Insert Tool and Method for Producing an Insert Tool

Abstract

An insert tool, in particular a chisel or a drill, has a tool head, with a shaft region in which a main body is arranged. The main body has a first hardness, and with a coating which has a second hardness that is greater than the first hardness. The coating has chromium carbide or consists of chromium carbide. Advantageously, the durability of the insert tool can be prolonged as a result.

Claims

1. An insert tool, having a tool head, having a shaft region in which a main body is arranged, wherein the main body has a first hardness, and having a coating which has a second hardness that is greater than the first hardness, wherein the coating has chromium carbide or consists of chromium carbide.

2. The insert tool according to claim 1, wherein the coating is arranged on the tool head and/or in the shaft region.

3. The insert tool according to claim 1, wherein the main body in the shaft region has a cylindrical lateral surface, at least in some sections.

4. The insert tool according to claim 1, wherein the coating has at least two coating elements which are arranged partly spaced apart from one another.

5. The insert tool according to claim 4, wherein the coating elements are spaced apart uniformly from one another.

6. The insert tool according to claim 1, wherein the coating extends rectilinearly, parallel or obliquely to a longitudinal axis of the insert tool and/or spirally around the longitudinal axis of the insert tool or is punctiform.

7. The insert tool according to claim 1, wherein in the region of the coating, an envelope curve of the coating has, at least partly, a greater radius than an envelope curve of the main body.

8. The insert tool according to claim 1, wherein the main body has a groove, which is arranged in the shaft region and/or on the tool head.

9. The insert tool according to claim 8, wherein the coating is arranged inside or outside the groove.

10. The insert tool according to claim 8, wherein a length of the coating element corresponds to between 15% and 85% of a length of the groove.

11. The insert tool according to claim 8, wherein the coating has an interruption which extends along the longitudinal axis of the insert tool.

12. A method for producing an insert tool, having a tool head, having a shaft region in which a main body is arranged, wherein the main body has a first hardness, and having a coating which has a second hardness that is greater than the first hardness, comprising: applying the coating via an LMD process.

13. The method for producing an insert tool according to claim 12, wherein the coating has multiple coating elements, which are produced successively via the LMD process.

14. The method for producing an insert tool according to claim 13, wherein the coating elements are applied counter to the feed direction of the insert tool, and wherein the start point of the coating process is arranged behind a tip of the insert tool.

15. The method for producing an insert tool according to claim 12, wherein the insert tool is heated before the coating process.

16. The insert tool of claim 1, wherein the insert tool is a chisel or a drill.

17. The insert tool according to claim 3, wherein the main body in the shaft region has a completely cylindrical lateral surface.

18. The insert tool according to claim 1, wherein the coating has at least two coating elements, which are arranged completely spaced apart from one another.

19. The insert tool according to claim 10, wherein a length of the coating element corresponds to between 40% and 60% of a length of the groove.

20. The method for producing an insert tool according to claim 13, wherein the coating has multiple coating elements which are produced beside one another or over one another, via the LMD process.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Further advantages can be gathered from the following drawings description. The drawings, the description and the claims contain numerous features in combination. Those skilled in the art will expediently also consider the features individually and combine them to form practical further combinations. Designations of features of different embodiments of the disclosure which substantially correspond are provided with the same number and with a letter identifying the embodiment.

[0020] FIG. 1a shows a first embodiment of an insert tool in a side view without a coating;

[0021] FIG. 1b shows the insert tool according to FIG. 1a with a coating;

[0022] FIG. 1c shows a cross section of the insert tool in the shaft region;

[0023] FIG. 2a shows a further embodiment of an insert tool with a coating;

[0024] FIG. 2b shows a cross section of the insert tool according to FIG. 2a in the shaft region;

[0025] FIG. 3a shows a further embodiment of an insert tool without a coating;

[0026] FIG. 3b shows the insert tool according to FIG. 3a with a coating;

[0027] FIG. 3c shows a cross-section of the insert tool according to FIG. 3b in the shaft region;

[0028] FIG. 4 shows a further embodiment of an insert tool with a coating;

[0029] FIG. 5a shows a further embodiment of an insert tool without a coating;

[0030] FIG. 5b shows the insert tool according to FIG. 5a with a coating;

[0031] FIG. 6a shows a further embodiment of an insert tool with a coating;

[0032] FIG. 6b shows a cross section through the insert tool according to FIG. 6a in the region of the tool head;

[0033] FIG. 7 shows a further embodiment of an insert tool with a coating;

[0034] FIG. 8 shows a further embodiment of an insert tool with a coating.

DETAILED DESCRIPTION

[0035] In FIG. 1a, a first embodiment of an insert tool 10 is shown in an uncoated state. By way of example, the insert tool 10 is formed as a pointed chisel. The insert tool 10a has a main body 12. The main body 12 consists of steel, which is preferably suitable for hardening. The insert tool 10 comprises a tool head 14, which is connected via a shaft region 16 to an insertion end 18.

[0036] The main body 12 extends from the insertion end 18 as far as the tool head 14 and, by way of example, is formed in one piece. It would also be conceivable for the main body 12 to consist of multiple pieces, which in particular are connected integrally to one another. By way of example, the insertion end 18 has an SDS-plus interface 20 and is provided to connect the insert tool 10 to a tool holder of a handheld power tool, not illustrated, preferably a hammer drill or a breaker. In the region of the insertion end 18, the insert tool 10 is enclosed when connected to the handheld power tool. The tool head 14 has a tip 22, which is substantially point-like. In the region of the tool head 14, the diameter of the insert tool 10, in particular that of the main body 12, decreases substantially continuously toward the tip 22.

[0037] The shaft region 16 of the insert tool 10 has a first subregion 24 and a second subregion 26. The first subregion 24 is arranged on the end of the shaft region 16 that faces away from the tool head 14. In the first subregion 24, the shaft region 16, in particular the main body 12, is substantially cylindrical. The cross section of the insert tool 10, in particular of the main body 12, is substantially constant in the first subregion 24. The second subregion 26 is arranged on the end of the shaft region 16 that faces the tool head 14. In the second subregion 26, the insert tool 10, in particular the main body 12, has grooves 28. The grooves 28 can be produced, for example, via forging or milling of the main body 12. By way of example, the insert tool 10 comprises four grooves 28. The grooves 28 extend along the longitudinal axis 30 of the insert tool 10. The grooves 28 can extend rectilinearly along the longitudinal axis 30, as shown, or spirally along the longitudinal axis 30. Preferably, the grooves 28 wind around the longitudinal axis 30 of the insert tool 10 in a range between 30° and 120°. By way of example, the grooves 28 each wind around the longitudinal axis 30 by about 90°. Alternatively, it would also be conceivable for the grooves 28 each to wind around the longitudinal axis 30 by more than 360°. The grooves 28 each begin at the same height in the second subregion 26 of the shaft region 16 and end at the same height in the region of the tool head 14.

[0038] Between two grooves 28 running beside each other there is arranged a land 32. The land 32 has a width 34 (see FIG. 1c) which is smaller than a width 36 of the grooves 28. The lands 32 follow the course of the grooves 28 and thus likewise extends spirally around the longitudinal axis 30.

[0039] In FIG. 1b, the insert tool 10 is shown in a coated state, wherein the insert tool 10 has a coating 38. The coating 38 has four coating elements 40. The coating elements 40 are each arranged in a groove 28. The coating elements 40, starting from the center of the grooves 28, extend toward the tool head 14, in particular to the tip 22 of the tool head 14. Alternatively, it would also be conceivable for the coating elements 40 to extend substantially in the region between the tip 22 and the grooves 28 and thus not reach or reach only insignificantly into the grooves 28.

[0040] The coating 38 or the coating elements 40 are applied via a laser metal deposition (LMD) process, in particular to an outer surface of the main body 12. The coating consists of a hard metal, which comprises a hard material and a metal matrix. By way of example, the hard material is formed as tungsten carbide and the metal matrix as NiBiSi, wherein the ratio is 60% by weight of hard material to 40% by weight of metal matrix. Advantageously, as a result it is possible to produce a coating 38 of which the hardness is greater than a hardness of the main body 12 of the insert tool 10. By means of the LMD process, the application of another hard metal as previously described is analogously conceivable. It is important to the disclosure that the hardness of the coating is greater than the hardness of the main body. If not otherwise described, the same coating is used by way of example in the following exemplary embodiments.

[0041] The size of the coating elements 40 is chosen in such a way that the coating 38 is produced via multiple individual method steps, in each of which a coating element 40 is applied. Advantageously, as a result the heating of the main body 12 during the LMD is reduced, in order to protect said main body. Following the application of a first coating element 40, the insert tool 10 is first rotated through 180° in order to apply a further coating element 40 to the opposite side. Then, for the third coating element 40, the insert tool is rotated by 90°, and rotated again by 180° for the fourth coating element 40. To implement a uniform coating without excessive heating of the insert tool 10, a period for the production of a coating element 40 is chosen in a range between 0 s and 10 s, preferably in a range between 1 and 3 s. Between the individual application steps or applications of individual coating elements 40, a pause step is carried out, in which the material can cool down. The pause step following the application of the first coating element can be carried out for a shorter time than the following pause steps. The duration of the pause steps lies in particular in a range below 1 min, preferably in a range between 10 s and 30 s.

[0042] In the region of the tool head 14, in particular in the region of the tip 22, the coating elements 40 merge into one another. Following the application of the coating 38, the tool head 14, in particular the tip 22, can be ground via a grinding method, in order to increase the removal performance of the insert tool 10.

[0043] In FIG. 1c, a cross section of the insert tool 10 in the second subregion 26 of the shaft region 16 is shown. The coating elements 40 are each arranged in a groove 28, in particular in a groove base 46 of the grooves 28. Alternatively or additionally, it would likewise be conceivable for the coating elements 40 to be at least partly arranged on one of the flanks 48 of the grooves 28. A maximum spacing 50 of the coating 38 from the longitudinal axis 30 is chosen to be smaller than a maximum spacing 52 of the land 32 from the longitudinal axis 30. As a result, the coating 38 is arranged completely in a space spanned by the lands 32.

[0044] Alternatively, it is also conceivable for multiple coating elements 40 to be arranged in each groove 28. By way of example, two coating elements can be arranged beside each other or three or more coating elements can also be arranged partly over one another. As a result, the individual coating elements can advantageously be smaller, which means that a shorter time is needed for each application of a coating element and, as a result, lower heating of the main body 12 is developed.

[0045] In FIGS. 2a and 2b, an alternative embodiment of the insert tool 10 is shown. As described previously, the insert tool 10a is formed as a pointed chisel and has a main body 12a with a tool head 14a having a tip 22a, a shaft region 16a and an insertion end (not illustrated). The shaft region 16a has a first cylindrical subregion 24a and a second subregion 26a, which comprises four grooves 28a. As opposed to the previous exemplary embodiment, the grooves 28a extend substantially rectilinearly along the longitudinal axis 30a of the insert tool 10a. The coating 38a of the insert tool 10a comprises four coating elements 40a, which are spaced apart completely from one another. The coating elements 40a are each arranged on a land 32a. The coating elements 40a consist of the same hard material as the previously described coating elements 40 and are likewise applied via an LMD process. The start point of the LMD process is approximately in the center of the land 32a, and the end point is in the region of the tool head 14a at a distance from the tip 22a, so that the tip 22a is not covered with the coating 38a.

[0046] In FIG. 2b, a cross section through the second subregion 26a of the insert tool 10a is shown. The coating elements 40a are applied completely to the lands 32a, in particular to a land spine 54a of the lands 32a. In addition, it would also be conceivable for further coating elements 40a to be arranged in the grooves 28a and/or for multiple coating elements 40a to be arranged on a land spine 54a. As a result of this arrangement, the maximum spacing of the lands 32a from the longitudinal axis 30a is smaller than the maximum spacing of the coating elements 40a from the longitudinal axis 30a.

[0047] In FIGS. 3a to 3c, a further alternative embodiment of the insert tool 10 is shown. In FIG. 3a, the insert tool 10b is shown in the uncoated state, and in the coated state in FIG. 3b. The insert tool 10b is, as previously described, formed as a pointed chisel and has a main body 12b with a tool head 14b having a tip 22b, a shaft region 16b and an insertion end 18b. As distinct from the preceding exemplary embodiments, the main body 12b has no different subregions in the shaft region 16b and is continuously cylindrical with a substantially constant external diameter.

[0048] The coating 38b has four coating elements 40b which, beginning in a region of the shaft region 16a facing the tool head 14b as far as the tool head 14b, have been applied by means of the previously described LMD process. The coating elements 40b extend rectilinearly and substantially parallel to one another along the longitudinal axis 30b of the insert tool 10b. The coating elements 40b end before the tip 22b, in order that the latter are not excessively heated during the LMD. In the shaft region 16b, the coating elements 40b have a substantially constant spacing from the longitudinal axis 30b. In the region of the tool head 14b, the spacing of the coating elements 40b to the longitudinal axis 30b, decreases continuously, in particular toward one another.

[0049] In FIG. 3c, a cross section through the insert tool 10b in the shaft region 16b is shown. The coating elements 40b form lands 32b, between which a groove 28b is arranged. As a result, grooves 28b and lands 32b, which prolong the service life of the insert tool 10b, can advantageously be produced by the coating elements 40b.

[0050] In FIG. 4, an alternative embodiment of the insert tool 10b is shown. As previously described, the insert tool 10c is formed as a pointed chisel and has a main body 12c with a tool head 14c having a tip 22c, a shaft region 16c and an insertion end 18c. The main body 12c itself has no grooves. The coating 38c has four coating elements 40c, which extend spirally around the longitudinal axis 30c of the insert tool 10c. By way of example, the coating elements 40c have a pitch such that they each wind once around the longitudinal axis 30c. The coating 38c and the coating elements 40c have been applied at a distance from one another by means of the LMD process. By way of example, the coating 38c is applied to the end of the shaft region 16c facing the tool head 14c and does not project into the tool head 14c. By means of the coating elements 40c, grooves 28c are formed in the interspaces.

[0051] In FIG. 5, a further alternative embodiment of the insert tool 10 is shown. The insert tool 10d is formed as a flat chisel and has a main body 12d with a tool head 14d, a shaft region 16d and an insertion end 18d. The shaft region 16d has a cylindrical cross section with a substantially constant external diameter. In the region of the tool head 14d, the external diameter of the main body 12d is enlarged. The tool head 14d has two side surfaces 58d substantially parallel to each other and a tip 22d, which is formed as a cutting edge 60d. The cutting edge 60d extends at right angles to the longitudinal axis 30d of the insert tool 10d. Furthermore, the insert tool 10d, in particular the main body 12d, has four grooves 28d. The grooves 28d are arranged on the tool head 14d and at a distance from the shaft region 16d. In particular, in each case two grooves 28d are arranged on one of the side surfaces 58d. The grooves 28d extend parallel to the longitudinal axis 30d of the insert tool. Between the grooves 28d and at the edge of the side surfaces 58d, there are formed lands 32d, which extend rectilinearly and parallel to the grooves 28d.

[0052] The coating 38d is applied to the main body 12d via an LMD process, as described previously, and, by way of example, has multiple coating elements 40d, which are applied in separate method steps. The coating 38d is arranged at the end of the tool head 14d that faces the tip 22d. In particular, the coating 38d has six coating elements 40d, which are each arranged on a land 32d and project into the tip 22d. Preferably, the coating elements 40d merge into one another in the region of the tip 22d, so that the tip 22d or the cutting edge 60d is covered substantially complete by the coating 38d.

[0053] In FIG. 6a, a further embodiment of the insert tool 10d formed as a flat chisel is shown. As described previously, the tool head 14e has a tip 22e formed as a cutting edge 60e and two side surfaces 58e parallel to each other, which are completely planar. The coating 38e consists of four coating elements 40e, wherein in each case two coating elements 40e are arranged on one of the two side surfaces 58e. The coating elements 40e extend rectilinearly and parallel to the longitudinal axis 30e of the insert tool 10e. In FIG. 6b, a cross section through the insert tool 10e in the region of the tool head 14e is shown. The coating elements 40e on the different side surfaces 58e are arranged opposite one another. However, it is also conceivable for the coating elements 40e to be arranged offset from one another on the different side surfaces 58e. Furthermore, it is conceivable that only one coating element 40e or three or more coating elements 40e are provided for each side surface 58e. In addition, it is likewise conceivable that a different number of coating elements 40e is arranged on the side surfaces 58e or that no coating element 40e is arranged on one of the side surfaces 58e.

[0054] In FIG. 7, a further embodiment of an insert tool 10f with a coating 38f is shown. The insert tool 10f has a main body 12f with a tool head 14f and a shaft region 16f The insert tool 10f is formed as a chisel. In the shaft region 16f, the main body 12f has a cylindrical cross-section with a substantially constant external diameter. In the region of the tool head 14f, the main body 12f likewise has a cylindrical cross-section with a substantially constant external diameter, wherein the external diameter of the main body 12f in the region of the tool head 14f is smaller than in the shaft region 16f. In the region of the tool head 14f, the main body 12f is rounded off toward the tip 22f.

[0055] The coating 38f has a multiplicity of coating elements 40f, which are applied by means of an LMD process in such a way that complete coating of the main body 12f in the region of the tool head 14f is achieved. The thickness of the coating 38f is chosen in such a way that it corresponds substantially to the difference of the external diameter of the shaft region 16f from the tool head 14f. To increase the removal performance of the chisel, the insert tool 10f can be machined by means of a grinding method after the application of the coating 38f.

[0056] In FIG. 8, a further alternative embodiment of the insert tool 10 is shown. As described previously, the insert tool 10g is formed as a pointed chisel and has a main body 12g with a tool head 14g having a tip 22g, a shaft region 16g and an insertion end (not illustrated). The shaft region 16g has a first cylindrical subregion (not illustrated) and a second subregion 26g, which comprises four grooves 28g. The grooves 28g are, by way of example, rectilinear.

[0057] The coating 38g was applied by means of an LMD process and consists of chromium carbide, for example, in this exemplary embodiment. By way of example, the coating 38g comprises one coating element 40g per groove 28g. The coating elements 40g extend substantially rectilinearly from the tip 22g of the insert tool 10 into the grooves 28g. All the coating elements 40g have an interruption 70g. The interruptions 70g, viewed axially, that is to say along the longitudinal axis 30g, have substantially the same length 72g. The length 72g of the interruption 70g corresponds to at least 5%, preferably at least 10%, preferably at least 25%, of a length 74g of the coating element 40g. By way of example, the length 72g of the interruption 70g is about 20% of the length 74g of the coating element 40g. In the region of the interruptions 70g, the insert tool 10g, viewed in the circumferential direction, has no coating 38g. As a result, in the region of the interruption 70g, the main body 12g of the insert tool 10g is advantageously not concomitantly heated by the LMD process. Advantageously, a start and end point of the interruptions 70g is arranged in such a way that it corresponds substantially to a start and end point of the grooves 28g.