EP2592281A1 - An Axial Fan - Google Patents

An Axial Fan Download PDF

Info

Publication number
EP2592281A1
EP2592281A1 EP20120195103 EP12195103A EP2592281A1 EP 2592281 A1 EP2592281 A1 EP 2592281A1 EP 20120195103 EP20120195103 EP 20120195103 EP 12195103 A EP12195103 A EP 12195103A EP 2592281 A1 EP2592281 A1 EP 2592281A1
Authority
EP
European Patent Office
Prior art keywords
axial fan
motor
vane
fan according
angle
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.)
Granted
Application number
EP20120195103
Other languages
German (de)
French (fr)
Other versions
EP2592281B1 (en
Inventor
Colin Biggs
Wayne Glover
Anthony Breen
Clement Nguyen
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.)
Nuaire Ltd
Original Assignee
Nuaire Ltd
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 Nuaire Ltd filed Critical Nuaire Ltd
Priority to PL12195103T priority Critical patent/PL2592281T3/en
Publication of EP2592281A1 publication Critical patent/EP2592281A1/en
Application granted granted Critical
Publication of EP2592281B1 publication Critical patent/EP2592281B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/64Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
    • F04D29/646Mounting or removal of fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F04D25/10Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation the unit having provisions for automatically changing direction of output air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F04D25/12Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation the unit being adapted for mounting in apertures
    • 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
    • F04D29/542Bladed diffusers
    • 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
    • F04D29/542Bladed diffusers
    • F04D29/544Blade shapes
    • 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
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps

Definitions

  • This invention relates generally to an axial fan and, more particularly, to an improved mounting arrangement for mounting the motor of an axial fan within an outer case.
  • an axial fan typically comprises an outer cylindrical case 10 within which a motor 12 is mounted, with pressed or fabricated steel brackets 14 being used to connect and hold the motor within the case 10.
  • An impeller 16 is also provided within the case 10, which comprises a plurality of blades 18 extending from a central hub, and which is connected to the shaft of the motor for propulsion thereby.
  • a support arm for a mounting arrangement for mounting a motor of an axial fan within an outer casing, the support arm comprising an elongate vane arranged and configured to extend between said motor and the inner wall of said casing, and a connecting portion for connecting said vane to said motor, said connecting portion comprising means for varying the angle of the surface of said vane relative to the direction of airflow through said axial fan.
  • the support arm vane is designed to be fixed to the motor and not varied in angular position during service.
  • the angle is pre-selected as a specific service angle and fixed in place.
  • the invention enables specific angled arm vane to be used in variable angular orientations dependent upon the "in service” requirements and the specific fan structure and size. Accordingly, it is preferred that the vane is secured with respect to the motor at a specific "in service” angular orientation and not subsequently varied.
  • the vane is secured to the motor by means of a tightening mechanical fixing such that the orientation of the vane cannot be varied (once fixed) without releasing the mechanical fixing by untightening.
  • said connecting portion comprises an arcuate slot defining a plurality of selectable angular orientations at which said elongate vane can be mounted.
  • the arcuate slot is provided on a connecting plate which is substantially perpendicular to, and formed integrally with, said elongate vane.
  • the arcuate slot is beneficially arranged and configured to receive a connector such that it extends through said slot into a mounting hole provided on said motor.
  • the angle of the surface of the vane measured between a first axis perpendicular to the longitudinal axis of said elongate vane and a second axis parallel to the longitudinal axis of said axial fan, is between 80° and 50°, and more preferably between 70° and 55°. In one preferred embodiment, the angle is between 65° and 60°.
  • the angle of the profile of the elongate vane varies along its length.
  • the elongate vane might be twisted through, say, 15° along its length.
  • the vane could be bent by, say, 15° at, say, 3/3 of its full length.
  • a support arm for a mounting arrangement for mounting a motor of an axial fan within an outer casing, the support arm comprising an elongate vane arranged and configured to extend between said motor and the inner wall of said casing, and a connecting portion for connecting said vane to said motor, wherein the angle of the profile of the elongate vane varies along its length.
  • the elongate vane might be twisted through, say, 15° along its length.
  • the vane could be bent by, say, 15° at, say, 3/3 of its full length.
  • the present invention extends to an axial fan comprising a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing, the mounting assembly comprising one or more support arms as defined above connected between said motor and the inner wall of said outer casing.
  • the support arms are connected between the motor and the inner walls of said outer casing by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of longitudinal distances from said impeller.
  • the motor may be provided with a plurality of discrete, beneficially substantially equi-distant, mounting holes defining the respective distances.
  • an axial fan comprising a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing, said mounting assembly comprising at least one elongate vane extending between the inner wall of said casing and said motor and being connected to said motor by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of distances from said impeller.
  • brackets that are manufactured in an aerofoil section and are twisted along their length, a significant improvement in aerodynamic performance (i.e. movement of larger volumes of air at higher pressure) can be achieved. Further improvement can be achieved by making the brackets adjustable, such that the distance thereof from the impeller can be varied and the angle thereof can be matched to the direction of airflow, depending on the type of impeller being used.
  • the fan further comprises an impeller 34 consisting of a plurality of blades 36 extending from a central hub.
  • the impeller 34 is housed within the case 30 and connected to the shaft of a motor 38 for propulsion thereby.
  • the motor 38 is mounted within the case 30 by four substantially equi-distant arms 40 which are connected between the outer circumference of the motor 38 and the inner wall of the cylindrical case 30.
  • each arm 40 comprises an elongate portion 40a and a mounting portion 40b.
  • the elongate portion 40a is of substantially aerofoil section and of a length sufficient to extend between the outer circumference of the motor casing and the inner wall of the cylindrical case.
  • the mounting portion 40b extends substantially perpendicular to the elongate portion 40a and is provided with an arcuate slot 42.
  • the arm 40 is connected to the motor by means of a screw or pin which extends through the arcuate slot 42 and into a mounting hole in the motor housing.
  • a plurality of mounting holes 46 may be provided along a portion of the length of the motor housing, such that the arm 40 may be mounted at a selected one of a number of distances from the impeller.
  • the arcuate slot 42 enables the angle of the elongate portion 40a of the arm 40 to be varied, as can be seen more clearly in Figure 6 of the drawings.
  • the angle referred to in this case is the angle between a first axis (X) which is perpendicular to the length of the elongate portion 40a of the arm and a second axis (Y) which is perpendicular to the flange 32 of the cylindrical case 30.
  • the mounting portion of the arm 40 is connected to the motor housing at the end of the arcuate slot 42 closest to the elongate portion 40a of the arm 40 and the arm 40 is at 90°.
  • connection point between the mounting portion 40b of the arm and the motor housing has moved along the arcuate slot 42 in a direction away from the elongate portion 40a of the arm 40 and the arm 40 is at 75°.
  • connection point has moved even further along the arcuate slot 42 in a direction away from the elongate portion 40a of the arm 40 and the arm 40 is at 60°.
  • Figure 7 shows the relationship of velocities for an axial fan blade at a working point, and the three velocities to be considered are:
  • Figure 13 shows the force applied on the impeller blade.
  • pressure of air is perpendicular to the surface of the impeller blade and creates a dynamic force oriented by the angle " ⁇ ".
  • the support arms should be oriented at the same angle as ⁇ .
  • the total efficiency of the fan can be increased by setting the angle of the support arms to match the direction of airflow, depending on the type of impeller and the angle of the impeller blades. It has been further observed that the total efficiency of the fan can be increased by changing the angle of the arms from 90° (prior art) to 60° as discussed above in relation to Figures 9 and 10 respectively. It has also been observed that, at least in some applications, the efficiency can start to drop again from an arm angle of around 55°. From these results, it is considered that, at least for some applications, the optimum arm angle may be 65° to 60°.
  • the air flow direction along the length of the impeller blade may be located within an interval of, say, 15°.
  • the airflow direction might be about 45° and the direction might change to about 60° further along the blade towards the motor, as illustrated in Figure 14 .
  • the arm 40 might be twisted through, say, 15° along its length.
  • the arm 40 could be bent by, say, 15° at, say, 3/3 of its full length. Whilst it is thought that the first embodiment ( Figure 3 ) might provide a solution closest to the ideal, the second embodiment ( Figure 4 ) may be more practical in terms of fabrication.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

An axial fan has a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing. At least one elongate vane extends between the inner wall of the casing and the motor and is connected to the motor by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of distances from said impeller. In one embodiment, this can be achieved by means of a plurality of discrete mounting holes defining the respective distances.

Description

  • This invention relates generally to an axial fan and, more particularly, to an improved mounting arrangement for mounting the motor of an axial fan within an outer case.
  • Axial fans are generally used to move high volumes of air at low static pressure. Referring to Figure 1 of the drawings, an axial fan typically comprises an outer cylindrical case 10 within which a motor 12 is mounted, with pressed or fabricated steel brackets 14 being used to connect and hold the motor within the case 10. An impeller 16 is also provided within the case 10, which comprises a plurality of blades 18 extending from a central hub, and which is connected to the shaft of the motor for propulsion thereby.
  • It is known to a person skilled in the art that, in order to maximise aerodynamic performance and efficiency, whilst minimising noise generation, it is desirable to maximise the distance between the rotating impeller 16, 18 and the bracket arrangement 14. In fact, if the bracket arrangement could be omitted completely then turbulence would be eliminated along with any losses caused thereby. In practice, however, there are significant limitations in this regard, for example, there may be tight constraints on the overall size of the product or design limitations on the length of the shaft of the motor on which the impeller is mounted.
  • It is therefore an object of the present invention to provide an improved mounting arrangement for mounting the motor of an axial fan within its outer case, which enables the aerodynamic performance of the axial fan to be significantly increased without a corresponding increase in input power or speed.
  • In accordance with a first aspect of the present invention, there is provided a support arm for a mounting arrangement for mounting a motor of an axial fan within an outer casing, the support arm comprising an elongate vane arranged and configured to extend between said motor and the inner wall of said casing, and a connecting portion for connecting said vane to said motor, said connecting portion comprising means for varying the angle of the surface of said vane relative to the direction of airflow through said axial fan.
  • The support arm vane is designed to be fixed to the motor and not varied in angular position during service. The angle is pre-selected as a specific service angle and fixed in place. The invention enables specific angled arm vane to be used in variable angular orientations dependent upon the "in service" requirements and the specific fan structure and size. Accordingly, it is preferred that the vane is secured with respect to the motor at a specific "in service" angular orientation and not subsequently varied. Beneficially the vane is secured to the motor by means of a tightening mechanical fixing such that the orientation of the vane cannot be varied (once fixed) without releasing the mechanical fixing by untightening.
  • Preferably, said connecting portion comprises an arcuate slot defining a plurality of selectable angular orientations at which said elongate vane can be mounted. In one exemplary embodiment, the arcuate slot is provided on a connecting plate which is substantially perpendicular to, and formed integrally with, said elongate vane. The arcuate slot is beneficially arranged and configured to receive a connector such that it extends through said slot into a mounting hole provided on said motor. In a preferred embodiment, the angle of the surface of the vane, measured between a first axis perpendicular to the longitudinal axis of said elongate vane and a second axis parallel to the longitudinal axis of said axial fan, is between 80° and 50°, and more preferably between 70° and 55°. In one preferred embodiment, the angle is between 65° and 60°.
  • Beneficially, the angle of the profile of the elongate vane varies along its length. In one embodiment, the elongate vane might be twisted through, say, 15° along its length. Alternatively, the vane could be bent by, say, 15° at, say, 3/3 of its full length.
  • In fact, in accordance with a second aspect of the present invention, there is provided a support arm for a mounting arrangement for mounting a motor of an axial fan within an outer casing, the support arm comprising an elongate vane arranged and configured to extend between said motor and the inner wall of said casing, and a connecting portion for connecting said vane to said motor, wherein the angle of the profile of the elongate vane varies along its length.
  • Once again, in one embodiment, the elongate vane might be twisted through, say, 15° along its length. Alternatively, the vane could be bent by, say, 15° at, say, 3/3 of its full length.
  • The present invention extends to an axial fan comprising a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing, the mounting assembly comprising one or more support arms as defined above connected between said motor and the inner wall of said outer casing.
  • Preferably, the support arms are connected between the motor and the inner walls of said outer casing by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of longitudinal distances from said impeller. Preferably, the motor may be provided with a plurality of discrete, beneficially substantially equi-distant, mounting holes defining the respective distances.
  • In accordance with a third aspect of the present invention, there is provided an axial fan comprising a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing, said mounting assembly comprising at least one elongate vane extending between the inner wall of said casing and said motor and being connected to said motor by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of distances from said impeller.
  • It has been determined that by providing mounting brackets that are manufactured in an aerofoil section and are twisted along their length, a significant improvement in aerodynamic performance (i.e. movement of larger volumes of air at higher pressure) can be achieved. Further improvement can be achieved by making the brackets adjustable, such that the distance thereof from the impeller can be varied and the angle thereof can be matched to the direction of airflow, depending on the type of impeller being used.
  • These and other aspects of the present invention will be apparent from, and elucidated with reference to, the embodiments described herein.
  • Embodiments of the present invention will now be described by way of examples only and with reference to the accompanying drawings, in which:
    • Figure 1 is a perspective view of an axial fan according to the prior art;
    • Figure 2 is a perspective view of an axial fan including a mounting arrangement according to an exemplary embodiment of the present invention;
    • Figure 3 is a perspective view of a mounting arm of a mounting arrangement according to a first exemplary embodiment of the present invention;
    • Figure 4 is a perspective view of a mounting arm of a mounting arrangement according to a second exemplary embodiment of the present invention;
    • Figure 5 is a close-up view of a motor-connecting portion of one of the mounting arms of the mounting arrangement of Figure 2;
    • Figure 6 is a schematic illustration showing the support arm at various angles relative to the airflow direction;
    • Figures 7 and 8 are illustrative of the relationship of velocities of an axial fan blade at two respective points;
    • Figures 9, 10, 11 and 12 are illustrative of airflow as a result of angling the support arms at 90°, the ideal position, under-rotation of the support arms, and over-rotation of the support arms, respectively;
    • Figure 13 illustrates the force applied to an impeller blade during use; and
    • Figure 14 illustrates the variation in airflow direction along the length of an impeller blade.
  • Referring to Figure 2 of the drawings, an axial fan according to an exemplary embodiment of the present invention comprises a cylindrical outer case 30 having a circumferential flange 32 at each end thereof, each flange extending upwardly relative to the outer wall of the case 30 and substantially perpendicular thereto. The fan further comprises an impeller 34 consisting of a plurality of blades 36 extending from a central hub. The impeller 34 is housed within the case 30 and connected to the shaft of a motor 38 for propulsion thereby. The motor 38 is mounted within the case 30 by four substantially equi-distant arms 40 which are connected between the outer circumference of the motor 38 and the inner wall of the cylindrical case 30.
  • Referring to Figure 5 of the drawings, each arm 40 comprises an elongate portion 40a and a mounting portion 40b. The elongate portion 40a is of substantially aerofoil section and of a length sufficient to extend between the outer circumference of the motor casing and the inner wall of the cylindrical case. The mounting portion 40b extends substantially perpendicular to the elongate portion 40a and is provided with an arcuate slot 42. In use, the arm 40 is connected to the motor by means of a screw or pin which extends through the arcuate slot 42 and into a mounting hole in the motor housing. As shown, a plurality of mounting holes 46 may be provided along a portion of the length of the motor housing, such that the arm 40 may be mounted at a selected one of a number of distances from the impeller.
  • The arcuate slot 42 enables the angle of the elongate portion 40a of the arm 40 to be varied, as can be seen more clearly in Figure 6 of the drawings. The angle referred to in this case is the angle between a first axis (X) which is perpendicular to the length of the elongate portion 40a of the arm and a second axis (Y) which is perpendicular to the flange 32 of the cylindrical case 30. Thus, in Figure 6a, the mounting portion of the arm 40 is connected to the motor housing at the end of the arcuate slot 42 closest to the elongate portion 40a of the arm 40 and the arm 40 is at 90°. In Figure 6b, the connection point between the mounting portion 40b of the arm and the motor housing has moved along the arcuate slot 42 in a direction away from the elongate portion 40a of the arm 40 and the arm 40 is at 75°. In Figure 6c, the connection point has moved even further along the arcuate slot 42 in a direction away from the elongate portion 40a of the arm 40 and the arm 40 is at 60°.
  • This ability to vary the angle of the arm 40 relative to the airflow caused by the impeller results in significant advantages in terms of increased aerodynamic performance, because the angle of the arm can be set to match the direction of the airflow, depending on the type of impeller used, as will now be described in more detail.
  • Consider first the basic theory in relation to an axial fan. Figure 7 shows the relationship of velocities for an axial fan blade at a working point, and the three velocities to be considered are:
    • Absolute air flow velocity (local air flow velocity/fix coordinates (x,y)): V = Q v S
      Figure imgb0001
      • Q v : Volume air flow (m3/s)
      • S : Section of the air flow considerate (m2)
      • At the inlet fan, this velocity is axial to the impeller.
    • Blade velocity: U = R . ω
      Figure imgb0002
      • R : Radius of the blade (m)
      • ω : Angular velocity of the blade (rad/s)
    • Relative air flow velocity (air flow velocity/rotation coordinates at the point considerate) : V = U = W
      Figure imgb0003
  • At the fan outlet, the airflow exhibits helicoidal movement and the velocities triangle at the point to be considered hereinafter is represented in Figure 8. An evaluation of the motor support arms and the effect on airflow of different angular orientations thereof relative to the airflow is illustrated in Figures 9,10, 11 and 12.
  • Referring to Figure 9, when the arm is fixed at 90° (Figure 3a), the angle formed by the direction of fluid and the surface of the arm is significant. As a consequence of the illustrated arrangement, at a high velocity airflow, turbulence (depicted at 50) occurs because of a flow separation of the air, which results in a consequential decrease in performance.
  • In contrast, if the arm is oriented to match the direction of air flow, better performance can be achieved. In an ideal case (a "laminar flow" situation), whereby the support arm is oriented precisely relative to the direction of air flow, the profile of the velocity can be considered to be as shown in Figure 10. If, on the other hand, the support arm is angled relative to the airflow, but by an insufficient amount, turbulence will once again occur (as illustrated in Figure 11), but still to a lesser extent that if the arms are fixed at 90°. So even if the ideal case is attained, turbulence is relatively low compared with prior art arrangements.
  • Finally, and for completeness, if the support arms are rotated too much relative to the direction of airflow, a similar case to the previous one occurs and the consequential turbulence is created because of the flow separation (air wake), as illustrated in Figure 12, but again to a lesser extent than in the case where the arms are fixed at 90°.
  • Depending on the impeller blade angle (which is a significant contributory factor of airflow direction), it is possible to estimate the ideal angular rotation of the support arms to optimise aerodynamic performance. Figure 13 shows the force applied on the impeller blade. Consider that pressure of air is perpendicular to the surface of the impeller blade and creates a dynamic force oriented by the angle "α". In order to achieve the optimum performance, the support arms should be oriented at the same angle as α. However, fluctuation of the air is constant, whereas the direction is variable, so the angle α can only be estimated by using the relationship: A = 90 - β ;
    Figure imgb0004

    where β is the impeller blade angle.
  • Experimental results have shown the total efficiency of the fan can be increased by setting the angle of the support arms to match the direction of airflow, depending on the type of impeller and the angle of the impeller blades. It has been further observed that the total efficiency of the fan can be increased by changing the angle of the arms from 90° (prior art) to 60° as discussed above in relation to Figures 9 and 10 respectively. It has also been observed that, at least in some applications, the efficiency can start to drop again from an arm angle of around 55°. From these results, it is considered that, at least for some applications, the optimum arm angle may be 65° to 60°.
  • Another significant consideration is that there is a variation of the air flow direction along the length of the impeller blade. This variation may be located within an interval of, say, 15°. For example, by the tip of the blade, the airflow direction might be about 45° and the direction might change to about 60° further along the blade towards the motor, as illustrated in Figure 14. Thus, in a preferred embodiment, it is desirable to have a variation, preferably progressive, of the support arm angle within the case, as well as having the arm orientated according to the air flow direction.
  • Referring to Figure 3, in one exemplary embodiment, the arm 40 might be twisted through, say, 15° along its length. Alternatively, as shown in Figure , the arm 40 could be bent by, say, 15° at, say, 3/3 of its full length. Whilst it is thought that the first embodiment (Figure 3) might provide a solution closest to the ideal, the second embodiment (Figure 4) may be more practical in terms of fabrication.
  • It should be noted that the above-mentioned embodiments illustrate rather than limit the invention, and that those skilled in the art will be capable of designing many alternative embodiments without departing from the scope of the invention as defined by the appended claims. In the claims, any reference signs placed in parentheses shall not be construed as limiting the claims. The word "comprising" and "comprises", and the like, does not exclude the presence of elements or steps other than those listed in any claim or the specification as a whole. The singular reference of an element does not exclude the plural reference of such elements and vice-versa. The invention may be implemented by means of hardware comprising several distinct elements. In a device claim enumerating several means, several of these means may be embodied by one and the same item of hardware. The mere fact that certain measures are recited in mutually different dependent claims does not indicate that a combination of these measures cannot be used to advantage.

Claims (13)

  1. An axial fan comprising a motor and an impeller housed within an outer casing, the fan further comprising a mounting assembly for mounting said motor within said casing, said mounting assembly comprising at least one elongate vane extending between the inner wall of said casing and said motor and being connected to said motor by means of a connector assembly comprising means for connecting said vane to said motor at a selected one of a plurality of distances from said impeller.
  2. An axial fan according to claim 1, wherein the motor housing is provided with a plurality of discrete mounting holes defining the respective distances.
  3. An axial fan according to claim 1 or claim 2, wherein the connector assembly for connecting the vane to the motor comprises a connecting portion said connecting portion comprising means for varying the angle of the surface of said vane relative to the direction of airflow through said axial fan.
  4. An axial fan according to any preceding claim, wherein the vane is secured with respect to the motor by means of a mechanical fixing such that the orientation of the vane cannot be varied once fixed, without releasing the mechanical fixing.
  5. An axial fan according to any preceding claim, wherein said connecting portion comprises an arcuate slot defining a plurality of selectable angular orientations at which said elongate vane can be mounted.
  6. An axial fan according to claim 5, wherein the arcuate slot is provided on a connecting plate which is substantially perpendicular to, and formed integrally with, said elongate vane.
  7. An axial fan according to claim 5 or claim 6, wherein the arcuate slot is arranged and configured to receive a connector such that said connector extends through said slot into a mounting hole provided on the housing of said motor.
  8. An axial fan according to any one of the preceding claims, wherein the angle of the surface of the vane, measured between a first axis perpendicular to the longitudinal axis of said elongate blade and a second axis parallel to the longitudinal axis of said axial fan, is between 80° and 50°.
  9. An axial fan according to claim 8, wherein said angle is between 70° and 55°.
  10. An axial fan according to claim 9, wherein said angle is between 65° and 60°.
  11. An axial fan according to any of the preceding claims, where the angle of the profile of the elongate vane varies along its length.
  12. An axial fan according to claim 11, wherein the elongate vane is twisted through along its length.
  13. An axial fan according to claim 12, wherein the vane is bent by an angle at a point along its full length.
EP12195103.2A 2007-12-14 2008-12-15 An Axial Fan Active EP2592281B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12195103T PL2592281T3 (en) 2007-12-14 2008-12-15 An Axial Fan

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0724355.3A GB2455553B (en) 2007-12-14 2007-12-14 Motor mounting assembly for an axial fan
EP08861453.2A EP2225468B1 (en) 2007-12-14 2008-12-15 Motor mounting assembly for an axial fan

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP08861453.2 Division 2008-12-15
EP08861453.2A Division EP2225468B1 (en) 2007-12-14 2008-12-15 Motor mounting assembly for an axial fan

Publications (2)

Publication Number Publication Date
EP2592281A1 true EP2592281A1 (en) 2013-05-15
EP2592281B1 EP2592281B1 (en) 2015-10-28

Family

ID=39048084

Family Applications (2)

Application Number Title Priority Date Filing Date
EP08861453.2A Active EP2225468B1 (en) 2007-12-14 2008-12-15 Motor mounting assembly for an axial fan
EP12195103.2A Active EP2592281B1 (en) 2007-12-14 2008-12-15 An Axial Fan

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP08861453.2A Active EP2225468B1 (en) 2007-12-14 2008-12-15 Motor mounting assembly for an axial fan

Country Status (5)

Country Link
EP (2) EP2225468B1 (en)
ES (1) ES2561717T3 (en)
GB (1) GB2455553B (en)
PL (1) PL2592281T3 (en)
WO (1) WO2009077737A2 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101839248B (en) * 2010-03-24 2011-08-24 常熟市鼓风机有限公司 Ventilation device for textile workshop
CN107129538B (en) 2010-04-27 2021-07-16 西兰制药公司 Peptide conjugates of GLP-1 receptor agonists and gastrin and uses thereof
WO2013064669A1 (en) 2011-11-03 2013-05-10 Zealand Pharma A/S Glp-1 receptor agonist peptide gastrin conjugates
CN104662038B (en) 2012-07-23 2018-11-06 西兰制药公司 Glucagon analogue
TWI608013B (en) 2012-09-17 2017-12-11 西蘭製藥公司 Glucagon analogues
CN105745222A (en) 2013-10-17 2016-07-06 西兰制药公司 Acylated glucagon analogues
US9988429B2 (en) 2013-10-17 2018-06-05 Zealand Pharma A/S Glucagon analogues
TWI670281B (en) 2013-11-06 2019-09-01 西蘭製藥公司 Gip-glp-1 dual agonist compounds and methods
CA2929107C (en) 2013-11-06 2023-09-26 Zealand Pharma A/S Glucagon-glp-1-gip triple agonist compounds
ES2883345T3 (en) 2014-10-29 2021-12-07 Zealand Pharma As GIP agonist compounds and methods
JP6989385B2 (en) 2015-04-16 2022-01-05 ジーランド ファーマ アクティーゼルスカブ Acylated glucagon analog
CN104879327A (en) * 2015-06-01 2015-09-02 蚌埠市蚌风风机有限公司 Axial flow fan
CN106122056B (en) * 2016-08-24 2018-11-27 中国船舶电站设备有限公司 A kind of load box cooling system and its dedicated axial flow blower
BR112019010624A2 (en) 2016-12-09 2019-10-22 Zealand Pharma As double acylated glp-1 / glp-2 agonists and composition
KR102156631B1 (en) * 2019-11-18 2020-09-16 (주)신광 Pump structure
CN113898419A (en) * 2021-10-10 2022-01-07 中国航发沈阳发动机研究所 Air inlet casing structure and assembling method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB723798A (en) * 1951-02-26 1955-02-09 Voith Gmbh J M Improvements in axial-flow turbines or pumps
GB1330620A (en) * 1971-05-14 1973-09-19 Trox Gmbh Geb Axialflow blower
US3790114A (en) * 1972-01-10 1974-02-05 Carrier Corp Fan motor mount
US20030133815A1 (en) * 2002-01-16 2003-07-17 Grant Alan Peter Mounting bracket for fan motor
US20050186070A1 (en) * 2004-02-23 2005-08-25 Ling-Zhong Zeng Fan assembly and method

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2037395A (en) * 1935-04-26 1936-04-14 Alfred E Seelig Multistage fan
GB500965A (en) * 1937-08-18 1939-02-20 Aerex Ltd Improvements relating to screw impeller fans and pumps
GB672194A (en) * 1949-11-01 1952-05-14 Westinghouse Electric Int Co Improvements in or relating to fans
CH318567A (en) * 1953-05-23 1957-01-15 Rolls Royce Multi-stage axial flow compressor
GB907323A (en) * 1958-12-29 1962-10-03 Entwicklungsbau Pirna Veb Improvements in or relating to axial flow compressors
CH399643A (en) * 1962-03-09 1965-09-30 A De Jong N V Ventilateur axial
JPS58102039A (en) * 1981-12-14 1983-06-17 Toshiba Corp Blower
JPH01117996A (en) * 1987-10-30 1989-05-10 Mitsubishi Electric Corp Electric fan with wind changeover mechanism
CH687637A5 (en) * 1993-11-04 1997-01-15 Micronel Ag Axialkleinventilator.
TW476391U (en) * 2001-03-14 2002-02-11 Chuan-Shing Jeng Structure improvement for propelling fan of heating gun or hair dryer
TWI281846B (en) * 2003-05-30 2007-05-21 Delta Electronics Inc Heat-dissipating device and a housing thereof
DE20312448U1 (en) * 2003-08-12 2003-10-30 Datech Technology Co Ventilator fan for electronic equipment has support ribs with cambered profile optimizing airflow to oncoming fan blades

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB723798A (en) * 1951-02-26 1955-02-09 Voith Gmbh J M Improvements in axial-flow turbines or pumps
GB1330620A (en) * 1971-05-14 1973-09-19 Trox Gmbh Geb Axialflow blower
US3790114A (en) * 1972-01-10 1974-02-05 Carrier Corp Fan motor mount
US20030133815A1 (en) * 2002-01-16 2003-07-17 Grant Alan Peter Mounting bracket for fan motor
US20050186070A1 (en) * 2004-02-23 2005-08-25 Ling-Zhong Zeng Fan assembly and method

Also Published As

Publication number Publication date
GB2455553A (en) 2009-06-17
WO2009077737A3 (en) 2009-08-20
PL2592281T3 (en) 2016-07-29
GB0724355D0 (en) 2008-01-30
GB2455553B (en) 2012-10-24
EP2225468B1 (en) 2013-09-25
ES2561717T3 (en) 2016-02-29
EP2592281B1 (en) 2015-10-28
EP2225468A2 (en) 2010-09-08
WO2009077737A2 (en) 2009-06-25

Similar Documents

Publication Publication Date Title
EP2592281B1 (en) An Axial Fan
KR102518997B1 (en) double inverted fan
US20050186070A1 (en) Fan assembly and method
US9512726B2 (en) Impeller and method for driving fluids using the same
US6244818B1 (en) Fan guard structure for additional supercharging function
US6045327A (en) Axial flow fan assembly and one-piece housing for axial flow fan assembly
FI122540B (en) Radiaalisiipipyörä
EP0471089A1 (en) Device for generating fluid flow and method of manufacture thereof
JP4374897B2 (en) Axial fan
WO2006011036A1 (en) Axial impeller with enhanced flow
US20080187439A1 (en) Blower assembly with pre-swirler
WO2008127611A1 (en) High efficiency fan blades with airflow-directing baffle elements
EP2530331A2 (en) Axial fan assembly for a vehicle cooling system
CN111441977B (en) Axial flow fan blade, fan assembly and air conditioner with same
CN106812721B (en) Centrifugal fan
EP2739861B1 (en) Axial blower
JP2020536193A (en) Axial fan blades with wavy wings and trailing edge serrations
JP3130089U (en) Centrifugal blower
US10662971B2 (en) Phi fan
KR20070066240A (en) Fan
EP2884115B1 (en) Axial fan with blade leading edge that protrudes axially upstream of the hub and that includes a bend (kink) as seen in a radial direction perpendicular to the radial extension of the blade
US20070122287A1 (en) Fan blade assembly
WO2007064314A1 (en) Fan blade and blade assembly
JP2008232019A (en) Impeller for turbofan
CN116658457A (en) Impeller, centrifugal fan and range hood

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

AC Divisional application: reference to earlier application

Ref document number: 2225468

Country of ref document: EP

Kind code of ref document: P

AK Designated contracting states

Kind code of ref document: A1

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

17P Request for examination filed

Effective date: 20131029

RBV Designated contracting states (corrected)

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

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: F04D 25/08 20060101AFI20150413BHEP

Ipc: F04D 29/56 20060101ALI20150413BHEP

Ipc: F04D 29/54 20060101ALI20150413BHEP

Ipc: F04D 29/64 20060101ALI20150413BHEP

INTG Intention to grant announced

Effective date: 20150522

INTC Intention to grant announced (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AC Divisional application: reference to earlier application

Ref document number: 2225468

Country of ref document: EP

Kind code of ref document: P

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

INTG Intention to grant announced

Effective date: 20150522

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 758112

Country of ref document: AT

Kind code of ref document: T

Effective date: 20151115

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008040948

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2561717

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20160229

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 758112

Country of ref document: AT

Kind code of ref document: T

Effective date: 20151028

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20151028

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: 20160228

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: 20160128

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: 20151028

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: 20151028

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

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: 20160129

Ref country code: FI

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

Effective date: 20151028

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: 20151028

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: 20151028

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: 20151028

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: 20160229

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

Ref country code: CZ

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

Effective date: 20151028

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: 20151028

Ref country code: LU

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: 20151215

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008040948

Country of ref document: DE

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

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: 20151028

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: 20151028

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: 20151028

Ref country code: SK

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

Effective date: 20151028

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: 20160729

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

Ref country code: CH

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

Effective date: 20151231

Ref country code: LI

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

Effective date: 20151231

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: 20151028

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

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: 20151028

Ref country code: HU

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

Effective date: 20081215

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

Ref country code: CY

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

Effective date: 20151028

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: 20151028

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

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: 20151028

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

Free format text: REGISTERED BETWEEN 20230817 AND 20230823

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

Ref country code: GB

Payment date: 20231229

Year of fee payment: 16

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

Ref country code: NL

Payment date: 20231222

Year of fee payment: 16

Ref country code: IE

Payment date: 20231228

Year of fee payment: 16

Ref country code: FR

Payment date: 20231219

Year of fee payment: 16

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

Ref country code: PL

Payment date: 20231124

Year of fee payment: 16

Ref country code: BE

Payment date: 20231219

Year of fee payment: 16

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

Ref country code: ES

Payment date: 20240110

Year of fee payment: 16

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

Ref country code: DE

Payment date: 20231222

Year of fee payment: 16