WO2007010601A1 - ドリル - Google Patents
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- Publication number
- WO2007010601A1 WO2007010601A1 PCT/JP2005/013319 JP2005013319W WO2007010601A1 WO 2007010601 A1 WO2007010601 A1 WO 2007010601A1 JP 2005013319 W JP2005013319 W JP 2005013319W WO 2007010601 A1 WO2007010601 A1 WO 2007010601A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- drill
- cutting edge
- less
- cutting
- range
- 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.)
- Ceased
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B51/00—Tools for drilling machines
- B23B51/02—Twist drills
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B35/00—Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
- C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
- B23B2224/24—Titanium aluminium nitride
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
- B23B2224/28—Titanium carbide
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2224/00—Materials of tools or workpieces composed of a compound including a metal
- B23B2224/32—Titanium carbide nitride (TiCN)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2228/00—Properties of materials of tools or workpieces, materials of tools or workpieces applied in a specific manner
- B23B2228/10—Coatings
- B23B2228/105—Coatings with specified thickness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2251/00—Details of tools for drilling machines
- B23B2251/14—Configuration of the cutting part, i.e. the main cutting edges
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B51/00—Tools for drilling machines
- B23B51/011—Micro drills
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T408/00—Cutting by use of rotating axially moving tool
- Y10T408/89—Tool or Tool with support
- Y10T408/909—Having peripherally spaced cutting edges
- Y10T408/9095—Having peripherally spaced cutting edges with axially extending relief channel
- Y10T408/9097—Spiral channel
Definitions
- the present invention relates to a drill, and more particularly to a drill capable of extending the tool life while ensuring machining efficiency.
- the wire cutting process is a process in which electricity is mainly applied to a brass wire and the electric discharge is generated.
- electricity is mainly applied to a brass wire and the electric discharge is generated.
- it is necessary to drill a starting hole in the work material that becomes a hole for the wire.
- a starting hole is formed by the discharge cage. Is drilled.
- the pilot hole was drilled with a 4mm drill, and then the contouring process was performed by wire cutting to ensure the hole accuracy.
- Japanese Patent Application Laid-Open No. 2003-266223 describes a technique related to a drill capable of drilling a starting hole even for a high-hardness work material.
- the axial length (groove length) of the chip discharge groove is set within the range of 2D or more and 5D or less with respect to the outer diameter D of the cutting edge, the rigidity of the drill is ensured. be able to.
- the drill can drill a starting hole in a high-hardness work material without breaking, and can improve machining efficiency as compared with electric discharge machining. As a whole, the processing efficiency of wire cutting can be improved.
- H7 tolerance hole finishing case by the combination of drill case and wire cut can be replaced by cutting only with the product of the present invention, and the processing time can be shortened.
- Open 2003—266223 paragraph [0021], Figure 2 etc.
- the present invention has been made to solve the above-described problems, and an object of the present invention is to provide a drill capable of extending the tool life while ensuring machining efficiency. Means for solving the problem
- the drill according to claim 1 has a drill body that is rotated around an axis, and a spiral or substantially straight line on the outer peripheral surface portion toward the tip force shank of the drill body. And a leading edge formed on a ridge line portion between the outer peripheral surface portion and a wall surface facing the rotation direction of the groove portion, and a cutting edge formed on a tip portion of the drill body
- the groove portion has a groove length, which is a dimension along the axis of the drill body, set in a range of 6D or more and 10D or less with respect to the outer diameter D of the cutting edge, and at least the
- the cutting edge is formed by coating the surface with a hard compound, the film thickness dimension of the hard compound is set to 1.0 m or less, and the cutting edge is composed of two pieces. Yes.
- the drill according to claim 2 is the drill according to claim 1, wherein the outer diameter D of the cutting edge is set to 1. Omm or less.
- the drill according to claim 3 is the drill according to claim 1 or 2, wherein the thickness dimension of the core thickness formed by the groove bottom of the groove is 0. It is set within the range of 35D or more and 0.55D or less.
- the drill according to claim 4 is the same as the drill according to any one of claims 1 to 3, and the hard compound applies the negative bias voltage to the cutting edge to apply the negative cutting voltage to the cutting edge.
- the surface roughening means is attached to the cutting blade by sputtering, and the surface roughening means has the bias voltage within the range of OkHz or more and 350 kHz or less. Apply periodically at the set frequency.
- the drill according to claim 5 is the drill according to claim 4, wherein the surface roughening means has a bias voltage set at a frequency set in a range of 150 kHz or more and 350 kHz or less.
- the negative voltage non-application time for each cycle is set in the range of 50 nsec or more and 20 OOnsec or less.
- the groove portion is a dimension along the axis of the drill body, and the groove length is set within a range of 6D or more and 10D or less with respect to the outer diameter D of the cutting edge.
- the groove length is smaller than 6D, the chip discharge performance is lowered, causing the drill to break due to chip clogging.
- the groove length is larger than 10D, the rigidity of the drill will be reduced, causing drill breakage.
- the film thickness dimension of the hard compound is set to 1.0 m or less.
- the cutting edge is rounded and the sharpness is lowered.
- the cutting performance of the chips is reduced, causing the drill to break due to chip clogging.
- the film thickness dimension of the hard compound is set to 1. O / zm or less, the sharpness is prevented from being lowered, the drill is prevented from being broken, and the life of the drill is extended. If you can, there is a positive effect.
- the leading edge strength is the thickness dimension in the axial direction view up to the heel as compared with the case where the cutting blade is composed of three blades. Can be secured. As a result, the rigidity of the drill can be secured, the drill can be prevented from being broken, and the life of the drill can be extended.
- the chip dischargeability and the drill rigidity can be improved synergistically.
- the life of the drill can be synergistically improved.
- the drill according to claim 2 in addition to the effect of the drill according to claim 1, it is constituted by a so-called small diameter drill in which the outer diameter D of the cutting edge is set to 1. Omm or less, Many small-diameter holes can be machined by preventing breakage of the drill.
- the film thickness dimension of the hard compound is set to 1.0 m or less.
- the film thickness dimension of the hard compound is relatively large with respect to the cutting edge, which greatly affects the sharpness.
- the film thickness dimension of the hard compound is larger than 1.0 m, the cutting edge is extremely rounded and the sharpness is remarkably lowered.
- the film thickness dimension of the hard compound is set to 1.0 m or less, there is an effect that breakage of the drill can be effectively prevented.
- the outer diameter D of the cutting edge is particularly set to 1. Omm or less. This makes it possible to effectively extend the life of the drill with respect to the small-diameter drill.
- the thickness of the core thickness formed by the groove bottom of the groove portion is the outer diameter D of the cutting edge. Is set within the range of 0.35D or more and 0.55D or less.
- the thickness dimension of the core thickness is smaller than 0.35D, the rigidity of the drill is lowered and the drill is easily broken.
- the thickness dimension of the core thickness is larger than 0.55D
- the groove portion becomes shallow, and chip discharge performance is lowered.
- chip welding is induced and drill breakage occurs.
- setting the thickness of the core thickness within the range of 0.35D or more and 0.55D or less can ensure the rigidity of the drill and chip evacuation, resulting in longer drill life. If you can achieve this, there is a positive effect.
- the hard compound has a negative bias voltage applied to the cutting edge of OkHz or more and 350kHz.
- the surface of the cutting edge is made to collide with positive ions and the surface is roughened, and then attached to the cutting edge by sputtering.
- the bias voltage is periodically changed, so that the adhesion strength of the hard compound to the cutting edge is improved, for example, excellent adhesion of 80 N or more at the critical load in the scratch test. There is an effect that strength can be obtained.
- the hard compound is attached to the cutting edge by a sputtering method, for example, the maximum diameter of fine particles called macropartical present on the surface of the hard composite is 10 m or less, and The percentage of the area occupied by macroparticals can be reduced to 10% or less. As a result, there is an effect that a relatively smooth coating surface can be obtained without processing such as polishing.
- the bias voltage when performing the surface roughening treatment is set within the range of 150 kHz or more and 350 kHz or less.
- the negative voltage non-application time for each cycle is set within the range of 50nsec or more and 2000nsec or less, so the adhesion strength of the hard compound to the cutting edge is remarkably improved. There is an effect that can be.
- FIG. 1 is a front view of a drill in an embodiment of the present invention.
- FIG. 2 is a front view of the drill.
- FIG. 3 is a diagram showing an etching process for roughening the surface of a drill
- (a) is a schematic diagram of a sputtering apparatus in the etching process
- (b) shows a time change of a bias voltage. It is a state diagram.
- FIG. 4 is a schematic view of a sputtering apparatus in a sputtering process.
- FIG. 5 is an enlarged photograph of a drill
- (a) is an enlarged photograph of the drill in the present embodiment
- (b) is an enlarged photograph of a conventional drill. It is a figure.
- FIG. 6 is a diagram showing test results of a first durability test.
- FIG. 7 A diagram showing the results of the endurance test, (a) showing the results of the second endurance test, and (b) showing the results of the third endurance test.
- FIG. 8 A diagram showing the test results of the efficiency test.
- (A) shows the test results of the fourth efficiency test.
- (B) is a diagram showing the test results of the fifth efficiency test, and
- (c) is a cross-sectional photograph of the caulking hole that is caulked using the drill of the present invention.
- (D) is a diagram showing a cross-sectional photograph of a caulking hole covered by electric discharge machining.
- FIG. 9 is a graph showing the results of a sixth efficiency test.
- FIG. 1 is a front view of a drill 1 according to an embodiment of the present invention.
- the axial lengths of the shank 2 and the drill body 3 are not shown.
- the drill 1 is a small-diameter cutting tool for drilling a starting hole, which is a hole for a wire when performing wire cutting mainly by rotational force transmitted from a processing machine (such as a drilling machine). As shown in FIG. 1, the shank 2 held by the processing machine and a drill body 3 for cutting a work material are mainly provided.
- the drill 1 is formed by coating the surface of Ti A1N, which is a hard composite, by a sputtering method, which will be described later, and the thickness of the TiAIN is within a range of 1. O / zm or less. Is set. Details will be described later (see Fig. 7 (a)).
- the drill 1 in the present embodiment is made of a cemented carbide that is sintered under pressure by adding cobalt as a binder to fine powder of tungsten carbide having an average particle size of 1.0 m or less. And the hardness of the drill 1 is secured.
- cermets that are not necessarily limited to this, ultra-high quality tool materials such as CBN (regular crystal boron nitride) sintered bodies may be used.
- powder high speed (sintered high speed steel), high speed Steel materials such as tool steel and alloy tool steel may be used.
- the shank 2 is a part held by the processing machine.
- the outer diameter is set larger than the outer diameter D of the cutting edge 5, and the shaft O and It is configured in a substantially parallel straight shape.
- the drill body 3 includes a groove portion 4 formed in a spiral shape on an outer peripheral surface portion thereof, a cutting edge 5 formed on a tip portion of the drill main body 3, a wall surface facing the rotation direction of the groove portion 4 and an outer peripheral surface portion.
- the leading edge 6 formed on the ridge line part and the flank 7 connected to the rear of the cutting edge 5 in the rotation direction are mainly provided, and the shank 2 is formed integrally with the connecting part 8.
- the groove 4 is a groove recessed in the outer peripheral surface of the drill body 3 in order to discharge chips.
- the leading edge 6 is disposed on the ridge line portion between the wall surface facing the rotation direction and the outer peripheral surface portion.
- the groove 4 in the present embodiment is formed in a spiral shape toward the tip side (left side in Fig. 1) force shank 2, but is not necessarily limited to this and is substantially parallel to the axis O. A straight line may be formed.
- the torsion angle which is an angle formed by the leading edge 6 and the straight line parallel to the axis O, is set within a range of 15 degrees or more and 35 degrees or less. Thereby, the rigidity of the drill body 3 and the chip dischargeability can be ensured.
- the groove length 1 which is a dimension along the axis O of the groove portion 4, is equal to the outer diameter D of the cutting edge 5.
- the cutting edge 5 is used for performing a drilling force of the work material by the rotational force of the processing machine.
- the drill body 3 is disposed at the tip portion.
- the force at which the tip angle of the cutting edge 5 is set to 120 degrees is not necessarily limited to this. If it is set within a range of 110 degrees or more and 140 degrees or less, good. As a result, the strength and biting property of the cutting edge 5 can be secured, the hole accuracy can be secured, and the drill 1 can have a long life.
- the relief surface 7 is a surface that is escaped in order to reduce friction during cutting, and is connected to the rear of the cutting edge 5 in the rotation direction.
- the connecting portion 8 is a portion that connects the shank 2 and the drill body 3, and is formed in a tapered shape that expands while being curved from the drill body 3 toward the shank 2.
- the connecting portion 8 in this embodiment is set to have a taper angle ⁇ of 20 degrees and an arc radius R of 10.
- FIG. 2 is a front end view of the drill 1.
- the margin 9 is for polishing the inner wall surface of the machining hole, and is continuously provided behind the cutting edge 5 in the rotation direction (clockwise in FIG. 2).
- the force composed of one margin 9 is not necessarily limited to this, and a second margin may be arranged behind the margin 9 in the rotational direction.
- the thickness dimension W of the core thickness formed by the groove bottom of the groove portion 4 can be set within the range of 0.35D or more and 0.55D or less with respect to the outer diameter D of the cutting edge 5. desirable.
- the thickness dimension W of the core thickness is smaller than 0.35D, the rigidity of the drill 1 is lowered and the drill 1 is easily broken.
- the thickness W of the core thickness is larger than 0.55D, the groove portion 4 becomes shallow, and the chip discharge performance decreases. As a result, chip welding is induced, causing drill 1 to break. From the above, by setting the thickness W of the core thickness within the range of 0.35D or more and 0.55D or less, it is possible to ensure the rigidity of the drill 1 and the chip dischargeability. Long life can be achieved.
- the thickness dimension W of the core thickness is variously changed depending on the hardness of the work material. For example, when processing a hard material exceeding 50 HRC, the rigidity of the drill 1 is increased. While it is desirable to set the thickness W of the core thickness within the range of not less than 0.45D and not more than 0.55D in order to ensure it, chip evacuation is required when processing 40HRC soft materials. To ensure the thickness, the thickness W of the core thickness is set within the range of 0.35D or more and 0.45D or less. It is desirable.
- the drill 1 in the present embodiment has the number of cutting edges 5 set to two, and the thickness dimension t of the blade thickness, which is the thickness from the leading edge 6 to the heel, is set. Secured. Details will be described later (see Fig. 7 (b)).
- FIG. 3 is a diagram showing an etching process for roughening the surface of the drill 1
- FIG. 3 (a) is a schematic diagram of the sputtering apparatus 30 in the etching process
- FIG. FIG. 6 is a state diagram showing a change in voltage over time.
- FIG. 4 is a schematic diagram of the sputtering apparatus 30 in the sputtering process.
- FIG. 5 is an enlarged photograph of drill 1
- FIG. 5 (a) is an enlarged photograph of drill 1 in the present embodiment
- FIG. 5 (b) is a conventional drill.
- a negative bias voltage is applied to the tool base material 20 disposed in the chamber 32 by a bias power source 34, thereby generating positive argon Ar +. Roughened by colliding with the tool base 20.
- the bias voltage is periodically changed by the controller 36 as shown in FIG. 3 (b). Specifically, a negative bias voltage of ⁇ 200V is applied in a pulse form at a frequency of 250 kHz, and a positive reverse voltage (for example, about + 20V) is applied to the negative voltage application time for each cycle.
- the pulse reverse time which is the negative voltage non-application time (reverse voltage application time)
- the surface roughening process according to claim 4 means an etching process.
- a hard compound is formed!
- a negative constant bias voltage for example, about 50V to about 60V
- a negative constant bias voltage for example, about 100 V
- argon ions Ar + collide with the target 38 and constituent materials such as TiAl and Ti are formed. Knock out.
- nitrogen gas or hydrocarbon gas CH
- TiAlN, TiCN, whose nitrogen atom N and carbon atom C were knocked out of the target 38, TiN or the like is deposited as a hard film on the surface of the tool base 20. It is also possible to apply a positive voltage to the tool base 20!
- (a) ((a-1), (a-2) and (a-3)) are the same as those in the above embodiment on a cemented carbide drill.
- (B) ((b-l), (b-2) and (b-3)) Shows the case where TiAIN is coated on the drill with the same shape by the arc ion plating method.
- (A-1) and (b-1), (a-2) and (b-2), and (a-3) and (b-3) are the same for each cutting edge. The picture was taken with a microscope and magnified 1000 times.
- the drill 1 of the present invention is compared with the conventional drill (see FIG. 5 (b)) by the arc ion plating method.
- an extremely smooth coating surface with few fine particles called surface macroparticulates can be obtained.
- the maximum diameter of the macropartical in the conventional drill is about 18 m and the occupied area is 20%
- the maximum diameter of the macroparticulate in the drill 1 of the present invention is about 6 ⁇ m
- the occupied area was 6%.
- the drill 1 in the present embodiment since the hard compound is adhered by the sputtering method, the maximum diameter of the macroparticulate existing on the surface of the hard composite is The ratio of the area occupied by the macropartical is 10% or less, and a smooth coating surface can be obtained. As a result, the surface roughness of the work material cut by the powerful drill 1 is improved, and a polishing process or the like for removing protrusions on the surface of the film caused by macropartical becomes unnecessary.
- a bias voltage of 200 V is applied to the tool base material 20 to perform etching (surface roughening treatment). Is applied periodically at a frequency of 250 kHz, and the non-application time (pulse reverse time) of the negative voltage per cycle is set to about 5000 nsec, so that the adhesion strength of the hard compound to the tool base material 20 is improved. Excellent adhesion strength of 1 OON or more can be obtained at the critical load in the scratch test, and dropout due to peeling or the like is suppressed, and durability that is practically satisfactory as a cutting tool can be obtained.
- the bias voltage in the present embodiment is a pulse, that is, a force configured to change in a rectangular shape, but is not necessarily limited to this, for example, other than a continuously changing waveform, etc. The shape can be changed.
- the negative voltage non-application time for each cycle is set in the range of 50 to 2000 nsec.
- first durability test to “third test”, respectively
- second durability test the same symbol as that of the drill 1 described above (for example, “D” for the outer diameter of the cutting edge 5) will be used.
- FIG. 6 is a diagram showing the test results of the first durability test.
- the first endurance test is a test to investigate the effect of groove length 1 on the durability of drill 1.
- the value of groove length 1 is variously changed within a certain range, and other cuttings are performed. Perform with constant conditions.
- the STEP processing is a processing in which the depth dimension of the processing hole is increased stepwise while the drill 1 is taken in and out and the chips in the groove portion 4 are discharged at the time of escape. It is. That is, since the chips are discharged through the groove 4 until the groove 4 is completely buried in the processing hole, the machining is performed at a stroke. After the groove 4 is completely buried in the processing hole, the chips are discharged by extracting the drill 1 from the processing hole. Then, when drill 1 is inserted into the drilled hole, the caulking hole is cut based on the STEP amount that has been preliminarily set, and drill 1 is again extracted from the drilled hole and chips are discharged. . The above operations are repeated until the target hole depth is reached.
- the detailed specifications of the first durability test are: Work material: SKD11 (60HRC), Machining depth: 5mm, Cutting blade outer diameter D: 0.5mm, Drill body axial dimension L: 14D Cutting speed V: 31.5 m / min, feed amount f: 0.02 mmZrev, STEP amount: 0.05 mm.
- Work material SKD11 (60HRC)
- Machining depth 5mm
- Cutting blade outer diameter D 0.5mm
- Drill body axial dimension L 14D
- Cutting speed V 31.5 m / min
- feed amount f 0.02 mmZrev
- STEP amount 0.05 mm.
- the groove length 1 when the groove length 1 is set within the range of 6D or more and 10D or less, the chip 1 can be discharged and the rigidity of the drill 1 can be secured to prevent the drill 1 from being broken. It can be said that it is possible to extend the service life.
- FIG. 7 is a diagram showing the test results of the endurance test
- FIG. 7 (a) is a diagram showing the test results of the second endurance test
- FIG. FIG. 5 is a diagram showing test results of a third endurance test.
- the second durability test is a test for examining the effect of the film thickness of the hard composite on the durability of drill 1.
- Fig. 7 (a) the film thickness dimension value of the hard compound is variously changed within a certain range, and other cutting conditions are kept constant.
- the durability of the drill 1 will be compared.
- the drill 1 in the present embodiment is composed of a small-diameter drill whose outer diameter D is set to 0.5 mm. It has a big effect. As a result, it is considered that the cutting performance of the chips is remarkably lowered, and the drill 1 is broken due to chip clogging.
- the film thickness dimension of the hard compound is set to 1.0 m or less, it is possible to prevent the chip 1 from being broken due to chip clogging by suppressing the cutting performance of the chip by cutting sharpness. It can be said that the life of the drill 1 can be effectively increased.
- the hard composite in the present embodiment may be a hard composite such as TiN, TiC, or TiCn, which is not necessarily limited to the force in which T1A1N is used. Further, the entire surface of the drill 1 is coated with a hard composite, but the surface of the cutting edge 5 is not necessarily limited to this, and it is sufficient that the surface of the drill 1 is coated.
- the third durability test is a test for examining the influence of the number of cutting edges 5 on the durability of the drill 1.
- the number of cutting edges 5, the thickness dimension W of the core thickness, and the blade Change the value of thickness dimension t within various ranges and make other cutting conditions constant.
- the detailed specifications of the third durability test are the same as the detailed specifications of the second durability test described above, except that the work material is fixed to SKD11 and the cutting speed V is fixed to 30 mZmin.
- the thickness thickness W of the core thickness is set to 0.19 mm
- the thickness dimension t of the blade thickness is set to 0.27 mm.
- the drill 1 could be processed without breaking. This is because by setting the number of cutting edges 5 to 2, the thickness t of the blade thickness can be secured, that is, the rigidity of the drill 1 can be secured and the life of the drill 1 can be extended. it is conceivable that.
- the number of cutting edges 5 is set to 2
- the thickness thickness W of the core thickness is set to 0.25 mm
- the thickness dimension t of the blade thickness is set to 0.36 mm.
- the No. 2 drill 1 has a larger thickness W of the core thickness and a thickness dimension t of the blade thickness than the No. 1 drill 1, so that the rigidity of the drill 1 is further secured. Therefore, it is considered that the drill 1 could have a longer life.
- the number of cutting edges 5 is set to 3
- the thickness thickness W of the core thickness is set to 0.19 mm
- the thickness dimension t of the blade thickness is set to 0.13 mm.
- the drill 1 broke when the number of drilled holes was nine, making subsequent machining difficult. This is probably because the thickness t of the blade thickness is secured by setting the number of the cutting blades 5 to 3, that is, the rigidity of the drill 1 cannot be secured, and the drill 1 is broken.
- the number of cutting edges 5 is set to 3
- the thickness thickness W of the core thickness is set to 0.25 mm
- the thickness dimension t of the blade thickness is set to 0.17 mm.
- the drill 1 broke when the number of drilled holes was one, making subsequent machining difficult. This is considered to be because the drill 1 could not be secured in the same way as the No. 3 drill 1, and the drill 1 was broken.
- the drill 1 of No. 4 has a shorter life span of the drill 1 compared to the drill 1 of No. 3 although the thickness dimension W of the core thickness and the thickness dimension t of the blade thickness are large. . This is considered an error due to experimental errors.
- FIG. 8 is a diagram showing the test results of the efficiency test
- FIG. 8 (a) is a diagram showing the test results of the fourth efficiency test
- FIG. FIG. 8 (a) is a diagram showing the test results of the fourth efficiency test
- FIG. 8 (c) is a diagram showing a cross-sectional photograph of a caulking hole that is caulked using the drill 1 of the present invention.
- FIG. 8 (d) is a view showing a cross-sectional photograph of the caulking hole that is caulked by the discharging force.
- the fourth and fifth efficiency tests are tests for examining the cutting efficiency of the drill 1 of the present invention.
- a starting hole having a processing depth of 15 mm is provided with a STEP force. Then, by calculating the time required for the starting hole force, the efficiency of the work using the drill 1 of the present invention and the efficiency of the discharge force are compared.
- the detailed introduction of the fifth efficiency test is the same as that in the above-mentioned fourth method except that the work material is HPM31, the feed amount f is fixed to 0.105 mm / rev, and the STEP amount is fixed to 0.15 mm.
- the details of the efficiency test are the same as the specifications.
- the time required for processing is 10 Os (seconds), whereas in the discharge casing, it is required for processing.
- the time spent was 200s.
- the cutting efficiency can be improved more than twice as compared with the case of electric discharge machining.
- the cutting hole cutting efficiency can be improved, and the wire cutting efficiency can be improved accordingly.
- the cross section of the Kaloe hole formed by using the drill 1 of the present invention is the cross section of the machined hole processed by electric discharge machining. Very smooth compared to.
- the surface roughness Ry of the drilled hole machined using the drill 1 of the present invention is 1. 130 m.
- the surface roughness Ry of the processed hole was 11. 349 / zm.
- the drill 1 of the present invention can be machined so that the surface of the machined hole is smooth as compared with electric discharge machining, that is, the machined hole can be machined with high accuracy. .
- FIG. 9 is a diagram showing the test results of the sixth efficiency test.
- the sixth efficiency test is a test for investigating the cutting efficiency of the drill 1 of the present invention. At a predetermined cutting speed V and feed rate f, a hole depth of 5 mm is drilled by STEP, and the drilling is performed. By calculating the time required for this, the efficiency of the cutting and wire cutting calorie using the drill 1 of the present invention is compared. The required accuracy of drilled holes is 0.5 mm in diameter.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Drilling Tools (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Description
Claims
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2007525468A JPWO2007010601A1 (ja) | 2005-07-20 | 2005-07-20 | ドリル |
| US11/988,576 US20080267726A1 (en) | 2005-07-20 | 2005-07-20 | Drill |
| DE112005003639T DE112005003639T5 (de) | 2005-07-20 | 2005-07-20 | Bohrer |
| PCT/JP2005/013319 WO2007010601A1 (ja) | 2005-07-20 | 2005-07-20 | ドリル |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/JP2005/013319 WO2007010601A1 (ja) | 2005-07-20 | 2005-07-20 | ドリル |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2007010601A1 true WO2007010601A1 (ja) | 2007-01-25 |
Family
ID=37668490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2005/013319 Ceased WO2007010601A1 (ja) | 2005-07-20 | 2005-07-20 | ドリル |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20080267726A1 (ja) |
| JP (1) | JPWO2007010601A1 (ja) |
| DE (1) | DE112005003639T5 (ja) |
| WO (1) | WO2007010601A1 (ja) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010264533A (ja) * | 2009-05-13 | 2010-11-25 | Osg Corp | 流体供給孔付き小径回転工具 |
| CN115090936A (zh) * | 2022-07-19 | 2022-09-23 | 厦门厦芝科技工具有限公司 | 一种侧刃带切削性能的钻头及优化工艺 |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE112005003529T5 (de) * | 2005-04-04 | 2008-05-15 | Osg Corporation, Toyokawa | Bohrer |
| JP2013022663A (ja) * | 2011-07-19 | 2013-02-04 | Mitsubishi Materials Corp | ドリル |
| US9272337B2 (en) * | 2012-08-17 | 2016-03-01 | Baker Hughes Incorporated | System and method for forming a bore in a workpiece |
| US20160052072A1 (en) * | 2014-08-22 | 2016-02-25 | Kennametal lnc. | Asymmetric end mills and applications thereof |
| JP6973069B2 (ja) * | 2015-02-23 | 2021-11-24 | 住友電気工業株式会社 | 回転工具 |
| US20190076932A1 (en) * | 2017-09-14 | 2019-03-14 | Spirit Aerosystems, Inc. | Apparatus and method for minimizing elongation in drilled holes |
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| JPS61260906A (ja) * | 1985-05-14 | 1986-11-19 | Sumitomo Electric Ind Ltd | 表面被覆超硬合金製ドリル |
| JPH01306111A (ja) * | 1988-06-03 | 1989-12-11 | Toshiba Tungaloy Co Ltd | プリント基板加工用の小径ドリル |
| JPH11333612A (ja) * | 1998-06-01 | 1999-12-07 | Toshiba Tungaloy Co Ltd | プリント配線板加工用の小径ドリル |
| JP2004332005A (ja) * | 2003-04-30 | 2004-11-25 | Kobe Steel Ltd | α型結晶構造主体のアルミナ皮膜の製造方法、α型結晶構造主体のアルミナ皮膜で被覆された部材およびその製造方法 |
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| JPS5226217B2 (ja) * | 1972-11-16 | 1977-07-13 | ||
| US4536108A (en) * | 1983-05-23 | 1985-08-20 | Federal-Mogul Corporation | Flexible microdrill |
| US4556347A (en) * | 1984-05-11 | 1985-12-03 | Lockheed Corporation | Split-point twist drill |
| JPS634211U (ja) * | 1986-06-23 | 1988-01-12 | ||
| US5143490A (en) * | 1991-07-26 | 1992-09-01 | Roto Zip Tool Corporation | Bit for cutting sheetrock |
| JPH09277108A (ja) * | 1996-02-14 | 1997-10-28 | Sumitomo Electric Ind Ltd | ドリル |
| SE518145C2 (sv) * | 1997-04-18 | 2002-09-03 | Sandvik Ab | Multiskiktbelagt skärverktyg |
| ES2201412T3 (es) * | 1997-05-29 | 2004-03-16 | Black & Decker Inc. | Broca helicoidal. |
| US6315504B1 (en) * | 1998-10-27 | 2001-11-13 | Nachi-Fujikoshi Corporation | Twist Drill |
| JP3720010B2 (ja) * | 2002-10-02 | 2005-11-24 | オーエスジー株式会社 | 深穴加工用ドリル |
| GB0320148D0 (en) * | 2003-08-28 | 2003-10-01 | Dormer Tools Sheffield Ltd | Partially coated drill tool |
| DE112005003529T5 (de) * | 2005-04-04 | 2008-05-15 | Osg Corporation, Toyokawa | Bohrer |
| DE102006042226A1 (de) * | 2006-09-06 | 2008-03-27 | Günther & Co. GmbH | Beschichteter Spiralbohrer |
| WO2009001681A1 (ja) * | 2007-06-22 | 2008-12-31 | Hitachi Tool Engineering, Ltd. | 深穴加工用小径ドリルおよび微細深穴加工方法 |
-
2005
- 2005-07-20 WO PCT/JP2005/013319 patent/WO2007010601A1/ja not_active Ceased
- 2005-07-20 DE DE112005003639T patent/DE112005003639T5/de not_active Withdrawn
- 2005-07-20 US US11/988,576 patent/US20080267726A1/en not_active Abandoned
- 2005-07-20 JP JP2007525468A patent/JPWO2007010601A1/ja active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61260906A (ja) * | 1985-05-14 | 1986-11-19 | Sumitomo Electric Ind Ltd | 表面被覆超硬合金製ドリル |
| JPH01306111A (ja) * | 1988-06-03 | 1989-12-11 | Toshiba Tungaloy Co Ltd | プリント基板加工用の小径ドリル |
| JPH11333612A (ja) * | 1998-06-01 | 1999-12-07 | Toshiba Tungaloy Co Ltd | プリント配線板加工用の小径ドリル |
| JP2004332005A (ja) * | 2003-04-30 | 2004-11-25 | Kobe Steel Ltd | α型結晶構造主体のアルミナ皮膜の製造方法、α型結晶構造主体のアルミナ皮膜で被覆された部材およびその製造方法 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010264533A (ja) * | 2009-05-13 | 2010-11-25 | Osg Corp | 流体供給孔付き小径回転工具 |
| CN115090936A (zh) * | 2022-07-19 | 2022-09-23 | 厦门厦芝科技工具有限公司 | 一种侧刃带切削性能的钻头及优化工艺 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20080267726A1 (en) | 2008-10-30 |
| JPWO2007010601A1 (ja) | 2009-01-29 |
| DE112005003639T5 (de) | 2008-05-29 |
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