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JPS63505B2 - - Google Patents
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JPS63505B2 - - Google Patents

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Publication number
JPS63505B2
JPS63505B2 JP59079786A JP7978684A JPS63505B2 JP S63505 B2 JPS63505 B2 JP S63505B2 JP 59079786 A JP59079786 A JP 59079786A JP 7978684 A JP7978684 A JP 7978684A JP S63505 B2 JPS63505 B2 JP S63505B2
Authority
JP
Japan
Prior art keywords
powder
cutting
ultra
alloy
hard sintered
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
Application number
JP59079786A
Other languages
Japanese (ja)
Other versions
JPS60224781A (en
Inventor
Hironori Yoshimura
Naohisa Ito
Kenichi Nishigaki
Mitsuo Koizumi
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.)
Mitsubishi Metal Corp
Original Assignee
Mitsubishi Metal Corp
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
Application filed by Mitsubishi Metal Corp filed Critical Mitsubishi Metal Corp
Priority to JP59079786A priority Critical patent/JPS60224781A/en
Publication of JPS60224781A publication Critical patent/JPS60224781A/en
Publication of JPS63505B2 publication Critical patent/JPS63505B2/ja
Granted legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/30Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Physical Vapour Deposition (AREA)
  • Chemical Vapour Deposition (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

〔産業上の利用分野〕 この発明は、高硬度かつ高強度を有し、切削工
具として使用した場合、すぐれた耐摩耗性および
耐塑性変形性を有し、これらの特性が要求される
高速切削にすぐれた切削性能を発揮する被覆超硬
質焼結合金の製造法に関するものである。 〔従来の技術及びその問題点〕 近年、切削加工の分野では加工能率向上のため
に高速切削が検討されているが、切削速度を大き
くすると、切削工具の刃先温度が上昇し、刃先が
摩耗するというよりはむしろ高温に起因して塑性
変形することによつて切削工具として寿命に至る
場合や、使用できない場合が多い。 例えば、現在切削工具として実用に供されてい
るWC基超硬合金やTiC基サーメツトはそれぞれ
結合金属であるCo、Niの含有量が4〜20重量%
(日本工業規格)と多いため、刃先温度が1000℃
を越えると刃先が急激に軟化するようになるの
で、切削速度が200m/分を越える条件の切削で
は使用できないのが現状である。 一方、上記WC基超硬合金の耐摩耗性を改善す
る目的でWC基超硬合金の表面に、元素周期表の
4a族の炭化物、窒化物、炭窒化物、炭酸化物、
酸窒化物および炭酸窒化物、ならびにAlの酸化
物および酸窒化物のうちの1層又は2層以上から
なる表面被覆層を形成した切削用被覆超硬合金が
実用化され、スローアウエイチツプの主流となり
つつあるが、この被覆超硬合金にしても基体は
Coを5〜10重量%含有したWC基超硬合金である
ために、切削速度が250m/分を越えると、刃先
が軟化してしまうという問題点があつた。 それで、切削速度が250m/分を越える切削で
は、Al2O3基セラミツクスが検討されたが、
Al2O3基セラミツクスは抗折力が50〜80Kg/mm2
低強度のため利用範囲が鋳造切削の一部に限定さ
れていた。 そこで、WC基超硬合金のCo量を減じて、合金
の硬さを向上させ、ひいては切削時の耐摩耗性を
向上させるとともに、耐塑性変形性をも向上させ
ようという試みがなされてきたが、いずれの試み
においてもWC基超硬合金中のCo量を減ずると、
合金の硬さと耐塑性変形性は向上するが、抗折力
が大巾に低下して上記セラミツクスと同等の強度
の合金となつてしまい、実用に供せないでいた。 〔発明の目的〕 したがつて、この発明の目的は、上記セラミツ
クスよりも高強度で、しかも一般のWC基超硬合
金並びの強度と、より高い硬度と耐塑性変形性と
を有し、250m/分を越える高速切削用の切削工
具としても使用することができる材料を製造する
ことである。 〔先行技術及び知見事項〕 本発明者らは、先に、 組成式:(M、W)(C、N)を有する複合金属
炭窒化物固溶体粉末(ただし、M=Ti、Zrおよ
びHfのうちの1種又は2種以上):20〜90重量
%、 炭化タングステン(以下、WCで示す。)粉
末:10〜80重量%、 Co粉末:0.5〜3重量%、 からなる配合組成を有する成形体を、窒素雰囲気
中で焼結することにより、小孔が少なく、硬さが
ロツクウエルA硬さ(以下、HRAで表わす。)で
92.5以上かつ抗折力が150Kg/mm2以上という高硬
度かつ高強度の超硬質焼結合金が得られることを
見い出したが、この度、 前記超硬質焼結合金は塑性変形を起しにくい特
性をも有し、このような合金を基体として、その
表面に元素周期表の4a族の炭化物、窒化物、炭
窒化物、炭酸化物、酸窒化物および炭酸窒化物、
ならびにAlの酸化物および酸窒化物のうちの1
層又は2層以上からなる表面被覆層を形成する
と、被覆超硬質焼結合金全体の耐塑性変形性が向
上し、又、基体の塑性変形による表面被覆層の剥
離が起こりにくいため、従来のWC基超硬合金の
表面に上記硬質物質を被覆した被覆WC基超硬合
金と比べて、表面被覆層による耐摩耗性向上の比
率がきわめて高く、これらの結果として、切削速
度が250m/分を越える高速で切削工具として使
用した場合でもすぐれた切削性能を示すことを発
見した。 〔発明の構成に欠くことができない事項〕 この発明は、上記知見に基いてなされた切削工
具用被覆超硬質焼結合金の製造法であり、 原料粉末として、組成式:(M、W)(C、N)
を有する複合金属炭窒化物固溶体粉末(ただし、
M:Ti、Zr、およびHfのうちの1種または2種
以上)、炭化タングステン粉末、およびCo粉末を
用意し、これら原料粉末を、重量%で、 複合金属炭窒化物固溶体粉末:20〜90%、 炭化タングステン粉末:10〜80%、 Co粉末:0.5〜3% からなる配合組成に配合し、通常の条件で混合
し、圧粉体に成形した後、窒素雰囲気中で焼結
し、高硬度および高強度を有する切削工具用の超
硬質焼結合金基体を製造し、 次に、前記超硬質焼結合金基体の少なくとも切
削面に、元素周期表の4a族の炭化物、窒化物、
炭窒化物、炭酸化物、酸窒化物および炭酸窒化
物、並びにAlの酸化物および酸窒化物のうちの
1層又は2層以上からなる表面被覆層を形成する
ことを特徴とするものである。 〔発明の構成要件〕 以下、この発明の構成を詳細に説明する。 () 基体の製造について (i) 原料粉末の粒度 複合金属炭窒化物固溶体粉末、WC粉末と
もに得られる合金の抗折力を向上させるため
には、粉末の粒度が細かい方が望ましい。例
えば、複合金属炭窒化物固溶体粉末の平均粒
径は、0.5〜5.0μmの範囲内、WC粉末の平均
粒径は0.5〜5.0μmの範囲内が好ましい。そ
して、Co粉末は0.5〜3.0μmの範囲内の平均
粒径であることが望ましい。 (ii) 配合組成 (a) (M、W)(C、N) この成分は、この発明により製造される
合金の第1の硬質分散相形成成分であつ
て、窒化されることにより組成が変化し、
合金の焼結性を向上させ、緻密な焼結体と
し、合金の抗折力を向上させる。又、固溶
体が金属分としてTi、ZrおよびHfの1種
または2種以上を必須成分とするので、そ
れ自体高硬度であるため、合金の硬さを向
上させる作用を有する。その含有量が20重
量%未満では前記の所望の効果が得られ
ず、一方、90重量%を越えると、合金の抗
折力が低下するようになることから、その
含有量を20〜90重量%と定めた。 (b) WC WCはこの発明により得られる合金の第
2の硬質分散相形成成分であつて、前記
(M、W)(C、N)がスケルトルを作るこ
とを阻害し、硬質相形成成分の分散を良く
し、合金の抗折力を向上させる作用を有す
るが、その合有量が10重量%未満では前記
の所望の効果が得られず、一方、80重量%
を越えると、切削時の耐摩耗性が低下する
ようになることから、その含有量を10〜80
重量%と定めた。 (c) Co Coは、この発明においては、従来のWC
基超硬合金中でのCoのように結合金属と
いう役割よりは、むしろ触媒的な役割を果
し、合金の主成分である前記(M、W)
(C、N)の窒化による固溶体組成の変化
を起こしやすくして、合金の焼結性を著し
く向上させ、合金の抵抗力を大巾に改善す
る効果を有するので、従来のWC基超硬合
金に含有されているCo量よりも少ない含
有量で効果を発揮するのである。 その含有量が0.5重量%未満では上記の
効果が十分でなく、一方、3重量%を越え
ると硬さが低下し、切削時の耐摩耗性も低
下して、従来のWC基超硬合金と耐摩耗性
における差がなくなるので、その含有量を
0.5〜3重量%と定めた。 この発明においては、上記3成分の他に、
WCの粒成長抑制剤としてWC基超硬合金に
添加されているTaC、NbC、VC、Cr3C2
を2重量%まで配合してもよい。 (iii) 混合 混合は通常の条件、例えば、ボールミルで
72時間湿式(例えばアルコール中)粉砕混合
することによつて行われる。 (iv) 成形 粉末混合物を乾燥した後、10〜30Kg/mm2
圧力でプレス成形して圧粉体とする。 (v) 焼結 焼結は、複合金属炭窒化物固溶体を窒化さ
せ、その組成を変化させ、合金の焼結性を改
善するために、窒素雰囲気中で行なうことが
必要である。窒素圧は0.01気圧以上が好まし
い。0.01気圧未満では複合金属炭窒化物固溶
体の窒化が十分に進まないからである。 そして、焼結温度は1400〜1800℃が好まし
い。1400℃未満では、未焼結で、焼結体中に
大巣が多数残存して、合金の抗折力が低下し
てしまうからであり、逆に、1800℃を超える
と、合金中の(M、W)(C、N)とWCが
粒成長を起こし、抗折力が低下してしまうか
らである。 () 表面被覆層の形成について (i) 層構成 表面被覆層は、元素周期表の4a族の炭化
物、窒化物、炭窒化物、炭酸化物、酸窒化物
および炭酸窒化物、並びにAlの酸化物およ
び酸窒化物のうとの1層又は2層以上から構
成される。 元素周期表の4a族とは、Ti、ZrおよびHf
からなる群のことである。したがつて、元素
周期表の4a族の炭化物、窒化物、炭窒化物、
炭酸化物、酸窒化物および炭酸窒化物、並び
にAlの酸化物および酸窒化物のうちの1層
又は2層以上とは、Tiの炭化物、窒化物、
炭窒化物、炭酸化物、酸窒化物および炭酸窒
化物、Zrの炭化物、窒化物、炭窒化物、炭
酸化物、酸窒化物および炭酸窒化物、Hfの
炭化物、窒化物、炭窒化物、炭酸化物、酸窒
化物および炭酸窒化物並びにAlの酸化物お
よび酸窒化物のうちから選ばれた1層、ある
いはその上に順次前記の1層以上を重ねたも
のを指す。 (ii) 平均層厚 1層又は2層以上からなる表面被覆層全体
の平均層厚は0.5〜20μmとするのが望まし
い。 平均層厚が0.5μm未満では所望の耐摩耗性
を確保することができず、一方20μmを越え
た平均層厚にすると、被覆超硬質焼結合金の
靭性劣化が著しくなるからである。 (iii) 層形成法 通常の化学蒸着法や物理蒸着法によつて形
成される。 〔実施例〕 次に、この発明の構成及び効果を実施例と比較
例により詳細に説明する。 実施例及び比較例 各原料粉末を第1表に示される配合組成に配合
し、ボールミルにて72時間湿式粉砕混合し、乾燥
した後、15Kg/mm2の圧力にてプレス成形して
[Industrial Application Field] This invention has high hardness and high strength, and when used as a cutting tool, has excellent wear resistance and plastic deformation resistance, and is suitable for high-speed cutting that requires these properties. The present invention relates to a method for producing a coated ultra-hard sintered alloy that exhibits excellent cutting performance. [Conventional technology and its problems] In recent years, high-speed cutting has been considered in the cutting field to improve processing efficiency, but increasing the cutting speed increases the temperature of the cutting tool's cutting edge and causes the cutting edge to wear out. Rather, in many cases, the cutting tool reaches the end of its life or cannot be used due to plastic deformation due to high temperatures. For example, WC-based cemented carbide and TiC-based cermet, which are currently in practical use as cutting tools, each have a content of 4 to 20% by weight of Co and Ni, which are bonding metals.
(Japanese Industrial Standards), so the cutting edge temperature is 1000℃.
If the cutting speed exceeds 200 m/min, the cutting edge will suddenly soften, so it cannot currently be used for cutting at cutting speeds exceeding 200 m/min. On the other hand, for the purpose of improving the wear resistance of the above-mentioned WC-based cemented carbide, the surface of the WC-based cemented carbide is coated with elements from the periodic table.
Group 4a carbides, nitrides, carbonitrides, carbonates,
Coated cemented carbide for cutting with a surface coating layer consisting of one or more layers of oxynitrides, carbonate nitrides, and oxides and oxynitrides of Al has been put into practical use and has become the mainstream for throw-away chips. However, even with this coated cemented carbide, the base is
Since it is a WC-based cemented carbide containing 5 to 10% by weight of Co, there was a problem in that the cutting edge softened when the cutting speed exceeded 250 m/min. Therefore, for cutting at cutting speeds exceeding 250 m/min, Al 2 O 3 -based ceramics were considered, but
Due to the low strength of Al 2 O tri- based ceramics, which has a transverse rupture strength of 50 to 80 Kg/mm 2 , its use has been limited to a portion of casting cutting. Therefore, attempts have been made to reduce the amount of Co in WC-based cemented carbide to improve the hardness of the alloy, which in turn improves its wear resistance during cutting, as well as its plastic deformation resistance. In both attempts, when the amount of Co in the WC-based cemented carbide is reduced,
Although the hardness and plastic deformation resistance of the alloy were improved, the transverse rupture strength was significantly reduced, resulting in an alloy with a strength equivalent to that of the above-mentioned ceramics, making it impossible to put it to practical use. [Object of the Invention] Therefore, the object of the present invention is to provide a material that has higher strength than the above-mentioned ceramics, has strength comparable to general WC-based cemented carbide, and has higher hardness and plastic deformation resistance. The object of the present invention is to produce a material that can also be used as a cutting tool for high-speed cutting in excess of /min. [Prior Art and Knowledge] The present inventors previously discovered a composite metal carbonitride solid solution powder having a composition formula: (M, W) (C, N) (where M = Ti, Zr, and Hf). (one type or two or more types): 20 to 90% by weight, tungsten carbide (hereinafter referred to as WC) powder: 10 to 80% by weight, Co powder: 0.5 to 3% by weight. By sintering it in a nitrogen atmosphere, it has fewer small pores and has a hardness of Rockwell A hardness (hereinafter referred to as HRA).
We have discovered that it is possible to obtain a superhard sintered alloy with high hardness and strength, with a transverse rupture strength of 92.5 or higher and a transverse rupture strength of 150Kg/ mm2 or higher. Using such an alloy as a substrate, carbides, nitrides, carbonitrides, carbonates, oxynitrides, and carbonitrides of group 4a of the periodic table of elements are formed on the surface of the alloy.
and one of Al oxides and oxynitrides
Forming a surface coating layer or a surface coating layer consisting of two or more layers improves the plastic deformation resistance of the entire coated ultra-hard sintered alloy, and also prevents peeling of the surface coating layer due to plastic deformation of the base, making it difficult to use conventional WC. Compared to coated WC-based cemented carbide, in which the surface of the base cemented carbide is coated with the above-mentioned hard material, the wear resistance improvement rate due to the surface coating layer is extremely high, and as a result, the cutting speed exceeds 250 m/min. It was discovered that it exhibits excellent cutting performance even when used as a cutting tool at high speeds. [Matters Essential to the Structure of the Invention] The present invention is a method for producing a coated ultra-hard sintered alloy for cutting tools based on the above-mentioned knowledge. C, N)
Composite metal carbonitride solid solution powder having (however,
M: one or more of Ti, Zr, and Hf), tungsten carbide powder, and Co powder are prepared, and these raw material powders are mixed in weight% as follows: Composite metal carbonitride solid solution powder: 20 to 90 %, tungsten carbide powder: 10~80%, Co powder: 0.5~3%, mixed under normal conditions, formed into a green compact, sintered in a nitrogen atmosphere, and then An ultra-hard sintered alloy base for a cutting tool having hardness and high strength is manufactured, and then at least the cutting surface of the ultra-hard sintered alloy base is coated with carbides, nitrides, etc. of group 4a of the periodic table of elements,
It is characterized by forming a surface coating layer consisting of one or more layers of carbonitrides, carbonates, oxynitrides, carbonate nitrides, and oxides and oxynitrides of Al. [Constituent elements of the invention] The configuration of the present invention will be explained in detail below. () Regarding manufacture of the substrate (i) Particle size of raw powder In order to improve the transverse rupture strength of the alloy obtained for both the composite metal carbonitride solid solution powder and the WC powder, it is desirable that the powder particle size be fine. For example, the average particle size of the composite metal carbonitride solid solution powder is preferably within the range of 0.5 to 5.0 μm, and the average particle size of the WC powder is preferably within the range of 0.5 to 5.0 μm. It is desirable that the Co powder has an average particle size within the range of 0.5 to 3.0 μm. (ii) Mixture composition (a) (M, W) (C, N) This component is the first hard dispersed phase forming component of the alloy produced by this invention, and the composition changes when nitrided. death,
Improves the sinterability of the alloy, makes it a dense sintered body, and improves the transverse rupture strength of the alloy. In addition, since the solid solution contains one or more of Ti, Zr and Hf as essential metal components, it itself has a high hardness and thus has the effect of improving the hardness of the alloy. If the content is less than 20% by weight, the desired effect described above cannot be obtained, while if it exceeds 90% by weight, the transverse rupture strength of the alloy will decrease. %. (b) WC WC is the second hard dispersed phase-forming component of the alloy obtained by this invention, and the above (M, W) (C, N) inhibits the formation of skeletons and inhibits the hard phase-forming component. It has the effect of improving dispersion and improving the transverse rupture strength of the alloy, but if the combined amount is less than 10% by weight, the desired effect described above cannot be obtained;
If the content exceeds 10 to 80, the wear resistance during cutting will decrease.
It was determined as weight%. (c) Co Co is the conventional WC in this invention.
The above (M, W), which is the main component of the alloy, plays a catalytic role rather than a binding metal role like Co in the base cemented carbide.
It has the effect of making it easier to change the solid solution composition due to nitridation of (C, N), significantly improving the sinterability of the alloy, and greatly improving the resistance of the alloy. It is effective with a smaller amount of Co than that contained in Co. If the content is less than 0.5% by weight, the above effects will not be sufficient, while if it exceeds 3% by weight, the hardness will decrease and the wear resistance during cutting will also decrease, making it different from conventional WC-based cemented carbides. Since there is no difference in wear resistance, the content can be reduced.
The content was determined to be 0.5 to 3% by weight. In this invention, in addition to the above three components,
Up to 2% by weight of TaC, NbC, VC, Cr 3 C 2, etc., which are added to WC-based cemented carbide as a WC grain growth inhibitor, may be added. (iii) Mixing Mixing is carried out under normal conditions, e.g. in a ball mill.
This is done by wet grinding (eg in alcohol) mixing for 72 hours. (iv) Molding After drying the powder mixture, it is press-molded at a pressure of 10 to 30 kg/mm 2 to form a green compact. (v) Sintering Sintering needs to be carried out in a nitrogen atmosphere in order to nitride the composite metal carbonitride solid solution, change its composition, and improve the sinterability of the alloy. The nitrogen pressure is preferably 0.01 atm or higher. This is because the nitridation of the composite metal carbonitride solid solution does not proceed sufficiently if the pressure is less than 0.01 atmosphere. The sintering temperature is preferably 1400 to 1800°C. If the temperature is lower than 1400℃, many large cavities will remain in the sintered compact and the transverse rupture strength of the alloy will decrease.On the other hand, if the temperature exceeds 1800℃, the ( This is because M, W) (C, N) and WC cause grain growth, resulting in a decrease in transverse rupture strength. () Regarding the formation of the surface coating layer (i) Layer structure The surface coating layer consists of carbides, nitrides, carbonitrides, carbonates, oxynitrides, and carbonitrides of group 4a of the periodic table of elements, and oxides of Al. and one or more layers of oxynitride. Group 4a of the periodic table of elements is Ti, Zr and Hf
It is a group consisting of. Therefore, carbides, nitrides, carbonitrides of group 4a of the periodic table of elements,
One or more layers of carbonates, oxynitrides, carbonate nitrides, and oxides and oxynitrides of Al are Ti carbides, nitrides,
Carbonitrides, carbonates, oxynitrides and carbonitrides, Zr carbides, nitrides, carbonitrides, carbonates, oxynitrides and carbonitrides, Hf carbides, nitrides, carbonitrides, carbonates , oxynitrides, carbonate nitrides, and oxides and oxynitrides of Al, or one or more of the above-mentioned layers are sequentially stacked thereon. (ii) Average layer thickness The average layer thickness of the entire surface coating layer consisting of one or more layers is preferably 0.5 to 20 μm. This is because if the average layer thickness is less than 0.5 μm, the desired wear resistance cannot be ensured, whereas if the average layer thickness exceeds 20 μm, the toughness of the coated ultra-hard sintered alloy will significantly deteriorate. (iii) Layer formation method Formed by ordinary chemical vapor deposition or physical vapor deposition. [Example] Next, the configuration and effects of the present invention will be explained in detail using Examples and Comparative Examples. Examples and Comparative Examples Each raw material powder was blended into the composition shown in Table 1, wet-pulverized and mixed in a ball mill for 72 hours, dried, and then press-molded at a pressure of 15 kg/mm 2 .

【表】【table】

【表】 圧粉体とし、ついでこの圧粉体を第1表に示され
る焼結条件にて焼結して、本発明超硬質焼結合金
基体1〜22と比較超硬質焼結合金基体1〜6を製
造した。前記基体のHRA及び抗折力も合わせて
第1表に示す。なお、比較超硬質焼結合金基体1
〜5は配合組成がこの発明の配合組成範囲から外
れたものであり(この発明の配合組成範囲から外
れた成分の配合率には※をつけて示す。)、比較超
硬質焼結合金基体5は更に窒素雰囲気中ではなく
真空中で焼結する点でも、この発明から外れたも
のである(※で示す)。又、比較超硬質焼結合金
基体6は窒素雰囲気中でなく真空中で焼結する点
でのみこの発明から外れている(※で示す)。 ついで、これらの基体からCIS・SNP432の形
状の切削チツプを製作した。 これらのチツプの全表面に、通常の化学蒸着法
(耐熱合金製反応容器内で、TiCを被覆する場合
は、TiCl4、CH4、H2ガスを流して1000℃で反応
させ、TiNを被覆する場合は、TiCl4、N2、H2
ガスを1000℃で反応させ、Tiの炭酸化物を被覆
する場合は、TiCl4、CO2、H2ガスを1000℃で反
応させ、Al2O3を被覆する場合はAlCl3、CO2
H2ガスを950℃で反応させる。また、複合化合物
を被覆する場合は、各種ガスを適宜混合して反応
させて被覆層を形成する。)を用いて、第2表に
示される層構成(層を構成する化合物を表わす式
は化学量論的に記載してある)および各層の平均
層厚をもつた1〜3層からなる表面被覆層を形成
することによつて、本発明被覆超硬質焼結合金チ
ツプ1〜29および比較被覆超硬質焼結合金チツプ
1〜6を製造した。 次いで、これらの切削チツプを下記の条件での
鋼の高速連続切削試験 被削材:SNCM8(ブリネル硬さ:240)の丸棒 切削条件 切削速度:300m/分 送 り:0.3mm/回転 切込み:1mm 切削時間:10分 ならびに、下記の条件での鋳鉄の高速断続切削試
験 被削材:FC25(ブリネル硬さ:140)の溝付き丸
棒 切削条件 切削速度:270m/分 送 り:0.3mm/回転 切込み:2mm 切削時間:10分 を行ない、鋼の高速連続切削試験では切刃のにげ
面摩耗幅とすくい面摩耗深さを、又、鋳鉄の高速
断続切削試験ではフランク摩耗幅とクレーター摩
耗深さを測定し、これらの結果を第2表に合わせ
て示した。 また、比較の目的で、表面被覆層を有していな
い本発明超硬質焼結合金基体4、5、6、8及び
9から作つた比較超硬質焼結合金チツプ1〜5と
P10相当のWC基超硬合金チツプ(従来合金チツ
プ1;組成は73%WC−15%TiC−5%TaC−7
%Co)、KO5相当のWC基超硬合金チツプ
[Table] Comparative ultra-hard sintered alloy substrates 1 to 1 to 22 of the ultra-hard sintered alloy substrates of the present invention were obtained by forming a green compact and then sintering this green compact under the sintering conditions shown in Table 1. -6 were produced. The HRA and transverse rupture strength of the substrate are also shown in Table 1. In addition, comparative ultra-hard sintered alloy substrate 1
Comparative ultra-hard sintered alloy substrates 5 to 5 have compounding compositions that are outside the compounding composition range of this invention (the compounding ratios of components that are out of the compounding composition range of this invention are marked with *). Further, this invention differs from the present invention in that it is sintered in a vacuum rather than in a nitrogen atmosphere (indicated by *). Furthermore, the comparative ultra-hard sintered alloy substrate 6 differs from the present invention only in that it is sintered in a vacuum instead of in a nitrogen atmosphere (indicated by *). Next, cutting chips in the shape of CIS/SNP432 were manufactured from these substrates. The entire surface of these chips is coated with TiN using the usual chemical vapor deposition method (when coating TiC in a heat-resistant alloy reaction vessel, react by flowing TiCl 4 , CH 4 , and H 2 gases at 1000°C) to coat TiN. TiCl 4 , N 2 , H 2
When reacting gases at 1000°C to coat Ti carbonate, react with TiCl 4 , CO 2 , H 2 gas at 1000°C, and when covering Al 2 O 3 use AlCl 3 , CO 2 ,
React H2 gas at 950℃. Further, when coating a composite compound, a coating layer is formed by appropriately mixing various gases and reacting them. ), a surface coating consisting of 1 to 3 layers with the layer structure shown in Table 2 (the formulas representing the compounds constituting the layers are written stoichiometrically) and the average layer thickness of each layer. Inventive coated ultra-hard sintered alloy chips 1-29 and comparative coated ultra-hard sintered alloy chips 1-6 were prepared by forming layers. Next, these cutting chips were tested for high-speed continuous cutting of steel under the following conditions: Work material: SNCM8 (Brinell hardness: 240) round bar cutting conditions: Cutting speed: 300 m/min Feed: 0.3 mm/rotational depth of cut: 1mm Cutting time: 10 minutes and high-speed interrupted cutting test of cast iron under the following conditions Work material: FC25 (Brinell hardness: 140) grooved round bar Cutting conditions Cutting speed: 270m/min Feed: 0.3mm/ Rotary depth of cut: 2 mm Cutting time: 10 minutes. In the high-speed continuous cutting test on steel, the wear width of the cutting edge and the wear depth on the rake face were measured, and in the high-speed intermittent cutting test on cast iron, the flank wear width and crater wear were measured. The depth was measured and the results are shown in Table 2. For the purpose of comparison, comparative ultra-hard sintered alloy chips 1 to 5 were prepared from the ultra-hard sintered alloy substrates 4, 5, 6, 8, and 9 of the present invention without a surface coating layer.
WC-based cemented carbide chip equivalent to P10 (conventional alloy chip 1; composition is 73% WC - 15% TiC - 5% TaC - 7
%Co), WC-based cemented carbide chip equivalent to KO5

【表】【table】

【表】【table】

〔発明の効果〕〔Effect of the invention〕

以上のように、本発明被覆超硬質焼結合金は、
基体が高硬度かつ高強度であり、しかも耐塑性変
形性にすぐれるので、この基体表面に硬質被覆層
を蒸着させることにより、切削工具として用いた
ときに、従来合金あるいは従来被覆合金では実用
上不可能であつた切削速度で250m/分を越える
高速切削を可能としたのである。
As described above, the coated super hard sintered alloy of the present invention is
The base material has high hardness and strength, and has excellent plastic deformation resistance, so by depositing a hard coating layer on the surface of this base material, when used as a cutting tool, it is practically impossible to use with conventional alloys or conventional coated alloys. This enabled high-speed cutting of over 250 m/min, which was previously impossible.

Claims (1)

【特許請求の範囲】 1 原料粉末として、組成式:(M、W)(C、
N)を有する複合金属炭窒化物固溶体粉末(ただ
し、M:Ti、Zr、およびHfのうちの1種または
2種以上)、炭化タングステン粉末、およびCo粉
末を用意し、これら原料粉末を、重量%で、 複合金属炭窒化物固溶体粉末:20〜90%、 炭化タングステン粉末:10〜80%、 Co粉末:0.5〜3% からなる配合組成に配合し、通常の条件で混合
し、圧粉体に成形した後、窒素雰囲気中で焼結
し、高硬度および高強度を有する切削工具用の超
硬質焼結合金基体を製造し、 次に、前記超硬質焼結合金基体の少なくとも切
削面に、元素周期表の4a族の炭化物、窒化物、
炭窒化物、炭酸化物、酸窒化物および炭酸窒化
物、並びにAlの酸化物および酸窒化物のうちの
1層又は2層以上からなる表面被覆層を形成する
ことを特徴とする切削工具用被覆超硬質焼結合金
の製造法。
[Claims] 1. As raw material powder, composition formula: (M, W) (C,
A composite metal carbonitride solid solution powder having N) (M: one or more of Ti, Zr, and Hf), tungsten carbide powder, and Co powder are prepared, and these raw material powders are %, composite metal carbonitride solid solution powder: 20-90%, tungsten carbide powder: 10-80%, Co powder: 0.5-3%, mixed under normal conditions, and made into a green compact. and then sintered in a nitrogen atmosphere to produce an ultra-hard sintered alloy base for a cutting tool having high hardness and high strength, and then, on at least the cutting surface of the ultra-hard sintered alloy base, carbides and nitrides of group 4a of the periodic table of elements;
A coating for a cutting tool characterized by forming a surface coating layer consisting of one or more layers of carbonitride, carbonate, oxynitride, carbonitride, and oxide and oxynitride of Al. A method for producing ultra-hard sintered alloys.
JP59079786A 1984-04-20 1984-04-20 Production of coated sintered hard alloy for cutting tool Granted JPS60224781A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59079786A JPS60224781A (en) 1984-04-20 1984-04-20 Production of coated sintered hard alloy for cutting tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59079786A JPS60224781A (en) 1984-04-20 1984-04-20 Production of coated sintered hard alloy for cutting tool

Publications (2)

Publication Number Publication Date
JPS60224781A JPS60224781A (en) 1985-11-09
JPS63505B2 true JPS63505B2 (en) 1988-01-07

Family

ID=13699889

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59079786A Granted JPS60224781A (en) 1984-04-20 1984-04-20 Production of coated sintered hard alloy for cutting tool

Country Status (1)

Country Link
JP (1) JPS60224781A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE527173C2 (en) * 2003-07-25 2006-01-17 Sandvik Intellectual Property Ways to manufacture a fine-grained cemented carbide

Also Published As

Publication number Publication date
JPS60224781A (en) 1985-11-09

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