Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPH0333771B2 - - Google Patents
[go: Go Back, main page]

JPH0333771B2 - - Google Patents

Info

Publication number
JPH0333771B2
JPH0333771B2 JP62121762A JP12176287A JPH0333771B2 JP H0333771 B2 JPH0333771 B2 JP H0333771B2 JP 62121762 A JP62121762 A JP 62121762A JP 12176287 A JP12176287 A JP 12176287A JP H0333771 B2 JPH0333771 B2 JP H0333771B2
Authority
JP
Japan
Prior art keywords
hard phase
carbide
nitrogen
sintered alloy
based 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 - Lifetime
Application number
JP62121762A
Other languages
Japanese (ja)
Other versions
JPS63286550A (en
Inventor
Takeshi Saito
Kozo Kitamura
Mitsuo Ueki
Keiichi Kobori
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.)
Tungaloy Corp
Original Assignee
Toshiba Tungaloy Co Ltd
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 Toshiba Tungaloy Co Ltd filed Critical Toshiba Tungaloy Co Ltd
Priority to JP12176287A priority Critical patent/JPS63286550A/en
Publication of JPS63286550A publication Critical patent/JPS63286550A/en
Publication of JPH0333771B2 publication Critical patent/JPH0333771B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Cutting Tools, Boring Holders, And Turrets (AREA)

Description

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

(産業上の利用分野) 本発明は、耐摩耗工具部品又は切削工具部品に
適する強度、耐摩耗性及び耐熱変形性にすぐれた
窒素含有炭化チタン基焼結合金に関するものであ
る。 (従来の技術) 一般に、炭化タングステンに比較して炭化チタ
ンは、鉄族金属との親和性に乏しく、又耐酸化性
にすぐれている。このらの理由から、特に鉄系材
料を切削するための切削工具部品用には、WC基
焼結合金に代り、TiCを主成分としたTiC基焼結
合金が実用化されている。しかしながら、TiC基
焼結合金は、WC基焼結合金に比較して強度が低
く、しかも高温における耐塑性変形性が劣るとい
う問題がある。これらの問題点の解決法として窒
素を含有したTiC基焼結合金が多数提案されてい
る。窒素を含有したTiC基焼結合金の代表例とし
ては、特開昭51−93711号公報及び特公昭56−
51201号公報がある。 (発明が解決しようとする問題点) 特開昭51−93711号公報は、重量%で、炭化タ
ングステン10〜60%、炭化チタン5〜40%、炭化
タンタル5〜30%、窒化チタン3〜20%、コバル
ト、ニツケル、鉄等の鉄族金属5〜20%の成分か
らなることを特徴とする切削用超硬合金である。
この特開昭51−93711号公報の合金は、TiCを主
成分とする組成に窒化チタンを添加することによ
り固溶体粒子の粒成長を抑制して微細結晶粒に
し、その結果、窒素無含有のTiC基焼結合金に比
べて高硬度で、耐摩耗性が向上しているものであ
る。また、窒化チタンは炭化チタンに比べて熱衝
撃抵抗が大きいことから、窒素無含有のTiC基焼
結合金に比較して耐熱衝撃性が改善されているも
のである。しかしながら、特開昭51−93711号公
報の合金は、窒素無含有のTiC基焼結合金と同様
に炭化チタンを核に持つ有核組織であるために結
晶粒の微細化が顕著でなく、しかも高温における
耐塑性変形性が劣るという問題がある。 特公昭56−51201号公報は、窒素を含有した
TiC基焼結合金で、チタン及び窒素に富む炭室化
物固溶体と、第6族金属成分に富むが窒素に乏し
いもう1つの硬質相により成る2相混合物であ
り、2相混合物は微細構造を形成し、チタン及び
窒素に富む炭窒化物相が第6族金属に富むが窒素
に乏しい相に包囲され、結合相合金との主界面を
形成していることを特徴とするものである。この
特公昭56−51201号公報の合金は、窒素無含有の
TiC基焼結合金と異なり、チタン及び窒素に富む
炭窒化物相を芯部にしたものであることから微細
結晶粒になつており、このために耐摩耗性、強度
及び耐熱変形性などの合金特性がすぐれているも
のである。しかしながら、この特公昭56−51201
号公報の合金は、スピノダル領域内に含まれる選
択された組成で、スピノダル反応を利用して作製
するものであるために、出発原料粉末、焼結時に
用いる焼結炉及び焼結雰囲気などの製造条件の制
御を従来の粉末冶金法と異なり非常に厳しくしな
ければ作製できないという問題がある。 本発明は、上述のような問題点を解決したもの
で、具体的には、TiとWとを含有する炭化物を
芯部とし、この芯部が炭窒化物の外周部で包囲さ
れてなる有芯構造の硬質相を焼結合金中に形成さ
せたもので、耐摩耗性、強度及び高温における耐
熱変形性のすぐれた窒素含有の炭化チタン基焼結
合金の提供を目的とするものである。 (問題点を解決するための手段) 本発明者らは、窒素を含有したTiC基焼結合金
の基本系であるTiC−TiN−Mo2C−Ni系合金
に、他の各種の炭化物を添加し、その添加炭化物
の役割について検討していた所、特に窒化チタン
と炭化モリブテンとの合計量に対する炭化タング
ステン量を適量添加し、焼結時の雰囲気制御によ
つては、他炭化物の添加に比較して合金組織が著
しく微細になり、しかも高温硬さが改良され、高
強度で、切削時の耐刃先変形性にすぐれるという
知見を得たものである。この知見に基づいて、本
発明を完成するに至つたものである。 すなわち、本発明の耐熱変形性にすぐれた窒素
含有炭化チタン基焼結合金は、Ni及び/又はCo
でなる結合相3〜18wt%と、残り硬質相と不可
避不純物とからなり、該硬質相は7〜34wt%の
窒化チタンと4〜24.5wt%の炭化タングステンと
4〜12.5wt%の炭化モリブデンと、さらに2wt%
以下の炭化ハフニウム、2wt%以下の炭化ジルコ
ニウム、5wt%以下の炭化ニオブ又は10wt%以下
の炭化タンタルの中の少なくとも1種と、残り炭
化チタンとからなる組成であつて、かつ該硬質相
はTiとWとを含有した複合炭化物の芯部をTiと
WとMoとHf、Zr、Nb、Taの中の少なくとも1
種とを含有した複合炭窒化物の外周部で包囲して
なる第1硬質相を0.4〜7vol%含有している(但
し、硬質相中に、窒化チタンの芯部を周期律表
4a、5a、6a族金属の炭化物及び窒化物の中の2
種以上の相互固溶体の外周部で包囲してなる有芯
硬質相を0.5〜5vol%含有している場合は除く。)
ことを特徴とするものである。 この本発明の耐熱変形性にすぐれた窒素含有炭
化チタン基焼結合金における硬質相は、具体的に
は、(Ti、W)Cの複合炭化物でなる芯部を
(Ti、W、Mo、M)(C、N)の複合炭窒化物
(以下、MはHf、Zr、Nb、Taの中の少なくとも
1種を表わす。)でなる外周部で包囲された第1
硬質相が0.4〜7vol%含有しているものである。
この第1硬質相を除いた、残りの硬質相は、例え
ばTiCの炭化物でなる芯部を(Ti、W、Mo、
M)(C、N)の複合炭窒化物でなる外周部で包
囲された第2硬質相、(Ti、W)(C、N)の複
合炭窒化物でなる芯部を(Ti、W、Mo、M)
(C、N)の複合炭窒化物でなる外周部で包囲さ
れた第3硬質相、Ti(C、N)の炭窒化物でなる
芯部を(Ti、W、Mo、M)(C、N)の複合炭
窒化物でなる外周部で包囲された第4硬質相、又
はTiNの窒化物でなる芯部を(Ti、W、Mo、
M)(C、N)の複合炭窒化物でなる外周部で包
囲された第5硬質相(但し、第5硬質相が0.5〜
5vol%含有している場合は除く。)などを挙げる
ことができる。特に、易焼結性及び焼結合金の耐
熱変形性から、硬質相は、第1硬質相と第2硬質
相とからなることが好ましいものである。これら
の硬質相を構成している芯部及び外周部は、化学
量組成又は非化学量論組成でなつているものであ
る。この硬質相として含有している第1硬質相の
平均粒径が0.1〜1.5μmであると、強度及び耐熱
変形性にすぐれる傾向にあることから、特に好ま
しいものである。また、第1硬質相を除いた、残
りの硬質相の平均粒径が3μm以下、好ましくは
1.0μm以下であると焼結合金の諸特性がすぐれる
傾向になる。 本発明の耐熱変形性にすぐれた窒素含有炭化チ
タン基焼結合金における結合相は、Ni及び/又
はCoでなるもので、他に硬質相を構成している
元素、特にMoとCが0.1%以下の不純物程度に固
溶している場合もある。 次に、本発明の耐熱変形性にすぐれた窒素含有
炭化チタン基焼結合金において、数値限定した理
由を以下に述べる。 結合相が3wt%未満になると、相対的に硬質相
が97wt%を超えて多くなるために難焼結性にな
る。このために、緻密で強度の高い合金を得るの
が困難になる。逆に、結合相が18wt%を超えて
多くなると、相対的に硬質相が82wt%未満にな
るために耐摩耗性が低下する。このために、結合
相は、3〜18wt%と定めたものである。 硬質相中の窒化チタンが7wt%未満になると、
硬質相全体が粗粒化の傾向を示し、耐摩耗性が低
下する。逆に、窒化チタンが34wt%を超えて多
くなると、難焼結性になり、緻密な焼結合金を得
るのが困難になる。このために、硬質相中の窒化
チタンは、7〜34wt%と定めたものである。 硬質相中の炭化タングステンが4wt%未満にな
ると、(Ti、W)Cを芯部とする第1硬質相が
0.4vol%未満となつて、硬質相を粗粒化し、耐摩
耗性及び耐塑性変形性の低下となる。逆に、炭化
タングステンが24.5wt%を超えて多くなると、硬
質相中に炭化タングステンが析出し、硬質相の微
細化を阻害して、強度を低下する。このために、
硬質相中の炭化タングステンは、4〜24.5wt%と
定めたものである。 硬質相中の炭化モリブデンが4wt%未満になる
と、難焼結性になり、緻密な焼結合金を得るのが
困難になる。逆に、炭化モリブデンが12.5wt%を
超えて多くなると、硬質相を形成している外周部
が粗大化して、強度低下となる。このために、硬
質相中の炭化モリブデンは、4〜12.5wt%と定め
たものである。 硬質相中に2wt%を超えた炭化ハフニウム、
2wt%を超えた炭化ジルコニウム、5wt%を超え
た炭化ニオブ、10wt%を超えた炭化タンタルが
存在すると、外周部が厚くなり、結局硬質相の粗
粒化が生じて強度低下になる。このために、硬質
相中には、炭化ハフニウム2wt%以下、炭化ジル
コニウム2wt%以下、炭化ニオブ5wt%以下、炭
化タンタル10wt%以下と定めたものである。 硬質相中の第1硬質相が0.4vol%未満になる
と、硬質相が粗粒化し、強度及び耐熱変形性を低
下する。逆に、第1硬質相が7vol%を超えて多く
なると炭化タングステンが析出し、硬質相の微細
化を阻害して強度及び耐熱変形性を低下する。こ
のために、硬質相中の第1硬質相は、0.4〜7vol
%と定めたものである。 本発明の耐熱変形性にすぐれた窒素含有炭化チ
タン基焼結合金を作製するには、出発原料粉末に
平均粒径が3μm以下のものを用いて、有機溶媒
中で湿式混合粉砕し、この混合粉砕粉末を従来の
粉末冶金法における成形方法でもつて成形した
後、必要に応じて脱脂処理後、真空中で1400〜
1500℃の温度で保持して焼結すればよい。特に、
焼結合金中に第1硬質相を形成させるために重要
なことは、成形後の圧粉体に付着又は固溶してい
る酸素量をできるだけ少なくし、焼結時の液相発
生までの昇温中は、H2、H2−CO、H2−N2又は
H2−CO−N2の減圧状ガス雰囲気にし、次いで液
相発生から焼結完了までを少し高真空にするのが
よい。 (作用) 本発明の耐熱変形性にすぐれた窒素含有炭化チ
タン基焼結合金は、第1硬質相が硬質相全体の結
晶を微細にする作用をし、特に第1硬質相中の芯
部に固溶しているWが第1硬質相の結晶を微細に
すると共に、硬質相全体の結晶を微細にする作用
をしているものである。また、硬質相の外周部中
に存在するHf、Zr、Nb、Taの中の少なくとも
1種は、耐酸化性を向上する作用、耐熱変形性を
向上する作用及び強度向上の作用がある。これら
の第1硬質相中の芯部と硬質相の外周部を形成し
ている複合炭窒化物との相互作用により、本発明
の焼結合金は、室温及び高温での硬さの向上、強
度の向上並びに耐摩耗性、耐酸化性及び耐熱変形
性にすぐれるという作用をもたらしてるものであ
る。 (実施例) 実施例 1 平均粒径1μmのWC粉末、平均粒径1〜3μmの
各種炭化物粉末、窒化物粉末、Ni粉末及びCo粉
末を出発原料として用いて、第1表の各試料を配
合した。この第1表の各試料をステンレス製容
器、超硬合金製ボールを用いてヘキサン溶媒中で
40時間混合した後、パラフイン混合、乾燥及び
1ton/cm2圧力で成形した。次に、成形圧粉体を真
空炉に設置して、1×10-2Torrの真空にした後、
H2−COの減圧ガス中で1350℃まで昇温し、次い
で5×10-2Torrの真空中、1400〜1500℃で1時
間保持にて焼結した。こうした得た本発明の焼結
合金の室温での硬さ、1000℃での硬さ、室温での
抵抗力を測定し、その結果を第2表に示した。ま
た、各焼結合金をX線マイクロアナライザー、走
査型電子顕微鏡により組織観察し、特に第1硬質
相の平均粒径及びその含有量を求めて第2表に併
記した。尚、比較品として、焼結条件が5×
10-2Torrの真空中の他は、上述と同様に行つて
得た比較品も第1表及び第2表に併記した。
(Industrial Application Field) The present invention relates to a nitrogen-containing titanium carbide-based sintered alloy that is suitable for wear-resistant tool parts or cutting tool parts and has excellent strength, wear resistance, and heat deformation resistance. (Prior Art) Generally, titanium carbide has poor affinity with iron group metals and has excellent oxidation resistance compared to tungsten carbide. For these reasons, TiC-based sintered alloys containing TiC as a main component have been put into practical use instead of WC-based sintered alloys, especially for cutting tool parts for cutting ferrous materials. However, TiC-based sintered alloys have a problem of lower strength than WC-based sintered alloys and poor plastic deformation resistance at high temperatures. As a solution to these problems, many nitrogen-containing TiC-based sintered alloys have been proposed. Representative examples of nitrogen-containing TiC-based sintered alloys include JP-A-51-93711 and JP-B-Sho 56-
There is a publication number 51201. (Problems to be Solved by the Invention) JP-A-51-93711 discloses that, in weight percent, tungsten carbide is 10 to 60%, titanium carbide is 5 to 40%, tantalum carbide is 5 to 30%, and titanium nitride is 3 to 20%. %, cobalt, nickel, iron, and other iron group metals by 5 to 20%.
The alloy disclosed in JP-A-51-93711 suppresses the grain growth of solid solution particles and makes fine crystal grains by adding titanium nitride to a composition whose main component is TiC. It has higher hardness and improved wear resistance than base sintered alloys. Furthermore, since titanium nitride has higher thermal shock resistance than titanium carbide, the thermal shock resistance is improved compared to a nitrogen-free TiC-based sintered alloy. However, the alloy disclosed in JP-A-51-93711 has a nucleated structure with titanium carbide as the nucleus, similar to the nitrogen-free TiC-based sintered alloy, so the grain refinement is not remarkable. There is a problem that the plastic deformation resistance at high temperatures is poor. Japanese Patent Publication No. 56-51201 discloses that nitrogen-containing
It is a TiC-based sintered alloy, which is a two-phase mixture consisting of a carbide solid solution rich in titanium and nitrogen and another hard phase rich in Group 6 metal components but poor in nitrogen, and the two-phase mixture forms a microstructure. However, it is characterized in that a carbonitride phase rich in titanium and nitrogen is surrounded by a phase rich in Group 6 metals but poor in nitrogen, forming the main interface with the binder phase alloy. The alloy disclosed in Japanese Patent Publication No. 56-51201 is a nitrogen-free alloy.
Unlike TiC-based sintered alloys, the core is a carbonitride phase rich in titanium and nitrogen, resulting in fine grains. It has excellent characteristics. However, this special public service 56-51201
The alloy disclosed in the publication has a selected composition within the spinodal region and is produced using a spinodal reaction, so it requires manufacturing of the starting raw material powder, the sintering furnace used during sintering, the sintering atmosphere, etc. Unlike the conventional powder metallurgy method, there is a problem in that it cannot be manufactured unless the conditions are controlled very strictly. The present invention solves the above-mentioned problems. Specifically, the present invention has a core made of a carbide containing Ti and W, and this core is surrounded by an outer periphery of carbonitride. The purpose of this invention is to provide a nitrogen-containing titanium carbide-based sintered alloy in which a hard phase with a core structure is formed in a sintered alloy, and which has excellent wear resistance, strength, and heat deformation resistance at high temperatures. (Means for solving the problem) The present inventors added various other carbides to TiC-TiN-Mo 2 C-Ni alloy, which is the basic system of nitrogen-containing TiC-based sintered alloy. However, when we were considering the role of added carbide, we found that by adding an appropriate amount of tungsten carbide relative to the total amount of titanium nitride and molybdenum carbide, and by controlling the atmosphere during sintering, compared to the addition of other carbides. It was discovered that the alloy structure becomes extremely fine, the high-temperature hardness is improved, the strength is high, and the edge deformation resistance during cutting is excellent. Based on this knowledge, we have completed the present invention. That is, the nitrogen-containing titanium carbide-based sintered alloy of the present invention, which has excellent heat deformation resistance, contains Ni and/or Co.
The hard phase consists of 7 to 34 wt% of titanium nitride, 4 to 24.5 wt% of tungsten carbide, and 4 to 12.5 wt% of molybdenum carbide. , plus 2wt%
A composition consisting of at least one of the following hafnium carbide, 2wt% or less zirconium carbide, 5wt% or less niobium carbide, or 10wt% or less tantalum carbide, and the remainder titanium carbide, and the hard phase is Ti The core of the composite carbide containing Ti, W, Mo, and at least one of Hf, Zr, Nb, and Ta
It contains 0.4 to 7 vol% of the first hard phase surrounded by the outer periphery of composite carbonitride containing seeds (however, the hard phase contains a core of titanium nitride according to the periodic table).
2 of carbides and nitrides of group 4a, 5a, 6a metals
Cases containing 0.5 to 5 vol% of a cored hard phase surrounded by the outer periphery of more than one type of mutual solid solution are excluded. )
It is characterized by this. Specifically, the hard phase in the nitrogen-containing titanium carbide-based sintered alloy with excellent heat deformation resistance of the present invention has a core made of a composite carbide of (Ti, W)C (Ti, W, Mo, M ) (C, N) (hereinafter, M represents at least one of Hf, Zr, Nb, Ta).
It contains 0.4 to 7 vol% of hard phase.
The remaining hard phase, excluding this first hard phase, has a core made of, for example, TiC carbide (Ti, W, Mo,
M) A second hard phase surrounded by an outer peripheral part made of a composite carbonitride of (C, N), a core part made of a composite carbonitride of (Ti, W) (C, N), Mo, M)
A third hard phase surrounded by a composite carbonitride of (C,N), a core made of carbonitride of Ti(C,N), (Ti, W, Mo,
M) A fifth hard phase surrounded by an outer periphery made of a composite carbonitride of (C, N) (however, the fifth hard phase is 0.5~
Excludes cases containing 5vol%. ), etc. In particular, from the viewpoint of easy sinterability and heat deformation resistance of the sintered alloy, it is preferable that the hard phase consists of a first hard phase and a second hard phase. The core portion and the outer peripheral portion constituting these hard phases have a stoichiometric composition or a non-stoichiometric composition. It is particularly preferable that the average particle diameter of the first hard phase contained as the hard phase is from 0.1 to 1.5 μm, since it tends to have excellent strength and heat deformation resistance. Further, the average particle size of the remaining hard phase excluding the first hard phase is preferably 3 μm or less, preferably
When the thickness is 1.0 μm or less, the properties of the sintered alloy tend to be excellent. The binder phase in the nitrogen-containing titanium carbide-based sintered alloy with excellent heat deformation resistance of the present invention is composed of Ni and/or Co, and 0.1% of other elements constituting the hard phase, particularly Mo and C. In some cases, the following impurities are dissolved in solid solution. Next, the reasons for limiting the numerical values in the nitrogen-containing titanium carbide-based sintered alloy with excellent heat deformation resistance of the present invention will be described below. When the binder phase is less than 3 wt%, the hard phase becomes relatively large, exceeding 97 wt%, making sintering difficult. This makes it difficult to obtain a dense and strong alloy. On the other hand, if the binder phase exceeds 18 wt%, the hard phase becomes relatively less than 82 wt%, resulting in a decrease in wear resistance. For this purpose, the content of the binder phase is determined to be 3 to 18 wt%. When titanium nitride in the hard phase is less than 7wt%,
The entire hard phase shows a tendency towards coarse graining, reducing wear resistance. On the other hand, if the amount of titanium nitride exceeds 34 wt%, sintering becomes difficult and it becomes difficult to obtain a dense sintered alloy. For this reason, the content of titanium nitride in the hard phase is determined to be 7 to 34 wt%. When the content of tungsten carbide in the hard phase is less than 4wt%, the first hard phase with (Ti, W)C as the core becomes
When the content is less than 0.4 vol%, the hard phase becomes coarse grained, resulting in a decrease in wear resistance and plastic deformation resistance. Conversely, when the amount of tungsten carbide exceeds 24.5 wt%, tungsten carbide precipitates in the hard phase, inhibits refinement of the hard phase, and reduces strength. For this,
The content of tungsten carbide in the hard phase is determined to be 4 to 24.5 wt%. When molybdenum carbide in the hard phase is less than 4 wt%, sintering becomes difficult and it becomes difficult to obtain a dense sintered alloy. On the other hand, if the amount of molybdenum carbide exceeds 12.5 wt%, the outer periphery forming the hard phase becomes coarse, resulting in a decrease in strength. For this reason, the molybdenum carbide content in the hard phase is determined to be 4 to 12.5 wt%. Hafnium carbide exceeding 2wt% in the hard phase,
If more than 2wt% of zirconium carbide, more than 5wt% of niobium carbide, or more than 10wt% of tantalum carbide is present, the outer periphery becomes thicker, and the hard phase eventually becomes coarser, resulting in a decrease in strength. For this reason, the hard phase contains hafnium carbide at most 2 wt%, zirconium carbide at most 2 wt%, niobium carbide at most 5 wt%, and tantalum carbide at most 10 wt%. When the first hard phase in the hard phase is less than 0.4 vol%, the hard phase becomes coarse grained, and the strength and heat deformation resistance are reduced. On the other hand, if the first hard phase exceeds 7 vol %, tungsten carbide will precipitate, inhibiting the refinement of the hard phase and reducing strength and heat deformation resistance. For this reason, the first hard phase in the hard phase is 0.4 to 7 vol.
%. In order to produce the nitrogen-containing titanium carbide-based sintered alloy with excellent heat deformation resistance of the present invention, starting raw material powder with an average particle size of 3 μm or less is wet-mixed and pulverized in an organic solvent. After molding the pulverized powder using the conventional powder metallurgy molding method, after degreasing as necessary, it is heated to 1400~
It is sufficient to sinter it by holding it at a temperature of 1500°C. especially,
In order to form the first hard phase in the sintered alloy, it is important to minimize the amount of oxygen attached to or dissolved in the green compact after molding, and to increase the amount of oxygen to the point where the liquid phase is generated during sintering. During heating, H 2 , H 2 −CO, H 2 −N 2 or
It is preferable to create a reduced pressure gas atmosphere of H 2 -CO-N 2 and then to create a slightly high vacuum from the generation of the liquid phase to the completion of sintering. (Function) In the nitrogen-containing titanium carbide-based sintered alloy of the present invention, which has excellent heat deformation resistance, the first hard phase acts to make the crystals of the entire hard phase finer, especially in the core part of the first hard phase. The W dissolved in the solid solution functions to make the crystals of the first hard phase fine and also to make the crystals of the entire hard phase fine. Furthermore, at least one of Hf, Zr, Nb, and Ta present in the outer peripheral portion of the hard phase has the effect of improving oxidation resistance, heat deformation resistance, and strength. Due to the interaction between the core in the first hard phase and the composite carbonitride forming the outer periphery of the hard phase, the sintered alloy of the present invention has improved hardness and strength at room and high temperatures. This has the effect of improving the wear resistance, oxidation resistance, and heat deformation resistance. (Example) Example 1 Using WC powder with an average particle size of 1 μm, various carbide powders, nitride powder, Ni powder, and Co powder with an average particle size of 1 to 3 μm as starting materials, each sample in Table 1 was blended. did. Each sample in Table 1 was placed in a hexane solvent using a stainless steel container and a cemented carbide ball.
After mixing for 40 hours, paraffin mixing, drying and
Molding was performed at a pressure of 1 ton/cm 2 . Next, the compacted compact was placed in a vacuum furnace to create a vacuum of 1×10 -2 Torr, and then
The temperature was raised to 1350° C. in a reduced pressure gas of H 2 —CO, and then sintered at 1400 to 1500° C. for 1 hour in a vacuum of 5×10 −2 Torr. The hardness at room temperature, hardness at 1000° C., and resistance at room temperature of the obtained sintered alloy of the present invention were measured, and the results are shown in Table 2. In addition, the structure of each sintered alloy was observed using an X-ray microanalyzer and a scanning electron microscope, and in particular, the average particle size and content of the first hard phase were determined and are also listed in Table 2. In addition, as a comparative product, the sintering conditions are 5×
Comparative products obtained in the same manner as above except in a vacuum of 10 -2 Torr are also listed in Tables 1 and 2.

【表】【table】

【表】 実施例 2 実施例1で得た各試料を用いて、下記の条件に
より切削試験を行い、その結果を第3表に示し
た。 旋削による切削試験条件 被削材 S48C(CHB233) φ250×750 切削速度 250m/min 送り速度 0.3mm/rev 切り込み量 1.5mm 切削時間 10min チツプ形状 SPGN 160308 0.1×(−30゜)ホーニング付 乾式切削
[Table] Example 2 Using each sample obtained in Example 1, a cutting test was conducted under the following conditions, and the results are shown in Table 3. Cutting test conditions by turning Work material S48C (CH B 233) φ250×750 Cutting speed 250m/min Feed rate 0.3mm/rev Depth of cut 1.5mm Cutting time 10min Chip shape SPGN 160308 0.1×(-30°) with honing Dry cutting

【表】【table】

【表】 (発明の効果) 以上の結果、本発明の耐熱変形性にすぐれた窒
素含有炭化チタン基焼結合金は、第1硬質相の存
在してない焼結合金及び本発明から外れた焼結合
金等の比較合金に比べて、硬さが僅かに向上し、
抵抗強度が約20〜60%向上し、鋼切削時における
逃げ面摩耗量が約2/5〜3/4に減少し、鋼切削時に
おける熱変形量が約1/2〜1/8に減少するという効
果がある。 このことから、本発明の焼結合金は、従来の炭
化チタン基焼結合金により用いられている旋削工
具領域用の切削工具部品及びあまり衝撃力が加わ
らない耐摩耗工具部品に他に、さらに高速領域又
は高送り領域用の切削工具部品、フライス用切削
工具部品、エンドミルやドリル等の穴あけ工具用
の切削工具部品、磁気テープ、紙、金属箔板等の
切断工具部品又はダイヤモンド、CBN、TiC、
TiN、Al2O3等の被覆層を形成させるための基材
としても応用できる産業上有用な材料である。
[Table] (Effects of the Invention) As a result, the nitrogen-containing titanium carbide-based sintered alloy of the present invention with excellent heat deformation resistance, the sintered alloy without the first hard phase, and the sintered alloy other than the present invention. Hardness is slightly improved compared to comparative alloys such as bonded metals,
The resistance strength is improved by about 20 to 60%, the amount of flank wear when cutting steel is reduced to about 2/5 to 3/4, and the amount of thermal deformation when cutting steel is reduced to about 1/2 to 1/8. It has the effect of For this reason, the sintered alloy of the present invention can be used in cutting tool parts for turning tool areas and wear-resistant tool parts that are not subjected to much impact force, which are used with conventional titanium carbide-based sintered alloys. Cutting tool parts for areas or high feed areas, cutting tool parts for milling, cutting tool parts for drilling tools such as end mills and drills, cutting tool parts for magnetic tape, paper, metal foil plates, etc., or diamond, CBN, TiC,
It is an industrially useful material that can also be used as a base material for forming coating layers such as TiN and Al 2 O 3 .

Claims (1)

【特許請求の範囲】 1 Ni及び/又はCoでなる結合相3〜18wt%
と、残り硬質相と不可避不純物とからなり、該硬
質相は7〜34wt%の窒化チタンと4〜24.5wt%
の炭化タングステンと4〜12.5wt%の炭化モリブ
デンと、さらに2wt%以下の炭化ハフニウム、
2wt%以下の炭化ジルコニウム、5wt%以下の炭
化ニオブ又は10wt%以下の炭化タンタルの中の
少なくとも1種と、残り炭化チタンとからなる組
成であつて、かつ該硬質相はTiとWとを含有し
た複合炭化物の芯部をTiとWとMoとHf、Zr、
Nb、Taの中の少なくとも1種とを含有した複合
炭窒化物の外周部で包囲してなる第1硬質相を
0.4〜7vol%含有している(但し、硬質相中に、
窒化チタンの芯部を周期律表4a、5a、6a族金属
の炭化物及び窒化物の中の2種以上の相互固溶体
の外周部で包囲してなる有芯硬質相を0.5〜5vol
%含有している場合は除く。)ことを特徴とする
耐熱変形性にすぐれた窒素含有炭化チタン基焼結
合金。 2 上記硬質相は、上記第1硬質相を0.4〜7vol
%と、残り炭化チタンの芯部をTiとWとMoと
Hf、Zr、Nb、Taの中の少なくとも1種とを含
有した複合炭窒化物の外周部で包囲してなる第2
硬質相とからなることを特徴とする特許請求の範
囲第1項記載の耐熱変形性にすぐれた窒素含有炭
化チタン基焼結合金。 3 上記第1硬質相は、平均粒径が0.1〜1.5μm
であることを特徴とする特許請求の範囲第1項又
は第2項記載の耐熱変形性にすぐれた窒素含有炭
化チタン基焼結合金。
[Claims] 1. 3 to 18 wt% binder phase made of Ni and/or Co.
, the remaining hard phase and unavoidable impurities, and the hard phase consists of 7 to 34 wt% titanium nitride and 4 to 24.5 wt% titanium nitride.
of tungsten carbide, 4 to 12.5 wt% of molybdenum carbide, and further 2 wt% or less of hafnium carbide,
A composition consisting of at least one of 2wt% or less zirconium carbide, 5wt% or less niobium carbide, or 10wt% or less tantalum carbide, and the remainder titanium carbide, and the hard phase contains Ti and W. The core of the composite carbide is made of Ti, W, Mo, Hf, Zr,
A first hard phase surrounded by a composite carbonitride containing at least one of Nb and Ta.
Contains 0.4 to 7 vol% (However, in the hard phase,
0.5 to 5 vol.
% is excluded. ) Nitrogen-containing titanium carbide-based sintered alloy with excellent heat deformation resistance. 2 The above hard phase contains 0.4 to 7 vol of the above first hard phase.
% and the remaining titanium carbide core with Ti, W, and Mo.
A second layer surrounded by a composite carbonitride containing at least one of Hf, Zr, Nb, and Ta.
A nitrogen-containing titanium carbide-based sintered alloy having excellent heat deformation resistance as claimed in claim 1, characterized in that the nitrogen-containing titanium carbide-based sintered alloy comprises a hard phase. 3 The first hard phase has an average particle size of 0.1 to 1.5 μm.
A nitrogen-containing titanium carbide-based sintered alloy having excellent heat deformation resistance as claimed in claim 1 or 2.
JP12176287A 1987-05-19 1987-05-19 Nitrogen-containing titanium carbide-base alloy having excellent resistance to thermal deformation Granted JPS63286550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12176287A JPS63286550A (en) 1987-05-19 1987-05-19 Nitrogen-containing titanium carbide-base alloy having excellent resistance to thermal deformation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12176287A JPS63286550A (en) 1987-05-19 1987-05-19 Nitrogen-containing titanium carbide-base alloy having excellent resistance to thermal deformation

Publications (2)

Publication Number Publication Date
JPS63286550A JPS63286550A (en) 1988-11-24
JPH0333771B2 true JPH0333771B2 (en) 1991-05-20

Family

ID=14819255

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12176287A Granted JPS63286550A (en) 1987-05-19 1987-05-19 Nitrogen-containing titanium carbide-base alloy having excellent resistance to thermal deformation

Country Status (1)

Country Link
JP (1) JPS63286550A (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5127110B2 (en) * 2004-01-29 2013-01-23 京セラ株式会社 TiCN-based cermet and method for producing the same
JP4659682B2 (en) * 2005-10-18 2011-03-30 日本特殊陶業株式会社 Cermet inserts and cutting tools
JP5127264B2 (en) * 2007-02-23 2013-01-23 京セラ株式会社 TiCN-based cermet
JP4974980B2 (en) * 2008-08-25 2012-07-11 京セラ株式会社 TiCN-based cermet
JP6172382B2 (en) * 2014-03-19 2017-08-02 株式会社タンガロイ Cermet tool
JP6380016B2 (en) * 2014-11-05 2018-08-29 株式会社タンガロイ Cermet tools and coated cermet tools
CN104630590B (en) * 2015-02-12 2016-08-24 成都邦普切削刀具股份有限公司 A kind of composite hard alloy material and preparation method thereof
US11111564B2 (en) * 2018-10-04 2021-09-07 Sumitomo Electric Hardmetal Corp. Cemented carbide, cutting tool including same, and method of producing cemented carbide
GB201917347D0 (en) * 2019-11-28 2020-01-15 Hyperion Materials & Tech Sweden Ab NbC-based cemented carbide
CN117105227B (en) * 2023-08-21 2025-09-05 黑龙江省科学院高技术研究院 A method for preparing titanium carbide powder surface-modified with hafnium oxide

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5627587A (en) * 1979-08-14 1981-03-17 Mitsubishi Electric Corp Correlative tracking unit
JPS6173857A (en) * 1984-09-19 1986-04-16 Mitsubishi Metal Corp Cermet for cutting tool
JPH0611897B2 (en) * 1986-10-09 1994-02-16 東芝タンガロイ株式会社 High strength sintered alloy

Also Published As

Publication number Publication date
JPS63286550A (en) 1988-11-24

Similar Documents

Publication Publication Date Title
US4343651A (en) Sintered compact for use in a tool
AU2017212472B2 (en) Binder compositions of tungsten tetraboride and abrasive methods thereof
US5918103A (en) Plate-crystalline tungsten carbide-containing hard alloy, composition for forming plate-crystalline tungsten carbide and process for preparing said hard alloy
JP2622131B2 (en) Alloys for cutting tools
JPH0860201A (en) Tungsten-based carburized carbide powder mixture and carburized carbide product produced therefrom
EP0759480A1 (en) Plate-crystalline tungsten carbide-containing hard alloy, composition for forming plate-crystalline tungsten carbide and process for preparing said hard alloy
US20040079191A1 (en) Hard alloy and W-based composite carbide powder used as starting material
JPH0333771B2 (en)
JP2597046B2 (en) Cutting insert and its manufacturing method
US20050226691A1 (en) Sintered body with high hardness for cutting cast iron and the method for producing same
JP2580168B2 (en) Nitrogen-containing tungsten carbide based sintered alloy
JP2006144089A (en) Hard metal made of superfine particle
JPH06212341A (en) Sintered hard alloy and its production
JPS6225631B2 (en)
JPS63286549A (en) Nitrogen-containing titanium carbide-base sintered alloy having excellent resistance to plastic deformation
JPH07278719A (en) Particulate plate crystal cemented carbide containing wc and its production
JPH0450373B2 (en)
JP3605740B2 (en) Carbide alloy for end mill
JPS60135552A (en) Hyperfine tungsten carbide-base sintered alloy
JPS644989B2 (en)
US5036028A (en) High density metal boride-based ceramic sintered body
JP2502322B2 (en) High toughness cermet
JP3232599B2 (en) High hardness cemented carbide
JPS6059195B2 (en) Manufacturing method of hard sintered material with excellent wear resistance and toughness
JP3045199B2 (en) Manufacturing method of high hardness cemented carbide

Legal Events

Date Code Title Description
S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R360 Written notification for declining of transfer of rights

Free format text: JAPANESE INTERMEDIATE CODE: R360

R370 Written measure of declining of transfer procedure

Free format text: JAPANESE INTERMEDIATE CODE: R370

S531 Written request for registration of change of domicile

Free format text: JAPANESE INTERMEDIATE CODE: R313531

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

LAPS Cancellation because of no payment of annual fees