TOOL WITH CUTTING EDGE AND METHOD OF MANUFACTURING IT
20200061747 ยท 2020-02-27
Assignee
- Hangzhou Great Star Industrial Co., Ltd. (Hangzhou City, Zhejiang Province, CN)
- Hangzhou Great Star Tools Co., Ltd. (Hangzhou City, Zhejiang Province, CN)
Inventors
Cpc classification
B25B7/22
PERFORMING OPERATIONS; TRANSPORTING
C23C24/10
CHEMISTRY; METALLURGY
C21D1/613
CHEMISTRY; METALLURGY
B23D65/00
PERFORMING OPERATIONS; TRANSPORTING
C21D9/18
CHEMISTRY; METALLURGY
B23K26/0006
PERFORMING OPERATIONS; TRANSPORTING
B23K26/34
PERFORMING OPERATIONS; TRANSPORTING
B23D29/02
PERFORMING OPERATIONS; TRANSPORTING
B23D61/00
PERFORMING OPERATIONS; TRANSPORTING
B23K31/025
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K26/34
PERFORMING OPERATIONS; TRANSPORTING
C21D9/18
CHEMISTRY; METALLURGY
Abstract
The present invention discloses a method of manufacturing a tool with a cutting edge comprising a substrate for supporting and a cladding layer for forming the cutting edge, and a transition zone connecting the substrate and the cladding layer; the method of manufacturing it includes: providing a first material used for forming the substrate and having a first side; providing a second material which is clad onto the first side by way of laser cladding to form the cladding layer, and forming a transition zone between the cladding layer and the substrate where the first material and the second material are metallurgically bonded. The tool obtained by adopting the manufacturing process according to the present invention combines the following advantages: good toughness of the cutter body, high hardness of the cutting edge, not easy breaking off of the cutter body and the cutting edge, and long service life.
Claims
1. A method of manufacturing a tool with a cutting edge, wherein: the tool with a cutting edge comprises a substrate for supporting and a cladding layer for forming the cutting edge, and a transition zone connecting the substrate and the cladding layer; the method of manufacturing comprises: providing a first material used for forming the substrate and having a first side; providing a second material which is clad onto the first side by way of laser cladding to form a cladding layer, and forming the transition zone between the cladding layer and the substrate where the first material and the second material are metallurgically bonded.
2. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the second material comprises at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, or comprises carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium; the second material further comprises nickel and/or cobalt.
3. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the second material comprises at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, or comprises carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium; the second material further comprises nickel and cobalt.
4. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the second material comprises at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and further comprises carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and further comprises nickel and/or cobalt.
5. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the second material comprises at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and further comprises carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and further comprises nickel and cobalt.
6. The method of manufacturing a tool with a cutting edge according to claim 2, wherein the carbon, the tungsten, the titanium, the chromium, and the vanadium are all powdered.
7. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the first material is quench-hardened steel.
8. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the first material comprises one or more of martensitic stainless steel, alloy structural steel, tool steel and spring steel.
9. The method of manufacturing a tool with a cutting edge according to claim 8, wherein the martensitic stainless steel is selected from the group consisting of 20Cr13, 30Cr13, 40Cr13, 50Cr15MoV, 68Cr17, 95Cr18 and 90Cr18MoV.
10. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the first material is selected from the group consisting of 50CrMo, 6CrW2Si, 60Si2Mn, 60Si2Cr, 60Si2CrV and 60CrMn.
11. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the laser cladding refers to melting, by using a laser device, the substances of the second material, which have a melting point lower than the temperature of a laser generated by the laser device at a set power of the laser device and at a set movement speed of the laser head, and carrying the substances having a melting point higher than the temperature of the laser to bond to the first side to form the cladding layer; and meanwhile the first side and the first material adjacent to the first side are melted under the action of the temperature of the laser, and are metallurgically bonded with the second material adjacent to the first side to form the transition zone.
12. The method of manufacturing a tool with a cutting edge according to claim 11, wherein the substances of the second material having a melting point higher than the temperature of the laser are dispersively distributed in the cladding layer.
13. The method of manufacturing a tool with a cutting edge according to claim 11, wherein the substances of the second material having a melting point higher than the temperature of the laser are evenly distributed in the cladding layer.
14. (canceled)
15. The method of manufacturing a tool with a cutting edge according to claim 11, wherein the power of the laser device is 1000 W, and the movement speed of the laser head during cladding is 2.0-15.0 mm/s.
16. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the method of manufacturing further comprises: vacuum quenching the tool blank after the laser cladding, the quenching temperature being 850-1250 C., and the quenching medium being quenching oil or inert gas; and vacuum tempering the tool blank after the quenching is completed, the tempering temperature being 200-600 C., and the soaking time being 2-8 hours.
17. The method of manufacturing a tool with a cutting edge according to claim 1, wherein the method of manufacturing further comprises: vacuum quenching the tool blank before the laser cladding, the quenching temperature being 850-1250 C., and quenching medium being quenching oil or inert gas; and vacuum tempering the tool blank after the quenching is completed, the tempering temperature being 200-600 C., and the soaking time being 2-8 hours.
18. (canceled)
19. A tool with a cutting edge, comprising a substrate for supporting and a cladding layer for forming the cutting edge, and a transition zone connecting the substrate and the cladding layer; the substrate is comprised of a first material, the first material being hardened stainless steel and having a first side; the cladding layer is comprised of a second material comprising at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, or comprises carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium; the second material further comprises nickel and/or cobalt; the transition zone is a region formed between the cladding layer and the substrate where the first material and the second material are metallurgically boned while the second material is clad onto the first side by way of laser cladding to form the cladding layer.
20. (canceled)
21. The tool with a cutting edge according to claim 19, wherein the cladding layer has a first edge for cutting or shearing, the first edge being smooth or serrated.
22. The tool with a cutting edge according to claim 19, wherein the tool with a cutting edge is manufactured by adopting the method of manufacturing a tool with a cutting edge according to claim 1.
23. The tool with a cutting edge according to claim 19, wherein the tool with a cutting edge is a cutter, a saw, an ax, aviation snips, or pliers with a cutting edge.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0043]
[0044]
[0045]
[0046]
[0047]
[0048]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0049] The tool with a cutting edge as defined in the present invention is used for cutting and/or shearing objects, includes a substrate, a cladding layer, and a transition zone connecting the substrate and the cladding layer. The substrate plays a role in supporting the cutting edge; the cutting edge can be used for cutting and/or shearing, and may be formed by grinding the blade edges after heat treatment of the cladding layer.
[0050]
[0051] It will be appreciated by those skilled in the art that the tool with a cutting edge according to the present invention may have a variety of shapes and configurations, for example, aviation snips as shown in
[0052] The first material is quench-hardened steel, and most preferred is steel having relatively high toughness, such as one or more of martensitic stainless steel, alloy structural steel, tool steel and spring steel. In a preferred embodiment, the martensitic stainless steel is selected from the group consisting of the standardized martensitic stainless steel with the following grades (Chinese grade): 20Cr13, 30Cr13, 40Cr13, 50Cr15MoV, 68Cr17, 95Cr18, 90Cr18MoV, etc. In another preferred embodiment, the first material is selected from the group consisting of 50CrMo, 6CrW2Si, 60Si2Mn, 60Si2Cr, 60Si2CrV and 60CrMn.
[0053] The second material has relatively high hardness and/or abrasion resistance. In a preferred embodiment, the second material is at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and the second material further includes nickel or cobalt. In yet another preferred embodiment, the second material is at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and the second material further includes nickel and cobalt. In a third preferred embodiment, the second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and the second material further includes nickel or cobalt. In a fourth preferred embodiment, the second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and the second material further includes nickel and cobalt. In a fifth preferred embodiment, the second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and further includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and further includes nickel or cobalt. In a sixth preferred embodiment, the second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and further includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and further includes nickel and cobalt. All of the substances of the above-mentioned second material are granular (they are powdered when they are fine granules).
[0054] Another aspect of the present invention provides a method of manufacturing a tool with a cutting edge as described above, and in a specific implementation, the method of manufacturing includes the steps of: 1) blanking the first material in accordance with the tool size to obtain a substrate with a first side; 2) cladding the second material onto the first side by way of laser cladding to form a cladding layer made of a second material, and a transition zone is formed between the cladding layer and the substrate where the first material and the second material are metallurgically bonded; 3) quenching and tempering; 4) grinding the blade edges; 5) assembling and packaging.
[0055] First, the first material is blanked and cut into a shape substantially corresponding to the substrate of the finished tool with a cutting edge. The cutting may be carried out using a wire cutting or a high-speed punch, or may be carried out using other cutting methods conventionally used in the art. The first material after cutting has a relatively flat first side.
[0056] Then, a laser cladding operation is performed using a CO2 gas laser device, a YAG solid laser device, a fiber laser device, or a DIODE semiconductor laser device. The power of the laser device is not less than 1000 W, and the movement speed of the laser head during cladding is 2.0-15.0 mm/s; and a layer of the second material is clad onto the first side of the first material after cutting to form a cladding layer, and a transition zone is formed between the cladding layer and the substrate which includes both the first material and the second material. In the transition zone, the first material and the second material are fused together, i.e., are metallurgically bonded.
[0057] Thereafter, the tool blank after the laser cladding is subjected to overall quenching and overall tempering. Both the quenching and tempering are performed in a vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium can be quenching oil and also can be inert gas. As a preferred option, the quenching medium is nitrogen. After the quenching is completed, the tool blank is vacuum tempered in the vacuum furnace, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0058] Finally, the tool blank after the quenching and tempering is ground in size and shape, especially grinding the cutting edge. The grinding may be carried out using the methods conventionally used in the art, for example by means of a grinder.
[0059] In another specific implementation of the method of manufacturing according to the present invention, it further includes quenching and tempering the substrate formed in step 1 before the laser cladding operation. The remaining steps are the same as those of the previous specific implementation and will not be described again here.
[0060] In yet another specific implementation of the method of manufacturing according to the present invention, it further includes obtaining a substrate with a first side which has a certain shape by hot forging after the first material is blanked in accordance with the tool size. The remaining steps are the same as those of the previous specific implementation and will not be described again here.
[0061] The metallographic structures of the substrate 1, the cladding layer 2, and the transition zone 3 obtained by the method of manufacturing according to the above-mentioned specific implementations or embodiments have substantially no holes (as shown in
[0062] After the laser cladding, quenching, and tempering treatments, the substrate has a hardness of 48-54 HRC, such hardness imparts good toughness to the substrate, making the substrate not easy to be broken. The cladding layer has a hardness of 60-70 HRC, which imparts good abrasion resistance to the cladding layer, making the service life of the cutting edge longer.
Embodiment 1 a Single-Edged Cutter
[0063] 1) Blanking the first material in accordance with the tool size to obtain a substrate with a first side. The first material is martensitic stainless steel. Then, a first quenching and a first tempering are performed in a vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0064] 2) Using a DIODE semiconductor laser device, and the power of the laser device is not less than 1000 W, the laser head performs a laser cladding operation with the movement speed of between 2.0 and 15.0 mm/s during cladding. The second material is clad onto the first side to form a cladding layer made of the second material, and a transition zone is formed between the cladding layer and the substrate where the first material and the second material are metallurgically bonded. The second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and the second material further includes both nickel and cobalt. The substances of the second material are all powdered.
[0065] 3) Performing a second quenching and a second tempering in the vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0066] 4) Grinding the blade edges.
[0067] 5) Assembling and packaging to obtain a single-edged cutter according to Embodiment 1.
[0068] The methods of manufacturing the single-edged cutters according to Embodiments 2 to 6 are the same as that of the single-edged cutter according to Embodiments 1 except for the differences listed in Table 1.
Table 1 Embodiments 2 to 6 of the Single-Edged Cutters
[0069]
TABLE-US-00001 TABLE 1 Differences from Embodiment 1 Embodiment 2 In Step 2), in addition to carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, the second material only includes nickel and does not include cobalt. Embodiment 3 In Step 2), in addition to carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, the second material only includes cobalt and does not include nickel. Embodiment 4 In Step 2), the second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and includes both nickel and cobalt. Embodiment 5 In Step 2), the second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and only includes nickel and does not include cobalt. Embodiment 6 In Step 2), the second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and only includes cobalt and does not include nickel.
Embodiment 7 a Single-Edged Cutter
[0070] 1) Blanking the first material in accordance with the tool size to obtain a substrate with a first side. The first material is martensitic stainless steel.
[0071] 2) Using a DIODE semiconductor laser device, the power of the laser device is not less than 1000 W, the laser head performs a laser cladding operation with the movement speed of between 2.0 and 15.0 mm/s during cladding. The second material is clad onto the first side to form a cladding layer made of the second material, and a transition zone is formed between the cladding layer and the substrate where the first material and the second material are metallurgically bonded. The second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and the second material further includes nickel and cobalt. The substances of the second material are all powdered.
[0072] 3) Performing quenching and tempering in a vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is quenching oil. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0073] 4) Grinding the blade edges.
[0074] 5) Assembling and packaging to obtain a single-edged cutter according to Embodiment 7
[0075] The methods of manufacturing the single-edged cutters according to Embodiments 8 to 12 are the same as that of the single-edged cutter according to Embodiments 7 except for the differences listed in Table 2.
Table 2 Embodiments 8 to 12 of the Single-Edged Cutters
[0076]
TABLE-US-00002 TABLE 2 Differences from Embodiment 7 Embodiment 8 In Step 2), the second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and includes both nickel and cobalt. Embodiment 9 In Step 2), the second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and only includes nickel and does not include cobalt. Embodiment 10 In step 2), the second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and only includes cobalt and does not include nickel. Embodiment 11 In Step 2), in addition to at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, the second material only includes nickel and does not include cobalt. Embodiment 12 In Step 2), in addition to at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, the second material only includes cobalt and does not include nickel.
Embodiment 13: Aviation Snips
[0077] 1) Blanking the first material in accordance with the tool size and hot forging to obtain a substrate with a first side. The first material is raw material such as alloy structural steel, tool steel, spring steel: bar material. Then, a first quenching and a first tempering are performed in a vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0078] 2) Using a DIODE semiconductor laser device, and the power of the laser device is not less than 1000 W, the laser head performs a laser cladding operation with the movement speed of between 2.0 and 15.0 mm/s during cladding. The second material is clad onto the first side to form a cladding layer made of the second material, and a transition zone is formed between the cladding layer and the substrate where the first material and the second material are metallurgically bonded. The second material includes at least one compound selected from the group consisting of tungsten carbide, titanium carbide, chromium carbide, vanadium carbide, aluminum oxide and zirconium oxide, and the second material further includes nickel and cobalt.
[0079] 3) Performing a second quenching and a second tempering in the vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0080] 4) Grinding the blade edges.
[0081] 5) Assembling and packaging to obtain the aviation snips according to Embodiment 13.
Embodiment 14 Pliers with a Cutting Edge
[0082] 1) Blanking the first material in accordance with the tool size and hot forging to obtain a substrate with a first side. The first material is alloy structural steel. Then, a first quenching and a first tempering are performed in a vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0083] 2) Using a CO2 gas laser device, the power of the laser device is not less than 1000 W, the laser head performs a laser cladding operation with the movement speed of between 2.0 and 15.0 mm/s during cladding. The second material is clad onto the first side to form a cladding layer made of the second material, and a transition zone is formed between the cladding layer and the substrate where the first material and the second material are metallurgically bonded. The second material includes carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, and the second material further includes nickel or cobalt.
[0084] 3) Performing a second quenching and a second tempering in the vacuum furnace. The quenching temperature is between 850 and 1250 C., and the quenching medium is nitrogen. The tempering is performed after the quenching is completed, the tempering temperature is between 200 and 600 C., and the soaking time is 2-8 hours.
[0085] 4) Grinding the blade edges.
[0086] 5) Assembling and packaging to obtain the pliers with a cutting edge of Embodiment 14.
[0087] Compared to the existing single-edged cutters, the test stroke is 20 mm, and 60 cycles are tested, the single-edged cutters with the blade manufactured using the methods according to the present invention have the sharpness and durability as shown in Table 3:
Table 3: Sharpness and Durability of Each Single-Edged Cutter
[0088]
TABLE-US-00003 TABLE 3 Serial number Item Sharpness (mm) Durability (mm) 1 Single-edged 56-66 300-333 cutters according to Embodiments 1 and 8 2 Single-edged 43-53 235-255 cutters according to Embodiments 2, 3, 9 and 10 3 Single-edged 50-60 242-273 cutters according to Embodiments 4 and 7 4 Single-edged 32-42 186-216 cutters according to Embodiments 5, 6, 11 and 12 5 Existing 30.7 109.3 single-edged cutter (50Cr15MoV whole cast blade) 6 Existing 24.3 77.6 single-edged cutter (30Cr13 whole cast blade)
[0089] It can be seen that both the sharpness and durability of the tools with a cutting edge according to embodiments of the present invention (with a single-edged cutter as an example) are improved relative to the blade of the existing single-edged cutter. Wherein, the use of both nickel and cobalt (for example, Embodiments 1, 4, 7 and 8) makes the sharpness increased by about 1 time and the durability increased by 2 to 3 times; the use of both nickel and cobalt and the use of carbon and at least one of the following four metal monomers: tungsten, titanium, chromium, vanadium, produce carbide during laser cladding (for example, Embodiments 1 and 8), the sharpness and durability thereof are the highest.
[0090] The 50Cr15MoV whole cast blade refers to a whole cast blade that the material of the substrate is 50Cr15MoV, and the blade is not subject to laser cladding process and has no cladding layer or transition layer, and the substrate is used for both supporting and forming the cutting edge. The 30Cr13 whole cast blade refers to a whole cast blade that the material of the substrate is 30Cr13, and the blade is not subject to laser cladding process and has no cladding layer or transition layer, and the substrate is used for both supporting and forming the cutting edge.
[0091] The preferred specific embodiments of the present invention have been described in detail above. It is to be understood that numerous modifications and variations can be made by those ordinary skilled in the art in accordance with the concepts of the present invention without any inventive effort. Hence, the technical solutions that can be derived by those skilled in the art according to the concepts of the present invention on the basis of the prior art through logical analysis, reasoning and limited experiments should be within the scope of protection defined by the claims.