JPS58209554A - Multiple coating material and its manufacture - Google Patents

Multiple coating material and its manufacture

Info

Publication number
JPS58209554A
JPS58209554A JP9279182A JP9279182A JPS58209554A JP S58209554 A JPS58209554 A JP S58209554A JP 9279182 A JP9279182 A JP 9279182A JP 9279182 A JP9279182 A JP 9279182A JP S58209554 A JPS58209554 A JP S58209554A
Authority
JP
Japan
Prior art keywords
coated
coating
thickness
wear
tin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP9279182A
Other languages
Japanese (ja)
Inventor
健 宮崎
裕介 井寄
紀雄 高橋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Proterial Ltd
Original Assignee
Hitachi Metals Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Metals Ltd filed Critical Hitachi Metals Ltd
Priority to JP9279182A priority Critical patent/JPS58209554A/en
Publication of JPS58209554A publication Critical patent/JPS58209554A/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明は硬質物質を被覆した材料、特に耐摩耗性、耐欠
損性に有効な多重被覆の施された材料およびイの製造法
に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a material coated with a hard substance, particularly a multi-coated material effective in wear resistance and chipping resistance, and a method for producing the same.

WCC超超硬合金TiC基ザーメット、およびTiN褪
サーすッ1〜に硬質物質を被覆して耐摩耗性を向上させ
ることが従来より行なわれてきた。
Conventionally, WCC cemented carbide TiC-based cermets and TiN abrasive cermets have been coated with hard substances to improve their wear resistance.

しかし耐摩耗性といっても、摩耗は、フランク部にみら
れるアブレッシブ摩耗、クレータ一部にみられる被剛材
との化学反応に基づく摩耗−1および境界摩耗でみられ
る主として酸化摩耗の3つの19耗に大別され、アブレ
ンジブな摩耗には硬さの高いもの、クレータ−摩耗には
化学的安定性が大さいもの、境界摩耗には耐酸化性とと
もに熱伝導F1の高いもの、などが有効であることが知
られている。
However, although it is called wear resistance, there are three types of wear: abrasive wear seen on the flank, wear caused by chemical reaction with the rigid material seen in some parts of the crater, and oxidative wear seen mainly as boundary wear. Materials with high hardness are effective for abrasive wear, materials with high chemical stability are effective for crater wear, and materials with high oxidation resistance and thermal conductivity F1 are effective for boundary wear. It is known that

このため従来から、炭化物、窒化物等の単一層を被覆す
るかわりに、 ■内層と外層の2層、あるいは内層、中間層、外層の3
層にそれぞれ・異なる性質をもった硬質物質を被覆する
方法。
For this reason, conventionally, instead of coating with a single layer of carbide, nitride, etc.,
A method in which each layer is coated with a hard material that has different properties.

■異なった性質を有する2〜3種の硬質物質の固溶物質
、例えば炭窒化物を被覆する方法等が耐摩耗性の改善方
法としで取られてさた。
(2) A method of coating a solid solution of two to three types of hard substances having different properties, such as carbonitride, has been used as a method of improving wear resistance.

しかし、上記■の場合には当然のことながら、例えば、
外層はフランク部での耐摩耗性は良好だがクレータ一部
の耐摩耗性が劣化する、等の現象が生じるため、飛貿的
な耐摩耗性向上は望めない。
However, in the case of ■ above, of course, for example,
Although the outer layer has good abrasion resistance at the flank part, phenomena such as deterioration in abrasion resistance at a part of the crater occur, so no improvement in abrasion resistance can be expected.

また、熱膨張率の異なる異種物質をかなりの厚みに被覆
するために、熱の変動に弱く切削時に欠損しやすい、と
いう欠点はまぬがれない。
In addition, since it is coated with a considerable thickness of different materials with different coefficients of thermal expansion, it is unavoidable that it is susceptible to thermal fluctuations and is prone to breakage during cutting.

また上記■の場合には、一般に異種砂質物質の固溶体は
、硬質物質のイれぞれの特長が助長されるよりはむしろ
欠点が助長される傾向がある、という問題点がある。
Furthermore, in the case of (2) above, there is a problem in that solid solutions of different types of sandy materials generally tend to enhance the disadvantages of the hard materials rather than promoting their respective characteristics.

従って上記■または■の方法は、共に有効な改善方法で
あるとはいえなかった。
Therefore, neither method (1) or (2) above could be said to be an effective improvement method.

本発明は上記従来技術の欠点を改良し、耐摩耗耐欠損性
に優れた新規なコーアイング工具を提供することを目的
とする。
The object of the present invention is to improve the above-mentioned drawbacks of the prior art and provide a new coring tool with excellent wear resistance and chipping resistance.

本発明はW C早起硬合金、TiC基サーメット、また
は”丁IN基す−メツ[・の表面に、TiNおよび1゛
IB よりなる被覆層が、単層の厚さ1μm以上、好ま
しくは0.5μm未満で合計2〜15μmの厚さにTi
 N、Ti B2を交互に少くとも6層成[、望ましく
は20層層成多重被覆したことを特徴とり・るbのであ
る。
The present invention is characterized in that a coating layer made of TiN and 1"IB is formed on the surface of a WC early-setting hard alloy, a TiC-based cermet, or a "TIN-based cermet" with a single layer thickness of 1 μm or more, preferably 0.1 μm or more. Ti to a total thickness of less than 5 μm and 2 to 15 μm
It is characterized by being coated with at least 6 layers, preferably 20 layers, of N, Ti and B2 alternately.

本発明による材料は、単層の厚さが1μm以下、好まし
くは0.5μm未満であるので、熱膨張係数の大きいT
iNの欠点をカバーすることが可能となり、究極的に被
覆材料層間の歪が均一に分散して応力集中を排除し、耐
熱衝撃性を高めることがてきる。また、TiB2は硬さ
が高くかつ熱伝導性に優れるため、耐フランク摩耗性の
みならず耐境i摩耗性をも著しく改説する。しかし、T
iB2は鉄系合金との親和性が大きいため、鋼ヴ鋳鉄等
庖切削した場合、単独ではクレータ−摩耗が進行しやす
い傾向にあるが、本発明においては、薄層を多重被覆し
ているので、この欠点は回避できる。
The material according to the invention has a monolayer thickness of less than 1 μm, preferably less than 0.5 μm, so that T
It becomes possible to cover the drawbacks of iN, and ultimately the strain between the coating material layers is uniformly distributed, stress concentration is eliminated, and thermal shock resistance is improved. Furthermore, since TiB2 has high hardness and excellent thermal conductivity, it significantly improves not only flank wear resistance but also boundary wear resistance. However, T
iB2 has a high affinity with iron-based alloys, so when cutting steel or cast iron, it tends to cause crater wear when used alone, but in the present invention, it is coated with multiple thin layers. , this drawback can be avoided.

また、本発明において被覆層を重ねる順序は母材、 T
I N、 T+ B2 、 Ti N、 Ti B2 
、・・・・・・でもよく、母材、 Ti 82 、 T
I N、 TI B2 。
In addition, in the present invention, the order in which the coating layers are stacked is base material, T
I N, T+ B2, Ti N, Ti B2
, . . . , the base material, Ti 82 , T
IN, TI B2.

TiN・・・・・・の順序の何れでも良い。Any order of TiN may be used.

本発明による製造方法、特に被覆層の形成方法は、化学
気相蒸着法により、Ti 、HおよびNを含んだガス、
例えばTi C+3 、T2 およびN2の混合ガスと
Ti、HおよびBを含んだガス、例えばT1Cl、Hお
よびBCI  の混合ガスを交ηに間欠的に導入するこ
とで簡潔かつ有効に多重被覆膜形成が可能である。
The manufacturing method according to the present invention, particularly the method for forming a coating layer, uses a gas containing Ti, H and N, by chemical vapor deposition method.
For example, by intermittently introducing a mixed gas of TiC+3, T2, and N2 and a gas containing Ti, H, and B, such as a mixed gas of T1Cl, H, and BCI, it is possible to easily and effectively form multiple coatings. is possible.

さらに、従来より知られているように、化学気相蒸着法
を用いる場合、Ti NM膜形成温度は約970℃、T
iB2被膜形成温度は920℃と低い。
Furthermore, as is conventionally known, when chemical vapor deposition is used, the Ti NM film formation temperature is approximately 970°C, T
The iB2 film formation temperature is as low as 920°C.

したがってTiN被覆からTiB2 被覆へ、あるいは
逆にTiB2 被覆からTiN被覆へと切替えるときに
被覆温度を変更する必要があり、このときに被覆粒子の
異状成長が生じることが避けられず、被膜の性質が劣化
する原因となっている。
Therefore, when switching from TiN coating to TiB2 coating, or conversely from TiB2 coating to TiN coating, it is necessary to change the coating temperature, and at this time, it is inevitable that abnormal growth of the coating particles will occur, and the properties of the coating will change. This causes deterioration.

ところが本願発明者らは、ガスを間欠的に混入した場合
には、気相からの析出粒子の核生成頻度は多くなるが成
長速度は遅くなることを見出し、これに基づいて本発明
を完成した。従って、本発明においては、ガスを間欠的
に混入させることが望ましく、これによりTiB2 を
被覆する温度をFiNと同一の温度に選んでも、微細な
粒子を得ることができるという優れた効果が得られる。
However, the inventors of the present application found that when gas is mixed intermittently, the frequency of nucleation of precipitated particles from the gas phase increases, but the growth rate slows down.Based on this, the present invention was completed. . Therefore, in the present invention, it is desirable to mix the gas intermittently, and this provides the excellent effect of being able to obtain fine particles even if the temperature at which TiB2 is coated is chosen to be the same as that for FiN. .

この場合電磁場をかけてプラズマ状態どして活性化悪名
を行なうことももちろん可能である。
In this case, it is of course possible to apply an electromagnetic field to activate the plasma state.

また、本発明において、多重被覆層は少なくとも8層以
上、望ましくは20層以上が良い。8層未満では前述し
た多重被覆の効果が十分発揮できない。また、各単層の
厚みは、被覆材料層間の歪を均一に分散させるために、
1μm以下好ましくは0.511m以下が良い。これは
、1μmを越えると耐欠損性が劣化するためである。
Further, in the present invention, the number of multiple coating layers is at least 8 or more, preferably 20 or more. If there are less than 8 layers, the effect of the multiple coating described above cannot be sufficiently exhibited. In addition, the thickness of each single layer is adjusted to uniformly distribute the strain between the coating material layers.
The thickness is preferably 1 μm or less, preferably 0.511 m or less. This is because if the thickness exceeds 1 μm, the fracture resistance deteriorates.

実施例1 W C−6%CO超硬合金上にT+ N、r; B2被
19を交nに各層0.1μm1合計6μmの被膜を被覆
した。このチップを試料へとする。
Example 1 WC-6%CO cemented carbide was coated with T+N, r; B2 coating 19 with each layer having a thickness of 0.1 μm and a total thickness of 6 μm. This chip is used as a sample.

同時に比較材として、上記超硬合金上に下層にT! N
、上層にTiB2をそれぞれ3μmずつ合計6μmの膜
厚を有する被膜を被覆した。このチップを試料Bとする
。これら2種の試料を以下の切削条件、即ち、 被削材   80M3 切削速度  200m/’min 送   リ        0.3mm/ rev切り
込み  2mm にて切削テストを行なった。比較量のBチップは17分
でフランク部の摩耗が進行し寿命に至ったのに対し、本
発明によるAチップは55分間の切削でも良好な切削性
能を示した。
At the same time, as a comparative material, T! N
The upper layer was coated with a TiB2 film having a total thickness of 6 μm, each having a thickness of 3 μm. This chip is designated as sample B. A cutting test was conducted on these two types of samples under the following cutting conditions: Work material: 80 M3 Cutting speed: 200 m/'min Feed: 0.3 mm/rev Depth of cut: 2 mm. While the comparative B chip reached the end of its life due to wear of the flank after 17 minutes, the A chip according to the present invention showed good cutting performance even after 55 minutes of cutting.

実施例2 W C−8%TiC−8%TaC−6%CO超硬合金土
にTiB2.TiN被膜を各層0.0511m合品18
μmの被膜を被覆した。このチップを試料Cとする。同
時に比較材として同じ超硬合金4−に下層にTiB 、
土層にTiNをそれぞれ3μ園。
Example 2 WC-8%TiC-8%TaC-6%CO TiB2. TiN coating 0.0511m each layer 18
A coating of μm was coated. This chip is designated as sample C. At the same time, the same cemented carbide 4- was used as a comparison material with TiB in the lower layer.
Add 3μ of TiN to each soil layer.

5μm 9合□18μmの膜厚をイjする被膜を被覆し
た。このチップを試料[〕とする。
A film having a thickness of 5 μm, 9 squares, and 18 μm was coated. Let this chip be the sample [].

次にこれら2種の試料を以上の断続切削条件叩ら 切削迷電   22011’In1n 送   リ          0.41111117
’ rev切り込み    1.5+nn+ 被削材    80M3 10mm幅の満(Jさ に(切削jス]・を行なった。比較材のDチップは40
回の衝撃C′欠損したが、本発明のCは700回の1!
I撃(b欠損に至らなかった。
Next, these two types of samples were subjected to the above intermittent cutting conditions.
' rev depth of cut 1.5+nn+ Work material 80M3 10mm wide (cutting j) was performed. D tip of comparison material was 40
The impact C' was lost, but the C of the present invention is 1 of 700 times!
I hit (did not result in b deficiency).

以1訂述した如く、本発明によれば、T! N。As described above, according to the present invention, T! N.

11[32の薄い被膜を交Hに多重被覆することに」、
す、耐)?耗竹、耐衝撃↑りに冨む被覆超硬合金をI′
すること/J((さるのでイの工業上の効果は大である
1、 手続補正書(方式) %式% 浦+lを−4る者 どi  +1   ・5081 111“l傘属株式会
社代  ノイ  古   河   野      L1
1!    火成   理    人 二
11 [Multiple coating of 32 thin films in alternation]
Su-tai)? I' is a coated cemented carbide that is highly wear-resistant and impact resistant.
What to do/J Furukawano L1
1! Osamu Ichinari Jinji

Claims (1)

【特許請求の範囲】 1、”vVC基if!1映合企、−r’ic基υ−メツ
1−1また(よ−「IN早サすメットの表面に、TiN
  および11B2よりなる被輩層が、中層の厚さ1μ
m以■・Cあって、含み12〜11jμmのI9ざに交
Tjに少くとし8に1以l−多重被覆されてなることを
18 mと・」る多重被覆材料。 2、[記単層のJνさが()、5μm以下であることを
特徴とする特M’IO^求の範囲第1項記載の多重被覆
材料。 3.1記被@層が20層以↓であることを1.′I徴と
りる持許晶求の範囲第1項または第21ji記載の多重
被覆N斜。 4、WC基超硬合仝、1’iC基サーメット、。したは
TiN基リーすツトを基体どして装入し4ある炉内に、
l’ i 、 tlおよびNを1【ん・Ijガスと−[
1゜H&;五〇Bを含んだガスを、交互に間欠的に導入
し、化学蒸も法にてTiNと−riB2  を交Haか
つ多層被覆することを特徴とする多重被覆材料の製造法
[Claims] 1. ``vVC group if!
and 11B2, the middle layer has a thickness of 1 μm.
A multi-coated material having a thickness of 18 m or more and having an I9 of 12 to 11 μm, reduced to an intersecting Tj of 12 to 11 μm, and 8 to 1 or more multi-coated. 2. The multi-coated material according to item 1, characterized in that the Jv of the single layer is 5 μm or less. 3.1 The number of covered @ layers is 20 or more ↓. 1. The multi-coated N slope according to item 1 or item 21ji. 4. WC-based cemented carbide, 1'iC-based cermet. Next, the TiN-based lead was charged as a substrate and placed in a 4-unit furnace.
l' i , tl and N with 1[n・Ij gas and -[
1. A method for producing a multi-coated material, which comprises alternately and intermittently introducing a gas containing 1°H &;
JP9279182A 1982-05-31 1982-05-31 Multiple coating material and its manufacture Pending JPS58209554A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9279182A JPS58209554A (en) 1982-05-31 1982-05-31 Multiple coating material and its manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9279182A JPS58209554A (en) 1982-05-31 1982-05-31 Multiple coating material and its manufacture

Publications (1)

Publication Number Publication Date
JPS58209554A true JPS58209554A (en) 1983-12-06

Family

ID=14064236

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9279182A Pending JPS58209554A (en) 1982-05-31 1982-05-31 Multiple coating material and its manufacture

Country Status (1)

Country Link
JP (1) JPS58209554A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145739A (en) * 1990-07-12 1992-09-08 Sarin Vinod K Abrasion resistant coated articles
US6228483B1 (en) 1990-07-12 2001-05-08 Trustees Of Boston University Abrasion resistant coated articles
WO2009070820A1 (en) * 2007-12-06 2009-06-11 Ceratizit Austria Gmbh Coated article

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145739A (en) * 1990-07-12 1992-09-08 Sarin Vinod K Abrasion resistant coated articles
US6228483B1 (en) 1990-07-12 2001-05-08 Trustees Of Boston University Abrasion resistant coated articles
WO2009070820A1 (en) * 2007-12-06 2009-06-11 Ceratizit Austria Gmbh Coated article
JP2011505261A (en) * 2007-12-06 2011-02-24 セラティチット オーストリア ゲゼルシャフト ミット ベシュレンクテル ハフツング Coated article
US8388709B2 (en) 2007-12-06 2013-03-05 Ceratizit Austria Gesellschaft GmbH Coated article

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