EP2122182B1 - Lüfterrad, system und getriebebaureihe - Google Patents

Lüfterrad, system und getriebebaureihe 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)
English (en)
French (fr)
Other versions
EP2122182A2 (de
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/pl
Priority to EP17000355.2A priority patent/EP3214316B1/de
Publication of EP2122182A2 publication Critical patent/EP2122182A2/de
Application granted granted Critical
Publication of EP2122182B1 publication Critical patent/EP2122182B1/de
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.
EP08707176.7A 2007-02-23 2008-01-22 Lüfterrad, system und getriebebaureihe Active EP2122182B1 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL08707176T PL2122182T3 (pl) 2007-02-23 2008-01-22 Wirnik wentylatora, system i typoszereg przekładni
EP17000355.2A EP3214316B1 (de) 2007-02-23 2008-01-22 System und getriebebaureihe

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007009369 2007-02-23
PCT/EP2008/000443 WO2008101577A2 (de) 2007-02-23 2008-01-22 Lüfterrad, system und getriebebaureihe

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP17000355.2A Division EP3214316B1 (de) 2007-02-23 2008-01-22 System und getriebebaureihe
EP17000355.2A Division-Into EP3214316B1 (de) 2007-02-23 2008-01-22 System und getriebebaureihe

Publications (2)

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

Family

ID=39316429

Family Applications (2)

Application Number Title Priority Date Filing Date
EP17000355.2A Active EP3214316B1 (de) 2007-02-23 2008-01-22 System und getriebebaureihe
EP08707176.7A Active EP2122182B1 (de) 2007-02-23 2008-01-22 Lüfterrad, system und getriebebaureihe

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP17000355.2A Active EP3214316B1 (de) 2007-02-23 2008-01-22 System und getriebebaureihe

Country Status (6)

Country Link
EP (2) EP3214316B1 (zh)
CN (2) CN101617128B (zh)
DE (1) DE102008010912B4 (zh)
HU (1) HUE045193T2 (zh)
PL (1) PL2122182T3 (zh)
WO (1) WO2008101577A2 (zh)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012013351A1 (de) * 2012-07-06 2014-05-08 Sew-Eurodrive Gmbh & Co Kg Getriebe mit einer Welle
DE102012215503B4 (de) 2012-08-31 2016-07-21 Siemens Aktiengesellschaft Rotor einer elektrischen Maschine und elektrische Maschine
EP3085997B1 (de) * 2015-04-23 2020-07-22 Flender GmbH Luftleithaube für ein getriebe und getriebe mit einer luftleithaube
CN104863893B (zh) * 2015-04-30 2017-09-22 广东美的制冷设备有限公司 风轮、风道、空气净化设备及风轮的制备方法
JP6435559B2 (ja) 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 モータアセンブリ及び無人航空機
WO2020164795A1 (de) 2019-02-12 2020-08-20 Sew-Eurodrive Gmbh & Co. Kg Antriebssystem, aufweisend einen elektromotor, ein getriebe und einen einen lüfter aufweisenden adapter
WO2020192963A1 (de) 2019-03-26 2020-10-01 Sew-Eurodrive Gmbh & Co. Kg Getriebe mit lüfteranordnung
US11885406B2 (en) * 2020-03-13 2024-01-30 Sew-Eurodrive Gmbh & Co. Kg Transmission having a fan assembly
DE102021206105A1 (de) * 2021-06-15 2022-12-15 Dana Motion Systems Deutschland GmbH Lüfterabdeckungsbaugruppe für ein Getriebe, Verfahren zu deren Herstellung, Baugruppe und modularer Satz

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 (de) * 1959-06-10 1967-11-02 Siemens Ag Einrichtung zur Geraeuschminderung an vielschaufligen Radiallueftern zur Belueftung elektrischer Maschinen
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 (de) * 1988-12-19 1990-06-21 Standard Elektrik Lorenz Ag Hochdruck-geblaese
JP2929834B2 (ja) * 1992-04-13 1999-08-03 ダイキン工業株式会社 遠心ファン
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 (sv) 1995-09-07 1998-09-28 Pm Luft Radialfläkthjul
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 (ja) * 2001-01-29 2007-09-26 ダイキン工業株式会社 送風ユニットのファンガード
US6514036B2 (en) * 2001-04-27 2003-02-04 Black & Decker Inc. Radial flow fan with impeller having blade configuration for noise reduction
DE10122516B4 (de) * 2001-05-09 2006-10-19 Mtu Friedrichshafen Gmbh Laufrad
US7191613B2 (en) * 2002-05-08 2007-03-20 Lg Electronics Inc. Turbo fan and air conditioner having the same applied thereto
DE102005031197B4 (de) * 2005-07-01 2016-10-13 Sew-Eurodrive Gmbh & Co Kg Antrieb und Lüfter

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

Similar Documents

Publication Publication Date Title
EP2122182B1 (de) Lüfterrad, system und getriebebaureihe
EP2122181B1 (de) Lüfterrad, system und getriebebaureihe
EP2778432B1 (de) Ventilatoranordnung mit Strömungsgleichrichter
EP1608875B1 (de) Radiallüfterrad, lüftereinheit und radiallüfteranordnung
EP3892860A1 (de) Axiallüfterrad
DE69924558T2 (de) Vakuumpumpe
WO2011038884A1 (de) Diagonalventilator
DE102008000168A1 (de) Gebläseanordnung mit Vordrallerzeuger
DE102007063023A1 (de) Zusammensetzbares Flügelrad
WO2021115806A1 (de) Lüfterrad für einen rotor und elektrische maschine
DE112017006146T5 (de) Trennbaugruppe mit einer einteiligen impulsturbine
DE3514207A1 (de) Lichtmaschine mit einem luefterrad zum ansaugen von kuehlluft fuer kraftfahrzeuge
DE10250171B4 (de) Kraftfahrzeugwechselstrommaschine mit einem Kühllufteinlaßfenster, welches einen ungleichmäßigen Öffnungsbereich entlang der Drehrichtung besitzt
EP2329149B1 (de) Diagonallüfter
EP0546361B1 (de) Axiallüfter
EP3608545A1 (de) Vakuumpumpe
EP3865711A1 (de) Ventilator mit abdeckscheibe an der rotorglocke
EP3592985B1 (de) Teilesatz und verfahren für die fertigung eines radiallüfters
DE102016013639A1 (de) Zweiflutige Strömungsmaschine
DE102020000478A1 (de) Antriebssystem, aufweisend einen Elektromotor, ein Gehäuse und einen einen Lüfter aufweisenden Adapter
WO2011012351A1 (de) Führungsgeometrie für halbaxiale lüfterräder
DE102019216704A1 (de) Lüfterrad für einen Kühlerlüfter eines Kraftfahrzeugs
EP1258636B1 (de) Lüfterrad sowie Lüfter, insbesondere Radiallüfter
DE3326299A1 (de) Spaltausbildung zwischen einem feststehenden und einem sich drehenden teil
DE19643043C2 (de) Schleuderrad-Windsichter mit radialem Feingutaustrag

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: CH

Payment date: 20230330

Year of fee payment: 16

Ref country code: AT

Payment date: 20230111

Year of fee payment: 16

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