Cutting blade

11172611 · 2021-11-16

Assignee

Inventors

Cpc classification

International classification

Abstract

A cutting blade for vegetation is provided for example for use in a straw chopper or rotary mower. The blade includes a first base material and a plurality of hard surface beads of at least two different materials formed on at least one surface of the base material extending up to a cutting edge of the base material wherein the plurality of hard surface beads lie alternately side by side with touching side edges and one contains at least one different material of a different hardness relative to the other so that differential wear rates are created, and a wear profile is controlled. The softer material is burnt away at the edge by the cladding laser to form pockets so that the blade is serrated by the pockets when supplied with additional wear increasing the pockets to maintain the serrations.

Claims

1. A method for forming a blade for mounting on a rotor of a cutting machine for cutting vegetation comprising: defining on a blade body a cutting edge; the blade body being formed of a base material; applying at least one strip of cladding material to the blade body at the cutting edge so as to provide at least one part of the cutting edge which has the cladding material thereon; the cladding material having a resistance to wear greater than that of the base material; and applying heat energy to the cutting edge at a plurality of spaced locations along the cutting edge so as to remove away portions of the cutting edge to form a series of recessed pockets along the cutting edge at the locations.

2. The method according to claim 1 wherein the heat energy is applied after said at least one strip is applied.

3. The method according to claim 1 wherein the recessed pockets are formed at locations on said cutting edge spaced from said at least one strip.

4. The method according to claim 1 wherein the heat energy is applied at the locations to the base material.

5. The method according to claim 1 wherein the recessed pockets are wider than spaces therebetween.

6. The method according to claim 1 wherein the spaced locations are covered by second strips of a second cladding material having a resistance to wear less than said at least one strip of said cladding material.

7. The method according to claim 1 wherein said at least one strip is applied so as to extend from a position at the cutting edge in a direction transverse to the cutting edge.

8. The method according to claim 1 wherein said at least one strip comprises a plurality of separate strips.

9. The method according to claim 8 wherein said plurality of separate strips are parallel.

10. The method according to claim 1 wherein said at least one strip comprises a plurality of parallel strip portions extending from a position at the cutting edge in a direction inclined to a right angle to the cutting edge.

11. The method according to claim 10 wherein the strips are inclined at an angle in the range 45 to 75 degrees relative to the cutting edge.

12. The method according to claim 1 wherein the blade member has one flat surface and one chamfered surface converging toward the flat surface at the cutting edge and the cladding material is applied on the flat surface.

13. The method according to claim 12 wherein the chamfered surface is flat.

14. The method according to claim 1 wherein the cladding material comprises a bead of material which is fused to the base material by laser heating.

15. The method according to claim 1 wherein said at least one strip comprises a plurality of side by side parallel strips which have side edges of each strip immediately adjacent a side edge of a next adjacent strip so that no part of the base material is exposed at the edge.

16. The method according to claim 15 at least one of the strips of cladding material has greater resistance to wear than others of the strips.

17. The method according to claim 16 wherein the different wear characteristics of the strips is provided by providing said cladding material in different thicknesses.

18. The method according to claim 16 wherein the different wear characteristics of the strips is provided by providing at least two cladding materials of different wear characteristics.

19. The method according to claim 18 wherein said at least two cladding materials are applied as alternate parallel beads.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) One embodiment of the invention will now be described in conjunction with the accompanying drawings in which:

(2) FIG. 1 is a bottom plan view of a first embodiment of self-sharpening, self-serrating cutting blade according to the invention for use in for example a straw chopper.

(3) FIG. 2 is an isometric view from the bottom and outer end of the blade of FIG. 1 showing the beads of coating material applied to the bottom flat surface.

(4) FIG. 3 is an isometric view of an edge portion of the embodiment of FIGS. 1 and 2.

(5) FIG. 4 is a schematic illustration of a method according to the invention of manufacturing of the embodiments of FIGS. 3 and 4.

(6) FIG. 5 is an isometric view from the bottom and end of a second embodiment of blade.

(7) FIG. 6 is aside elevational view of a further embodiment of blade.

(8) FIGS. 7 to 10 are various views of a further embodiment of self-sharpening, self-serrating cutting blade according to the invention for use in the apparatus of FIGS. 1 to 5 where the blade has a serrated cutting edge.

(9) FIG. 11 is an isometric view of an edge portion of a yet further embodiment of blade similar to that of FIG. 3 according to the invention.

(10) In the drawings like characters of reference indicate corresponding parts in the different figures.

DETAILED DESCRIPTION

(11) The blade herein can be used for example in the straw chopper construction of the general type shown in the prior patents of Redekop Manufacturing which are U.S. Pat. Nos. 6,840,854; 5,232,405 and 5,482,508, the disclosures of which are incorporated herein by reference.

(12) The blades includes a plate 10 having a mounting hole 11 through the plate for mounting on a bushing carried on a pin of a rotor (not shown). While one mounting hole is shown allowing the blade to act as a flail pivotal around the axis of the mounting hole, other mounting arrangements can be provided.

(13) The blade 10 comprises a generally flat elongate blade of a base material 12 having a top surface 13, a bottom surface 14, two side edges 15, 16 and an end edge 17. The blade is typically stamped from uncoiled strip steel rolls but other manufacturing arrangements can be used.

(14) At least one side edge 15 or 16, and typically both side edges, is chamfered at edge 18 to form a cutting edge 19, 19A on the blade member 12 where the chamfered edge 18 is inclined from the top surface 13 to the sharp edge 19 in the bottom surface 14.

(15) In accordance with the present arrangement, a first cladding material 20 and a second cladding material 21 are applied to the blade member on the surface 14 in parallel side by side touching strips or beads so that each strip extends from an end 22 at a position intersecting the cutting edge 19 along the blade member in a direction transverse to the cutting edge to an end 23 on the surface spaced from the edge 58.

(16) Both cladding materials 20 and 21 are of a greater hardness than the first base material 12 and the first cladding material 20 is of greater hardness than the second cladding material 21.

(17) The first and second cladding materials are applied as a bead using a CNC control system shown schematically in FIG. 4 to accurately lay down and apply the material so that the first and second cladding materials 20, 21 are applied accurately as parallel beads with touching side edges 24. The beads are applied alternately along the bottom surface 14 opposite the cutting face 13 at the end 17 and extending partly along the surface 14.

(18) The first and second cladding materials 20, 21 alternately intersect the cutting edge 19 and lie directly side by side so that no part of the base material 12 is exposed between the materials 20, 21 at the cutting edge 19.

(19) In FIGS. 1 to 4, the chamfered surface 13 is flat and lies at an angle to the flat surface 14 so that the blade edge when initially formed is not serrated. However serrations are formed in the cladding process and continue to form during use as explained hereinafter and as the wear operates to wear back the edge of the less hard material 21 leaving the edges at the harder material 20 less worn and therefore more pronounced.

(20) The blade has a transverse flat outer edge 17 with the cutting edge 19, 19A extending from the outer edge 17 along one or both sides of the blade 10. The angle of the clad beads is in the range 45 to 75 degrees to the cutting edge 19 so that the parallel and touching beads 20, 21 are inclined from their ends 22 toward the end of the blade with the hole 11 and terminate at the end 23 of the beads.

(21) This forms an end section 25 of the blade 10 which is covered by the of the harder cladding material 20′ between the end edge 17 and the sides of the last portion of the second cladding material as indicated at 211. This section 25 shown in FIG. 1 is coated with the first harder material 20 so that this part is maintained at the lower wear condition defined by the harder material. From that point on, the materials 20, 21 alternate to form the side by side beads. The section 25 is thus defined in shape by the end edge 17, by a semicircular edge 26 and by side edges 27 and 28 which extend outwardly from the edge 26 to the outer side edges 15, 16. The side edges are inclined at the same angle as the beads which is inclined from the side edges 15, 16 at approximately 70 degrees along the blade 10 toward the end 111 with the hole 11. The semicircular edge 26 smoothly connects the inside ends 23 of the beads from one side of the blade to the other. As also shown in FIG. 1, the beads are longer at the end 17 of the blade 12 than at a position spaced from the end 17 of the blade member so that the edge 23 converges toward the edge 17 to join the semicircular edge 26. This reduces the required amount of coating material as the area at the end edge 17 is more heavily worn in the cutting action thus requiring a greater length of the cladding material than at the part of the blade remote from the edge 17 where less wear occurs.

(22) In FIG. 4 is shown the method for forming the blade described where the blade body 10 has the flat lower surface 14 to be clad facing upwardly and the upper surface 13, having the chamfered edges 18 facing downwardly.

(23) A supply 30 of a cladding material 31, typically in powder form, deposits a plurality of strips 20, 21 of the cladding material on to the blade body 10 so as to extend on the blade body in a direction transverse to the edge as previously described. Each strip 20, 21 is formed independently starting at the end 33 spaced from the edge 19, 18A and moves toward the edge. As the material is laid down, the material is heated by a guided laser beam from a controlled laser 34 under control of a CNC control system 35 which also controls the movement of the supply 30. Both the location, the power, and focal point of the laser is controlled so that the required amount of heat is applied to the material at the locations required. The strips 20, 21 thus extend between an end 36 of each strip at a position at the edge 19 and the end 33 of the strip remote from the edge 19.

(24) As shown in FIG. 3, the system lays down a series of alternate strips including the first set of strips 20 of a first hardness and the second set of strips 21 of a second hardness. The strips 20 and 21 are directly side by side as described above.

(25) As shown in FIG. 3 the energy applied by the laser 34 to the locations between each strip 20 and the next so as to burn away a portion of the edge 19 between the strips 20 to form a recessed pocket 37 at the edge in the area between the strips 20 defined by the strips 21.

(26) In a preferred step in the method, an increased power is applied to the laser while applying the strips 21. This has two effects. Firstly it vaporizes some carbide from the mixture so as to reduce the hardness of the strips 21. Secondly it increases the burn effect at the edge 19 to form the pocket 37. These effects can be controlled and obtained by changing many different control parameters including but not limited to controlling the power supplied to the laser, and/or the focal point of the laser and/or the speed of movement which controls the dwell time at the edge.

(27) Depending on the accuracy of the control, a smaller pocket may be formed at the edge 19 in the strips 20 but the recessed pockets 37 at the strips 21 are deeper than a portion of the edge 19 at the strips 20 which may be recessed to form a shallow pocket or may not be recessed at all. This forms a serrated edge as shown with cutting points 38 at the junction between the pocket 37 at the strip 21 and the remaining unburnt or less burnt part of the edge 19 at the strip 20.

(28) In FIG. 3, the locations between each strip 20 and the next is covered by a second strip 21 having a wear rate less than said first strips 20. This difference in wear can be obtained in the process by application of the same material using different control parameters, or more preferably it can be obtained as described above by using different cladding materials.

(29) Thus in FIG. 3, the strips 20 and 21 are directly side by side and at least one of the strips 20 of cladding material has greater resistance to wear than others 21 of the strips.

(30) This arrangement as shown in FIG. 3 avoids the complex expensive process for grinding of the chamfered edge with grooves or serrations so that the chamfered edge itself before cladding is flat. The serrations which assist in the cutting action are thus formed by the burned pockets 37 which are maintained as the blade wears by the difference in hardness at the strips 19 relative to the spaces therebetween. The heating action between the strips to burn the edge 19 can be provided by the laser or may be a separate operation after the cladding material in the strip 21 is applied. Alternatively another system can be used to form the pockets, which can be heating or burning or cutting or may use other processes.

(31) The effect obtained is that the thin strip of hard material at the bottom surface continues to form a cutting edge as it and the parent material above it are worn away. As the thin clad material at the edge extends along the full edge leaving no parent material forming the edge, the full length of the edge remains sharp. As the two types of the material wear differently so that the material in the valleys wears more quickly, this material wears away from the edge more quickly to maintain the structure of the valley.

(32) Thus in one aspect of the invention, the cutting blade is provided that includes at least one surface that is clad with at least two different types of laser clad material. One side of the cutting surface has a plurality of clad beads extending from the cutting edge transversely toward the center of the blade. The blade has a straight cutting edge. The laser clad material with the higher hardness and lowest wear rate is deposited to the edge of the cutting blade. The laser clad material with the lower hardness and higher wear rate is deposited away from the edge. The clad material is deposited in beads of alternating hardness. The blade parent material is of a third hardness which is lower than the two laser clad bead harness values.

(33) In the field, the blade parent material wears away quickly creating a self-sharpened cutting edge. Because alternating stripes of the laser clad beads started back from the edge 19 at the inner end 23, the parent material continues to wear back to the start of the laser clad bead at the end 23. This now self sharpens creating a serrated pocket. As foreign objects hit and chip the edge 19 or coatings 20 and 21 the blade re-sharpens and continues to cut well.

(34) Areas of the blade that are critical for cutting such as the end corners of the blade at the junction between the edges 19, 19A and the end 17 are coated with the harder laser clad material 20 to ensure blade wear is best controlled in these areas.

(35) This type of blade is desired by a farmer that harvests a lot of crop that is laying down on the ground or has a very abrasive soil environment. The blade when supplied with the pockets 37 already has the serrated edge which cuts best and further wear further increases the serrated shape thus further increasing cutting action. The blade is thus effective and inexpensive to produce in that it does not require convention grinding of the serrated shape.

(36) In a second embodiment shown in FIG. 6, the difference in the wear conditions between the two sets of beads on the cutting blade is provided by two different thicknesses of the laser clad material. In this case the same cladding material can be used but the materials also may be different. Thus in FIG. 6, one side of the cutting surface has a plurality of clad beads 201 and 211 extending from the cutting edge 19 transversely toward the center of the blade. The blade has a straight cutting edge. A laser clad material 201 with the thickest and thus lowest wear rate is deposited to the edge of the cutting blade. The laser clad material 211 with the thinnest and thus higher wear rate is deposited next to the thickest laser clad bead. The clad material is deposited in beads of alternating thickness. The blade parent material is of a third hardness with a higher wear rate than the two thicknesses of laser clad beads.

(37) In the field, the blade parent material at the pockets 37 continues to wear thus continuing to maintain a self-sharpened cutting edge. Because alternating strips of the laser clad beads were deposited in different thicknesses, the thinnest beads 211 wear away quicker and while wearing self sharpens creating a pocket. The beads 201 thus wear less and hence provide no pocket or a pocket of reduced depth so that the edge is serrated. As foreign objects hit and chip the edge or coating the blade re-sharpens and continues to cut well.

(38) Areas of the blade that are critical for cutting such as the end corners of the blade are coated with the thickest laser clad material to ensure blade wear is best controlled in these areas.

(39) As shown in FIG. 5 is shown a further embodiment similar to that of FIG. 1 where the alternate beads 59 and 60 of harder and softer cladding materials are arranged at an angle of inclination opposite to that of FIG. 1. That is the beads start at the edge 19, extend transversely of the edge 19 toward a center line of the bade and then incline toward the end 17 rather than the hole 11. This forms end portions 202 of the harder cladding material at the end 17 which are triangular in shape but again protect the important end location against wear.

(40) In a further embodiment shown in FIGS. 7 to 10, the blade includes a top surface 70 and a bottom surface 71. The top surface is chamfered at the side edges 72, 73 to form the cutting edges 74, 75 as before. However in this embodiment the chamfered surfaces 72 and 73 are serrated to form a series of serrations at spaced positions along the cutting edge. Each serration starts at the respective cutting edge 74 and extends at an angle to the cutting edge. Thus as shown in the top plan view of FIG. 11 and the cross-section of FIG. 12, each serration is formed by a cutting a valley 77 between each rib 76 which is triangular in cross-section to provide a top apex 78 with a valley 77 between each rib and the next.

(41) Thus the chamfered edge comprises a plurality of parallel ribs 76 with a valley 77 between each rib and the next. As shown in FIGS. 8 and 10, the beads 59 of the first harder material are located on the flat bottom surface 71 as a series of beads each at a position and angle aligned with a respective one of the ribs 76 and the second material of lower hardness is located on the flat bottom surface as a series of beads 60 each at a position and angle aligned with a respective one of the valleys 77. The angle of the serrations to the edge 74 can vary but the beads or strips of the first and second materials 59, 60 are inclined to the cutting edge 74 at the same angle as the serrations and perpendicular to the cutting edge of the serrations.

(42) In this way as the less hard material 60 wears in the valley, this continues to maintain the valley of the serration while the sharp ribs remain as ribs by the hardest material 59.

(43) In FIG. 11 the strips 91 are applied as in FIG. 14 but no intervening strips 92 are applied so that between the strips 91 the parent material of the blade body forms the section between the strips 91. This is possible in the situation where the parent material is sufficiently hard.

(44) As shown in FIG. 11, the locations between each strip and the next is defined by the base material. The application of the laser energy acts to cut the edge 83 to form the pocket 93. Whereas the edge 83 at the strips 91 has no pocket or a much smaller pocket.

(45) Thus as shown, the strips 91 are spaced each from the next at positions along the edge leaving a space between the strips 91. As described above, the strips 91 are of greater hardness than the strips 92 and than the body between the strips 91 as in FIG. 11. In the embodiment of FIG. 11, again the same laser can be used in the spaces simply for cutting the pockets 93.