom Drehsinn des Lüfterrads, da jeder Lüfterflügel 11 eine Symmetrieebene aufweist, in der die Drehachse des Lüfterrads liegt.The fan wheel is driven by the shaft. The shaft thus drives the fan blades 11, thereby producing an approximately radially or obliquely outwardly directed air flow. This direction of the air flow is independent of the direction of rotation of the fan wheel, since each fan blade 11 has a plane of symmetry in which the axis of rotation of the fan wheel is located.

Der Grundkörper 10, der Luftleitring 12 und jeweils zwei benachbarte Lüfterflügel 11 bilden Luftkanäle, durch die Luftströmung geleitet wird.The main body 10, the air guide ring 12 and two adjacent fan blades 11 form air channels, is passed through the air flow.

Figur 2 zeigt die Rückseite des Lüfterrads aus Figur 1. Ein Auflagering 20 des Grundkörpers 10 und die Auflagekanten 21 jedes Lüfterrads 11 liegen in einer gemeinsamen Ebene. Somit ist ein Betrieb des Lüfterrads dicht an der Gehäusewand eines Getriebes durchführbar, wobei die beschriebene Ebene parallel zu der Gehäusewand des Getriebes ausgerichtet und in geringem Abstand zu dieser angeordnet ist. FIG. 2 shows the back of the fan FIG. 1 , A support ring 20 of the main body 10 and the support edges 21 of each fan 11 are in a common plane. Thus, an operation of the fan is close to the housing wall of a transmission feasible, the plane described is aligned parallel to the housing wall of the transmission and arranged at a small distance to this.

Das Lüfterrad mit Grundkörper, Lüfterflügeln und Leitring ist vorzugsweise einstückig hergestellt, insbesondere als Gussteil aus Aluminium oder Kunststoff, wobei im Fall einer Verwendung von Kunststoff besonders vorzugsweise der Kunststoff zur Vermeidung elektrostatischer Aufladung elektrisch leitfähig ausgebildet ist.The fan with body, fan blades and guide ring is preferably made in one piece, in particular as a casting of aluminum or plastic, wherein in the case of use of plastic particularly preferably the plastic to avoid electrostatic charge is formed electrically conductive.

In einem alternativen Ausführungsbeispiel ist das Lüfterrad aus Stahl gefertigt.In an alternative embodiment, the fan is made of steel.

In montierter Position formen - wie in Figur 2 dargestellt - die radialen Begrenzungskanten 22, die äußere Begrenzungskante 23 des Luftleitrings 12 und die Gehäusewand eine Öffnung, durch die die Luftströmung in radial nach außen geleitet wird. Der Luftleitring 12 erstreckt sich somit nicht über die gesamte axiale Länge des Lüfterrads und insbesondere der Lüfterflügel 11.Form in mounted position - as in FIG. 2 illustrated - the radial boundary edges 22, the outer boundary edge 23 of the air guide ring 12 and the housing wall an opening through which the air flow is passed in radially outward. The air guide ring 12 thus does not extend over the entire axial length of the fan and in particular the fan blades 11th

Figur 3 zeigt eine Draufsicht der Vorderseite des Lüfterrads nach Figur 1. Auf dem Grundkörper 10 sind die Lüfterflügel 11 angebracht, wobei die Lüfterflügel 11 jeweils eine Symmetrieebene aufweisen, die die Rotationsachse des Lüfterrads enthält. Die Lüfterflügel 11 stehen somit im Wesentlichen, also abgesehen von Schrägungen der Oberflächen der Lüfterflügel 11, senkrecht auf einem ringartigen, kegelstrumpfförmigen Bereich 35 des Grundkörpers 10. FIG. 3 shows a top view of the front of the fan after FIG. 1 , On the main body 10, the fan blades 11 are mounted, wherein the fan blades 11 each have a plane of symmetry, which contains the axis of rotation of the fan. The fan blades 11 are thus substantially, that is, apart from inclinations of the surfaces of the fan blades 11, perpendicular to an annular, truncated cone-shaped portion 35 of the body 10th

Jeder Lüfterflügel 11 ist in bezug auf eine lüfterfeste Referenzrichtung 36 jeweils in einem Winkel w1 angeordnet. Die Lüfterflügel 11 sind unregelmäßig angeordnet: Insbesondere sind die Differenzbeträge je zweier Winkel w1 nicht als ganzzahliges Vielfaches eines Grundbetrags darstellbar. Somit werden Resonanzanregungen durch die Lüfterflügel 11 vermindert, insbesondere wird die Frequenz der Resonanzanregungen herabgesetzt.Each fan blade 11 is arranged with respect to a fan-fixed reference direction 36 each at an angle w1. The fan blades 11 are irregularly arranged: In particular, the difference amounts of each two angles w1 can not be represented as an integer multiple of a basic amount. Thus, resonance excitations are reduced by the fan blades 11, in particular, the frequency of the resonance excitations is reduced.

In einer vorteilhaften Ausgestaltung ist das Lüfterrad auf einer Getriebewelle montiert und die Zahl der Lüfterflügel und die Zähnezahl des Zahnrads der Getriebewelle weisen keinen gemeinsamen Teiler auf. Besonders vorzugsweise weist die Zahl der Lüfterflügel und die Zähnezahl jedes Zahnrads des Getriebes keinen gemeinsamen Teiler auf. Somit sind Resonanzeffekte vorteilhaft vermindert.In an advantageous embodiment, the fan is mounted on a gear shaft and the number of fan blades and the number of teeth of the gear shaft of the gear shaft have no common divider. Particularly preferably, the number of fan blades and the number of teeth of each gear of the transmission has no common divider. Thus, resonance effects are advantageously reduced.

Bei einem alternativen Ausführungsbeispiel weist das Lüfterrad eine SpiegelSymmetrieebene auf, in der vorzugsweise die Drehachse des Lüfterrades enthalten ist.In an alternative embodiment, the fan wheel on a mirror symmetry plane, in which preferably the axis of rotation of the fan wheel is included.

Der Außendurchmesser des Grundkörper 10 in Figur 3 ist deutlich kleiner als der Außendurchmesser des Lüfterrads gewählt. Vorzugsweise beträgt der Außendurchmesser des Grundkörpers 10 zwei Drittel des Außendurchmessers des Lüfterrads und damit des Luftleitrings 12, und besonders vorzugsweise ist der Außendurchmesser des Grundkörpers 10 gegenüber dem Innendurchmesser des Luftleitrings 12 um zehn bis zwanzig Prozent reduziert. Somit sind günstige Strömungsverhältnisse für den Lüfter erreichbar.The outer diameter of the main body 10 in FIG. 3 is much smaller than the outer diameter of the fan selected. Preferably, the outer diameter of the base body 10 is two-thirds of the outer diameter of the fan and thus of the air guide ring 12, and more preferably, the outer diameter of the base body 10 relative to the inner diameter of the air guide ring 12 is reduced by ten to twenty percent. Thus, favorable flow conditions for the fan can be achieved.

Der Luftleitring 12 ist aus einem ersten Leitring 33 und einem zweiten Leitring 34 zusammengesetzt, die jeweils für sich ringartig und kegelstumpfförmig ausgebildet sind. Der Öffnungswinkel des zweiten Leitrings 34 ist größer gewählt als der Öffnungswinkel des ersten Leitrings 33.The air guide ring 12 is composed of a first guide ring 33 and a second guide ring 34, which are each designed to be annular and frusto-conical. The opening angle of the second guide ring 34 is selected larger than the opening angle of the first guide ring 33.

Jeweils ein erster Lüfterflügel 31, ein zweiter Lüfterflügel 32, ein von diesen eingeschlossenes Segment 30 des kegelstumpfförmigen Bereichs 35 des Grundkörpers 10 und ein von den beiden Lüfterflügeln 31, 32 eingeschlossenes Segment 37 des Luftleitrings 12 bilden eine Luftkanal, durch welchen bei Betrieb Luft strömt.In each case, a first fan blade 31, a second fan blade 32, a segment 30 of the frusto-conical region 35 of the base body 10 and a segment 37 of the air guide ring 12 enclosed by the two fan blades 31, 32 form an air channel through which air flows during operation.

Jeder dieser derart gebildeten Luftkanäle weist einen Öffnungswinkel oder Winkelabstand w2, also den Winkel zwischen den begrenzenden Lüfterflügeln 31, 32, also zwischen zwei nächsten Nachbarn, auf und einen Winkel w3 der Mittenebene des Luftkanals in Bezug auf eine Referenzrichtung 36. Der Öffnungswinkel w2 ergibt sich somit jeweils aus der Differenz der Winkel w1 zu den begrenzenden Lüfterflügeln 31, 32. Der Winkel w3 unterscheidet sich im Beispiel nach der Figur 3 von den Winkeln w1 zu den begrenzenden Lüfterflügeln 31, 32 jeweils um einen konstanten, das heißt von der Nummer der Lüfterflügel unabhängigen, Betrag. Die Abfolge der Öffnungswinkel w2 und die Abfolge der Winkel w3 definiert jeweils eine unregelmäßige Zahlenfolge. Bei unsymmetrischen Ausformungen der Luftkanäle und/oder Lüfterflügel ändern sich die Zusammenhänge der Winkel w1, w2, w3 untereinander entsprechend. Insbesondere sind zur Definition der Winkel statt der erwähnten Mittenebenen ausgezeichnete Richtungen, beispielsweise Richtungen von Kanten der Lüfterflügel, verwendbar.Each of these air ducts formed in this way has an opening angle or angular distance w2, ie the angle between the delimiting fan blades 31, 32, ie between two nearest neighbors, and an angle w3 of the center plane of the air duct with respect to a reference direction 36. The opening angle w2 results thus in each case from the difference of the angle w1 to the limiting fan blades 31, 32. The angle w3 differs in the example according to the FIG. 3 from the angles w1 to the limiting fan blades 31, 32 each by a constant, that is independent of the number of fan blades, amount. The sequence of opening angles w2 and the sequence of angles w3 defines an irregular sequence of numbers. In the case of asymmetrical formations of the air ducts and / or fan blades, the relationships of the angles w1, w2, w3 with each other change corresponding. In particular, for defining the angles, instead of the center planes mentioned, excellent directions, for example, directions of edges of the fan blades, are usable.

Figur 4 zeigt eine Schnittansicht entlang der in Figur 4 mit A-A bezeichneten Axialebene. FIG. 4 shows a sectional view taken along in FIG FIG. 4 with AA designated axial plane.

Die Lüfterflügel 11 weisen in etwa rechtwinklige Zurücknehmungen 40 auf, so dass die Lüfterflügel 11 bei Betrieb an einem ersten Bereich einer in der Figur 4 von oben aufzusetzenden Lüfterhaube in einem geringeren Abstand entlangstreichen als in einem zweiten Bereich. Dieser zweite Bereich enthält Lufteinlässe für die Luftzufuhr zum Lüfterrad, und durch die Zurücknehmung 40 werden periodische Schwingungsanregnungen an den Lufteinlässen durch ein Vorbeistreichen der Lüfterflügel 10 in großer Nähe vermieden.The fan blades 11 have approximately rectangular recesses 40, so that the fan blades 11 in operation at a first area in the FIG. 4 from the top to be mounted fan cover at a shorter distance than in a second area. This second area contains air inlets for the air supply to the fan wheel, and by the recess 40 periodic vibration excitations at the air inlets are avoided by a Vorbeistreichen the fan blades 10 in close proximity.

Der Grundkörper 10 umfasst zumindest eine Nabe 13 zur kraftschlüssigen Verbindung des Lüfterrads auf einer Welle und einen kegelstumpfförmigen Bereich 35. Dieser kegelstumpfförmige Bereich 35 formt mit dem ersten Leitring 33 und dem zweiten Leitring 34 einen düsenförmigen Luftkanal, wobei die düsenartige Verengung in etwa bei dem minimalen Abstand m von Luftleitring 12 und Grundkörper 12 gebildet ist. Dieser minimale Abstand m bewirkt einen minimalen Querschnitt des durch ein Segment des Luftleitrings 12, ein Segment des kegelstumpfförmigen Bereichs 35 und zwei benachbarte Lüfterflügel 11 begrenzten Luftkanals, wobei dieser Querschnitt in etwa an derselben Position wie der minimale Abstand angenommen wird. Die genaue Position des minimalen Querschnitts in Bezug auf den minimalen Abstand hängt von der konkreten Gestaltung des Querschnitts des Luftleitrings 12 und des kegelstumpfförmigen Bereichs ab.The main body 10 comprises at least one hub 13 for non-positive connection of the impeller on a shaft and a frusto-conical portion 35. This frusto-conical portion 35 forms with the first guide ring 33 and the second guide ring 34 a nozzle-shaped air passage, wherein the nozzle-like constriction is approximately at the minimum Distance m is formed by air guide ring 12 and body 12. This minimum distance m causes a minimum cross-section of the air channel delimited by a segment of the air guide ring 12, a segment of the frusto-conical region 35 and two adjacent fan blades 11, this cross section being assumed to be approximately at the same position as the minimum distance. The exact position of the minimum cross section with respect to the minimum distance depends on the specific configuration of the cross section of the air guide ring 12 and the frusto-conical region.

Der Luftleitring 12 ist zumindest aus einem ersten Leitring 33 und einem zweiten Leitring 34 gebildet, wobei der Öffnungswinkel des kegelstumpfförmigen ersten Leitrings 33 kleiner ist als der Öffnungswinkel des kegelstumpfförmigen zweiten Leitrings 34. Erster Leitring 33 und zweiter Leitring 34 sind entlang eines konzentrischen Rings verbunden. Die Gestaltung der Öffnungswinkel der Leitringe 33, 34 ist derart, dass der Luftleitring 12 in einen Kegelmantel 42 einbeschreibbar ist, wobei der Kegelmantel 42 den Luftleitring 12 an zwei konzentrischen Schnittkreisen 43, 44 berührt, der Kegelmantel 42 aber das Innere des Luftleitrings 12 nicht schneidet. Der Luftleitring 12 weist somit einen axialen Querschnitt auf, dessen Außenkontur konkav geformt ist.The air guide ring 12 is formed at least from a first guide ring 33 and a second guide ring 34, wherein the opening angle of the frusto-conical first guide ring 33 is smaller than the opening angle of the frusto-conical second guide ring 34. First guide ring 33 and second guide ring 34 are connected along a concentric ring. The design of the opening angle of the guide rings 33, 34 is such that the air guide ring 12 can be inscribed in a conical surface 42, wherein the conical surface 42 touches the air guide ring 12 at two concentric cutting circles 43, 44, the conical surface 42 but not the interior of the air guide ring 12 cuts. The air guide ring 12 thus has an axial cross section, whose outer contour is concave.

Auf der der Welle zugewandten Innenseite des Luftleitrings 12 ist dementsprechend - um eine konstante Wandstärke auszubilden - eine konvexe Oberfläche ausgebildet, wobei konvex die Eigenschaft meint, dass die Verbindungslinie zweier Punkte auf der Innenseite des Luftleitrings 12 immer zumindest teilweise im Inneren des Luftleitrings 12 verläuft.Accordingly, in order to form a constant wall thickness, a convex surface is formed on the inner side of the air guide ring 12 facing the shaft, where convex the property that the connecting line of two points on the inside of the air guide ring 12 always runs at least partially inside the air guide ring 12.

Die Innenkontur des Querschnitts des Luftleitrings 12 ist somit mit entgegengesetztem Vorzeichen gekrümmt wie die Außenkontur des Querschnitts des kegelstumpfförmigen Bereichs 35, insbesondere dessen radialen Auslaufs. Beide Konturen sind somit konvex geformt, wobei die konvexen Ausformungen aufeinander zu gerichtet sind.The inner contour of the cross section of the air guide ring 12 is thus curved with opposite signs as the outer contour of the cross section of the frusto-conical portion 35, in particular its radial outlet. Both contours are thus convex, with the convexities facing each other.

Aus der beschriebenen Gestaltung von erstem Leitring 33 und zweiten Leitring 34 resultiert eine Verengung und ein minimaler Abstand m, der einen Düseneffekt in dem zugehörigen Luftkanal bewirkt.From the described design of first guide ring 33 and second guide ring 34 results in a constriction and a minimum distance m, which causes a nozzle effect in the associated air duct.

In alternativen Ausbildungsbeispielen ist die Innenseite des Luftleitrings konvex gestaltet, aber nicht durch zwei verbundene Kegelstümpfe, sondern durch beispielsweise eine parabelförmige oder eine kreisbogenförmige Querschnittskontur beschrieben. Auch in diesen Fällen bewirkt eine resultierende Querschnittsverengung einen Düseneffekt, mit dem ein Luftstrom leitbar ist.In alternative exemplary embodiments, the inside of the air guide ring is convex, but not described by two connected truncated cones, but by, for example, a parabolic or a circular arc-shaped cross-sectional contour. Even in these cases, a resulting cross-sectional constriction causes a nozzle effect with which an air flow can be conducted.

Der Luftleitring 12 erstreckt sich axial nicht über die gesamte Länge des Lüfterrads, insbesondere der Lüfterflügel 11. Vielmehr endet der zweite Leitring 34 in einem axialen Abstand von der durch den Auflagering 20 definierten Ebene. Hierdurch ist eine radiale Öffnung 41 für die Luftkanäle gebildet, durch die - in montiertem Zustand - Luft in radialer Richtung entlang der Gehäusewand des Getriebes leitbar ist.The air guide ring 12 does not extend axially over the entire length of the fan, in particular the fan blades 11. Rather, the second guide ring 34 terminates at an axial distance from the plane defined by the support ring 20. In this way, a radial opening 41 is formed for the air ducts through which - in the assembled state - air in the radial direction along the housing wall of the transmission can be conducted.

Figur 5 zeigt eine Getriebe 50 mit montiertem Lüfter 57. Eine Lüfterhaube 51 umgibt das Lüfterrad. Zur Darstellung ist in Figur 5 nur eine Hälfte der Lüfterhaube 51 gezeigt. FIG. 5 shows a gear 50 with mounted fan 57. A fan cover 51 surrounds the fan. For illustration is in FIG. 5 only one half of the fan cowl 51 is shown.

Die Nabe 13 des Lüfterrads sitzt auf einem Zwischenteil 54 und ist kraftschlüssig mit diesem verbunden, wobei das Zwischenteil 54 wiederum auf einer Welle 53 des Getriebes angeordnet und zumindest formschlüssig mit dieser verbunden ist. Die Welle 53 ist die eintreibende Welle des Getriebes 50.The hub 13 of the fan wheel sits on an intermediate part 54 and is non-positively connected thereto, wherein the intermediate part 54 in turn is arranged on a shaft 53 of the transmission and is at least positively connected thereto. The shaft 53 is the driving shaft of the transmission 50.

Die Lüfterhaube 51 weist einen ringförmigen Bereich mit Lufteinlässen 55 auf, durch den der Lüfter Luft ansaugt. Die axiale Ausrichtung der Lüfterflügel 11 bewirkt, dass unabhängig vom Drehsinn in derselben axialen Richtung angesaugt wird. Somit ist die Ansaugseite des Lüfterrads eindeutig definiert als die Seite, durch weiche die Luft einströmt. Die Luftkanäle weisen eine Öffnung auf, durch die demnach unabhängig vom Drehsinn Luft austritt. Somit ist ein Luftaustritt gebildet.The fan cover 51 has an annular area with air inlets 55, through which the fan draws air. The axial orientation of the fan blades 11 causes, regardless of the direction of rotation is sucked in the same axial direction. Thus, the suction side of the fan is clearly defined as the side through which the air flows. The air ducts have an opening through which air therefore exits independently of the direction of rotation. Thus, an air outlet is formed.

Der Durchmesser des Bereichs mit Lufteinlässen 55 ist gleich dem Innendurchmesser des ersten Leitrings 33.The diameter of the area with air inlets 55 is equal to the inner diameter of the first guide ring 33.

Die Lüfterflügel 11 streifen bei einer Drehbewegung an den Lufteinlässen 55 vorbei. Zur Geräuschminderung weisen die Lüfterflügel 11 jeweils eine Zurücknehmung 40 auf, so dass nur ein Teilbereich des Bereichs der Lufteinlässe 55 von den Lüfterflügeln 11 in geringem Abstand überstrichen wird, während ein anderer, radial weiter innen liegender Teilbereich in größerem Abstand überstrichen wird. Die radiale Ausdehnung des radial weiter innen liegenden Teilbereichs ist größer als die radiale Ausdehnung des radial weiter außen liegenden Teilbereichs. Somit sind Pfeifgeräusche vermindert.The fan blades 11 strip past the air inlets 55 during a rotational movement. To reduce noise, the fan blades 11 each have a recess 40, so that only a portion of the area of the air inlets 55 is swept by the fan blades 11 at a small distance, while another, radially further inboard portion is covered at a greater distance. The radial extent of the radially further inner subregion is greater than the radial extent of the radially outer subregion. Thus whistling sounds are reduced.

Figur 6 zeigt den Lüfter aus Figur 5 in einer Seitenansicht. Das Lüfterrad ist über einem Kegelradtopf 61 montiert. FIG. 6 shows the fan FIG. 5 in a side view. The fan wheel is mounted above a bevel gear pot 61.

Durch Lüfterflügel 11 ist Luft bewegbar, die durch den kegelstumpfförmigen Bereich 35 und den ersten Leitring 33 und den zweiten Leitring 34 auf Luftauslässe 56 geleitet werden.By fan blades 11 air is moved, which are passed through the frusto-conical portion 35 and the first guide ring 33 and the second guide ring 34 on air outlets 56.

Zwischen Lüfterhaube 51 und erstem Leitring 33 ist ein Zwischenraum 60 vorgesehen. Wie durch Vergleich mit Figur 4 ersichtlich ist, ist die Zurücknehmung 40 der Lüfterflügel 11 in axialer Richtung etwa doppelt so lang wie die axiale Ausdehnung des Zwischenraums 60.Between the fan cover 51 and the first guide ring 33, a gap 60 is provided. As by comparison with FIG. 4 it can be seen, the recess 40 of the fan blades 11 in the axial direction is about twice as long as the axial extent of the gap 60th

Die entlang der radiale Begrenzungskante 22 der Lüfterflügel 11 vorgesehene Zurücknahme des zweiten Leitrings 34 ermöglicht eine Montage des Lüfterrads auf einer Welle, die aus einer Seitenwand des Getriebes 50 ragt. Dies ist beispielsweise bei Stirnradgetrieben der Fall. In diesem Fall ist das Lüfterrad direkt vor dieser Seitenwand montierbar, und die von den Lüfterflügeln 11 bewegte Luft strömt radial nach außen und somit entlang der Gehäusewand. Die Gehäusewand deckt einen Teilbereichs des Luftaustritts der Luftkanäle ab, und zwar denjenigen Teilbereich, der axial ausgerichtet ist, dessen Flächennormale also parallel zur Wellenachse angeordnet ist. Somit ist bei einer Montage vor einer Gehäusewand der in Figur 6 durch einen Kegelradtopf 61 geschaffene Abstand des Lüfterrads vom Gehäuse des Getriebes 50 verzichtbar, denn die Luft wird in diesem Fall radial nach außen geleitet. Hierdurch ist ein kompaktes Baumaß des Getriebes mit Lüfter erreichbar.The provided along the radial boundary edge 22 of the fan blades 11 withdrawal of the second guide ring 34 allows mounting of the fan on a shaft which protrudes from a side wall of the transmission 50. This is the case, for example, with spur gears. In this case, the fan is mounted directly in front of this side wall, and the moving of the fan blades 11 air flows radially outwards and thus along the housing wall. The housing wall covers a portion of the air outlet of the air ducts, namely that portion which is axially aligned, the surface normal is thus arranged parallel to the shaft axis. Thus, when mounted in front of a housing wall in FIG. 6 created by a Kegelradtopf 61 distance of the fan from the housing of the transmission 50, because the air is directed in this case radially outward. As a result, a compact dimensions of the transmission with fan can be achieved.

Durch die Verwendung eines Lüfterrads bei unterschiedlichen Varianten von Getrieben wird eine Baureihe gebildet, bei deren Varianten solche Komponenten, die den Lüfter, insbesondere das Lüfterrad bilden, einheitlich einsetzbar sind. Somit ist die Teilevielfalt der Baureihe reduziert.By using a fan in different variants of transmissions, a series is formed in whose variants, such components that form the fan, in particular the fan, are uniformly used. Thus, the variety of parts of the series is reduced.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

  • 10 Grundkörper10 basic body
  • 11 Lüfterflügel11 fan blades
  • 12 Luftleitring12 air guide ring
  • 13 Nabe13 hub
  • 20 Auflagering20 support ring
  • 21 Auflagekante21 bearing edge
  • 22 radiale Begrenzungskante22 radial boundary edge
  • 23 äußere Begrenzungskante23 outer boundary edge
  • 30 Segment30 segment
  • 31 erster Lüfterflügel31 first fan blade
  • 32 zweiter Lüfterflügel32 second fan blades
  • 33 erster Leitring33 first guide ring
  • 34 zweiter Leitring34 second guide ring
  • 35 kegelstumpfförmiger Bereich35 frustoconical area
  • 36 Referenzrichtung36 Reference direction
  • 37 Segment37 segment
  • w1, w2, w3 Winkelw1, w2, w3 angles
  • m minimaler Abstandm minimum distance
  • 40 Zurücknehmung40 recovery
  • 41 radiale Öffnung41 radial opening
  • 42 Kegelmantel42 conical jacket
  • 43, 44 Schnittkreis43, 44 cutting circle
  • 50 Getriebe50 gears
  • 51 Lüfterhaube51 Fan cover
  • 52 Rahmen52 frames
  • 53 Welle53 wave
  • 54 Zwischenteil54 intermediate part
  • 55 Lufteinlässe55 air inlets
  • 56 Luftauslässe56 air outlets
  • 57 Lüfter57 fans
  • 60 Zwischenraum60 space
  • 61 Kegelradtopf61 bevel gear pot

Claims (13)

  1. A fan impeller with fan blades (11, 31, 32),
    wherein
    a number n >2 of non-regularly arranged fan blades (11, 31, 32) is provided, and wherein the fan blades (11, 31, 32) are formed identically, wherein a number of air ducts is provided which are limited in each case by at least the fan blades (11, 31, 32), an air guide ring (12) and a base body (10),
    characterised in that
    the fan blades (11, 31, 32) are axially set back as far as a radius on the intake side and in that the maximum axial extent of the fan blades (11, 31, 32) is greater than the maximum axial extent of the air guide ring (12), and
    in that the air ducts in each case form an air exit which comprises a radially oriented and an axially oriented partial region.
  2. A fan impeller according to the preceding claim,
    characterised in that
    the cross-section of the air guide ring (12) is shaped convexly on its inside and is shaped concavely on its outside such that the wall thickness of the air guide ring (12) is substantially constant.
  3. A fan impeller according to at least one of the preceding claims,
    wherein
    the base body (10) has a frustoconical region (35) and the air guide ring (12) can be inscribed concentrically in a mathematical cone such that the air guide ring (12) contacts the mathematical cone in a first and a second axial region, and in a third axial region a minimum distance is provided between the air guide ring (12) and the mathematical cone,
    wherein the third axial region is arranged between the first axial region and the second axial region,
    and at least two fan blades (11, 31, 32) in each case, a segment (30) of the frustoconical region (35) and a segment (37) of the air guide ring (12) form an air duct running radially or obliquely outwards.
  4. A fan impeller according to at least one of the preceding claims,
    characterised in that
    at least two different types of air ducts are formed on a fan impeller.
  5. A fan impeller according to at least one of the preceding claims,
    characterised in that
    each air duct can be described by a geometric variable,
    and the sequence of the geometric variable of the air ducts upon revolution of the fan (57) represents an irregular sequence,
    and/or in that
    the geometric variable of each air duct is the angle between the delimiting fan blades (11, 31, 32) or the angle of a delimiting fan blade (11, 31, 32) relative to a reference direction (36) which is fixed relative to the fan.
  6. A fan impeller according to Claim 5,
    characterised in that
    the geometric variable of each air duct is the angular position of the centre of gravity or of the central plane of the air duct or the angle of a marked direction of the air duct relative to a reference direction (36) which is fixed relative to the fan.
  7. A fan impeller according to at least one of the preceding claims,
    characterised in that
    the maximum axial extent of the fan blades (11, 31, 32) is more than twice as great as the maximum axial extent of the air guide ring (12),
    and/or in that
    the fan blades (11, 31, 32) on the intake side are axially set back as far as a radius by more than one third of the maximum axial turnout of the fan blades (11, 31, 32).
  8. A fan impeller according to at least one of the preceding claims,
    characterised in that
    the radial extent of the base body (10) is smaller than the external diameter of the fan impeller, in particular at least fifteen percent smaller than the internal diameter of the air guide ring (12).
  9. A system, in particular transmission (50),
    comprising a fan (57) having
    a fan impeller with fan blades (11, 31, 32)
    and a fan cowl (51)
    characterised in that
    the fan impeller is formed according to one of the preceding claims,
    the fan cowl at least partially surrounds the fan impeller
    and the fan cowl (51) has a region with axial air inlets (55),
    the fan blades (11, 31, 32) in a first partial region of the region with axial air inlets (55) being at a constant distance from the fan cowl (51),
    and in a second partial region of the region with axial air inlets (55) the distance of the fan blades (11, 31, 32) from the fan cowl (51) being greater than the constant distance in the first partial region, in particular more than twice as great,
    and/or in that
    the fan blades (11, 31, 32) extend radially beyond the region with axial air inlets (55).
  10. A system according to Claim 9,
    characterised in that
    the system is a transmission (50), with the fan impeller being arranged on a shaft (53) of the transmission (50), in particular the input shaft (53).
  11. A system according to Claim 10,
    characterised in that
    the number of the fan blades (11, 31, 32) and the tooth number of the gear wheel of the input shaft do not have a common divisor,
    and/or in that
    the number of the fan blades (11, 31, 32) and the tooth number of each gear wheel of the transmission do not have a common divisor.
  12. A transmission series,
    with variants which comprise in each case a fan (57) with fan impeller and at least one gear stage,
    characterised in that
    a fan impeller according to one of Claims 1 to 8 is formed,
    in that the fan impeller in a first variant is mounted on the input shaft (53) of a bevel-gear stage
    and in that the fan impeller in a second variant is mounted on the input shaft (53) of a spur-gear stage.
  13. A transmission series according to Claim 12, characterised in that
    in the first variant air can be guided radially through air ducts
    and in the second variant air can be guided through the air ducts at an angle to the radial direction and at an angle to the axial direction, in particular in an axial plane of the fan impeller obliquely to the axis of the fan impeller,
    and/or in that
    in the first variant a housing wall of the transmission (50) partially covers the air exit of the air ducts, in particular the axially oriented partial region of the air exit.
EP08707176.7A 2007-02-23 2008-01-22 Ventilator wheel, system and transmission line Active EP2122182B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL08707176T PL2122182T3 (en) 2007-02-23 2008-01-22 Ventilator wheel, system and transmission line
EP17000355.2A EP3214316B1 (en) 2007-02-23 2008-01-22 System and series of gears

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007009369 2007-02-23
PCT/EP2008/000443 WO2008101577A2 (en) 2007-02-23 2008-01-22 Ventilator wheel, system and transmission line

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP17000355.2A Division EP3214316B1 (en) 2007-02-23 2008-01-22 System and series of gears
EP17000355.2A Division-Into EP3214316B1 (en) 2007-02-23 2008-01-22 System and series of gears

Publications (2)

Publication Number Publication Date
EP2122182A2 EP2122182A2 (en) 2009-11-25
EP2122182B1 true EP2122182B1 (en) 2019-05-01

Family

ID=39316429

Family Applications (2)

Application Number Title Priority Date Filing Date
EP08707176.7A Active EP2122182B1 (en) 2007-02-23 2008-01-22 Ventilator wheel, system and transmission line
EP17000355.2A Active EP3214316B1 (en) 2007-02-23 2008-01-22 System and series of gears

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP17000355.2A Active EP3214316B1 (en) 2007-02-23 2008-01-22 System and series of gears

Country Status (6)

Country Link
EP (2) EP2122182B1 (en)
CN (2) CN103410775B (en)
DE (1) DE102008010912B4 (en)
HU (1) HUE045193T2 (en)
PL (1) PL2122182T3 (en)
WO (1) WO2008101577A2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012013351A1 (en) * 2012-07-06 2014-05-08 Sew-Eurodrive Gmbh & Co Kg Gear with a shaft
DE102012215503B4 (en) * 2012-08-31 2016-07-21 Siemens Aktiengesellschaft Rotor of an electric machine and electric machine
EP3085997B1 (en) 2015-04-23 2020-07-22 Flender GmbH Air guidance hood for a gearbox and gearbox with an air guidance hood
CN104863893B (en) * 2015-04-30 2017-09-22 广东美的制冷设备有限公司 Wind wheel, air channel, the preparation method of air cleaning facility and wind wheel
JP6435559B2 (en) * 2015-06-01 2018-12-12 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co.,Ltd Motor assembly and unmanned aerial vehicle
DE102020000478A1 (en) 2019-02-12 2020-08-13 Sew-Eurodrive Gmbh & Co. Kg Drive system, having an electric motor, a housing and an adapter having a fan
EP3948028A1 (en) * 2019-03-26 2022-02-09 Sew-Eurodrive GmbH & Co. KG Transmission having a fan assembly
BR112022015339A2 (en) 2020-03-13 2022-09-27 Sew Eurodrive Gmbh & Co Kg TRANSMISSION WITH A FAN ARRANGEMENT
DE102021206105A1 (en) * 2021-06-15 2022-12-15 Dana Motion Systems Deutschland GmbH Transmission fan shroud assembly, method of manufacture, assembly and modular kit

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3285502A (en) * 1965-01-25 1966-11-15 Brookside Corp Balanced fan construction
EP0757181A2 (en) * 1995-08-03 1997-02-05 Valeo Thermique Moteur Axial flow fan

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1447915A (en) 1920-10-06 1923-03-06 American Blower Co Centrifugal fan
US1447916A (en) * 1920-12-18 1923-03-06 American Blower Co Centrifugal fan
DE1253402B (en) * 1959-06-10 1967-11-02 Siemens Ag Device for noise reduction on multi-blade radial fans for ventilation of electrical machines
US3179329A (en) 1961-08-16 1965-04-20 Ruth D Mayne Turbine type blower wheel
GB1293553A (en) 1969-02-18 1972-10-18 Cav Ltd Radial flow fans
US4046489A (en) * 1975-10-08 1977-09-06 Eagle Motive Industries, Inc. Aerodynamic fan blade
JPS5644495A (en) * 1979-09-20 1981-04-23 Nissan Motor Co Ltd Impeller for centrifugal compressor
GB2090338B (en) 1980-12-31 1984-05-10 Birmid Qualcast Home & Garden Centrifugal fan
US5000660A (en) 1989-08-11 1991-03-19 Airflow Research And Manufacturing Corporation Variable skew fan
DE3842697A1 (en) 1988-12-19 1990-06-21 Standard Elektrik Lorenz Ag HIGH PRESSURE BLOWER
JP2929834B2 (en) * 1992-04-13 1999-08-03 ダイキン工業株式会社 Centrifugal fan
US5348447A (en) * 1992-12-30 1994-09-20 J & D Sales Improved fan housing with easy access
US5474427A (en) * 1993-10-12 1995-12-12 J & D Sales Of Eau Claire Wisconsin Fan screen assembly
US5478201A (en) 1994-06-13 1995-12-26 Carrier Corporation Centrifugal fan inlet orifice and impeller assembly
SE508332C2 (en) 1995-09-07 1998-09-28 Pm Luft Centrifugal Impeller
US6082969A (en) 1997-12-15 2000-07-04 Caterpillar Inc. Quiet compact radiator cooling fan
US6213718B1 (en) * 1998-04-27 2001-04-10 Emerson Electric Co. Air circulation fan with removable shroud
JP3982181B2 (en) * 2001-01-29 2007-09-26 ダイキン工業株式会社 Fan guard for blower unit
US6514036B2 (en) * 2001-04-27 2003-02-04 Black & Decker Inc. Radial flow fan with impeller having blade configuration for noise reduction
DE10122516B4 (en) 2001-05-09 2006-10-19 Mtu Friedrichshafen Gmbh Wheel
US7191613B2 (en) * 2002-05-08 2007-03-20 Lg Electronics Inc. Turbo fan and air conditioner having the same applied thereto
DE102005031197B4 (en) 2005-07-01 2016-10-13 Sew-Eurodrive Gmbh & Co Kg Drive and fan

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3285502A (en) * 1965-01-25 1966-11-15 Brookside Corp Balanced fan construction
EP0757181A2 (en) * 1995-08-03 1997-02-05 Valeo Thermique Moteur Axial flow fan

Also Published As

Publication number Publication date
CN103410775A (en) 2013-11-27
CN103410775B (en) 2016-08-10
CN101617128A (en) 2009-12-30
PL2122182T3 (en) 2019-10-31
WO2008101577A3 (en) 2008-10-16
HUE045193T2 (en) 2019-12-30
DE102008010912B4 (en) 2020-11-12
EP3214316A1 (en) 2017-09-06
DE102008010912A1 (en) 2008-08-28
EP2122182A2 (en) 2009-11-25
WO2008101577A2 (en) 2008-08-28
CN101617128B (en) 2013-09-18
EP3214316B1 (en) 2019-08-07

Similar Documents

Publication Publication Date Title
EP2122182B1 (en) Ventilator wheel, system and transmission line
EP2122181B1 (en) Ventilator wheel, system and transmission line
EP2778432B1 (en) Ventilator assembly with flow rectifier
EP1608875B1 (en) Radial fan wheel, fan unit, and radial fan arrangement
EP3892860A1 (en) Axial fan impeller
DE69924558T2 (en) vacuum pump
WO2011038884A1 (en) Cross-flow fan
DE102008000168A1 (en) Blower arrangement with pre-swirl generator
DE102007063023A1 (en) Composable impeller
EP4073389A1 (en) Impeller wheel for a rotor, and electric machine
DE112017006146T5 (en) SEPARATION ASSEMBLY WITH ONE-PIECE IMPULSE TURBINE
DE3514207A1 (en) Dynamo having a rotor wheel for sucking in cooling air for motor vehicles
DE10250171B4 (en) Automotive alternator with a cooling air inlet window, which has a non-uniform opening area along the direction of rotation
EP0546361B1 (en) Axial fan
EP3608545A1 (en) Vacuum pump
EP3592985B1 (en) Parts kit and method for producing a radial blower
DE102016013639A1 (en) Two-flow turbomachine
DE102020000478A1 (en) Drive system, having an electric motor, a housing and an adapter having a fan
WO2011012351A1 (en) Guide geometry for half-axial fan wheels
DE102019216704A1 (en) Fan wheel for a radiator fan of a motor vehicle
EP1258636B1 (en) Fan rotor and fan, particularly a radial fan
DE3326299A1 (en) GAP TRAINING BETWEEN A FIXED AND A TURNING PART
DE19643043C2 (en) Centrifugal air classifier with radial fine material discharge
DE10111292A1 (en) Fan arrangement for an electrical machine
EP2298643B1 (en) Drive rotor with air duct

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: 20090923

AK Designated contracting states

Kind code of ref document: A2

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

DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20161109

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: F04D 29/66 20060101ALI20181121BHEP

Ipc: F04D 29/28 20060101AFI20181121BHEP

Ipc: F04D 29/70 20060101ALI20181121BHEP

INTG Intention to grant announced

Effective date: 20181217

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

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

Ref country code: CH

Ref legal event code: NV

Representative=s name: HEPP WENGER RYFFEL AG, CH

Ref country code: AT

Ref legal event code: REF

Ref document number: 1127306

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190515

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502008016731

Country of ref document: DE

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: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: SK

Ref legal event code: T3

Ref document number: E 31590

Country of ref document: SK

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

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: 20190501

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: 20190501

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: 20190501

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: 20190801

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: 20190901

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: 20190501

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

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: 20190801

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: 20190802

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: 20190501

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E045193

Country of ref document: HU

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

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: 20190901

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

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: 20190501

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: 20190501

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: 20190501

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502008016731

Country of ref document: DE

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: 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: 20190501

26N No opposition filed

Effective date: 20200204

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: 20190501

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: 20190501

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: 20200122

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: 20200122

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: 20190501

Ref country code: CY

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: 20190501

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

Ref country code: IT

Payment date: 20221213

Year of fee payment: 16

Ref country code: BE

Payment date: 20230130

Year of fee payment: 16

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

Ref country code: SK

Payment date: 20231220

Year of fee payment: 17

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

Ref country code: GB

Payment date: 20231130

Year of fee payment: 17

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

Ref country code: NL

Payment date: 20231215

Year of fee payment: 17

Ref country code: FR

Payment date: 20231212

Year of fee payment: 17

Ref country code: FI

Payment date: 20231218

Year of fee payment: 17

Ref country code: CZ

Payment date: 20231201

Year of fee payment: 17

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

Ref country code: PL

Payment date: 20231012

Year of fee payment: 17

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

Ref country code: AT

Payment date: 20240109

Year of fee payment: 17

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

Ref country code: HU

Payment date: 20231205

Year of fee payment: 17

Ref country code: DE

Payment date: 20240131

Year of fee payment: 17

Ref country code: CH

Payment date: 20240202

Year of fee payment: 17