EP2182109B1 - Method of manufacturing a refiner - Google Patents

Method of manufacturing a refiner Download PDF

Info

Publication number
EP2182109B1
EP2182109B1 EP09174199.1A EP09174199A EP2182109B1 EP 2182109 B1 EP2182109 B1 EP 2182109B1 EP 09174199 A EP09174199 A EP 09174199A EP 2182109 B1 EP2182109 B1 EP 2182109B1
Authority
EP
European Patent Office
Prior art keywords
refiner
disc
frame
frame structure
rotor
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.)
Not-in-force
Application number
EP09174199.1A
Other languages
German (de)
French (fr)
Other versions
EP2182109A2 (en
EP2182109A3 (en
Inventor
Petteri Vuorio
Veikko Seppälä
Olli Touvinen
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.)
Valmet Technologies Oy
Original Assignee
Valmet Technologies Oy
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 Valmet Technologies Oy filed Critical Valmet Technologies Oy
Publication of EP2182109A2 publication Critical patent/EP2182109A2/en
Publication of EP2182109A3 publication Critical patent/EP2182109A3/en
Application granted granted Critical
Publication of EP2182109B1 publication Critical patent/EP2182109B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21DTREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20Methods of refining
    • D21D1/30Disc mills
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21DTREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20Methods of refining
    • D21D1/30Disc mills
    • D21D1/303Double disc mills

Definitions

  • the invention relates to a method for adapting a pulp making process to line of production changes.
  • Refiners are used in a pulp making process to refine lignocellulose-containing material.
  • the refiners comprise a frame which houses a refiner chamber generally, depending on the refiner type, provided with one or more fixed refiner element, i.e. a stator or a stator element, arranged fixedly, i.e. non-rotatingly, in connection with the frame of the refiner, as well as one or more refiner element, i.e. a rotor, rotatable via a shaft.
  • WO 85/04431 A1 shows an apparatus for refining lignocellulose-containing material, the apparatus comprising a pressure-proof refiner housing with opposed refiner members, which between themselves define a gap. Liquid is supplied to the gap via radial passageways in a rotatable refiner member, and the rotation of the refiner member brings about the desired pressure in the liquid, which pressure exceeds the pressure in the gap.
  • US 3 893 631 A shows a high speed ground wood disc refiner having a pair of oppositely facing fixed refiner plates and twin rotating discs each carrying refining plates juxtaposed the fixed plates.
  • the rotating discs are axially adjusted on the drive shaft by a parallel piston-cylinder hydraulic system which insures that an equal and opposite thrust force is produced by each rotating head. Since the thrust forces are absorbed by the drive shaft, this arrangement permits the use of very light bearings on the drive shaft, resulting in economies of manufacture and maintenance.
  • the object of the present invention is achieved by a method for adapting a pulp making process to line of production changes according to claim 1, 2 or 3.
  • the method according to the invention comprises changing the structure of at least one disc refiner.
  • the refiner comprises a frame structure which comprises a pressure frame surrounding a refiner chamber and a base frame supporting the pressure frame.
  • the refiner further comprises at least one rotor rotatable via a shaft.
  • the method comprises changing the frame structure of the disc refiner at least over a section belonging to the pressure frame such that the refiner chamber of the refiner is arrangeable to comprise a rotor comprising a conical refining surface section and a stator comprising a conical refining surface section or such that two single disc refiners are combinable into one double disc refiner comprising two rotors.
  • the method comprises removing an end element being in connection with the frame structure of at least one disc refiner from the connection with the frame structure of the disc refiner, arranging in the rotor of the refiner a rotor element comprising a conical refining surface section, arranging in connection with the end element a stator comprising a conical refining surface section, arranging in the frame structure of the refiner, in connection with the pressure frame, an extension sleeve or an extension structure in order to increase extent of the refiner chamber in a direction of the shaft of the refiner, and fastening the end element in connection with the pressure frame of the refiner such that the extension sleeve or the extension structure remains located between the end element and the pressure frame of the refiner.
  • the extension sleeve or the extension structure enables the extent of the refiner chamber of the refiner to be increased in the direction of the shaft of the refiner in a simple manner such that a stator comprising a conical refining surface section and a rotor comprising a conical refining surface section may be arranged in the refiner chamber of the refiner.
  • the method comprises removing from a first disc refiner an end element and a stator arranged in connection therewith, thereby forming a first frame structure section of the refiner, removing from a second disc refiner an end element and a stator arranged in connection therewith, thereby forming a second frame structure section of the refiner, placing the rotors of the refiners towards one another such that a blade gap is provided between the rotors, and supporting the frame structure sections against one another by one or more support elements to be arranged in connection with said frame structure sections, thus forming a double disc refiner.
  • two partial refiner structures are provided which, when combined with one another, enable a double disc refiner comprising two rotors to be manufactured.
  • Figure 1 is a schematic cross-sectional side view showing a prior art disc refiner 1.
  • the disc refiner 1 comprises a frame structure 2 which comprises a pressure frame 3 and a base frame 4 of the refiner to support the pressure frame 3.
  • Figure 1 only shows part of the base frame 4.
  • the pressure frame 3 houses a refiner chamber 5 provided with a refiner element, i.e. a rotor 7, rotatable, i.e. rotating, via a shaft 6 as well as a fixed, i.e. non-rotating, refiner element, i.e. a stator 9, arranged in connection with an end element 8 of the refiner 1.
  • the end element 8 is fastened to the pressure frame 3, the end element 8 thus forming part of the pressure frame 3.
  • the rotor 7 is provided with a refining surface 10 of the rotor 7 while the stator 9 is provided with a refining surface 11 of the stator 9.
  • the stator 9 and the end element 8 are further provided with feed openings 12 through which fibrous material to be refined may be fed to a blade gap 13 located between the stator 9 and the rotor 7.
  • Figure 1 shows the blade gap 13 substantially larger than it really is.
  • the refiner naturally further comprises a discharge opening (not shown in the figure) for discharging already refined material from the refiner chamber.
  • the general structure and operational principle of refiners are known per se to those skilled in the art, so they do not have to be discussed in closer detail herein.
  • Figure 2 is a schematic cross-sectional side view showning a refiner 14.
  • the refiner 14 shown in Figure 2 is a disc cone refiner and it comprises a frame structure 2 which comprises a pressure frame 3 and a base frame 4 of the refiner to support the pressure frame 3.
  • Figure 2 only shows part of the base frame 4.
  • the pressure frame 3 houses a refiner chamber 5 which is provided with a rotor 7 rotatable via a shaft 6 as well as a stator 9 arranged in connection with an end element 8 of the refiner 14.
  • the stator 9 and the end element 8 comprise feed openings 12 through which fibrous material to be refined may be fed to a blade gap 13 located between the stator 9 and the rotor 7.
  • Figure 2 further shows an extension sleeve 15 or an extension structure 15 which is placed between the pressure frame 3 and the end element 8 of the refiner 1 and by means of which the extent of the refiner chamber has been increased in a direction of the shaft of the refiner 1.
  • the rotor 7 is formed from a first rotor element 7' and a second rotor element 7".
  • the second rotor element 7" is arranged in connection with the first rotor element 7' such that when the first rotor element 7' rotates, also the second rotor element 7" rotates.
  • the second rotor element 7" is provided with a refining surface 10 comprising both a conical refining surface section 10' and a disc-like refining surface section 10".
  • the stator 9 of the refiner 1 is further provided with a refining surface 11 which comprises both a conical refining surface section 11' and a disc-like refining surface section 11".
  • the refiner 14 according to Figure 2 is formed from a disc refiner 1 which is in use and which is similar to that shown in Figure 1 by removing the end element 8 from connection with the frame structure 2, i.e. the pressure frame 3, and at some stage by removing the stator 9 of the original disc refiner 1 from connection with the end element 8.
  • the second rotor element 7" of the rotor 7 which comprises a refining surface 10 and which is shown in Figure 2 is fastened in connection with the rotor of the original disc refiner 1, the rotor of the original disc refiner corresponding with the first rotor element 7' of the rotor 7 shown in Figure 2 .
  • the first rotor element 7' forms the frame of the rotor 7.
  • first rotor element 7' may be machined in order to fasten the second rotor element 7" in connection with the first rotor element 7'.
  • second rotor element 7" may also be supported in connection with the shaft 6 or a possible extension thereof.
  • the stator 9 intended for the refiner being manufactured is fastened in connection with the end element 8.
  • the extension sleeve 15 or the extension structure 15 is placed between the end element 8 and the pressure frame 3.
  • the extension sleeve 15 may be placed between the end element 8 and the pressure frame 3 while end assembling the refiner 14, in which case the end element 8, the extension sleeve 15 and the pressure frame 3 of the refiner 1 are at the same time fastened to one another by simultaneosly using the same fastening means, such as fastening bolts (for the sake of clarity not shown in the figures), thus closing the structure of the refiner 14.
  • the extension sleeve 15 may be situated between the end element 8 and the pressure frame 3 also earlier, in which case the extension sleeve 15 is fastened separately to the pressure frame 3 of the refiner 14.
  • the extension sleeve 15 is used for increasing the extent of the refiner chamber 5 of the refiner 14 in the direction of the shaft 6 of the refiner 1 since it would be impossible to accommodate the stator 9 and the rotor 7 comprising both a disc-like refining surface section 10", 11" and a conical refining surface section 10', 11' in the refiner chamber 5 provided in the original disc refiner.
  • an ordinary disc refiner may be modified into a refiner comprising both a disc-like refining surface section and a conical refining surface section, i.e. into a so-called disc cone refiner.
  • the old disc refiner may be utilized almost completely, the original disc-like stator being the only somewhat important redundant part, if not being used for forming a disc-like refining surface section 11" in the modernized refiner.
  • the extension sleeve 15 enables the extent of the refiner chamber 5 to be increased in the direction of the shaft 6 in a very simple manner.
  • the extension sleeve 15 forms an extension element structure within the area of the refiner chamber 5 in order to increase the extent of the refiner chamber 5 in the direction of the shaft 6 of the refiner.
  • the novel end element 8 instead of using in the refiner 14 an old end element 8, it is possible to form a novel end element 8 e.g. by casting, the novel end element 8 also comprising a section which corresponds with the extension sleeve 15 and which elongates a section corresponding with the frame structure, i.e. the pressure frame, of the refiner, and fasten this novel end element to the frame structure 2, i.e. the pressure frame 3, of the refiner 1, thus changing the frame structure of the original, used refiner within the area of the refiner chamber such that the extent of the refiner chamber increases in the direction of the shaft of the refiner.
  • the novel end element in addition to the end element, also comprises an extension element structure for increasing the extent of the refiner chamber in the direction of the shaft of the refiner.
  • the rotor 7 of the refiner 14 may also be implemented such that in addition to the old stator, also the old rotor is removed from the original disc refiner 1 from the shaft 6 of the refiner 1 and, in place thereof, a rotor 7 is installed which is formed from at least one rotor element and which comprises at least a conical refining surface 10' but possibly a disc-like refining surface 10" as well.
  • a corresponding stator comprising at least a conical refining surface 11' but possibly also a disc-like refining surface 11" to be installed in place of the original disc-like stator.
  • both the original stator and rotor may be replaced by a stator and rotor comprising conical refining surfaces only, in which case the old disc refiner may be changed into a cone refiner.
  • Figure 3 is a schematic cross-sectional side view showing a double disc refiner 16.
  • the refiner 16 according to Figure 3 is thus a double disc refiner or a DD refiner whose refiner chamber 5 is provided with two rotors 7 arranged towards one another such that a blade gap 13 is provided between the rotors 7. With respect to the rest of the structure of the refiner 16, Figure 3 shows the blade gap 13 substantially larger than it really is.
  • the refiner 16 further comprises two shafts 6 such that the rotors 7 may be rotated irrespective of one another.
  • the frame structure has two frame structure sections separate from one another: a first frame structure section 2' as seen in Figure 3 on the left side of the left-hand rotor 7, and a second frame structure section 2" on the right side of the right-hand rotor 7.
  • the frame structure sections 2' and 2" are combined with one another by one or more support elements 17, whereby the frame structure 2 of the refiner 16 according to Figure 3 comprises a first frame structure section 2', a second frame structure section 2" and one or more support elements 17 which are arranged at least partly, in their entirety as seen in Figure 3 , between the first frame structure section 2' and the second frame structure section 2", supporting the first frame structure section 2' and the second frame structure section 2" against one another and at the same time forming part of the pressure frame 3 surrounding the refiner chamber 5 of the refiner 16.
  • the support element 17 may also be an element similar to the extension sleeve 15 or the extension structure 15 shown in Figure 2 if the support element 17 is formed from one part only.
  • the refiner 16 shown in Figure 3 may be formed from two used disc refiners 1 shown in Figure 1 by removing the end elements of said disc refiners from connection with the frame structure of the refiner. Together with the end element, the stator provided in connection with the end element is removed from the refiners. Next, when necessary, some frame structure is removed by machining from at least one or both of the used refiners from the area of the refiner chamber from the pressure frame surrounding the rotor 7 such that said refiners may be installed with respect to one another such that the refining surfaces of the rotors 7 thereof come towards one another such that a blade gap 13 is provided between said refining surfaces.
  • the frame structures of said refiners that are still separate from one another, the frame stuctures in Figure 3 thus corresponding with the first frame structure section 2' and the second frame structure section 2", are combined with one another by means of one or more support elements 17 such that one refiner structure is formed wherein the frame structures of the originally separate disc refiners and one or more support elements 17 form a substantially closed refiner chamber.
  • the support elements 17 increase the extent of the refiner chamber in the direction of the shaft of the refiner such that the refiner unit formed from two rotors is more easily accommodated inside the refiner.
  • two used disc refiners may thus be changed into one double disc refiner provided with two rotors which rotate irrespectively of one another.
  • Such a change is easy to make only by removing the end elements and stators of the used disc refiners and, when necessary, by removing either from one disc refiner or from both disc refiners at least part of the frame structure surrounding the rotor as well as by combining with one another the remaining sections of the original refiners by suitable support elements.
  • only feed openings 12 have to be arranged through one of the rotors and through the frame structure section in connection with said rotor in order to feed material to be refined into the blade gap 13 located between the rotors 7.
  • the feed openings 12 are shown schematically in Figure 3 in the right-hand rotor 7 and in the second frame structure section 2".
  • the gap between a background surface of the rotor and the frame structure may be sealed by a mechanical seal such that the material fed to be refined may enter the refiner chamber only via the blade gap 13.
  • a discharge opening or channel (not shown in the figure) for refined material is also provided in connection with the refiner chamber of the refiner.
  • Figure 4 is a schematic cross-sectional side view showing another double disc refiner 18, and Figure 5 is a schematic end view showing a double disc refiner similar to that of Figure 4 .
  • the refiner shown in Figures 4 and 5 has a frame structure 2 which comprises, as the refiner according to Figure 3 , a first frame structure section 2' and a second frame structure section 2", a pressure frame 3 housing a refiner chamber 5, and a base frame 4 of the refiner to support the pressure frame.
  • Inside the refiner chamber 5 are two rotors 7, each being rotatable irrespective of one another via a corresponding shaft 6.
  • FIG. 4 further schematically shows a discharge opening 21 for discharging refined material from the refiner.
  • the structure of the refiner according to Figures 4 and 5 is similar to that of Figure 3 , differing, however, from the refiner according to Figure 3 in that the first frame structure section 2' and the second frame structure section 2" of the refiner 18 are supported against one another by a support element 20 connecting or fastening the base frame 4 of the first frame structure section 2' and the base frame 4 of the second frame structure section 2" to one another;
  • Figure 4 shows the support element 20 schematically in dotted line.
  • the pressure frame 3 resides between the first frame structure section 2' and the second frame structure section 2" but does not support the frame structure sections 2', 2" against one another.
  • the refiner chamber 5 is formed by a separate pressure frame 3 added during the change of the refiner and formed from an upper part 3' and a lower part 3".
  • the refiner 18 shown in Figures 4 and 5 may be formed from two used disc refiners 1 shown in Figure 1 by removing the end elements of said disc refiners from connection with the frame structure of the refiner. Along with the end element, a stator provided in connection with the end element is removed from the refiners. Next, at least part of the pressure frame 3 is also removed from both refiners from connection with the rest of the frame structure. The rotors and frame structures remaining from the refiners are arranged in connection with one another such that the refining surfaces of the rotors 7 come towards one another such that a blade gap 13 is provided between said refining surfaces.
  • a new pressure frame 3 is arranged around the rotors 7, the pressure frame 3 consisting of an upper part 3' and a lower part 3" and being received between a frame part corresponding with the first frame structure section 2' and remaining from one old disc refiner and a frame part corresponding with the second frame structure section 2" and remaining from the other old disc refiner.
  • the frame structure of the old disc refiners is thus changed over the section belonging to the pressure frame of the refiner such that at least part of the old pressure frame is removed from both refiners and said two pressure frames or sections removed therefrom are replaced at least partly by one new pressure frame.
  • the new pressure frame 3 does not support the first frame structure section 2' and the second frame structure section 2" against one another but one or more support elements 20 are arranged in connection with the first frame structure section 2' and the second frame structure section 2" to fasten the first frame structure section 2' and the second frame structure section 2" to one another and to support them against one another.
  • the support element 20 may be e.g. a disc-like structure, as shown in Figures 4 and 5 , which may be made e.g. of metal.
  • an old disc refiner may be changed e.g. into a disc cone refiner or two old disc refiners may be changed into a double disc refiner.
  • This enables the structural parts and the related actuators of old refiners to be utilized in an extensive manner when updating the refining processes, which lowers the costs caused by the changes. For example, by changing two old disc refiners into one double disc refiner a considerable amount of energy can be saved since double disc refiners consume typically about 10 to 30% less energy than disc refiners.
  • the quality of pulp produced by a double disc refiner is, however, usable for high-quality printing papers.
  • the features disclosed in this application may be used as such, irrespective of other features.
  • the features disclosed in this application may be combined in order to provide different combinations.
  • a disc cone refiner it may be necessary to machine the frame structure, i.e. in practice the pressure frame, of the original refiner inside the pressure frame within the area of the refiner chamber in order to enable the conical refining surface section of the stator to be installed in an easy manner concentrically with respect to the conical refining surface section of the rotor.
  • the concentricity of the rotors does not set equally high requirements.
  • the machining may be carried out such that the refiner chamber is at the same time carved out not only in a direction of the shaft but also in a direction of a radius, whereby the length and diameter of a refiner blade solution to be arranged in the refiner chamber may be larger.
  • the machining of the frame structure of the refiner within the area of the refiner chamber may also be carried out because it enables refiner blades to be replaced or replacement of the refiner blades to be made easier to implement, which constitutes grounds for machining the frame structure of the refiner when applying the solution of the invention to the case of the double disc refiner in particular.

Landscapes

  • Paper (AREA)

Description

  • The invention relates to a method for adapting a pulp making process to line of production changes.
  • Refiners are used in a pulp making process to refine lignocellulose-containing material. The refiners comprise a frame which houses a refiner chamber generally, depending on the refiner type, provided with one or more fixed refiner element, i.e. a stator or a stator element, arranged fixedly, i.e. non-rotatingly, in connection with the frame of the refiner, as well as one or more refiner element, i.e. a rotor, rotatable via a shaft.
  • As manufacturing processes change, e.g. when production volumes change, a refiner being used may become redundant. Since particularly the frame structures of refiners last for decades, it may cause significant economic losses to purchase an entirely new refiner and remove the redundant one. These losses could be reduced by utilizing some parts of the old refiner. However, particularly in situations wherein the line of production changes regarding either the raw material to be used or the quality of pulp to be produced, it is extremely difficult to even to some extent utilize the old refiner.
  • WO 85/04431 A1 shows an apparatus for refining lignocellulose-containing material, the apparatus comprising a pressure-proof refiner housing with opposed refiner members, which between themselves define a gap. Liquid is supplied to the gap via radial passageways in a rotatable refiner member, and the rotation of the refiner member brings about the desired pressure in the liquid, which pressure exceeds the pressure in the gap.
  • US 3 893 631 A shows a high speed ground wood disc refiner having a pair of oppositely facing fixed refiner plates and twin rotating discs each carrying refining plates juxtaposed the fixed plates. The rotating discs are axially adjusted on the drive shaft by a parallel piston-cylinder hydraulic system which insures that an equal and opposite thrust force is produced by each rotating head. Since the thrust forces are absorbed by the drive shaft, this arrangement permits the use of very light bearings on the drive shaft, resulting in economies of manufacture and maintenance.
  • Summary of the Invention
  • It is the object of the present invention to provide a new, simple and cost-efficient method for adapting a pulp making process to line of production changes in which existing refiners can be used.
  • The object of the present invention is achieved by a method for adapting a pulp making process to line of production changes according to claim 1, 2 or 3.
  • Further advantageous developments of the present invention are defined in the dependent claims.
  • The method according to the invention comprises changing the structure of at least one disc refiner. The refiner comprises a frame structure which comprises a pressure frame surrounding a refiner chamber and a base frame supporting the pressure frame. The refiner further comprises at least one rotor rotatable via a shaft. The method comprises changing the frame structure of the disc refiner at least over a section belonging to the pressure frame such that the refiner chamber of the refiner is arrangeable to comprise a rotor comprising a conical refining surface section and a stator comprising a conical refining surface section or such that two single disc refiners are combinable into one double disc refiner comprising two rotors.
  • The process of changing an old disc refiner to be removed from use into a refiner of another type enables a vast majority of the structure of the refiner to be removed from use and actuators associated therewith to be used when manufacturing a new refiner. On account of such utilization of parts, it is also rather an inexpensive procedure to change an old refiner into a refiner of another type. In addition, the energy consumption per mass ton of a refiner produced by such a changing procedure is clearly lower than the energy consumption of the disc refiner being changed.
  • According to the invention, the method comprises removing an end element being in connection with the frame structure of at least one disc refiner from the connection with the frame structure of the disc refiner, arranging in the rotor of the refiner a rotor element comprising a conical refining surface section, arranging in connection with the end element a stator comprising a conical refining surface section, arranging in the frame structure of the refiner, in connection with the pressure frame, an extension sleeve or an extension structure in order to increase extent of the refiner chamber in a direction of the shaft of the refiner, and fastening the end element in connection with the pressure frame of the refiner such that the extension sleeve or the extension structure remains located between the end element and the pressure frame of the refiner.
  • The extension sleeve or the extension structure enables the extent of the refiner chamber of the refiner to be increased in the direction of the shaft of the refiner in a simple manner such that a stator comprising a conical refining surface section and a rotor comprising a conical refining surface section may be arranged in the refiner chamber of the refiner.
  • According to the invention, the method comprises removing from a first disc refiner an end element and a stator arranged in connection therewith, thereby forming a first frame structure section of the refiner, removing from a second disc refiner an end element and a stator arranged in connection therewith, thereby forming a second frame structure section of the refiner, placing the rotors of the refiners towards one another such that a blade gap is provided between the rotors, and supporting the frame structure sections against one another by one or more support elements to be arranged in connection with said frame structure sections, thus forming a double disc refiner.
  • By removing from two disc refiners to be removed from use the end element and the stators arranged in connection therewith, two partial refiner structures are provided which, when combined with one another, enable a double disc refiner comprising two rotors to be manufactured.
  • BRIEF DESCRIPTION OF THE FIGURES
  • Some embodiments of the invention are described in closer detail in the accompanying drawings, in which
    • Figure 1 is a schematic cross-sectional side view showing a prior art refiner,
    • Figure 2 is a schematic cross-sectional side view showning a disc cone refiner according to the invention,
    • Figure 3 is a schematic cross-sectional side view showing a double disc refiner according to the invention,
    • Figure 4 is a schematic cross-sectional side view showing another double disc refiner according to the invention, and
    • Figure 5 is a schematic end view showing a double disc refiner similar to that of Figure 4.
  • For the sake of clarity, the figures show some embodiments of the invention in a simplified manner. In the figures, like reference numbers identify like elements.
  • DETAILED DESCRIPTION OF THE INVENTION
  • Figure 1 is a schematic cross-sectional side view showing a prior art disc refiner 1. The disc refiner 1 comprises a frame structure 2 which comprises a pressure frame 3 and a base frame 4 of the refiner to support the pressure frame 3. Figure 1 only shows part of the base frame 4. The pressure frame 3 houses a refiner chamber 5 provided with a refiner element, i.e. a rotor 7, rotatable, i.e. rotating, via a shaft 6 as well as a fixed, i.e. non-rotating, refiner element, i.e. a stator 9, arranged in connection with an end element 8 of the refiner 1. The end element 8 is fastened to the pressure frame 3, the end element 8 thus forming part of the pressure frame 3. The rotor 7 is provided with a refining surface 10 of the rotor 7 while the stator 9 is provided with a refining surface 11 of the stator 9. The stator 9 and the end element 8 are further provided with feed openings 12 through which fibrous material to be refined may be fed to a blade gap 13 located between the stator 9 and the rotor 7. With respect to the rest of the structure of the refiner 1, Figure 1 shows the blade gap 13 substantially larger than it really is. The refiner naturally further comprises a discharge opening (not shown in the figure) for discharging already refined material from the refiner chamber. Further, the general structure and operational principle of refiners are known per se to those skilled in the art, so they do not have to be discussed in closer detail herein.
  • Figure 2 is a schematic cross-sectional side view showning a refiner 14. The refiner 14 shown in Figure 2 is a disc cone refiner and it comprises a frame structure 2 which comprises a pressure frame 3 and a base frame 4 of the refiner to support the pressure frame 3. Figure 2 only shows part of the base frame 4. The pressure frame 3 houses a refiner chamber 5 which is provided with a rotor 7 rotatable via a shaft 6 as well as a stator 9 arranged in connection with an end element 8 of the refiner 14. The stator 9 and the end element 8 comprise feed openings 12 through which fibrous material to be refined may be fed to a blade gap 13 located between the stator 9 and the rotor 7. Figure 2 further shows an extension sleeve 15 or an extension structure 15 which is placed between the pressure frame 3 and the end element 8 of the refiner 1 and by means of which the extent of the refiner chamber has been increased in a direction of the shaft of the refiner 1.
  • In the refiner 14 according to Figure 2, the rotor 7 is formed from a first rotor element 7' and a second rotor element 7". The second rotor element 7" is arranged in connection with the first rotor element 7' such that when the first rotor element 7' rotates, also the second rotor element 7" rotates. The second rotor element 7" is provided with a refining surface 10 comprising both a conical refining surface section 10' and a disc-like refining surface section 10". The stator 9 of the refiner 1 is further provided with a refining surface 11 which comprises both a conical refining surface section 11' and a disc-like refining surface section 11".
  • The refiner 14 according to Figure 2 is formed from a disc refiner 1 which is in use and which is similar to that shown in Figure 1 by removing the end element 8 from connection with the frame structure 2, i.e. the pressure frame 3, and at some stage by removing the stator 9 of the original disc refiner 1 from connection with the end element 8. Next, the second rotor element 7" of the rotor 7 which comprises a refining surface 10 and which is shown in Figure 2 is fastened in connection with the rotor of the original disc refiner 1, the rotor of the original disc refiner corresponding with the first rotor element 7' of the rotor 7 shown in Figure 2. In such a case, it may also be considered that the first rotor element 7' forms the frame of the rotor 7. When necessary, the first rotor element 7' may be machined in order to fasten the second rotor element 7" in connection with the first rotor element 7'. In addition, in the manner shown in Figure 2, the second rotor element 7" may also be supported in connection with the shaft 6 or a possible extension thereof.
  • At some stage, the stator 9 intended for the refiner being manufactured is fastened in connection with the end element 8. At some stage, the extension sleeve 15 or the extension structure 15 is placed between the end element 8 and the pressure frame 3. The extension sleeve 15 may be placed between the end element 8 and the pressure frame 3 while end assembling the refiner 14, in which case the end element 8, the extension sleeve 15 and the pressure frame 3 of the refiner 1 are at the same time fastened to one another by simultaneosly using the same fastening means, such as fastening bolts (for the sake of clarity not shown in the figures), thus closing the structure of the refiner 14. The extension sleeve 15 may be situated between the end element 8 and the pressure frame 3 also earlier, in which case the extension sleeve 15 is fastened separately to the pressure frame 3 of the refiner 14. The extension sleeve 15 is used for increasing the extent of the refiner chamber 5 of the refiner 14 in the direction of the shaft 6 of the refiner 1 since it would be impossible to accommodate the stator 9 and the rotor 7 comprising both a disc-like refining surface section 10", 11" and a conical refining surface section 10', 11' in the refiner chamber 5 provided in the original disc refiner.
  • In the above-disclosed manner, an ordinary disc refiner may be modified into a refiner comprising both a disc-like refining surface section and a conical refining surface section, i.e. into a so-called disc cone refiner. When modernizing a refiner, the old disc refiner may be utilized almost completely, the original disc-like stator being the only somewhat important redundant part, if not being used for forming a disc-like refining surface section 11" in the modernized refiner. The extension sleeve 15 enables the extent of the refiner chamber 5 to be increased in the direction of the shaft 6 in a very simple manner. In the embodiment according to Figure 2, the extension sleeve 15 forms an extension element structure within the area of the refiner chamber 5 in order to increase the extent of the refiner chamber 5 in the direction of the shaft 6 of the refiner.
  • Instead of using in the refiner 14 an old end element 8, it is possible to form a novel end element 8 e.g. by casting, the novel end element 8 also comprising a section which corresponds with the extension sleeve 15 and which elongates a section corresponding with the frame structure, i.e. the pressure frame, of the refiner, and fasten this novel end element to the frame structure 2, i.e. the pressure frame 3, of the refiner 1, thus changing the frame structure of the original, used refiner within the area of the refiner chamber such that the extent of the refiner chamber increases in the direction of the shaft of the refiner. In such a case, in addition to the end element, the novel end element also comprises an extension element structure for increasing the extent of the refiner chamber in the direction of the shaft of the refiner.
  • The rotor 7 of the refiner 14 may also be implemented such that in addition to the old stator, also the old rotor is removed from the original disc refiner 1 from the shaft 6 of the refiner 1 and, in place thereof, a rotor 7 is installed which is formed from at least one rotor element and which comprises at least a conical refining surface 10' but possibly a disc-like refining surface 10" as well. This also enables a corresponding stator comprising at least a conical refining surface 11' but possibly also a disc-like refining surface 11" to be installed in place of the original disc-like stator. In a similar manner, both the original stator and rotor may be replaced by a stator and rotor comprising conical refining surfaces only, in which case the old disc refiner may be changed into a cone refiner.
  • Figure 3 is a schematic cross-sectional side view showing a double disc refiner 16. The refiner 16 according to Figure 3 is thus a double disc refiner or a DD refiner whose refiner chamber 5 is provided with two rotors 7 arranged towards one another such that a blade gap 13 is provided between the rotors 7. With respect to the rest of the structure of the refiner 16, Figure 3 shows the blade gap 13 substantially larger than it really is. The refiner 16 further comprises two shafts 6 such that the rotors 7 may be rotated irrespective of one another. In the refiner 16, the frame structure has two frame structure sections separate from one another: a first frame structure section 2' as seen in Figure 3 on the left side of the left-hand rotor 7, and a second frame structure section 2" on the right side of the right-hand rotor 7. The frame structure sections 2' and 2" are combined with one another by one or more support elements 17, whereby the frame structure 2 of the refiner 16 according to Figure 3 comprises a first frame structure section 2', a second frame structure section 2" and one or more support elements 17 which are arranged at least partly, in their entirety as seen in Figure 3, between the first frame structure section 2' and the second frame structure section 2", supporting the first frame structure section 2' and the second frame structure section 2" against one another and at the same time forming part of the pressure frame 3 surrounding the refiner chamber 5 of the refiner 16. The support element 17 may also be an element similar to the extension sleeve 15 or the extension structure 15 shown in Figure 2 if the support element 17 is formed from one part only.
  • The refiner 16 shown in Figure 3 may be formed from two used disc refiners 1 shown in Figure 1 by removing the end elements of said disc refiners from connection with the frame structure of the refiner. Together with the end element, the stator provided in connection with the end element is removed from the refiners. Next, when necessary, some frame structure is removed by machining from at least one or both of the used refiners from the area of the refiner chamber from the pressure frame surrounding the rotor 7 such that said refiners may be installed with respect to one another such that the refining surfaces of the rotors 7 thereof come towards one another such that a blade gap 13 is provided between said refining surfaces. Next, the frame structures of said refiners that are still separate from one another, the frame stuctures in Figure 3 thus corresponding with the first frame structure section 2' and the second frame structure section 2", are combined with one another by means of one or more support elements 17 such that one refiner structure is formed wherein the frame structures of the originally separate disc refiners and one or more support elements 17 form a substantially closed refiner chamber. The support elements 17 increase the extent of the refiner chamber in the direction of the shaft of the refiner such that the refiner unit formed from two rotors is more easily accommodated inside the refiner.
  • In the solution shown in Figure 3, two used disc refiners may thus be changed into one double disc refiner provided with two rotors which rotate irrespectively of one another. Such a change is easy to make only by removing the end elements and stators of the used disc refiners and, when necessary, by removing either from one disc refiner or from both disc refiners at least part of the frame structure surrounding the rotor as well as by combining with one another the remaining sections of the original refiners by suitable support elements. In addition to this, only feed openings 12 have to be arranged through one of the rotors and through the frame structure section in connection with said rotor in order to feed material to be refined into the blade gap 13 located between the rotors 7. The feed openings 12 are shown schematically in Figure 3 in the right-hand rotor 7 and in the second frame structure section 2". The gap between a background surface of the rotor and the frame structure may be sealed by a mechanical seal such that the material fed to be refined may enter the refiner chamber only via the blade gap 13. Naturally, a discharge opening or channel (not shown in the figure) for refined material is also provided in connection with the refiner chamber of the refiner.
  • Figure 4 is a schematic cross-sectional side view showing another double disc refiner 18, and Figure 5 is a schematic end view showing a double disc refiner similar to that of Figure 4. The refiner shown in Figures 4 and 5 has a frame structure 2 which comprises, as the refiner according to Figure 3, a first frame structure section 2' and a second frame structure section 2", a pressure frame 3 housing a refiner chamber 5, and a base frame 4 of the refiner to support the pressure frame. Inside the refiner chamber 5 are two rotors 7, each being rotatable irrespective of one another via a corresponding shaft 6. Between the rotors 7 a blade gap 13 is provided whereto the fibrous material to be refined is fed via feed openings 12 arranged in the right-hand rotor 7 as seen in Figure 4 as well as via a feed channel 19. The feed channel 19 may be provided with a screw conveyor for making the feed of the material to be refined more efficient. Figure 4 further schematically shows a discharge opening 21 for discharging refined material from the refiner.
  • The structure of the refiner according to Figures 4 and 5 is similar to that of Figure 3, differing, however, from the refiner according to Figure 3 in that the first frame structure section 2' and the second frame structure section 2" of the refiner 18 are supported against one another by a support element 20 connecting or fastening the base frame 4 of the first frame structure section 2' and the base frame 4 of the second frame structure section 2" to one another; Figure 4 shows the support element 20 schematically in dotted line. The pressure frame 3 resides between the first frame structure section 2' and the second frame structure section 2" but does not support the frame structure sections 2', 2" against one another. In addition, the refiner chamber 5 is formed by a separate pressure frame 3 added during the change of the refiner and formed from an upper part 3' and a lower part 3".
  • The refiner 18 shown in Figures 4 and 5 may be formed from two used disc refiners 1 shown in Figure 1 by removing the end elements of said disc refiners from connection with the frame structure of the refiner. Along with the end element, a stator provided in connection with the end element is removed from the refiners. Next, at least part of the pressure frame 3 is also removed from both refiners from connection with the rest of the frame structure. The rotors and frame structures remaining from the refiners are arranged
    in connection with one another such that the refining surfaces of the rotors 7 come towards one another such that a blade gap 13 is provided between said refining surfaces. A new pressure frame 3 is arranged around the rotors 7, the pressure frame 3 consisting of an upper part 3' and a lower part 3" and being received between a frame part corresponding with the first frame structure section 2' and remaining from one old disc refiner and a frame part corresponding with the second frame structure section 2" and remaining from the other old disc refiner. In this case, the frame structure of the old disc refiners is thus changed over the section belonging to the pressure frame of the refiner such that at least part of the old pressure frame is removed from both refiners and said two pressure frames or sections removed therefrom are replaced at least partly by one new pressure frame. However, the new pressure frame 3 does not support the first frame structure section 2' and the second frame structure section 2" against one another but one or more support elements 20 are arranged in connection with the first frame structure section 2' and the second frame structure section 2" to fasten the first frame structure section 2' and the second frame structure section 2" to one another and to support them against one another. The support element 20 may be e.g. a disc-like structure, as shown in Figures 4 and 5, which may be made e.g. of metal.
  • In the disclosed manners, an old disc refiner may be changed e.g. into a disc cone refiner or two old disc refiners may be changed into a double disc refiner. This enables the structural parts and the related actuators of old refiners to be utilized in an extensive manner when updating the refining processes, which lowers the costs caused by the changes. For example, by changing two old disc refiners into one double disc refiner a considerable amount of energy can be saved since double disc refiners consume typically about 10 to 30% less energy than disc refiners. In addition, the quality of pulp produced by a double disc refiner is, however, usable for high-quality printing papers.
  • In some cases, the features disclosed in this application may be used as such, irrespective of other features. On the other hand, when necessary, the features disclosed in this application may be combined in order to provide different combinations.
  • The drawings and the related description are only intended to illustrate embodiments of the invention, i.e. the details of the invention may vary within the scope of the invention as defined by the appended claims.
  • In the implementation of a disc cone refiner, it may be necessary to machine the frame structure, i.e. in practice the pressure frame, of the original refiner inside the pressure frame within the area of the refiner chamber in order to enable the conical refining surface section of the stator to be installed in an easy manner concentrically with respect to the conical refining surface section of the rotor. In the case of a double disc refiner, the concentricity of the rotors does not set equally high requirements. The machining may be carried out such that the refiner chamber is at the same time carved out not only in a direction of the shaft but also in a direction of a radius, whereby the length and diameter of a refiner blade solution to be arranged in the refiner chamber may be larger. The machining of the frame structure of the refiner within the area of the refiner chamber may also be carried out because it enables refiner blades to be replaced or replacement of the refiner blades to be made easier to implement, which constitutes grounds for machining the frame structure of the refiner when applying the solution of the invention to the case of the double disc refiner in particular.

Claims (3)

  1. A method fod modifying a disc refiner into a disc cone refiner the method comprises the steps of:
    - changing a structure of at least one disc refiner (1) into a structure of a disc cone refiner (14), each of which refiners (1, 14) comprises a frame structure (2), the frame structure (2) comprising a pressure frame (3) surrounding a refiner chamber (5) and a base frame (4) supporting the pressure frame (3), and each of which refiners (1, 14) further comprises at least one rotor (7) rotatable via a shaft (6),
    - changing the frame structure (2) of the disc refiner (1) at least over a section belonging to the pressure frame (3) such that the refiner chamber (5) of the disc cone refiner (14) is configured to comprise a rotor (7) comprising a conical refining surface section (10'),
    - removing an end element (8) being in connection with the frame structure (2) of the disc refiner (1) from the connection with the frame structure (2) of the disc refiner (1),
    - arranging in the rotor (7) of the disc cone refiner (14) a rotor element (7") comprising a conical refining surface section (10'),
    - arranging in connection with the end element (8) a stator (9) comprising a conical refining surface section (11'),
    - arranging in the frame structure (2) of the disc cone refiner (14), in connection with the pressure frame (3), an extension sleeve (15) or an extension structure (15) in order to increase extent of the refiner chamber (5) in a direction of the shaft (6) of the disc cone refiner (1), and
    - fastening the end element (8) in connection with the pressure frame (3) of the disc cone refiner (14) such that the extension sleeve (15) or the extension structure (15) remains located between the end element (8) and the pressure frame (3) of the disc cone refiner (14).
  2. A method for modifying at least one disc refiner into a double disc refiner, the method comprises the steps of:
    - changing a structure of at least one disc refiner (1) into a structure of a double disc refiner (16, 18), each of which refiners (1, 16, 18) comprises a frame structure (2), the frame structure (2) comprising a pressure frame (3) surrounding a refiner chamber (5) and a base frame (4) supporting the pressure frame (3), and the refiner (1, 16, 18) further comprising at least one rotor (7) rotatable via a shaft (6),
    - changing the frame structure (2) of the disc refiner (1) at least over a section belonging to the pressure frame (3) such that two single disc refiners (1) are combinable into one double disc refiner (16, 18) comprising two rotors (7),
    - removing from a first disc refiner (1) an end element (8) being in connection with the frame structure (2) and a stator (9) arranged in connection therewith, thereby forming a first frame structure section (2') of the double disc refiner (16, 18),
    - removing from a second disc refiner (1) an end element (8) being in connection with the frame structure (2) and a stator (9) arranged in connection therewith, thereby forming a second frame structure section (2") of the double disc refiner (16, 18), removing from the first and/or the second disc refiner (1) at least part of the pressure frame (3) of the frame structure (2) of the disc refiner (1)
    - placing the rotors (7) of the disc refiners (1) towards one another such that a blade gap (13) is provided between the rotors (7) in the structure of the double disc refiner (16, 18), and
    - supporting the frame structure sections (2', 2") against one another by one or more support elements (17, 20) to be arranged in connection with said frame structure sections, thus forming the double disc refiner (16, 18).
  3. A method as claimed in claim 1, characterized in that the rotor element (7") further comprises a disc-like (10") refining surface section, and in that the stator (9) further comprises a disc-like (11") refining surface section.
EP09174199.1A 2008-10-31 2009-10-27 Method of manufacturing a refiner Not-in-force EP2182109B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FI20086034A FI121544B (en) 2008-10-31 2008-10-31 A method of making a refiner and a refiner

Publications (3)

Publication Number Publication Date
EP2182109A2 EP2182109A2 (en) 2010-05-05
EP2182109A3 EP2182109A3 (en) 2014-08-13
EP2182109B1 true EP2182109B1 (en) 2016-11-30

Family

ID=39924671

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09174199.1A Not-in-force EP2182109B1 (en) 2008-10-31 2009-10-27 Method of manufacturing a refiner

Country Status (3)

Country Link
EP (1) EP2182109B1 (en)
CA (1) CA2684191C (en)
FI (1) FI121544B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016120407B4 (en) * 2016-10-26 2018-10-04 Institut Für Holztechnologie Dresden Gemeinnützige Gmbh Housing arrangement for a refiner

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893631A (en) * 1974-07-17 1975-07-08 Sprout Waldron & Co Inc Twin refiner with double floating discs
SE8401845D0 (en) * 1984-04-03 1984-04-03 Sunds Defibrator SET AND DEVICE FOR REFINING LIGNOCELULOSALLY MATERIAL

Also Published As

Publication number Publication date
FI121544B (en) 2010-12-31
FI20086034A0 (en) 2008-10-31
FI20086034A (en) 2010-05-01
CA2684191A1 (en) 2010-04-30
EP2182109A2 (en) 2010-05-05
CA2684191C (en) 2016-11-22
EP2182109A3 (en) 2014-08-13

Similar Documents

Publication Publication Date Title
EP1157160B1 (en) Tangential discharge disk refiner
EP0566570B1 (en) Controlled intensity high speed double disc refiner
CA2639890C (en) Multi-zone paper fiber refiner
US7694902B2 (en) Self-aligning and actively compensating refiner stator plate system
EP3212842B1 (en) Blade element for refiner
CA1246374A (en) Two stage high consistency refiner
EP2182109B1 (en) Method of manufacturing a refiner
EP2960367B1 (en) Single-disc refiner
CA3128925A1 (en) Refiner plate segment
US5398877A (en) Multi-disc refiner with free floating plate mechanism
CN101507935B (en) Beater disintegrating machine
NO811328L (en) PROCEDURE AND APPARATUS FOR CONTROL OF REFINE MASS.
CN101463574B (en) Double-cutting feed disc pulping machine
FI122363B (en) A method of making a refiner and a refiner
US7451946B2 (en) Refining element
CN105780575B (en) A kind of flat taper grinding disc of high consistency refining machine structure
EP4050154A1 (en) Disc refiner sliding head adjustment assembly
FI120630B (en) A method for installing or replacing a refiner sharpener
FI89514B (en) Foerfarande Foer att saenka energifoerbrukningen vid raffinering av fibermaterial
Ушаков et al. EQUIPMENT FOR KNIFE BEATING OF FIBRE HIGH CONCENTRATION SEMI-PRODUCTS
CN118076779A (en) Abrasive sheet for refiner
CA3177258A1 (en) Blade element for refiner
WO2013066239A1 (en) Method and arrangement for adjustable play in a rotating machine

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

AK Designated contracting states

Kind code of ref document: A2

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

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

Owner name: VALMET TECHNOLOGIES, INC.

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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 MK MT NL NO PL PT RO SE SI SK SM TR

RIC1 Information provided on ipc code assigned before grant

Ipc: D21D 1/30 20060101AFI20140710BHEP

17P Request for examination filed

Effective date: 20150211

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 MK MT NL NO PL PT RO SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160620

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 849914

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161215

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: 602009042739

Country of ref document: DE

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

Ref country code: LV

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

Effective date: 20161130

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20161130

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: 20161130

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: 20161130

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: 20170301

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: 20170228

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

Ref country code: PL

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: 20161130

Ref country code: ES

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

Effective date: 20161130

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: 20170330

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: 20161130

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: 20161130

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: 20161130

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: 20161130

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: 20161130

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: 20161130

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: 20161130

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: 20161130

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

Ref country code: SM

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

Effective date: 20161130

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: 20170228

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: 20161130

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: 20161130

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602009042739

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

26N No opposition filed

Effective date: 20170831

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: 20161130

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

Ref country code: MC

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

Effective date: 20161130

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Effective date: 20171027

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180629

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

Ref country code: GB

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

Effective date: 20171027

Ref country code: LI

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

Effective date: 20171031

Ref country code: LU

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

Effective date: 20171027

Ref country code: CH

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

Effective date: 20171031

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

Ref country code: FR

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

Effective date: 20171031

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 NON-PAYMENT OF DUE FEES

Effective date: 20171027

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

Ref country code: IE

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

Effective date: 20171027

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

Ref country code: HU

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

Effective date: 20091027

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

Ref country code: CY

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

Effective date: 20161130

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

Ref country code: MK

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

Effective date: 20161130

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: 20161130

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

Ref country code: IS

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

Effective date: 20170330

REG Reference to a national code

Ref country code: AT

Ref legal event code: UEP

Ref document number: 849914

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161130

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

Ref country code: DE

Payment date: 20211020

Year of fee payment: 13

Ref country code: AT

Payment date: 20211021

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602009042739

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 849914

Country of ref document: AT

Kind code of ref document: T

Effective date: 20221027

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 NON-PAYMENT OF DUE FEES

Effective date: 20230503

Ref country code: AT

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

Effective date: 20221027