JPH0365431B2 - - Google Patents

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Publication number
JPH0365431B2
JPH0365431B2 JP58163300A JP16330083A JPH0365431B2 JP H0365431 B2 JPH0365431 B2 JP H0365431B2 JP 58163300 A JP58163300 A JP 58163300A JP 16330083 A JP16330083 A JP 16330083A JP H0365431 B2 JPH0365431 B2 JP H0365431B2
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JP
Japan
Prior art keywords
layer
coating layer
base material
wear
nitride
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
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JP58163300A
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Japanese (ja)
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JPS6056061A (en
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Priority to JP16330083A priority Critical patent/JPS6056061A/en
Publication of JPS6056061A publication Critical patent/JPS6056061A/en
Publication of JPH0365431B2 publication Critical patent/JPH0365431B2/ja
Granted legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physical Vapour Deposition (AREA)
  • Chemical Vapour Deposition (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

〔発明の技術分野〕 本発明は基材とその表面を被覆する耐摩耗性の
被覆層とから成る耐摩耗部品に関し、更に詳しく
は、該被覆層の有用性を一層高度に発揮できるよ
うにし耐摩耗部品に関する。 〔発明の技術的背景とその問題点〕 コンプレツサーのブレードなど各種の摺動部品
の特性としては耐摩耗性が要求される。この要求
を満たすために、ステンレス鋼などで構成した基
材の表面に窒化処理、浸炭処理、ホウ化処理など
を施して表面の硬度を高めることが行なわれてき
た。しかしながら、この場合の表面硬化層はヴイ
ツカース硬さ(Hv)で500〜1000程度であり、必
ずしも充分な硬度とはいえず耐摩耗性の点で満足
すべき結果を与えることがなかつた。 そのため、最近では基材の表面に直接TiN、
TiC,SiCなどのセラミツクス材を数μmコーテ
イングして被覆層を形成することが行なわれてい
る。この場合には、形成されたセラミツクス被覆
層の硬度はHvで約2000と高いので耐摩耗性とい
う点では充分に満足のいくものである。 しかしながら、この場合、応々にして基材とセ
ラミツクス被覆層との熱膨張率が異なるため両者
間の密着性に難点が生じ剥離等の現象が起き易く
なる。また、被覆層の厚みは数μmと極めて薄
く、しかも基材は例えば鉄の場合Hvで約200と極
めて軟らかいので、被覆層に外力が印加されたと
き基材が該外力に抵抗し得ず結局は損壊等の現象
が起こり、耐摩耗性という点では極めて有用な被
覆層の効果が充分に発揮されないという問題があ
つた。 〔発明の目的〕 本発明は、上記した欠点を解消し、セラミツク
ス被覆層の効果を充分に発揮し得る耐摩耗部品の
提供を目的とする。 〔発明の概要〕 本発明者は上記目的を達成すべく鋭意研究を重
ねる中で、基材の表面に直接セラミツクス被覆層
を形成するのではなく、基材の表面に一旦、表面
硬化処理を施して該表面を硬化し、しかる後にこ
の硬化層の上にセラミツクス被覆層を形成すれ
ば、たとえ該被覆層に外力が印加されても、該硬
化層は硬いのでいわば軟かい基材本体に対する防
護壁として作用することにより、得られた耐摩耗
部品は損壊しないということを着想し、本発明の
耐摩耗部品を開発するに至つた。 すなわち本発明の耐摩耗部品は、鉄若しくは鉄
系合金、チタン若しくはチタン系合金又はアルミ
ニウム若しくはアルミニウム系合金のいずれかで
ある基材と、該基材の表面に窒化処理、浸炭処理
又はホウ化処理のいずれかの表面硬化処理を施し
て形成した硬化層と、該硬化層の表面に形成した
周期律表a族、a族、a族に属するいずれ
かの元素、ケイ素又はホウ素の窒化物、炭化物又
はホウ化物のいずれかの層又は複合層からなる被
覆層から構成される耐摩耗部品であつて、該被覆
層がプラズマ化学的蒸着方法(PCVD法)により
形成されたものであることを特徴とする。 まず、基材としては、鉄(Fe)若しくはステ
ンレススチールなどのFe系合金、チタン(Ti)
若しくはTi−6Al−4VなどのTi系合金、アルミ
ニウム(Al)若しくはAl−Cu系、Al−Mg系な
どのAl系合金である。これらの材質のうち、Fe
若しくはFe系合金はその表面への硬化層形成が
容易なので特に好ましい。 上記した基材の表面には表面硬化処理が施され
て所定厚みの硬化層が形成される。 表面硬化処理としては、表面硬化法として常用
されている窒化処理、浸炭処理、ホウ化処理のい
ずれかを適宜に選定して行なう。このとき、どの
処理方法を採択するかということは、基材の種類
(表面硬化処理が可能か否か)、後刻に形成する被
覆層の種類(得られた硬化層の上に被覆層を密着
して形成できるのか否か)に関係する問題や、ま
た、得られるであろう硬化層は硬くかつその熱膨
張係数が基材と被覆層のそれの中間の値になるの
か否かに関する問題、などを考慮して決めればよ
い。とくに、窒化処理の場合、得られる硬化層の
硬度は浸炭処理、ホウ化処理の場合よりも幾分小
さいが、処理時の温度は500〜600℃(浸炭処理の
場合約900℃、ホウ化処理の場合約1000℃)と低
く処理時におけるエネルギー効率が大であるの
で、好ましい。硬化層の厚みは、通常、表面から
50〜200μm程度であればよい。 なお、基材としてFe若しくはFe系合金を用い
たとき、窒化処理時、硬化層の表面には、硬くて
脆いFe2〜3N相(ε相)が選択的に形成されるの
で、次のセラミツクス被覆層形成に先立つてこの
相を研磨、研削のような方法で除去することある
いは体積率を減少させることが好ましい。 この硬化層の上にセラミツクス被覆層が形成さ
れる。用いるセラミツクスとしては、周規律表
a族、Va族、a族に属するいずれか1種以上
の元素又はSi若しくはBの窒化物、炭化物、ホウ
化物のいずれか1種以上である。この場合、セラ
ミツクスとしては、硬化層が窒化処理による層で
あれば窒化物を、硬化層が浸炭処理による層であ
れば炭化物を、硬化層がホウ化処理による層であ
ればホウ化物をそれぞれ用いることが好ましい。 窒化物としては、例えば、窒化チタン
(TiN)、窒化ジルコニウム(ZrN)、窒化ハフニ
ウム(HfN)、窒化バナジウム(VN)、窒化ニオ
ブ(NbN)、窒化タンタル(TaN)、窒化クロム
(CrN,Cr2N)、窒化モリブデン(Mo2N,
MoN)、窒化タングステン(W2N,WN2
W2N3)、窒化シリコン(Si3N4)、窒化ボロン
(BN)があげられ;炭化物としては、炭化チタ
ン(TiC)、炭化ジルコニウム(ZrC)、炭化ハフ
ニウム(HfC)、炭化バナジウム(VC)、炭化ニ
オブ(NbC)、炭化タンタル(TaC)、炭化クロ
ム(Cr3N2,Cr7C3,Cr23C6)、炭化モリブデン
(Mo2C,MoC)、炭化タングステン(W2C,
WC)、炭化シリコン(SiC)、炭化ボロン(B4C)
があげられ;ホウ化物としては、ホウ化チタン
(TiB2)、ホウ化ジルコニウム(ZrB2)、ホウ化ハ
フニウム(HfB2)、ホウ化バナジウム(VB2)ホ
ウ化ニオブ(NbB,Nb3B4,NbB2)、ホウ化タ
ンタル(Ta2B,TaB,Ta3B4)ホウ化クロム
(Cr3B2,CrB)、ホウ化モリブデン(Mo2B,
MoB,Mo2B5)、ホウ化タングステン(W2B,
WB,W2B5)があげられる。これらセラミツク
スのうち、被覆層が比較的容易に形成できる。入
手し易すいなどの点からして、窒化物又は炭化物
は好ましい。とくにTiN,TiC,SiCが好ましい。 これらの被覆層の形成は、プラズマ化学的蒸着
法(PCVD法)を適用して行う。PCVD法は、基
材を陰極とし、金属ハロゲン化物の蒸気ガスと
N2又はN2+H2の低圧(数Torr,400〜600℃)
の雰囲気中でグロー放電を起こし、基材表面を被
覆する方法である。かかるPCVD法は、耐摩耗性
に優れた被覆層が得られること、被覆層と硬化層
との密着性が良好であること、成膜操作も比較的
簡単であること、などの点から優れている。 被覆層の厚みは任意であるが、あまり厚くする
と硬化層との間で熱応力を発生して剥離し易すく
なるので、通常は2μm程度である。 〔発明の実施例〕 鉄系合金としてSLS304,SCM1,S45C,
SACM1を選び、チタン系合金としてTi−3Al−
2.5V,Ti−6Al−4Vを選び、アルミニウム系合
金としてA5083、A5052を選んだ。各試料の形状
はフアレツクス試験用の丸棒であつた。 角試片に適宜に下記する条件の角表面硬化処理
を施して硬化層を形成した。硬化層の厚み約50〜
200μm。 窒化処理:N2とH2の容積混合比が1:3で全ガ
ス圧が2Torrの雰囲気中に試片を入れ、これを
570℃で2時間イオン窒化処理した。 浸炭処理:ガス圧3Torrのメタンガス中に試片を
置き、これを950℃で1時間イオン浸炭処理し
た。 ホウ化処理:ボロン、フエロボロン、アルミニウ
ム及び塩化アンモニウムの混合粉末中に試片を
埋設したのち、全体を1000℃で3時間加熱処理
した。 形成された各硬化層のHvを測定し、しかる後、
その上に表に示したような条件のPCVD法を適用
して各被覆層をそれぞれ形成しそれらのHvを測
定した。被覆層の厚みはいずれも2μmであつた。 比較のために、基材の表面に表面硬化処理を施
さず基材の表面に直接同一の製造条件で各被覆層
を形成した部品を製造した。 得られた各部品につき、その耐摩耗性をフアレ
ツクス試験機を用いて調べて評価を下した。ま
た、硬化層と被覆層との密置性に関しては、部品
を200〜300℃に加熱して室温に急冷するという熱
サイクル操作を5回反復し、そのときの被覆層の
剥離の有無又はクラツク発生の有無を観察して評
価した。密着性良好を○印、不可を×印、その中
間を△印で示した。
[Technical Field of the Invention] The present invention relates to a wear-resistant part consisting of a base material and a wear-resistant coating layer covering the surface of the base material, and more specifically, to a wear-resistant part that enables the coating layer to exhibit its usefulness to a higher degree. Concerning wear parts. [Technical background of the invention and its problems] Abrasion resistance is required as a characteristic of various sliding parts such as compressor blades. In order to meet this requirement, the surface of a base material made of stainless steel or the like has been subjected to nitriding, carburizing, boriding, etc. to increase the hardness of the surface. However, the hardened surface layer in this case had a Witzkers hardness (Hv) of about 500 to 1000, which was not necessarily sufficient hardness and did not provide satisfactory results in terms of wear resistance. Therefore, recently, TiN is applied directly to the surface of the base material.
A coating layer is formed by coating a ceramic material such as TiC or SiC with a thickness of several micrometers. In this case, the hardness of the ceramic coating layer formed is as high as about 2000 Hv, so it is fully satisfactory in terms of wear resistance. However, in this case, since the thermal expansion coefficients of the base material and the ceramic coating layer differ depending on the case, there is a problem in the adhesion between the two, and phenomena such as peeling are likely to occur. In addition, the thickness of the coating layer is extremely thin, a few μm, and the base material is extremely soft, for example, with Hv of about 200 in the case of iron, so when an external force is applied to the coating layer, the base material cannot resist the external force and eventually However, there was a problem in that phenomena such as breakage occurred, and the coating layer, which is extremely useful in terms of wear resistance, was not sufficiently effective. [Object of the Invention] The object of the present invention is to provide a wear-resistant part that can eliminate the above-mentioned drawbacks and fully exhibit the effects of the ceramic coating layer. [Summary of the Invention] In the course of intensive research to achieve the above object, the inventor of the present invention did not directly form a ceramic coating layer on the surface of the base material, but instead applied a surface hardening treatment to the surface of the base material. If the surface is hardened and then a ceramic coating layer is formed on this hardened layer, even if an external force is applied to the coating layer, the hardened layer will be hard and will act as a protective wall against the soft base material body. The inventors came up with the idea that the wear-resistant parts obtained would not be damaged by acting as an anti-wear component, and developed the wear-resistant parts of the present invention. That is, the wear-resistant parts of the present invention include a base material made of iron or an iron-based alloy, titanium or a titanium-based alloy, or aluminum or an aluminum-based alloy, and a surface of the base material that is nitrided, carburized, or borided. A hardened layer formed by performing any of the surface hardening treatments, and a nitride or carbide of any element belonging to group a, group a, group a of the periodic table, silicon or boron formed on the surface of the hardened layer. or a wear-resistant part comprising a coating layer consisting of any layer or composite layer of a boride, characterized in that the coating layer is formed by a plasma chemical vapor deposition method (PCVD method). do. First, the base material is iron (Fe), Fe-based alloys such as stainless steel, titanium (Ti), etc.
Alternatively, it is a Ti-based alloy such as Ti-6Al-4V, aluminum (Al), or an Al-based alloy such as Al-Cu-based or Al-Mg-based. Among these materials, Fe
Alternatively, Fe-based alloys are particularly preferred because they allow easy formation of a hardened layer on their surfaces. A surface hardening treatment is performed on the surface of the base material described above to form a hardened layer of a predetermined thickness. As the surface hardening treatment, any one of nitriding treatment, carburizing treatment, and boriding treatment, which are commonly used as surface hardening methods, is appropriately selected and carried out. At this time, which treatment method to adopt depends on the type of base material (whether surface hardening treatment is possible or not), the type of coating layer to be formed later (the coating layer is tightly adhered to the cured layer, etc.) and whether the resulting cured layer will be hard and have a coefficient of thermal expansion intermediate between those of the base material and the coating layer. You can decide by taking these things into consideration. In particular, in the case of nitriding, the hardness of the hardened layer obtained is somewhat lower than that of carburizing and boriding, but the temperature during treatment is 500 to 600°C (approximately 900°C in case of carburizing, It is preferable because it is low (approximately 1000°C) and has high energy efficiency during processing. The thickness of the hardened layer is usually from the surface to
It may be about 50 to 200 μm. Note that when Fe or Fe-based alloys are used as the base material, a hard and brittle Fe 2-3 N phase (ε phase) is selectively formed on the surface of the hardened layer during nitriding. It is preferable to remove the lever phase by a method such as polishing or grinding or to reduce the volume fraction prior to forming the ceramic coating layer. A ceramic coating layer is formed on this hardened layer. The ceramic used is any one or more elements belonging to group a, group Va, or group a of the periodic table, or one or more of nitrides, carbides, and borides of Si or B. In this case, the ceramic used is nitride if the hardened layer is a nitrided layer, carbide if the hardened layer is carburized, and boride if the hardened layer is a borided layer. It is preferable. Examples of nitrides include titanium nitride (TiN), zirconium nitride (ZrN), hafnium nitride (HfN), vanadium nitride (VN), niobium nitride (NbN), tantalum nitride (TaN), and chromium nitride (CrN, Cr2 ). N), molybdenum nitride (Mo 2 N,
MoN), tungsten nitride (W 2 N, WN 2 ,
Examples of carbides include titanium carbide ( TiC ), zirconium carbide (ZrC) , hafnium carbide (HfC) , and vanadium carbide ( VC). ), niobium carbide (NbC), tantalum carbide (TaC), chromium carbide (Cr 3 N 2 , Cr 7 C 3 , Cr 23 C 6 ), molybdenum carbide (Mo 2 C, MoC), tungsten carbide (W 2 C,
WC), silicon carbide (SiC), boron carbide (B 4 C)
Examples of borides include titanium boride (TiB 2 ), zirconium boride (ZrB 2 ), hafnium boride (HfB 2 ), vanadium boride (VB 2 ), niobium boride (NbB, Nb 3 B 4 ) , NbB 2 ), tantalum boride (Ta 2 B, TaB, Ta 3 B 4 ), chromium boride (Cr 3 B 2 , CrB), molybdenum boride (Mo 2 B,
MoB, Mo 2 B 5 ), tungsten boride (W 2 B,
WB, W 2 B 5 ). Of these ceramics, a coating layer can be formed relatively easily. Nitride or carbide is preferable from the viewpoint of easy availability. Particularly preferred are TiN, TiC, and SiC. These coating layers are formed by applying plasma chemical vapor deposition (PCVD). In the PCVD method, the base material is used as a cathode and metal halide vapor gas is used as the cathode.
Low pressure of N 2 or N 2 + H 2 (several Torr, 400-600℃)
In this method, glow discharge is generated in an atmosphere of 100% to coat the surface of a base material. This PCVD method has advantages in that it provides a coating layer with excellent abrasion resistance, has good adhesion between the coating layer and the hardened layer, and is relatively easy to form a film. There is. The thickness of the coating layer is arbitrary, but if it is too thick, thermal stress will be generated between the coating layer and the cured layer, making it easy to peel off, so it is usually about 2 μm. [Embodiment of the invention] As iron-based alloys, SLS304, SCM1, S45C,
Select SACM1 and use Ti−3Al− as the titanium alloy.
2.5V, Ti-6Al-4V were selected, and A5083 and A5052 were selected as aluminum alloys. The shape of each sample was a round bar for the Farex test. The corner specimen was subjected to corner surface hardening treatment under the conditions described below to form a hardened layer. Hardened layer thickness: approx. 50~
200μm. Nitriding treatment: A specimen is placed in an atmosphere with a volumetric mixing ratio of N 2 and H 2 of 1:3 and a total gas pressure of 2 Torr.
Ion nitriding was performed at 570°C for 2 hours. Carburizing treatment: The specimen was placed in methane gas at a gas pressure of 3 Torr, and was subjected to ion carburization treatment at 950°C for 1 hour. Boring treatment: After embedding the specimen in a mixed powder of boron, ferroboron, aluminum, and ammonium chloride, the entire specimen was heat-treated at 1000° C. for 3 hours. Measure the Hv of each cured layer formed, and then
Each coating layer was formed thereon by applying the PCVD method under the conditions shown in the table, and their Hv was measured. The thickness of each coating layer was 2 μm. For comparison, parts were manufactured in which each coating layer was formed directly on the surface of the base material under the same manufacturing conditions without subjecting the surface of the base material to surface hardening treatment. The wear resistance of each of the obtained parts was examined and evaluated using a Farex tester. Regarding the adhesion between the cured layer and the coating layer, we repeated a thermal cycle operation of heating the part to 200 to 300°C and rapidly cooling it to room temperature five times, and checked whether or not the coating layer peeled off or cracked. The presence or absence of occurrence was observed and evaluated. Good adhesion is indicated by ◯, poor adhesion is indicated by ×, and the middle is indicated by △.

【表】【table】

【表】 さらに、比較のために、基材の表面に前記
PCVD法と同様の表面硬化処理を施し、次表の条
件のPVD法(比較例19〜23)およびCVD法(比
較例24,25)を用いて各被覆層を形成した部品を
製造した。 得られた各部品につき、前記と同様の評価を行
つた。 得られた各部品において、PVD法を用いた比
較例19〜23は品位にバラツキを生じており、ま
た、CVD法を用いた比較例24および25は被覆時
の加熱により基材が軟化した部品としての耐摩耗
性は不十分であり、実用に使用することはできな
かつた。
[Table] Furthermore, for comparison, the above-mentioned
A surface hardening treatment similar to the PCVD method was performed, and parts were manufactured in which each coating layer was formed using the PVD method (Comparative Examples 19 to 23) and the CVD method (Comparative Examples 24 and 25) under the conditions shown in the following table. Each of the obtained parts was evaluated in the same manner as described above. Among the parts obtained, Comparative Examples 19 to 23 using the PVD method had variations in quality, and Comparative Examples 24 and 25 using the CVD method had parts whose base material had softened due to heating during coating. Its wear resistance was insufficient, and it could not be used for practical purposes.

【表】【table】

〔発明の効果〕〔Effect of the invention〕

表から明らかなように、本発明の耐摩耗部品
は、基材に直接セラミツクス被覆層を形成する従
来のものに比べて、基材との密着性に優れると同
時に基材表面の硬化層が硬く、薄い被覆層に外力
が加わつた場合でも、被覆層が陥没したりするこ
とがなく、被覆層の耐摩耗性が有効に発揮される
ので、その使用寿命が長くなるばかりではなく使
用時における信頼性も高まつて有用である。
As is clear from the table, the wear-resistant parts of the present invention have superior adhesion to the base material, and at the same time have a hard hardened layer on the surface of the base material, compared to conventional products in which a ceramic coating layer is directly formed on the base material. Even if external force is applied to the thin coating layer, the coating layer will not cave in and the wear resistance of the coating layer will be effectively demonstrated, which not only extends its service life but also increases reliability during use. It is also useful because of its increased functionality.

Claims (1)

【特許請求の範囲】 1 鉄若しくは鉄系合金、チタン若しくはチタン
系合金又はアルミニウム若しくはアルミニウム系
合金のいずれかである基材と、該基材の表面に窒
化処理、浸炭処理又はホウ化処理のいずれかの表
面硬化処理を施して形成した硬化層と、該硬化層
の表面に形成した周期律表a族、a族、a
族に属するいずれかの元素、ケイ素又はホウ素の
窒化物、炭化物又はホウ化物のいずれかの層又は
複合層からなる被覆層から構成される耐摩耗部品
であつて、該被覆層がプラズマ化学的蒸着法
(PCVD法)により形成されたものであることを
特徴とする耐摩耗部品。 2 該基材がステンレス鋼であり、該硬化層が窒
化鉄を主成分とする層であり、かつ、該被覆層が
窒化チタン層である特許請求の範囲第1項記載の
耐摩耗部品。
[Claims] 1. A base material made of iron or an iron-based alloy, titanium or a titanium-based alloy, or aluminum or an aluminum-based alloy, and a surface of the base material subjected to any of nitriding, carburizing, or boriding. A hardened layer formed by performing the above surface hardening treatment, and a group a, group a, a of the periodic table formed on the surface of the hardened layer.
A wear-resistant part comprising a coating layer consisting of a layer or a composite layer of a nitride, carbide or boride of any element belonging to the Group 1, silicon or boron, the coating layer being formed by plasma chemical vapor deposition. A wear-resistant part characterized by being formed by a method (PCVD method). 2. The wear-resistant component according to claim 1, wherein the base material is stainless steel, the hardened layer is a layer containing iron nitride as a main component, and the coating layer is a titanium nitride layer.
JP16330083A 1983-09-07 1983-09-07 Wear resistant parts Granted JPS6056061A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16330083A JPS6056061A (en) 1983-09-07 1983-09-07 Wear resistant parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16330083A JPS6056061A (en) 1983-09-07 1983-09-07 Wear resistant parts

Publications (2)

Publication Number Publication Date
JPS6056061A JPS6056061A (en) 1985-04-01
JPH0365431B2 true JPH0365431B2 (en) 1991-10-11

Family

ID=15771203

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16330083A Granted JPS6056061A (en) 1983-09-07 1983-09-07 Wear resistant parts

Country Status (1)

Country Link
JP (1) JPS6056061A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61272381A (en) * 1985-05-27 1986-12-02 Kanai Hiroyuki Lightweight traveler
KR890002162B1 (en) * 1985-11-28 1989-06-21 가부시키가이샤 도시바 Sliding members coated ceramic and a method for manufacture thereof
US5300951A (en) * 1985-11-28 1994-04-05 Kabushiki Kaisha Toshiba Member coated with ceramic material and method of manufacturing the same
JPS62218667A (en) * 1986-03-20 1987-09-26 Mitsubishi Heavy Ind Ltd Piston of hydraulic pump or motor
JPH0753908B2 (en) * 1986-03-20 1995-06-07 株式会社東芝 High-speed sliding member manufacturing method
US4904528A (en) * 1987-12-24 1990-02-27 United Technologies Corporation Coated gas turbine engine compressor components
JPH02134468A (en) * 1988-11-11 1990-05-23 Teikoku Piston Ring Co Ltd Piston ring
JPH02134467A (en) * 1988-11-11 1990-05-23 Teikoku Piston Ring Co Ltd Piston ring
JPH03247766A (en) * 1990-02-26 1991-11-05 Limes:Kk Formation of thin film by plasma cvd method
JP3341846B2 (en) * 1991-04-04 2002-11-05 住友電気工業株式会社 Ion nitriding-ceramic coating continuous treatment method
JP3314812B2 (en) * 1991-04-24 2002-08-19 住友電気工業株式会社 Ion nitriding method of metal surface using glow discharge
US5272015A (en) * 1991-12-19 1993-12-21 General Motors Corporation Wear resistant hyper-eutectic aluminum-silicon alloys having surface implanted wear resistant particles
US5518820A (en) * 1992-06-16 1996-05-21 General Electric Company Case-hardened titanium aluminide bearing
JPH0740529Y2 (en) * 1993-04-27 1995-09-20 金井 宏之 Lightweight traveler
JP2016027296A (en) * 2014-07-02 2016-02-18 旭硝子株式会社 Heat cycle system
EP3199821B1 (en) 2014-12-25 2023-08-30 IHI Corporation Compressor blade for engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5915984B2 (en) * 1974-11-21 1984-04-12 セイコーエプソン株式会社 Exterior parts for watches
JPS5179644A (en) * 1974-12-16 1976-07-12 Suwa Seikosha Kk TOKEI YOGA ISOBUHIN

Also Published As

Publication number Publication date
JPS6056061A (en) 1985-04-01

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