JPS5959879A - Multi-coated material and its production - Google Patents
Multi-coated material and its productionInfo
- Publication number
- JPS5959879A JPS5959879A JP17054082A JP17054082A JPS5959879A JP S5959879 A JPS5959879 A JP S5959879A JP 17054082 A JP17054082 A JP 17054082A JP 17054082 A JP17054082 A JP 17054082A JP S5959879 A JPS5959879 A JP S5959879A
- Authority
- JP
- Japan
- Prior art keywords
- layers
- coating
- tin
- resistance
- thickness
- 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.)
- Pending
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
- C23C16/34—Nitrides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
- C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Vapour Deposition (AREA)
Abstract
Description
【発明の詳細な説明】
本デト明は硬質物質を被覆した+A il’l 、持に
耐1’? 141′1、耐欠損性に有効な多層被覆の施
された材料d。DETAILED DESCRIPTION OF THE INVENTION The present invention is coated with a hard material and has a durability of 1'? 141'1, material d with multilayer coating effective for fracture resistance.
J、びイの製造法に関りる。Involved in the manufacturing method of J.B.
WCC超超硬合金FIC基リーすッ1−1およびTiN
基リーすットに硬質物質を被覆しC耐摩耗f〕1を向1
−さぜることが従来より行なわれ(きた。WCC cemented carbide FIC base 1-1 and TiN
The base sheet is coated with a hard material to provide C wear resistance f〕1 facing 1.
-Soaking has traditionally been done.
[2かし耐摩耗1′[どいってし、111粍は、ノラン
ク部にみられるアブレツシブ摩耗、クレータ一部にみら
れる被削4Δどの化学反応に1i1づ<1?X耗、おJ
、び堤W淳耗(みられるglEとして酸化摩耗の33つ
の11L社に人別され、ノノルッシゾ’ci:摩耗には
硬さの高いしの、クレータ−摩耗には化学的安定t!1
が人さいしの、境界摩耗には耐酸化1’lどとbに熱伝
導1′jの61いものが、それぞれ有効(゛あることが
知られている。[2 However, the wear resistance 1' [111 mm is due to the abrasive wear seen in the no-rank part and the 4Δ of the workpiece seen in a part of the crater.Which chemical reaction is 1i1<1? X wear, OJ
, Bitsutsumi W abrasion (glE seen) is classified into 33 11L companies of oxidative wear, nonorushizo'ci: high hardness for wear, chemical stability for crater wear!1
However, it is known that oxidation resistance 1'l, b, and heat conduction 1'j are effective for boundary wear.
このため従来から、炭化物、窒化物等の単一層を被覆す
るかわりに、
(1)内層と外層の2層、あるいは内層、中間層、タト
層の3層1.二’fiれe゛れ異なる性質をもっノ5−
硬貿物質を波黄するh払。For this reason, conventionally, instead of coating with a single layer of carbide, nitride, etc., (1) two layers, an inner layer and an outer layer, or three layers, an inner layer, an intermediate layer, and a top layer. Both have different properties5-
H payment to wave yellow the hard trade material.
(■異なったM費を右りる2〜31J1の硬質物質の固
溶物質、例えば炭窒化物を′fIJ!覆づる方法Nが耐
摩ネl−の改善lj法として取られ(−きた。(■Method N of covering 2-31J1 solid solutions of hard substances, such as carbonitrides, which depend on different M costs, has been adopted as a method for improving wear resistance.
しかし、−1記■の場合には当然のことイf /N l
’J、例えば、外層はフランク部での耐摩耗性は良好だ
/デク1ノータ一部の耐摩1[、Mが劣化する、等の規
象が生じるため、飛躍的な耐摩耗性向J−(3L望めイ
(い。However, in the case of -1 ■, it is natural that if/N l
'J, for example, the outer layer has good wear resistance at the flank part/Dek1 Nota Some wear resistance 1 [, M deteriorates, etc., so the wear resistance increases dramatically J-( I want 3L.
また、熱r#服;Iこの異イiる賀種物質をがイにりの
厚みに被M?#るために、熱の変動に弱く切削時に欠に
1しやりい、という欠点はまぬがれない。Also, do you want to apply this different material to the thickness of your skin? Because of this, it has the unavoidable disadvantage that it is sensitive to heat fluctuations and has to be cut during cutting.
二りだ上記■の場合には、一般に異種籾買物貿の固溶1
ホは、硬質物質のぞれぞれの特長/Jc助長されるより
(ユむしろ欠f−1!が助長される1頃向/′I(ある
、という問題点がある。In the case of ■ above, generally the solid solution 1 of the different types of paddy shopping trade is
There is a problem that each feature of the hard material /Jc is promoted, but rather the lack f-1! is promoted.
従って一1記イりまたは■の方法は、共に有効な改善方
法であるとはいえながった。Therefore, it could not be said that methods 11-1 and 2 are effective improvement methods.
本発明は上記従来技術の欠点を改良し、耐摩社、耐欠損
性に優れたI′i規な:二1−−シーイングニL具を提
供することを目的とする。The object of the present invention is to improve the above-mentioned drawbacks of the prior art and to provide an I'i type tool having excellent fracture resistance.
本発明はw C単用硬合金、TiC基リーすッ1−また
(よ丁tN基→プーメットの大面に、1−1[3Nおよ
び−F’iNよりなる被覆層が、単層の厚さ 1μmn
1ス下、ayましりに710.5μm未満で合1t2−
15μmの厚さにTi r3N、 −1’i Nヲ交l
zニ少<トモ6Ffm以−U、望ましくは20層以jニ
多重被覆したことを特徴とするbのζcj<iる。The present invention is based on w C single-purpose hard alloy, TiC base 1-Also (Yoding tN group → Pumet), and a coating layer consisting of 1-1 [3N and -F'iN is applied to the thickness of the single layer. 1 μm
1st below, less than 710.5μm on ay side
Cross Ti r3N, -1'i N to a thickness of 15 μm.
ζcj<i of b, characterized in that z<tomo 6Ffm or more, preferably 20 or more layers, are multi-coated.
本発明による月利は、単層の厚さが1μnl以下、りf
ましくは0,5μn1未満(パあるので、熱膨張係数の
人さい−7−113Nの欠点をカバーりることが可能と
なり、究搏的に被覆材オ゛す層間の歪が均一(J分j)
々しく応力集中を(Jl除し、耐熱沙J fi’ +l
(!高めることがC゛きる。The monthly profit according to the present invention is based on the monolayer thickness of 1 μnl or less,
Preferably less than 0.5 μn1 (P), so it becomes possible to overcome the shortcoming of -7-113N in thermal expansion coefficient, and ultimately uniform strain between layers of the coating material (J j)
Vigorously reduce stress concentration (Jl divided by heat resistance J fi' +l
(!It is possible to raise C.
Jた、丁rr3Nu、TiNに比べC1便さか高くかつ
λ:! fl/i導t’l−にIVれるため、耐フノン
ク厚耗f1のみならずh1境W摩粍性をも著しく改善り
る。また、Ti13NIJ畝系合金どの親11 t’l
が大きいため、鋼や鋳鉄等を切削した場合、中伸(はク
レータ−摩耗の進行が早い傾向にあるが、本発明にa3
いては、化学的安定性の高いTiNど交ηに薄層を多重
被覆しくいるので、この欠点は回避できる。J, just rr3Nu, C1 flight is higher than TiN and λ:! Since fl/i conduction t'l- is IV, not only the thickness resistance f1 but also the abrasion resistance of h1 boundary W is significantly improved. In addition, Ti13NIJ ridge type alloy which parent 11t'l
When cutting steel, cast iron, etc., due to the large
In this case, this drawback can be avoided by applying multiple thin layers to TiN, which has high chemical stability.
また、本発明において被覆層を車ねる順序は、母材、
−r’i IJN、 Ti N、 −I’i [3N、
’I i N、 −・・・でもよく、L1祠、 l−
i N、 Ti BN、 l’i N。In addition, in the present invention, the order in which the coating layer is applied is as follows:
-r'i IJN, Ti N, -I'i [3N,
'I i N, -...maybe, L1 shrine, l-
i N, Ti BN, l'i N.
i i t3 N・・・・・・の順序の回れでも良い。The order of i t3 N... may be changed.
ネ光明による製造方法、特に被覆層の形成1)法は、化
学気相蒸着法において従来がら用いられ−(いるl−i
、1lJ5よびNを含んだ混合ガス、例えばTi c1
3.1−12 およびN2の混合ガスに間欠的に8を含
/υだガス、例えばBCI を混入(ることで、簡潔
かつ有効に多重被覆膜形成が可能ど4する。The manufacturing method by Nekomei, especially the method 1) for forming the coating layer, has been conventionally used in the chemical vapor deposition method.
, 1lJ5 and N, for example Ti c1
3.1-12 A gas containing 8/υ, for example, BCI, is intermittently mixed into the mixed gas of 1-12 and N2, thereby making it possible to easily and effectively form multiple coatings.
さらに従来J、り知られCいるJ、うに、化学蒸盾法を
用いる場合、1−iN被膜形成温度は約97 (1’C
11’1r3N?i*膜形成温磨は920℃と低い。し
たがっU−ri13Nm覆からTiN被覆へ、あるいは
逆(こ1’iN被覆から一1川INN被覆へと切t4え
るどきに被覆温度を変更する必要があり、このと5に被
覆粒子の異状成長が生じることが避(づられず、被膜の
性質が劣化Jる原因どなつ(いる。Furthermore, when using the conventional chemical vapor shield method, the 1-iN film formation temperature is approximately 97 (1'C
11'1r3N? The i* film formation temperature is as low as 920°C. Therefore, it is necessary to change the coating temperature when changing from U-ri 13Nm coating to TiN coating, or vice versa (from 1'iN coating to 11kawa INN coating, and this also causes abnormal growth of coated particles. There are many reasons why the properties of the coating deteriorate.
ところが本願発明者らは、ガスを間欠的に混入した場合
には、気相からの析出粒子の核生成頻度は多くなるが成
長速度は荏くなることを児出し、これに基づいて本発明
を完成した。従つ℃、本発明においては、ガスを間欠的
に混入さ)Lることが望ましく、これにより、−11N
を被覆づる濡麿をTiBNど同一の温度に選んでも、微
細な粒子を1イることがC′きるという優れた効果が得
られる。However, the present inventors discovered that when gas is mixed intermittently, the frequency of nucleation of precipitated particles from the gas phase increases, but the growth rate decreases, and based on this, the present invention was developed. completed. Accordingly, in the present invention, it is desirable to mix gas intermittently, so that -11N
Even if the coating temperature is chosen to be the same as that of TiBN, the excellent effect of reducing the number of fine particles by C' can be obtained.
この場合、電磁場をか()でプラズマ状態どして活↑l
l化蒸着を行なうことも、もJ)ろん可能である。In this case, the electromagnetic field is activated into a plasma state with ↑l
Of course, it is also possible to carry out chloride deposition.
また、本発明において、多([被覆層は少なくとも8層
以上、望ましくは20層以上が良い。8層未満Cは前述
した多重波1″f1の効果が十分梵揮でき4jい。また
各中層の厚みは、被覆材料肋間の歪を均一に分11(さ
Uるために、1μm11以上好ましくは0.5μm1以
上が良い。これは、1μn1を越えると耐欠損性が劣化
するためCある9、
実施例1
WC−6%CO超硬合金上に王i N、 T−i BN
被膜を交7Xiに各層0.1μm1合計6μmの被膜を
被覆した。このデツプを試別Δどする。In addition, in the present invention, the number of coating layers is preferably at least 8 layers, preferably 20 layers or more. Less than 8 layers will not allow the effect of the multiplexed wave 1"f1 described above to be fully exploited. The thickness of the coating material should be 1 μm or more, preferably 0.5 μm or more, in order to evenly distribute the strain between the ribs of the coating material.This is because if it exceeds 1 μm, the fracture resistance will deteriorate. Example 1 WangiN, TiBN on WC-6%CO cemented carbide
The coatings were coated on a 7Xi grid with each layer having a thickness of 0.1 .mu.m and a total thickness of 6 .mu.m. This depth is tested by Δ.
同時に比較量として、上記超硬合金−Lに下層に1’
i N 1.1層に1ft3Nをそれぞれ3tzmずッ
合#’F 671 Illの膜庁を有す−る被膜を被覆
した。この升ツブを試別1−3とりる。これら2(小の
試別を以下の切削条11、即ら、
被削1.I 80M3
切削速度 2oomy ra r n送 リ
0,3n+M rev切り込み 2mm
にて切削デス1へを(jなった。比較量のBチップは1
3分で′フランク部の摩耗が進行し寿命に至ったのに対
し、水子ご明によるAデツプは30分間の切削でも良好
な切削性能を示した。At the same time, as a comparison amount, 1' was added to the lower layer of the above cemented carbide-L.
iN 1.1 layer was coated with a film having a film thickness of 3 tzm and #'F 671 Ill of 1 ft3N each. Take this test volume 1-3. These 2 (small) cutting strips 11 are as follows: Workpiece 1.I 80M3 Cutting speed 2 omy ra r n feed
0.3n+M rev cutting depth 2mm to cutting edge 1 (j). Comparison amount B chip is 1
In 3 minutes, the wear of the 'flank part progressed and reached the end of its service life, whereas the A depth made by Goaki Mizuko showed good cutting performance even after 30 minutes of cutting.
実施例2
W C−8%iic 8%TaC−G%Co mV金
合金上Ti N、Ti BN被膜を各層0.0571m
合48μmの被膜を被覆した。このチップを試料Oとす
る。同時に比較材として同じ超硬合金十に下層にニーf
i 13N、 JJiに1−iNをそれぞれ3μm5
μm 1合ル18μmの膜厚を右りる被膜を被覆した。Example 2 WC-8%IIC 8%TaC-G%Com mV TiN, TiBN coating on gold alloy, each layer 0.0571m
A total of 48 μm coating was applied. This chip is designated as sample O. At the same time, the same cemented carbide was used as a comparison material and the lower layer was made of knee f.
i 13N, 1-iN to JJi, 3μm5 each
A film having a film thickness of 18 μm per μm was coated.
このチップを試料[)とする。Let this chip be the sample [).
次にこれら2種の試r1を以下の断続切削条件、即ち
切削速度 200m、、’ m i ++)ス
リ 0.41111n/’ re
V切り込み 1.5mm
被削材 80M3
10 m 111幅のtM f”Jき
にて切削デス1へを行なった。比較材のDチップは40
回の衝撃C欠損しlJが、本発明のCは920回の衝撃
でも欠損に至らなかった。Next, these two types of trials r1 were subjected to the following intermittent cutting conditions: cutting speed 200 m, ' m i ++)
0.41111n/' re
V depth of cut 1.5mm Work material 80M3 10m 111 width tM f"J cutting was performed. The D tip of the comparison material was 40
The C of the present invention was not damaged even after 920 impacts.
以上計速した如く、本発明にJ、れば、−T’113N
。As measured above, if the present invention is J, -T'113N
.
1−1Nの薄い被膜を交1:jに多重被覆づるCどによ
り、耐摩耗↑([、耐栴撃牲に冨む被覆超硬合金を1q
ることが(パきるのでその]二業−トの効果は大−Cあ
る。A thin coating of 1-1N is applied to the coating layer 1:j to provide wear resistance ↑ ([, 1q of coated cemented carbide rich in erosion resistance
The effect of the second job is great.
Claims (1)
−iN基」J−メツ1−の表面に、−1−! 13 N
お、J、ぴTi NJ、リイTる被覆層が、単層の厚さ
I tl to以小で゛あつC,合512〜15μn1
の厚さに交liに少くとL)8層以−1多小被覆され(
なることを1j1徴とりる多重被11′ジ。 2、十こ11単層の庁さが0.5μm)1以l;(゛あ
ることを特徴とする特約請求の範囲第11f4記載の多
層被覆材料。 3.1記被1”+J層が20層以」−であることを1!
1徴とする特971請求の範囲第1珀または第21(’
4記載の多重 ン皮 前 4A 利 、。 4、WCC超超硬合金r;c塁す−メツ1〜、または王
iN阜す−メツI・を基体としC−装入し4′ある炉内
に、T i 、 1−18よびNを含んだ混合ガスと前
記ガスに口を含んだガスを、交互に間欠的に導入し、化
学蒸着法に−U’TfBNとTiNを交7:7にかつ多
層被覆りることを特徴どりる多1■I伺わ1の製j6法
。[Claims] i, WC-based cemented carbide ric-based tree i~, or 1
-iN group" on the surface of J-meth1-, -1-! 13N
The coating layer has a thickness smaller than that of a single layer, totaling 512 to 15 μn1.
The thickness of li and L) is coated with 8 or more layers (
Multiple cover 11'ji which takes 1j1 character to become. 2. The multilayer coating material according to special claim 11f4, characterized in that the thickness of the single layer is 0.5 μm) or more. 1!
971 Claim 1 or 21 ('
The multiplex skin described in 4 A. 4. T i , 1-18 and N are charged into a 4′ furnace using WCC cemented carbide R; A multilayer film characterized by alternately and intermittently introducing a mixed gas containing the above gas and a gas containing the above gas, and coating U'TfBN and TiN in a 7:7 ratio and in multiple layers using a chemical vapor deposition method. 1■ I heard 1's manufacturing j6 method.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17054082A JPS5959879A (en) | 1982-09-29 | 1982-09-29 | Multi-coated material and its production |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17054082A JPS5959879A (en) | 1982-09-29 | 1982-09-29 | Multi-coated material and its production |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5959879A true JPS5959879A (en) | 1984-04-05 |
Family
ID=15906795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17054082A Pending JPS5959879A (en) | 1982-09-29 | 1982-09-29 | Multi-coated material and its production |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5959879A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62280363A (en) * | 1986-05-29 | 1987-12-05 | Nippon Tungsten Co Ltd | Coated hard tool |
JPH0238585A (en) * | 1988-06-14 | 1990-02-07 | Gte Lab Inc | Method for composite coating and adhering on a fire-proof base material |
US7267701B2 (en) * | 2002-05-21 | 2007-09-11 | Walter Aktiengesellschaft | TiBN coating |
CN103252939A (en) * | 2013-05-17 | 2013-08-21 | 宜昌后皇真空科技有限公司 | Chromium nitride/boron nitride titanium nano composite multi-layer coating cutter and preparation method thereof |
-
1982
- 1982-09-29 JP JP17054082A patent/JPS5959879A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62280363A (en) * | 1986-05-29 | 1987-12-05 | Nippon Tungsten Co Ltd | Coated hard tool |
JPH0238585A (en) * | 1988-06-14 | 1990-02-07 | Gte Lab Inc | Method for composite coating and adhering on a fire-proof base material |
US7267701B2 (en) * | 2002-05-21 | 2007-09-11 | Walter Aktiengesellschaft | TiBN coating |
CN103252939A (en) * | 2013-05-17 | 2013-08-21 | 宜昌后皇真空科技有限公司 | Chromium nitride/boron nitride titanium nano composite multi-layer coating cutter and preparation method thereof |
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