JPS6156306B2 - - Google Patents
Info
- Publication number
- JPS6156306B2 JPS6156306B2 JP53097487A JP9748778A JPS6156306B2 JP S6156306 B2 JPS6156306 B2 JP S6156306B2 JP 53097487 A JP53097487 A JP 53097487A JP 9748778 A JP9748778 A JP 9748778A JP S6156306 B2 JPS6156306 B2 JP S6156306B2
- Authority
- JP
- Japan
- Prior art keywords
- metal
- weight
- alloy
- hard
- group
- 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
- 229910045601 alloy Inorganic materials 0.000 claims description 63
- 239000000956 alloy Substances 0.000 claims description 63
- 229910052751 metal Inorganic materials 0.000 claims description 54
- 239000002184 metal Substances 0.000 claims description 53
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 36
- 229910052760 oxygen Inorganic materials 0.000 claims description 36
- 239000001301 oxygen Substances 0.000 claims description 36
- 239000000843 powder Substances 0.000 claims description 29
- 239000010936 titanium Substances 0.000 claims description 17
- 229910052799 carbon Inorganic materials 0.000 claims description 14
- -1 Iron group metals Chemical class 0.000 claims description 13
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 12
- 150000001875 compounds Chemical class 0.000 claims description 9
- 239000007789 gas Substances 0.000 claims description 9
- 238000005245 sintering Methods 0.000 claims description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 7
- 150000002739 metals Chemical class 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 5
- 229910052719 titanium Inorganic materials 0.000 claims description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 150000001247 metal acetylides Chemical class 0.000 claims description 4
- 150000004767 nitrides Chemical class 0.000 claims description 4
- 150000004649 carbonic acid derivatives Chemical class 0.000 claims description 3
- 229910052709 silver Inorganic materials 0.000 claims description 2
- 229910052755 nonmetal Inorganic materials 0.000 claims 3
- 238000001816 cooling Methods 0.000 claims 2
- 238000010438 heat treatment Methods 0.000 claims 2
- 229910052802 copper Inorganic materials 0.000 claims 1
- 229910052726 zirconium Inorganic materials 0.000 description 15
- 239000012071 phase Substances 0.000 description 13
- 229910052782 aluminium Inorganic materials 0.000 description 12
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 239000011195 cermet Substances 0.000 description 4
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 3
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 3
- 229910001928 zirconium oxide Inorganic materials 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 241000894007 species Species 0.000 description 2
- 238000004227 thermal cracking Methods 0.000 description 2
- FOZHTJJTSSSURD-UHFFFAOYSA-J titanium(4+);dicarbonate Chemical compound [Ti+4].[O-]C([O-])=O.[O-]C([O-])=O FOZHTJJTSSSURD-UHFFFAOYSA-J 0.000 description 2
- DSSYKIVIOFKYAU-XCBNKYQSSA-N (R)-camphor Chemical compound C1C[C@@]2(C)C(=O)C[C@@H]1C2(C)C DSSYKIVIOFKYAU-XCBNKYQSSA-N 0.000 description 1
- 229910000521 B alloy Inorganic materials 0.000 description 1
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 241000723346 Cinnamomum camphora Species 0.000 description 1
- 208000025599 Heat Stress disease Diseases 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- 229910010421 TiNx Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229960000846 camphor Drugs 0.000 description 1
- 229930008380 camphor Natural products 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Description
本発明は、Tiを主成とする焼結硬質合金にZr
と酸素あるいはZrとAlと酸素とを含有させるこ
とにより、切削特性の著しく改善された焼結硬質
合金に関する。
従来、サーメツトにZrを添加することにより、
耐摩耗性、熱的靭性を向上させた合金は知られて
いるが、サーメツトにZrと酸素あるいはZrとAl
と酸素とを含有させ、更に性能を向上させたもの
については知られていない。
本発明は、ZrをZrあるいはZrの化合物例えば
ZrC、ZrNの形で配合してやり、酸化チタン、炭
酸化チタン、炭酸窒化チタン、酸窒化チタンを1
種又は2種以上配合および/又はCOガス焼結す
ることにより脱酸素の防止、あるいは酸素の富化
をさせてやることによつてZrと酸素を合金中へ含
有させ、切削性能を大幅に向上させた合金であ
る。またAlを含有させZrとAlと酸素を含有させ
ると、更に切削性能向上となる。
Zrと酸素が合金中に含有すると、高速切削時に
おける刃先の耐塑性変形性および耐熱亀裂性がZr
単独の場合よりも更に著しく向上する。この理由
については定かでないが、合金中の硬質相もしく
は結合相中で原子オーダーでZrの酸素の結合が生
じ、酸化ジルコニウム的性質がサーメツトに付加
されるために耐塑性変形性、耐熱亀裂性向上とな
るものと思われる。
Zrの酸素の他、更にAlを添加することによ
り、更に切削性能が向上する。前述したようにZr
と酸素の結びつきにより、酸化ジルコニウム的性
質が付加されるが、Alと酸素が結びつくと酸化
アルミニウム的性質が付加され、酸化ジルコニウ
ム、酸化アルミニウムの両方の性質が重なり、切
削性能が大巾に向上するものと考えられる。
aおよび/又はaおよび/又はa族金族
および/又はAlおよび非金属元素との化合物、
例えばTi3AlC、Ti3AlN、Ti2AlC、Ti2AlN、
V2AlC、Ta2AlC、AlNの粉末(以上の分子式は
平均のもので、当然のことながら組成変動はあ
る)は、液相出現近傍まで安定故、Alの蒸発が
起らず、合金中に安定にAlを固溶させるのに有
利である。
本発明合金の制限について述べると、Zrと酸素
あるいはZrとAlと酸素を含む硬質合金であつ
て、aおよび/又はaおよび/又はa族金
属と非金属成分とより成る硬質合金を主して鉄族
金属で結合した合金で、硬質相の金属成分の20モ
ル%以上Tiであり、Zrの合金中の総量が0.01〜10
重量%、Alの合金中の総量が0.1〜10重量%より
なる。Zrが0.01重量%以下のときは、Zrの効果が
なく、10重量%以上のときは焼結性が悪化する。
またAlが0.1重量%以下のときAlの効果がなく、
10重量%以上のときは焼結性が悪化する。Tiが
硬質相の金属成分の20モル%以下のときはサーメ
ツトとしての耐摩耗性の良さが無くなる。
本発明合金の硬質相の総組成を原子比で、(
aA、aB、aC)(Cu、Nv、Ow)zと表わす
と
A、B、C、u、v、w、zの範囲は
0.15≦A≦0.98、0.01≦B≦0.30、0.01≦C≦
0.50、0.49≦u≦0.95、0.04≦v≦0.49、0.01≦w
≦0.20、0.80≦z≦1.05
である。A、B、Cの範囲はサーメツトとしての
切削性能を維持するため好適な範囲であり、Ti
の如きa族金属も最も多く含む。
次に硬質相の非金属成分について述べると非金
属成分の炭素、窒素、酸素のモル分率をu、v、
wと表記した場合、vが0.04以下であると、窒素
による合金微細化効果および酸素を安定に含ませ
る効果がなくZrとAlが添加された場合、vが0.49
を越えると焼結性が悪くなる。またwが0.01以下
であると酸素含有の効果がなく、0.20以上である
と焼結性が悪くなる。zは化学量論パラメータで
金属(第a族金属+第a族金属+第a族金
属)グラム原子当りの炭素および窒素および酸素
のグラム原子の結合数であり、0.80ないし1.05の
間に変動する。0.80以下は脆い相が存在し、1.0
以上になるとFree Carbonが存在するが、1.05ま
では性能上問題がない。
結合金属は合金全体を100重量%としたとき、
3〜25重量%であるが、3%以下ではぬれ性が悪
く、25%以上では耐摩耗性の劣化となるからであ
る。
また結合用金属として鉄族金属の他、Cu、
Ag、Si、Bを1種又は2種以上結合金属の0.2〜
2.5重量%含有するが、鉄族金属のCo、Ni、Feを
置換して5重量%以下の微量添加でも発明の効果
は維持される。
すなわちCuを添加すると粒成長を抑制し、熱
伝導性も向上する。また表面と内部の組織を均一
にする働らきもある。Agを添加するとぬれ性が
良くなり、熱伝導性の向上も期待できる。Si、B
も焼結性の向上に寄与する。
また金属結合相にはTi、Zr、Al、Hf、V、
Nb、Ta、Cr、Mo、W、C、N、Oの硬質相形
成元素が含有されるのは当然のことである。
以上のように本発明は、原料として酸化物、炭
酸化物、酸窒化物、炭酸窒化物を用い、焼結法と
してCOガス焼結を行い、脱酸素の防止および/
もしくは酸素富化させているが、酸素の含有して
いない完粉をCOガス焼結することによつても合
金中に酸素を含有させることができる。またCO
ガス圧を0.01〜300Torrの範囲としたのは、
0.01Torr以下では酸素がCO、CO2ガスとして放
出されやすくなり、300Torr以上では浸炭が激し
くなり、炭素量の変動が大きくなるからである。
本発明の合金の応用は実施例に記載にとゞまら
ず、切削工具のみならず、ペンボール、耐摩工
具、ダイス、耐摩部品(アペツクスシール)、装
飾品等にも応用できる。
以下に実施例を示すが、実施例中の炭化物、窒
化物、炭窒化物例えばTiC、TiNは便宜上TiC、
TiNと表示しており、実際はTiCx、TiNxであ
る。
実施例 1
市販のTiC粉末、TiN粉末、WC粉末、Mo2C粉
末及びTiO0.95粉末、ならびにNi粉末、Co粉末、
TaN粉末、ZrN粉末、AlN粉末とを用いて第1表
の組成で配合した。これを直径10mmのTiC−Mo
−Ni製ボールを用い18−8ステンレス内張ポツ
トによりアセトンを加えて、湿式ボールミルで96
時間混合した。この混合粉末に対し、カンフアー
を3%加えて2t/cm2で型押した。
この型押体を焼結するに際して、昇温過程では
1200℃までは10-3mmHgの真空下にし、1200℃か
ら1380℃までをCOガス分圧50Torrに保持し、そ
の後10-3mmHg以下の真空下で1380℃で60分焼成
して合金を作成した。得られた合金の分析を行つ
た結果第2表に示す如く表わされた。得られた合
金の機械的特性を第3表に、切削性能を第4表に
示す。
第3表、第4表より明らかなように、Zrと酸素
を含んだ合金A、ZrとAlと酸素を含んだ合金B
の本発明合金は比較合金Cと比べ、抗折力、硬度
には殆んど差が認められないが、切削試験結果か
ら明らかなように、本発明合金A、Bは耐摩耗
性、耐塑性変形性、耐熱疲労靭性において比較合
金Cに比べ一段とすぐれていることがわかる。特
にZrとAlと酸素を含むB合金がすぐれているこ
とがわかる。
The present invention combines Zr into a sintered hard alloy mainly composed of Ti.
This invention relates to a sintered hard alloy whose cutting characteristics are significantly improved by containing Zr, Al, and oxygen, or Zr, Al, and oxygen. Conventionally, by adding Zr to cermet,
Alloys with improved wear resistance and thermal toughness are known, but cermets containing Zr and oxygen or Zr and Al
It is not known that the performance has been further improved by containing oxygen and oxygen. In the present invention, Zr can be replaced with Zr or Zr compounds such as
Titanium oxide, titanium carbonate, titanium carbonate nitride, and titanium oxynitride are mixed in the form of ZrC and ZrN.
Combining a species or two or more species and/or sintering with CO gas prevents deoxidation, or enriches oxygen to incorporate Zr and oxygen into the alloy, greatly improving cutting performance. It is an alloy made of aluminum. Furthermore, when Al is contained and Zr, Al, and oxygen are contained, the cutting performance is further improved. When Zr and oxygen are contained in the alloy, the plastic deformation resistance and thermal cracking resistance of the cutting edge during high-speed cutting decreases due to Zr.
This is an even more significant improvement than when used alone. The reason for this is not clear, but the bonding of oxygen in Zr occurs on the atomic order in the hard phase or binder phase of the alloy, adding properties similar to zirconium oxide to the cermet, improving plastic deformation resistance and thermal cracking resistance. It seems that this will be the case. In addition to oxygen in Zr, adding Al further improves cutting performance. As mentioned above, Zr
When Al and oxygen combine, properties similar to zirconium oxide are added, but when Al and oxygen combine, properties similar to aluminum oxide are added, and the properties of both zirconium oxide and aluminum oxide overlap, greatly improving cutting performance. considered to be a thing. a and/or a and/or a group metal and/or a compound with Al and a nonmetallic element;
For example, Ti 3 AlC, Ti 3 AlN, Ti 2 AlC, Ti 2 AlN,
The powders of V 2 AlC, Ta 2 AlC, and AlN (the above molecular formulas are averages, and of course there are variations in composition) are stable up to the point where they appear in the liquid phase, so no evaporation of Al occurs in the alloy. This is advantageous for stably dissolving Al in solid solution. Regarding the limitations of the alloy of the present invention, it is a hard alloy containing Zr and oxygen or Zr, Al and oxygen, and mainly consists of a and/or a and/or group a metal and a non-metallic component. Alloys combined with iron group metals, in which the metal component of the hard phase is Ti and the total amount of Zr in the alloy is 0.01 to 10% by mole.
The total amount of Al in the alloy is from 0.1 to 10% by weight. When Zr is 0.01% by weight or less, Zr has no effect, and when it is 10% by weight or more, sinterability deteriorates.
Also, when Al is less than 0.1% by weight, there is no effect of Al,
When it is 10% by weight or more, sinterability deteriorates. When Ti is less than 20 mol% of the metal component of the hard phase, the wear resistance as a cermet is lost. The total composition of the hard phase of the invention alloy in atomic ratio is (
a A , a B , a C ) (C u , N v , O w ) When expressed as z , the range of A, B, C, u, v, w, and z is 0.15≦A≦0.98, 0.01≦B≦0.30 , 0.01≦C≦
0.50, 0.49≦u≦0.95, 0.04≦v≦0.49, 0.01≦w
≦0.20, 0.80≦z≦1.05. The ranges A, B, and C are suitable for maintaining cutting performance as a cermet, and Ti
It also contains the largest amount of group a metals. Next, regarding the nonmetallic components of the hard phase, the molar fractions of carbon, nitrogen, and oxygen in the nonmetallic components are u, v,
When expressed as w, if v is 0.04 or less, nitrogen will not have the effect of refining the alloy or stably containing oxygen, and if Zr and Al are added, v will be 0.49.
If it exceeds this, sinterability will deteriorate. Further, if w is 0.01 or less, there is no effect of oxygen inclusion, and if w is 0.20 or more, sinterability deteriorates. z is the stoichiometric parameter, which is the number of bonds in gram atoms of carbon and nitrogen and oxygen per gram atom of metal (Group A metal + Group A metal + Group A metal), varying between 0.80 and 1.05 . Below 0.80, a brittle phase exists, and 1.0
Above that, Free Carbon exists, but there are no performance problems up to 1.05. When the bonding metal is 100% by weight of the entire alloy,
The content is 3 to 25% by weight, but if it is less than 3%, the wettability will be poor, and if it is more than 25%, the abrasion resistance will deteriorate. In addition to iron group metals as bonding metals, Cu,
0.2~ of a metal that combines one or more types of Ag, Si, and B
Although the content is 2.5% by weight, the effect of the invention can be maintained even if a trace amount of 5% by weight or less is added by replacing the iron group metals Co, Ni, and Fe. In other words, adding Cu suppresses grain growth and improves thermal conductivity. It also has the function of making the surface and internal structure uniform. Adding Ag improves wettability and can also be expected to improve thermal conductivity. Si,B
Also contributes to improving sinterability. In addition, the metal bonding phase includes Ti, Zr, Al, Hf, V,
Naturally, hard phase forming elements such as Nb, Ta, Cr, Mo, W, C, N, and O are contained. As described above, the present invention uses oxides, carbonates, oxynitrides, and carbonate nitrides as raw materials and performs CO gas sintering as a sintering method to prevent deoxidation and/or
Alternatively, oxygen can be contained in the alloy by sintering a finished powder that is oxygen-enriched but does not contain oxygen with CO gas. Also CO
The gas pressure was set in the range of 0.01 to 300 Torr because
This is because below 0.01 Torr, oxygen is likely to be released as CO and CO 2 gases, and above 300 Torr, carburization becomes intense and the carbon content fluctuates greatly. Applications of the alloy of the present invention are not limited to those described in the examples, but can also be applied not only to cutting tools but also to pen balls, wear-resistant tools, dies, wear-resistant parts (apex seals), ornaments, etc. Examples are shown below, but carbides, nitrides, carbonitrides such as TiC and TiN in the examples are replaced with TiC, TiC, and TiN for convenience.
Although it is displayed as TiN, it is actually TiCx or TiNx. Example 1 Commercially available TiC powder, TiN powder , WC powder, Mo 2 C powder and TiO 0.95 powder, as well as Ni powder, Co powder,
TaN powder, ZrN powder, and AlN powder were blended according to the composition shown in Table 1. This is TiC−Mo with a diameter of 10 mm.
- Add acetone using a Ni ball and an 18-8 stainless steel lined pot, and use a wet ball mill to
Mixed for an hour. To this mixed powder, 3% camphor was added and stamped at 2t/cm 2 . When sintering this stamped body, in the temperature raising process,
The alloy is created under a vacuum of 10 -3 mmHg up to 1200°C, maintained at a CO gas partial pressure of 50 Torr from 1200°C to 1380°C, and then fired at 1380°C for 60 minutes under a vacuum of 10 -3 mmHg or less to create an alloy. did. The results of analysis of the obtained alloy are shown in Table 2. The mechanical properties of the obtained alloy are shown in Table 3, and the cutting performance is shown in Table 4. As is clear from Tables 3 and 4, Alloy A containing Zr and oxygen, Alloy B containing Zr, Al, and oxygen
There is almost no difference in transverse rupture strength and hardness between the alloys of the present invention and comparative alloy C, but as is clear from the cutting test results, alloys A and B of the present invention have superior wear resistance and plasticity resistance. It can be seen that the deformability and thermal fatigue toughness are far superior to Comparative Alloy C. It can be seen that the B alloy containing Zr, Al, and oxygen is particularly excellent.
【表】【table】
【表】【table】
【表】【table】
【表】
実施例 2
a、a、a族の炭化物、窒化物、炭窒化
物粉末及び炭酸化チタン、酸窒化チタン、炭酸窒
化チタン、酸化チタン、Zr、Zrの化合物、ならび
にa族および/又はa族および/又はa族
金属および/又はAlおよび非金属元素との化合
物、Ni粉末、Co粉末、Cu粉末、Ag粉末、SiN粉
末、SiC粉末、Si粉末、BN粉末、TiB2粉末とい
うように各種の粉末を用い、実施例1と同様な方
法にて第5表に示す如く合金を作成した。得られ
た合金の機械的特性を第6表に、切削性能を第7
表に示す。なお、第5表ではZrを硬質相中に、
Alを結合相に分離一括表示してあるが、実際は
Zr、Alはそれぞれ部分的に結合相にも硬質相の
両者に固溶するものと思われる。
第6表、第7表からわかるように、本発明合金
と比較合金は抗折力、硬度において殆んど差異は
みられないが、切削試験結果では耐摩耗性、耐塑
性変形性、耐熱疲労靭性において本発明合金の方
が優れていることがわかる。特にZrとAlと酸素
を[Table] Example 2 a, a, group a carbides, nitrides, carbonitride powders and titanium carbonate, titanium oxynitride, titanium carbonate nitride, titanium oxide, Zr, Zr compounds, and group a and/or Group A and/or Group A metals and/or compounds with Al and non-metallic elements, Ni powder, Co powder, Cu powder, Ag powder, SiN powder, SiC powder, Si powder, BN powder, TiB2 powder, etc. Alloys shown in Table 5 were prepared using various powders in the same manner as in Example 1. The mechanical properties of the obtained alloy are shown in Table 6, and the cutting performance is shown in Table 7.
Shown in the table. In addition, in Table 5, Zr is added to the hard phase.
Al is shown separated into a bonded phase all at once, but in reality it is
It is thought that Zr and Al are partially dissolved in both the binder phase and the hard phase. As can be seen from Tables 6 and 7, there is almost no difference in transverse rupture strength and hardness between the alloy of the present invention and the comparative alloy, but the cutting test results show that the alloys have excellent wear resistance, plastic deformation resistance, and thermal fatigue resistance. It can be seen that the alloy of the present invention is superior in toughness. Especially Zr, Al and oxygen
【表】【table】
【表】【table】
【表】【table】
【表】【table】
【表】【table】
【表】
実施例 3
市販のTiC粉末、TiN粉末、WC粉末、Mo2C粉
末、ZrC粉末、Ni粉末、Co粉末、TaN粉末とを用
いて実施例1と同様の方法にて、第8表に示す如
く合金を作成した。得られた合金の機械的特性を
第9表に、切削性能を第10表に示す。
第8表からわかるように、本実施例は原料に酸
化物を用いていないが、実施例1と同様なCOガ
ス焼結法を用いるため合金中に酸素が含有してい
ることがわかる。
第9表の抗折力、硬度では本発明合金と比較合
金の差異はみられないが、第10表の切削試験結果
から明らかなように、本発明合金は耐摩耗性、耐
塑性変形性、耐熱疲労靭性において比較合金より
優れていることがわかる。[Table] Example 3 Using commercially available TiC powder, TiN powder, WC powder, Mo 2 C powder, ZrC powder, Ni powder, Co powder, and TaN powder, the results shown in Table 8 were prepared in the same manner as in Example 1. An alloy was prepared as shown below. The mechanical properties of the obtained alloy are shown in Table 9, and the cutting performance is shown in Table 10. As can be seen from Table 8, this example does not use an oxide as a raw material, but since the same CO gas sintering method as in Example 1 is used, it can be seen that oxygen is contained in the alloy. Although there is no difference between the inventive alloy and the comparative alloy in terms of transverse rupture strength and hardness in Table 9, as is clear from the cutting test results in Table 10, the inventive alloy has wear resistance, plastic deformation resistance, It can be seen that the heat fatigue toughness is superior to the comparative alloys.
【表】【table】
【表】【table】
【表】【table】
【表】【table】
Claims (1)
を100重量%としたとき、0.01〜10重量%のZrと
酸素を含む硬質合金であつて、a、a、およ
びa族金属と非金属成分とよりなる硬質化合物
を主として鉄族金属で結合した合金で、硬質相の
金属成分が主としてTiであり、硬質相の非金属
成分に炭素と窒素および酸素とを含み、硬質相の
総組成を原子比で (aA、aB、aC)(Cu、Nv、Ow)zと
表わすと、 A、B、C、u、v、w、zの範囲は 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 であり、さらに前記金属結合相の鉄族金属は、合
金全体を100重量%としたとき、3〜25重量%で
あることを特徴とする焼結硬質合金。 2 Tiが硬質相の金属成分の20モル%以上95%
以下よりなることを特徴とする特許請求の範囲第
1項記載の焼結硬質合金。 3 硬質相及び結合金属中のZrの総量が合金全体
を100重量%としたとき、0.01〜10重量%のZrと
酸素を含む硬質合金であつて、a、aおよび
a族金属と非金属成分とよりなる硬質化合物を
主として鉄族金属で結合した合金で、硬質相の金
属成分が主としてTiであり、硬質相の非金属成
分に炭素と窒素および酸素とを含み、硬質相の総
組成を原子比で (aA、aB、aC)(Cu、Nv、Ow)zで
表わすと、 A、B、C、u、v、w、zの範囲は 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 であり、さらに前記金属結合相の鉄族金属は、合
金全体を100重量%としたとき、3〜25重量%で
あり、更に、硬質相および結合金属中にAlが総
量で合金全体を100重量%としたとき、0.1〜10重
量%含有することを特徴とする焼結硬質合金。 4 硬質相及び結合金属中のZrの総量が合金全体
を100重量%としたとき、0.01〜10重量%のZrと
酸素を含む硬質合金であつて、a、aおよび
a族金属と非金属成分とよりなる硬質化合物を
主として鉄族金属で結合した合金で、硬質相の金
属成分が主としてTiであり、硬質相の非金属成
分に炭素と窒素および酸素とを含み、硬質相の総
組成を原子比で (aA、aB、aC)(Cu、Nv、Ow)zと
表わすと、 A、B、C、u、v、w、zの範囲は 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 であり、さらに前記金属結合相の鉄族金属は、合
金全体を100重量%としたとき、3〜25重量%で
あり、結合金属として鉄族金属の他、Cu、Ag、
Si、Bを1種または2種以上を結合金属の0.2〜
2.5重量%を含むことを特徴とする焼結硬質合
金。 5 a、a、a族金属の炭化物、窒化物、
酸化物、炭酸化物、炭窒化物の1種以上と、Zrあ
るいはZrC又はZrNを1種または2種以上と鉄族
金属を混合し、昇温、焼結、冷却過程の一部また
は全部の過程で断続的もしくは連続的にCOガス
分圧を0.01〜300Torrに保持することにより脱酸
素を防止し、合金中にZrと酸素を含有せしめた
a、aおよびa族金属と非金属成分とよりな
る硬質化合物を主として鉄族金属で結合した合金
で、硬質相の金属成分が主としてTiであり、硬
質相の非金属成分に炭素と窒素および酸素とを含
み、硬質相の総組成を原子比で (aA、aB、aC)(Cu、Nv、Ow)zと
表わすと、 A、B、C、u、v、w、zの範囲は 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 であり、さらに前記金属結合相の鉄族金属は、合
金全体を100重量%としたとき、3〜25重量%で
あり、かつ、Zrが硬質相および結合金属中の総量
で0.01〜10重量%、結合金属中では0.01〜3重量
%であることを特徴とする焼結硬質合金の製造
法。 6 a、a、a族金属の炭化物、窒化物、
酸化物、炭酸化物、炭窒化物の1種以上と、酸窒
化チタン、炭酸窒化チタンの粉末を1種または2
種以上、ZrあるいはZrC又はZrNを1種または2
種以上と鉄族金属を混合し、昇温、焼結、冷却過
程の一部または全部の過程で断続的もしくは連続
的にCOガス分圧を0.01〜300Torrに保持すること
により脱酸素を防止し、合金中にZrと酸素を含有
せしめたa、aおよびa族金属と非金属成
分とよりなる硬質化合物を主として鉄族金属で結
合した合金で、合金全体を100重量%としたとき
硬質相および結合金属中のZrの総量が0.01〜10重
量%であり、硬質相の金属成分が主としてTiで
あり、硬質相の非金属成分に炭素と窒素および酸
素とを含み、硬質相の総組成を原子比で (aA、aB、aC)(Cu、Nv、Ow)zと
表わすと、 A、B、C、u、v、w、zの範囲は 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 であり、さらに前記金属結合相の鉄族金属は、合
金全体を100重量%としたとき、3〜25重量%で
あり、結合金属中のZrが0.01〜3重量%であるこ
とを特徴とする焼結硬質合金の製造法。[Scope of Claims] 1. A hard alloy containing Zr and oxygen in an amount of 0.01 to 10% by weight when the total amount of Zr in the hard phase and bond metal is 100% by weight of the entire alloy, which comprises a, a, and An alloy in which a hard compound consisting of a group A metal and a non-metal component is combined mainly with an iron group metal, the metal component of the hard phase is mainly Ti, and the non-metal component of the hard phase contains carbon, nitrogen and oxygen, When the total composition of the hard phase is expressed as (a A , a B , a C ) (C u , N v , O w ) z in atomic ratio, the range of A, B, C, u, v, w, z is as follows. 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05 Iron group metals are alloys A sintered hard alloy characterized in that the content is 3 to 25% by weight when the total weight is 100%. 2 Ti is 20 mol% or more of the metal component of the hard phase and 95%
A sintered hard alloy according to claim 1, characterized by comprising the following: 3. A hard alloy containing 0.01 to 10% by weight of Zr and oxygen, where the total amount of Zr in the hard phase and bonding metal is 100% by weight of the entire alloy, and is composed of group a, group a, and group a metals and nonmetallic components. It is an alloy in which hard compounds consisting of Expressed as a ratio (a A , a B , a C ) (C u , N v , O w ) z , the range of A, B, C, u, v, w, z is 0.15≦A≦0.98 0.01≦ B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05, and furthermore, the iron group metal of the metal binding phase was 100% by weight of the entire alloy. A sintered hard alloy characterized in that the hard phase and the bonding metal contain Al in a total amount of 0.1 to 10% by weight when the total amount of the alloy is 100% by weight. 4. A hard alloy containing 0.01 to 10% by weight of Zr and oxygen when the total amount of Zr in the hard phase and bonding metal is 100% by weight of the entire alloy, and is composed of a, group a and group a metals and non-metallic components. It is an alloy in which hard compounds consisting of Expressed as a ratio (a A , a B , a C ) (C u , N v , O w ) z , the range of A, B, C, u, v, w, z is 0.15≦A≦0.98 0.01≦ B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05, and furthermore, the iron group metal of the metal binding phase was 100% by weight of the entire alloy. 3 to 25% by weight, and in addition to iron group metals, Cu, Ag,
0.2~ of a metal that combines one or more types of Si and B
A sintered hard alloy characterized in that it contains 2.5% by weight. 5 a, a, group a metal carbides, nitrides,
A mixture of one or more oxides, carbonates, carbonitrides, one or more Zr, ZrC, or ZrN, and iron group metal, and part or all of the heating, sintering, and cooling processes. The CO gas partial pressure is maintained at 0.01 to 300 Torr intermittently or continuously to prevent deoxidation, and the alloy is made of group a, group a, and a metals and nonmetallic components containing Zr and oxygen. It is an alloy in which hard compounds are combined mainly with iron group metals, the metal component of the hard phase is mainly Ti, the non-metallic components of the hard phase include carbon, nitrogen, and oxygen, and the total composition of the hard phase is expressed as an atomic ratio ( a A , a B , a C ) (C u , N v , O w ) z , the range of A, B, C, u, v, w, z is 0.15≦A≦0.98 0.01≦B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05, and furthermore, the iron group metal of the metal binding phase is 3 when the entire alloy is 100% by weight. - 25% by weight, and the total amount of Zr in the hard phase and the binding metal is 0.01 to 10% by weight, and the total amount of Zr in the binding metal is 0.01 to 3% by weight. 6 a, a, group a metal carbides, nitrides,
One or more of oxides, carbonates, and carbonitrides, and one or two powders of titanium oxynitride and titanium carbonitride.
One or two types of Zr or ZrC or ZrN
Deoxidation can be prevented by mixing ferrous metals with iron group metals and maintaining the CO gas partial pressure intermittently or continuously at 0.01 to 300 Torr during part or all of the heating, sintering, and cooling processes. , an alloy in which a hard compound consisting of a, a, and a group metals containing Zr and oxygen and non-metal components is combined mainly with iron group metals, and when the entire alloy is taken as 100% by weight, the hard phase and The total amount of Zr in the bond metal is 0.01 to 10% by weight, the metal component of the hard phase is mainly Ti, the non-metallic components of the hard phase include carbon, nitrogen, and oxygen, and the total composition of the hard phase is atomic. Expressed as a ratio (a A , a B , a C ) (C u , N v , O w ) z , the range of A, B, C, u, v, w, z is 0.15≦A≦0.98 0.01≦ B≦0.30 0.01≦C≦0.50 0.49≦u≦0.95 0.04≦v≦0.49 0.01≦w≦0.20 0.80≦z≦1.05, and furthermore, the iron group metal of the metal binding phase was 100% by weight of the entire alloy. 3 to 25% by weight, and the Zr content in the bonding metal is 0.01 to 3% by weight.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9748778A JPS5524957A (en) | 1978-08-10 | 1978-08-10 | Sintered hard alloy and production thereof |
| DE2902139A DE2902139C2 (en) | 1978-01-21 | 1979-01-19 | Sintered carbide and its manufacturing process |
| FR7901316A FR2423546B1 (en) | 1978-01-21 | 1979-01-19 | HARD SINTERED METALS AND THEIR MANUFACTURING METHOD |
| GB7902257A GB2015574B (en) | 1978-01-21 | 1979-01-22 | Sintered metals and the method for producing the same |
| US07/267,644 US4973355A (en) | 1978-01-21 | 1988-10-31 | Sintered hard metals and the method for producing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9748778A JPS5524957A (en) | 1978-08-10 | 1978-08-10 | Sintered hard alloy and production thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5524957A JPS5524957A (en) | 1980-02-22 |
| JPS6156306B2 true JPS6156306B2 (en) | 1986-12-02 |
Family
ID=14193624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9748778A Granted JPS5524957A (en) | 1978-01-21 | 1978-08-10 | Sintered hard alloy and production thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5524957A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06156640A (en) * | 1992-11-20 | 1994-06-03 | Kiyuudenkou:Kk | Automatic pipe warehouse |
-
1978
- 1978-08-10 JP JP9748778A patent/JPS5524957A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06156640A (en) * | 1992-11-20 | 1994-06-03 | Kiyuudenkou:Kk | Automatic pipe warehouse |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5524957A (en) | 1980-02-22 |
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