JPH0123241B2 - - Google Patents
Info
- Publication number
- JPH0123241B2 JPH0123241B2 JP6195183A JP6195183A JPH0123241B2 JP H0123241 B2 JPH0123241 B2 JP H0123241B2 JP 6195183 A JP6195183 A JP 6195183A JP 6195183 A JP6195183 A JP 6195183A JP H0123241 B2 JPH0123241 B2 JP H0123241B2
- Authority
- JP
- Japan
- Prior art keywords
- composite
- cutting
- lower layer
- powder
- forming component
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24D—TOOLS FOR GRINDING, BUFFING OR SHARPENING
- B24D3/00—Physical features of abrasive bodies, or sheets, e.g. abrasive surfaces of special nature; Abrasive bodies or sheets characterised by their constituents
- B24D3/001—Physical features of abrasive bodies, or sheets, e.g. abrasive surfaces of special nature; Abrasive bodies or sheets characterised by their constituents the constituent being used as supporting member
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
この発明は、すぐれた耐摩耗性を有すると共
に、刃先部分にろう付けされる複合体の相互接合
強度が高く、したがつて安定した切削性能を長期
に亘つて発揮する複合切削チツプに関するもので
ある。
従来、一般に、分散相が立方晶窒化ほう素(以
下CBNで示す)で構成され、一方結合相がTiC、
TiCN、WC、およびAlNなどのうちの1種また
は2種以上、および/または鉄族金属などで構成
されたCBN基焼結材料の上層部分と、分散層が
WCで構成され、一方結合相がCoで構成された
WC基超硬合金の下層部分とからなる複合体を、
WC基超硬合金や高速度鋼などで構成されたチツ
プの刃先部分にろう付けしてなる複合切削チツプ
が実用に供されている。
しかし、上記の従来複合切削チツプにおいて
は、上記の複合体が、高温高圧、例えば温度:
1400℃、圧力:55Kbの条件下での焼結により製
造されるものであることから、この焼結時に下層
部分の結合相を構成するCoが上層部分に拡散し、
このCo拡散が原因で上層部分の耐摩耗性が劣化
するようになるばかりでなく、この複合切削チツ
プ自体が高価なものであるため、使用寿命後、再
研削を施して再使用しているが、Coの拡散量が
一定でないので、切削寿命のバラツキが大きく、
その管理に著しい不都合をきたすなどの問題点が
あるものであつた。
そこで、本発明者等は、上述のような観点か
ら、複合切削チツプにおける複合体の下層部分を
構成するCBN基焼結材料のもつすぐれた耐摩耗
性を損なうことのない、しかも複合切削チツプに
おける複合体の下層部分として適した特性を有す
る材料を開発すべく研究を行なつた結果、上記の
従来複合切削チツプにおける複合体の下層部分
を、WC基超硬合金に代つて、重量%で、
硬質分散相形成成分としての周期律表の4a、
5a、および6a族金属、さらにMg、Ca、Al、お
よびSiの炭化物、窒化物、酸化物、およびほう化
物、並びにこれらの2種以上の固溶体のうちの1
種または2種以上:10〜70%、
結合相形成成分としてのWまたはW―Mo合金
および不可避不純物:残り、
からなる組成を有するサーメツトで構成すると、
このサーメツトは、焼結時にCBN基焼結材料か
らなる上層部分への結合相形成成分の拡散がない
ので、前記上層部分のもつすぐれた耐摩耗性が損
なわれることがなく、しかも前記上層部分との接
合強度が高く、かつWC基超硬合金に比して一段
とすぐれた剛性および耐熱性を有していることか
ら、この結果の複合切削チツプは、すぐれた切削
性能をきわめて長期に亘つて安定的に発揮するよ
うになるという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、CBN基焼結材料の上
層部分と、サーメツトの下層部分との複合体を刃
先部分にろう付けしてなる複合切削チツプにおい
て、前記下層部分を、重量%で、
硬質分散相形成成分としての周期律表の4a、
5a、および6a族金属、さらにMg、Ca、Al、お
よびSiの炭化物、窒化物、酸化物、およびほう化
物、並びにこれらの2種以上の固溶体のうちの1
種または2種以上:10〜70%、
結合相形成成分としてのWまたはW―Mo合金
および不可避不純物:残り、
からなる組成を有するサーメツトで構成したこと
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の複合体の下
層部分において、硬質分散相形成成分の含有量を
10〜70%と限定したのは、その含有量が10%未満
では相対的に結合相形成成分の含有量が90%を越
えて多くなりすぎ、所望の耐摩耗性を確保するこ
とができず、一方70%を越えて含有させると、相
対的に結合相形成成分の含有量が30%未満となつ
てしまい、著しい靭性不足をきたすようになるこ
とから、その含有量を10〜70%と定めたのであ
る。
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。
実施例
複合体における上層部分形成用原料粉末とし
て、平均粒径:5μmを有するCBN粉末、同1μm
のTiN粉末、同1.5μmのTi0.5N0.5粉末、同2μmの
AlN粉末、同2.2μmのWC粉末、同1.2μmのCo粉
末を用意し、さらに同下層部分形成用原料粉末と
して、平均粒径:0.8μmのW粉末、同1.5μmの
(Ti0.6WJ0.4)C0.7N0.3粉末、同1.2μmのTiN粉末、
同0.5μmのAl2O3粉末、同0.4μmのMgO粉末、同
2.0μmのZrC粉末、同1.5μmのTaC粉末、同1.8μ
mのNbC粉末、および同0.4μmのCaO粉末を用意
し、これら原料粉末をそれぞれ第1表に示される
配合組成に配合し、いずれもボールミルにて72時
間混合した後、上層部分については、直径:8mm
φ×厚さ:1.5mmの寸法をもつた圧粉体にプレス
成形し、一方下層部分については、所定の圧力に
て成形した圧粉体を、同じく第1表に示される条
件で焼結した後、外径:8mmφ×厚さ:3mmの寸
法に研磨し、ついでこのように成形した上層部分
圧粉体と下層部分焼結体とを重ね合せた状態でス
テンレス鋼製容器に装入し、この容器を、圧力:
10-4mmHgの真空中、温度:1100℃に30分間保持
して、その内部を十分に脱ガスした後、ガードル
型超高圧高温装置に装入し、圧力媒体としてパイ
ロフエライトを使用し、また加熱体としては黒鉛
製円筒を用い、圧力:55Kb、温度:1400℃、保
持時間:30分の条件で焼結することによつて複合
体を成形し、引続いて、所定寸法に切出した前記
複合体を、ISO規格のSNGN432に則した形状を
もつWC基超硬合金製切削チツプの刃先部分にろ
う付けすることにより本発明複合切削チツプ1〜
8および従来複合切削チツプ1〜2を製造した。
つぎに、この結果得られた本発明複合切削チツ
プ1〜8および従来複合切削チツプ1〜2につい
て、
被削材:焼入れ鋼丸棒(材質:SKD―11、硬
さ:HRC60)、
切削速度:70m/mm、
送り :0.1mm/rev.、
切込み :0.2mm、
切削時間:15mm、
This invention relates to a composite cutting chip that has excellent wear resistance and has high mutual bonding strength of the composite material brazed to the cutting edge, and therefore exhibits stable cutting performance over a long period of time. . Conventionally, the dispersed phase was generally composed of cubic boron nitride (hereinafter referred to as CBN), while the binder phase was composed of TiC,
An upper layer of a CBN-based sintered material made of one or more of TiCN, WC, AlN, etc. and/or an iron group metal, and a dispersion layer.
Composed of WC, while the bonded phase was composed of Co
A composite consisting of a lower layer of WC-based cemented carbide,
Composite cutting tips made of WC-based cemented carbide, high-speed steel, etc., and brazed to the cutting edge are in practical use. However, in the above-mentioned conventional composite cutting tip, the above-mentioned composite is heated at high temperature and high pressure, e.g.
Since it is manufactured by sintering at 1400℃ and pressure: 55Kb, Co, which constitutes the binder phase in the lower layer, diffuses into the upper layer during sintering.
Not only does the wear resistance of the upper layer deteriorate due to this Co diffusion, but the composite cutting chip itself is expensive, so it is re-ground and reused after its useful life. , since the amount of Co diffusion is not constant, there is a large variation in cutting life.
There were problems such as significant inconvenience in its management. Therefore, from the above-mentioned viewpoint, the present inventors have developed a composite cutting chip that does not impair the excellent wear resistance of the CBN-based sintered material that constitutes the lower layer of the composite in the composite cutting chip. As a result of conducting research to develop a material with properties suitable for the lower layer of the composite, we replaced the lower layer of the composite in the conventional composite cutting tip with WC-based cemented carbide by weight%. 4a of the periodic table as a hard dispersed phase forming component,
5a and 6a group metals, as well as carbides, nitrides, oxides, and borides of Mg, Ca, Al, and Si, and one of solid solutions of two or more of these.
Species or two or more species: 10 to 70%, W or W-Mo alloy as a binder phase forming component, and unavoidable impurities: the remainder:
In this cermet, there is no diffusion of binder phase-forming components into the upper layer made of CBN-based sintered material during sintering, so the excellent wear resistance of the upper layer is not impaired, and moreover, the upper layer is The resulting composite cutting chip has high bonding strength and superior rigidity and heat resistance compared to WC-based cemented carbide, resulting in excellent cutting performance that is stable over an extremely long period of time. We have obtained the knowledge that it will become more effective. Therefore, the present invention has been made based on the above knowledge, and provides a composite cutting chip in which a composite of an upper layer of CBN-based sintered material and a lower layer of cermet is brazed to the cutting edge. 4a of the periodic table as a hard dispersed phase forming component,
5a and 6a group metals, as well as carbides, nitrides, oxides, and borides of Mg, Ca, Al, and Si, and one of solid solutions of two or more of these.
The present invention is characterized in that it is made of a cermet having a composition consisting of a species or two or more species: 10 to 70%, W or W--Mo alloy as a binder phase forming component, and the remainder: unavoidable impurities. In addition, in the lower layer part of the composite of the composite cutting tip of this invention, the content of the hard dispersed phase forming component is
The reason for limiting the content to 10 to 70% is that if the content is less than 10%, the content of the binder phase forming component will be relatively too high, exceeding 90%, and it will not be possible to secure the desired wear resistance. On the other hand, if the content exceeds 70%, the content of the binder phase forming component will be relatively less than 30%, resulting in a significant lack of toughness. It was established. Next, the composite cutting chip of the present invention will be specifically explained using examples. Example: CBN powder with an average particle size of 5 μm and 1 μm as raw material powder for forming the upper layer in a composite
TiN powder of 1.5 μm, Ti 0.5 N 0.5 powder of 2 μm
AlN powder, 2.2 μm WC powder, and 1.2 μm Co powder were prepared, and as raw material powders for forming the lower layer, W powder with an average particle size of 0.8 μm, and (Ti 0.6 WJ 0.4 ) with an average particle size of 1.5 μm. C 0.7 N 0.3 powder, 1.2 μm TiN powder,
Al 2 O 3 powder of 0.5 μm, MgO powder of 0.4 μm,
2.0μm ZrC powder, 1.5μm TaC powder, 1.8μm
NbC powder with a diameter of 0.4 μm and CaO powder with a diameter of 0.4 μm were prepared, and these raw material powders were blended into the composition shown in Table 1. After mixing both in a ball mill for 72 hours, the upper layer part had a diameter of :8mm
It was press-formed into a green compact with dimensions of φ x thickness: 1.5 mm, and the lower layer was formed at a predetermined pressure and sintered under the same conditions shown in Table 1. After that, it was polished to dimensions of outer diameter: 8 mmφ x thickness: 3 mm, and then the upper layer partial compact and the lower layer partial sintered compact formed in this way were stacked and charged into a stainless steel container. Pressure this container:
After maintaining the temperature at 1100℃ for 30 minutes in a vacuum of 10 -4 mmHg to fully degas the inside, it was charged into a girdle-type ultra-high pressure and high temperature device, using pyroferrite as the pressure medium, and A graphite cylinder was used as the heating element, and the composite was sintered under the conditions of pressure: 55 Kb, temperature: 1400°C, and holding time: 30 minutes. Composite cutting tips 1 to 1 of the present invention are produced by brazing the composite to the cutting edge of a WC-based cemented carbide cutting tip having a shape conforming to ISO standard SNGN432.
8 and conventional composite cutting chips 1 and 2 were manufactured. Next, regarding the composite cutting chips 1 to 8 of the present invention and the conventional composite cutting chips 1 to 2 obtained as a result, Work material: Hardened steel round bar (Material: SKD-11, Hardness: H R C60), Cutting Speed: 70m/mm, feed: 0.1mm/rev., depth of cut: 0.2mm, cutting time: 15mm,
【表】
切削:使用せず、
の条件での連続切削試験、および、
被削材:焼入れ鋼角材(材質:SKD―11、硬
さ:HRC50)、
切削速度:120m/mm、
送り :0.3mm/刃、
切込み :0.7mm、
切削時間:15mm、
切削油剤:使用せず、
の条件でのフライス切削試験を行ない、上記連続
切削試験では切刃の逃げ面摩耗幅とすくい面摩耗
深さを測定し、またフライス切削試験では切刃に
チツピングが発生するまでの切削時間を測定し
た。これらの測定結果を第1表に示した。
第1表に示される結果から、本発明複合切削チ
ツプ1〜8は、いずれも連続切削試験ですぐれた
耐摩耗性を有し、かつフライス切削試験でもチツ
ピングの発生が全く見られないのに対して、従来
複合切削チツプ1〜2においては、耐摩耗性が相
対的に低く、しかもチツピング発生や複合体の剥
離が見られ、本発明複合切削チツプに比して切削
特性の劣ることが明らかである。
上述のように、この発明の複合切削チツプにお
いては、複合体を構成する下層部分の上層部分に
対する接合強度が著しく高く、かつ下層部分はす
ぐれた剛性および耐熱性を有しているので、切削
に際しては、すぐれた耐摩耗性を示すほか、切刃
にチツピングや剥離の発生がなく、すぐれた切削
性能を長期に亘つて発揮するものである。[Table] Cutting: Continuous cutting test under the conditions of , Work material: Hardened steel square material (Material: SKD-11, Hardness: H R C50), Cutting speed: 120 m/mm, Feed: A milling test was conducted under the following conditions: 0.3mm/blade, depth of cut: 0.7mm, cutting time: 15mm, cutting fluid: not used, and in the above continuous cutting test, the flank wear width and rake face wear depth of the cutting edge were measured. In addition, in the milling cutting test, the cutting time until chipping occurred on the cutting edge was measured. The results of these measurements are shown in Table 1. From the results shown in Table 1, composite cutting chips 1 to 8 of the present invention all have excellent wear resistance in continuous cutting tests, and no chipping is observed in milling tests. Therefore, the conventional composite cutting chips 1 and 2 had relatively low wear resistance, and chipping and peeling of the composite were observed, and it is clear that the cutting properties were inferior to the composite cutting chips of the present invention. be. As mentioned above, in the composite cutting tip of the present invention, the bonding strength of the lower layer to the upper layer of the composite is extremely high, and the lower layer has excellent rigidity and heat resistance, so that it is easy to cut when cutting. In addition to exhibiting excellent wear resistance, the cutting edge exhibits no chipping or peeling, and exhibits excellent cutting performance over a long period of time.
Claims (1)
サーメツトの下層部分との複合体を刃先部分にろ
う付けしてなる複合切削チツプにおいて、前記下
層部分を、重量%で、 硬質分散相形成成分としての周期律表の4a、
5a、および6a族金属、さらにMg、Ca、Al、お
よびSiの炭化物、窒化物、酸化物、およびほう化
物、並びにこれらの2種以上の固溶体のうちの1
種または2種以上:10〜70%、 結合相形成成分としてのWまたはW―Mo合金
および不可避不純物:残り、 からなる組成を有するサーメツトで構成したこと
を特徴とする複合切削チツプ。[Claims] 1. An upper layer portion of a cubic boron nitride-based sintered material;
In a composite cutting chip formed by brazing a composite with a lower layer portion of cermet to the cutting edge portion, the lower layer portion is classified as 4a of the periodic table as a hard dispersed phase forming component in weight%.
5a and 6a group metals, as well as carbides, nitrides, oxides, and borides of Mg, Ca, Al, and Si, and one of solid solutions of two or more of these.
1. A composite cutting chip characterized in that it is made of a cermet having a composition of: 10 to 70% of a species or two or more species, W or W-Mo alloy as a binder phase forming component, and the remainder of unavoidable impurities.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6195183A JPS59187412A (en) | 1983-04-08 | 1983-04-08 | Composite cutting tip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6195183A JPS59187412A (en) | 1983-04-08 | 1983-04-08 | Composite cutting tip |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59187412A JPS59187412A (en) | 1984-10-24 |
| JPH0123241B2 true JPH0123241B2 (en) | 1989-05-01 |
Family
ID=13186008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6195183A Granted JPS59187412A (en) | 1983-04-08 | 1983-04-08 | Composite cutting tip |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59187412A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0248192Y2 (en) * | 1986-11-12 | 1990-12-18 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS57179083A (en) * | 1981-04-27 | 1982-11-04 | Sumitomo Electric Industries | Composite sintered body for tool and manufacture |
| JPS57180741U (en) * | 1981-05-12 | 1982-11-16 |
-
1983
- 1983-04-08 JP JP6195183A patent/JPS59187412A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59187412A (en) | 1984-10-24 |
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