JPS6218622B2 - - Google Patents
Info
- Publication number
- JPS6218622B2 JPS6218622B2 JP53023237A JP2323778A JPS6218622B2 JP S6218622 B2 JPS6218622 B2 JP S6218622B2 JP 53023237 A JP53023237 A JP 53023237A JP 2323778 A JP2323778 A JP 2323778A JP S6218622 B2 JPS6218622 B2 JP S6218622B2
- Authority
- JP
- Japan
- Prior art keywords
- atomic
- atom
- nitrogen
- carbon
- hard phase
- 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
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 44
- 229910052757 nitrogen Inorganic materials 0.000 claims description 32
- 229910045601 alloy Inorganic materials 0.000 claims description 30
- 239000000956 alloy Substances 0.000 claims description 30
- 229910052721 tungsten Inorganic materials 0.000 claims description 30
- 229910052750 molybdenum Inorganic materials 0.000 claims description 26
- 229910052799 carbon Inorganic materials 0.000 claims description 24
- 229910052751 metal Inorganic materials 0.000 claims description 18
- 239000002184 metal Substances 0.000 claims description 18
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 16
- 125000004429 atom Chemical group 0.000 claims description 12
- 239000000203 mixture Substances 0.000 claims description 10
- 239000001301 oxygen Substances 0.000 claims description 9
- 229910052760 oxygen Inorganic materials 0.000 claims description 9
- 239000012298 atmosphere Substances 0.000 claims description 8
- 150000001875 compounds Chemical class 0.000 claims description 8
- 239000013078 crystal Substances 0.000 claims description 8
- 239000002994 raw material Substances 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims description 6
- 238000006467 substitution reaction Methods 0.000 claims description 6
- 229910002091 carbon monoxide Inorganic materials 0.000 claims description 5
- 238000003763 carbonization Methods 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 5
- 238000005245 sintering Methods 0.000 claims description 5
- -1 iron group metals Chemical class 0.000 claims description 4
- 125000004430 oxygen atom Chemical group O* 0.000 claims description 4
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 2
- 229910002090 carbon oxide Inorganic materials 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 claims description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims 3
- 239000002131 composite material Substances 0.000 claims 1
- 238000002156 mixing Methods 0.000 claims 1
- 238000010298 pulverizing process Methods 0.000 claims 1
- 239000000843 powder Substances 0.000 description 12
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 7
- 238000006243 chemical reaction Methods 0.000 description 7
- 239000006104 solid solution Substances 0.000 description 7
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 6
- 239000001257 hydrogen Substances 0.000 description 6
- 229910052739 hydrogen Inorganic materials 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 230000008092 positive effect Effects 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 229910009043 WC-Co Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000005256 carbonitriding Methods 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910001004 magnetic alloy Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 210000004243 sweat Anatomy 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Description
Wは資源が少ないこと、戦略物資であることか
ら近年その値上りが著しい。Wを主成分とする、
いわゆるWC基超硬合金はますます高価格となら
ざるを得ず、遠からる資源の枯渇により使用でき
なくなる危険さえある。
これに対処するために、WCを(Mo,W)C
によつて置換しようとするこころみもあるが、
(特開昭51−146306)長時間の熱処理が必要であ
るなど実用的ではない。
そこで、発明者らはこれらについて鋭意研究し
次の点に気付いた。
その第1点は(W,Mo)CにNを含ませて、
(W,Mo)(C,N)zにすると長時間の熱処理
なしにヘキサゴナルWCタイプの安定な原料が得
られることである。
第2点はさらに(W,Mo)(C,N)zにOを
加え、(W,Mo)(C,N,O)zにするとより
安定になることを見出した。
第3点は(W,Mo)(C,N)zをしくは
(W,Mo)(C,N,O)zにCrを加え(W,
Mo,Cr)(C,N)zもしくは(W,Mo,Cr)
(C,N,O)zとすると軽量、安価な原料が得
られることも判明した。
第4点はこれら原料粉末を製造するに当つては
酸化物および/もしくは金属および/もしくは炭
化物および/もしくは炭素の混合物をその炭化工
程のうちの一部で700℃以上の温度でかつ窒素分
圧が300Torr以上の圧力下に粉末を置くと安定な
粉末が得られることも判つた。
第5点は上記金属粉末を使用して主として鉄族
金属で結合させた場合、出来上つた合金中に組成
の異なる2種類以上の単純ヘキサゴナルWC型の
硬質相が存在する場合に靭性の高い合金が生ずる
ことも判つた。
さらに1種もしくはそれ以上のMC型相以下に
M2C型相が存在する場合M2C相が均一に分散する
場合に高硬度高靭性を示すことも判つた。
以上5点が本発明の根幹をなすものであり、通
常の超硬合金の場合と同様にMO型相の一部が
a,Va,a族金属と非金属元素とより成るB1
型固溶体によつて置換された場合および鉄属結合
金属中にAg,Si,B,Cu,Al等の通常の超硬合
金に添加される元素が存在したり、当然常に起つ
ていることであるが硬質相形成元素が固溶したり
する場合にも本発明の効果が妨げられるものでな
い。
以下発明の限定範囲について述べる。
本発明の最も重要なMoとWとを含む単純ヘキ
サゴナル相および/もしくはM2C型が共存する場
合の系では結合金属と焼結した最終合金につき次
の値Aに関し
A=(窒素原子%/(Mo+W)原子%)
×(1−W原子%/(Mo+W)原子%)
0.005A0.5なる範囲が適すると判つた。
下限は窒素の好影響がこれ以下ではでて来ない
範囲であり、上限はこれを越えて窒素の含有量が
増加すると、焼結しにくくなり、性能がでないこ
とによる。
このうち最も適す範囲は
0.01A0.4である。
次に酸素の効果については、次の値Bに関し、
B=(酸素原子%/(Mo+W)原子%
×(1−W原子%/(Mo+W)原子%)
0.005≦B≦0.05
なる範囲が適すると判つた。下限は酸素の好影響
がこれ以下ではでて来ない範囲であり上限はこれ
を越えて酸素の含有量が増加とすると焼結しにく
くなり性能がでないことになる。
このうち最も適す範囲は
0.01≦B≦0.04である。
WとMo量は原子比にしてはW/Moが5/95〜
90/10であることが望ましい。5/95未満である
と不安定であり、90/10を越えると置換の利点
(軽量化、安価化)が生じないからである。
W,Moを置換できるCr量は原子比にして(W
+Mo)の0.5以下である。それ以上になると耐蝕
性は向上するが合金が脆化する。
主として切削用工具にはシンプル・ヘキサゴナ
ル相以外にB1型固溶体を形成させると有利であ
ることが知られている。この構成元素はTi,
Zr,Hf,V,Nb,Ta,Cr,Mo,Wいわゆる
a,Va,a族遷移金属とC,N,Oの非金属
成分である。
B1型固溶体量は切削用途に応じて変化させる
ことが望ましいが45体積%までの置換が行われ
る。この場合の置換量は1〜45体積%の範囲が適
当である。45体積%を越えると、本来のMoとW
の固溶体の特性即ち耐衝撃性、高温特性などがう
しなわれるのでこのましくない。
この場合窒素量についてはその一部がB1型固
溶体に吸蔵されるが、
Aの定義を
A=(窒素原子%/aaa族金属原子%)
(1−W原子%/aaa族金属原子%)
と変えて種々実験した結果、実験的に0.005A
0.5なる範囲がやはり適すると判つた。
このうち最適範囲は
0.01A0.4である。
また、酸素量についてはその1部がB1型固溶
体に吸蔵されるが
Bの定義を
B=(酸素原子%/aaa族金属原子%)
(1−W原子%/aaa族金族原子%)
と変えて種々実験した結果、実験的に
0.005≦B≦0.05
がやはり適する範囲であつた。
このうち最適範囲は
0.01≦B≦0.04である。
なお結合金属としては鉄族金属が組成物の3〜
50重量%含まれることが必要である3%未満では
もろすぎ、50%以上では柔かくて使用できないか
らである。
また合金作成中に上記シンプル・ヘキサゴナル
化合物が分解する場合があるが、この場合M2C型
の化合物が生じるが、この場合該化合物が10容量
%を越えない場合、結合金属にFeを含有させる
ことにより該化合物を球状化できるので強靭性を
保つことができる。
次に原料作成方法についてであるが、通常の
H2水素雰囲気中では(Mo,W)粉末+炭素によ
る炭化の場合、酸化物粉末+炭素による還元、炭
化を一度に行う場合もしくはこれらの組合せのい
ずれの場合も炭化をすすめるには高温にさらさな
ければならないが、高温下では(Mo,W)Cが
(Mo,W)2Cに分解してしまうので、低温長時間
の加熱を要する。しかるにこれを要素雰囲気中で
行うとこれらの加熱が不要で極めて好都合であ
る。窒素雰囲気としては(Mo,W)(C,N)の
分解窒素圧を検討したところ、温度によつて差が
あるが、炭窒化反応の起る700℃以上で300Torr
以上の外圧が必要であることが判つた。水素が共
存することは必ずしも害にはならないが、窒化反
応を妨げないためには、水素量は窒素量の体積に
して2倍以下、好ましくは、同量以下が望まし
い、アンモニア分解ガスを使用する場合には窒素
を富化する必要がある。
又、酸素を含む原料作成のためには、雰囲気中
にCO,CO2の共存が必要である。この場合には
水素量は上記制限をうけない、しかし全雰囲気の
50%を越えることは好ましくない。
又、合金焼結中の脱窒素、脱酸素を防止するた
めに窒素、酸化炭素雰囲気下で加熱焼結すること
は効果がある。
以下実施例について述べる。
実施例 1
2μのMo2Cと2μのWC粉末及び炭素粉末さ
らに拡散助剤としてCoを微量加え、最終炭窒化
物の組成が(Mo0.8,W0.2)(C0.95,N0.0
5)1.0となるように混合した混合物を窒素分圧
0.5気圧の窒素一水素気流中1800℃で30分間反応
させた。
X線回折結果ではMo2Cのピークは完全に消え
全てWCタイプのシンプル・ヘキサゴナルタイプ
の結晶形を示した。
この粉末にCo粉末を加え、最終合金の組成が
(Mo0.8,W0.2)(C,N)10重量%Coとし
た。該混合粉末は型押後、所定の形状にした後焼
結を行つた。この焼結条件は1000℃まで
10-2Torrの真空下加熱し1000℃から1400℃まで
を一酸化炭素雰囲気10Torrの減圧下で加熱し
た。同時に炭化物製造工程に窒素を用いず焼結工
程にて一酸化炭素を用いない条件下で行なつた合
金を作成し、本発明の方法と比較した。その結果
を表1に示す。
Because W is a scarce resource and is a strategic material, its price has increased significantly in recent years. The main component is W.
So-called WC-based cemented carbide has no choice but to become increasingly expensive, and there is even a risk that it will become unusable due to resource depletion in the future. To deal with this, we define WC as (Mo,W)C
There are attempts to replace it with
(Unexamined Japanese Patent Publication No. 51-146306) It is not practical as it requires a long heat treatment. Therefore, the inventors conducted extensive research on these issues and noticed the following points. The first point is to include N in (W, Mo)C,
When (W, Mo) (C, N) z is used, a stable hexagonal WC type raw material can be obtained without long-term heat treatment. The second point was found to be more stable by adding O to (W, Mo) (C, N) z to make (W, Mo) (C, N, O) z. The third point is (W, Mo) (C, N) z or (W, Mo) (C, N, O) z plus Cr (W,
Mo, Cr) (C, N)z or (W, Mo, Cr)
It has also been found that (C,N,O)z provides a lightweight and inexpensive raw material. The fourth point is that when producing these raw material powders, a mixture of oxides and/or metals and/or carbides and/or carbon is heated at a temperature of 700°C or higher and at a nitrogen partial pressure during part of the carbonization process. It was also found that a stable powder could be obtained if the powder was placed under a pressure of 300 Torr or higher. The fifth point is that when the above metal powders are used and bonded mainly with iron group metals, an alloy with high toughness can be obtained if two or more types of simple hexagonal WC type hard phases with different compositions are present in the resulting alloy. It was also found that this occurs. Furthermore, one or more MC types or less
It was also found that when an M 2 C type phase exists and the M 2 C phase is uniformly dispersed, high hardness and high toughness are exhibited. The above five points form the basis of the present invention, and as in the case of ordinary cemented carbide, a part of the MO type phase consists of a, Va, and a group metals and nonmetallic elements.
Naturally, this happens all the time when elements added to ordinary cemented carbide such as Ag, Si, B, Cu, Al, etc. are present in the iron-metal bonding metal when they are substituted by a type solid solution. The effects of the present invention are not hindered even when hard phase forming elements are dissolved in solid solution. The limited scope of the invention will be described below. In the system where a simple hexagonal phase containing Mo and W and/or M 2 C type coexist, which is the most important of the present invention, for the final alloy sintered with the bonding metal, the following value A = (Nitrogen atomic %/ It was found that a range of (Mo+W) atomic %) x (1-W atomic %/(Mo+W) atomic %) 0.005A0.5 is suitable. The lower limit is the range below which the positive effect of nitrogen does not appear, and the upper limit is because if the nitrogen content increases beyond this, sintering becomes difficult and performance deteriorates. Among these, the most suitable range is 0.01A0.4. Next, regarding the effect of oxygen, regarding the following value B, the following range is suitable: B = (oxygen atomic % / (Mo + W) atomic % × (1-W atomic % / (Mo + W) atomic %) 0.005≦B≦0.05 The lower limit is the range below which the positive effect of oxygen does not appear, and the upper limit is the range below which if the oxygen content increases, it will become difficult to sinter and the performance will deteriorate. The range is 0.01≦B≦0.04.The atomic ratio of W and Mo is 5/95~
Preferably 90/10. This is because if it is less than 5/95, it is unstable, and if it exceeds 90/10, the advantages of substitution (lighter weight, lower cost) will not occur. The amount of Cr that can replace W and Mo is expressed as an atomic ratio (W
+Mo) is 0.5 or less. If it exceeds this range, the corrosion resistance will improve, but the alloy will become brittle. It is known that it is advantageous to form a B1 type solid solution in addition to the simple hexagonal phase mainly for cutting tools. The constituent elements are Ti,
These are Zr, Hf, V, Nb, Ta, Cr, Mo, W, so-called a, Va, group a transition metals, and nonmetallic components of C, N, and O. The amount of B1 type solid solution is preferably changed depending on the cutting application, but substitution is performed up to 45% by volume. In this case, the appropriate amount of substitution is in the range of 1 to 45% by volume. If it exceeds 45% by volume, the original Mo and W
This is undesirable because the properties of the solid solution, such as impact resistance and high temperature properties, will be impaired. In this case, a part of the amount of nitrogen is occluded by the B1 type solid solution, but the definition of A is A = (Nitrogen atomic % / AAA group metal atomic %) (1 - W atomic % / AAA group metal atomic %) As a result of various experiments with different changes, experimentally 0.005A
It was found that a range of 0.5 is suitable. Among these, the optimum range is 0.01A0.4. Also, regarding the amount of oxygen, a part of it is occluded by the B1 type solid solution, but the definition of B is as follows: B = (oxygen atom%/AAA group metal atom%) (1-W atom%/AAA group metal atom%) As a result of various experiments with different values, it was experimentally found that 0.005≦B≦0.05 is still a suitable range. Among these, the optimal range is 0.01≦B≦0.04. In addition, as the binding metal, iron group metal is used as the bonding metal in the composition.
This is because if the content is less than 3%, which is required to contain 50% by weight, it will be too brittle, and if it is more than 50%, it will be too soft to use. In addition, the simple hexagonal compound mentioned above may decompose during alloy preparation, and in this case, an M 2 C type compound is generated. In this case, if the amount of this compound does not exceed 10% by volume, it is necessary to incorporate Fe into the bonding metal. This makes it possible to make the compound spherical, thereby maintaining its toughness. Next, regarding the raw material preparation method, the usual
In H 2 hydrogen atmosphere, in the case of carbonization with (Mo, W) powder + carbon, reduction with oxide powder + carbon, carbonization all at once, or a combination of these, exposure to high temperatures is required to promote carbonization. However, since (Mo, W) C decomposes into (Mo, W) 2 C at high temperatures, long-term heating at low temperatures is required. However, if this is carried out in an elemental atmosphere, these heatings are unnecessary and it is extremely convenient. As for the nitrogen atmosphere, we investigated the decomposition nitrogen pressure of (Mo, W) (C, N) and found that it differs depending on the temperature, but it is 300 Torr above 700℃ where carbonitriding reaction occurs.
It was found that more external pressure was required. The coexistence of hydrogen is not necessarily harmful, but in order not to interfere with the nitriding reaction, the amount of hydrogen should be less than twice the volume of nitrogen, preferably less than the same amount, and ammonia decomposition gas should be used. Nitrogen enrichment may be necessary in some cases. Furthermore, in order to create a raw material containing oxygen, it is necessary for CO and CO 2 to coexist in the atmosphere. In this case, the amount of hydrogen is not subject to the above restrictions, but the amount of hydrogen in the total atmosphere is
It is not preferable to exceed 50%. Furthermore, in order to prevent denitrification and deoxidation during alloy sintering, it is effective to heat and sinter the alloy in a nitrogen or carbon oxide atmosphere. Examples will be described below. Example 1 2μ of Mo 2 C, 2μ of WC powder and carbon powder, and a trace amount of Co as a diffusion aid were added, and the composition of the final carbonitride was (Mo 0.8 , W 0.2 ) (C 0.95 , N 0.0
5 ) The nitrogen partial pressure of the mixture is 1.0 .
The reaction was carried out at 1800°C for 30 minutes in a flow of nitrogen and hydrogen at 0.5 atm. In the X-ray diffraction results, the Mo 2 C peak completely disappeared, and all showed a WC type simple hexagonal type crystal form. Co powder was added to this powder to make the final alloy composition (Mo 0.8 , W 0.2 )(C,N) 10% by weight Co. The mixed powder was stamped, shaped into a predetermined shape, and then sintered. This sintering condition is up to 1000℃
It was heated under a vacuum of 10 -2 Torr and heated from 1000°C to 1400°C under a reduced pressure of 10 Torr in a carbon monoxide atmosphere. At the same time, an alloy was prepared in which nitrogen was not used in the carbide manufacturing process and carbon monoxide was not used in the sintering process, and compared with the method of the present invention. The results are shown in Table 1.
【表】
本発明合金はWC型以外は結合相のみで他相の
折出がなく極めて反応率がよい。従来合金では反
応率が悪いことが判る。
本発明合金は軽量であり、テスト結果によると
耐衝撃性、高温硬度にすぐれているので、あらゆ
る工具用途および耐摩耗用途に向くことがわかつ
た。
実施例 2
2μのMo2Cと1μのWCと1μのCr3C3粉末お
よび炭素粉末と拡散助剤としてFeを加え実施例
1に準じて合金を作成した。硬質相に換算した組
成は
(Mo0.8W0.15Cr0.05)(C0.93N0.06O0.01)
であり、結合相はCo/Ni比が1:1で9.5wt%の
ものができた。(微量のFeを含んでいる)
X線回折で解折したところ本合金は遊離炭素も
複合化合物も含まないWC型のシンプル・ヘキサ
ゴナル相とF.C.C.γ相のみ認められた。
本合金は人工汗にひたしたところ表2に示すよ
うに腐蝕量が少くWC−Co合金に比べ耐蝕性に優
れていることが判つた。又軽量でもあるので、時
計側などの装飾品、耐触用途、非磁性合金に用い
ると好都合であることがわかつた。[Table] Except for the WC type, the alloys of the present invention have only a binder phase, and no other phases are precipitated, and the reaction rate is extremely high. It can be seen that the reaction rate of conventional alloys is poor. The alloy of the present invention is lightweight, and test results show that it has excellent impact resistance and high temperature hardness, making it suitable for all types of tool applications and wear-resistant applications. Example 2 An alloy was prepared according to Example 1 by adding 2μ of Mo 2 C, 1μ of WC, 1μ of Cr 3 C 3 powder, carbon powder, and Fe as a diffusion aid. The composition converted into the hard phase was (Mo 0.8 W 0.15 Cr 0.05 ) (C 0.93 N 0.06 O 0.01 ), and the binder phase had a Co/Ni ratio of 1:1 and was 9.5 wt%. (Contains a small amount of Fe) When analyzed by X-ray diffraction, this alloy was found to contain only a WC-type simple hexagonal phase and an FCCγ phase that do not contain free carbon or complex compounds. When this alloy was soaked in artificial sweat, it was found that the amount of corrosion was small as shown in Table 2, and it was found to have superior corrosion resistance compared to the WC-Co alloy. In addition, since it is lightweight, it has been found to be convenient for use in decorative items such as watch parts, anti-corrosion applications, and non-magnetic alloys.
【表】
実施例 3
MoO3粉末とWO3粉末をMoとwの比率で8:2
になるように計算された量になるように秤量し
た。同時に酸化物の酸素が除去するのに必要な炭
素を加え、さらに反応時に窒素を固定させる触媒
としてFeを0.2%加えた。該混合物を(NH3+
10Vol%Co)ガス気流中で1500℃で1時間反応さ
せた。
化合物をX線で調べて見ると(Mo0.7W0.3)
(C0.93N0.06O0.01)0.98のヘキサゴナルタイ
プの化合物が生成された。
本炭酸窒化物にCo及びNiを10重量%(但し
Co/Ni=1)加えて混合し、実施例1の方法に
従つて合金を作成した。最終合金の特性を調べて
みるとA=0.2,B=0.03であつた。又抗析力は
210Kg/mm2ときわめて強靭であり、耐衝撃性にす
ぐれる合金であつた。
実施例 4
Coを10重量%、Niを10重量%、実施例3で作
製したMoとWの複炭酸窒化物と炭素との合量を
80重量%とし、炭素量を種々変えた合金を作製し
た。得られた合金の抗折力と添加炭素量および合
金中に析出したM2C型の結晶構造をもつ(Mo,
W)2(C,N,O)の量を表4に「M2C析出
量」として示す。[Table] Example 3 MoO 3 powder and WO 3 powder at a Mo:w ratio of 8:2
It was weighed to give the calculated amount. At the same time, carbon was added to remove the oxygen oxide, and 0.2% Fe was added as a catalyst to fix nitrogen during the reaction. The mixture was converted into (NH 3 +
The reaction was carried out at 1500°C for 1 hour in a gas stream (10Vol%Co). When the compound is examined with X-rays (Mo 0.7 W 0.3 )
A hexagonal type compound of (C 0.93 N 0.06 O 0.01 ) 0.98 was produced. 10% by weight of Co and Ni in this carbonitride (however,
Co/Ni=1) and mixed to produce an alloy according to the method of Example 1. When the properties of the final alloy were investigated, it was found that A=0.2 and B=0.03. Also, the anti-analytical power is
The alloy was extremely strong at 210Kg/mm 2 and had excellent impact resistance. Example 4 Co was 10% by weight, Ni was 10% by weight, and the total amount of Mo and W double carbonitride prepared in Example 3 and carbon was
Alloys with various amounts of carbon were prepared, with a carbon content of 80% by weight. The transverse rupture strength of the obtained alloy, the amount of added carbon, and the M 2 C type crystal structure precipitated in the alloy (Mo,
The amount of W) 2 (C, N, O) is shown in Table 4 as "M 2 C precipitation amount".
【表】【table】
【表】
上述の如く、M2C型の結晶構造をもつ(Mo,
W)2(C,N,O)が10容量%以上析出すると
抗折力が大巾に低下することがわかる。[Table] As mentioned above, it has an M 2 C type crystal structure (Mo,
It can be seen that when 10% by volume or more of W) 2 (C, N, O) precipitates, the transverse rupture strength decreases significantly.
Claims (1)
MoとWの複炭化物を硬質相とし、3〜50重量%
の鉄族金属によつて結合した合金において、該硬
質相中の炭素の一部が窒素と酸素で置換され、そ
の置換量が 0.005≦〔窒素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
5 0.005≦〔酸素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
05 であることを特徴とするMoを含む超硬質合金。 2 特許請求の範囲第1項記載の合金において、
結晶構造がシンプル・ヘキサゴナル型であるMo
とWの複炭化物中に、結晶構造がM2C型のMoと
Wの複炭化物が1〜10容量%含まれることを特徴
とするMoを含む超硬質合金。 3 結晶構造がシンプル・ヘキサゴナル型である
MoとWの複炭化物を硬質相とし、3〜50重量%
の鉄族金属によつて結合した合金において、該硬
質相中の炭素の一部が窒素と酸素で置換され、そ
の置換量が 0.005≦〔窒素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
5 0.005≦〔酸素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
05 である硬質相において、MoとWが1〜50%(原
子比)の範囲でCrと置換されていることを特徴
とするMoを含む超硬質合金。 4 結晶構造がシンプル・ヘキサゴナル型である
MoとWの複炭化物を硬質相とし、3〜50重量%
の鉄族金属によつて結合した合金において、該硬
質相中の炭素の一部が窒素と酸素で置換され、そ
の置換量が 0.005≦〔窒素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
5 0.005≦〔酸素原子%/(Mo+W)原子%〕 ×〔1−W原子%/(Mo+W)原子%〕≦0.
05 である合金を製造するにあたり、MoとWと炭素
の混合物もしくはMoの酸化物とWの酸化物と炭
素の混合物の炭化加熱処理過程において、700℃
以上の温度で300Torr以上の窒素を含む雰囲気お
よび/または1Torr以上の酸化炭素を含む雰囲気
で加熱保持して製造したMoとWの複化合物原料
を製造し、ついでこの原料に鉄族金属を加え、混
合粉砕したのち型押し、真空もしくは減圧窒素お
よび/又は一酸化炭素雰囲気中1200℃〜1450℃の
温度で焼結することを特徴とするMoを含む超硬
質合金の製造法。[Claims] 1. The crystal structure is simple hexagonal.
Double carbide of Mo and W as hard phase, 3 to 50% by weight
In an alloy bonded by iron group metals, part of the carbon in the hard phase is replaced by nitrogen and oxygen, and the amount of substitution is 0.005≦[nitrogen atomic %/(Mo+W) atomic %] × [1- W atomic%/(Mo+W) atomic%〕≦0.
5 0.005≦[Oxygen atom%/(Mo+W) atom%] × [1-W atom%/(Mo+W) atom%]≦0.
05 A superhard alloy containing Mo. 2. In the alloy according to claim 1,
Mo with a simple hexagonal crystal structure
1. A superhard alloy containing Mo, characterized in that the double carbide of Mo and W having an M 2 C type crystal structure is contained in the double carbide of Mo and W in an amount of 1 to 10% by volume. 3. The crystal structure is simple and hexagonal.
Double carbide of Mo and W as hard phase, 3 to 50% by weight
In an alloy bonded by iron group metals, part of the carbon in the hard phase is replaced by nitrogen and oxygen, and the amount of substitution is 0.005≦[nitrogen atomic %/(Mo+W) atomic %] × [1- W atomic%/(Mo+W) atomic%〕≦0.
5 0.005≦[Oxygen atom%/(Mo+W) atom%] × [1-W atom%/(Mo+W) atom%]≦0.
05 A superhard alloy containing Mo, characterized in that in the hard phase, Mo and W are substituted with Cr in a range of 1 to 50% (atomic ratio). 4. The crystal structure is simple hexagonal.
Double carbide of Mo and W as hard phase, 3 to 50% by weight
In an alloy bonded by iron group metals, part of the carbon in the hard phase is replaced by nitrogen and oxygen, and the amount of substitution is 0.005≦[nitrogen atomic %/(Mo+W) atomic %] × [1- W atomic%/(Mo+W) atomic%〕≦0.
5 0.005≦[Oxygen atom%/(Mo+W) atom%] × [1-W atom%/(Mo+W) atom%]≦0.
05, in the process of carbonization heat treatment of a mixture of Mo, W, and carbon or a mixture of Mo oxide, W oxide, and carbon at 700℃.
Producing a composite compound raw material of Mo and W produced by heating and holding in an atmosphere containing nitrogen of 300 Torr or more and/or carbon oxide of 1 Torr or more at a temperature above, then adding an iron group metal to this raw material, A method for producing a superhard alloy containing Mo, which comprises mixing and pulverizing, stamping, and sintering at a temperature of 1200°C to 1450°C in a vacuum or reduced pressure nitrogen and/or carbon monoxide atmosphere.
Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2323778A JPS54115610A (en) | 1978-02-28 | 1978-02-28 | Mo-containing sintered hard alloy and manufacture thereof |
| US05/971,835 US4265662A (en) | 1977-12-29 | 1978-12-19 | Hard alloy containing molybdenum and tungsten |
| CA318,566A CA1115994A (en) | 1977-12-29 | 1978-12-22 | Hard alloy containing molybdenum and tungsten |
| GB7849945A GB2011949B (en) | 1977-12-29 | 1978-12-22 | Hard alloy containing molybdenum and tungsten |
| DE19782856513 DE2856513A1 (en) | 1977-12-29 | 1978-12-28 | HARD ALLOY CONTAINS MOLYBDAEN AND TUNGSTEN |
| SE7813363A SE433503B (en) | 1977-12-29 | 1978-12-28 | HARD alloy based on tungsten molybdenum carbide |
| AU42963/78A AU523578B2 (en) | 1977-12-29 | 1978-12-28 | Hard alloy containing molybdenum and tungsten |
| FR7836800A FR2413473B1 (en) | 1977-12-29 | 1978-12-28 | PROCESS FOR PRODUCING HARD ALLOYS CONTAINING MOLYBDENE AND TUNGSTENE AND NOVEL PRODUCTS THUS OBTAINED |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2323778A JPS54115610A (en) | 1978-02-28 | 1978-02-28 | Mo-containing sintered hard alloy and manufacture thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS54115610A JPS54115610A (en) | 1979-09-08 |
| JPS6218622B2 true JPS6218622B2 (en) | 1987-04-23 |
Family
ID=12104993
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2323778A Granted JPS54115610A (en) | 1977-12-29 | 1978-02-28 | Mo-containing sintered hard alloy and manufacture thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS54115610A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4126451B2 (en) * | 2002-03-22 | 2008-07-30 | 京セラ株式会社 | Cemented carbide |
-
1978
- 1978-02-28 JP JP2323778A patent/JPS54115610A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS54115610A (en) | 1979-09-08 |
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