EP0746689B1 - Boitier a recirculation controlee pour utilisation avec un ventilateur axial a pales entourees par un anneau cylindrique - Google Patents

Boitier a recirculation controlee pour utilisation avec un ventilateur axial a pales entourees par un anneau cylindrique Download PDF

Info

Publication number
EP0746689B1
EP0746689B1 EP94926638A EP94926638A EP0746689B1 EP 0746689 B1 EP0746689 B1 EP 0746689B1 EP 94926638 A EP94926638 A EP 94926638A EP 94926638 A EP94926638 A EP 94926638A EP 0746689 B1 EP0746689 B1 EP 0746689B1
Authority
EP
European Patent Office
Prior art keywords
fan
housing
vanes
band
combination
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.)
Expired - Lifetime
Application number
EP94926638A
Other languages
German (de)
English (en)
Other versions
EP0746689A4 (fr
EP0746689A1 (fr
Inventor
Martin G. Yapp
Robert Van Houten
Robert Ives Hickey
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Robert Bosch LLC
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 Robert Bosch GmbH, Robert Bosch LLC filed Critical Robert Bosch GmbH
Publication of EP0746689A1 publication Critical patent/EP0746689A1/fr
Publication of EP0746689A4 publication Critical patent/EP0746689A4/fr
Application granted granted Critical
Publication of EP0746689B1 publication Critical patent/EP0746689B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/545Ducts

Definitions

  • banded axial-flow fan This application relates primarily to banded, axial-flow fans that are used in combination with a housing.
  • banded axial-flow fan we use the term banded axial-flow fan to describe a fan having a hub that rotates on an axis and has blades extending in an outwardly direction (for example, generally radially) from the hub to a circular band that connects the blade tips. Blade rotation tends to force air in the general direction of the fan axis.
  • fan and housing combination we use the term fan and housing combination to describe such axial flow fans in combination with a housing (e.g., a shroud or a duct) that guides airflow entering and/or leaving the fan.
  • a housing e.g., a shroud or a duct
  • shroud we mean an airflow guide shaped and positioned to guide airflow moving between the fan and a heat exchanger.
  • An example of a banded shrouded fan that moves air through a heat exchanger is disclosed in Gray U.S. Patent, 4,548,548, which is hereby incorporated by reference.
  • duct we mean an elongated flow path such a those used in heat, ventilation, and air conditioning systems.
  • Fig. 1B In order to compare the invention to the prior art, a figure from the '548 patent is reproduced here as Fig. 1B.
  • US-A-4685513 discloses a compact fan and shroud package for radiators with fan blades cared rearwardly supporting a rotating shroud at an optimised distance from the radiator for improved airflow through the radiator.
  • the package comprises a fan having a hub that rotates on an axis and blades extending outwardly from the hub to a circular band that connects the blade tips, the package further comprising a housing to control airflow entering the fan, leaving the fan or both, a portion of the housing being positioned outward of the fan band so that there are running clearances between the fan band and housing such that recirculating airflow moves in the pathway between the fan and housing.
  • the housing may be a single injection moulded unit.
  • Airflow recirculation can be explained as follows.
  • the fan generates a pressure difference between the upstream side of the fan (the side from which air is drawn) and the downstream side of the fan (the side of the fan which exhausts the airflow) -- i.e., pressure is higher on the downstream side than on the upstream side.
  • Airflow recirculation is the undesired flow of air from the downstream to the upstream side of the fan, resulting from this pressure difference.
  • the recirculating airflow passes through the running clearance between the housing and the band.
  • One way to reduce recirculation is to reduce the fan-to-housing clearance.
  • Another way to reduce recirculation is to incorporate labyrinth seals between the fan and the housing. In some cases these methods may present difficulties in economic manufacture.
  • a fan and housing combination comprising a fan having a hub that rotates on an axis and blades extending outwardly from the hub to a circular band that connects the blade tips, the combination further comprising a housing to control airflow entering the fan, leaving the fan, or both; a portion of the housing being positioned outward of the fan band so that there are running clearances between the band and the housing such that recirculating airflow moves in a pathway between the band and the housing; in which the stationary flow control vanes are connected to the housing in a position to encounter and redirect recirculating airflow, said housing and said vanes being a single injection molded plastic unit.
  • a fan and housing combination comprising a fan having a hub that rotates on an axis and blades extending outwardly from the hub to a circular band that connects the blade tips, the combination also comprising a housing to control air flow entering the fan, leaving the fan, or both; a portion of the housing being positioned outward of the fan band so that there are running clearances between the band and the housing such that recirculating airflow moves in a pathway between the band and the housing; the housing further comprising a rearward housing segment having a reduction in radius at a location rearward of the trailing edge of the fan band, and elongated motor supports which extend from the rearward housing segment to a centrally positioned motor mount; in which the stationary flow control vanes are connected to the housing in a position to encounter and redirect recirculating airflow, an airflow recirculation pathway being formed between the fan band and the housing, and at least a portion of the vanes being positioned in the pathway.
  • the invention features certain configurations for banded, axial-flow fan and housing combinations that provide a surprising combination of efficiency, low noise, and manufacturability.
  • the invention generally features fan and housing combinations which include stationary flow control vanes (e.g. thin members) positioned to encounter and redirect recirculating airflow.
  • stationary flow control vanes e.g. thin members
  • a portion of the housing is positioned outward of the fan band, and there are running clearances between the band and the housing such that recirculating airflow moves in a pathway between the fan and the housing.
  • the stationary flow control vanes are attached to the housing.
  • Recirculating airflow generally has a swirling (rotational) component of velocity imparted either by the fan blading or by vicious effects in the recirculation passage.
  • this swirl causes the fan blades to operate locally at an angle of attack different from that of the main flow.
  • Swirl also may increase inflow turbulence, which causes broadband noise, and it may lead to flow non-uniformities causing undesirable tones.
  • the invention is particularly suited for shrouded fans that draw airflow through an upstream heat exchanger, but the invention also can be applied to fans that blow air through a downstream heat exchanger. It is also particularly suited for ducted fans.
  • the first configuration features placement of the vanes generally within the space between the fan band and the housing, although embodiments in which the vanes continue downstream of the fan band are also included within the first configuration.
  • This configuration is best suited for applications in which there are axial packaging constraints, such as automotive applications in which a shrouded fan draws air through a heat exchanger immediately adjacent (usually upstream of) the fan.
  • the second configuration features placement of the vanes such that they are at least partially (or even entirely) upstream of the fan band from the perspective of the primary airflow.
  • Such configurations are particularly suited for ducted fans, such as those in airhandlers for heating, ventilating and/or cooling buildings, where axial space is less constrained.
  • the housing and vanes are a single injection molded plastic unit.
  • the vanes may be injection molded as part of an array that is assembled with the housing.
  • Preferred embodiments are also characterized by a fan-to-housing (usually a shroud) running clearance of at least 0.25% of the fan diameter.
  • a fan-to-housing usually a shroud running clearance of at least 0.25% of the fan diameter.
  • running clearance we use the term running clearance to designate the spacing between the fan band and portions of the housing that extend around the fan band.
  • the housing is characterized by a reduction in radius at a location rearward of the trailing edge of the fan band.
  • the pathway of recirculating airflow can include an inlet formed between the trailing edge of the fan band and the portion of the housing at the reduced radius.
  • the trailing edge of the fan band is the rearward-most portion of the band.
  • the band includes a lip that extends rearward of the blade trailing edge.
  • at least a portion of the vanes is positioned radially outward of the inlet to the recirculation pathway.
  • the above-described housing radius reduction can reduce the housing radius R r (see Fig. 2A) to a value approximately equal to, or even less than, the outer radius of the trailing edge of the fan band (R b , see Fig. 2A, described below).
  • approximately equal in this context means a radius that would risk interference if the portion of the housing with the reduced radius were not offset axially from the fan band.
  • the two radii may differ by less than standard or nominal radial running clearance "C" (see Fig. 2A).
  • the housing comprises a rearward housing segment extending from the radius reduction rearwardly to the rearward housing (shroud) terminus.
  • Elongated motor supports may be attached to that rearward housing segment, extending from the housing to a centrally positioned motor mount.
  • the inside diameter of the housing may increase, producing a flare to improve performance.
  • an inlet to the recirculation pathway is formed between the housing and the trailing edge of the band; the housing comprises a rearward portion which extends first rearwardly and then inwardly and forwardly, forming a pocket axially rearward of the inlet of the recirculation flow path.
  • Such pockets may have a rounded back or a straight back.
  • a portion of the vanes may extend into the pocket, and at least a portion of the vanes is axially rearward of the trailing edge of the band.
  • the vanes may be characterized by a reduction in radius at a position axially rearward of the trailing edge of the fan band.
  • the recirculating airflow pathway includes an outlet formed between the housing and an outwardly flaring segment of the leading edge of the fan band. Advantages may be achieved according to the invention with other geometries that do not include this detail, however.
  • the vanes may be straight (radial or non-radial) taken in a section in a plane normal to the fan axis. Alternatively, the vanes may be curved taken in a section in a plane normal to the fan axis.
  • the space through which airflow recirculates comprises a restriction upstream (from the perspective of recirculating airflow) of the vanes.
  • a restriction upstream from the perspective of recirculating airflow
  • the band comprises a lip flaring outwardly to establish the above described restriction.
  • the vanes may be part of a single injection molded plastic piece.
  • the vanes may be arranged in an array whose inward tips are connected by an inner ring.
  • the inner ring gives structural rigidity to the vane assembly, which allows the housing to be formed around the vane assembly.
  • the vanes may be molded in various configurations that better match the direction of incoming recirculating airflow. These configurations may be particularly beneficial in fans producing a relatively low pressure rise at some segment of the duty cycle.
  • the vanes may be molded so that the end faces of the vanes are beveled (preferably at least 20° and most preferably at least 30°) so that the high pressure side surfaces extend slightly further upstream (from the perspective of recirculation airflow) than the low pressure side surfaces.
  • the sides of the vanes can also be hooked so that the high pressure side surfaces are concave near the upstream end of the vanes (e.g. so that the radius of the concave portion is between 0.1S and 1.0S, where S is the spacing between adjacent vanes).
  • the vanes may be angled slightly from purely radial, with the radially inward tip being inclined towards recirculation flow impinging on the vanes.
  • the vanes (or at least the high pressure side of the vanes, with the low pressure side being straight) may be curved in a planar section normal to the fan axis (e.g., the section may be cylindrical with a radius of curvature of between 0.15D and 0.3D).
  • Fig. 1A is a side view in section of a fan and shroud according to the invention, including an upstream heat exchanger.
  • Fig. 1B shows a prior art fan.
  • Figs. 2A-2D are views in section of portions of fan and shroud combinations according to the invention, showing alternative configurations of the shroud radius reduction.
  • Figs. 3A and 3B are sections of fan and shroud combinations showing variations in shroud design upstream of the vanes.
  • Figs. 4A-4C are diagrammatic representations of arrays of vanes according to the invention in circumferential view.
  • Figs. 5A and 5B are side views, in section, of other fan/shroud combinations according to the invention, in which a heat exchanger is downstream of the fan.
  • Fig. 6 is a diagrammatic representation of a fan and duct combination according to the invention.
  • Figs. 7-9 are side views in section of other fan and housing combinations.
  • Fig. 10 is a side view in section of a fan and duct showing vanes upstream of the fan band.
  • Figs. 11 is a side view in section of a ducted, banded fan being used with a dual-ring vane assembly.
  • Fig. 12 is an end view of the vanes taken along 12-12 of Fig. 11, showing only a portion of the vanes.
  • Fig. 13A is a close-up of the circled portion of Fig. 12.
  • Figs. 13B and 13C are similar views of alternative configurations.
  • Fig. 14A is a sectional view taken along 14A-14A of Fig. 12 showing square leading edge details for a pair of vanes.
  • Fig. 14B is a section of an alternative vane configuration.
  • Fig. 15 is perspective view of one particular vane embodiment according to the invention.
  • FIG. 1A fan 20 is positioned in shroud 26 to pull air through heat exchanger 21.
  • Axis A is the fan's rotational axis.
  • Fan 20 has a band 24 connecting the outer tips of blades 22. Band 24 terminates at its upstream edge in a lip 30.
  • Vanes 28 are attached to shroud 26.
  • Figs. 4A-4C are sectional views (perpendicular to the fan axis) of arrays of vanes 28, showing the alternative configurations of the vanes. The sections are taken looking rearwardly along the fan axis, and the direction of fan rotation is clockwise.
  • vanes 28E are radial.
  • vanes 28F are straight, and they are angled from the radial direction.
  • vanes 28G are curved to receive airflow having a rotational component in the direction of fan rotation.
  • the design of vanes 28 and shroud 26 permits the entire shroud and the vanes to be injection molded as a single unit.
  • the spacing between vanes 28 is selected to remove swirl without excessively blocking airflow. In typical applications there will be more than 10 and less than 1000 (e.g., 30-200) of these vanes, although there may be fewer or more in specific applications.
  • Fan 20 and shroud 26 are designed with running clearances to avoid interference between band 24 and shroud 26.
  • Shroud 26 has a radius reduction rearward of band 24 (formed by shroud segments 27 and 29), which reduces the shroud radius (R r ) to less than the outer radius (R b ) of band 24 at its trailing edge, plus clearance "C”.
  • Fig. 2A illustrates R r , R b and R c on a fan and housing similar to that shown in Fig. 1A.
  • Shroud 26 is mounted to radiator 21 by mounts 23.
  • Fig. 1B is a figure reproduced from Gray, U.S. 4,548,548.
  • the recirculation flow path between the shroud and the band does not include vanes.
  • the radius of the shroud is relatively constant rearward of the lip of the band, at a value that must provide clearance between the band and the shroud.
  • the radius of the fan band R b , the radius of the shroud after the reduction R r , and clearance "C" are shown in Fig. 2A, discussed below.
  • the widths of inlet 34 and outlet 36 are as narrow as manufacturing processes permit to minimize leakage and resulting lost energy.
  • Figs. 2A-2D are diagrammatic representations of details of fan/shroud combinations that are similar to the one shown in Fig. 1A, with differing inlets to the recirculation flow path space.
  • fan blades terminate in a similar band. Vanes are included in the space between the fan band and the shroud.
  • the shroud includes a radius reduction rearward of the trailing edge of the fan band. The specific designs of the shrouds differ in these radius reductions, thus providing different inlets to the recirculation flow path.
  • the embodiments of Figs. 2A-2D will only be described to highlight the differences among those embodiments.
  • Features in Figs. 2A-2D are numbered with numbers corresponding to those used in Figs. 1A.
  • shroud radius reduction segments 27A and 29A are rearward of the trailing edge of band 24A.
  • the inner radius of segment 29A is less than the outer radius of the trailing edge of band 24A.
  • shroud segment 29B has an inner radius slightly larger than the outer radius of the trailing edge of band 24B.
  • segment 29C has a radius approximately equal to that of the fan band. Segment 26C flares outwardly, to optimize performance in some applications.
  • the thickness of the shroud may decrease with rearward extent, so that the outer shroud diameter in this segment flares less or is generally cylindrical.
  • segment 29D is rounded to form a pocket 48D. This geometry allows a large amount of flare to be used on an injection moldable part. Vanes 28D extend into the pocket.
  • Figs 3A and 3B are sections of fan and housing combinations that are similar to the fan of Fig 1A, except in the configuration of shroud 26' and 26'' upstream of the fan.
  • fan blade 22 terminates in a band 24.
  • Vanes 28 are positioned in the recirculation flow path.
  • Motor supports 37 extend from a downstream extension of the shroud.
  • a restriction is not formed between the band 24' and shroud 26'.
  • the radius of shroud segment 26" is essentially constant, and a restriction is formed between band 24 and shroud 26''. Both configurations are within the spirit of the invention.
  • Figs. 5A and 5B show two alternative fan and housing configurations in which the fan is upstream of the heat exchanger, and the shroud guides airflow (shown generally with an arrow) from the fan into the heat exchanger.
  • fan blade 54 has a band 55 with a lip 56 that forms an inlet to the fan. Airflow recirculation takes place through inlet 67 into space 57 between the shroud 58 and the band 55, and exits outlet 68. Vanes 59 are positioned-in space 57 to encounter recirculating airflow and reduce swirl in the recirculating airflow.
  • Fan motor 65 is positioned between the fan and the heat exchanger 62.
  • Shroud 58 includes a segment 60 to which motor supports 61 are attached.
  • Fig. 5B fan 70 blows air into downstream heat exchanger 82.
  • motor 71 of the assembly of Fig. 5B is upstream of the fan.
  • the fan band 75 has a lip 76 on the downstream side, and the inlet to the fan is formed by a shroud segment 80 which curves inwardly and back toward heat exchanger 82.
  • the motor 71 is attached to support 81. Recirculating airflow moves through inlet 83 to space 77 between band 75 and shroud 78, and exits outlet 84. Vanes 79 are positioned in space 77 to encounter that recirculating airflow and to reduce swirl in it. In this configuration, the inlet restriction upstream of the vanes and the vane shaping referenced below may be beneficial.
  • Fig. 6 is a section showing a variation of the invention useful in ducted fans.
  • the vanes 44 are provided as a separately molded part having a flared rear face 49 which terminates in an edge 50 that forms the inlet 52 for the recirculation flow path.
  • the blades 48, the band 46 and the duct 51 are similar to those described below.
  • Fig. 7 shows a fan 640 housed in a shroud 642 which guides airflow through a radiator (not shown) upstream of the fan.
  • Vanes 644 are L-shaped in this view and radial in a plane perpendicular to the fan axis.
  • Lip 646 forms a restriction inlet 648 with lip 647.
  • the vanes are spaced from 3.2 to 12.7mm (1/8 to 1/2 of an inch) apart around the circumference, with the smaller spacing being used in very small fans.
  • the fan and housing combination of Fig. 7 can also be used (with some modification) as a ducted fan.
  • the width of the recirculation outlet is at least twice the width of the recirculation inlet. Increasing the width of outlet reduces the velocity of the leakage flow thus reducing flow disruption as the recirculation flow enters the main flow.
  • fan 780 has a band 782 with an upstream edge that turns back axially to form lip 784.
  • Shroud 786 includes vanes 788.
  • a lip 790 on shroud 786 forms a restriction 792 in the recirculation path, which feeds the airflow to vanes 788 and from there to outlet 794.
  • the outlet to the recirculation path is at least twice as wide as the restriction.
  • band 800 of fan 801 has a trailing lip 802 which forms restriction 803 with shroud 804.
  • Leakage vanes 805 extend from shroud 804.
  • Bell mouth 807 together with the axially forward edge of band 800 form outlet 806 to the recirculation path.
  • Fig. 10 depicts a fan 90 in which the housing 92 is a duct or shroud having vanes 94 upstream of band 96.
  • Inlet 91 is formed between the upstream edge of band 96 and duct 92.
  • This inlet (“X") is on the order of 0.005D-0.02D. Recirculation airflow is entrained into vanes 94 and leaves through the open sides 98 of the slots between vanes 94.
  • the array of vanes is provided by a dual ring structure 217 which fits within the duct 212 just upstream of the fan 214.
  • the vane assembly may be made from molded plastic, hard plastic foam, or any suitable material which may be fashioned into the requisite geometry. As shown in Fig. 11, the assembly consists of an outer ring 216, an inner ring 218, and a plurality of vanes 220 disposed generally radially between the two rings 216, 218.
  • the ring 218 gives structural rigidity to the assembly. This is beneficial if it is desired to form the housing by wrapping sheet metal, or some other flexible material, around the perimeter of the outer ring 216 to form the duct.
  • the inner ring 218 also divides the duct into separate flow passageways, an inner primary passageway 222 through which the primary flow passes, and an outer, annular recirculation passageway 224 through which the recirculation flow passes.
  • the inner ring 218 helps to inhibit radial flow, where it exists, from reentering the fan.
  • a banded fan 214 in which the band 226 terminates in a curved lip 228.
  • the curved lip 228 forms a restriction 230 in the recirculation passageway 224.
  • the vanes 220 may be substantially flat, non-shaped vanes. Such vanes generally may provide adequate performance. As explained below, however, for other applications (e.g., low pressure rise fans or fans that are designed both for high and low pressure rise) additional vane shaping can improve performance.
  • Tangential deflection of airflow is reduced by bevelling the end face 234 of each of the vanes 220, as shown in Fig. 14B.
  • the end face 234 is beveled such that the high pressure side surface 236 of the vane projects further upstream (taken from the perspective of the recirculation flow) than the low pressure side surface 238.
  • the bevel angle, ⁇ can be at least 20°, and is preferably 30° or more.
  • the high pressure side surface 236 is made concave by the addition of a cylindrical region 242 at the leading edge 250, i.e., the juncture of the high pressure side surface 236 and end face 234.
  • the radius of curvature r of the cylindrical region 242 can be on the same order as 1/2 of the spacing between vanes.
  • the vanes can be non-radial in a section perpendicular to a plane normal to the fan axis.
  • the innermost tips 250 of the vanes 220 are inclined into the impinging recirculation flow.
  • the lean angle, ⁇ should preferably be between 3° and 10° from radial.
  • vanes (or at least the high pressure side of the vanes) of some embodiments are slightly cylindrical in a plane normal to the fan axis.
  • the center of curvature is parallel with the fan centerline and is placed on a tangent to the outside periphery of the vane.
  • the radius of curvature is approximately 20% of the fan diameter.
  • the vanes are radial at the outer periphery of the device, and are more inclined toward the flow as radius decreases.
  • Fig. 15 is a perspective view of a portion of a dual ring structure 217 looking axially toward the rear face 232 of vanes 240. As described above, the leading edge 242 of vanes 220 is beveled, and the high pressure side face 236 is shaped. The vanes are slightly cylindrical in a plane normal to the fan axis.
  • vanes can be used with fan/shroud combinations that blow air through a downstream heat exchanger.
  • they can be used with the fan/shroud combinations as generally described in a commonly owned U.S. Patent Application titled Fan Inlet With Curved Lip And Cylindrical Member Forming Labyrinth Seal, filed on June 17, 1993, by Michael Sortor, and given serial number 08/079,317.

Claims (18)

  1. Combinaison d'un ventilateur (20) et d'un boítier, comprenant un ventilateur ayant un moyeu qui tourne sur un axe et des pales (22) qui s'étendent vers l'extérieur du moyeu vers une bande circulaire (24) qui raccorde les bouts des pales, la combinaison comprenant en outre un boítier destiné au réglage de la circulation de l'air entrant dans le ventilateur, de l'air quittant le ventilateur ou des deux, une partie (26) du boítier étant disposée vers l'extérieur de la bande du ventilateur afin qu'il existe des espaces de passage entre la bande et le boítier si bien qu'un courant d'air qui recircule se déplace dans un trajet formé entre la bande et le boítier, caractérisée en ce que des ailettes fixes (28) de réglage de circulation sont raccordées au boítier en position telle qu'elles rencontrent et redirigent le courant d'air qui recircule, le boítier et les ailettes étant formés par une seule unité de matière plastique moulée par injection.
  2. Combinaison d'un ventilateur et d'un boítier selon la revendication 1, combinée à un échangeur de chaleur, dans laquelle le boítier est disposé en amont d'un échangeur de chaleur, si bien que le ventilateur pousse l'air à travers l'échangeur de chaleur.
  3. Combinaison d'un ventilateur (20) et d'un boítier comprenant un ventilateur ayant un moyeu qui tourne sur un axe et des pales qui s'étendent à l'extérieur du moyeu vers une bande circulaire qui raccorde les bouts des pales, la combinaison comprenant aussi un boítier destiné au réglage de la circulation de l'air entrant dans le ventilateur, de l'air quittant le ventilateur ou des deux, une partie du boítier étant disposée à l'extérieur de la bande du ventilateur afin qu'il existe des espaces de passage entre la bande et le boítier et que le courant d'air qui recircule se déplace suivant un trajet compris entre la bande et le boítier, le boítier comprenant en outre un segment de boítier (27, 29) tourné vers l'arrière et ayant une réduction de rayon à un emplacement qui se trouve en arrière du bord de fuite de la bande de ventilateur, et des supports allongés (37) de moteur qui s'étendent depuis le segment de boítier tourné vers l'arrière vers une monture de moteur placée au centre, caractérisée en ce que des ailettes fixes (28) de réglage de circulation sont raccordées au boítier en position telle qu'elles rencontrent et redirigent le courant d'air qui recircule, un trajet de recirculation du courant d'air étant formé entre la bande de ventilateur et le boítier, et une partie au moins des ailettes étant disposée dans ce trajet.
  4. Combinaison d'un ventilateur et d'un boítier selon la revendication 3, dans laquelle le trajet a une entrée formée entre la bande (24) de ventilateur et le boítier (26), une partie au moins des ailettes (28) est disposée radialement à l'extérieur de l'entrée (34) du trajet et la face radialement la plus interne des ailettes est arrondie ou chanfreinée.
  5. Combinaison d'un ventilateur et d'un boítier selon la revendication 3, dans laquelle, lorsque le boítier s'étend vers l'arrière depuis l'emplacement de réduction de rayon, le diamètre interne du boítier (29C, 29D) augmente.
  6. Ensemble d'un ventilateur et d'un boítier selon la revendication 5, dans lequel lorsque le boítier s'étend vers l'arrière depuis l'emplacement de réduction de rayon, l'épaisseur du boítier (29C) diminue.
  7. Combinaison d'un ventilateur et d'un boítier selon la revendication 1 ou 3, dans laquelle les ailettes (28F) considérées en coupe dans un plan perpendiculaire à l'axe du ventilateur ne sont pas radiales.
  8. Combinaison d'un ventilateur et d'un boítier selon la revendication 1 ou 3, dans laquelle les ailettes (28G) sont courbées, lorsqu'elles sont considérées en coupe par un plan perpendiculaire à l'axe du ventilateur.
  9. Combinaison d'un ventilateur et d'un boítier selon la revendication 1 ou 3, caractérisée en ce que les ailettes (79, 94, 220) sont positionnées au moins en partie en amont de la bande de ventilateur (75, 96, 226).
  10. Combinaison d'un ventilateur et d'un boítier selon la revendication 3, dans laquelle les ailettes font toutes partie d'un seul ensemble de matière plastique moulée par injection.
  11. Combinaison d'un ventilateur et d'un boítier selon la revendication 1 ou 3, dans laquelle les ailettes (220) ont une face chanfreinée d'extrémité (234).
  12. Combinaison d'un ventilateur et d'un boítier selon la revendication 11, dans laquelle les faces d'extrémité (234) des ailettes (220) sont chanfreinées avec un angle d'au moins 20°.
  13. Combinaison d'un ventilateur et d'un boítier selon la revendication 12, dans laquelle les ailettes sont disposées suivant un arrangement dont les bouts tournés vers l'intérieur sont raccordés par une bague interne.
  14. Combinaison d'un ventilateur et d'un boítier selon la revendication 11, dans laquelle le côté à haute pression (236) des ailettes a une partie concave (242) adjacente à la face d'extrémité des ailettes.
  15. Combinaison d'un ventilateur et d'un boítier selon la revendication 14, dans laquelle le rayon de la partie concave est compris entre 0,1 S et 1,0 S, S étant l'espacement des ailettes adjacentes.
  16. Combinaison d'un ventilateur et d'un boítier selon la revendication 15, dans laquelle le côté à haute pression (236) des ailettes est courbé dans un plan perpendiculaire à l'axe du ventilateur.
  17. Combinaison d'un ventilateur et d'un boítier selon la revendication 16, dans laquelle le côté à haute pression (236) des ailettes est pratiquement cylindrique en coupe dans un plan perpendiculaire à l'axe du ventilateur, avec un rayon de courbure compris entre 0,15 D et 0,3 D, D étant le diamètre du ventilateur.
  18. Combinaison d'un ventilateur et d'un boítier selon la revendication 11, dans laquelle :
    a) les faces d'extrémité (234) des ailettes (220) sont chanfreinées suivant un angle au moins égal à 20°,
    b) le côté à haute pression (236) des ailettes (220) a une partie concave (242) adjacente à la face d'extrémité des ailettes, ayant un rayon de courbure compris entre 0,1 S et 1,0 S, S étant l'espacement des ailettes adjacentes, et
    c) le côté à haute pression (236) des ailettes est pratiquement cylindrique en coupe dans un plan perpendiculaire à l'axe du ventilateur, avec un rayon de courbure compris entre 0,15 D et 0,3 D, D étant le diamètre du ventilateur.
EP94926638A 1993-08-30 1994-08-30 Boitier a recirculation controlee pour utilisation avec un ventilateur axial a pales entourees par un anneau cylindrique Expired - Lifetime EP0746689B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11395293A 1993-08-30 1993-08-30
US113952 1993-08-30
PCT/US1994/009782 WO1995006822A1 (fr) 1993-08-30 1994-08-30 Boitier de commande de reprise d'air destine aux soufflantes a ailettes pour debit axial

Publications (3)

Publication Number Publication Date
EP0746689A1 EP0746689A1 (fr) 1996-12-11
EP0746689A4 EP0746689A4 (fr) 1998-07-15
EP0746689B1 true EP0746689B1 (fr) 2002-04-24

Family

ID=22352489

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94926638A Expired - Lifetime EP0746689B1 (fr) 1993-08-30 1994-08-30 Boitier a recirculation controlee pour utilisation avec un ventilateur axial a pales entourees par un anneau cylindrique

Country Status (6)

Country Link
EP (1) EP0746689B1 (fr)
JP (1) JPH09505375A (fr)
AT (1) ATE216757T1 (fr)
DE (1) DE69430488T2 (fr)
ES (1) ES2173121T3 (fr)
WO (1) WO1995006822A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1914402A1 (fr) * 2006-10-11 2008-04-23 Behr GmbH & Co. KG Ventilateur axial et procédé destiné à éviter un flux de recirculation
DE102009012025A1 (de) 2009-03-10 2010-09-16 Behr Gmbh & Co. Kg Kühlvorrichtung für ein Kraftfahrzeug
WO2014109970A1 (fr) * 2013-01-11 2014-07-17 Carrier Corporation Ventilo-convecteur comportant un ventilateur caréné

Families Citing this family (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5577888A (en) * 1995-06-23 1996-11-26 Siemens Electric Limited High efficiency, low-noise, axial fan assembly
JP3304246B2 (ja) * 1995-10-18 2002-07-22 日立建機株式会社 エンジン冷却装置
JP4592908B2 (ja) * 2000-09-28 2010-12-08 株式会社ティラド ファンのシール構造
JP4862224B2 (ja) * 2001-06-06 2012-01-25 株式会社デンソー 軸流ファン及び熱交換装置
KR100729650B1 (ko) * 2002-02-27 2007-06-18 한라공조주식회사 소음저감구조를 가지는 쉬라우드
US6874990B2 (en) * 2003-01-29 2005-04-05 Siemens Vdo Automotive Inc. Integral tip seal in a fan-shroud structure
JP4024228B2 (ja) * 2004-06-07 2007-12-19 本田技研工業株式会社 自動2輪車用ラジエタ冷却装置
FR2874409B1 (fr) * 2004-08-19 2006-10-13 Max Sardou Ventilateur de tunnel
DE102005042556A1 (de) * 2005-09-08 2007-03-15 Temic Automotive Electric Motors Gmbh Lüfter
EP1862675B1 (fr) 2006-05-31 2009-09-30 Robert Bosch GmbH Ensemble de ventilateur axial
JP2009127422A (ja) * 2007-11-19 2009-06-11 Denso Corp 送風ファン
CN103591047B (zh) * 2008-04-15 2017-04-12 博格华纳公司 开放式叶片发动机冷却风扇护罩导向翼瓣
US8211930B2 (en) 2008-05-20 2012-07-03 Astrazeneca Ab Phenyl and benzodioxinyl substituted indazoles derivatives
DE102008046508A1 (de) * 2008-09-09 2010-03-11 Behr Gmbh & Co. Kg Lüftervorrichtung zur Belüftung eines Verbrennungsmotors, Kühlsystem mit zumindest einer Lüftervorrichtung
GB0903682D0 (en) 2009-03-04 2009-04-15 Dyson Technology Ltd A fan
GB2468312A (en) 2009-03-04 2010-09-08 Dyson Technology Ltd Fan assembly
GB0919473D0 (en) 2009-11-06 2009-12-23 Dyson Technology Ltd A fan
WO2011147318A1 (fr) 2010-05-27 2011-12-01 Li Dezheng Dispositif pour souffler de l'air au moyen d'un ensemble buse à fente étroite
GB2482549A (en) * 2010-08-06 2012-02-08 Dyson Technology Ltd A fan assembly with a heater
GB2482547A (en) 2010-08-06 2012-02-08 Dyson Technology Ltd A fan assembly with a heater
DE102010039219A1 (de) * 2010-08-11 2012-02-16 Behr Gmbh & Co. Kg Lüfter, insbesondere für ein Motorkühlungsgebläse in einem Kraftfahrzeug
JP5588565B2 (ja) 2010-10-13 2014-09-10 ダイソン テクノロジー リミテッド 送風機組立体
ES2619373T3 (es) 2010-10-18 2017-06-26 Dyson Technology Limited Conjunto de ventilador
GB2484670B (en) 2010-10-18 2018-04-25 Dyson Technology Ltd A fan assembly
WO2012059730A1 (fr) 2010-11-02 2012-05-10 Dyson Technology Limited Ensemble ventilateur
GB2493506B (en) 2011-07-27 2013-09-11 Dyson Technology Ltd A fan assembly
BR112014001474A2 (pt) 2011-07-27 2017-02-21 Dyson Technology Ltd conjunto de ventilador
GB201119500D0 (en) 2011-11-11 2011-12-21 Dyson Technology Ltd A fan assembly
GB2496877B (en) 2011-11-24 2014-05-07 Dyson Technology Ltd A fan assembly
JP5549686B2 (ja) * 2012-01-12 2014-07-16 株式会社デンソー 送風装置
GB2499041A (en) 2012-02-06 2013-08-07 Dyson Technology Ltd Bladeless fan including an ionizer
GB2499042A (en) 2012-02-06 2013-08-07 Dyson Technology Ltd A nozzle for a fan assembly
GB2499044B (en) 2012-02-06 2014-03-19 Dyson Technology Ltd A fan
GB2500017B (en) 2012-03-06 2015-07-29 Dyson Technology Ltd A Humidifying Apparatus
GB2500010B (en) 2012-03-06 2016-08-24 Dyson Technology Ltd A humidifying apparatus
GB2500012B (en) 2012-03-06 2016-07-06 Dyson Technology Ltd A Humidifying Apparatus
MY167968A (en) 2012-03-06 2018-10-09 Dyson Technology Ltd A fan assembly
GB2500011B (en) 2012-03-06 2016-07-06 Dyson Technology Ltd A Humidifying Apparatus
GB2512192B (en) 2012-03-06 2015-08-05 Dyson Technology Ltd A Humidifying Apparatus
GB2500903B (en) 2012-04-04 2015-06-24 Dyson Technology Ltd Heating apparatus
GB2501301B (en) 2012-04-19 2016-02-03 Dyson Technology Ltd A fan assembly
DE102012023454A1 (de) * 2012-11-30 2014-06-05 Brose Fahrzeugteile GmbH & Co. Kommanditgesellschaft, Würzburg Lüftereinrichtung und Fahrzeug mit einer Lüftereinrichtung
BR302013003358S1 (pt) 2013-01-18 2014-11-25 Dyson Technology Ltd Configuração aplicada em umidificador
AU350181S (en) 2013-01-18 2013-08-15 Dyson Technology Ltd Humidifier or fan
AU350140S (en) 2013-01-18 2013-08-13 Dyson Technology Ltd Humidifier or fan
AU350179S (en) 2013-01-18 2013-08-15 Dyson Technology Ltd Humidifier or fan
RU2684043C2 (ru) 2013-01-29 2019-04-03 Дайсон Текнолоджи Лимитед Вентилятор в сборе
GB2510195B (en) 2013-01-29 2016-04-27 Dyson Technology Ltd A fan assembly
CA152655S (en) 2013-03-07 2014-05-20 Dyson Technology Ltd Fan
BR302013004394S1 (pt) 2013-03-07 2014-12-02 Dyson Technology Ltd Configuração aplicada a ventilador
USD729372S1 (en) 2013-03-07 2015-05-12 Dyson Technology Limited Fan
CA152657S (en) 2013-03-07 2014-05-20 Dyson Technology Ltd Fan
CA152656S (en) 2013-03-07 2014-05-20 Dyson Technology Ltd Fan
CA152658S (en) 2013-03-07 2014-05-20 Dyson Technology Ltd Fan
TWD172707S (zh) 2013-08-01 2015-12-21 戴森科技有限公司 風扇
CA154722S (en) 2013-08-01 2015-02-16 Dyson Technology Ltd Fan
CA154723S (en) 2013-08-01 2015-02-16 Dyson Technology Ltd Fan
JP6224952B2 (ja) * 2013-08-19 2017-11-01 株式会社Soken 送風装置
GB2518638B (en) 2013-09-26 2016-10-12 Dyson Technology Ltd Humidifying apparatus
EP2886872A1 (fr) * 2013-12-17 2015-06-24 Delphi Automotive Systems Luxembourg SA Ventilateur de moteur
DE102013227025A1 (de) 2013-12-20 2015-06-25 MAHLE Behr GmbH & Co. KG Axiallüfter
GB2528708B (en) 2014-07-29 2016-06-29 Dyson Technology Ltd A fan assembly
GB2528704A (en) 2014-07-29 2016-02-03 Dyson Technology Ltd Humidifying apparatus
GB2528709B (en) 2014-07-29 2017-02-08 Dyson Technology Ltd Humidifying apparatus
JP2018096312A (ja) 2016-12-15 2018-06-21 ダイキン工業株式会社 送風機、及び送風機を有する冷凍装置
US11396888B1 (en) 2017-11-09 2022-07-26 Williams International Co., L.L.C. System and method for guiding compressible gas flowing through a duct
JP7224927B2 (ja) * 2019-01-16 2023-02-20 株式会社川本製作所 軸流ポンプ
JP6970359B2 (ja) * 2020-01-31 2021-11-24 ダイキン工業株式会社 送風装置及びそれを備えた冷凍装置
JP6856165B2 (ja) * 2020-10-19 2021-04-07 ダイキン工業株式会社 送風機、及び送風機を有する冷凍装置

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR84439E (fr) * 1961-09-11 1965-02-05 Ventilateur axial
BE747870A (fr) * 1969-03-27 1970-09-24 Aerospatiale Perfectionnements apportes aux carenages pour helices ou ventilateurs
US3677660A (en) * 1969-04-08 1972-07-18 Mitsubishi Heavy Ind Ltd Propeller with kort nozzle
US3832085A (en) * 1972-10-04 1974-08-27 Ford Motor Co Automotive fan shroud
DE2849675A1 (de) * 1978-11-16 1980-06-12 Sueddeutsche Kuehler Behr Kuehlanlage fuer brennkraftmaschinen, insbesondere in fahrzeugen
US4685513A (en) * 1981-11-24 1987-08-11 General Motors Corporation Engine cooling fan and fan shrouding arrangement
US4448573A (en) * 1982-03-25 1984-05-15 General Electric Company Single-stage, multiple outlet centrifugal blower
SE451873B (sv) * 1982-07-29 1987-11-02 Do G Pk I Experiment Axialflekt
DK345883D0 (da) * 1983-07-28 1983-07-28 Nordisk Ventilator Aksialventilator
US4548548A (en) * 1984-05-23 1985-10-22 Airflow Research And Manufacturing Corp. Fan and housing
DE3539604C1 (de) * 1985-11-08 1987-02-19 Turbo Lufttechnik Gmbh Axialgeblaese
DE8614073U1 (fr) * 1986-05-24 1988-04-07 Daimler-Benz Ag
JP3063129B2 (ja) * 1990-09-03 2000-07-12 株式会社デンソー 自動車用冷却ファン装置

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1914402A1 (fr) * 2006-10-11 2008-04-23 Behr GmbH & Co. KG Ventilateur axial et procédé destiné à éviter un flux de recirculation
DE102009012025A1 (de) 2009-03-10 2010-09-16 Behr Gmbh & Co. Kg Kühlvorrichtung für ein Kraftfahrzeug
EP2236788A1 (fr) 2009-03-10 2010-10-06 Behr GmbH & Co. KG Dispositif de refroidissement pour un véhicule automobile
US8573931B2 (en) 2009-03-10 2013-11-05 Behr Gmbh & Co. Kg Cooling apparatus for a motor vehicle
WO2014109970A1 (fr) * 2013-01-11 2014-07-17 Carrier Corporation Ventilo-convecteur comportant un ventilateur caréné
US10731881B2 (en) 2013-01-11 2020-08-04 Carrier Corporation Fan coil unit with shrouded fan

Also Published As

Publication number Publication date
WO1995006822A1 (fr) 1995-03-09
DE69430488T2 (de) 2002-12-19
EP0746689A4 (fr) 1998-07-15
DE69430488D1 (de) 2002-05-29
EP0746689A1 (fr) 1996-12-11
JPH09505375A (ja) 1997-05-27
ES2173121T3 (es) 2002-10-16
ATE216757T1 (de) 2002-05-15

Similar Documents

Publication Publication Date Title
EP0746689B1 (fr) Boitier a recirculation controlee pour utilisation avec un ventilateur axial a pales entourees par un anneau cylindrique
US5489186A (en) Housing with recirculation control for use with banded axial-flow fans
EP1340921B1 (fr) Ensemble ventilateur
US5423660A (en) Fan inlet with curved lip and cylindrical member forming labyrinth seal
AU759980B2 (en) Deswirler system for centrifugal compressor
EP0955468B1 (fr) Ventilateur radial et assemblage ventilateur/orifice
EP0622549B1 (fr) Compresseur radial et diffuseur à pales
KR100566501B1 (ko) 송풍기 및 이를 이용한 공기조화기용 실외기
EP0583091B1 (fr) Ventilateur
EP1016790B1 (fr) Stator pour ventilateur axial
EP0601119B1 (fr) Ventilateur a biais vers l'avant, et a inclinaison et a cambrage dans le sens de la corde
KR20050005086A (ko) 축류팬 쉬라우드의 스테이터
NZ569987A (en) Improved impeller for a ventilation fan that has an aerofoil section and a centrifugal accelerator portion
JPS6130160B2 (fr)
US20160305448A1 (en) Cooling fan module and system
US6206635B1 (en) Fan stator
JP2001501284A (ja) 軸流ファン
EP0602007B1 (fr) Soufflante et diffuseur d'aspirateur
CN106884804B (zh) 离心式鼓风机
JP2003184792A (ja) 送風機
JP3366265B2 (ja) 遠心送風機
JP6005256B2 (ja) 羽根車及びこれを用いた軸流送風機
JP2001248597A (ja) ターボ圧縮機及びターボ送風機
US11261871B2 (en) Dual stage blower assembly
JP2004197694A (ja) 送風機

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: 19960323

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE DE ES FR GB IT LU NL SE

A4 Supplementary search report drawn up and despatched

Effective date: 19980529

AK Designated contracting states

Kind code of ref document: A4

Designated state(s): AT BE DE ES FR GB IT LU NL SE

RHK1 Main classification (correction)

Ipc: F04D 29/54

17Q First examination report despatched

Effective date: 19990914

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

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

Owner name: ROBERT BOSCH CORPORATION

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE DE ES FR GB IT LU NL SE

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

Ref country code: NL

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

Effective date: 20020424

Ref country code: BE

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: 20020424

Ref country code: AT

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: 20020424

REF Corresponds to:

Ref document number: 216757

Country of ref document: AT

Date of ref document: 20020515

Kind code of ref document: T

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 69430488

Country of ref document: DE

Date of ref document: 20020529

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

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: 20020724

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: 20020830

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2173121

Country of ref document: ES

Kind code of ref document: T3

ET Fr: translation filed
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

26N No opposition filed

Effective date: 20030127

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

Ref country code: IT

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

Effective date: 20050830

PGRI Patent reinstated in contracting state [announced from national office to epo]

Ref country code: IT

Effective date: 20090401

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

Ref country code: ES

Payment date: 20130828

Year of fee payment: 20

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

Ref country code: FR

Payment date: 20130820

Year of fee payment: 20

Ref country code: GB

Payment date: 20130823

Year of fee payment: 20

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

Ref country code: IT

Payment date: 20130823

Year of fee payment: 20

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

Ref country code: DE

Payment date: 20131025

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69430488

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20140829

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

Ref country code: DE

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20140902

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

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20140829

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20150108

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

Ref country code: ES

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20140831