JPS6112963B2 - - Google Patents
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- Publication number
- JPS6112963B2 JPS6112963B2 JP54144218A JP14421879A JPS6112963B2 JP S6112963 B2 JPS6112963 B2 JP S6112963B2 JP 54144218 A JP54144218 A JP 54144218A JP 14421879 A JP14421879 A JP 14421879A JP S6112963 B2 JPS6112963 B2 JP S6112963B2
- Authority
- JP
- Japan
- Prior art keywords
- cutting
- composite sintered
- cutting edge
- layer
- piece
- 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.)
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- Powder Metallurgy (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
【発明の詳細な説明】
この発明は、すぐれた靭性と耐熱耐摩耗性を有
し、特に難削材を切削するに際して、切削チツプ
の切刃部に取付けて使用するのに適した複合焼結
部片に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention provides a composite sintered material having excellent toughness and heat and wear resistance, and which is suitable for use by being attached to the cutting edge of a cutting tip, especially when cutting difficult-to-cut materials. It concerns pieces.
従来、一般にAlおよびAl合金、CuおよびCu合
金などの非鉄金属材料や、プラスチツク、ゴム、
黒鉛、およびセラミツクなどの非金属材料などの
穴あけ加工や高速仕上上切削などに、それぞれ等
しい肉厚のダイヤモンド基焼結材料の切刃層と、
炭化タングステン(以下WCで示す)基超硬合金
の保持層との2層複合体からなる等肉積層構造の
複合焼結部片を、切刃部にろう付けなどにより前
記ダイヤモンド基焼結材料の切刃層が上部に位置
せしめられた状態で取付けた切削チツプが使用さ
れている。 Traditionally, nonferrous metal materials such as Al and Al alloys, Cu and Cu alloys, plastics, rubber,
For drilling and high-speed finishing cutting of non-metallic materials such as graphite and ceramics, a cutting edge layer of diamond-based sintered material with the same wall thickness,
A composite sintered piece with an equal-thickness laminated structure consisting of a two-layer composite with a retaining layer of tungsten carbide (hereinafter referred to as WC)-based cemented carbide is attached to the cutting edge by brazing the diamond-based sintered material. A cutting tip is used which is mounted with the cutting edge layer positioned at the top.
しかし、上記従来複合焼結部片においては、こ
れを構成する保持層が切削チツプの切刃部に取付
けられた時に逃げ面に露出し、かつ十分満足する
靭性をもつものではなく、さらに、特に保持層に
おける切刃層との界面部には、焼結時にWC粒の
異常に細長い粒成長が発生し、これが原因で切刃
層と保持層との界面接合強度は劣つたものになつ
ていることから、これを切削に供した場合には所
望の満足する切削特性を示さないという問題があ
つた。 However, in the above-mentioned conventional composite sintered piece, the retaining layer constituting it is exposed on the flank when attached to the cutting edge of the cutting tip, and does not have sufficiently satisfactory toughness. At the interface between the cutting edge layer and the holding layer, abnormally elongated grain growth of WC grains occurs during sintering, and this causes the interfacial bonding strength between the cutting edge layer and the holding layer to deteriorate. Therefore, when this material was subjected to cutting, there was a problem in that it did not exhibit desired and satisfactory cutting characteristics.
本発明者等は、上述のような観点から、上記の
従来切削チツプの切刃用複合焼結部片のもつ問題
点を解決すべく研究を行なつた結果、前記保持層
形成材料を高速度鋼や合金工具鋼などのダイヤモ
ンド基焼結材料との接合性が良く、かつ高靭性を
有する特殊鋼で構成し、ただし、この場合切削チ
ツプの切刃部に取付けられた時に逃げ面となる部
分に前記特殊鋼が露出していると、切削時におけ
る逃げ面の耐熱耐摩耗性が著しく低下するように
なることから、前記逃げ面およびすくい面には特
殊鋼の保持層が露出しない、すなわちこれらの部
分をダイヤモンド基焼結材料の切刃層で構成する
偏肉積層構造にすると、この結果の複合焼結部片
は、前記切刃層と保持層との界面接合強度が著し
く高く、かつ靭性および耐熱耐摩耗性のすぐれた
ものとなるという知見を得たのである。 From the above-mentioned viewpoint, the present inventors conducted research to solve the problems of the above-mentioned conventional composite sintered pieces for cutting edges of cutting chips. It is made of special steel that has good bondability with diamond-based sintered materials such as steel and alloy tool steel, and has high toughness.However, in this case, the part that becomes the flank when attached to the cutting edge of the cutting tip If the special steel is exposed on the flank surface, the heat and wear resistance of the flank surface during cutting will be significantly reduced. When the section is made into an uneven thickness laminated structure consisting of a cutting edge layer of diamond-based sintered material, the resulting composite sintered piece has extremely high interfacial bonding strength between the cutting edge layer and the retaining layer, and has high toughness. They found that it has excellent heat and abrasion resistance.
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、切削チツプの切刃部に
取付けられる複合焼結部片がダイヤモンド基焼結
材料からなる切刃層と、特殊鋼からなる保持層と
の2層複合体で構成され、かつ切削チツプの切刃
部に取付けられた時に逃げ面およびすくい面とな
る部分がダイヤモンド基焼結材料の切刃層で占め
られる偏肉積層構造をもつことに特徴を有するも
のである。 Therefore, the present invention has been made based on the above knowledge, and provides that the composite sintered piece attached to the cutting edge of the cutting tip has a cutting edge layer made of a diamond-based sintered material and a cutting edge layer made of special steel. The uneven thickness laminated structure is composed of a two-layer composite with a retaining layer, and the portion that becomes the flank and rake face when attached to the cutting edge of a cutting tip is occupied by the cutting edge layer of diamond-based sintered material. It is characterized by having the following.
ついで、この発明の複合焼結部片を実施例によ
り説明する。 Next, the composite sintered piece of the present invention will be explained with reference to examples.
実施例 1
予め平均粒径4.5μmのFe粉末:73.5%、同3.0
μmのCr粉末:18%、同0.6μmのMo粉末:3
%、同0.7μmのW粉末:3%、同5.0μmのV粉
末:1%、および同0.3μmの炭素粉末:1.5%
(以上重量%)からなる混合粉末より、1.0ton/
cm2の圧力で直径12mmφ×厚さ3.0mmの寸法をも
ち、かつ第1図に斜視図で示される形状、すなわ
ちドリル刃の先端で切削成形された中心深さ3.0
mmの円錐状凹み1aを有する保持層形成のための
圧粉体片1を調製し、この圧粉体片1を、Zr製円
筒型薄肉容器内に装入し、ついでその上に平均粒
径0.5μmのダイヤモンド粉末:95容量%、同1.2
μmのCo粉末:5容量%からなる切刃層形成の
ための混合粉末:60mgを装入充填した後、この容
器全体を通常の超高圧高温発生装置に挿入し、圧
力:55kb、温度:1400℃、保時時間:30分の条
件で焼結し、焼結後、温度:1300℃まで徐冷した
後急冷し、最終的に温度:600℃に15分間保持し
て保持層に硬さを付与する処理を施すことによつ
て本発明複合焼結部片素材Tを製造した。Example 1 Fe powder with an average particle size of 4.5 μm: 73.5%, 3.0%
μm Cr powder: 18%, 0.6 μm Mo powder: 3
%, 0.7 μm W powder: 3%, 5.0 μm V powder: 1%, and 0.3 μm carbon powder: 1.5%
From a mixed powder consisting of (more than 1% by weight), 1.0ton/
It has dimensions of 12 mmφ in diameter x 3.0 mm in thickness under a pressure of cm 2 , and has a shape shown in the perspective view in Figure 1, that is, a center depth of 3.0 mm formed by cutting with the tip of the drill bit.
A compacted powder piece 1 for forming a retaining layer having a conical recess 1a of mm is prepared, this compacted powder piece 1 is charged into a cylindrical thin-walled container made of Zr, and the average particle diameter 0.5μm diamond powder: 95% by volume, 1.2%
After charging and filling 60mg of mixed powder for forming a cutting edge layer consisting of 5% by volume of μm Co powder, the entire container was inserted into a normal ultra-high pressure and high temperature generator, and the pressure: 55kb, temperature: 1400 ℃, holding time: 30 minutes, and after sintering, slowly cooled to 1300℃, then rapidly cooled, and finally held at 600℃ for 15 minutes to harden the retaining layer. The composite sintered piece material T of the present invention was manufactured by applying the following treatment.
この結果得られた本発明複合焼結部片素材T
は、直径12mmφ×厚さ2.5mmの寸法を有し、かつ
第2図に縦断面図で示されるように、ダイヤモン
ド基焼結材料の切刃層Aと、高速度鋼(JIS・
SKH−9に相当)の保持層Bとの偏肉積層複合
体からなるものであつた。 The resulting composite sintered piece material T of the present invention
has dimensions of 12 mmφ in diameter x 2.5 mm in thickness, and as shown in the longitudinal cross-sectional view in Fig. 2, the cutting edge layer A is made of diamond-based sintered material and high-speed steel (JIS/
It consisted of an uneven thickness laminated composite with a retaining layer B (corresponding to SKH-9).
また、比較の目的で、保持層形成のための圧粉
体片1′の形状を第3図に斜視図で示される円板
状とすると共に、その寸法を12mmφ×厚さ:2.0
mmとする以外は、上記本発明複合焼結部片素材T
の製造条件と同一の条件にて、第4図に縦断面図
で示される等肉積層構造をもち、かつ切刃層
A′の肉厚が0.5mmにして、保持層B′の肉厚が2.0mm
の比較複合焼結部片素材T′を製造した。 In addition, for the purpose of comparison, the shape of the compacted powder piece 1' for forming the retaining layer was assumed to be a disk shape as shown in the perspective view in Fig. 3, and its dimensions were 12 mmφ x thickness: 2.0 mm.
Except for mm, the above-mentioned composite sintered piece material T of the present invention
Under the same manufacturing conditions as the manufacturing conditions of
The wall thickness of A′ is 0.5 mm, and the wall thickness of retaining layer B′ is 2.0 mm.
A comparative composite sintered piece material T′ was produced.
さらに、比較の目的で、保持層形成のための混
合粉末の配合組成を、平均粒径:1.0μmのWC粉
末:94容量%、同1.5μmのCo粉末:6容量%と
する以外は、上記比較複合焼結部片素材T′の製
造条件と同一の条件にて、第4図に示される比較
複合焼結部片素材T′と同じ断面構造、すなわ
ち、ダイヤモンド基焼結材料の切刃層A″と、WC
基超硬合金の保持層B″との2層複合体からな
り、かつそれぞれの厚さが0.5および2.0mmの均一
厚さを有する等肉積層構造の従来複合焼結部片素
材T″を製造した。 Furthermore, for the purpose of comparison, the composition of the mixed powder for forming the retention layer was the same as above, except that the composition was 94% by volume of WC powder with an average particle size of 1.0 μm and 6% by volume of Co powder with an average particle size of 1.5 μm. Under the same manufacturing conditions as the comparative composite sintered piece material T', the same cross-sectional structure as the comparative composite sintered piece material T' shown in FIG. 4, that is, the cutting edge layer of the diamond-based sintered material A″ and WC
Manufacture a conventional composite sintered piece material T'' with an equal thickness laminated structure consisting of a two-layer composite with a retaining layer B'' of base cemented carbide, each having a uniform thickness of 0.5 and 2.0 mm. did.
つぎに、上記本発明複合焼結部片素材T、比較
複合焼結部片素材T′、および従来複合焼結部片
素材T″を、それぞれ第5図に斜視図で示される
ように均等四つ割りにして本発明複合焼結部片
P、比較複合焼結部片P′、および従来複合焼結部
片P″とした後、第6図に平面図で示されるよう
に、平面寸法:127mm□×厚さ:4.8mmのWC基超
硬合金製切削チツプ(スローアウエイチツプ)H
の四隅のうちの1隅の切刃部に、本発明複合焼結
部片Pにあつては、第7図に部分斜視図で示され
るように逃げ面fおよびすくい面Cがダイヤモン
ド基焼結材料の切刃層Aで占められ、一方比較複
合焼結部片P′および従来複合焼結部片P″にあつ
ては、第8図に同じく部分斜視図で示されるよう
に、ダイヤモンド基焼結材料の切刃層A′,A″を
上部に位置せしめた状態で、銀ろうを使用してろ
う付けし、さらにこれをバイトに取付け、つい
で、被削材:アルミニウム鋳鉄、切削速度:
200m/min、送り:0.1mm/rev、切込み:0.5
mm、切削油:使用の条件で穴あけ加工を行なう切
削試験に供し、使用寿命に到るまでの加工穴数お
よび加工穴の仕上げ面粗さを測定した。 Next, the above-mentioned composite sintered piece material T of the present invention, comparative composite sintered piece material T', and conventional composite sintered piece material T'' were each equally divided into four pieces as shown in the perspective view of FIG. After dividing into the present invention composite sintered piece P, comparative composite sintered piece P', and conventional composite sintered piece P'', as shown in the plan view in FIG. 6, the planar dimensions are: 127mm□×Thickness: 4.8mm WC-based cemented carbide cutting tip (throw-away tip) H
In the case of the composite sintered piece P of the present invention, the flank face f and the rake face C are diamond-based sintered, as shown in a partial perspective view in FIG. The cutting edge layer A of the material is occupied by the diamond-based sintered layer A, while the comparative composite sintered piece P′ and the conventional composite sintered piece P″ have diamond-based sintered With the cutting edge layers A′ and A″ of the bonding material positioned on top, solder is applied using silver solder, and this is further attached to the cutting tool. Then, workpiece material: aluminum cast iron, cutting speed:
200m/min, feed: 0.1mm/rev, depth of cut: 0.5
mm, cutting oil: A cutting test was performed in which holes were drilled under the conditions of use, and the number of holes machined and the finished surface roughness of the machined holes until the end of the service life were measured.
この結果本発明複合焼結部片Pは、2500個加工
後、正常摩耗により寿命に達し、また穴仕上げ面
粗さ:2Sのすぐれた切削特性を示すのに対し
て、逃げ面fに高速度鋼の保持層B′が露出する比
較複合焼結部片P′は、6000個で寿命に達すると共
に、穴仕上げ面粗さも7sと悪く、さらに従来複合
焼結部片P″は、チツピングの発生を伴い、20000
個で寿命に到り、その仕上げ面粗さも4sを示すも
のであつた。 As a result, the composite sintered piece P of the present invention reached the end of its service life due to normal wear after machining 2500 pieces, and also exhibited excellent cutting characteristics with a hole finish surface roughness of 2S, while the flank face f was cut at high speed. The comparison composite sintered piece P′, in which the steel retaining layer B′ is exposed, reached its lifespan after 6000 pieces and had a poor hole finish surface roughness of 7s, and the conventional composite sintered piece P″ also suffered from chipping. with 20000
It reached the end of its service life, and its finished surface roughness was 4s.
実施例 2
保持層形成のための混合粉末の配当割合を、平
均粒径4.0μmのFe粉末:84%、同5.0μmのCr
粉末:10%、同0.7μmのMo粉末:4%、同6.0
μmのV粉末:1%、および同0.3μmの炭素粉
末:1%(以上重量%)とすると共に、焼結後の
徐冷終了温度を1100℃とする以外は、上記実施例
1の本発明複合焼結部片Pの製造条件と同一の条
件にて、ダイヤモンド基焼結材料の切刃層と、合
金工具鋼(JIS・SKD11に相当)の保持層との2
層複合体からなり、かつ偏肉積層構造を有する本
発明複合焼結部片を製造した。Example 2 The distribution ratio of the mixed powder for forming the retention layer was 84% for Fe powder with an average particle size of 4.0 μm, and 84% for Cr powder with an average particle size of 5.0 μm.
Powder: 10%, 0.7 μm Mo powder: 4%, 6.0
The present invention of Example 1 above except that the V powder of μm: 1% and the carbon powder of 0.3 μm: 1% (more than 1% by weight), and the slow cooling end temperature after sintering was 1100 ° C. Under the same manufacturing conditions as the composite sintered piece P, a cutting layer of diamond-based sintered material and a retaining layer of alloy tool steel (equivalent to JIS/SKD11) were combined.
A composite sintered piece of the present invention consisting of a layer composite and having a laminated structure with uneven thickness was manufactured.
この結果得られた本発明複合焼結部片を実施例
1におけると同様に切削チツプに取付け、さらに
これをバイトに取付けて、被削材:Al−13%Si合
金、切削速度:600m/min、送り:0.1mm/rev、
切込み:0.5mmの条件で切削試験を行ない、逃げ
面摩耗巾が0.2mmに到るまでの切削時間を測定し
た。 The resulting composite sintered piece of the present invention was attached to a cutting tip in the same manner as in Example 1, and this was further attached to a cutting tool. Work material: Al-13%Si alloy, cutting speed: 600 m/min. , feed: 0.1mm/rev,
A cutting test was conducted under the condition that the depth of cut was 0.5 mm, and the cutting time until the flank wear width reached 0.2 mm was measured.
また、上記実施例1で製造した比較複合焼結部
片P′および従来複合焼結部片P″についても、同
一の条件にて切削試験を行なつた。 Further, cutting tests were also conducted on the comparative composite sintered piece P' produced in Example 1 and the conventional composite sintered piece P'' under the same conditions.
この結果本発明複合焼結部片は、145分の切削
時間で正常摩耗により所定摩耗量に達したのに対
して、比較複合焼結部片P′は18分で、また従来複
合焼結部片P″は15分でそれぞれ所定摩耗量に到
るものであつた。 As a result, the composite sintered piece of the present invention reached the specified amount of wear due to normal wear after a cutting time of 145 minutes, whereas the comparative composite sintered piece P′ reached the specified amount of wear in 18 minutes, and the conventional composite sintered piece Each piece P″ reached a predetermined amount of wear in 15 minutes.
上述のように、この発明の複合焼結部片は、保
持層がWC基超硬合金に比して著しくすぐれた靭
性並びにダイヤモンド基焼結材料との界面接合強
度が高い特殊鋼で構成され、かつ切刃層がダイヤ
モンド基焼結材料で構成され、さらに切削チツプ
の切刃部に取付けられた時に前記切刃層が、逃げ
面およびすくい面を占める偏肉積層構造をもつの
で、すぐれた靭性と耐熱耐摩耗性をもつようにな
り、したがつてこれを切削チツプの切刃部に取付
けて、特に難削材の切削に使用した場合には、き
わめてすぐれた切削性能を発揮するのである。 As mentioned above, in the composite sintered piece of the present invention, the retaining layer is made of special steel that has significantly superior toughness compared to WC-based cemented carbide and high interfacial bonding strength with diamond-based sintered material, In addition, the cutting edge layer is made of a diamond-based sintered material, and when attached to the cutting edge of the cutting tip, the cutting edge layer has a laminated structure with uneven thickness that occupies the flank and rake surfaces, so it has excellent toughness. Therefore, when it is attached to the cutting edge of a cutting chip and used for cutting difficult-to-cut materials, it exhibits extremely excellent cutting performance.
第1図および第3図は圧粉体片を示す斜視図、
第2図および第4図は複合焼結部片素材を示す縦
断面図、第5図は複合焼結部片の分割態様を示す
斜視図、第6図は複合焼結部片の切削チツプの切
刃部への取付け態様を示す平面図、第7図および
第8図は同じく複合焼結部片の切削チツプの切刃
部への取付け態様を示す部分斜視図である。
1,1′……圧粉体片、T……本発明複合焼結
部片素材、T′……比較複合焼結部片素材、T″…
…従来複合焼結部片素材、A,A′,A″……切刃
層、B,B′,B″……保持層、P……本発明複合
焼結部片、P′……比較複合焼結部片、P″……従
来複合焼結部片、H……切削チツプ、f……逃げ
面、C……すくい面。
FIGS. 1 and 3 are perspective views showing compacted powder pieces;
Figures 2 and 4 are longitudinal sectional views showing the composite sintered piece material, Figure 5 is a perspective view showing how the composite sintered piece is divided, and Figure 6 is a cutting tip of the composite sintered piece. FIGS. 7 and 8 are a plan view showing how the cutting tip of the composite sintered piece is attached to the cutting edge, and a partial perspective view showing how the cutting tip of the composite sintered piece is attached to the cutting edge. 1,1'...Powder compact piece, T...Composite sintered piece material of the present invention, T'...Comparative composite sintered piece material, T''...
...Conventional composite sintered piece material, A, A', A''... Cutting edge layer, B, B', B''... Holding layer, P... Composite sintered piece of the present invention, P'... Comparison Composite sintered piece, P″... conventional composite sintered piece, H... cutting tip, f... flank face, C... rake face.
Claims (1)
部片にして、この複合焼結部片がダイヤモンド基
焼結材料の切刃層と、特殊鋼の保持層との2層複
合体からなり、かつ切削チツプの切刃部に取付け
られた時に逃げ面およびすくい面となる部分が、
前記ダイヤモンド基焼結材料の切刃層で占められ
る偏肉積層構造をもつことを特徴とする切削チツ
プの切刃用複合焼結部片。1. A composite sintered piece to be attached to the cutting edge of a cutting tip, this composite sintered piece is composed of a two-layer composite of a cutting edge layer of diamond-based sintered material and a retaining layer of special steel, And the part that becomes the flank and rake face when attached to the cutting edge of the cutting tip,
A composite sintered piece for a cutting edge of a cutting tip, characterized in that it has an uneven thickness laminated structure occupied by the cutting edge layer of the diamond-based sintered material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14421879A JPS5669305A (en) | 1979-11-07 | 1979-11-07 | Composite sintered part piece for cutting edge of cutting tip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14421879A JPS5669305A (en) | 1979-11-07 | 1979-11-07 | Composite sintered part piece for cutting edge of cutting tip |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5669305A JPS5669305A (en) | 1981-06-10 |
| JPS6112963B2 true JPS6112963B2 (en) | 1986-04-11 |
Family
ID=15356981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14421879A Granted JPS5669305A (en) | 1979-11-07 | 1979-11-07 | Composite sintered part piece for cutting edge of cutting tip |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5669305A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0710443B2 (en) * | 1984-12-28 | 1995-02-08 | 京セラ株式会社 | Cutting tip |
| CN107649688B (en) * | 2017-08-21 | 2019-07-09 | 武汉速博酷新材料科技有限公司 | An easy-to-process diamond thermally conductive composite material and its preparation method and application |
-
1979
- 1979-11-07 JP JP14421879A patent/JPS5669305A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5669305A (en) | 1981-06-10 |
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