JPS621464B2 - - Google Patents
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- JPS621464B2 JPS621464B2 JP58048499A JP4849983A JPS621464B2 JP S621464 B2 JPS621464 B2 JP S621464B2 JP 58048499 A JP58048499 A JP 58048499A JP 4849983 A JP4849983 A JP 4849983A JP S621464 B2 JPS621464 B2 JP S621464B2
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- phase
- powder
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- sintered alloy
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Description
この発明は、高靭性および高硬度を有し、さら
にすぐれた耐摩耗性、耐塑性変形性、および耐衝
撃性を有し、したがつて、これらの特性が要求さ
れる高速切削や、高送り切削および深切り込み切
削などの重切削に用いられる切削工具として、さ
らに熱間圧延ロール、熱間線引ロール、熱間圧縮
ダイス、熱間鍛造ダイス、および熱間押出しパン
チなどの比較的長時間高温にさらされる熱間加工
用工具として使用した場合にすぐれた性能を発揮
する超耐熱焼結合金およびその製造法に関するも
のである。
近年、加工能率向上のために高速切削化や高送
り切削化が検討されているが、切削速度を高くし
たり、送り量を多くしたりすると、切削工具の刃
先温度が上昇し、刃先が摩耗よりは、むしろ高温
に起因する塑性変形によつて使用寿命に至る場合
が多い。
しかしながら、現在実用に供されている硬質相
が主として炭化タングステン(以下WCで示す)
や炭化チタン(以下TiCで示す)で構成され、一
方結合相が主として鉄族金属で構成されている
WC基超硬合金やTiC基サーメツトは、刃先温度
が1000℃を越えると急激に軟化するようになるた
めに、これらのWC基超硬合金やTiC基サーメツ
トは勿論のこと、これらの表面に硬質被覆層を形
成したものにおいても、その使用条件は刃先温度
が1000℃を若干上廻る程度に制限されている。
また、硬質相がTiとWの複合炭化物固溶体
(以下、(Ti、W)Cで示す)あるいは、複合炭
窒化物固溶体(以下、(Ti、W)CNで示す)で構
成され、一方結合相がW―Mo合金で構成された
サーメツトが提案され、このサーメツトを高速切
削や重切削に切削工具として用いる試みもなされ
ているが、この従来サーメツトは、焼結性が悪
く、しかも原料粉末として使用される(Ti、
W)C粉末あるいは(Ti、W)CN粉末における
C濃度が比較的高いために、焼結時にその一部が
W粉末の一部と反応して脆いW2Cを形成し、こ
のW2Cの存在によつて耐衝撃性の劣つたものと
なることから、十分満足する切削性能を示さない
のが現状である。
そこで、本発明者等は、上述のような観点か
ら、特にすぐれた耐塑性変形性および耐衝撃性、
されに耐摩耗性が要求される鋼などの高速切削や
重切削に切削工具として使用するのに適した材料
を開発すべく研究を行つた結果、重量%で、
Tiの炭化物、窒化物、および炭窒化物(以
下、それぞれTiC、TiN、およびTiCNで示
し、これらを総称してTiの炭・窒化物とい
う)のうちの1種または2種以上の粉末:50〜
30%、
ZrおよびHfの炭化物、窒化物、および炭窒
化物(以下、それぞれZrC、ZrN、ZrCN、
HfC、HfN、およびHfCNで示し、これらを総
称して(Zr、Hf)の炭・窒化物という)のう
ちの1種または2種以上の粉末:5〜35%、
酸化マグネシウム(以下MgOで示す)粉
末:0.5〜10%、
W粉末:残り、
TiC、TiN、およびTiCNのうちの1種また
は2種以上の粉末:5〜30%、
ZrC、ZrN、ZrCN、HfC、HfN、および
HfCNのうちの1種または2種以上の粉末:5
〜35%、
MgO:0.5〜10%、
酸化アルミニウム(以下Al2O3で示す)およ
び酸化イツトリウム(以下Y2O3で示す)のう
ちの1種または2種の粉末:0.5〜10%、
W粉末:残り、
以上またはの配合組成をもつた圧粉体を、
真空中、あるいは不活性ガス雰囲気中、1800〜
2700℃の範囲内の高温で焼結すると、
硬質相形成成分としてのTiと、Wと、Zrお
よびHfのうちの1種または2種との複合炭化
物固溶体および複合炭窒化物固溶体(以下、そ
れぞれ(Ti、W、Zr、Hf)Cおよび(Ti、
W、Zr、Hf)CNで示す)のうちのいずれか1
種:10〜60%、
同じく硬質相形成成分としてのMgO:0.01
〜1%、
結合相形成成分としてのWおよび不可避不純
物:残り、
硬質相形成成分としての(Ti、W、Zr、
Hf)Cおよび(Ti、W、Zr、Hf)CNのうちの
いずれか1種:10〜60%、
硬質相形成成分としてのMgO:0.01〜1
%、
同じく硬質相形成成分としてのAl2O3および
Y2O3のうちの1種または2種:0.5〜10%、
結合相形成成分としてのWおよび不可避不純
物:残り、
以上またはの組成、並びに上記の(Ti、
W、Zr、Hf)Cおよび(Ti、W、Zr、Hf)CN
が、TiとWに富む相と、ZrおよびHfのいずれ
か、または両方に富む相との2相構造を有する超
耐熱焼結合金が得られ、この超耐熱焼結合金にお
いては、焼結時に、MgOが、この焼結工程で形
成された(Ti、W、Zr、Hf)Cおよび(Ti、
W、Zr、Hf)CN(以下、これを総称して複合
炭・窒化物固溶体という)中のC成分と反応し
て、この複合炭・窒化物固溶体中のC成分が減少
するようになり、この結果焼結性が著しく向上す
るようになると共に、脆いW2Cが形成しにくく
なることから、すぐれた耐衝撃性をもつようにな
り、さらに硬質相としての複合炭・窒化物固溶体
が、上記のように微細なWとTiに富む相と、同
じく微細なZrおよびHfのいずれか、または両方
に富む相との2相構造をもつことから、耐摩耗性
および耐塑性変形性が一段と向上したものとな
り、したがつて、これを高速切削や重切削などの
切削工具として用いた場合にはすぐれた切削性能
を発揮するという知見を得たのである。
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、以下に配合組成および成分組成、並
びに焼結温度を上記の通りに限定した理由を説明
する。
(a) 複合炭・窒化物固溶体
この成分は、主体硬質相形成成分であつて、焼
結合金にすぐれた耐摩耗性と耐塑性変形性を付与
する作用をもつものであり、かつこの硬質相は、
原料粉末として、Tiの炭・窒化物粉末および
(Zr、Hf)の炭・窒化物粉末を配合することによ
つて形成されるが、その配合量がそれぞれ5%未
満では前記複合炭・窒化物固溶体の含有量が10%
未満となつてしまい、前記作用に所望の効果が得
られず、一方Tiの炭・窒化物粉末にあつては30
%を越え、かつ(Zr、Hf)の炭・窒化物粉末に
あつては35%を越えて、それぞれ配合すると、前
記複合炭・窒化物固溶体の含有量が60%を越えて
高くなりすぎ、焼結合金の靭性が著しく低下する
ようになることから、Tiの炭・窒化物粉末の配
合量を5〜30%、(Zr、Hf)の炭・窒化物粉末の
配合量を5〜35%と定めて、焼結合金中の複合
炭・窒化物固溶体の含有量が10〜60%となるよう
にした。
(b) MgO
MgOは、その大半が焼結時に、この焼結工程
で形成された複合炭・窒化物固溶体中のCと反応
して、この複合炭・窒化物固溶体中のC量を減少
させると同時に、焼結性を改善し、かつそのわず
かな量が焼結合金中に残留して耐衝撃性を著しく
向上させる作用をもつが、その配合量が0.5%未
満では所望の焼結性改善効果が得られないばかり
でなく、焼結合金中に残留するMgOの量が0.01
%未満となつてしまつて所望の耐衝撃性を確保す
ることができず、一方10%を越えた配合量にする
と、焼結温度が低い場合は焼結合金中のMgO含
有量が1%を越えて高くなつてしまい、この結
果、焼結合金の耐塑性変形性が低下するようにな
るばかりでなく、焼結合金中に巣が形成され易く
なつて耐衝撃性も劣化するようになることから、
MgOの配合量を0.5〜10%、すなわちMgOの含有
量を0.01〜1%と定めた。
(c) Al2O3およびY2O3
これらの成分は、そのほとんどが素地中に均一
に分散して焼結性を向上させると共に、焼結合金
の耐摩耗性および耐衝撃性をさらに一段と向上さ
せる作用をもつので必要に応じて配合(含有)さ
れるが、その配合(含有)量が0.5%未満では前
記作用に所望の向上効果が得られず、一方その配
合(含有)量が10%を越えると、焼結合金の耐衝
撃性および耐塑性変形性に劣化傾向が現われるよ
うになることから、その配合(含有)量を0.5〜
10%と定めた。
(d) Wおよび不可避不純物
Wは、その一部が硬質相に固溶するが、大部分
は結合相として存在して硬質相と強固に結合し、
焼結合金にすぐれた耐衝撃性を付与する作用を有
するものである。また、不可避不純物として
Mo、Cr、Fe、Ni、Co、Re、Pt、およびPdなど
のうちの1種または2種以上を含有しても、それ
ぞれの成分含有量が1%以下であれば焼結合金の
特性が何ら損なわれるものではない。
(e) 焼結温度
焼結温度が1800℃未満では、MgOの蒸発が不
十分で、このため焼結合金における炭素量の減少
が少なく、所望の焼結性および耐衝撃性を確保す
ることができず、一方2700℃を越えた焼結温度に
すると、焼結合金に液相が発生して、その形状が
変化するようになることから、焼結温度を1800〜
2700℃と定めた。
つぎに、この発明の超耐熱焼結合金を実施例に
より具体的に説明する。
実施例 1
原料粉末として、平均粒径1.5μmを有する
TiC粉末、同1.2μmのTiN粉末、同1.0μmのZrC
粉末、同1.5μmのHfC粉末、同0.4μmのMgO粉
末、同0.5μmのAl2O3粉末、同0.4μmのY2O3粉
末、および同0.8μmのW粉末を用意し、これら
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、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
して圧粉体とし、ついでこの圧粉体を760torrの
窒素雰囲気中で、それぞれ第1表に示される温度
に2時間保持の条件で焼結することによつて、同
じく第2表に示される成分組成をもつた本発明焼
結合金1〜31および比較焼結合金1〜5をそれぞ
れ製造
The present invention has high toughness and hardness, as well as excellent wear resistance, plastic deformation resistance, and impact resistance. Cutting tools used for heavy cutting such as cutting and deep-cut cutting, as well as cutting tools used for relatively long and high temperatures such as hot rolling rolls, hot drawing rolls, hot compression dies, hot forging dies, and hot extrusion punches. The present invention relates to a super heat-resistant sintered alloy that exhibits excellent performance when used as a hot working tool exposed to heat, and a method for producing the same. In recent years, high-speed cutting and high-feed cutting have been considered in order to improve machining efficiency, but increasing the cutting speed or feed rate increases the temperature of the cutting tool's cutting edge and causes the cutting edge to wear out. Rather, in many cases, the service life is reached due to plastic deformation caused by high temperatures. However, the hard phase currently in practical use is mainly tungsten carbide (hereinafter referred to as WC).
and titanium carbide (hereinafter referred to as TiC), while the binder phase is mainly composed of iron group metals.
WC-based cemented carbide and TiC-based cermet suddenly soften when the cutting edge temperature exceeds 1000°C. Even for those with a coating layer, the usage conditions are limited to a blade edge temperature of slightly over 1000°C. In addition, the hard phase is composed of a composite carbide solid solution of Ti and W (hereinafter referred to as (Ti, W)C) or a composite carbonitride solid solution (hereinafter referred to as (Ti, W)CN), while the binder phase A cermet composed of a W-Mo alloy has been proposed, and attempts have been made to use this cermet as a cutting tool for high-speed cutting and heavy-duty cutting, but this conventional cermet has poor sinterability and is difficult to use as a raw material powder. be done (Ti,
Because the C concentration in the W)C powder or (Ti, W)CN powder is relatively high, a part of it reacts with a part of the W powder during sintering to form brittle W 2 C, and this W 2 C The presence of these materials results in poor impact resistance, and the current situation is that they do not exhibit sufficiently satisfactory cutting performance. Therefore, from the above-mentioned viewpoints, the present inventors have developed a method that has particularly excellent plastic deformation resistance and impact resistance.
As a result of conducting research to develop materials suitable for use as cutting tools for high-speed cutting and heavy cutting of steels that require wear resistance, we found that Ti carbides, nitrides, and Powder of one or more types of carbonitrides (hereinafter referred to as TiC, TiN, and TiCN, collectively referred to as Ti carbon/nitride): 50 ~
30%, Zr and Hf carbides, nitrides, and carbonitrides (hereinafter ZrC, ZrN, ZrCN, respectively)
Powder of one or more of HfC, HfN, and HfCN, collectively referred to as (Zr, Hf) carbon/nitride: 5 to 35%, magnesium oxide (hereinafter referred to as MgO) ) Powder: 0.5 to 10%, W powder: remainder, powder of one or more of TiC, TiN, and TiCN: 5 to 30%, ZrC, ZrN, ZrCN, HfC, HfN, and
Powder of one or more types of HfCN: 5
~35%, MgO: 0.5-10%, powder of one or two of aluminum oxide (hereinafter referred to as Al 2 O 3 ) and yttrium oxide (hereinafter referred to as Y 2 O 3 ): 0.5-10%, W powder: The remaining powder compact with a blending composition of
In vacuum or inert gas atmosphere, 1800~
When sintered at a high temperature within the range of 2700°C, a composite carbide solid solution and a composite carbonitride solid solution (hereinafter referred to as (Ti, W, Zr, Hf)C and (Ti,
Any one of W, Zr, Hf) (indicated by CN)
Seeds: 10-60%, MgO as a hard phase forming component: 0.01
~1%, W as a binder phase forming component and unavoidable impurities: the remainder, (Ti, W, Zr,
Any one of Hf)C and (Ti, W, Zr, Hf)CN: 10 to 60%, MgO as a hard phase forming component: 0.01 to 1
%, Al 2 O 3 and also as hard phase forming components
One or two of Y 2 O 3 : 0.5 to 10%, W as a binder phase forming component and unavoidable impurities: the remainder, the above composition, and the above (Ti,
W, Zr, Hf)C and (Ti, W, Zr, Hf)CN
However, a super heat-resistant sintered alloy with a two-phase structure of a phase rich in Ti and W and a phase rich in either or both of Zr and Hf is obtained, and in this super heat-resistant sintered alloy, during sintering, , MgO, (Ti, W, Zr, Hf)C and (Ti,
W, Zr, Hf) CN (hereinafter collectively referred to as composite carbon/nitride solid solution) reacts with the C component in this composite carbon/nitride solid solution, and the C component in this composite carbon/nitride solid solution decreases. As a result, sintering properties are significantly improved, and brittle W 2 C is difficult to form, resulting in excellent impact resistance.Furthermore, the composite carbon/nitride solid solution as a hard phase As mentioned above, it has a two-phase structure of a fine phase rich in W and Ti and a fine phase rich in either or both of Zr and Hf, which further improves wear resistance and plastic deformation resistance. Therefore, it was found that when used as a cutting tool for high-speed cutting or heavy cutting, it exhibits excellent cutting performance. This invention has been made based on the above findings, and the reason why the blending composition, component composition, and sintering temperature are limited as described above will be explained below. (a) Composite carbon/nitride solid solution This component is the main hard phase forming component, and has the effect of imparting excellent wear resistance and plastic deformation resistance to the sintered alloy, and this hard phase teeth,
It is formed by blending Ti carbon/nitride powder and (Zr, Hf) carbon/nitride powder as raw material powder, but if the blending amount is less than 5% each, the composite carbon/nitride powder Solid solution content is 10%
On the other hand, in the case of Ti carbon/nitride powder, the desired effect cannot be obtained.
%, and in the case of (Zr, Hf) carbon/nitride powder, exceeds 35%, the content of the composite carbon/nitride solid solution becomes too high, exceeding 60%, Since the toughness of the sintered alloy will be significantly reduced, the amount of Ti carbon/nitride powder should be increased to 5-30%, and the amount of (Zr, Hf) carbon/nitride powder should be increased to 5-35%. The content of the composite carbon/nitride solid solution in the sintered alloy was determined to be 10 to 60%. (b) MgO During sintering, most of MgO reacts with C in the composite carbon/nitride solid solution formed in this sintering process, reducing the amount of C in the composite carbon/nitride solid solution. At the same time, it improves sinterability, and a small amount of it remains in the sintered alloy and has the effect of significantly improving impact resistance, but if the amount is less than 0.5%, the desired sinterability improvement is not achieved. Not only is there no effect, but the amount of MgO remaining in the sintered alloy is 0.01
If the MgO content exceeds 10%, the MgO content in the sintered alloy will exceed 1% if the sintering temperature is low. As a result, not only the plastic deformation resistance of the sintered alloy decreases, but also cavities are more likely to form in the sintered alloy, resulting in a deterioration of its impact resistance. from,
The blending amount of MgO was determined to be 0.5 to 10%, that is, the MgO content was determined to be 0.01 to 1%. (c) Al 2 O 3 and Y 2 O 3 Most of these components are uniformly dispersed in the matrix, improving sinterability and further improving the wear resistance and impact resistance of the sintered alloy. Since it has the effect of improving the effect, it is blended (contained) as necessary, but if the blended (contained) amount is less than 0.5%, the desired effect of improving the above effect cannot be obtained; %, the impact resistance and plastic deformation resistance of the sintered alloy tend to deteriorate.
It was set at 10%. (d) W and unavoidable impurities A part of W is solidly dissolved in the hard phase, but most of it is present as a binder phase and is strongly bonded to the hard phase.
It has the effect of imparting excellent impact resistance to the sintered alloy. In addition, as an unavoidable impurity
Even if it contains one or more of Mo, Cr, Fe, Ni, Co, Re, Pt, and Pd, the characteristics of the sintered alloy will be affected if the content of each component is 1% or less. Nothing will be harmed. (e) Sintering temperature If the sintering temperature is less than 1800°C, the evaporation of MgO will be insufficient, and therefore the amount of carbon in the sintered alloy will decrease less, making it difficult to secure the desired sinterability and impact resistance. On the other hand, if the sintering temperature exceeds 2700℃, a liquid phase will occur in the sintered alloy and its shape will change.
The temperature was set at 2700℃. Next, the super heat-resistant sintered alloy of the present invention will be specifically explained with reference to Examples. Example 1 Raw material powder has an average particle size of 1.5 μm
TiC powder, 1.2μm TiN powder, 1.0μm ZrC
Prepare powder, HfC powder of 1.5 μm, MgO powder of 0.4 μm, Al 2 O 3 powder of 0.5 μm, Y 2 O 3 powder of 0.4 μm, and W powder of 0.8 μm, and use these raw materials. Each 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 to form a green compact. The sintered alloy 1 of the present invention having the component composition also shown in Table 2 was obtained by sintering the body in a nitrogen atmosphere of 760 torr under the conditions of holding the temperature shown in Table 1 for 2 hours. ~31 and comparative sintered alloys 1 to 5 were manufactured respectively.
【表】【table】
【表】【table】
【表】【table】
【表】
した。
ついで、この結果得られた本発明焼結合金1〜
31および比較焼結合金1〜5の硬さ(ロツクウエ
ル硬さAスケール)および抗折力を測定すると共
に、これよりSNP433の形状をもつた切削チツプ
を切出し、
被削材:SNCM―8(硬さ:HB250)、
切削速度:200m/min、
送り:0.3mm/rev.、
切込み:2mm、
切削時間:10min、
の条件での高速連続切削試験、並びに、
被削材:SNCM―8(硬さ:HB270)、
切削速度:120m/min、
送り:0.4mm/rev.、
切込み:3mm、
切削時間:3min、
の条件での断続切削試験を行ない、上記高速連続
切削試験では、切刃の逃げ面摩耗幅およびすくい
面摩耗深さを測定し、また上記断続切削試験では【expressed. Next, the resulting sintered alloys of the present invention 1-
31 and Comparative Sintered Alloys 1 to 5 were measured for their hardness (Rockwell hardness A scale) and transverse rupture strength, and cutting chips with the shape of SNP433 were cut from them. Work material: SNCM-8 (hard). Cutting speed: 200 m/min, Feed: 0.3 mm/rev., Depth of cut: 2 mm, Cutting time: 10 min, High-speed continuous cutting test under the following conditions, and Work material: SNCM-8 ( Hardness: H B 270), Cutting speed: 120m/min, Feed: 0.4mm/rev., Depth of cut: 3mm, Cutting time: 3min. The flank wear width and rake face wear depth of the blade were measured, and in the above interrupted cutting test,
【表】【table】
【表】
10個の試験切刃のうち、その刃先に欠損が発生し
た切刃数を測定した。これらの測定結果を第3表
に示した。また、比較の目的で、ISOのP10グレ
ードのWC基超硬合金製切削チツプ(以下従来切
削チツプ1という)およびTiC―10%Mo―15%
Niの組成(以上重量%、以下%は重量%を示
す)を有するTiC基サーメツト製切削チツプ(以
下従来切削チツプ2という)についても上記の切
削条件で切削試験を行ない、この結果も第3表に
示した。
第3表に示される結果から明らかなように、本
発明焼結合金1〜31は、いずれも高硬度および高
靭性を有し、いずれの切削試験でもすぐれた耐摩
耗性および耐衝撃性を示すのに対して、MgOを
含有しない比較焼結合金1、並びに(Ti、W、
Zr)Cを含有しない比較焼結合金2、3は、焼結
性および耐衝撃性に劣るものであるために、特に
連続切削試験では全切刃あるいはほとんどの切刃
に欠損が発生し、また(Ti、W、Zr)Cの含有
量がこの発明の範囲から高い方に外れた比較焼結
合金4、5は、比較的すぐれた耐摩耗性を示すも
のの、靭性が劣るものであるため、断続切削試験
ではほとんどの切刃に欠損が発生した。さらに従
来切削チツプ1、2は耐摩耗性および耐衝撃性に
劣り、きわめて悪い切削性能しか示さないことが
明らかである。
実施例 2
原料粉末として、実施例1で用いた原料粉末の
ほかに、平均粒径1.5μmを有するTiC0.7N0.3粉
末、同1.2μmのTiC0.6N0.4粉末、同1.0μmの
TiC0.5N0.5粉末、同1.5μmのTiC0.4N0.6粉末、同
1.2μmのZrC0.7N0.3粉末、および同1.0μmの
HfC0.7N0.3粉末(以上重量比)を用意し、これら
原料粉末を、第4表に示される配合組成に配合し
た後、実施例1におけると同一の条件で湿式粉砕
混合し、乾燥し、成形して圧粉体とし、ついでそ
れぞれ第4表に示される各種圧力のN2ガスある
いはArガス雰囲気中、温度:2000℃に2時間保
持の条件で焼結することによつて、第5表に示さ
れる成分組成をもつた本発明焼結合金32〜49をそ
れぞれ製造した。[Table] Among the 10 test cutting edges, the number of cutting edges with chipping was measured. The results of these measurements are shown in Table 3. For comparison purposes, an ISO P10 grade WC-based cemented carbide cutting tip (hereinafter referred to as conventional cutting tip 1) and TiC-10%Mo-15%
A cutting test was also conducted under the above cutting conditions for a TiC-based cermet cutting tip (hereinafter referred to as conventional cutting tip 2) having a composition of Ni (the above weight %, below % indicates weight %), and the results are also shown in Table 3. It was shown to. As is clear from the results shown in Table 3, all of the sintered alloys 1 to 31 of the present invention have high hardness and high toughness, and exhibit excellent wear resistance and impact resistance in all cutting tests. In contrast, comparative sintered alloy 1 containing no MgO and (Ti, W,
Comparative sintered alloys 2 and 3 that do not contain Zr)C have inferior sintering properties and impact resistance, so in continuous cutting tests in particular, all or most of the cutting edges were damaged, and Comparative sintered alloys 4 and 5, in which the content of (Ti, W, Zr)C is higher than the range of the present invention, show relatively excellent wear resistance but have poor toughness. In the interrupted cutting test, most of the cutting edges were damaged. Furthermore, it is clear that the conventional cutting chips 1, 2 have poor wear resistance and impact resistance, and exhibit very poor cutting performance. Example 2 In addition to the raw material powder used in Example 1, as raw material powders, TiC 0.7 N 0.3 powder with an average particle size of 1.5 μm, TiC 0.6 N 0.4 powder with an average particle size of 1.2 μm, 1.0 μm
TiC 0.5 N 0.5 powder, 1.5 μm TiC 0.4 N 0.6 powder ,
1.2 μm ZrC 0.7 N 0.3 powder and 1.0 μm ZrC 0.7 N 0.3 powder .
HfC 0.7 N 0.3 powder ( weight ratio above) was prepared, these raw material powders were blended into the composition shown in Table 4, and then wet-pulverized and mixed under the same conditions as in Example 1. By drying, molding to form a compact, and then sintering at a temperature of 2000 °C for 2 hours in an N2 gas or Ar gas atmosphere at various pressures shown in Table 4, Sintered alloys 32 to 49 of the present invention having the component compositions shown in Table 5 were manufactured, respectively.
【表】【table】
【表】
ついで、この結果得られた本発明焼結合金32〜
49について、硬さおよび抗折力を測定すると共
に、これよりSNP433の形状をもつた切削チツプ
を切出し、さらに比較の目的で用意したISOの
P30グレードのWC基超硬合金製切削チツプ(以
下従来切削チツプという)と共に、
被削材:SNCM―8(硬さ:HB265)、
切削速度:100m/min、
送り:0.8mm/rev.、
切込み:4mm、
切削時間:10min、
の条件での高送り連続切削試験、並びに、
被削材:SNCM―8(硬さ:HB275)、
切削速度:100m/min、
送り:0.45mm/rev.、
切込み:3mm、
切削時間:3min、
の条件での断続切削試験を行ない、実施例1にお
けると同様に、それぞれ切刃の逃げ面摩耗幅およ
びすくい面摩耗深さ、並びに欠損切刃数を測定し[Table] Next, the resulting sintered alloys of the present invention 32~
49, the hardness and transverse rupture strength were measured, and cutting chips with the shape of SNP433 were cut from this, and ISO chips prepared for comparison purposes were also measured.
Along with P30 grade WC-based cemented carbide cutting tips (hereinafter referred to as conventional cutting tips), workpiece material: SNCM-8 (hardness: H B 265), cutting speed: 100m/min, feed: 0.8mm/rev. , Depth of cut: 4 mm, Cutting time: 10 min, High feed continuous cutting test under the conditions of , Work material: SNCM-8 (hardness: H B 275), Cutting speed: 100 m/min, Feed: 0.45 mm/ An interrupted cutting test was conducted under the following conditions: rev., depth of cut: 3 mm, cutting time: 3 min, and as in Example 1, the flank wear width and rake face wear depth of the cutting edge, as well as the number of missing cutting edges, were measured. measure
【表】
た。これらの測定結果を第6表に合せて示した。
第6表に示される結果から、本発明焼結合金32
〜49は、いずれも高硬度および高靭性を有し、高
送り連続切削および断続切削においてすぐれた切
削性能を示すのに対して、従来切削チツプ3は特
に耐塑性変形性に劣るために高送り連続切削試験
では3分で切削不能となるものであつた。
実施例 3
原料粉末として、実施例1で用いた粉末のほか
に、さらに不純物として、平均粒径0.8μmのMo
粉末、同2.5μmのNi粉末、同1.2μmのCo粉末、
および同3.0μmのRe粉末を用意し、これら原料
粉末をそれぞれ第7表に示される配合組成に配合
した後、実施例1におけると同一の条件で湿式粉
砕混合し、乾燥し、成形して圧粉体とし、ついで
これらの圧粉体を、300torrの窒素雰囲気中で、
それぞれ第6表に示される温度に2時間保持の条
件で焼結することによつて、同じく第8表に示さ
れる成分組成をもつた本発明焼結合金50〜79およ
び比較焼結合金6〜13をそれぞれ製造した。[Table] These measurement results are also shown in Table 6. From the results shown in Table 6, the present invention sintered alloy 32
-49 all have high hardness and high toughness, and show excellent cutting performance in high-feed continuous cutting and interrupted cutting, whereas conventional cutting tip 3 has particularly poor plastic deformation resistance, so it is difficult to use high-feed cutting. In a continuous cutting test, it became impossible to cut after 3 minutes. Example 3 In addition to the powder used in Example 1, as a raw material powder, Mo with an average particle size of 0.8 μm was added as an impurity.
powder, 2.5μm Ni powder, 1.2μm Co powder,
After preparing the same 3.0 μm Re powder and blending these raw powders into the compositions shown in Table 7, they were wet-pulverized and mixed under the same conditions as in Example 1, dried, molded, and pressed. powder, and then these green compacts in a nitrogen atmosphere of 300 torr,
Sintered alloys 50 to 79 of the present invention and comparative sintered alloys 6 to 6, each having the composition shown in Table 8, were obtained by sintering them at the temperatures shown in Table 6 for 2 hours. 13 were produced respectively.
【表】【table】
【表】【table】
【表】【table】
【表】
つぎに、これらの本発明焼結合金50〜79および
比較焼結合金6〜13について、硬さおよび抗折力
を測定すると共に、これよりSNP433の形状をも
つた切削チツプを切出し、さらに比較の目的で用
意したISOのP40グレードのWC基超硬合金製切
削チツプ(以下従来切削チツプ4という)と共
に、
被削材:SNCM―8(硬さ:HB265)、
切削速度:60m/min、
送り:0.7mm/rev.、
切込み:10mm、
切削時間:3min、
の条件での高送り連続切削試験、並びに、
被削材:SNCM―8(硬さ:HB275)、
切削速度:80m/min、
送り:0.5mm/rev.、
切込み:3mm、
切削時間:3min、
の条件での断続切削試験を行ない、実施例1にお
けると同様に、それぞれ切刃の逃げ面摩耗幅およ[Table] Next, hardness and transverse rupture strength were measured for these sintered alloys 50 to 79 of the present invention and comparative sintered alloys 6 to 13, and cutting chips with the shape of SNP433 were cut from them. Furthermore, along with an ISO P40 grade WC-based cemented carbide cutting chip (hereinafter referred to as conventional cutting chip 4) prepared for comparison purposes, workpiece material: SNCM-8 (hardness: H B 265), cutting speed: 60 m /min, Feed: 0.7mm/rev., Depth of cut: 10mm, Cutting time: 3min, High feed continuous cutting test under the following conditions, Work material: SNCM-8 (Hardness: H B 275), Cutting speed An interrupted cutting test was conducted under the following conditions: : 80 m/min, feed: 0.5 mm/rev., depth of cut: 3 mm, cutting time: 3 min, and as in Example 1, the width of flank wear of the cutting edge and
【表】【table】
【表】
びすくい面摩耗深さ、並びに欠損切刃数を測定し
た。これらの測定結果を第9表に合せて示した。
第9表に示される結果から、本発明焼結合金50
〜79は、いずれも高硬度および高靭性を有し、い
ずれの切削試験でもすぐれた性能を示し、特に本
発明焼結合金56〜59、および同76〜79に見られる
ように、Mo、Ni、Co、またはReなどの不純物を
含有しても、その含有量が1%以下であれば焼結
合金の特性にほとんど影響を及ぼさないことが明
らかである。これに対してMgOまたはAl2O3の配
合(含有)量がこの発明の範囲から高い方に外れ
た比較焼結合金6および7、複合炭・窒化物固溶
体の含有量がこの発明の範囲から低い方に外れた
比較焼結合金8および9、不純物たるNiの含有
量が1%を越えて高い比較焼結合金10および11、
さらに焼結温度がこの発明の範囲から外れて低い
条件で製造した比較焼結合金12および13において
は、いずれも靭性不足が原因で、きわめて悪い切
削性能しか示さず、また従来切削チツプ4は、本
発明焼結合金とほぼ同等のすぐれた耐衝撃性をも
つものの、耐塑性変形性に劣るために高送り連続
切削試験では0.8分で切削不能に至るものであつ
た。
上述のように、この発明の超耐熱焼結合金は、
高靭性および高硬度を有し、かつ耐摩耗性、耐塑
性変形性、および耐衝撃性にすぐれているので、
これらの特性が要求される鋼の高速切削や重切削
などに切削工具として用いた場合にすぐれた切削
性能を示し、さらに熱間圧延ロール、熱間線引ロ
ール、熱間圧縮ダイス、熱間鍛造ダイス、さらに
は熱間押出しパンチなどの比較的長時間高温にさ
らされる熱間加工用工具として用いた場合にもす
ぐれた性能を長期に亘つて発揮するなど工業上有
用な特性を有するのである。[Table] The wear depth of the rake face and the number of chipped cutting edges were measured. These measurement results are also shown in Table 9. From the results shown in Table 9, the present invention sintered alloy 50
-79 all have high hardness and high toughness, and show excellent performance in all cutting tests.In particular, as seen in the present invention sintered alloys 56-59 and 76-79, Mo, Ni It is clear that even if impurities such as , Co, or Re are contained, if the content is 1% or less, the properties of the sintered alloy are hardly affected. On the other hand, Comparative Sintered Alloys 6 and 7 have a blending (content) amount of MgO or Al 2 O 3 that is outside the range of the present invention, and Comparative Sintered Alloys 6 and 7 have a content of composite carbon/nitride solid solution that is outside the range of the present invention. Comparative sintered alloys 8 and 9 are on the lower side, comparative sintered alloys 10 and 11 have a high content of Ni as an impurity, exceeding 1%,
Furthermore, Comparative Sintered Alloys 12 and 13, which were manufactured at a low sintering temperature outside the range of the present invention, both exhibited extremely poor cutting performance due to insufficient toughness, and the conventional cutting tip 4 exhibited extremely poor cutting performance. Although it had excellent impact resistance almost equivalent to that of the sintered alloy of the present invention, it was inferior in plastic deformation resistance and could not be cut in 0.8 minutes in a high-feed continuous cutting test. As mentioned above, the super heat-resistant sintered alloy of this invention is
It has high toughness and hardness, as well as excellent wear resistance, plastic deformation resistance, and impact resistance.
It exhibits excellent cutting performance when used as a cutting tool for high-speed cutting and heavy cutting of steel that require these characteristics, and is also suitable for hot rolling rolls, hot drawing rolls, hot compression dies, hot forging. It has industrially useful properties such as exhibiting excellent performance over a long period of time when used as a hot processing tool such as a die or even a hot extrusion punch that is exposed to high temperatures for a relatively long period of time.
Claims (1)
よびHfのうちの1種または2種との複合炭化物
固溶体および複合炭窒化物固溶体のうちのいずれ
か1種:10〜60%、 同じく硬質相形成成分としての酸化マグネシウ
ム:0.01〜1%、 結合相形成成分としてのWおよび不可避不純
物:残り、 からなる組成(以上重量%)を有し、かつ上記の
複合炭化物固溶体および複合炭窒化物固溶体は、
TiおよびWに富む相と、ZrおよびHfのいずれ
か、または両方に富む相との2相構造を有するこ
とを特徴とする高靭性および高硬度を有し、かつ
耐摩耗性、耐塑性変形性、および耐衝撃性にすぐ
れた超耐熱焼結合金。 2 硬質相形成成分としてのTiと、Wと、Zrお
よびHfのうちの1種または2種との複合炭化物
固溶体および複合炭窒化物固溶体のうちのいずれ
か1種:10〜60%、 同じく硬質相形成成分としての酸化マグネシウ
ム:0.01〜1%、 同じく硬質相形成成分としての酸化アルミニウ
ムおよび酸化イツトリウムのうちの1種または2
種:0.5〜10%、 結合相形成成分としてのWおよび不可避不純
物:残り からなる組成(以上重量%)を有し、かつ上記の
複合炭化物固溶体および複合炭窒化物固溶体は、
TiおよびWに富む相と、ZrおよびHfのいずれ
か、または両方に富む相との2相構造を有するこ
とを特徴とする高靭性および高硬度を有し、かつ
耐摩耗性、耐塑性変形性、および耐衝撃性にすぐ
れた超耐熱焼結合金。[Claims] 1 Any one of a composite carbide solid solution and a composite carbonitride solid solution of Ti, W, and one or two of Zr and Hf as hard phase forming components: 10 -60%, magnesium oxide as a hard phase forming component: 0.01 to 1%, W as a binder phase forming component and unavoidable impurities: the remainder (weight%), and the above composite carbide solid solution and composite carbonitride solid solution,
It has a two-phase structure of a phase rich in Ti and W and a phase rich in either or both of Zr and Hf.It has high toughness and hardness, and has good wear resistance and plastic deformation resistance. , and a super heat-resistant sintered alloy with excellent impact resistance. 2 Any one of composite carbide solid solutions and composite carbonitride solid solutions of Ti as hard phase forming components, W, and one or two of Zr and Hf: 10 to 60%, also hard Magnesium oxide as a phase-forming component: 0.01 to 1%, and one or two of aluminum oxide and yttrium oxide as hard phase-forming components.
Species: 0.5 to 10%, W as a binder phase forming component, and unavoidable impurities: the remainder (weight%), and the above composite carbide solid solution and composite carbonitride solid solution,
It has a two-phase structure of a phase rich in Ti and W and a phase rich in either or both of Zr and Hf.It has high toughness and hardness, and has good wear resistance and plastic deformation resistance. , and a super heat-resistant sintered alloy with excellent impact resistance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58048499A JPS59173237A (en) | 1983-03-23 | 1983-03-23 | Ultra-heat resistant sintered alloy and preparation thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58048499A JPS59173237A (en) | 1983-03-23 | 1983-03-23 | Ultra-heat resistant sintered alloy and preparation thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59173237A JPS59173237A (en) | 1984-10-01 |
| JPS621464B2 true JPS621464B2 (en) | 1987-01-13 |
Family
ID=12805067
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58048499A Granted JPS59173237A (en) | 1983-03-23 | 1983-03-23 | Ultra-heat resistant sintered alloy and preparation thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59173237A (en) |
-
1983
- 1983-03-23 JP JP58048499A patent/JPS59173237A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59173237A (en) | 1984-10-01 |
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