JPH083750A - Heat resistant coating member - Google Patents
Heat resistant coating memberInfo
- Publication number
- JPH083750A JPH083750A JP16301194A JP16301194A JPH083750A JP H083750 A JPH083750 A JP H083750A JP 16301194 A JP16301194 A JP 16301194A JP 16301194 A JP16301194 A JP 16301194A JP H083750 A JPH083750 A JP H083750A
- Authority
- JP
- Japan
- Prior art keywords
- titanium
- layer
- base material
- coated
- hard layer
- 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.)
- Granted
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 37
- 239000011248 coating agent Substances 0.000 title claims abstract description 35
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 12
- 239000000956 alloy Substances 0.000 claims abstract description 12
- 239000000919 ceramic Substances 0.000 claims abstract description 8
- 239000007769 metal material Substances 0.000 claims abstract description 7
- 239000010410 layer Substances 0.000 claims description 62
- 239000010936 titanium Substances 0.000 claims description 51
- 239000000463 material Substances 0.000 claims description 42
- 229910052719 titanium Inorganic materials 0.000 claims description 38
- 229910052782 aluminium Inorganic materials 0.000 claims description 16
- 229910052799 carbon Inorganic materials 0.000 claims description 16
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 14
- 229910052757 nitrogen Inorganic materials 0.000 claims description 13
- 229910052760 oxygen Inorganic materials 0.000 claims description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 9
- 229910052726 zirconium Inorganic materials 0.000 claims description 9
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 8
- 239000001301 oxygen Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 7
- 239000002356 single layer Substances 0.000 claims description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 5
- 150000001875 compounds Chemical class 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- 229910052721 tungsten Inorganic materials 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- 150000004767 nitrides Chemical class 0.000 claims description 4
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052720 vanadium Inorganic materials 0.000 claims description 4
- 229910052735 hafnium Inorganic materials 0.000 claims description 3
- 150000001247 metal acetylides Chemical class 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052755 nonmetal Inorganic materials 0.000 claims description 3
- 239000006104 solid solution Substances 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 claims description 2
- 150000004649 carbonic acid derivatives Chemical class 0.000 claims description 2
- 230000000737 periodic effect Effects 0.000 claims description 2
- -1 compound nitride Chemical class 0.000 claims 4
- 229910002091 carbon monoxide Inorganic materials 0.000 claims 2
- 229910002090 carbon oxide Inorganic materials 0.000 claims 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims 1
- 230000003247 decreasing effect Effects 0.000 claims 1
- 239000000758 substrate Substances 0.000 abstract description 9
- 230000003647 oxidation Effects 0.000 abstract description 3
- 238000007254 oxidation reaction Methods 0.000 abstract description 3
- 230000035939 shock Effects 0.000 abstract description 3
- 239000010935 stainless steel Substances 0.000 abstract description 3
- 229910001220 stainless steel Inorganic materials 0.000 abstract description 3
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 abstract 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 abstract 1
- 229910052593 corundum Inorganic materials 0.000 abstract 1
- 230000004927 fusion Effects 0.000 abstract 1
- 229910001845 yogo sapphire Inorganic materials 0.000 abstract 1
- 238000005520 cutting process Methods 0.000 description 20
- 230000000052 comparative effect Effects 0.000 description 15
- 230000000694 effects Effects 0.000 description 10
- 239000007789 gas Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 238000006243 chemical reaction Methods 0.000 description 5
- 238000003466 welding Methods 0.000 description 5
- 239000008199 coating composition Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000005240 physical vapour deposition Methods 0.000 description 4
- 229910052715 tantalum Inorganic materials 0.000 description 4
- 239000011195 cermet Substances 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 239000011247 coating layer Substances 0.000 description 3
- 238000005530 etching Methods 0.000 description 3
- 239000012495 reaction gas Substances 0.000 description 3
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 229910000997 High-speed steel Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 238000010849 ion bombardment Methods 0.000 description 2
- 238000007733 ion plating Methods 0.000 description 2
- 238000005268 plasma chemical vapour deposition Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910003178 Mo2C Inorganic materials 0.000 description 1
- 229910019802 NbC Inorganic materials 0.000 description 1
- GQPLMRYTRLFLPF-UHFFFAOYSA-N Nitrous Oxide Chemical class [O-][N+]#N GQPLMRYTRLFLPF-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 229910002065 alloy metal Inorganic materials 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 238000009837 dry grinding Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 102200082816 rs34868397 Human genes 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910003468 tantalcarbide Inorganic materials 0.000 description 1
- 238000002230 thermal chemical vapour deposition Methods 0.000 description 1
- 229910003470 tongbaite Inorganic materials 0.000 description 1
Landscapes
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Chemical Vapour Deposition (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、ステンレス鋼,高速度
鋼,ダイス鋼,Ti合金,Al合金,耐熱合金に代表さ
れる金属材料、または超硬合金,サーメットに代表され
る焼結合金、もしくはAl2O3系焼結体,ZrO2系焼
結体,SiC系焼結体,Si3N4系焼結体に代表される
セラミックス焼結体の基材上に、チタン・アルミニウム
炭窒酸化物の硬質層を被覆してなる被覆部材に関し、具
体的には、例えば旋削工具,フライス工具,エンドミ
ル,ドリルに代表される切削工具、スリッター,製缶工
具,金型に代表される耐摩耗工具、または釣具,ゴルフ
クラブ、時計用部品,メガネの枠,タイピン,ブロー
チ,イヤリングに代表されるスポーツ用部材や装飾用部
材として適する耐熱性被覆部材に関する。The present invention relates to a metal material typified by stainless steel, high speed steel, die steel, Ti alloy, Al alloy, heat resistant alloy, or cemented carbide, and sintered alloy typified by cermet. Alternatively, titanium / aluminum carbonitride is formed on the base material of a ceramics sintered body represented by an Al 2 O 3 system sintered body, a ZrO 2 system sintered body, a SiC system sintered body, and a Si 3 N 4 system sintered body. Regarding a covering member formed by coating a hard oxide layer, specifically, for example, turning tools, milling tools, end mills, cutting tools typified by drills, slitters, can-making tools, and wear resistance typified by dies. The present invention relates to a heat-resistant covering member suitable as a sports member or a decorative member represented by tools, fishing tackles, golf clubs, watch parts, eyeglass frames, tie pins, broaches, and earrings.
【0002】[0002]
【従来の技術】金属材料,焼結合金またはセラミックス
焼結体の基材上に、周期律表の4a,5a,6a族金属
の炭化物,窒化物,炭酸化物,窒酸化物およびこれらの
相互固溶体または酸化アルミニウムの中の1種の単層、
もしくは2種以上の複層の被膜を被覆してなる被覆部材
が多数提案されており、これらの中の1部の被覆部材に
ついては、切削工具,耐摩耗工具,スポーツ用部材,装
飾用部材などに実用されている。2. Description of the Related Art Carbides, nitrides, carbonates, nitrous oxides of the metals of groups 4a, 5a and 6a of the periodic table and their mutual solid solutions are formed on a base material of a metal material, a sintered alloy or a ceramics sintered body. Or a single layer of aluminum oxide,
Alternatively, a large number of coating members formed by coating two or more types of multi-layer coatings have been proposed, and some of these coating members include cutting tools, wear-resistant tools, sports members, and decorative members. Has been put to practical use.
【0003】これらの従来の被覆部材の内、Ti化合物
の被膜が被覆された被覆部材は、切削工具や耐摩耗工具
に用いた場合に満足できるような耐摩耗性を示さず、比
較的短時間で寿命に至るという問題があり、この問題を
解決しようとした代表的なものに、特開昭62−565
65号公報がある。Among these conventional coated members, a coated member coated with a Ti compound coating does not exhibit sufficient wear resistance when used as a cutting tool or wear resistant tool, and is relatively short in time. However, there is a problem of reaching the end of life, and a typical example that attempts to solve this problem is JP-A-62-565.
There is a publication No. 65.
【0004】[0004]
【発明が解決しようとする課題】特開昭62−5656
5号公報には、基材の表面にTiとAlの炭化物,窒化
物,および炭窒化物のうちの1種の単層または2種以上
の複層でなる硬質被覆層を0.5〜10μm厚さで形成
した耐摩耗性にすぐれた表面被覆硬質部材について記載
されている。Problems to be Solved by the Invention JP-A-62-5656
JP-A No. 5-55 discloses that a hard coating layer composed of a single layer of Ti and Al carbides, nitrides, and carbonitrides of Ti and Al or a multi-layer of two or more layers is formed on the surface of a base material at 0.5 to 10 μm. It describes a surface-coated hard member formed of a thickness and having excellent wear resistance.
【0005】同公報に記載されている表面被覆硬質部材
は、耐摩耗性の向上したすぐれた被覆硬質部材ではある
が、例えば切削工具として用いた場合に、高速切削また
は重切削のように、より高温の条件で使用すると、硬質
被覆層の酸化,摩耗の進行が速く、耐熱衝撃性に劣り、
相手材である被削材との溶着も生じやすくなり短寿命に
なるという問題がある。The surface-coated hard member described in the above publication is an excellent coated hard member having improved wear resistance, but when it is used as a cutting tool, for example, high-speed cutting or heavy cutting, When used under high temperature conditions, the hard coating layer rapidly oxidizes and wears, resulting in poor thermal shock resistance.
There is also a problem that welding with a work material which is a mating material easily occurs and the life becomes short.
【0006】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、低温領域から高温領域に至るまで
の広い領域において、耐摩耗性,耐酸化性,耐熱衝撃
性,耐欠損性および耐溶着性に優れる耐熱性被覆部材の
提供を目的とする。The present invention has solved the above-mentioned problems, and specifically, it has wear resistance, oxidation resistance, thermal shock resistance, and thermal resistance in a wide range from a low temperature region to a high temperature region. An object of the present invention is to provide a heat-resistant covering member having excellent chipping property and welding resistance.
【0007】[0007]
【課題を解決するための手段】本発明者らは、超硬合金
の基材上にTiとAlとの化合物の被膜を被覆した被覆
部材が低温領域で使用すると割合にすぐれた効果を発揮
するのに対し、高温領域で使用するとその効果が低減さ
れるという問題を検討していた所、TiとAlとの化合
物被膜中に酸素元素を微量含有させると低温領域から高
温領域まで耐摩耗性の低減が生じなく、諸特性がバラン
スよくすぐれて顕著に寿命が向上するという知見を得
て、本発明を完成するに至ったものである。Means for Solving the Problems The inventors of the present invention exert a particularly excellent effect when a coating member obtained by coating a film of a compound of Ti and Al on a base material of cemented carbide is used in a low temperature region. On the other hand, when the problem that the effect is reduced when used in the high temperature region was investigated, when a trace amount of oxygen element was contained in the compound film of Ti and Al, the wear resistance from the low temperature region to the high temperature region was improved. The present invention has been completed based on the knowledge that the characteristics are well-balanced and the life is remarkably improved without reduction.
【0008】すなわち、本発明の耐熱性被覆部材は、金
属,合金またはセラミックス焼結体の基材上に、チタン
・アルミニウム炭窒酸化物の硬質層が0.1〜15μm
の膜厚で被覆されていることを特徴とする。That is, in the heat resistant coating member of the present invention, a hard layer of titanium / aluminum oxycarbonitride is 0.1 to 15 μm on a base material of a metal, alloy or ceramics sintered body.
It is characterized by being coated with a film thickness of.
【0009】本発明の被覆部材における基材は、硬質層
を被覆するときに加熱する温度に耐えることができる金
属材料,焼結合金またはセラミックス焼結体からなり、
具体的には例えばステンレス鋼,高速度鋼,ダイス
鋼,,チタン合金,Al合金,耐熱合金の金属材料、ま
たは超硬合金,サーメットの焼結合金、Al2O3系焼結
体,Si3N4系焼結体,サイアロン系焼結体,ZrO2
系焼結体のセラミックス焼結体を挙げることができる。
これらの内、切削工具または耐摩耗工具として用いる場
合には、超硬合金,窒素含有TiC系サーメットもしく
はセラミックス焼結体の基材が特に好ましい。The base material in the coating member of the present invention is made of a metal material, a sintered alloy or a ceramics sintered body capable of withstanding the temperature of heating when coating the hard layer,
Specifically, for example, stainless steel, high-speed steel, die steel, titanium alloy, Al alloy, heat-resistant alloy metal material, cemented carbide, cermet sintered alloy, Al 2 O 3 system sintered body, Si 3 N 4 type sintered body, sialon type sintered body, ZrO 2
A ceramic sintered body of a system sintered body can be mentioned.
Among these, when used as a cutting tool or an abrasion resistant tool, a cemented carbide, a nitrogen-containing TiC-based cermet or a ceramics sintered body is particularly preferable.
【0010】この基材上に被覆される硬質層は、基材に
直接隣接して被覆させる場合には基材材質により、特に
硬質層中の酸素元素の含有量が変動していることも好ま
しく、具体的には、例えば、焼結合金の基材では、硬質
層の表面から基材側に向って酸素元素が漸減しているこ
とが好ましく、逆にセラミックス焼結体の基材では、硬
質層の表面から基材側に向って酸素元素が漸増している
ことが硬質層と基材との密着性の点で好ましいことであ
る。この硬質層は、化学量論的組成または非化学量論的
組成であってもよいが、特に(Tia,Alb)
(CX,NY,OZ)Rと表わしたときに、〔但し、Tiは
チタン、Alはアルミニウム、Cは炭素、Nは窒素、O
は酸素を示し、aおよびbは金属元素であるTiとAl
のそれぞれの原子比を表わし、X,YおよびZは非金属
元素であるCとNとOのそれぞれの原子比を表わし、R
はTiとAlとを合計した金属元素に対するCとNとO
とを合計した非金属元素の原子比を表わす)a+b=
1、0.95≧a≧0.05、X+Y+Z=1、0.8
9≧X≧0.1、0.89≧Y≧0.1、0.25≧Z
≧0.01、1.10≧R≧0.80の条件を満足する
チタン・アルミニウム炭窒酸化物でなる場合が強度,耐
摩耗性,耐溶着性から特に好ましいものである。It is also preferable that the hard layer coated on the substrate has a variable oxygen element content, particularly in the hard layer, depending on the material of the substrate when the hard layer is coated directly on the substrate. Specifically, for example, in a sintered alloy base material, it is preferable that the oxygen element gradually decreases from the surface of the hard layer toward the base material side. It is preferable that the oxygen element gradually increases from the surface of the layer toward the base material side from the viewpoint of adhesion between the hard layer and the base material. The hard layer may be stoichiometric or non-stoichiometric, but in particular (Tia, Alb)
When expressed as (C X , N Y , O Z ) R , [wherein Ti is titanium, Al is aluminum, C is carbon, N is nitrogen, O is
Indicates oxygen, and a and b are metal elements Ti and Al.
And X, Y, and Z represent the atomic ratios of C, N, and O, which are nonmetallic elements, and R
Is C, N and O for the metal element which is the sum of Ti and Al.
Represents the atomic ratio of the non-metal elements, which is the sum of) and a + b =
1, 0.95 ≧ a ≧ 0.05, X + Y + Z = 1, 0.8
9 ≧ X ≧ 0.1, 0.89 ≧ Y ≧ 0.1, 0.25 ≧ Z
It is particularly preferable to use titanium / aluminum carbonitride oxide satisfying the conditions of ≧ 0.01 and 1.10 ≧ R ≧ 0.80 from the viewpoint of strength, wear resistance and welding resistance.
【0011】また、本発明の被覆部材における被膜構成
としては、上述した基材と硬質層との間に、基材と硬質
層との主として密着性を高める内層を介在させることも
好ましく、この内層としては、具体的には、例えばT
i,Zr,Hf,V,Nb,Ta,Cr,Mo,Wの金
属,TiC,ZrC,HfC,VC,NbC,TaC,
Cr3C2,Mo2C ,WC,TiN,ZrN,CrN,
Ti(C,N),Ti(C,O),Ti(N,O),T
i(C,N,O),(Ti,Zr)C,(Ti,Z)
N,(Ti,Z)(C,N),(Ti,Ta)C,(T
i,W)C,(Ti,Ta,W)(CN),(Ti,T
a,W)N,(Ti,Zr,Ta)Cを挙げることがで
きる。これらの内層は、基材の材質によって選定するこ
とが好ましく、基材が焼結合金の場合には、例えばTi
C,TiN,Ti(C,N),Ti(C,O),Ti
(N,O),Ti(C,N,O),(Ti,Zr)C,
(Ti,Hf)C,(Ti,V)C,(Ti,Nb)
C,(Ti,Cr)C,(Ti,Mo)C,(Ti,
W)C,(Ti,Zr)N,(Ti,V)N,(Ti,
Cr)N,(Ti,Zr)(C,N),(Ti,Zr)
(C,O),(Ti,Zr)(N,O),(Ti,Z
r)(C,N,O)の1種の単層または2種以上の多層
でなることが基材と硬質層の密着性の媒介性、被覆部材
としての耐摩耗性および耐欠損性から特に好ましいこと
である。Further, the coating composition in the coating member of the present invention
As between the base material and the hard layer described above, the base material and the hard layer
It is also possible to interpose an inner layer that mainly improves adhesion with the layer.
The inner layer is preferably, for example, T
i, Zr, Hf, V, Nb, Ta, Cr, Mo, W gold
Genus, TiC, ZrC, HfC, VC, NbC, TaC,
Cr3C2, Mo2C , WC, TiN, ZrN, CrN,
Ti (C, N), Ti (C, O), Ti (N, O), T
i (C, N, O), (Ti, Zr) C, (Ti, Z)
N, (Ti, Z) (C, N), (Ti, Ta) C, (T
i, W) C, (Ti, Ta, W) (CN), (Ti, T
a, W) N, (Ti, Zr, Ta) C
Wear. These inner layers can be selected according to the material of the base material.
Is preferable, and when the base material is a sintered alloy, for example, Ti
C, TiN, Ti (C, N), Ti (C, O), Ti
(N, O), Ti (C, N, O), (Ti, Zr) C,
(Ti, Hf) C, (Ti, V) C, (Ti, Nb)
C, (Ti, Cr) C, (Ti, Mo) C, (Ti,
W) C, (Ti, Zr) N, (Ti, V) N, (Ti,
Cr) N, (Ti, Zr) (C, N), (Ti, Zr)
(C, O), (Ti, Zr) (N, O), (Ti, Z
r) One single layer of (C, N, O) or multiple layers of two or more
Consists of the mediation of the adhesion between the base material and the hard layer, the covering member
Is particularly preferable from the viewpoint of wear resistance and fracture resistance as
Is.
【0012】さらに、硬質層に隣接して外層を形成する
被膜構成とすることも好ましく、外層が酸化アルミニウ
ムでなる場合には、高温における耐溶着性,耐酸化性,
耐摩耗性にすぐれることから、好ましいことである。こ
れらの被覆層の最表面、具体的には、硬質層の表面また
は酸化アルミニウムの外層の表面に、さらに窒化チタ
ン,窒酸化チタン,炭窒酸化チタンの外層を被覆する
と、装飾的効果,使用前後の判別の容易性効果または色
むら防止効果にもなって好ましいことである。Further, it is also preferable that the outer layer is formed adjacent to the hard layer, and when the outer layer is made of aluminum oxide, the welding resistance, the oxidation resistance at high temperature,
It is preferable because it has excellent wear resistance. When the outermost surface of these coating layers, specifically, the surface of the hard layer or the surface of the outer layer of aluminum oxide, is further coated with the outer layer of titanium nitride, titanium oxynitride, or titanium oxycarbonitride, the decorative effect, before and after use It is also preferable because it has an effect of facilitating the discrimination of or the effect of preventing color unevenness.
【0013】本発明の被覆部材における被膜構成の内、
硬質層のみの構成でなる場合には、被膜厚さが0.1〜
15μmでなるもので、0.1μm未満の厚さになる
と、硬質層の効果が弱く、耐摩耗性の低下が著しく、逆
に15μmを超えた厚さになると、被膜の剥離が生じや
すくなる。硬質層の厚さは、好ましくは0.5〜10μ
m、特に成膜時間などを含めた工業的製造上から0.5
〜8μmが好ましい。この硬質層の他に、内層を介在さ
せる構成でなる場合には、内層の厚さが0.1〜5μm
であることが好ましく、さらに外層を形成させる構成で
なる場合には、外層の厚さが0.1〜5μmであること
が好ましく、内層と硬質層または内層と硬質層と外層と
いう被膜の総厚さが0.5〜15μmでなることが好ま
しいことである。Of the film constitutions in the covering member of the present invention,
When the hard layer only is used, the coating thickness is 0.1 to
When the thickness is less than 0.1 μm, the effect of the hard layer is weak and the wear resistance is significantly deteriorated. On the contrary, when the thickness exceeds 15 μm, peeling of the coating is likely to occur. The hard layer preferably has a thickness of 0.5 to 10 μm.
m, especially 0.5 in terms of industrial production including film forming time
-8 μm is preferable. When the inner layer is formed in addition to the hard layer, the inner layer has a thickness of 0.1 to 5 μm.
When the outer layer is formed, the outer layer preferably has a thickness of 0.1 to 5 μm, and the total thickness of the inner layer and the hard layer or the inner layer, the hard layer and the outer layer. Is preferably 0.5 to 15 μm.
【0014】本発明の被覆部材は、市販または従来から
提案されている各種の基材を用いて、従来から行われて
いる化学蒸着法(CVD法)や物理蒸着法(PVD法)
を応用することにより作製することができる。具体的に
は、CVD法の場合には、プラズマCVD法が好まし
く、このプラズマCVD法やPVD法におけるガス圧の
調整、特に酸素元素を供給するためのガス圧の調整が重
要である。また、イオンプレーティング法やスパッタ法
のPVD法により成膜すると、被膜に大きな圧縮応力を
残留させることができて、耐欠損性が顕著にすぐれるこ
とから好ましいことである。The coated member of the present invention uses various types of base materials that are commercially available or conventionally proposed, and the conventional chemical vapor deposition method (CVD method) or physical vapor deposition method (PVD method) is used.
Can be produced by applying. Specifically, in the case of the CVD method, the plasma CVD method is preferable, and it is important to adjust the gas pressure in the plasma CVD method or the PVD method, particularly to adjust the gas pressure for supplying oxygen element. Further, it is preferable to form the film by the PVD method such as the ion plating method or the sputtering method because a large compressive stress can be left in the film and the fracture resistance is remarkably improved.
【0015】[0015]
【作用】本発明の被覆部材は、基材上に被覆されたチタ
ン・アルミニウム炭窒酸化物の硬質層が耐熱性を高める
作用をし、その結果、高温における耐摩耗性,耐溶着性
および耐酸化性を向上させる作用をしていること、特に
焼結合金の基材でなる場合には、硬質層に大きな圧縮応
力を残留させる作用が生じ、その結果被膜の強度および
耐摩耗性を高める間接的作用となっている。In the coated member of the present invention, the hard layer of titanium / aluminum oxycarbonitride coated on the base material acts to enhance heat resistance, and as a result, wear resistance, welding resistance and acid resistance at high temperature. It has the effect of improving the chemical conversion property, especially when it is made of a sintered alloy base material, it causes the effect of leaving a large compressive stress in the hard layer, resulting in an increase in the strength and wear resistance of the coating. It has become an action.
【0016】[0016]
【実施例1】イオンプレーティング装置の反応容器内
に、市販の超硬合金(JIS規格、P30相当材種、S
DKN42ZTN形状)の基材を設置した後、加熱工
程、Arのエッチング工程および被覆工程を施して、本
発明品1〜5と比較品1〜3を得た。この内、本発明品
1〜5は、基材を設置した電子加熱式反応容器内を1×
10-5Torrの高真空状態まで排気した後、Arガス
を導入し、2×10-3Torrの圧力状態とし、本発明
品1〜3については出力10kw,60分間加熱して基
材を400℃保持、本発明品4,5については出力12
kw,60分間加熱して基材を420℃保持による加熱
を行った。次に、反応容器内の圧力を1×10-3Tor
rまで変化させて、基材側に−300Vの電圧を印加
し、反応容器と基材間にグロー放電を発生させて基材表
面を30分間Arイオンボンバード処理によるArエッ
チングを行った。次いで、表1に示した被覆条件(窒素
ガス純度5Nを使用)による被覆を行って、本発明品1
〜5を得た。Example 1 A commercially available cemented carbide (JIS standard, P30 equivalent grade, S
After a base material of DKN42ZTN shape) was installed, a heating step, an Ar etching step and a coating step were performed to obtain inventive products 1 to 5 and comparative products 1 to 3. Among these, the products 1 to 5 of the present invention have 1 ×
After exhausting to a high vacuum state of 10 −5 Torr, Ar gas was introduced to make a pressure state of 2 × 10 −3 Torr, and for the products 1 to 3 of the present invention, the output was 10 kw, and the substrate was heated for 60 minutes to 400 times. Hold at ℃, output 12 for products 4 and 5 of the present invention
The base material was heated at 420 ° C. by heating for 60 minutes with kw. Next, the pressure inside the reaction vessel is set to 1 × 10 −3 Tor.
The voltage was changed to r and a voltage of −300 V was applied to the base material side to generate glow discharge between the reaction vessel and the base material, and the base material surface was subjected to Ar etching by Ar ion bombardment for 30 minutes. Then, coating was performed under the coating conditions shown in Table 1 (using a nitrogen gas purity of 5N) to obtain the product 1 of the present invention.
~ 5 was obtained.
【0017】一方、比較品1〜3は、基材を設置した抵
抗加熱式反応容器内を1×10-4Torrに真空排気し
た後、Arガスを導入し、4×10-4〜1×10-4To
rrの圧力状態で出力20kw,60分間加熱して基材
を500℃保持による加熱を行った。次に,反応容器内
の圧力を8×10-2TorrのArガス中、基材側に直
流電圧−600V印加し、基材表面を10分間Arイオ
ンボンバード処理によるArエッチングを行った。次い
で、表1に示した被覆条件による被覆を行って、比較品
1〜3を得た。On the other hand, in Comparative Products 1 to 3, 4 × 10 −4 to 1 × was introduced by introducing Ar gas after evacuating the inside of the resistance heating type reaction vessel having the base material to 1 × 10 −4 Torr. 10 -4 To
The substrate was heated at a temperature of rr at an output of 20 kw for 60 minutes to hold the substrate at 500 ° C. Next, a DC voltage of -600 V was applied to the base material side in Ar gas of 8 × 10 -2 Torr in the reaction vessel, and the base material surface was subjected to Ar etching by Ar ion bombardment for 10 minutes. Then, coating was performed under the coating conditions shown in Table 1 to obtain comparative products 1 to 3.
【0018】こうして得た本発明品1〜5および比較品
1〜3のそれぞれの被膜組成成分は、X線回折装置およ
びグロー放電発光分析装置により解析し、表2に示し
た。また、それぞれの被膜厚さは、走査型電子顕微鏡で
調べ、さらにそれぞれの被膜表面からCu−Kα線によ
るX線回折法でもって被膜の残留応力を求めて表2に併
記した。The coating composition components of the invention products 1 to 5 and the comparative products 1 to 3 thus obtained were analyzed by an X-ray diffractometer and a glow discharge emission spectrometer, and are shown in Table 2. The film thickness of each film was examined by a scanning electron microscope, and the residual stress of the film was determined from the surface of each film by the X-ray diffraction method using Cu-Kα ray.
【0019】次に、本発明品1〜5および比較品1〜3
を用いて、被削材:SCM440、工具形状:SDKN
42ZTN、切削速度:161m/min、切込み:2
mm、送り:0.2mm/刃、乾式フライス切削による
条件で100×150mm2面を20パス切削後の平均
逃げ面摩耗量を求めて、表2に併記した。Next, products 1 to 5 of the present invention and comparative products 1 to 3
Work Material: SCM440, Tool Shape: SDKN
42ZTN, cutting speed: 161m / min, depth of cut: 2
mm, feed: 0.2 mm / blade, the average flank wear amount after cutting 20 passes of 100 × 150 mm 2 surface under the condition of dry milling cutting was also shown in Table 2.
【0020】[0020]
【表1】 [Table 1]
【0021】[0021]
【表2】 [Table 2]
【0022】[0022]
【実施例2】市販の超硬合金(JIS規格、K10相当
材種)に基材を用いた以外は、本発明品6〜10の硬質
層の形成は、実施例1の本発明品1〜5と略同様にし
(反応ガス組成,ガス圧力を主として調整)、比較品4
〜6の硬質層の形成は、実施例1の比較品1〜3と略同
様にして行い、内層の形成は従来から行われているイオ
ンプレーティング法の条件でもって行った。Example 2 The hard layers of the products 6 to 10 of the present invention were formed in the same manner as the products 1 to 1 of the present invention except that the substrate was used for a commercially available cemented carbide (JIS standard, K10 equivalent grade). Comparative product 4 in the same manner as 5 (mainly adjusting reaction gas composition and gas pressure)
The hard layers of Nos. 6 to 6 were formed in substantially the same manner as the comparative products 1 to 3 of Example 1, and the inner layers were formed under the conditions of the ion plating method which has been conventionally used.
【0023】本発明品6〜10および比較品4〜6のそ
れぞれの被膜組成成分は、実施例1と同様にして求め
て、その結果を表3に示した。表3に示した本発明品6
〜10および比較品4〜6を用いて、被削材:S48
C、切削速度:150m/min、切込み:1.5m
m、送り:0.3mm/rev、切削時間:30mi
n、乾式旋削による第1切削条件と、被削材:FC3
5、切削速度:150m/min、切込み:1.5m
m、送り:0.3mm/rev、切削時間:10mi
n、乾式旋削による第2切削条件でもって切削試験を行
い、そのときのそれぞれの平均逃げ面摩耗量を求めて、
表3に示した。The coating composition components of the invention products 6 to 10 and the comparative products 4 to 6 were determined in the same manner as in Example 1, and the results are shown in Table 3. Invention product 6 shown in Table 3
-10 and comparative products 4-6, work material: S48
C, cutting speed: 150 m / min, depth of cut: 1.5 m
m, feed: 0.3 mm / rev, cutting time: 30 mi
n, the first cutting conditions by dry turning and the work material: FC3
5, cutting speed: 150m / min, depth of cut: 1.5m
m, feed: 0.3 mm / rev, cutting time: 10 mi
n, a cutting test is performed under the second cutting condition by dry turning, and the average flank wear amount at each time is obtained,
The results are shown in Table 3.
【0024】[0024]
【表3】 [Table 3]
【0025】[0025]
【実施例3】市販の超硬合金(JIS規格P30相当材
種、SNMG120408形状)を基材として用いて、
基材上に内層と硬質層と外層とを被覆して本発明品11
〜16を作製し、基材上に第1層〜第4層を順次被覆し
て比較品7,8を作製した。本発明品における内層と外
層、および比較品の被膜は、従来から行われているプラ
ズマ熱CVD法で被覆し、本発明品11〜14の硬質層
は、実施例1の本発明品1〜5と略同様にし、(反応ガ
ス組成,ガス圧力,を主として調整)本発明品15,1
6の硬質層は、TiCl:40cc/min、AlCl
3:30〜35cc/min、NH3:150〜200c
c/min、H2:2000cc/min、CH4:25
0cc/min、O2:40cc/minの反応ガス組
成、炉内圧力1.0Torr、バイアス電圧−500
V、被覆時間45分でもって被覆した。Example 3 Using a commercially available cemented carbide (JIS standard P30 equivalent grade, SNMG120408 shape) as a base material,
The present invention product 11 obtained by coating a base material with an inner layer, a hard layer and an outer layer.
To 16 were produced, and the first to fourth layers were sequentially coated on the base material to produce comparative products 7 and 8. The inner and outer layers of the product of the present invention and the coatings of the comparative product are coated by the conventional plasma thermal CVD method, and the hard layers of the products 11 to 14 of the present invention are the hard layers of the products of Example 1 to 1 to 5 of the invention. In the same manner as described above (mainly adjusting the reaction gas composition and gas pressure), the product of the present invention 15, 1
The hard layer of 6 is TiCl: 40 cc / min, AlCl
3 : 30 to 35 cc / min, NH 3 : 150 to 200 c
c / min, H 2 : 2000 cc / min, CH 4 : 25
0 cc / min, O 2 : 40 cc / min reaction gas composition, furnace pressure 1.0 Torr, bias voltage −500
V, coating time 45 minutes.
【0026】こうして得た本発明品11〜16および比
較品7,8のそれぞれの被膜組成成分は、実施例1と同
様にして求めて、その結果を表4に示した。表4に示し
た本発明品11〜16および比較品7,8を用いて、被
削材:S45C(HB190)、切削速度:300m/
min、送り:0.5mm/rev、切込み:2.0m
m、切削時間:60minの条件でもって旋削試験を行
い、その結果を表4に併記した。また、本発明品11〜
16および比較品7,8の被膜表面から引掻き硬さ試験
機に相当する機器でもってスクラッチ強度試験を行い、
そのときの被膜が剥離しない最大荷重を求めて表4に併
記した。さらに、本発明品11〜16および比較品7,
8の被膜の残留応力を実施例1と同様にして求めて、そ
の結果を表4に併記した。The coating composition components of the inventive products 11 to 16 and the comparative products 7 and 8 thus obtained were determined in the same manner as in Example 1, and the results are shown in Table 4. Using the inventive products 11 to 16 and the comparative products 7 and 8 shown in Table 4, a work material: S45C (H B 190), a cutting speed: 300 m /
min, feed: 0.5 mm / rev, depth of cut: 2.0 m
A turning test was conducted under the conditions of m, cutting time: 60 min, and the results are also shown in Table 4. Further, the products 11 to 11 of the present invention
Scratch strength test was carried out from the coating surface of 16 and comparative products 7 and 8 with a device equivalent to a scratch hardness tester,
The maximum load at which the coating film did not peel off at that time was determined and listed in Table 4. Further, the present invention products 11 to 16 and the comparative product 7,
The residual stress of the coating film No. 8 was determined in the same manner as in Example 1, and the results are also shown in Table 4.
【0027】[0027]
【表4】 [Table 4]
【0028】[0028]
【発明の効果】本発明の耐熱被覆部材は、チタン・アル
ミニウム炭窒化物被膜が被覆された従来の被覆部材に比
べて、被膜に残留する圧縮応力が高く、被膜の耐剥離性
が優れており、その結果、切削工具として用いた場合に
おける耐摩耗性(被膜の剥離および微小チッピング含む
摩耗)が約3〜4倍も優れているという顕著な効果があ
る。EFFECTS OF THE INVENTION The heat-resistant coated member of the present invention has a higher compressive stress remaining in the coating and is excellent in peel resistance as compared with the conventional coated member coated with a titanium / aluminum carbonitride coating. As a result, there is a remarkable effect that the wear resistance (wear including peeling of the coating and fine chipping) when used as a cutting tool is excellent by about 3 to 4 times.
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 FI 技術表示箇所 C23C 16/34 // C23C 30/00 C ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Internal reference number FI technical display location C23C 16/34 // C23C 30/00 C
Claims (6)
焼結体の基材上に、チタン・アルミニウム炭窒酸化物の
硬質層が0.1〜15μmの膜厚で被覆されていること
を特徴とする耐熱性被覆部材。1. A hard material layer of titanium / aluminum carbonitride oxide is coated on a base material of a metal material, a sintered alloy or a ceramics sintered body in a film thickness of 0.1 to 15 μm. A heat resistant covering member.
表の4a,5a,6a族金属並びにこれらの炭化物,窒
化物,炭酸化物,窒酸化物およびこれらの相互固溶体ま
たはこれらの混合物の中から選ばれた1種の単層もしく
は2種以上の多層でなる内層が被覆されていることを特
徴とする請求項1記載の耐熱性被覆部材。2. A metal of group 4a, 5a, 6a of the periodic table, and their carbides, nitrides, carbonates, oxynitrides and mutual solid solutions thereof, or a mutual solid solution thereof, between the base material and the hard layer. The heat-resistant coated member according to claim 1, characterized in that the heat-resistant coated member is coated with an inner layer composed of one kind of single layer or two or more kinds of multilayers selected from the mixture.
は、Tiの炭化物,窒化物,炭窒化物,炭酸化物,窒酸
化物,炭窒酸化物、またはZr,Hf,V,Nb,T
a,Cr,Mo,Wの中の少なくとも1種の元素とTi
との複合炭化物,複合窒化物,複合炭窒化物,複合炭酸
化物,複合窒酸化物,複合炭窒酸化物の中から選ばれた
1種の単層または2種以上の多層でなることを特徴とす
る請求項2記載の耐熱性被覆部材。3. The base material is made of a sintered alloy, and the inner layer is made of Ti carbide, nitride, carbonitride, carbon oxide, oxynitride, oxycarbonitride, or Zr, Hf, V, Nb, T
at least one element of a, Cr, Mo and W and Ti
Characterized by being composed of one kind of single layer or two or more kinds of layers selected from compound carbide, compound nitride, compound carbonitride, compound carbon oxide, compound carbon monoxide, and compound carbon monoxide. The heat resistant coating member according to claim 2.
ム,窒化チタン,炭窒化チタン,窒酸化チタン,炭窒酸
化チタンの中の1種の単層または2種以上の多層でなる
外層が被覆されていることを特徴とする請求項1,2ま
たは3記載の耐熱性被覆部材。4. An outer layer formed of a single layer of aluminum oxide, titanium nitride, titanium carbonitride, titanium oxynitride, or titanium oxycarbonitride or a multilayer of two or more types is coated adjacent to the hard layer. The heat-resistant coating member according to claim 1, 2, or 3, characterized in that.
基材側に向って酸素元素が漸減していることを特徴とす
る請求項1,2,3または4記載の耐熱性被覆部材。5. The heat resistant coating member according to claim 1, wherein the hard layer has oxygen elements gradually decreasing from the surface of the hard layer toward the base material side. .
チタン・アルミニウム炭窒酸化物でなることを特徴とす
る請求項1,2,3,4または5記載の耐熱性被覆部
材。 (Tia,Alb)(CX,NY,OZ)R‥‥‥‥‥(A) 〔但し、(A)式中のTiはチタン、Alはアルミニウ
ム、Cは炭素、Nは窒素、Oは酸素を示し、aおよびb
は金属元素であるTiとAlのそれぞれの原子比を表わ
し、X,YおよびZは非金属元素であるCとNとOのそ
れぞれの原子比を表わし、RはTiとAlとを合計した
金属元素に対するCとNとOとを合計した非金属元素の
原子比を表わし、それぞれはa+b=1、0.95≧a
≧0.05、X+Y+Z=1、0.89≧X≧0.1、
0.89≧Y≧0.1、0.25≧Z≧0.01、1.
10≧R≧0.80の関係にある〕6. The heat resistant coating member according to claim 1, wherein the hard layer is made of titanium / aluminum carbonitride oxide represented by the following formula (A). (Tia, Alb) (C X , N Y, O Z) R ‥‥‥‥‥ (A) [where, Ti is titanium in the formula (A), Al is aluminum, C is carbon, N is the nitrogen, O Represents oxygen, and a and b
Represents the atomic ratio of each of the metal elements Ti and Al, X, Y and Z represent the atomic ratio of each of the non-metal elements C, N and O, and R represents the metal which is the sum of Ti and Al. Represents the atomic ratio of the non-metal element, which is the sum of C, N, and O with respect to the element, and a + b = 1, 0.95 ≧ a, respectively.
≧ 0.05, X + Y + Z = 1, 0.89 ≧ X ≧ 0.1,
0.89 ≧ Y ≧ 0.1, 0.25 ≧ Z ≧ 0.01, 1.
10 ≧ R ≧ 0.80]
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP06163011A JP3130734B2 (en) | 1994-06-22 | 1994-06-22 | Heat resistant coating |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP06163011A JP3130734B2 (en) | 1994-06-22 | 1994-06-22 | Heat resistant coating |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH083750A true JPH083750A (en) | 1996-01-09 |
| JP3130734B2 JP3130734B2 (en) | 2001-01-31 |
Family
ID=15765504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP06163011A Expired - Lifetime JP3130734B2 (en) | 1994-06-22 | 1994-06-22 | Heat resistant coating |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3130734B2 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999050016A1 (en) * | 1998-04-01 | 1999-10-07 | Mitsubishi Heavy Industries, Ltd. | Gear shaping method and device and spiral bevel gear cutter |
| JP2002028803A (en) * | 2000-05-10 | 2002-01-29 | Mitsubishi Materials Corp | Throwaway cutting insert made of surface-coated tungsten carbide based cemented carbide with excellent interlayer adhesion with hard coating layer |
| US6565957B2 (en) | 2000-12-22 | 2003-05-20 | Mitsubishi Materials Corporation | Coated cutting tool |
| US7264668B2 (en) * | 2001-10-16 | 2007-09-04 | The Chinese University Of Hong Kong | Decorative hard coating and method for manufacture |
| US8747990B2 (en) | 2009-11-06 | 2014-06-10 | Tungaloy Corporation | Coated tool |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6449430B1 (en) | 1999-01-11 | 2002-09-10 | Fuji Photo Film Co., Ltd. | Lens-fitted photo film unit and assembling method for the same |
-
1994
- 1994-06-22 JP JP06163011A patent/JP3130734B2/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999050016A1 (en) * | 1998-04-01 | 1999-10-07 | Mitsubishi Heavy Industries, Ltd. | Gear shaping method and device and spiral bevel gear cutter |
| US6416262B1 (en) | 1998-04-01 | 2002-07-09 | Mitsubishi Heavy Industries, Ltd. | Gear shaping method and device and spiral bevel gear cutter |
| JP2002028803A (en) * | 2000-05-10 | 2002-01-29 | Mitsubishi Materials Corp | Throwaway cutting insert made of surface-coated tungsten carbide based cemented carbide with excellent interlayer adhesion with hard coating layer |
| US6565957B2 (en) | 2000-12-22 | 2003-05-20 | Mitsubishi Materials Corporation | Coated cutting tool |
| US7264668B2 (en) * | 2001-10-16 | 2007-09-04 | The Chinese University Of Hong Kong | Decorative hard coating and method for manufacture |
| US8747990B2 (en) | 2009-11-06 | 2014-06-10 | Tungaloy Corporation | Coated tool |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3130734B2 (en) | 2001-01-31 |
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