EP1362679B1 - Chipping machine - Google Patents

Chipping machine Download PDF

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Publication number
EP1362679B1
EP1362679B1 EP03010331A EP03010331A EP1362679B1 EP 1362679 B1 EP1362679 B1 EP 1362679B1 EP 03010331 A EP03010331 A EP 03010331A EP 03010331 A EP03010331 A EP 03010331A EP 1362679 B1 EP1362679 B1 EP 1362679B1
Authority
EP
European Patent Office
Prior art keywords
rotor
chipper
chipper according
mating
cutter arrangement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP03010331A
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German (de)
French (fr)
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EP1362679A3 (en
EP1362679A2 (en
Inventor
Miroslav Prochazka
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PROCHAZKA, MIROSLAV
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Individual
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Publication of EP1362679A3 publication Critical patent/EP1362679A3/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B27WORKING OR PRESERVING WOOD OR SIMILAR MATERIAL; NAILING OR STAPLING MACHINES IN GENERAL
    • B27BSAWS FOR WOOD OR SIMILAR MATERIAL; COMPONENTS OR ACCESSORIES THEREFOR
    • B27B33/00Sawing tools for saw mills, sawing machines, or sawing devices
    • B27B33/20Edge trimming saw blades or tools combined with means to disintegrate waste
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B02CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
    • B02CCRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
    • B02C18/00Disintegrating by knives or other cutting or tearing members which chop material into fragments
    • B02C18/06Disintegrating by knives or other cutting or tearing members which chop material into fragments with rotating knives
    • B02C18/16Details
    • B02C18/18Knives; Mountings thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B27WORKING OR PRESERVING WOOD OR SIMILAR MATERIAL; NAILING OR STAPLING MACHINES IN GENERAL
    • B27LREMOVING BARK OR VESTIGES OF BRANCHES; SPLITTING WOOD; MANUFACTURE OF VENEER, WOODEN STICKS, WOOD SHAVINGS, WOOD FIBRES OR WOOD POWDER
    • B27L11/00Manufacture of wood shavings, chips, powder, or the like; Tools therefor
    • B27L11/005Tools therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B27WORKING OR PRESERVING WOOD OR SIMILAR MATERIAL; NAILING OR STAPLING MACHINES IN GENERAL
    • B27LREMOVING BARK OR VESTIGES OF BRANCHES; SPLITTING WOOD; MANUFACTURE OF VENEER, WOODEN STICKS, WOOD SHAVINGS, WOOD FIBRES OR WOOD POWDER
    • B27L11/00Manufacture of wood shavings, chips, powder, or the like; Tools therefor
    • B27L11/02Manufacture of wood shavings, chips, powder, or the like; Tools therefor of wood shavings or the like

Definitions

  • the invention relates to a chopping machine according to the preamble of patent claim 1.
  • Such a chipper is known for example from the US 4776375 A and from the DE 41 26 910 C1 .
  • the knife edges describe an approximately circular cylindrical rotor surface.
  • the knife edges are strongly inclined to the axis-parallel generatrices and the planes of the blades are tilted relative to the rotor axis.
  • a chipper with a conical rotor and obliquely to the rotor axis extending feed direction is from the US 3,375,859 known.
  • a chopping machine whose rotor consists of a circular cylindrical drum and a plurality of Messerblökken mounted on this.
  • the knife blocks are offset from each other in the axial direction and in the circumferential direction and each have a central and two lateral cutting, the lateral cutting having a smaller distance from the drum than the central cutting edge.
  • the fixed counter knife contains, in accordance with the axial offset of the knife blocks in the axial direction, a plurality of radially alternately stepped knife sections.
  • the rotor is designed as a disc with a plurality of substantially radial cutting, in front of which a counter knife blade is fixedly arranged.
  • a feeder includes a tube which is inclined at an angle to the plane of the rotor disc and tapers downwardly in a V-shape.
  • the US 3,319,673 shows a chipper with wound on a circular cylindrical rotor knife edges.
  • the rotor can also be subdivided into several identical sub-rotors.
  • a plurality of disks with blades of small axial extent are assembled to form an axially wider rotor package.
  • the present invention has for its object to provide an advantageous such chopping machine with improved smoothness of the rotor.
  • the surface described as a rotor casing of the cutting edges of the blade assembly rotating about the rotor axis is preferably mirror-symmetrical with respect to a median plane lying in the axial direction in the middle between the two end positions.
  • the radius of the rotor shell varies from the maximum radius monotonously, in particular continuously to the end radii.
  • the rotor shell may have a substantially biconical shape.
  • the counter blade arrangement follows with its counter edges at a small distance from the contour of the rotor shell.
  • the counter knife arrangement on which the wood chips are supported, advantageously forms with several counter knife strips an upwardly widening receptacle, in which the typically elongated wood chips rests self-centering under the action of gravity.
  • the acceptance angle is upwards perpendicular to the feed direction of the wood chips advantageously between 135 ° and 170 °. Due to the large acceptance angle, the vertical distance to the counter-blades in the center, where the counter-blades converge towards one another, is advantageously low, even in the case of wood chips with a large diameter.
  • the counter-knife arrangement forms an opposite to the direction of rotation of the rotor expanding receptacle for the wood chips, so that this pressed during the chopping process under the action of the forces exerted by the knife assembly forces towards the center of Aufname and thus centered by the hacking process itself in the counter-blade arrangement and is stabilized in position.
  • the measure of the radii of the rotor shell which reduce towards the axial end positions on the one hand and the receptacle that widens counter to the direction of rotation of the rotor can be implemented independently of one another or even combined.
  • the individual opposing edges of the counter knife strips are preferably straight.
  • the counter knife arrangement can have exactly two counter knife strips. These are then preferably inclined against the tangential direction of the rotor shell in the counter blade arrangement by a deviating from 90 ° edge inclination angle.
  • the cutting edges of the knife assembly are preferably straight.
  • the cutting edges can advantageously be inclined against the tangential direction of the rotor shell at the respective knife edge by 90 ° different cutting angle of inclination.
  • the orientation of the knife blades with respect to the tangential direction is advantageously different from the orientation of the cutting edges with respect to the tangential direction, so that cutting edges and counter edges are moved past each other with the inclusion of a shear angle.
  • the inclination of cutting edges and associated mating edges may be mirror symmetric with respect to a plane containing the rotor axis.
  • the shearing action is particularly advantageous in hard inclusions in wood chips, for example, metal pieces (nails) in demolition wood, which shows that the formation of such a shear angle, the cutting edges of the blades are less stressed.
  • the average course and the tangential direction at the middle of the mating edge or cutting edge can be used as a measure in a corresponding manner.
  • the knife assembly preferably includes a plurality of individual blades, which describe axially successive, possibly overlapping portions of the rotor shell and / or which are arranged angularly offset about the rotor axis, preferably with a uniform angular approach.
  • the knives are connected via a carrier arrangement with the driven rotor shaft, which is advantageously mounted axially on both sides of the rotor shell.
  • the connection with the rotor shaft preferably takes place via carrier disks, on which base plates are fixedly and in a defined orientation, on which in turn knife plates are fastened.
  • the blade plates are advantageously removably attached to the base plates releasably secured to allow the exact alignment of the opposite edges of the counter strips in the counter blade assembly and in particular to be able to reuse the blades when worn by regrinding can.
  • a guide between knife plates and base plates or be provided on those involved elements. The adjustment is preferably carried out in a direction perpendicular to a straight cutting edge direction in the blade plate plane.
  • the supply of the wood chips in the feeder is typically horizontal, but may also be inclined so that the wood chips move under the influence of gravity in the direction of the rotor or is promoted uphill.
  • the feed direction is preferably perpendicular to the rotor axis and / or a centering device aligned with the center plane is provided in the feed device.
  • the centering device advantageously has elements which form a downwardly narrowed channel with oblique abutment surfaces on both sides, wherein these abutment surfaces advantageously merge steplessly with the opposing strips of the counterblade assembly.
  • An upwardly opposite, the direction of rotation of the rotor opposite widening counter-blade arrangement may also be advantageous in conjunction with a straight edge knife a cylindrical tube shell.
  • the feed direction ZR is typically horizontal for controlled, even feed, but may also be sloping or rising toward the rotor.
  • the rotor of the chipper is indicated by a knife assembly with several knives whose cutting offset in the case sketched in four by 90 ° with respect to the rotor axis RA and parallel to this or to the plane of the Fig. 1 perpendicular cutting planes S1, S2, S3, S4 run and describe a rotationally symmetrical to the rotor axis RA surface during rotation, which is referred to as a rotor shell MA.
  • the knives are not shown for clarity. There are advantageously provided at least two blades in the knife assembly. The maximum number of knives depends on the width of the machine and the length of the knives. Depending on the number of knives, their angular offset and / or axial offset may vary.
  • the mechanical connection of the knife assembly to the drive shaft RW is typically given by discs on which support plates are welded for the blades.
  • a counter-blade arrangement GM Stationarily fixed to the machine is a counter-blade arrangement GM, on which opposite edges GK are formed, which follow SP at a short distance of typically less than 3 mm, in particular less than 1 mm, of the contour of the rotor shell MA, as in FIG Fig. 2 is illustrated.
  • Fig. 2 forms a simplified view in the direction of arrow A in Fig. 1 which runs approximately tangentially to the rotor shell in the counter knife assembly GM.
  • the rotor shell extends in the axial direction AR of the rotor axis RA between two end positions designated with axial positions AE (L) and AE (R).
  • the rotor shell MA has in its course in the axial direction at a lying between two end positions AE axial position AO a maximum radius RM, which is greater than the rotor shell radii RE at the end positions.
  • the rotor shell is preferably mirror-symmetrical to a center plane MB lying at AO and in particular can have at least approximately a biconical shape.
  • the knives of the knife assembly are typically not only angularly offset, but also offset in the axial direction and individually cover only a portion of the axial extent LR of the rotor shell, so that in four axially offset knife positions corresponding to four associated shell sections M2 (L), M1 (L), M1 (R) and M2 (R), which may also overlap slightly at the section boundaries AZ (L) A0, AZ (R).
  • the rotor shell has the radius RZ.
  • the axial lengths of the sections can be essentially the same as outlined, so that u. U. in all sections the same individual blades can be used. In another embodiment, the axial lengths of the sections may also vary and in particular be smaller for the central sections M1 than for the external sections M2.
  • the volume of construction claimed by the rotor is significantly lower compared to a cylindrical rotor shell, since a lower limit for the maximum radius is predetermined by the maximum diameter of the logs to be chopped.
  • the end radii RE are advantageously at least 30%, in particular at least 45% of the maximum radius RM.
  • the upper limit for the end radii RE is advantageously 90%, in particular 80% of the maximum radius.
  • the opening angle WP of in Fig. 2 sketched biconical rotor shell MA is advantageously at least 120 °, preferably at least 130 °, in particular at least 140 °.
  • An upper limit for the opening angle WP is advantageously at a maximum of 170 °, preferably a maximum of 160 °, in particular a maximum of 150 °.
  • the Fig. 3 shows a simplified representation of the rotor and counter-knife arrangement in the direction of arrow B of Fig. 1 through the counter-blade arrangement radially to the rotor axis RA.
  • the counter knife assembly includes two counter strips as a counter knife GM, which may be designed in particular as square bars, but whose cross-sectional shape is not necessarily rectangular.
  • the opposing edges GK are formed, which, as in Fig. 2 sketched in a tangential line of sight, advantageously follow the contour of the rotor shell with a small gap spacing SP.
  • the mating edges are preferably straight.
  • a counter blade is provided on each side of the axial position of the maximum radius.
  • the counter-blades are sketched schematically with counter-edges reaching completely towards each other. In real construction can advantageously remain a small gap of a few mm between the two opposite edges.
  • FIG. 3 Schematically approximated are in Fig. 3 Further, the cutting planes S1, S2 and S4 according to the notation in Fig. 1 , The rear cutting plane S3 is not registered.
  • the cutting lines of the cutting planes S2 and S4 with the rotor shell at least approximately reflect the contour of the rotor shell. Knife blades lying in the cutting plane S2 move out of the plane of the drawing, while knife blades lying in the cutting plane S4 move into the plane of the drawing.
  • first cutting projection angle WES For the cutting plane S1 or lying in this knife cutting edges an inclination angle against a rotor axis RA containing and going through the cutting axial plane is entered as the first cutting projection angle WES. Accordingly, a first counter-edge projection angle WEK is shown for the inclination of the opposing edges GK of the counter-blade arrangement against the same axial plane, which is assumed to be perpendicular to the plane of the drawing.
  • At least one of the two first projection angles WES, WEK is different from zero.
  • the orientations of the cutting planes or lying in these cutting edges of the orientation of the mating edges so that forms a shear angle WS between them and cutting edges and mating edges only at one point, which in the further movement of the cutting plane in the arrow along the cutting edge and Counter edge moves, directly opposite.
  • the shear angle WS can be open in another advantageous embodiment to the center plane MB, so that wood chips cut and / or the center plane, but not outwardly, is crowded.
  • the cutting edges are in the rotor axis RA containing planes, so that in the projection in the direction of arrow B, the cutting plane S1 coincides with the rotor axis RA.
  • the counter-edges GK of the counter-knife arrangement run qualitatively at the preferred large acceptance angle WAU, as in FIG Fig. 3 . 5 and 6 sketched, with the formed by the mutually angled opposite edges against the direction of rotation of the rotor, in the pictures so upwards.
  • the cutting planes are inclined against radial planes passing through the cutting edges.
  • cutting planes S1 and opposing edges GK can be inclined in opposite directions and, in particular, the first projection angles WEK and WES can be the same but opposite in magnitude, resulting in a particularly uniform course of the gap spacing SP (preferably straight courses of knife edges and counter edges).
  • Fig. 2 Straight courses of knife edges and counter edges are of very particular advantage both for the manufacture and for regrinding.
  • the affected rotor shell section then has a slightly curved generatrix. In the figures, a straight course of the generatrices is simplified in each case sketched.
  • Fig. 4 is a view according to arrow C off Fig. 1 sketched on the counter knife assembly and a supplied tree trunk against the feed direction ZR.
  • the feature is illustrated that both the centering plate ZB and the counter blade assembly with the counter knives GM and the opposing edges formed on this GK a widening upwards to the wood chips recording with a vertically measured Make receiving angle WAU, so that the wood chips are centered both under their own weight and possibly under the action of the knife assembly in the recording.
  • the acceptance angle is preferably in a range between 135 ° and 170 °.
  • the bearing surface of the centering device which z. B. may be formed by a shaped centering ZB, z. B. transition from an initially at least approximately straight horizontal course over in an angled course and the counter knife GM forming counter knife edges join advantageously continuously to the course of the centering.
  • Fig. 5 is a first advantageous embodiment of a rotor in side view and in Fig. 6 with radial viewing direction according to arrow D of Fig. 5 outlined.
  • the knife assembly includes a plurality of blades ME1, ME2, ME3, ME4, which are offset by the rotor axis by 90 ° and in the axial direction by the same, approximately the blade width corresponding axial distances and with respect to a center plane MB mirror-symmetrical, substantially biconical rotor shell MA, which by the cutting edges of the knives ME1 and ME3 at the central plane comprises two inner shell sections M1 and then to these by the cutting edges of the blades ME2 and ME4 two outer sections M2.
  • the cutting edges of the knives are straight and lie in respective axial planes ER, ie in cutting planes containing the rotor axis.
  • the angle WES in a projection after Fig. 3 is in this case zero, as can be seen from the Fig. 3 corresponding view in Fig. 6 for the knives ME1 and ME3 clearly shows.
  • Dotted line the course of the opposite edges GK of the counter blade assembly is entered, which are inclined to the knife edges.
  • Fig. 11 is in a direction parallel to the rotor axis magnified a knife according to the orientation of ME1 of the example Fig. 5 and Fig. 6 shown with in the cutting plane S1 extending cutting edge SK, for whose end points on the rotor shell the shell portion M1 delimiting circular paths with radii RM and RZ are located.
  • the knife is made of a flat plate MP constant thickness with ground cutting edge.
  • Deviating from the embodiment according to Fig. 5 and Fig. 6 is in Fig. 7 in axial direction and in Fig. 8 outlined in the radial direction of arrow E an embodiment in which the cutting edges of the plurality of knives ME11, ME21, ME31, ME41 of the knife assembly are not in the rotor axis containing axis planes ER, but as in Fig. 1 indicated, the cutting planes run tilted against such axial planes.
  • Fig. 8 Deviating from the embodiment according to Fig. 5 and Fig. 6 is in Fig. 7 in axial direction and in Fig. 8 outlined in the radial direction of arrow E an embodiment in which the cutting edges of the plurality of knives ME11, ME21, ME31, ME41 of the knife assembly are not in the rotor axis containing axis planes ER, but as in Fig. 1 indicated, the cutting planes run tilted against such axial planes.
  • Counter edges GK lie in a plane with a counter-attack angle WRK, which is different from the angle of attack WRS.
  • the cutting planes and the plane of the opposing edges GK form a shear angle WS against each other.
  • angle of attack WRS and counter-attack angle WRK can also be the same and opposite in magnitude.
  • the occurrence of a non-zero angle of attack is correlated with the occurrence of a projection angle after Fig. 3 and synonymous with a deviating from 90 ° orientation of the cutting edge or counter edge against the respective tangential direction.
  • the knives are advantageously mounted in both embodiments on base plates GP, which in turn connected to carrier discs TS, in particular welded.
  • the attachment of the knife on the base plates is advantageously solvable to replace knives after wear or re-insert after regrinding the knife edges.
  • the knives on the base plates are adjustable.
  • the knife edges are straight and the adjustment direction is perpendicular to the knife edge.
  • Fig. 9 and Fig. 10 is an advantageous embodiment for detachable attachment of flat blade plates MP sketched on carrier plates TS base plates outlined.
  • a knife plate MP between the base plate GP and a pressure plate DP is braced by means of one or more screws as fasteners BE and held in a non-positive manner in a conventional manner.
  • the knives may be displaceable and alignable to a limited extent in all directions in the knife plane and may be held solely in a non-positive manner by the frictional forces of the clamping.
  • the blade plate MP elongated holes LL or slots which are perpendicular to the straight cutting edge SK.
  • Fig. 10 corresponds to the viewing direction in the direction of the arrow F, Fig. 11 in the direction of arrow G of Fig. 9 ,
  • the Fig. 12 shows a further example of the contour of a rotor shell MAT, which here comprises a central portion MTM with a substantially constant maximum radius RM and on both sides of these subsequent outer sections MTS with continuously decreasing to RE radius.
  • the rotor shell is again symmetrical to a center plane MB.
  • An associated knife assembly could, for example, in the outer sections MTS as in the examples Fig. 5 to Fig. 8 and in the middle section a knife assembly as in the DE 41 26 910 C1 contain.
  • At the rotor shell contour after Fig. 12 contains the counter knife assembly then z. B. at least three counter knife.
  • the formation of the counter knife arrangement as upwardly widening recording is also in a contour of in Fig. 12 sketched arrangement possible.

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  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Forests & Forestry (AREA)
  • Manufacturing & Machinery (AREA)
  • Food Science & Technology (AREA)
  • Debarking, Splitting, And Disintegration Of Timber (AREA)
  • Crushing And Pulverization Processes (AREA)

Abstract

The rotor casing has a maximum radius (RM) at an axial position spaced from the respective end settings and the end radii (RE) of the casing at the two axial end settings are less than this maximum radius and/or the counter-cutters comprise a number of cutter strips (GK) forming a chop material mounting which expands against the direction of the turning rotor. The maximum radius in the axial direction lies approximately in the middle between two end settings and the rotor casing itself runs mirror-symmetrically to the center plane (MB). The maximum radius of the casing diminishes steadily towards the end settings and the end radius (RE) amounts to 45% of the maximum radius.

Description

Die Erfindung betrifft eine Hackmaschine nach dem Oberbegriff des Patentanspruchs 1.The invention relates to a chopping machine according to the preamble of patent claim 1.

Eine derartige Hackmaschine ist beispielsweise bekannt aus der US 4776375 A und aus der DE 41 26 910 C1 . Bei der bekannten Hackmaschine beschreiben die Messerkanten eine annähernd kreiszylindrische Rotormantelfläche. Die Messerkanten sind stark gegen die achsparallelen Mantellinien geneigt und die Ebenen der Messerplatten sind relativ zur Rotorachse gekippt.Such a chipper is known for example from the US 4776375 A and from the DE 41 26 910 C1 , In the known chipper machine, the knife edges describe an approximately circular cylindrical rotor surface. The knife edges are strongly inclined to the axis-parallel generatrices and the planes of the blades are tilted relative to the rotor axis.

Eine Hackmaschine mit einem konischen Rotor und schräg zu dessen Rotorachse verlaufender Zuführrichtung ist aus der US 3 375 859 bekannt.A chipper with a conical rotor and obliquely to the rotor axis extending feed direction is from the US 3,375,859 known.

In der US 4 776 375 ist eine Hackmaschine beschrieben, deren Rotor durch eine kreiszylindrische Trommel und eine Mehrzahl von auf dieser befestigten Messerblökken besteht. Die Messerblöcke sind in axialer Richtung und in Umfangsrichtung gegeneinander versetzt und weisen jeweils eine mittlere und zwei seitliche Schneiden auf, wobei die seitlichen Schneiden einen geringeren Abstand zur Trommel besitzen als die mittlere Schneide. Das feststehende Gegenmesser enthält entsprechend dem axialen Versatz der Messerblöcke in axialer Richtung eine Mehrzahl von radial alternierend gestuften Messerabschnitten.In the US 4,776,375 a chopping machine is described, whose rotor consists of a circular cylindrical drum and a plurality of Messerblökken mounted on this. The knife blocks are offset from each other in the axial direction and in the circumferential direction and each have a central and two lateral cutting, the lateral cutting having a smaller distance from the drum than the central cutting edge. The fixed counter knife contains, in accordance with the axial offset of the knife blocks in the axial direction, a plurality of radially alternately stepped knife sections.

Bei einer in der US 2 697 557 beschriebenen Hackmaschine ist der Rotor als eine Scheibe mit mehreren im wesentlichen radialen Schneiden ausgeführt, vor welchem eine Gegenmesserschneide feststehend angeordnet ist. Eine Zuführeinrichtung enthält ein Rohr, welches schräg gegen die Ebene der Rotorscheibe geneigt ist und nach unten V-förmig zuläuft.At one in the US 2 697 557 described chopping machine, the rotor is designed as a disc with a plurality of substantially radial cutting, in front of which a counter knife blade is fixedly arranged. A feeder includes a tube which is inclined at an angle to the plane of the rotor disc and tapers downwardly in a V-shape.

Die US 3 319 673 zeigt eine Hackmaschine mit auf einem kreiszylindrischen Rotor gewunden verlaufenden Messerschneiden. Der Rotor kann auch in mehrere gleiche Teilrotoren unterteilt sein. Bei einer aus der CH 379 107 bekannten Anordnung sind eine Mehrzahl von Scheiben mit Schneiden geringer achsialer Erstreckung zu einem achsial breiteren Rotorpaket zusammengebaut.The US 3,319,673 shows a chipper with wound on a circular cylindrical rotor knife edges. The rotor can also be subdivided into several identical sub-rotors. In an arrangement known from CH 379 107, a plurality of disks with blades of small axial extent are assembled to form an axially wider rotor package.

Der vorliegenden Erfindung liegt die Aufgabe zugrunde, eine vorteilhafte derartige Hackmaschine mit verbesserter Laufruhe des Rotors anzugeben.The present invention has for its object to provide an advantageous such chopping machine with improved smoothness of the rotor.

Die Erfindung ist im Patentanspruch 1 beschrieben. Die abhängigen Ansprüche enthalten vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung.The invention is described in claim 1. The dependent claims contain advantageous refinements and developments of the invention.

Es zeigt sich überraschend, dass eine Hackmaschine nach der Erfindung wesentlich ruhiger läuft und mit geringer Antriebsleistung auskommt als eine herkömmliche Hackmaschine der eingangs beschriebenen Art.It turns out, surprisingly, that a chipper machine according to the invention runs much quieter and requires less drive power than a conventional chopping machine of the type described above.

Die als Rotormantel von den Schneidkanten der um die Rotorachse rotierenden Messeranordnung beschriebene Fläche ist vorzugsweise spiegelsymmetrisch bezüglich einer in achsialer Richtung in der Mitte zwischen den beiden Endlagen liegenden Mittelebene. Der Radius des Rotormantels varingert sich von dem Maximalradius monoton, insbesondere kontinuierlich zu den Endradien. Der Rotormantel kann insbesondere eine im wesentlichen bikonische Form besitzen. Die Gegenmesseranordnung folgt mit ihren Gegenkanten mit geringem Abstand der Kontur des Rotormantels.The surface described as a rotor casing of the cutting edges of the blade assembly rotating about the rotor axis is preferably mirror-symmetrical with respect to a median plane lying in the axial direction in the middle between the two end positions. The radius of the rotor shell varies from the maximum radius monotonously, in particular continuously to the end radii. In particular, the rotor shell may have a substantially biconical shape. The counter blade arrangement follows with its counter edges at a small distance from the contour of the rotor shell.

Die Gegenmesseranordnung, an welcher sich das Hackgut abstützt, bildet vorteilhafterweise mit mehreren Gegenmesserleisten eine sich nach oben erweiternde Aufnahme, in welcher das typischerweise längliche Hackgut unter Schwerkraftwirkung selbstzentrierend einliegt. Der Aufnahmewinkel liegt nach oben senkrecht zur Vorschubrichtung des Hackguts vorteilhafterweise zwischen 135° und 170°. Durch den großen Aufnahmewinkel ist auch bei Hackgut mit großem Durchmesser der vertikale Abstand zu den Gegenmessern in der Mitte, wo die Gegenmesser aufeinander zulaufen, vorteilhaft gering.The counter knife arrangement, on which the wood chips are supported, advantageously forms with several counter knife strips an upwardly widening receptacle, in which the typically elongated wood chips rests self-centering under the action of gravity. The acceptance angle is upwards perpendicular to the feed direction of the wood chips advantageously between 135 ° and 170 °. Due to the large acceptance angle, the vertical distance to the counter-blades in the center, where the counter-blades converge towards one another, is advantageously low, even in the case of wood chips with a large diameter.

In anderer vorteilhafter Ausführung bildet die Gegenmesseranordnung eine sich entgegen der Drehrichtung des Rotors erweiternde Aufnahme für das Hackgut, so dass dieses beim Hackvorgang unter der Einwirkung der von der Messeranordnung ausgeübten Kräfte zur Mitte der Aufname hin gedrängt und damit durch den Hackvorgang selbst in der Gegenmesseranordnung zentriert und lagestabilisiert wird. Die Maßnahme der zu den achsialen Endlagen hin sich verringernden Radien des Rotormantels einerseits und der entgegen der Drehrichtung des Rotors sich erweiternden Aufnahme können unabhängig voneinander oder auch kombiniert realisiert sein.In another advantageous embodiment, the counter-knife arrangement forms an opposite to the direction of rotation of the rotor expanding receptacle for the wood chips, so that this pressed during the chopping process under the action of the forces exerted by the knife assembly forces towards the center of Aufname and thus centered by the hacking process itself in the counter-blade arrangement and is stabilized in position. The measure of the radii of the rotor shell which reduce towards the axial end positions on the one hand and the receptacle that widens counter to the direction of rotation of the rotor can be implemented independently of one another or even combined.

Die einzelnen Gegenkanten der Gegenmesserleisten sind vorzugsweise gerade. Insbesondere kann die Gegenmesseranordnung genau zwei Gegenmesserleisten aufweisen. Diese sind dann vorzugsweise gegen die Tangentialrichtung des Rotormantels bei der Gegenmesseranordnung um einen von 90° abweichenden Kantenneigungswinkel geneigt ist.The individual opposing edges of the counter knife strips are preferably straight. In particular, the counter knife arrangement can have exactly two counter knife strips. These are then preferably inclined against the tangential direction of the rotor shell in the counter blade arrangement by a deviating from 90 ° edge inclination angle.

In entsprechender Weise sind die Schneidkanten der Messeranordnung vorzugsweise gerade. Auch die Schneidkanten können vorteilhafterweise gegen die Tangentialrichtung des Rotormantels bei der jeweiligen Messerschneide um von 90° abweichende Schneiden-Neigungswinkel geneigt sein. Die Ausrichtung der Messerschneiden bezüglich der Tangentialrichtung ist vorteilhafterweise von der Ausrichtung der Schneidkanten bezüglich der Tangentialrichtung verschieden, so dass Schneidkanten und Gegenkanten unter Einschluß eines Scherenwinkels aneinander vorbeibewegt werden. Die Neigung von Schneidkanten und zugeordneten Gegenkanten kann spiegelsymmetrisch bezüglich einer die Rotorachse enthaltenden Ebene sein. Die Scherwirkung ist insbesondere auch vorteilhaft bei harten Einschlüssen im Hackgut, beispielsweise Metallstücken (Nägeln) in Abbruchholz, wobei sich zeigt, dass durch die Ausbildung eines solchen Scherenwinkels die Schneidkanten der Messer weniger beansprucht werden.In a corresponding manner, the cutting edges of the knife assembly are preferably straight. Also, the cutting edges can advantageously be inclined against the tangential direction of the rotor shell at the respective knife edge by 90 ° different cutting angle of inclination. The orientation of the knife blades with respect to the tangential direction is advantageously different from the orientation of the cutting edges with respect to the tangential direction, so that cutting edges and counter edges are moved past each other with the inclusion of a shear angle. The inclination of cutting edges and associated mating edges may be mirror symmetric with respect to a plane containing the rotor axis. The shearing action is particularly advantageous in hard inclusions in wood chips, for example, metal pieces (nails) in demolition wood, which shows that the formation of such a shear angle, the cutting edges of the blades are less stressed.

Bei gekrümmten Gegenkanten oder Schneidkanten kann in entsprechender Weise der gemittelte Verlauf und die Tangentialrichtung an der Mitte der Gegenkante bzw. Schneidkante als Maß dienen.In the case of curved mating edges or cutting edges, the average course and the tangential direction at the middle of the mating edge or cutting edge can be used as a measure in a corresponding manner.

Die Messeranordnung enthält vorzugsweise mehrere Einzelmesser, welche achsial aufeinanderfolgende, gegebenenfalls überlappende Abschnitte des Rotormantels beschreiben und/oder welche um die Rotorachse winkelversetzt angeordnet sind, vorzugsweise mit gleichmäßigem Winkelansatz.The knife assembly preferably includes a plurality of individual blades, which describe axially successive, possibly overlapping portions of the rotor shell and / or which are arranged angularly offset about the rotor axis, preferably with a uniform angular approach.

Die Messer sind über eine Trägeranordnung mit der angetriebenen Rotorwelle verbunden, welche vorteilhafterweise achsial beidseitig des Rotormantels gelagert ist. Die Verbindung mit der Rotorwelle erfolgt vorzugsweise über Trägerscheiben, auf welchen Grundplatten fest und in definierter Ausrichtung angeordnet sind, auf welchen wiederum Messerplatten befestigt sind. Die Messerplatten sind vorteilhafterweise verstellbar auf den Grundplatten lösbar befestigt, um die genaue Ausrichtung auf die Gegenkanten der Gegenleisten in der Gegenmesseranordnung zu ermöglichen und insbesondere die Messerplatten bei Verschleiß durch Nachschleifen wieder verwenden zu können. Hierfür kann eine Führung zwischen Messerplatten und Grundplatten oder an derer beteiligter Elemente vorgesehen sein. Die Verstellmöglichkeit erfolgt vorzugsweise in einer zu einer geraden Schneidkante senkrechten Richtung in der Messerplattenebene.The knives are connected via a carrier arrangement with the driven rotor shaft, which is advantageously mounted axially on both sides of the rotor shell. The connection with the rotor shaft preferably takes place via carrier disks, on which base plates are fixedly and in a defined orientation, on which in turn knife plates are fastened. The blade plates are advantageously removably attached to the base plates releasably secured to allow the exact alignment of the opposite edges of the counter strips in the counter blade assembly and in particular to be able to reuse the blades when worn by regrinding can. For this purpose, a guide between knife plates and base plates or be provided on those involved elements. The adjustment is preferably carried out in a direction perpendicular to a straight cutting edge direction in the blade plate plane.

Die Zuführung des Hackguts in der Zuführeinrichtung erfolgt typischerweise horizontal, kann aber auch so geneigt sein, dass das Hackgut sich unter Schwerkrafteinfluss in Richtung des Rotors bewegt oder nach oben ansteigend gefördert wird. Insbesondere bei zu einer Mittelebene spiegelsymmetrischem Rotormantel verläuft die Zuführrichtung vorzugsweise senkrecht zur Rotorachse und/oder ist in der Zuführeinrichtung eine auf die Mittelebene ausgerichtete Zentriereinrichtung vorgesehen. Die Zentriervorrichtung weist dabei vorteilhafterweise Elemente auf, welche eine nach unten verengte Rinne mit beidseitigen schrägen Anlageflächen bilden, wobei diese Anlageflächen vorteilhafterweise stufenlos auf die Gegenleisten der Gegenmesseranordnung übergehen. Eine nach oben, der Drehrichtung des Rotors entgegengesetzt sich erweiternde Gegenmesseranordnung kann auch vorteilhaft in Verbindung mit einer geraden Messerkante eines zylindrischen Rohrmantels sein.The supply of the wood chips in the feeder is typically horizontal, but may also be inclined so that the wood chips move under the influence of gravity in the direction of the rotor or is promoted uphill. In particular, in the case of a mirror-symmetrical rotor mantle to a center plane, the feed direction is preferably perpendicular to the rotor axis and / or a centering device aligned with the center plane is provided in the feed device. The centering device advantageously has elements which form a downwardly narrowed channel with oblique abutment surfaces on both sides, wherein these abutment surfaces advantageously merge steplessly with the opposing strips of the counterblade assembly. An upwardly opposite, the direction of rotation of the rotor opposite widening counter-blade arrangement may also be advantageous in conjunction with a straight edge knife a cylindrical tube shell.

Die Erfindung ist nachfolgend anhand bevorzugter Ausführungsbeispiele unter Bezugnahme auf die Abbildungen noch eingehend veranschaulicht. Dabei zeigt

Fig. 1
eine Seitenansicht einer erfindungsgemäßen Hackmaschine,
Fig. 2
eine Ansicht von Rotormantel und Gegenmesseranordnung mit Blickrichtung A nach Fig. 1,
Fig. 3
eine Ansicht von Rotormantel und Gegenmesseranordnung mit Blickrichtung B nach Fig. 1,
Fig. 4
eine Ansicht von Gegenmesseranordnung und Zuführeinrichtung mit Blickrichtung C entgegen der Zuführeinrichtung,
Fig. 5
eine erste Messeranordnung in Richtung der Rotorachse,
Fig. 6
eine Ansicht zu Fig. 5 mit Blickrichtung radial auf die Rotorachse,
Fig. 7
eine Messeranordnung mit gegen die Tangentialrichtung geneigten Schneidkanten,
Fig. 8
eine Radialansicht zu Fig. 7,
Fig. 9
eine Draufsicht auf eine Messerplatte zu Fig. 8,
Fig. 10
einen Schnitt durch eine Messerbefestigung nach Fig. 9,
Fig. 11
eine Seitenansicht einer Messerposition nach Fig. 5,
Fig. 12
eine weitere Kontur eines Rotormantels.
The invention is illustrated below with reference to preferred embodiments with reference to the figures still in detail. It shows
Fig. 1
a side view of a chopping machine according to the invention,
Fig. 2
a view of the rotor shell and counter-blade arrangement looking in the direction A to Fig. 1 .
Fig. 3
a view of the rotor shell and counter-blade arrangement with a view B after Fig. 1 .
Fig. 4
a view of the counter blade arrangement and feed device facing in the direction C against the feeder,
Fig. 5
a first knife arrangement in the direction of the rotor axis,
Fig. 6
a view too Fig. 5 looking radially towards the rotor axis,
Fig. 7
a knife arrangement with cutting edges inclined towards the tangential direction,
Fig. 8
a radial view too Fig. 7 .
Fig. 9
a plan view of a blade plate Fig. 8 .
Fig. 10
a section through a knife attachment after Fig. 9 .
Fig. 11
a side view of a knife position after Fig. 5 .
Fig. 12
another contour of a rotor shell.

Bei der in Fig. 1 in Seitenansicht skizzierten Anordnung ist als typisches Hackgut ein Baumstamm-Abschnitt BS in einer Zuführeinrichtung mittels eines Kettenförderers KF in Zuführrichtung ZR über eine Zentriereinrichtung ZE mit einem Zentrierblech ZB auf den Rotor einer Trommelhackmaschine zu bewegt. Die Zuführrichtung ZR ist typischerweise horizontal für kontrollierten gleichmäßigen Vorschub, kann aber auch zum Rotor hin abfallend oder ansteigend sein.At the in Fig. 1 outlined in side elevation as a typical wood chips a tree trunk section BS in a feeder by means of a chain conveyor KF in the feed direction ZR via a centering device ZE with a centering plate ZB on the rotor of a drum chipper moves. The feed direction ZR is typically horizontal for controlled, even feed, but may also be sloping or rising toward the rotor.

Der Rotor der Hackmaschine ist angedeutet durch eine Messeranordnung mit mehreren Messern, deren Schneiden im skizzierten Fall in vier um 90° bezüglich der Rotorachse RA versetzten und zu dieser parallelen bzw. zur Zeichenebene der Fig. 1 senkrechten Schneidenebenen S1, S2, S3, S4 verlaufen und bei der Rotation eine zur Rotorachse RA rotationssymmetrische Fläche beschreiben, welche als Rotormantel MA bezeichnet ist. Die Messer sind der Übersichtlichkeit halber nicht mit eingezeichnet. Es sind vorteilhafterweise mindestens zwei Messer in der Messeranordnung vorgesehen. Die maximale Anzahl der Messer ist u. a. durch die Breite der Maschine und die Länge der Messer bestimmt. Je nach Anzahl der Messer kann deren Winkelversatz und/oder achsialer Versatz variieren. Die mechanische Verbindung der Messeranordnung mit der Antriebswelle RW ist typischerweise durch Scheiben gegeben, auf welchen Trägerplatten für die Messer aufgeschweißt sind.The rotor of the chipper is indicated by a knife assembly with several knives whose cutting offset in the case sketched in four by 90 ° with respect to the rotor axis RA and parallel to this or to the plane of the Fig. 1 perpendicular cutting planes S1, S2, S3, S4 run and describe a rotationally symmetrical to the rotor axis RA surface during rotation, which is referred to as a rotor shell MA. The knives are not shown for clarity. There are advantageously provided at least two blades in the knife assembly. The maximum number of knives depends on the width of the machine and the length of the knives. Depending on the number of knives, their angular offset and / or axial offset may vary. The mechanical connection of the knife assembly to the drive shaft RW is typically given by discs on which support plates are welded for the blades.

Ortsfest an der Maschine ist eine Gegenmesseranordnung GM angebracht, an welcher Gegenkanten GK ausgebildet sind, die in geringem Abstand SP von typischerweise weniger als 3 mm, insbesondere weniger als 1 mm der Kontur des Rotormantels MA folgen, wie in Fig. 2 veranschaulicht ist. Fig. 2 bildet eine vereinfachte Ansicht in Richtung des Pfeiles A in Fig. 1, welche ungefähr tangential zum Rotormantel bei der Gegenmesseranordnung GM verläuft.Stationarily fixed to the machine is a counter-blade arrangement GM, on which opposite edges GK are formed, which follow SP at a short distance of typically less than 3 mm, in particular less than 1 mm, of the contour of the rotor shell MA, as in FIG Fig. 2 is illustrated. Fig. 2 forms a simplified view in the direction of arrow A in Fig. 1 which runs approximately tangentially to the rotor shell in the counter knife assembly GM.

Der Rotormantel erstreckt sich in achsialer Richtung AR der Rotorachse RA zwischen zwei mit achsialen Positionen AE (L) und AE (R) bezeichneten Endlagen. Der Rotormantel MA weist in seinem Verlauf in achsialer Richtung an einer zwischen beiden Endlagen AE liegenden Achsialposition AO einen Maximalradius RM auf, der größer ist als die Rotormantelradien RE an den Endlagen. Der Rotormantel ist wie skizziert bevorzugt spiegelsymmetrisch zu einer bei AO liegenden Mittelebene MB und kann insbesondere zumindest angenähert eine bikonische Form aufweisen.The rotor shell extends in the axial direction AR of the rotor axis RA between two end positions designated with axial positions AE (L) and AE (R). The rotor shell MA has in its course in the axial direction at a lying between two end positions AE axial position AO a maximum radius RM, which is greater than the rotor shell radii RE at the end positions. As sketched, the rotor shell is preferably mirror-symmetrical to a center plane MB lying at AO and in particular can have at least approximately a biconical shape.

Die Messer der Messeranordnung sind typischerweise nicht nur winkelversetzt, sondern auch in achsialer Richtung versetzt und decken einzeln nur einen Teil der achsialen Erstreckung LR des Rotormantels ab, so dass sich bei in achsialer Richtung vier versetzten Messerpositionen entsprechend vier zugeordnete Mantelabschnitte M2 (L), M1 (L), M1 (R) und M2 (R) ergeben, welche an den Abschnittsgrenzen AZ (L) AO, AZ (R) auch geringfügig überlappen können. An den Abschnittsgrenzen AZ weist der Rotormantel den Radius RZ auf. Die achsialen Längen der Abschnitte können wie skizziert im wesentlichen gleich sein, so dass u. U. in allen Abschnitten gleiche Einzelmesser eingesetzt werden können. In anderer Ausführung können die achsialen Längen der Abschnitte auch variieren und insbesondere für die mittleren Abschnitte M1 geringer sein als für die äußeren Abschnitte M2.The knives of the knife assembly are typically not only angularly offset, but also offset in the axial direction and individually cover only a portion of the axial extent LR of the rotor shell, so that in four axially offset knife positions corresponding to four associated shell sections M2 (L), M1 (L), M1 (R) and M2 (R), which may also overlap slightly at the section boundaries AZ (L) A0, AZ (R). At the section boundaries AZ, the rotor shell has the radius RZ. The axial lengths of the sections can be essentially the same as outlined, so that u. U. in all sections the same individual blades can be used. In another embodiment, the axial lengths of the sections may also vary and in particular be smaller for the central sections M1 than for the external sections M2.

Insbesondere für den typischen Fall von Baumstämmen oder anderem Rundholz oder Langholz als Hackgut liegt das Verhältnis von Maximalradius RM und achsialer Länge LR des Rotormantels vorteilhafterweise zwischen RM/LR=0,75 und LR/RM=0,75.In particular, for the typical case of logs or other roundwood or long wood as wood chips, the ratio of maximum radius RM and axial length LR of the rotor shell is advantageously between RM / LR = 0.75 and LR / RM = 0.75.

Durch die gegenüber dem Maximalradius RM in den Endlagen geringeren Radien RE wird das vom Rotor beanspruchte Bauvolumen gegenüber einem zylindrischen Rotormantel deutlich geringer, da eine Untergrenze für den maximalen Radius durch den maximalen Durchmesser der zu hackenden Stämme vorgegeben ist.By compared to the maximum radius RM in the end positions lower radii RE, the volume of construction claimed by the rotor is significantly lower compared to a cylindrical rotor shell, since a lower limit for the maximum radius is predetermined by the maximum diameter of the logs to be chopped.

Die Endradien RE betragen vorteilhafterweise wenigstens 30 %, insbesondere wenigstens 45 % des Maximalradius RM. Die Obergrenze für die Endradien RE liegt vorteilhafterweise bei 90 %, insbesondere bei 80 % des Maximalradius. Der Öffnungswinkel WP des in Fig. 2 skizzierten bikonischen Rotormantels MA beträgt vorteilhafterweise wenigstens 120°, vorzugsweise wenigstens 130°, insbesondere wenigstens 140°. Eine Obergrenze für den Öffnungswinkel WP liegt vorteilhafterweise bei maximal 170°, vorzugsweise maximal 160°, insbesondere maximal 150°.The end radii RE are advantageously at least 30%, in particular at least 45% of the maximum radius RM. The upper limit for the end radii RE is advantageously 90%, in particular 80% of the maximum radius. The opening angle WP of in Fig. 2 sketched biconical rotor shell MA is advantageously at least 120 °, preferably at least 130 °, in particular at least 140 °. An upper limit for the opening angle WP is advantageously at a maximum of 170 °, preferably a maximum of 160 °, in particular a maximum of 150 °.

Die Fig. 3 zeigt eine vereinfachte Darstellung von Rotor und Gegenmesseranordnung in Blickrichtung des Pfeils B von Fig. 1 durch die Gegenmesseranordnung radial zur Rotorachse RA. Die Gegenmesseranordnung enthält zwei Gegenleisten als Gegenmesser GM, welche insbesondere auch als Vierkantleisten ausgeführt sein können, deren Querschnittsform aber nicht notwendig rechteckig ist. An den Gegenmessern GM sind die Gegenkanten GK ausgebildet, welche, wie in Fig. 2 in tangentialer Blickrichtung skizziert, vorteilhafterweise der Kontur des Rotormantels mit geringem Spaltabstand SP folgen. Die Gegenkanten sind vorzugsweise gerade. Vorzugsweise ist auf jeder Seite der achsialen Position des Maximalradius je ein Gegenmesser vorgesehen. Die Gegenmesser sind schematisch mit vollständig aufeinander zu reichenden Gegenkanten skizziert. In realer Konstruktion kann vorteilhafterweise eine geringe Lücke von wenigen mm zwischen den beiden Gegenkanten frei bleiben.The Fig. 3 shows a simplified representation of the rotor and counter-knife arrangement in the direction of arrow B of Fig. 1 through the counter-blade arrangement radially to the rotor axis RA. The counter knife assembly includes two counter strips as a counter knife GM, which may be designed in particular as square bars, but whose cross-sectional shape is not necessarily rectangular. On the counter knives GM, the opposing edges GK are formed, which, as in Fig. 2 sketched in a tangential line of sight, advantageously follow the contour of the rotor shell with a small gap spacing SP. The mating edges are preferably straight. Preferably, a counter blade is provided on each side of the axial position of the maximum radius. The counter-blades are sketched schematically with counter-edges reaching completely towards each other. In real construction can advantageously remain a small gap of a few mm between the two opposite edges.

Schematisch angenähert eingezeichnet sind in Fig. 3 ferner die Schneidenebenen S1, S2 und S4 nach der Notation in Fig. 1. Die hinten liegende Schneidenebene S3 ist nicht eingetragen. Die Schnittlinien der Schneidenebenen S2 und S4 mit dem Rotormantel geben wenigstens annähernd die Kontur des Rotormantels wieder. In der Schneidenebene S2 liegende Messerschneiden bewegen sich aus der Zeichenebene heraus, in der Schneidenebene S4 liegende Messerschneiden in die Zeichenebene hinein.Schematically approximated are in Fig. 3 Further, the cutting planes S1, S2 and S4 according to the notation in Fig. 1 , The rear cutting plane S3 is not registered. The cutting lines of the cutting planes S2 and S4 with the rotor shell at least approximately reflect the contour of the rotor shell. Knife blades lying in the cutting plane S2 move out of the plane of the drawing, while knife blades lying in the cutting plane S4 move into the plane of the drawing.

Für die Schneidenebene S1 bzw. in dieser liegende Messer-Schneidkanten ist ein Neigungswinkel gegen eine die Rotorachse RA enthaltende und durch die Schneiden gehende Achsialebene als erster Schneiden-Projektionswinkel WES eingetragen. Entsprechend ist für die Neigung der Gegenkanten GK der Gegenmesseranordnung gegen dieselbe Achsialebene, welche als senkrecht zur Zeichenebene stehend angenommen ist, ein erster Gegenkanten-Projektionswinkel WEK eingezeichnet.For the cutting plane S1 or lying in this knife cutting edges an inclination angle against a rotor axis RA containing and going through the cutting axial plane is entered as the first cutting projection angle WES. Accordingly, a first counter-edge projection angle WEK is shown for the inclination of the opposing edges GK of the counter-blade arrangement against the same axial plane, which is assumed to be perpendicular to the plane of the drawing.

Vorzugsweise ist wenigstens einer der beiden ersten Projektionswinkel WES, WEK von Null verschieden. Vorteilhafterweise sind in der Projektion nach Fig. 3 die Ausrichtungen der Schneidenebenen bzw. der in diesen liegenden Schneidkanten von der Ausrichtung der Gegenkanten verschieden, so dass sich zwischen diesen ein Scherenwinkel WS ausbildet und Schneidkanten und Gegenkanten jeweils nur an einer Stelle, welche sich bei der Weiterbewegung der Schneidebene in Pfeilrichtung entlang der Schneidkante und Gegenkante verschiebt, unmittelbar gegenüberstehen. Der Scherenwinkel WS kann in anderer vorteilhafter Ausführung zur Mittelebene MB hin offen sein, so dass Hackgut geschnitten und/oder zur Mittelebene hin, nicht aber nach außen, gedrängt wird.Preferably, at least one of the two first projection angles WES, WEK is different from zero. Advantageously, in the projection after Fig. 3 the orientations of the cutting planes or lying in these cutting edges of the orientation of the mating edges, so that forms a shear angle WS between them and cutting edges and mating edges only at one point, which in the further movement of the cutting plane in the arrow along the cutting edge and Counter edge moves, directly opposite. The shear angle WS can be open in another advantageous embodiment to the center plane MB, so that wood chips cut and / or the center plane, but not outwardly, is crowded.

In einer ersten vorteilhaften Ausführungsform, welche in Fig. 5 und 6 dargestellt ist, liegen die Schneiden in die Rotorachse RA enthaltenden Ebenen, so dass in der Projektion in Pfeilrichtung B die Schneidenebene S1 mit der Rotorachse RA zusammenfällt. Die Gegenkanten GK der Gegenmesseranordnung verlaufen bei dem bevorzugten großen Aufnahmewinkel WAU qualitativ, wie in Fig. 3, 5 und 6 skizziert, mit der durch die gegeneinander angewinkelte Gegenkanten gebildeten Spitze entgegen der Drehrichtung des Rotors, in den Abbildungen also nach oben.In a first advantageous embodiment, which in Fig. 5 and 6 is shown, the cutting edges are in the rotor axis RA containing planes, so that in the projection in the direction of arrow B, the cutting plane S1 coincides with the rotor axis RA. The counter-edges GK of the counter-knife arrangement run qualitatively at the preferred large acceptance angle WAU, as in FIG Fig. 3 . 5 and 6 sketched, with the formed by the mutually angled opposite edges against the direction of rotation of the rotor, in the pictures so upwards.

In einer zweiten vorteilhaften Ausführungsform sind die Schneidenebenen gegen durch die Schneiden gehende Radialebenen geneigt.In a second advantageous embodiment, the cutting planes are inclined against radial planes passing through the cutting edges.

In anderer Ausführung können Schneidenebenen S1 und Gegenkanten GK entgegengesetzt geneigt und insbesondere auch die ersten Projektionswinkel WEK und WES dem Betrage nach gleich aber entgegengesetzt gerichtet sein, woraus sich bei bevorzugt geraden Verläufen von Messerschneiden und Gegenkanten ein besonders gleichmäßiger Verlauf des Spaltabstands SP (Fig. 2) ergibt. Gerade Verläufe von Messerschneiden und Gegenkanten sind sowohl für die Herstellung als auch für das Nachschleifen von ganz besonderem Vorteil. Der betroffene Rotormantelabschnitt weist dann eine leicht gekrümmte Mantellinie auf. In den Figuren ist vereinfacht jeweils ein gerader Verlauf der Mantellinien skizziert.In another embodiment, cutting planes S1 and opposing edges GK can be inclined in opposite directions and, in particular, the first projection angles WEK and WES can be the same but opposite in magnitude, resulting in a particularly uniform course of the gap spacing SP (preferably straight courses of knife edges and counter edges). Fig. 2 ). Straight courses of knife edges and counter edges are of very particular advantage both for the manufacture and for regrinding. The affected rotor shell section then has a slightly curved generatrix. In the figures, a straight course of the generatrices is simplified in each case sketched.

In Fig. 4 ist eine Ansicht entsprechend Pfeil C aus Fig. 1 auf die Gegenmesseranordnung und einen zugeführten Baumstamm entgegen der Zuführrichtung ZR skizziert. In dieser Ansicht ist das Merkmal veranschaulicht, dass sowohl das Zentrierblech ZB als auch die Gegenmesseranordnung mit den Gegenmessern GM und den an diesen ausgebildeten Gegenkanten GK eine sich nach oben zum Hackgut hin erweiternde Aufnahme mit einem vertikal gemessenen Aufnahmewinkel WAU bilden, so dass das Hackgut sowohl unter dem eigenen Gewicht als auch eventuell unter der Einwirkung der Messeranordnung in der Aufnahme zentriert wird. Der Aufnahmewinkel liegt vorzugsweise in einem Bereich zwischen 135° und 170°.In Fig. 4 is a view according to arrow C off Fig. 1 sketched on the counter knife assembly and a supplied tree trunk against the feed direction ZR. In this view, the feature is illustrated that both the centering plate ZB and the counter blade assembly with the counter knives GM and the opposing edges formed on this GK a widening upwards to the wood chips recording with a vertically measured Make receiving angle WAU, so that the wood chips are centered both under their own weight and possibly under the action of the knife assembly in the recording. The acceptance angle is preferably in a range between 135 ° and 170 °.

Die Auflagefläche der Zentriereinrichtung welche z. B. durch ein geformtes Zentrierblech ZB gebildet sein kann, kann z. B. von einem anfänglich zumindest annähernd geraden horizontalen Verlauf über in einen angewinkelten Verlauf übergehen und die die Gegenmesser GM bildenden Gegenmesserleisten schließen sich vorteilhafterweise stufenlos an den Verlauf des Zentrierblechs an.The bearing surface of the centering device which z. B. may be formed by a shaped centering ZB, z. B. transition from an initially at least approximately straight horizontal course over in an angled course and the counter knife GM forming counter knife edges join advantageously continuously to the course of the centering.

In Fig. 4 sind zusätzlich noch die Verläufe von Rotormantel MA und Rotorachse RA entgegen der Blickrichtung eingetragen.In Fig. 4 In addition, the gradients of rotor shell MA and rotor axis RA are registered against the line of sight.

In Fig. 5 ist eine erste vorteilhafte Ausführungsform eines Rotors in Seitenansicht und in Fig. 6 mit radialer Blickrichtung nach Pfeil D von Fig. 5 skizziert. Bei dieser Ausführungsform enthält die Messeranordnung mehrere Messer ME1, ME2, ME3, ME4, welche um die Rotorachse um jeweils 90° und in achsialer Richtung um gleiche, ungefähr der Messerbreite entsprechende Achsialabstände versetzt sind und einen bezüglich einer Mittelebene MB spiegelsymmetrischen, im wesentlichen bikonischen Rotormantel MA erzeugen, welcher durch die Schneidkanten der Messer ME1 bzw. ME3 bei der Mittelebene zwei innere Mantelabschnitte M1 und an diese anschließend durch die Schneidkanten der Messer ME2 bzw. ME4 zwei außenliegende Abschnitte M2 umfasst. Die Schneidkanten der Messer sind gerade und liegen jeweils in Achsenebenen ER, d. h. in Schneidenebenen, welche die Rotorachse enthalten. Der Winkel WES in einer Projektion nach Fig. 3 ist in diesem Fall gleich Null, wie sich aus der Fig. 3 entsprechenden Ansicht in Fig. 6 für die Messer ME1 und ME3 anschaulich zeigt. Mit punktierter Linie ist der Verlauf der Gegenkanten GK der Gegenmesseranordnung eingetragen, welche geneigt zu den Messerschneiden verlaufen.In Fig. 5 is a first advantageous embodiment of a rotor in side view and in Fig. 6 with radial viewing direction according to arrow D of Fig. 5 outlined. In this embodiment, the knife assembly includes a plurality of blades ME1, ME2, ME3, ME4, which are offset by the rotor axis by 90 ° and in the axial direction by the same, approximately the blade width corresponding axial distances and with respect to a center plane MB mirror-symmetrical, substantially biconical rotor shell MA, which by the cutting edges of the knives ME1 and ME3 at the central plane comprises two inner shell sections M1 and then to these by the cutting edges of the blades ME2 and ME4 two outer sections M2. The cutting edges of the knives are straight and lie in respective axial planes ER, ie in cutting planes containing the rotor axis. The angle WES in a projection after Fig. 3 is in this case zero, as can be seen from the Fig. 3 corresponding view in Fig. 6 for the knives ME1 and ME3 clearly shows. Dotted line the course of the opposite edges GK of the counter blade assembly is entered, which are inclined to the knife edges.

In Fig. 11 ist in zur Rotorachse paralleler Blickrichtung vergrößert ein Messer entsprechend der Ausrichtung von ME1 des Beispiels nach Fig. 5 und Fig. 6 dargestellt mit in der Schneidenebene S1 verlaufender Schneidkante SK, für deren Endpunkte die auf dem Rotormantel den Mantelabschnitt M1 begrenzenden Kreisbahnen mit Radien RM bzw. RZ eingezeichnet sind. Das Messer ist aus einer ebenen Platte MP konstanter Dicke mit angeschliffener Schneidkante hergestellt.In Fig. 11 is in a direction parallel to the rotor axis magnified a knife according to the orientation of ME1 of the example Fig. 5 and Fig. 6 shown with in the cutting plane S1 extending cutting edge SK, for whose end points on the rotor shell the shell portion M1 delimiting circular paths with radii RM and RZ are located. The knife is made of a flat plate MP constant thickness with ground cutting edge.

Abweichend von dem Ausführungsbeispiel nach Fig. 5 und Fig. 6 ist in Fig. 7 in achsialer Blickrichtung und in Fig. 8 in radialer Blickrichtung nach Pfeil E eine Ausführungsform skizziert, bei welcher die Schneiden der mehreren Messer ME11, ME21, ME31, ME41 der Messeranordnung nicht in die Rotorachse enthaltenden Achsenebenen ER liegen, sondern wie in Fig. 1 angedeutet, die Schneidenebenen gegen solche Achsenebenen gekippt verlaufen. In Fig. 8 ist dies für die Schneiden des Messers ME11 durch den Anstellwinkel WRS einer senkrecht zur Zeichenebene stehenden, die Schneide des Messers ME11 enthaltenden und zur Rotorachse RA parallelen Schneidenebene S11 gegen eine die Rotorachse enthaltende Ebene ER durch die Schneide des Messers ME11 charakterisiert. Gegenkanten GK liegen in einer Ebene mit einem Gegen-Anstellwinkel WRK, welcher von dem Anstellwinkel WRS verschieden ist. Die Schneidenebenen und die Ebene der Gegenkanten GK bilden einen Scherenwinkel WS gegeneinander. In anderer Ausführung können Anstellwinkel WRS und Gegenanstellwinkel WRK auch dem Betrag nach gleich und entgegengesetzt gerichtet sein.Deviating from the embodiment according to Fig. 5 and Fig. 6 is in Fig. 7 in axial direction and in Fig. 8 outlined in the radial direction of arrow E an embodiment in which the cutting edges of the plurality of knives ME11, ME21, ME31, ME41 of the knife assembly are not in the rotor axis containing axis planes ER, but as in Fig. 1 indicated, the cutting planes run tilted against such axial planes. In Fig. 8 this is characterized by the angle of incidence WRS of a cutting plane S11 perpendicular to the plane of the drawing, containing the blade of the blade ME11 and parallel to the rotor axis RA, against a plane ER containing the rotor axis by the blade of the blade ME11. Counter edges GK lie in a plane with a counter-attack angle WRK, which is different from the angle of attack WRS. The cutting planes and the plane of the opposing edges GK form a shear angle WS against each other. In another embodiment, angle of attack WRS and counter-attack angle WRK can also be the same and opposite in magnitude.

Das Auftreten eines Anstellwinkels ungleich Null ist korreliert mit dem Auftreten eines Projektionswinkels nach Fig. 3 und gleichbedeutend mit einer von 90° abweichenden Ausrichtung der Schneidkante oder Gegenkante gegen die jeweilige Tangentialrichtung.The occurrence of a non-zero angle of attack is correlated with the occurrence of a projection angle after Fig. 3 and synonymous with a deviating from 90 ° orientation of the cutting edge or counter edge against the respective tangential direction.

Die Messer sind in beiden Ausführungsbeispielen vorteilhafterweise auf Grundplatten GP befestigt, welche ihrerseits mit Trägerscheiben TS verbunden, insbesondere verschweißt sind. Die Befestigung der Messer auf den Grundplatten ist vorteilhafterweise lösbar, um Messer nach Verschleiß auszutauschen oder nach Nachschleifen der Messerschneiden wieder einzusetzen. Um nachgeschliffene Messer exakt positionieren und wieder einen geringen Abstandsspalt SP einstellen zu können, sind die Messer auf den Grundplatten verstellbar. Vorzugsweise sind die Messerschneiden gerade und die Verstellrichtung verläuft senkrecht zu der Messerschneide.The knives are advantageously mounted in both embodiments on base plates GP, which in turn connected to carrier discs TS, in particular welded. The attachment of the knife on the base plates is advantageously solvable to replace knives after wear or re-insert after regrinding the knife edges. In order to be able to precisely position reground knives and to be able to set a small gap SP again, the knives on the base plates are adjustable. Preferably, the knife edges are straight and the adjustment direction is perpendicular to the knife edge.

In Fig. 9 und Fig. 10 ist eine vorteilhafte Ausführungsform zur lösbaren Befestigung von ebenen Messerplatten MP auf mit Trägerscheiben TS verbundenen Grundplatten skizziert. Dabei wird in an sich bekannter Weise eine Messerplatte MP zwischen der Grundplatte GP und einer Druckplatte DP mittels eines oder mehrerer Schrauben als Befestigungselemente BE verspannt und kraftschlüssig gehalten. Die Messer können in einer ersten Ausführungsform in der Messerebene in begrenztem Umfang in alle Richtungen verschiebbar und ausrichtbar sein und allein kraftschlüssig durch die Reibungskräfte der Verspannung gehalten sein. Gemäß einer bevorzugten Ausführungsform weist die Messerplatte MP Langlöcher LL oder Schlitze auf, welche senkrecht zur geraden Schneidkante SK verlaufen. In der Grundplatte GP und/oder der Druckplatte DP sind mit den Schlitzen oder Langlöchern korrespondierende Längsführungselemente LF vorhanden, so dass bei Längsverstellung der Messer immer automatisch eine exakte Ausrichtung der Messerschneide gewährleistet ist und nur deren Position in Verschieberichtung, welche die Weite des Abstandsspalts SP bestimmt, einzustellen ist. Fig. 10 entspricht der Blickrichtung in Pfeilrichtung F, Fig. 11 in Pfeilrichtung G von Fig. 9.In Fig. 9 and Fig. 10 is an advantageous embodiment for detachable attachment of flat blade plates MP sketched on carrier plates TS base plates outlined. In this case, a knife plate MP between the base plate GP and a pressure plate DP is braced by means of one or more screws as fasteners BE and held in a non-positive manner in a conventional manner. In a first embodiment, the knives may be displaceable and alignable to a limited extent in all directions in the knife plane and may be held solely in a non-positive manner by the frictional forces of the clamping. According to a preferred embodiment, the blade plate MP elongated holes LL or slots which are perpendicular to the straight cutting edge SK. In the base plate GP and / or the pressure plate DP are provided with the slots or slots corresponding longitudinal guide elements LF, so that automatically ensures an exact alignment of the knife edge in longitudinal adjustment of the knife is and only their position in the direction of displacement, which determines the width of the clearance gap SP, is set. Fig. 10 corresponds to the viewing direction in the direction of the arrow F, Fig. 11 in the direction of arrow G of Fig. 9 ,

Die Fig. 12 zeigt ein weiteres Beispiel für die Kontur eines Rotormantels MAT, welcher hier einen mittleren Abschnitt MTM mit im wesentlichen konstantem Maximalradius RM und an diesen beidseitig anschließend außenliegende Abschnitte MTS mit kontinuierlich bis auf RE abnehmendem Radius umfasst. Der Rotormantel sei wieder symmetrisch zu einer Mittelebene MB. Eine zugehörige Messeranordnung könnte beispielsweise in den äußeren Abschnitten MTS wie bei den Beispielen nach Fig. 5 bis Fig. 8 und im mittleren Abschnitt eine Messeranordnung wie bei der DE 41 26 910 C1 enthalten. Bei der Rotormantelkontur nach Fig. 12 enthält die Gegenmesseranordnung dann z. B. wenigstens drei Gegenmesser. Die Ausbildung der Gegenmesseranordnung als sich nach oben erweiternde Aufnahme ist auch bei einer Kontur der in Fig. 12 skizzierten Anordnung möglich.The Fig. 12 shows a further example of the contour of a rotor shell MAT, which here comprises a central portion MTM with a substantially constant maximum radius RM and on both sides of these subsequent outer sections MTS with continuously decreasing to RE radius. The rotor shell is again symmetrical to a center plane MB. An associated knife assembly could, for example, in the outer sections MTS as in the examples Fig. 5 to Fig. 8 and in the middle section a knife assembly as in the DE 41 26 910 C1 contain. At the rotor shell contour after Fig. 12 contains the counter knife assembly then z. B. at least three counter knife. The formation of the counter knife arrangement as upwardly widening recording is also in a contour of in Fig. 12 sketched arrangement possible.

Die vorstehend und die in den Ansprüchen angegebenen sowie die den Abbildungen entnehmbaren Merkmale sind sowohl einzeln als auch in verschiedener Kombination vorteilhaft realisierbar. Die Erfindung ist nicht auf die beschriebenen Ausführungsbeispiele beschränkt, sondern im Rahmen fachmännischen Könnens in mancherlei Weise abwandelbar. Insbesondere sind weitere Konturen des Rotormantels möglich, welche von den einfachen, bevorzugten Beispielen abweichen. Die einzelnen Achsialabschnitte des Rotormantels können mit unterschiedlicher achsialer Erstreckung und/oder unterschiedlicher Ausrichtung der Mantellinienabschnitte ausgeführt sein und eine unterschiedliche Zahl von Messern enthalten. Rotormantellinien und/oder Messer-Schneidkanten und oder Gegenmesser-Gegenkanten können vollständig oder abschnittsweise gekrümmt sein.The features indicated above and in the claims, as well as the features which can be seen in the figures, can be implemented advantageously both individually and in various combinations. The invention is not limited to the exemplary embodiments described, but can be modified in many ways within the scope of expert knowledge. In particular, further contours of the rotor shell are possible, which deviate from the simple, preferred examples. The individual axial sections of the rotor shell can be designed with different axial extent and / or different orientation of the generatrix sections and contain a different number of blades. Rotor mantle lines and / or knife cutting edges and or counter knife mating edges may be fully or partially curved.

Claims (17)

  1. Chipper, in particular for chipping articles to be chipped, in particular elongate pieces of wood such as log sections, timber, etc., having a chipper rotor and a feeding device, wherein the chipper rotor has a cutter arrangement which rotates about a rotor axis (RA) and the cutting edges (SK) of which describe a rotor circumference (MA) which is rotationally symmetrical to the rotor axis and extends in the axial direction between two end positions (AE), and wherein on the feeding device there is a mating cutter arrangement having mating edges (GK) which follow the rotor circumference at a small spacing (SP), characterized in that the radius of the rotor circumference decreases monotonically from a maximum radius (RM) at an axial position (AO) spaced apart from the two end positions in the axial direction with respect to the two end positions (AE) as far as smaller end radii (RE) of the rotor circumference in the two axial end positions (AE), and in that the mating cutter arrangement having a plurality of mating cutter strips (GM) forms a holder for the articles to be chipped, said holder widening along the rotor circumference counter to the direction of rotation of the rotor.
  2. Chipper according to Claim 1, characterized in that the maximum radius in the axial direction (AR) is located approximately in the centre between the two end positions (AE).
  3. Chipper according to Claim 1 or 2, characterized in that the rotor circumference extends in a mirror-symmetrical manner with respect to a centre plane (MB) between the two end positions.
  4. Chipper according to one of Claims 1 to 3, characterized in that the end radii (RE) are at least 30%, in particular at least 45%, of the maximum radius (RM).
  5. Chipper according to one of Claims 1 to 4, characterized in that the end radii (RE) are at most 80% of the maximum radius (RM).
  6. Chipper according to one of Claims 1 to 5, characterized in that the maximum radius (RM) and the axial length (LR) of the rotor circumference differ from one another by at most 25% of the value which is larger in each case.
  7. Chipper according to one of Claims 1 to 6, characterized in that the cutter arrangement is subdivided in the axial direction into a plurality of sections (M1, M2) having separate individual cutters.
  8. Chipper according to one of Claims 1 to 7, characterized in that the cutter arrangement has a plurality of cutters that are arranged in an angularly offset manner around the rotor axis.
  9. Chipper according to one of Claims 1 to 8, characterized in that the cutter arrangement has planar cutters having sharpened cutting edges (SK) .
  10. Chipper according to one of Claims 1 to 9, characterized in that the cutter arrangement has cutters having straight cutting edges.
  11. Chipper according to one of Claims 1 to 10, characterized in that in the cutter arrangement cutters are fastened to a cutter carrier and can be adjusted perpendicularly to the cutting edge.
  12. Chipper according to one of Claims 1 to 11, characterized in that the feeding device (ZR) extends in the feeding direction perpendicularly to the axial direction (AR) of the rotor.
  13. Chipper according to one of Claims 1 to 12, characterized in that the feeding device comprises a centring device.
  14. Chipper according to Claim 13, characterized in that the centring device contains a downwardly narrowed channel having abutment surfaces on both sides for the articles to be chipped.
  15. Chipper according to Claim 14, characterized in that the abutment surfaces merge in a substantially continuous manner into the mating cutter arrangement (GM).
  16. Chipper according to one of Claims 1 to 15, characterized in that the mating cutter arrangement contains mating cutters having straight mating edges (GK).
  17. Chipper according to one of Claims 1 to 16, characterized in that cutting edges of the cutter arrangement and corresponding mating edges of the mating cutter arrangement extend in different orientations with respect to the tangential direction of the rotor circumference.
EP03010331A 2002-05-14 2003-05-08 Chipping machine Expired - Lifetime EP1362679B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10221308 2002-05-14
DE10221308A DE10221308B4 (en) 2002-05-14 2002-05-14 Hoe

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EP1362679A2 EP1362679A2 (en) 2003-11-19
EP1362679A3 EP1362679A3 (en) 2007-10-10
EP1362679B1 true EP1362679B1 (en) 2012-01-04

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EP03010331A Expired - Lifetime EP1362679B1 (en) 2002-05-14 2003-05-08 Chipping machine

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AT (1) ATE539865T1 (en)
DE (1) DE10221308B4 (en)

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Publication number Priority date Publication date Assignee Title
CN107737621A (en) * 2017-11-30 2018-02-27 河南荣成机械工程有限公司 Composite blade formula flexibility kinetic energy grain dejacketer

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2697557A (en) 1952-03-17 1954-12-21 Murray D J Mfg Co Wood chipper
US2873923A (en) * 1956-07-16 1959-02-17 Columbia Veneer Company Wood rechipper
CH379107A (en) * 1960-08-15 1964-06-30 Alba Werkzeug Cutting tool
DE1211375B (en) * 1962-04-13 1966-02-24 Ind Companie Kleinewefers Kons Drum chippers for the production of wood chips
DE1282905B (en) * 1964-05-15 1968-11-14 Hombak Maschinenfab Kg Cutting machine with knife-bearing, cylindrical tool
US3375859A (en) * 1965-09-03 1968-04-02 Salem Equipment Inc Wood chipping apparatus
AT385231B (en) * 1986-01-17 1988-03-10 Starchl Maximilian DRUM CHOPPER
US4776375A (en) 1986-10-14 1988-10-11 Stanley Arasmith Winged cutting knife for producing wood chips or flakes
DE4126910C1 (en) * 1991-08-14 1992-09-24 Georg Weiss Gmbh, 8201 Schechen, De

Also Published As

Publication number Publication date
DE10221308B4 (en) 2007-04-12
EP1362679A3 (en) 2007-10-10
DE10221308A1 (en) 2003-12-11
ATE539865T1 (en) 2012-01-15
EP1362679A2 (en) 2003-11-19

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