JPH0335041B2 - - Google Patents
Info
- Publication number
- JPH0335041B2 JPH0335041B2 JP60146973A JP14697385A JPH0335041B2 JP H0335041 B2 JPH0335041 B2 JP H0335041B2 JP 60146973 A JP60146973 A JP 60146973A JP 14697385 A JP14697385 A JP 14697385A JP H0335041 B2 JPH0335041 B2 JP H0335041B2
- Authority
- JP
- Japan
- Prior art keywords
- cutting
- cutting edge
- metal
- composite
- layer
- 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.)
- Expired - Lifetime
Links
Landscapes
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
〔産業上の利用分野〕
この発明は、切刃が窒化ほう素(以下BNで示
す)基超高圧焼結材料で構成され、これを支持す
る支持材が炭化タングステン(以下WCで示す)
基超硬合金や、炭化チタン(以下TiCで示す)基
サーメツトなどのサーメツトで構成され、ダイス
鋼や高速度鋼などの高硬度鋼の連続切削は勿論の
こと、フライス切削や端面切削などの断続切削に
用いた場合にもすぐれた切削性能を発揮する複合
切削チツプに関するものである。
〔従来の技術〕
従来、立方晶BN(以下CBNで示す)や六方晶
BN(以下WBNで示す)を主成分とし、TiCや
TiN、さらにAl2O3などを結合相形成成分として
含有するBN基超高圧焼結材料で構成された切刃
を、これの焼結時にWC基超硬合金またはサーメ
ツトで構成された支持材に同時接合してなる複合
切削チツプを、高硬度鋼の連続切削に切削工具と
して用いた場合にすぐれた耐摩耗性を示すことは
良く知られるところである。
〔発明が解決しようとする問題点〕
しかし、上記の従来複合切削チツプは、上記の
ように高硬度鋼の連続切削にすぐれた切削性能を
発揮するものの、高硬度鋼の断続切削に用いた場
合には、切刃に欠けが発生し易く、信頼性不足の
ために実用に供することができないのが現状であ
る。
〔問題点を解決するための手段〕
そこで、本発明者等は、上述のような観点か
ら、刃先がBN基超高圧焼結材料からなり、一方
これの支持材がWC基超硬合金またはサーメツト
からなる上記の従来複合切削チツプに着目し、こ
の複合切削チツプを、高硬度鋼の連続切削は勿論
のこと、断続切削にも切削工具として使用するこ
とを可能とすべく研究を行なつた結果、
(a) 上記の従来複合切削チツプを断続切削に用い
た場合に、切刃に欠けが発生し易くなるのは、
支持材中に結合相形成成分として含有するCo
やNiなどの金属成分が切刃の焼結時に切刃中
に拡散溶浸し、このように金属成分が溶浸した
切刃においては、その切削加工時に、高温強度
が低下するばかりでなく、この溶浸した金属成
分と、結合相形成成分として含有するTiCや
TiN、さらにAl2O3などとの間には大きな熱膨
張差が生じるようになることから、切刃中に引
張り応力が生じ易くなることに原因があるもの
と考えられること。
(b) 上記の従来複合切削チツプの切刃と支持材の
間に、CoやNiなどの金属成分に対するぬれ性
がきわめて低く、かつ切刃の焼結時に容易に軟
化拡散現象を生じない、周期律表の4aおよび
5a族金属の窒化物または炭窒化物からなる高
融点化合物層を介在させると、焼結時における
支持材から切刃への前記金属成分の溶浸が著し
く抑制されるようになり、この結果溶浸した金
属成分が原因の欠けが切刃に発生しないように
なること。
(c) 上記高融点化合物層は、特に切刃を構成する
BN基超高圧焼結材料に対する接合強度が低い
が、この間に周期律表の4aおよび5a族金属か
らなる金属層を介在させると、この金属層は、
両方に対する接合強度が著しく高いので、切刃
と支持材との間には強固な接合が確保されるこ
と。
以上(a)〜(c)に示される知見を得たのである。
したがつて、この発明は、上記知見にもとづい
てなされたものであつて、
BN基超高圧焼結材料製切刃を、周期律表の4a
および5a族金属からなる金属層と、同4aおよび
5a族金属の窒化物または炭窒化物からなる高融
点化合物層の合計で2層以上の交互積層で構成さ
れ、かつ前記切刃に接して前記金属層が配置され
た平均層厚:0.1〜100μmの結合層を介して、WC
基超硬合金またはサーメツト製支持材に接合して
なる高い接合強度を有する複合切削チツプに特徴
を有するものである。
なお、この発明の複合切削チツプにおいて、結
合層の平均層厚を0.1〜100μmと限定したのは、
その厚さが0.1μm未満では上記作用に所望の効果
を確保することができず、一方その厚さが100μm
を越えるとチツプ自体の剛性が低下し、塑性変形
し易くなることから、その厚さを0.1〜100μmと
定めた。
〔実施例〕
つぎに、この発明の複合切削チツプを実施例に
より具体的に説明する。
それぞれ第1表に示される組成をもち、かつ直
径:10mm×厚さ:2mmの寸法をもつた支持材を用
意し、この支持材の切刃との接合面に通常の物理
気相蒸着法により、同じく第1表に示される組成
および厚さの結合層を形成し、前記結合層の形成
にあたつては、最上層、すなわち切刃と接する層
が金属層となるように交互積層配置し、一方切刃
として同じく第1表に示される組成をもち、かつ
直径:10mmφ×厚さ:2mmの寸法をもつた圧粉体
を用意し、ついで、前記切刃用圧粉体と支持材と
を前記結合層をはさんだ状態で、通常の超高圧高
温発生装置に装入し、温度:1200〜1400℃、圧
力:30〜60kbの範囲内の所定の条件で焼結する
ことによつて本発明複合切削チツプ1〜13をそれ
ぞれ製造した。
また、比較の目的で、結合層を形成しない以外
は、同一の条件で従来複合切削チツプ1,2をそ
れぞれ製造した。
ついで、これらの複合切削チツプをワイヤカツ
トにより4分割した状態で、WC基超硬合金台金
にろう付けし、研磨してSNP432の形状をもつた
切削工具を製造し、
被削材:高速度鋼(SKD−11、硬さ:HR
C60)、
切削速度:150m/min、
[Industrial Application Field] In this invention, the cutting edge is made of boron nitride (hereinafter referred to as BN)-based ultra-high pressure sintered material, and the supporting material that supports this is made of tungsten carbide (hereinafter referred to as WC).
It is composed of cermets such as base cemented carbide and titanium carbide (hereinafter referred to as TiC) base cermets, and can be used not only for continuous cutting of high-hardness steel such as die steel and high-speed steel, but also for intermittent cutting such as milling and end face cutting. This invention relates to a composite cutting chip that exhibits excellent cutting performance when used for cutting. [Conventional technology] Conventionally, cubic BN (hereinafter referred to as CBN) and hexagonal crystal
The main component is BN (hereinafter referred to as WBN), and TiC and
A cutting edge made of a BN-based ultra-high pressure sintered material containing TiN and Al 2 O 3 as binder phase forming components is sintered into a support material made of WC-based cemented carbide or cermet. It is well known that a composite cutting chip formed by simultaneous bonding exhibits excellent wear resistance when used as a cutting tool for continuous cutting of high-hardness steel. [Problems to be Solved by the Invention] However, although the above-mentioned conventional composite cutting chips exhibit excellent cutting performance in continuous cutting of high-hardness steel, they do not work well when used for interrupted cutting of high-hardness steel. Currently, the cutting edge tends to chip and cannot be put to practical use due to lack of reliability. [Means for Solving the Problems] Therefore, from the above-mentioned viewpoint, the present inventors proposed a method in which the cutting edge is made of a BN-based ultra-high pressure sintered material, while the supporting material is made of a WC-based cemented carbide or a cermet. We focused on the above-mentioned conventional composite cutting chip, which consists of , (a) When the above conventional composite cutting tip is used for interrupted cutting, the reason why chipping is likely to occur on the cutting edge is as follows.
Co contained as a binder phase forming component in the support material
Metal components such as Ni and Ni are diffused and infiltrated into the cutting edge during sintering of the cutting edge, and the high-temperature strength of the cutting edge infiltrated with metal components in this way is not only reduced during cutting, but also The infiltrated metal component and TiC contained as a binder phase forming component
This is thought to be due to the fact that a large difference in thermal expansion occurs between TiN and Al 2 O 3 , etc., making it easier for tensile stress to occur in the cutting edge. (b) Between the cutting edge and the supporting material of the conventional composite cutting chip mentioned above, the wettability to metal components such as Co and Ni is extremely low, and the softening and diffusion phenomenon does not easily occur during sintering of the cutting edge. Table 4a and
When a high melting point compound layer consisting of a nitride or carbonitride of a group 5a metal is interposed, the infiltration of the metal component from the support material to the cutting edge during sintering is significantly suppressed, resulting in a reduction in melting. Chips caused by immersed metal components will no longer occur on the cutting edge. (c) The high melting point compound layer particularly constitutes the cutting edge.
The bonding strength to the BN-based ultra-high pressure sintered material is low, but if a metal layer made of metals from groups 4a and 5a of the periodic table is interposed between them, this metal layer will
Since the bonding strength for both is extremely high, a strong bond is ensured between the cutting edge and the supporting material. The findings shown in (a) to (c) above were obtained. Therefore, the present invention has been made based on the above knowledge, and it provides a cutting blade made of a BN-based ultra-high pressure sintered material that meets the requirements of 4a of the periodic table.
and a metal layer consisting of a group 5a metal,
Consisting of a total of two or more alternating layers of high melting point compound layers consisting of nitrides or carbonitrides of group 5a metals, and the average layer thickness of the metal layers arranged in contact with the cutting edge: 0.1 to 100 μm Through the bonding layer of WC
It is characterized by a composite cutting chip that has high bonding strength and is bonded to a base cemented carbide or cermet support. In addition, in the composite cutting chip of this invention, the average layer thickness of the bonding layer is limited to 0.1 to 100 μm because
If the thickness is less than 0.1 μm, the desired effect cannot be achieved in the above action, while if the thickness is 100 μm
If the thickness exceeds this, the rigidity of the chip itself decreases and it becomes more susceptible to plastic deformation, so the thickness was set at 0.1 to 100 μm. [Example] Next, the composite cutting chip of the present invention will be specifically explained with reference to an example. A supporting material having the composition shown in Table 1 and having dimensions of 10 mm in diameter and 2 mm in thickness is prepared, and the surface of the supporting material to be joined to the cutting edge is coated by a normal physical vapor deposition method. , a bonding layer having the composition and thickness also shown in Table 1 is formed, and in forming the bonding layer, the uppermost layer, that is, the layer in contact with the cutting blade, is arranged in alternating layers so that it is a metal layer. On the other hand, a green compact having the same composition shown in Table 1 as a cutting blade and having dimensions of diameter: 10 mmφ x thickness: 2 mm is prepared, and then the green compact for the cutting blade and the supporting material are prepared. The bonding layer is placed in a normal ultra-high pressure and high temperature generator and sintered under predetermined conditions within the range of temperature: 1200-1400℃ and pressure: 30-60kb. Invention composite cutting chips 1 to 13 were manufactured, respectively. For comparison purposes, conventional composite cutting chips 1 and 2 were manufactured under the same conditions except that no bonding layer was formed. Next, these composite cutting chips were cut into four parts by wire cutting, brazed to a WC-based cemented carbide base metal, and polished to produce a cutting tool with the shape of SNP432. Work material: high speed steel. (SKD−11, hardness: H R
C60), cutting speed: 150m/min,
第1表に示される結果から、本発明複合切削チ
ツプ1〜13および従来複合切削チツプ1,2とも
高硬度鋼の連続切削にすぐれた耐摩耗性を示すも
のの、高硬度鋼の断続切削においては、本発明複
合切削チツプ1〜13がいずれもすぐれた切削性能
を示すのに対して、従来複合切削チツプ1,2は
いずれもほとんどの切刃に欠けが発生し、短時間
で使用寿命に至るものであつた。
上述のように、この発明の複合切削チツプは、
高硬度鋼の連続切削は勿論のこと、高硬度鋼の断
続切削に用いた場合にも切刃に欠けなどの発生な
く、著しく長期に亘つてすぐれた切削性能を発揮
し、きわめて信頼性の高いものである。
From the results shown in Table 1, although both the composite cutting chips 1 to 13 of the present invention and the conventional composite cutting chips 1 and 2 exhibit excellent wear resistance in continuous cutting of high-hardness steel, they show excellent wear resistance in interrupted cutting of high-hardness steel. Composite cutting chips 1 to 13 of the present invention all exhibit excellent cutting performance, whereas conventional composite cutting chips 1 and 2 all suffer from chipping on most of their cutting edges and reach the end of their service life in a short period of time. It was hot. As mentioned above, the composite cutting tip of the present invention
Not only continuous cutting of high-hardness steel, but also when used for interrupted cutting of high-hardness steel, there is no chipping of the cutting edge, and it exhibits excellent cutting performance over a long period of time, making it extremely reliable. It is something.
Claims (1)
律表の4aおよび5a族金属からなる金属層と、同
4aおよび5a族金属の窒化物または炭窒化物から
なる高融点化合物層の合計で2層以上の交互積層
で構成され、かつ前記切刃に接して前記金属層が
配置された平均層厚:0.1〜100μmの結合層を介
して、炭化タングステン基超硬合金またはサーメ
ツト製支持材に接合してなる高い接合強度を有す
る複合切削チツプ。1 A cutting blade made of a boron nitride-based ultra-high pressure sintered material is coated with a metal layer made of metals from groups 4a and 5a of the periodic table.
Consisting of two or more alternating layers of high melting point compound layers consisting of nitrides or carbonitrides of group 4a and 5a metals, and the average layer thickness of the metal layers arranged in contact with the cutting edge: 0.1 A composite cutting chip with high bonding strength that is bonded to a tungsten carbide-based cemented carbide or cermet support material through a ~100μm bonding layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14697385A JPS629808A (en) | 1985-07-04 | 1985-07-04 | Composite cutting tip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14697385A JPS629808A (en) | 1985-07-04 | 1985-07-04 | Composite cutting tip |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS629808A JPS629808A (en) | 1987-01-17 |
| JPH0335041B2 true JPH0335041B2 (en) | 1991-05-24 |
Family
ID=15419750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14697385A Granted JPS629808A (en) | 1985-07-04 | 1985-07-04 | Composite cutting tip |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS629808A (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5232318A (en) * | 1990-09-17 | 1993-08-03 | Kennametal Inc. | Coated cutting tools |
| US5266388A (en) * | 1990-09-17 | 1993-11-30 | Kennametal Inc. | Binder enriched coated cutting tool |
| KR100233154B1 (en) * | 1990-09-17 | 1999-12-01 | 디. 티. 코퍼 | Coated cutting tools |
| US5250367A (en) * | 1990-09-17 | 1993-10-05 | Kennametal Inc. | Binder enriched CVD and PVD coated cutting tool |
| US5325747A (en) * | 1990-09-17 | 1994-07-05 | Kennametal Inc. | Method of machining using coated cutting tools |
| CN104858458B (en) * | 2014-02-26 | 2018-09-14 | 三菱综合材料株式会社 | The surface-coated cutting tool of abnormal damage resistance and excellent in wear resistance |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6053721B2 (en) * | 1979-06-18 | 1985-11-27 | 三菱マテリアル株式会社 | Composite sintered parts for cutting tools |
-
1985
- 1985-07-04 JP JP14697385A patent/JPS629808A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS629808A (en) | 1987-01-17 |
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