WO1997041265A1 - Method for the manufacturing of cutting tools - Google Patents

Method for the manufacturing of cutting tools Download PDF

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Publication number
WO1997041265A1
WO1997041265A1 PCT/SE1997/000713 SE9700713W WO9741265A1 WO 1997041265 A1 WO1997041265 A1 WO 1997041265A1 SE 9700713 W SE9700713 W SE 9700713W WO 9741265 A1 WO9741265 A1 WO 9741265A1
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WO
WIPO (PCT)
Prior art keywords
insert
hardening
cutting
milling cutter
forming
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
Application number
PCT/SE1997/000713
Other languages
French (fr)
Inventor
Göran Pantzar
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sandvik AB
Original Assignee
Sandvik AB
Priority date (The priority date 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 date listed.)
Filing date
Publication date
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=20402381&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO1997041265(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Sandvik AB filed Critical Sandvik AB
Priority to EP97921065A priority Critical patent/EP0904417B1/en
Priority to AT97921065T priority patent/ATE225408T1/en
Priority to JP9538810A priority patent/JP2000509106A/en
Priority to DE69716060T priority patent/DE69716060T2/en
Publication of WO1997041265A1 publication Critical patent/WO1997041265A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/22Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for drills; for milling cutters; for machine cutting tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C5/00Milling-cutters
    • B23C5/16Milling-cutters characterised by physical features other than shape
    • B23C5/20Milling-cutters characterised by physical features other than shape with removable cutter bits or teeth or cutting inserts
    • B23C5/22Securing arrangements for bits or teeth or cutting inserts
    • B23C5/2204Securing arrangements for bits or teeth or cutting inserts with cutting inserts clamped against the walls of the recess in the cutter body by a clamping member acting upon the wall of a hole in the insert
    • B23C5/2208Securing arrangements for bits or teeth or cutting inserts with cutting inserts clamped against the walls of the recess in the cutter body by a clamping member acting upon the wall of a hole in the insert for plate-like cutting inserts 
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T407/00Cutters, for shaping
    • Y10T407/19Rotary cutting tool
    • Y10T407/1906Rotary cutting tool including holder [i.e., head] having seat for inserted tool
    • Y10T407/1932Rotary cutting tool including holder [i.e., head] having seat for inserted tool with means to fasten tool seat to holder

Definitions

  • the present invention relates to a new method for the manufacturing of cutting tools, such as milling cutter bodies with indexable cutting inserts, in accordance with claim 1. Also drills with seats for several cutting inserts of a hard material may come in question.
  • the tool When milling, the tool is given a rotating main motion at the same time as the workpiece or the tool performs a rectilinear or a rotating feeding motion.
  • a feeding along a curve may also take place in copying milling machines and in numerically operated milling machines.
  • the milling cutter body may consist of a face milling cutter, a corner milling cutter or a cylindrical milling cutter. These have in common that they usually carry a plurality of cutting inserts of a hard material, such as cemented carbide.
  • These cutting inserts are normally ofthe indexable type, i.e. they may be detached and turned or "indexed" when a cutting edge has been worn out and the operator wishes to turn a new cutting edge into the operative position.
  • the operative cutting edges of the cutting inserts describe substantially identical rotation orbits, i.e., in for instance a face cutting miller or a corner cutting miller they shall have substantially the same axial and radial positions in the milling cutter body.
  • this implies extraordinarily high precision requirements when manufacturing the insert seats in the milling cutter body. If for instance the axial positioning is unsatisfactory a so called axial throw arises, which causes a deteriorated surface smoothness.
  • R a values of maximally 1,5 ⁇ m, R z values of between 10 and 15 ⁇ m, R max of 10 ⁇ m and WT values of between 5 and 8 ⁇ m often occur.
  • the axial height difference between two cutting edges should not exceed a few ⁇ m.
  • a milling cutter body is manufactured by starting off from a piece of bar material of tool steel, such as, e.g., the one with the code designation 42CrMo4H in toughened condition (hardness 270-310 HB). Shape and form are established by cutting machining, such as turning of the basic shape and milling out ofthe seats for the cutting inserts. Further, the bottom support surfaces ofthe insert seats are provided with a central, threaded hole for the threadening ofthe locking screw ofthe cutting insert, or of a tubular shim screw for the fastening of a shim to the cutting insert. When the shaping ofthe milling cutter body is terminated, it is hardened.
  • the purpose of hardening is to give the steel (in this case normally the tool steel) a suitable hardness, either throughout or to a certain depth under the surface.
  • a suitable hardness either throughout or to a certain depth under the surface.
  • oil or air - depending on the composition - martensite is obtained.
  • the hardness ofthe martensite depends on the carbon content.
  • Milling cutter bodies are either locally hardened in the regions around the insert seats, or they are hardened throughout, normally to a hardness degree of between 40 and 52 H R C, preferably between 43 and 47 H R C. At this hardening and the subsequent oil cooling, it is unavoidable that yieldings and distortions in the material bring about minor shifts ofthe positions ofthe insert seats.
  • a primary object ofthe present invention is to form cutting positions in a milling cutter body with an increased position precision.
  • the method comprises hardening a steel body at least in regions thereof in which insert seats are to be disposed, and thereafter forming finished support surfaces of insert seats in the hardened regions.
  • the support surfaces are rough-formed prior to the hardening step and are finish-formed after the hardening step.
  • Figure 1 shows a milling cutter body in perspective, obliquely from above, on which the invention may be applied.
  • Figure 2 shows an exploded view of an insert seat obliquely from above, on which the invention may be applied.
  • Figure 3 shows a cross-section of an insert seat.
  • Figure 1 shows generally a milling cutter body 1 with six insert seats 2, all according to prior art.
  • each insert seat there is a mounted cutting insert 3 and a shim 4, which have been fastened in the insert seat by means of a locking screw 5.
  • a milled-out chip pocket 6 In front of each cutting insert, in the direction of rotation, there is a milled-out chip pocket 6.
  • an insert seat comprises a bottom support surface 7 with a threaded hole 8 intended for threadening of a shim screw 9.
  • the head of the shim screw clamps the shim 4.
  • this shim does not bear upon the side surfaces 10 and 1 1 , which thus are free surfaces.
  • a cutting insert 3 for instance a square indexable cutting insert, by means of a locking screw 5, which is threaded into the inner thread ofthe shim screw 9.
  • Two ofthe side surfaces 12 of the cutting insert bear upon the support surfaces 13 and 14, respectively, in the insert seat. Normally, these are angled to correspond to the positive orienteation ofthe side surfaces 12.
  • FIG 1 the rotation plane of the operative cutting corners is illustrated by a ring 15.
  • a ring 15 As mentioned above, it is an endeavoured aim that all operative cutting cornes lie in this plane, but according to known technique differences of up to 60 ⁇ m between two cutting inserts may occur. This depends greatly on fluctuations that arise at the hardening.
  • Figure 3 shows an insert seat with a cutting insert 3 and a shim 4.
  • the side surface 12 bears against the support surface 13 ofthe insert seat.
  • the eccentric distance d which for illustrative purposes is shown strongly exaggerated, designates the prestressing, which as known is there for forcing the cutting insert into the insert seat, against support surfaces 13, 14, so that a strong and stable bearing is obtained between the side surfaces ofthe cutting insert and the support surfaces ofthe insert seat.
  • a surprisingly better precision for the positioning ofthe insert seats is obtained, and thereby also a corresponding improvement ofthe positioning ofthe operative cutting edges, by the fact that the manufacturing ofthe insert seats is made after the hardening ofthe carrier or holder as such, i.e., in this case the milling cutter body.
  • the bar section is rough-formed (e.g. rough- turned) and thereafter it is neutral-hardened and annealed in accordance with a known technique to about 45 H R C.
  • the purpose ofthe annealing is to give to the steel a suitable hardness, whereby an improved toughness is also attained. Only thereafter are the insert seats and the chip pockets produced (e.g., by finish-turning). By rough-turning before the hardening, a sufficient hardening depth is accompished by means of practically any known cooling oil.
  • a further obtained advantage depends on the radically reduced radial throw (i.e. variations ofthe distance C), namely a considerably increased cutting insert life.
  • the wear is considerably reduced on the operative main cutting edges. This is of major importance when machining wearing materials, such as titanium and titanium-based materials.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Milling Processes (AREA)
  • Turning (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Lubricants (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

According to known technique, rotating cutting tools such as milling cutter bodies have been manufactured by first shaping them by cutting machining and then hardening them, entirely or partly. When hardening, small dislocations arise in the material, which for instance gives an axial throw between the insert seats in a milling cutter body. By hardening after the shaping of the tool, such as according to the invention, the tolerances have been reduced quite considerably.

Description

METHOD FOR THE MANUFACTURING OF CUTTING TOOLS
The present invention relates to a new method for the manufacturing of cutting tools, such as milling cutter bodies with indexable cutting inserts, in accordance with claim 1. Also drills with seats for several cutting inserts of a hard material may come in question.
When milling, the tool is given a rotating main motion at the same time as the workpiece or the tool performs a rectilinear or a rotating feeding motion. A feeding along a curve may also take place in copying milling machines and in numerically operated milling machines. E.g., the milling cutter body may consist of a face milling cutter, a corner milling cutter or a cylindrical milling cutter. These have in common that they usually carry a plurality of cutting inserts of a hard material, such as cemented carbide. These cutting inserts are normally ofthe indexable type, i.e. they may be detached and turned or "indexed" when a cutting edge has been worn out and the operator wishes to turn a new cutting edge into the operative position. To obtain a fine and smooth surface on the workpiece, it is necessary that the operative cutting edges of the cutting inserts describe substantially identical rotation orbits, i.e., in for instance a face cutting miller or a corner cutting miller they shall have substantially the same axial and radial positions in the milling cutter body. Inter alia, this implies extraordinarily high precision requirements when manufacturing the insert seats in the milling cutter body. If for instance the axial positioning is unsatisfactory a so called axial throw arises, which causes a deteriorated surface smoothness.
At several different face cutting miller applications, very high demands are set on the surface smoothness and Ra values of maximally 1,5 μm, Rz values of between 10 and 15 μm, Rmax of 10 μm and WT values of between 5 and 8 μm often occur. In order to at all achieve these surface criteria, it is necessary to adjust the cutting edges with a very high precision, both absolutely and relative to the other cutting edges in the milling cutter body. Thus, the axial height difference between two cutting edges should not exceed a few μm. Suitably, one should be able to position cutting edges within an axial tolerance range of 5 μm, and preferably even less. This has proved to be impossible
CONFIRMATION COPY because ofthe internal differences that occur between the positions in the milling cutter body ofthe insert seats, and thereby, also the cutting inserts.
According to known technique, a milling cutter body is manufactured by starting off from a piece of bar material of tool steel, such as, e.g., the one with the code designation 42CrMo4H in toughened condition (hardness 270-310 HB). Shape and form are established by cutting machining, such as turning of the basic shape and milling out ofthe seats for the cutting inserts. Further, the bottom support surfaces ofthe insert seats are provided with a central, threaded hole for the threadening ofthe locking screw ofthe cutting insert, or of a tubular shim screw for the fastening of a shim to the cutting insert. When the shaping ofthe milling cutter body is terminated, it is hardened. The purpose of hardening is to give the steel (in this case normally the tool steel) a suitable hardness, either throughout or to a certain depth under the surface. By heating to the austenitic range, followed by a fast cooling in water, oil or air - depending on the composition - martensite is obtained. The hardness ofthe martensite depends on the carbon content. Milling cutter bodies are either locally hardened in the regions around the insert seats, or they are hardened throughout, normally to a hardness degree of between 40 and 52 HRC, preferably between 43 and 47 HRC. At this hardening and the subsequent oil cooling, it is unavoidable that yieldings and distortions in the material bring about minor shifts ofthe positions ofthe insert seats. Thus, differences of 50 to 60 μm may for instance occur between the axial positions of two insert seats. Thereby, the positions ofthe cutting inserts will of course deviate to the same extent. In many cases, this may turn out to be unacceptable, and therefore, at some applications, a possibility must exist to finely adjust the cutting edges axially, for instance by fastening the cutting inserts in movable cassettes; see for instance SE-C-501 915 (Hessman et al.). Thus, a primary object ofthe present invention is to form cutting positions in a milling cutter body with an increased position precision.
A second object ofthe present invention is to reduce the axial throw between two insert seats in a milling cutter body to less than 20 μm, preferably 10 μm. Still another object ofthe present invention is to avoid complicated constructions with a plurality of different machine parts. These and further objects which are obvious for the skilled man have been possible to attain by manufacturing a milling cutter body according to the method as defined in claim 1. Further, these and further apparent objects have been attained by a method of manufacturing a rotary tool holder (such as a milling tool holder or a drill) having a plurality of insert seats, each seat including support surfaces adapted to engage a cutting insert. The method comprises hardening a steel body at least in regions thereof in which insert seats are to be disposed, and thereafter forming finished support surfaces of insert seats in the hardened regions. Preferably, the support surfaces are rough-formed prior to the hardening step and are finish-formed after the hardening step. For illustrative but non limiting purposes, the invention will now be described in more detail with reference to the appended drawings. These are herewith briefly presented:
Figure 1 shows a milling cutter body in perspective, obliquely from above, on which the invention may be applied. Figure 2 shows an exploded view of an insert seat obliquely from above, on which the invention may be applied.
Figure 3 shows a cross-section of an insert seat.
Figure 1 shows generally a milling cutter body 1 with six insert seats 2, all according to prior art. In each insert seat there is a mounted cutting insert 3 and a shim 4, which have been fastened in the insert seat by means of a locking screw 5. In front of each cutting insert, in the direction of rotation, there is a milled-out chip pocket 6.
The mounting per se of a cutting insert may be clearly seen in figure 2. Normally, an insert seat comprises a bottom support surface 7 with a threaded hole 8 intended for threadening of a shim screw 9. The head of the shim screw clamps the shim 4. Usually, this shim does not bear upon the side surfaces 10 and 1 1 , which thus are free surfaces. On top ofthe shim 4 is clamped a cutting insert 3, for instance a square indexable cutting insert, by means of a locking screw 5, which is threaded into the inner thread ofthe shim screw 9. Two ofthe side surfaces 12 of the cutting insert bear upon the support surfaces 13 and 14, respectively, in the insert seat. Normally, these are angled to correspond to the positive orienteation ofthe side surfaces 12. Further, in figure 1 the rotation plane of the operative cutting corners is illustrated by a ring 15. As mentioned above, it is an endeavoured aim that all operative cutting cornes lie in this plane, but according to known technique differences of up to 60 μm between two cutting inserts may occur. This depends greatly on fluctuations that arise at the hardening.
Figure 3 shows an insert seat with a cutting insert 3 and a shim 4. The side surface 12 bears against the support surface 13 ofthe insert seat. The eccentric distance d, which for illustrative purposes is shown strongly exaggerated, designates the prestressing, which as known is there for forcing the cutting insert into the insert seat, against support surfaces 13, 14, so that a strong and stable bearing is obtained between the side surfaces ofthe cutting insert and the support surfaces ofthe insert seat. According to the invention, a surprisingly better precision for the positioning ofthe insert seats is obtained, and thereby also a corresponding improvement ofthe positioning ofthe operative cutting edges, by the fact that the manufacturing ofthe insert seats is made after the hardening ofthe carrier or holder as such, i.e., in this case the milling cutter body. Thus, by milling out the bottom support surface 7 and the side support surfaces 13, 14 of the insert seat, and by drilling and threading the hole 8, after and not before the hardening ofthe milling cutter body, for instance the axial throw ofthe inserts seats has been reduced to less than 10 μm.
According to the method of the invention, one starts off from the same types of tool steel as in the prior art. First the bar section is rough-formed (e.g. rough- turned) and thereafter it is neutral-hardened and annealed in accordance with a known technique to about 45 HRC. As known, the purpose ofthe annealing is to give to the steel a suitable hardness, whereby an improved toughness is also attained. Only thereafter are the insert seats and the chip pockets produced (e.g., by finish-turning). By rough-turning before the hardening, a sufficient hardening depth is accompished by means of practically any known cooling oil.
As mentioned above, after the hardening has been performed, the manufacturing ofthe insert seats per se occurs. By means ofthe modern cutting tools of today, the inventor has succeeded in accomplishing the insert seats by in principle the same types of tools as hitherto used for unhardened steel. Thus, end mills and threading taps of solid cemented carbide and/or Coronite (registered trademark) are used. Thereby, surprisingly low axial and radial throws, respectively, have been obtained. The axial and radial deviations of the insert seats, i.e. the measures D and C, respectively, in figure 1 , have varied by less than 10 μm, between the lowest and the highest value.
A further obtained advantage depends on the radically reduced radial throw (i.e. variations ofthe distance C), namely a considerably increased cutting insert life. Thus, by the reduced radial throw, the wear is considerably reduced on the operative main cutting edges. This is of major importance when machining wearing materials, such as titanium and titanium-based materials.

Claims

Claims
1. Method for the manufacturing of cutting tools comprising a rotating holder with a plurality of insert seats, which are intended for accomodating a cutting insert of a hard material, the holder being made of steel which is partly hardened or through-hardened, characterized in that the hardening is made before the manufacturing of the insert seats.
2. Method according to claim 1, wherein the holder consists of a milling cutter body and each insert seat comprises a bottom support surface (7), at least two support or abutment surfaces (13, 14) and a threadened hole (8) in the bottom support surface, which hole is intended to accomodate a locking screw for the fastening of a cutting insert (3) or a shim screw for the fastening of a shim (4).
3. Method according to claim 1 or 2, wherein the milling cutter body is manufactured starting off from a piece of bar of tool steel, which is rough-turned to the desired shape ofthe intended milling cutter body before the hardening.
4. Method according to any of the preceding claims, wherein the hardened parts of tool steel have a hardness of between 40 and 52 HRC, preferably between 43 and
47 HRC.
5. A method for manufacturing a rotary tool holder having a plurality of insert seats, each seat including support surfaces adapted to engage a cutting insert, the method comprising the steps of:
A) hardening a steel body at least in regions thereof in which insert seats are to be disposed, and thereafter
B) forming finished support surfaces of insert seats in the hardened regions.
6. The method according to claim 5, further comprising, prior to step A, the step of rough- forming the support surfaces; and step B comprises finish-forming the support surfaces.
7. The method according to claim 5, wherein the rough-forming is performed by rough-turning, and the finish-forming is performed by finish-turning.
8. The method according to claim 5, wherein step A comprises hardening the entire steel body.
9. The method according to claim 5, wherein step A comprises hardening only a portion of a thickness ofthe body.
10. The method according to claim 5, wherein step A hardens the steel body to a hardness of from 40 to 52 HRC.
1 1. The method according to claim 5, wherein step A hardens the steel body to a hardness of from 43 to 47 HRC.
12. The method according to claim 1, wherein step B comprises forming, for each seat, a finished bottom support surface and at least two finished abutment support surfaces and a threaded hole in the bottom support surface.
PCT/SE1997/000713 1996-04-26 1997-04-28 Method for the manufacturing of cutting tools Ceased WO1997041265A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP97921065A EP0904417B1 (en) 1996-04-26 1997-04-28 Method for the manufacturing of cutting tools
AT97921065T ATE225408T1 (en) 1996-04-26 1997-04-28 METHOD FOR PRODUCING CUTTING TOOLS
JP9538810A JP2000509106A (en) 1996-04-26 1997-04-28 Manufacturing method of cutting tool
DE69716060T DE69716060T2 (en) 1996-04-26 1997-04-28 METHOD FOR PRODUCING CUTTING TOOLS

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9601625A SE506672C2 (en) 1996-04-26 1996-04-26 Method of manufacturing cutting tools
SE9601625-8 1996-04-26

Publications (1)

Publication Number Publication Date
WO1997041265A1 true WO1997041265A1 (en) 1997-11-06

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ID=20402381

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE1997/000713 Ceased WO1997041265A1 (en) 1996-04-26 1997-04-28 Method for the manufacturing of cutting tools

Country Status (8)

Country Link
US (1) US6016720A (en)
EP (1) EP0904417B1 (en)
JP (1) JP2000509106A (en)
AT (1) ATE225408T1 (en)
DE (1) DE69716060T2 (en)
ES (1) ES2184085T3 (en)
SE (1) SE506672C2 (en)
WO (1) WO1997041265A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006052194A1 (en) * 2004-11-10 2006-05-18 Sandvik Intellectual Property Ab Cutting tool for metal working an method for producing it

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE528820C2 (en) * 2004-12-14 2007-02-20 Seco Tools Ab Drilling tool with adjustable cassette
US20080240869A1 (en) * 2007-04-02 2008-10-02 Zibra, Llc Reverse tipped router bit
DE102008038272B4 (en) * 2008-08-18 2012-10-04 Leitz Gmbh & Co. Kg milling tool

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4108692A (en) * 1975-01-13 1978-08-22 Smith International, Inc. Rock bit roller cutter and method therefor
EP0303419A1 (en) * 1987-08-10 1989-02-15 Smith International, Inc. Process for laser hardsurfacing drill bit cones having hard cutter inserts
EP0555697A1 (en) * 1992-02-10 1993-08-18 Bayer Ag Process for the preparation of dialkyle carbonates

Family Cites Families (1)

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Publication number Priority date Publication date Assignee Title
JP2814760B2 (en) * 1991-02-15 1998-10-27 三菱マテリアル株式会社 Cutting tools

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4108692A (en) * 1975-01-13 1978-08-22 Smith International, Inc. Rock bit roller cutter and method therefor
EP0303419A1 (en) * 1987-08-10 1989-02-15 Smith International, Inc. Process for laser hardsurfacing drill bit cones having hard cutter inserts
EP0555697A1 (en) * 1992-02-10 1993-08-18 Bayer Ag Process for the preparation of dialkyle carbonates

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006052194A1 (en) * 2004-11-10 2006-05-18 Sandvik Intellectual Property Ab Cutting tool for metal working an method for producing it

Also Published As

Publication number Publication date
JP2000509106A (en) 2000-07-18
US6016720A (en) 2000-01-25
SE9601625D0 (en) 1996-04-26
EP0904417B1 (en) 2002-10-02
DE69716060D1 (en) 2002-11-07
DE69716060T2 (en) 2003-06-26
SE506672C2 (en) 1998-01-26
SE9601625L (en) 1997-10-27
ATE225408T1 (en) 2002-10-15
EP0904417A1 (en) 1999-03-31
ES2184085T3 (en) 2003-04-01

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