JPS63270467A - Coated ferrous alloy excellent in surface accuracy and its production - Google Patents
Coated ferrous alloy excellent in surface accuracy and its productionInfo
- Publication number
- JPS63270467A JPS63270467A JP10573387A JP10573387A JPS63270467A JP S63270467 A JPS63270467 A JP S63270467A JP 10573387 A JP10573387 A JP 10573387A JP 10573387 A JP10573387 A JP 10573387A JP S63270467 A JPS63270467 A JP S63270467A
- Authority
- JP
- Japan
- Prior art keywords
- titanium
- iron
- based alloy
- layer
- coating 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
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 51
- 239000000956 alloy Substances 0.000 title claims abstract description 51
- 238000004519 manufacturing process Methods 0.000 title claims description 9
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 title 1
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 28
- 238000006243 chemical reaction Methods 0.000 claims abstract description 16
- 229910000765 intermetallic Inorganic materials 0.000 claims abstract description 13
- 229910005438 FeTi Inorganic materials 0.000 claims abstract description 11
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 11
- 229930195733 hydrocarbon Natural products 0.000 claims abstract description 11
- 150000002430 hydrocarbons Chemical class 0.000 claims abstract description 11
- 239000004215 Carbon black (E152) Substances 0.000 claims abstract description 9
- -1 TiC Chemical class 0.000 claims abstract description 7
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 claims abstract description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 102
- 229910052742 iron Inorganic materials 0.000 claims description 50
- 239000010936 titanium Substances 0.000 claims description 44
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 24
- 239000000758 substrate Substances 0.000 claims description 22
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 claims description 16
- 238000000034 method Methods 0.000 claims description 11
- IXQWNVPHFNLUGD-UHFFFAOYSA-N iron titanium Chemical compound [Ti].[Fe] IXQWNVPHFNLUGD-UHFFFAOYSA-N 0.000 claims description 10
- 229910052757 nitrogen Inorganic materials 0.000 claims description 10
- FOZHTJJTSSSURD-UHFFFAOYSA-J titanium(4+);dicarbonate Chemical compound [Ti+4].[O-]C([O-])=O.[O-]C([O-])=O FOZHTJJTSSSURD-UHFFFAOYSA-J 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 150000003609 titanium compounds Chemical class 0.000 claims description 8
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 6
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 claims description 6
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 claims description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 4
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 4
- 239000001257 hydrogen Substances 0.000 claims description 3
- 229910052739 hydrogen Inorganic materials 0.000 claims description 3
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims description 2
- 229910021529 ammonia Inorganic materials 0.000 claims description 2
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 2
- 239000001569 carbon dioxide Substances 0.000 claims description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 claims description 2
- 150000002431 hydrogen Chemical class 0.000 claims 1
- 239000010410 layer Substances 0.000 abstract description 67
- 239000011247 coating layer Substances 0.000 abstract description 56
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 abstract description 7
- 229910000640 Fe alloy Inorganic materials 0.000 abstract description 2
- 150000001875 compounds Chemical class 0.000 abstract 4
- 229910002593 Fe-Ti Inorganic materials 0.000 abstract 2
- 229910003074 TiCl4 Inorganic materials 0.000 abstract 1
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 150000004820 halides Chemical class 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 0.000 abstract 1
- 239000000047 product Substances 0.000 description 34
- 230000000052 comparative effect Effects 0.000 description 19
- 238000005229 chemical vapour deposition Methods 0.000 description 7
- 238000005520 cutting process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 150000004767 nitrides Chemical class 0.000 description 4
- 238000005240 physical vapour deposition Methods 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000001746 injection moulding Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229910052582 BN Inorganic materials 0.000 description 2
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 238000007730 finishing process Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000004826 seaming Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 239000013589 supplement Substances 0.000 description 2
- 230000003746 surface roughness Effects 0.000 description 2
- 235000012976 tarts Nutrition 0.000 description 2
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 229910000889 permalloy Inorganic materials 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000004065 semiconductor 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
- 239000010959 steel Substances 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Landscapes
- Chemical Vapour Deposition (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、ダイス、プラグ、ロール、パンチ又は各種の
金型などの1耐摩耗工具部品、ドリル。DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to wear-resistant tool parts such as dies, plugs, rolls, punches or various molds, and drills.
タップ、エンドミル又はリーマなどの穴あけ工具、旋削
工具、プライス工具などの切削工具部品、ハサミ、カミ
ソリの刃又は切断刃などの各種工具部品、精密機械部品
及び原子炉用、宇宙開発用、半導体用、化学反応装置用
2医療機器用等の特殊用途部品に適用できる表面精度の
すぐれた被覆鉄基合金及びその製造方法に関するもので
ある。Drilling tools such as taps, end mills and reamers, cutting tool parts such as turning tools and price tools, various tool parts such as scissors, razor blades and cutting blades, precision machine parts and for nuclear reactors, space development, semiconductors, etc. The present invention relates to a coated iron-based alloy with excellent surface precision that can be applied to special purpose parts such as chemical reaction equipment, medical equipment, etc., and a method for manufacturing the same.
(従来の技術)
ステンレス、ダイス鋼又は高速度鋼等の鉄基合金の表面
に炭化チタン、炭窒化チタン又は炭窒酸化チタンの被覆
層を形成した被覆鉄基合金が実用化されている。鉄基合
金の表面に被覆層を形成する方法としては、大別すると
、化学蒸着法(CVD法)と物理蒸着法(PVD法)が
ある。(Prior Art) A coated iron-based alloy in which a coating layer of titanium carbide, titanium carbonitride, or titanium carbonitride oxide is formed on the surface of an iron-based alloy such as stainless steel, die steel, or high-speed steel has been put into practical use. Methods for forming a coating layer on the surface of an iron-based alloy can be broadly classified into chemical vapor deposition (CVD) and physical vapor deposition (PVD).
この内、後者による被覆鉄基合金は、低温で処理できる
けれども、耐摩耗工具部品又は穴あけ工具部品を含めた
切削工具部品等のように苛酷な条件で用いる場合は被覆
層が剥離し易いという問題がある。また、蒸着物の方向
性に関連し、複雑形状品の表面全体に、均一に被覆層を
形成するのが困難であるという問題がある。一方、前者
による被覆鉄基合金は、後者によるものよりも被膜のつ
きまわりも良好で、しかも高温で処理されることから被
覆層の耐剥離性がすぐれているけれども、鉄基合金と被
覆層との境界部において相互拡散が激しくなるために耐
剥離性にバラツキが生じるという問題がある。しかしな
がら、被覆層の耐剥離性は、PVD法による場合に比較
してすぐれているということから、CVD法による被覆
鉄基合金の安定化への期待が高まっている。Of these, the latter coated iron-based alloy can be processed at low temperatures, but the coating layer tends to peel off when used under harsh conditions such as wear-resistant tool parts or cutting tool parts including drilling tool parts. There is. Additionally, there is a problem in that it is difficult to uniformly form a coating layer over the entire surface of a complex-shaped product due to the directionality of the deposit. On the other hand, the former coated iron-based alloy has better coating coverage than the latter, and is treated at high temperatures, so the coating layer has better peeling resistance. There is a problem in that interdiffusion becomes intense at the boundary between the two, resulting in variations in peeling resistance. However, since the peeling resistance of the coating layer is superior to that obtained by the PVD method, there are increasing expectations for stabilization of the coated iron-based alloy by the CVD method.
(発明が解決しようとする問題点)
本発明者らは、CVD法により超硬合金の表面に炭化チ
タンの被覆層を直接形成させた場合は一応問題なく実用
化されているのに対し、鉄基合金の表面に炭化チタンの
被覆層を直接形成させた場合には以下のような問題があ
ることを確認した。(Problems to be Solved by the Invention) The present inventors discovered that, while direct formation of a coating layer of titanium carbide on the surface of cemented carbide using the CVD method has been put to practical use without any problems, It was confirmed that the following problems occur when a titanium carbide coating layer is directly formed on the surface of the base alloy.
鉄基合金の表面に炭化チタンの被覆層をCVD法により
直接形成させた場合には、被覆層の表面に凹凸が生じる
こと、この被覆層表面の凹凸が被覆層の剥離を誘発する
こと及び耐摩耗工具部品や切削工具部品として応用した
場合に被加工面が荒れてしまうという問題がある。また
、被覆層表面に凹凸があるために被覆鉄基合金をロール
のように鏡面状態で使用する場合には、被覆層表面を鏡
面にするのが困難であるという問題がある。When a coating layer of titanium carbide is directly formed on the surface of an iron-based alloy by the CVD method, unevenness occurs on the surface of the coating layer, and this unevenness on the surface of the coating layer induces peeling of the coating layer, and there are problems with resistance. When applied as wear tool parts or cutting tool parts, there is a problem in that the processed surface becomes rough. Further, since the surface of the coating layer has irregularities, when the coated iron-based alloy is used in a mirror-like state like a roll, there is a problem in that it is difficult to make the surface of the coating layer a mirror-like surface.
本発明は、と記のような問題点を解決したもので、具体
的には鉄基合金の表面にチタン化合物と鉄−チタンの金
属間化合物とでなる中間層と、チタン化合物でなる外層
とからなる被WI層を形成したもので、被覆層の密着性
、被覆層の耐剥離性及び外層の表面オ^度にすぐれた被
覆鉄基合金の提供を目的とするものである。The present invention solves the above problems. Specifically, the present invention has an intermediate layer made of a titanium compound and an iron-titanium intermetallic compound on the surface of an iron-based alloy, and an outer layer made of a titanium compound. The object of the present invention is to provide a coated iron-based alloy with excellent adhesion of the coating layer, peeling resistance of the coating layer, and surface roughness of the outer layer.
(問題点を解決するための手段)
本発明者らは、鉄基合金の表面に炭化チタンを被覆した
場合に生じる被覆層表面の凹凸の原因は、第1に、鉄基
合金中の鉄がCVD処理の初期に炭化チタンの被覆層中
へ拡散して鉄金属として存在すること、第2に、鉄基合
金と被覆層との界面近傍に局所的・に鉄の多量な場所が
生じ、この場所から炭化チタンの柱状晶が扇状に発達す
ることにあると確認したものである。そこで、被覆層中
に鉄を単独で存在させないようにすることを検討してい
た所、被覆層中に拡散した鉄をチタンとの金属間化合物
にすると被覆層の表面が平滑になるという知見を得たも
のである。この知見に基づいて本発明を完成するに至っ
たものである。(Means for Solving the Problems) The present inventors have discovered that the cause of the unevenness on the surface of the coating layer that occurs when titanium carbide is coated on the surface of an iron-based alloy is, firstly, that the iron in the iron-based alloy is At the beginning of the CVD process, it diffuses into the titanium carbide coating layer and exists as iron metal.Secondly, a large amount of iron locally occurs near the interface between the iron-based alloy and the coating layer. It was confirmed that this was due to the fact that columnar crystals of titanium carbide developed in a fan shape from the location. Therefore, we were considering preventing the presence of iron alone in the coating layer, and discovered that if the iron diffused into the coating layer was made into an intermetallic compound with titanium, the surface of the coating layer would become smooth. That's what I got. Based on this knowledge, we have completed the present invention.
すなわち、本発明の表面精度のすぐれた被覆鉄基合金は
、鉄基合金の基体と炭化チタン、炭窒化チタン、炭酸化
チタン、炭窒酸化チタン、窒化チタンの中の少なくとも
1種でなる外層との間に中間層を介在させてなる被覆鉄
基合金において、前記中間層は炭化チタン、炭窒化チタ
ン、炭酸化チタン、炭窒酸化チタンの中の少なくとも1
種のチタン化合物と鉄−チタンの金属間化合物とからな
ることを特徴とするものである。That is, the coated iron-based alloy of the present invention with excellent surface precision comprises a base of iron-based alloy, an outer layer made of at least one of titanium carbide, titanium carbonitride, titanium carbonate, titanium carbonitride oxide, and titanium nitride. In a coated iron-based alloy having an intermediate layer interposed therebetween, the intermediate layer comprises at least one of titanium carbide, titanium carbonitride, titanium carbonate, and titanium carbonitride oxide.
It is characterized by consisting of a seed titanium compound and an iron-titanium intermetallic compound.
本発明の表面精度のすぐれた被覆鉄基合金における中間
層は、例えばTicとFe2Ti。The intermediate layer in the coated iron-based alloy with excellent surface precision of the present invention is, for example, Tic and Fe2Ti.
TiCとFe2TiとFeTi。TiC, Fe2Ti and FeTi.
TiCとFeTi 。TiC and FeTi.
Ti(C,N)とFe2Ti。Ti(C,N) and Fe2Ti.
Ti(C,N)とFe2TiとFeTi 。Ti(C,N), Fe2Ti and FeTi.
Ti(C,N)とFeTi 。Ti(C,N) and FeTi.
Ti(C,N、O)とFe2Ti。Ti(C,N,O) and Fe2Ti.
Ti(C,N、O)とFe2TiとFeTi。Ti (C, N, O), Fe2Ti and FeTi.
Ti(C,N、O)とFeTi。Ti(C,N,O) and FeTi.
TicとTi(C,N)とFe2Tiなどを挙げること
ができる。ここに挙げた中間層中のチタン化合物及び外
層を形成するチタン化合物は、化学量論値又は非化学量
論値になっていてもよい、これらの中間層は、平均厚さ
2JLm以下である場合に表面精度のすぐれた被覆鉄基
合金が得られるもので、用途により異なるが中間層厚さ
は、特に平均厚さ0.05〜Iμm以下であると鉄基合
金と外層との耐剥離性にすぐれるので好ましいものであ
る。Examples include Tic, Ti(C,N), and Fe2Ti. The titanium compounds in the intermediate layer and the titanium compounds forming the outer layer mentioned here may be stoichiometric or non-stoichiometric, provided that these intermediate layers have an average thickness of 2 JLm or less. A coated iron-based alloy with excellent surface precision can be obtained.Although it varies depending on the application, an average thickness of 0.05 to Iμm or less improves the peeling resistance between the iron-based alloy and the outer layer. It is preferable because it is excellent.
本発明の表面精度のすぐれた被覆鉄基合金における中間
層と外層とでなる被覆層は、用途により異なるが、1〜
20μmの厚さからなり、特に2〜10.wmであると
耐摩耗性及び耐剥離性にすぐれることから著しい寿命向
上が達成できるものである。この被覆層中の外層は、少
なくとも1層で構成されるものである。また、外層の表
面に、更に周期律表4a、5a、6a族金属の炭化物、
窒化物、炭酸化物、窒酸化物、A旦の酸化物、窒化物、
Siの炭化物、窒化物及びこれらの相互固溶体、もしく
はダイヤモンド、立方晶窒化ホウ素などの少なくとも1
種の高硬質物質でなる最外層を積層することも好ましい
ことである。The coating layer consisting of the intermediate layer and the outer layer in the coated iron-based alloy with excellent surface precision of the present invention varies depending on the application, but
20 μm thick, especially 2 to 10 μm thick. If it is wm, it has excellent wear resistance and peeling resistance, so that a significant improvement in life can be achieved. The outer layer in this coating layer is composed of at least one layer. Further, on the surface of the outer layer, carbides of metals of groups 4a, 5a, and 6a of the periodic table,
Nitride, carbonate, nitride, oxide of A, nitride,
At least one of Si carbides, nitrides, mutual solid solutions thereof, diamond, cubic boron nitride, etc.
It is also preferable to laminate the outermost layer of a highly rigid material.
本発明の表面精度のすぐれた被覆鉄ノ、(合金を製造す
るには、基体の表面に鉄とチタン又は鉄−チタンの合金
をメッキ又はPVD法で被覆した後、CVD法により外
層を形成する雰囲気中での炭素ポテンシャルを高くして
800℃〜1100℃で中間層を形成し、次いで同一反
応容器内で炭素ポテンシャルを低くして外層を形成する
方法でも可能である。しかしながら、工程の簡素化及び
被覆鉄基合金の安定化から次の方法が特に好ましいもの
である。To produce the coated iron alloy (alloy) of the present invention with excellent surface precision, the surface of the substrate is coated with iron and titanium or an iron-titanium alloy by plating or PVD, and then an outer layer is formed by CVD. It is also possible to form an intermediate layer at 800°C to 1100°C by increasing the carbon potential in the atmosphere, and then forming an outer layer by lowering the carbon potential in the same reaction vessel.However, the process can be simplified. The following method is particularly preferred from the viewpoint of stabilization of the coated iron-based alloy.
すなわち、本発明の表面精度のすぐれた被覆鉄基合金の
製造方法は、反応容器内に設置された鉄基合金の基体を
800℃〜1100℃に保持し、前記反応容器内をハロ
ゲン化チタンと水素と炭化水素と、必要に応じて窒素、
アンモニア、ヒドラジン、一酸化炭素、二酸化炭素の中
の少なくとも1種とからなる雰囲気に保持して、前記基
体の表面に被覆層を形成させる被覆鉄基合金の製造方法
において、前記炭化水素/前記水素のガス体積比が17
1O以下で、かつ前記ハロゲン化チタン中のチタン元素
/前記炭化水素中の炭素元素の体積比が174以下にな
る雰囲気にして、前記基体の表面に炭化チタン、炭窒化
チタン、炭酸化チタン、炭窒酸化チタンの中の少なくと
も1種のチタン化合物と鉄−チタンの金属間化合物とで
なる中間層と、炭化チタン、炭窒化チタン、炭酸化チタ
ン、炭窒酸化チタン、窒化チタンの中の少なくとも1種
の外層とからなる被覆層を形成することを特徴とするも
のである。That is, in the method of manufacturing a coated iron-based alloy with excellent surface precision of the present invention, an iron-based alloy substrate placed in a reaction vessel is maintained at 800°C to 1100°C, and the inside of the reaction vessel is heated with titanium halide. Hydrogen and hydrocarbons and optionally nitrogen,
A method for producing a coated iron-based alloy comprising forming a coating layer on the surface of the substrate by maintaining the substrate in an atmosphere consisting of at least one of ammonia, hydrazine, carbon monoxide, and carbon dioxide, wherein the hydrocarbon/hydrogen gas volume ratio is 17
Titanium carbide, titanium carbonitride, titanium carbonate, carbon an intermediate layer consisting of at least one titanium compound among titanium nitride oxides and an intermetallic compound of iron-titanium; and at least one of titanium carbide, titanium carbonitride, titanium carbonate, titanium carbonitride oxide, and titanium nitride. It is characterized by forming a covering layer consisting of an outer layer of seeds.
本発明の表面精度のすぐれた被覆鉄基合金の製造方法に
おける炭化水素/水素のガス体積比と/\ロゲン化チタ
ン中のチタン元素/炭化水素中の炭素元素の体積比は、
反応容器内の炭素ポテンシャルに大きく影響しているも
ので、炭化チタンと鉄−チタンの金属間化合物とでなる
中間層を基体の表面に形成させる場合は、炭化水素/水
素のガス体積比を 1710〜5/10G、炭窒化チタ
ンと鉄−チタンの金属間化合物、炭酸化チタンと鉄−チ
タンの金属間化合物又は炭窒酸化チタンと鉄−チタンの
金属間化合物とでなる中間層を基体の表面に形成させる
場合は、炭化水素/水素のガス体積比を8/100〜1
/100にすると、特に被覆層の表面精度がすぐれるの
で好ましいことである。また、これらの中間層を基体の
表面に形成する場合は、ハロゲン化チタン中のチタン元
素/炭化水素中の炭素元素の体積比を175以下にする
と、特に基体と中間層との密着性及び被覆層の表面精度
にすぐれる°ことから好ましいことである。In the method of manufacturing a coated iron-based alloy with excellent surface precision of the present invention, the gas volume ratio of hydrocarbon/hydrogen and the volume ratio of titanium element in titanium rogenide/carbon element in hydrocarbon are as follows:
If an intermediate layer consisting of titanium carbide and an intermetallic compound of iron-titanium is to be formed on the surface of the substrate, which has a large influence on the carbon potential in the reaction vessel, the hydrocarbon/hydrogen gas volume ratio should be set to 1710. ~5/10G, an intermetallic compound of titanium carbonitride and iron-titanium, an intermetallic compound of titanium carbonate and iron-titanium, or an intermetallic compound of titanium carbonitride and iron-titanium is formed on the surface of the substrate. When forming a hydrocarbon/hydrogen gas volume ratio of 8/100 to 1
/100 is preferable because the surface precision of the coating layer is particularly excellent. In addition, when forming these intermediate layers on the surface of the substrate, it is recommended to keep the volume ratio of titanium element in titanium halide/carbon element in hydrocarbon to 175 or less, especially to improve the adhesion between the substrate and the intermediate layer and the coating. This is preferable because the surface accuracy of the layer is excellent.
さらに、反応容器内は、雰囲気ガス圧力によっても炭素
ポテンシャルが変動し、特に、350tart〜650
torrの減圧状態にすることが好ましいことである。Furthermore, the carbon potential inside the reaction vessel fluctuates depending on the atmospheric gas pressure, especially from 350 tart to 650 tart.
It is preferable to use a reduced pressure state of torr.
(作用)
本発明の表面精度のすぐれた被覆鉄基合金は、中間層が
基体と外層との密着性を高めるための媒介的役割を果た
すと共に、外層の表面を平滑にする作用をしているもの
である。また、本発明の表面精度のすぐれた被覆鉄基合
金の製造方法は、反応容器内の雰囲気ガス組成比が炭素
ポテンシャルの制御を容易にすると共に、基体の表面の
中間層を安定に形成する作用をしているものである。(Function) In the coated iron-based alloy with excellent surface precision of the present invention, the intermediate layer plays a mediating role in increasing the adhesion between the base and the outer layer, and also functions to smooth the surface of the outer layer. It is something. In addition, in the method of manufacturing a coated iron-based alloy with excellent surface precision according to the present invention, the atmospheric gas composition ratio in the reaction vessel facilitates control of the carbon potential and has the effect of stably forming an intermediate layer on the surface of the substrate. This is what we do.
(実施例)
実施例1
反応容器内に5KDII製の金型でなる基体を設置した
後、TiC又4 、CH4、H2を用いて、反応容器
内を体積比で Ti/C辷2/25 、 CH4/H2
# 1/25(7)雰囲気にし、圧力600torr、
温度1030℃で30分保持し、次いで、体積比でTi
/C辷2/25 、 CH4/)I2# 2/25
の雰囲気にし、保持時IHI I a o分の他は上述
と同様の条件により基体の表面に被覆層を形成させて本
発明品Aを得た。(Example) Example 1 After installing a substrate made of a mold made of 5KDII in a reaction vessel, the interior of the reaction vessel was filled with TiC, CH4, and H2 at a volume ratio of Ti/C 2/25, CH4/H2
# 1/25 (7) atmosphere, pressure 600 torr,
The temperature was kept at 1030°C for 30 minutes, and then the volume ratio of Ti
/C 2/25, CH4/)I2# 2/25
A product A of the present invention was obtained by forming a coating layer on the surface of the substrate under the same conditions as described above except for the IHI I ao content during holding.
比較として、体積比で Ti/C# 17150 、
CH4/H2#3150 の雰囲気にし、圧力10
0 torr 、保持時間210分の他は上述と同様
の条件により基体の表面に被覆層を形成させて比較量A
を得た。こうして得た本発明品Aと比較量Aとの表面を
仕−に−、げ(ラップ)加工し、Al2O3系セラミッ
クス粉末成形加工を行った。このときの、仕上げ加工に
要した作業時間、仕上げ後の表面寸法精度及び粉末成形
加工時の寿命時間を第1表に示した。For comparison, the volume ratio is Ti/C# 17150,
CH4/H2 #3150 atmosphere, pressure 10
A coating layer was formed on the surface of the substrate under the same conditions as above except that the temperature was 0 torr and the holding time was 210 minutes.
I got it. The surfaces of the product A of the present invention and the comparative product A thus obtained were subjected to a lapping process, and an Al2O3 ceramic powder molding process was performed. Table 1 shows the working time required for finishing, the surface dimensional accuracy after finishing, and the life time during powder molding.
第 1 表
本発明品A及び比較量Aの被覆層をX&1回析及び走査
型顕微鏡にて調べた所、本発明品Aの被覆層は、Fe2
TiとFeTiとTicの混在した中間層が約1μm厚
さとTiCの外層が約77zm厚さであった。比較量A
の被覆層は、約81LmのTiC層であった0本発明品
Aのx&!回折結果を第1図に示した。第1図中のFe
の回折線は基体の5KDIIによるものである。また1
本発明品の被覆層の組織を第2図に示した。Table 1 When the coating layers of the invention product A and the comparative amount A were examined using X&1 diffraction and a scanning microscope, it was found that the coating layer of the invention product A was Fe2
The intermediate layer containing a mixture of Ti, FeTi, and Tic had a thickness of about 1 μm, and the outer layer of TiC had a thickness of about 77 zm. Comparison amount A
The coating layer was a TiC layer of about 81 Lm x&! of Invention Product A. The diffraction results are shown in FIG. Fe in Figure 1
The diffraction line is due to 5KDII of the substrate. Also 1
FIG. 2 shows the structure of the coating layer of the product of the present invention.
実施例2
反応容器内に5KH9製のパンチでなる基体を設置した
後、TiC文a + C2H6+ H2を用いて、反
応容器内を体積比で Ti/C# 4/25 、 C2
H6/H2#1150 の雰囲気にし、圧力500
torr 。Example 2 After installing a substrate made of a punch made of 5KH9 in a reaction vessel, the interior of the reaction vessel was filled with Ti/C# 4/25, C2 in volume ratio using TiC pattern a + C2H6 + H2.
H6/H2#1150 atmosphere, pressure 500
torr.
温度1000℃で30分保持し8次いで1体積比で 〒
i/C= 4/25 、 C2H6/H2辷?/100
の雰囲気にし、保持時間150分の他は上述と同様の条
件により基体の表面に被覆層を形成させて本発明品Bを
得た。Hold at a temperature of 1000°C for 30 minutes, and then mix at a volume ratio of 8 and 1.
i/C=4/25, C2H6/H2? /100
A coating layer was formed on the surface of the substrate under the same conditions as described above except that the atmosphere was 150 minutes and the holding time was 150 minutes to obtain product B of the present invention.
比較として、体積比で Ti/C辷8/25 、 C2
H6/H2#1/8の雰囲気7圧力10 torr
、保持時間180分の他は上述と同様の条件により基体
の表面に被覆層を形成させて比較量Bを得た。For comparison, the volume ratio of Ti/C is 8/25, C2
H6/H2#1/8 atmosphere 7 pressure 10 torr
A comparative amount B was obtained by forming a coating layer on the surface of the substrate under the same conditions as described above except for a holding time of 180 minutes.
こうして得た本発明品Bと比較量Bを5US304製の
0.5m+*厚板の冷間打抜きに用いた所、本発明品B
は、比較量Bの約2倍の寿命であった・
本発明品B及び比較量Bの被WIMを実施例1での方法
と同様にして調べた所、本発明品Aの被覆層は、Fe2
TiとTiCの混在した中間層が約0.7μm厚さとT
iCの外層が約4μm厚さであった。比較量Bの被覆層
は、約5pmのT i 0層であった・
実施例3
SKH57製のダイスを基体とし1反応容器内の雰囲気
が Ti/C= 2/25 、 CHa/H2辷l/2
5 で、保持時間10分、その後反応容器内の雰囲気
がTi/C# 2/25 、 CHa/H2# 2/2
5 テ、保持時間80分の他は実施例1の本発明品A
と同様の条件により基体の表面に被覆層を形成させて本
発明品Cを得た。When the thus obtained product B of the present invention and comparative amount B were used for cold punching of a 0.5 m + * thick plate made of 5US304, product B of the present invention
The lifespan of the product A was approximately twice as long as that of the comparative amount B. When the WIM of the inventive product B and the comparative amount B were examined in the same manner as in Example 1, the coating layer of the inventive product A was found to be Fe2
The intermediate layer containing Ti and TiC has a thickness of approximately 0.7 μm and T
The outer layer of iC was approximately 4 μm thick. The coating layer of comparative amount B was a Ti 0 layer of about 5 pm.Example 3 A die made of SKH57 was used as a base, and the atmosphere in one reaction vessel was Ti/C=2/25, CHa/H2/L/ 2
5, the holding time was 10 minutes, and then the atmosphere in the reaction vessel was Ti/C# 2/25, CHa/H2# 2/2.
5 Te, invention product A of Example 1 except for holding time 80 minutes
A coating layer was formed on the surface of the substrate under the same conditions as described above to obtain product C of the present invention.
比較として、保持時間90分の他は実施例1の比較量A
と同様の条件により基体の表面に被覆層を形成させて比
較量Cを得た。For comparison, the comparative amount A of Example 1 was used except for the retention time of 90 minutes.
A comparative amount C was obtained by forming a coating layer on the surface of the substrate under the same conditions as described above.
この本発明品Cと比較量Cを仕上げ(ラップ)加工した
後、パーマロイ製のテープレコーダ部品の絞り加工に用
いた。このときの、仕上げ加工に要した作業時間、仕上
げ後の表面寸法精度及び絞り加工時の寿命迄の加工個数
を第2表に示した。After finishing (lapping) the product C of the present invention and the comparative product C, they were used for drawing of permalloy tape recorder parts. Table 2 shows the working time required for the finishing process, the surface dimensional accuracy after finishing, and the number of pieces processed until the life of the drawing process.
第 2 表
本発明品C及び比較量Cの被覆層を実施例1での方法と
同様にして調べた所1本発明品Cの被覆層は、Fe2T
iとFeTiとTiCc7)混在した中間層が約0.5
pm厚さとTiCの外層が約2.5μmであった。比較
量Cの被覆層は、約31mのTi0層であった。Table 2 The coating layers of the invention product C and the comparative amount C were examined in the same manner as in Example 1.1 The coating layer of the invention product C was Fe2T.
i, FeTi, and TiCc7) mixed intermediate layer is approximately 0.5
pm thickness and the outer layer of TiC was approximately 2.5 μm. The coating layer of comparative amount C was about 31 m of Ti0 layer.
実施例4
SUS44OC製のシーミングロールを基体として、他
は実施例3の本発明品Cと同様な条件で被覆層を形成し
た後、TiC文a、N2 、H2を用いて、従来と同様
の雰囲気にし、1000’C,450torr 、 6
0分保持にてTiNの最外層を形成して本発明品りを得
た。Example 4 After forming a coating layer using a seaming roll made of SUS44OC as a base under the same conditions as the invention product C of Example 3, a coating layer was formed using TiC material a, N2, and H2 in the same manner as before. Atmosphere: 1000'C, 450torr, 6
The outermost layer of TiN was formed by holding for 0 minutes to obtain a product of the present invention.
比較として、同様の基体に実施例3の比較量Cと同様の
条件で被覆層を形成させた後、さらに上述と同条件にて
TENの被覆層を形成して比較量りを得た。For comparison, a coating layer was formed on the same substrate under the same conditions as the comparative amount C of Example 3, and then a TEN coating layer was further formed under the same conditions as described above to obtain a comparative sample.
こうして得た本発明品りと比較量りを仕上げ加工した後
、缶胴と缶蓋との巻締めに使用した。このときの仕上げ
加工に要した作業時間、ノミ命名の巻締め缶数を第3表
に示した。After finishing the products of the present invention and comparison scales thus obtained, they were used for seaming the can bodies and can lids together. Table 3 shows the working time required for the finishing process and the number of cans sealed with a chisel.
以下余白
第 3 表
本発明品り及び比較量りの被覆層を実施例1での方法と
同様にして調べた所、本発明品りの被覆層は、実施例3
と同様の中間層と外層の他に約3μmのTiN外層が形
成されたものであった。比較量りの被覆層は、約3ルm
のTi0層と約3pmのTiN層が形成されたものであ
った。Table 3: The coating layer of the product of the present invention and the comparison weight were examined in the same manner as in Example 1, and the coating layer of the product of the present invention was found to be
In addition to the same intermediate layer and outer layer, a TiN outer layer of about 3 μm was formed. The comparative coating layer is approximately 3 m
A TiO layer of about 3 pm and a TiN layer of about 3 pm were formed.
実施例5
SKD61製の金型を基体とし、
TiC文a 、CH4、H2を用いて、第1段階での
雰囲気で保持時間を20分、第2段階での雰囲気で保持
時間を40分とし、その他の条件は、実施例1の本発明
品Aと同様の条件で被!!2層を形成した後、20va
i%N2と80voi%(T i 0文4 、CH4
、H2)を用いて、体積比で Ti/C# 1/10
、 CH4/H2辷?/+00の雰囲気で、圧力450
torr 、温度1000℃、保持時間30分で処
理し、次いでTiC見a 、NHa 、H?を用い
て従来と同様の雰囲気で、圧力400tarr。Example 5 Using a mold made of SKD61 as a base, using TiC pattern a, CH4, and H2, holding time was 20 minutes in the atmosphere in the first stage, holding time was 40 minutes in the atmosphere in the second stage, Other conditions were the same as those for product A of the present invention in Example 1! ! After forming two layers, 20va
i%N2 and 80voi% (T i 0 sentence 4, CH4
, H2) at a volume ratio of Ti/C# 1/10.
, CH4/H2? /+00 atmosphere, pressure 450
torr, a temperature of 1000°C, and a holding time of 30 minutes, and then TiC, NHa, and H? under the same atmosphere as before, at a pressure of 400 tarr.
温度800℃、保持時間30分で処理して本発明品Eを
得た。A product E of the present invention was obtained by processing at a temperature of 800° C. and a holding time of 30 minutes.
比較として、同様の基体に実施例1の比較量Aを作成し
た条件の内、保持時間60分の他は同条件で処理した後
、TiCfJ、a 、NH4、H2を用いて、圧力4
00 tarr 、温度800℃、保持時間30分で
処理して本発明品Eを得た。For comparison, a similar substrate was treated under the same conditions under which comparative amount A of Example 1 was prepared, except for a holding time of 60 minutes, and then a pressure of 4 was applied using TiCfJ,a, NH4, and H2.
00 tarr, temperature of 800° C., and holding time of 30 minutes to obtain product E of the present invention.
こうして得た本発明品Eと比較量Eを仕上げ加工した後
、プラスチ−7りの射出成形に使用した。The product E of the present invention thus obtained and the comparative amount E were subjected to finishing processing and then used for injection molding of Plasti-7.
このときの、仕上げ加工に要した作業時間、仕上げ後の
表面寸法精度、射出成形時の寿命迄の成形個数及び射出
成形加工後の被加工物の表面状態を調べて、その結果を
第4表に示した。At this time, we investigated the working time required for finishing, the surface dimensional accuracy after finishing, the number of molded pieces until the service life during injection molding, and the surface condition of the workpiece after injection molding, and the results are shown in Table 4. It was shown to.
以下余白
本発明品E及び比較量Eの被覆層を実施例1での方法と
同様にして調べた所、本発明品Eの被覆層は、Fe;+
TiとFeTiとTieの混在した中間層が約0.8B
m厚さと約0.8μm厚さのTicの外層と約1.0ル
m厚さの
Ti(C,N)外層と約1.0μm厚さのT i N外
層が形成されたものであった。比較量Eの被覆層は、約
2.5μmPXさ0’) T i C層と約1.0AL
m厚さのT i N層とが形成されたものであった。Below, the coating layers of the present invention product E and the comparative amount E were examined in the same manner as in Example 1, and it was found that the coating layer of the present invention product E was Fe;
The intermediate layer containing Ti, FeTi, and Tie is approximately 0.8B.
A Tic outer layer with a thickness of about 0.8 μm, a Ti(C,N) outer layer with a thickness of about 1.0 μm, and an outer layer of TiN with a thickness of about 1.0 μm were formed. . The comparative amount E of the coating layer is approximately 2.5 μm P
m thick TiN layer was formed.
(発明の効果)
本発明の表面精度のすぐれた被覆鉄基合金は、従来の被
覆鉄基合金に比較して、表面が平滑であるために鏡面仕
上げ加工して使用する場合には約40%〜10倍の加工
時間の短縮が可能で、そのときの加工面精には、約2.
5倍〜3倍もすぐれたものが得られるという効果がある
。また、本発明の被覆鉄基合金は、表面精度がすぐれて
いることは、中間層が基体と被覆層との密着性を高めて
いることから約1.4倍から25倍も寿命を向上させる
という効果がある。さらに、本発明の被覆鉄基合金によ
り加工された被加工部品の表面粗さは、従来の被覆鉄基
合金で加工された被加工部品よりもすぐれているという
効果がある。(Effects of the Invention) The coated iron-based alloy of the present invention has a smooth surface compared to conventional coated iron-based alloys, so when used after mirror finishing, the coated iron-based alloy has a surface precision of about 40% It is possible to shorten the machining time by ~10 times, and the machining surface accuracy at that time is approximately 2.
The effect is that a product that is 5 to 3 times better can be obtained. In addition, the coated iron-based alloy of the present invention has excellent surface precision, and the intermediate layer improves the adhesion between the base and the coating layer, which improves the service life by approximately 1.4 to 25 times. There is an effect. Furthermore, the surface roughness of workpieces machined using the coated iron-based alloy of the present invention is superior to that of workpieces machined using conventional coated iron-based alloys.
これらの他に、本発明の被覆鉄基合金の外層の表面に外
層との密着性にすぐれた、例えば窒化チタン、酸化アル
ミニウム、ダイヤモンド又は立方晶窒化ホウ素などの最
外層の被覆層を形成すると1本発明の被覆鉄基合金は、
さらに寿命向上及び用途拡大を計ることができるもので
産業上有用なものである。In addition to these, if an outermost coating layer, such as titanium nitride, aluminum oxide, diamond, or cubic boron nitride, which has excellent adhesion to the outer layer, is formed on the surface of the outer layer of the coated iron-based alloy of the present invention, The coated iron-based alloy of the present invention is
Furthermore, it is industrially useful because it can extend its lifespan and expand its uses.
第1図は、実施例1で得た本発明品Aの中間層のX線回
折結果である。
第2図は、実施例1で得た本発明品Aの被覆層の組織で
ある。
第2図中1が外層、2が中間層、3が基体を表わす。
特許出願人 東芝タンガロイ株式会社
同 冨士ダイス株式会社
第1 図
第2図
丁続補1EJF(方式)
1 、−1+件の表示
特願昭62−105733号
2、発明の名称
表面精度のすぐれた被覆鉄基合金及びその製造方法
コミ0補市をする者
・If (’lとの関係 特許出願人
神奈川県用崎市を区塚越1丁目7番地
昭和62年7月28日(発送日)
5、補!Eの対象
4、図面の簡単な説明
6、補正の内容
(1) 明細占21頁図面の簡単な説明の欄3行目〜
4行目の「被覆層の組織」を「被覆層の結晶の構造」と
補正する。
以上FIG. 1 shows the results of X-ray diffraction of the intermediate layer of product A of the present invention obtained in Example 1. FIG. 2 shows the structure of the coating layer of the product A of the present invention obtained in Example 1. In FIG. 2, 1 represents the outer layer, 2 represents the intermediate layer, and 3 represents the base body. Patent Applicant: Toshiba Tungaloy Co., Ltd. Fuji Dice Co., Ltd. 1 Figure 2 Figure 2 Supplement 1 EJF (method) 1 , -1+ indications Patent Application No. 105733/1982 2 Name of the invention Coating with excellent surface precision Iron-based alloys and their manufacturing method Persons/If ('l) Relationship with patent applicant 1-7 Tsukagoe, Yozaki City, Kanagawa Prefecture July 28, 1988 (shipment date) 5. Supplement! Subject 4 of E, Brief explanation of drawings 6, Contents of amendment (1) Page 21 of the specification, line 3 of the brief explanation of drawings column ~
The "structure of the covering layer" in the fourth line is corrected to "crystal structure of the covering layer". that's all
Claims (4)
酸化チタン、炭窒酸化チタン、窒化チタンの中の少なく
とも1種でなる外層との間に中間層を介在させてなる被
覆鉄基合金において、前記中間層は炭化チタン、炭窒化
チタン、炭酸化チタン、炭窒酸化チタンの中の少なくと
も1種のチタン化合物と鉄−チタン、金属間化合物とか
らなることを特徴とする表面精度のすぐれた被覆鉄基合
金。(1) A coated iron base formed by interposing an intermediate layer between a base of an iron-based alloy and an outer layer made of at least one of titanium carbide, titanium carbonitride, titanium carbonate, titanium carbonitride, and titanium nitride. In the alloy, the intermediate layer is made of at least one titanium compound selected from titanium carbide, titanium carbonitride, titanium carbonate, and titanium carbonitoxide, and iron-titanium, and an intermetallic compound. Excellent coated iron-based alloy.
特徴とする特許請求の範囲第1項記載の表面精度のすぐ
れた被覆鉄基合金。(2) The coated iron-based alloy with excellent surface precision according to claim 1, wherein the intermediate layer has an average thickness of 1 μm or less.
2Tiであることを特徴とする特許請求の範囲第1項記
載の表面精度のすぐれた被覆鉄基合金。(3) The above intermetallic compound is FeTi and/or Fe_
The coated iron-based alloy with excellent surface precision according to claim 1, characterized in that it is 2Ti.
℃〜1100℃に保持し、前記反応容器内をハロゲン化
チタンと水素と炭化水素と、必要に応じて窒素、アンモ
ニア、ヒドラジン、一酸化炭素、二酸化炭素の中の少な
くとも1種とからなる雰囲気に保持して、前記基体の表
面に被覆層を形成させる被覆鉄基合金の製造方法におい
て、前記炭化水素/前記水素のガス体積比が1/10以
下で、かつ前記ハロゲン化チタン中のチタン元素/前記
炭化水素中の炭素元素の体積比が1/4以下になる雰囲
気にして、前記基体の表面に炭化チタン、炭窒化チタン
、炭酸化チタン、炭窒酸化チタンの中の少なくとも1種
のチタン化合物と鉄−チタンの金属間化合物とでなる中
間層と、炭化チタン、炭酸化チタン、炭酸化チタン、炭
窒酸化チタン、窒化チタンの中の少なくとも1種の外層
とからなる被覆層を形成することを特徴とする表面精度
のすぐれた被覆鉄基合金の製造方法。(4) The iron-based alloy substrate installed in the reaction vessel
°C to 1100 °C, and the inside of the reaction vessel is made into an atmosphere consisting of titanium halide, hydrogen, hydrocarbons, and, if necessary, at least one of nitrogen, ammonia, hydrazine, carbon monoxide, and carbon dioxide. In the method for producing a coated iron-based alloy in which the hydrocarbon/hydrogen gas volume ratio is 1/10 or less, and the titanium element in the titanium halide/ At least one titanium compound selected from titanium carbide, titanium carbonitride, titanium carbonate, and titanium carbonitoxide is added to the surface of the substrate in an atmosphere in which the volume ratio of carbon element in the hydrocarbon is 1/4 or less. and an intermetallic compound of iron-titanium, and an outer layer of at least one of titanium carbide, titanium carbonate, titanium carbonate, titanium carbonitride, and titanium nitride. A method for manufacturing a coated iron-based alloy with excellent surface precision.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10573387A JPH089784B2 (en) | 1987-04-28 | 1987-04-28 | Coated iron-based alloy with excellent surface accuracy and method for producing the same |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10573387A JPH089784B2 (en) | 1987-04-28 | 1987-04-28 | Coated iron-based alloy with excellent surface accuracy and method for producing the same |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63270467A true JPS63270467A (en) | 1988-11-08 |
JPH089784B2 JPH089784B2 (en) | 1996-01-31 |
Family
ID=14415486
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10573387A Expired - Fee Related JPH089784B2 (en) | 1987-04-28 | 1987-04-28 | Coated iron-based alloy with excellent surface accuracy and method for producing the same |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH089784B2 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0397131A2 (en) * | 1989-05-09 | 1990-11-14 | Fujitsu Limited | Method of manufacturing a contact in semiconductor devices |
JPH03278431A (en) * | 1989-05-09 | 1991-12-10 | Fujitsu Ltd | Manufacture of semiconductor device |
JPH04154955A (en) * | 1990-10-17 | 1992-05-27 | Toshiba Corp | Spinning device |
JP2008518101A (en) * | 2004-10-27 | 2008-05-29 | ユニバーズィテート シュトゥットガルト | Corrosion prevention method for structural members made of heat-resistant steel |
GB2476004A (en) * | 2011-02-23 | 2011-06-08 | Portal Medical Ltd | Medicament dispenser with metal component having fluoride or carbide layer |
-
1987
- 1987-04-28 JP JP10573387A patent/JPH089784B2/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0397131A2 (en) * | 1989-05-09 | 1990-11-14 | Fujitsu Limited | Method of manufacturing a contact in semiconductor devices |
JPH03278431A (en) * | 1989-05-09 | 1991-12-10 | Fujitsu Ltd | Manufacture of semiconductor device |
JPH04154955A (en) * | 1990-10-17 | 1992-05-27 | Toshiba Corp | Spinning device |
JP2008518101A (en) * | 2004-10-27 | 2008-05-29 | ユニバーズィテート シュトゥットガルト | Corrosion prevention method for structural members made of heat-resistant steel |
GB2476004A (en) * | 2011-02-23 | 2011-06-08 | Portal Medical Ltd | Medicament dispenser with metal component having fluoride or carbide layer |
GB2476004B (en) * | 2011-02-23 | 2011-12-28 | Portal Medical Ltd | Medicament Dispenser Device |
Also Published As
Publication number | Publication date |
---|---|
JPH089784B2 (en) | 1996-01-31 |
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