KR19980059980A - Cutting coated carbide tool and manufacturing method thereof - Google Patents

Cutting coated carbide tool and manufacturing method thereof Download PDF

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KR19980059980A
KR19980059980A KR1019960079327A KR19960079327A KR19980059980A KR 19980059980 A KR19980059980 A KR 19980059980A KR 1019960079327 A KR1019960079327 A KR 1019960079327A KR 19960079327 A KR19960079327 A KR 19960079327A KR 19980059980 A KR19980059980 A KR 19980059980A
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layer
vapor deposition
chemical vapor
coating
ticn
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KR1019960079327A
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Korean (ko)
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김종성
이상훈
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양수제
대한중석 주식회사
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Publication of KR19980059980A publication Critical patent/KR19980059980A/en

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Abstract

본 발명은 절삭공구 모재표면에 코팅되는 코팅층 내부의 잔류응력을 제거하여 밀착성을 높이고, 내마모성 및 인성을 증대시켜 사용수명을 향상시키는 절삭공구에 관한 것으로, 모재 표면에 증온화학 증착법에 따른 TiCN층과, 고온화학 증착법에 따른 TiC층 및 금속산화물층을 코팅하여서 된 절삭용 피복 초경합금 공구 및 그 제조방법에 관한 기술이다.The present invention relates to a cutting tool that improves the service life by removing the residual stress inside the coating layer coated on the cutting tool base material surface, increasing wear resistance and toughness, and the TiCN layer according to the temperature-temperature chemical vapor deposition method on the base material surface. The present invention relates to a cutting coated cemented carbide tool obtained by coating a TiC layer and a metal oxide layer according to a high temperature chemical vapor deposition method, and a method of manufacturing the same.

Description

절삭용 피복 초경합금 공구 및 그 제조방법Cutting coated carbide tool and manufacturing method thereof

본 발명은 금속 절삭 가공용 공구재료로 사용되는 피복 초경합금 인서트에 관한 것으로, 보다 상세하게는 절삭 공구 모재의 표면에 코팅되는 코팅층을 중온 및 고온화학증착법으로 적층되게 피복 처리함으로써 코팅층 내부의 잔류응력을 제거하여 밀착성을 높이고, 내마모성과 인성에 따른 사용 수명을 향상시키는데 적합한 절삭용 피복 초경합금 공구 및 그 제조방법에 관한 것이다.The present invention relates to a coated cemented carbide insert used as a tool material for metal cutting, and more particularly, to remove the residual stress inside the coating layer by coating the coating layer coated on the surface of the cutting tool base material by lamination by medium temperature and high temperature chemical vapor deposition. The present invention relates to a cutting-coated cemented carbide tool suitable for improving adhesiveness and improving service life due to wear resistance and toughness.

일반적으로 절삭공구는 철, 강(합금강)등의 소재를 절삭 가공하는 용도로 사용되는데, 내마모성 및 인성을 보다 좋게 하기 위하여 공급 모재 표면에 각종 금속 산화물, 탄화물 등을 화학증착법으로 피복하고 있다.Generally, cutting tools are used for cutting materials such as iron and steel (alloy steel), and various metal oxides and carbides are coated on the surface of the supply base material by chemical vapor deposition for better wear resistance and toughness.

통상적인 화학증착법은 고온화학증착법과 중온화학증착법이 있다.Conventional chemical vapor deposition methods include high temperature chemical vapor deposition and medium temperature chemical vapor deposition.

고완화학증착법은 사염화티타늄, 질소, 메탄, 수소, 가스 등을 함유하는 가스 혼합체를 900℃~1100℃ 정도의 온도에서 초경합금 모재와 반응시켜 티타늄화합물인 TiC, TiCN, TiN 등을 피복층으로 하고, 그 상면에는 AlCl3, CO2등의 기체를 반응시켜 세라믹의 일종인 알루미나(혹은 산화알루미늄)를 피복층으로 한다.In the chemical vapor deposition method, a gas mixture containing titanium tetrachloride, nitrogen, methane, hydrogen, gas, and the like is reacted with a cemented carbide base material at a temperature of about 900 ° C to 1100 ° C, and a titanium compound, TiC, TiCN, TiN, etc., is used as a coating layer. The upper surface is made of alumina (or aluminum oxide), which is a kind of ceramic, as a coating layer by reacting gases such as AlCl 3 and CO 2 .

상기 티타늄화합물로 하는 피복층은 두 층으로 할 수 있다. 예로서 1층으로는 TiN층으로 하는, 2층으로는 TiCN층으로 하는데, 이들의 층을 바꿀 수도 있다.The coating layer made of the titanium compound may be made of two layers. For example, although a TiN layer is used as one layer and a TiCN layer is used as two layers, these layers can also be changed.

이와 같은 고온화학증착법에 따른 적층구조는 내마모용 공구나 초경공구에 적용하여 절삭성능과 공구수명을 어느 정도 향상시키고 있으나, 고온으로 코팅하므로써 코팅층 직하와 모재계면 사이의 경계부위에 원하지 않는 경질상인 에타(η : eta)상 화합물이 형성되어 공구수명에 나쁜 영향을 미침에 따라 적용 영역의 축소를 초래한다.The laminated structure according to the high temperature chemical vapor deposition method is applied to wear-resistant tools or carbide tools to improve the cutting performance and tool life to some extent, but by applying the coating at high temperature, unwanted hard phases on the boundary between the coating layer and the base material interface An eta (eta) phase compound is formed, which adversely affects tool life, resulting in a reduction of the application area.

에타상 화합물은 경도는 높지만 취성이 있고, 모재와 코팅층의 부착력을 감소시킨다.The eta phase compound has high hardness but is brittle, and reduces adhesion between the base material and the coating layer.

따라서 부착력 저하 및 공구의 인성을 저하시키므로 절삭공구로써의 제기능을 다하지 못하는 결점이 있다.Therefore, there is a drawback that the adhesive force is lowered and the toughness of the tool is lowered, thereby failing to function as a cutting tool.

이에 본 발명자는 상기한 결점을 개선하기 위해 도 1과 같이 모재(1) 표면에 700~900℃ 온도인 증온화학증착법에 의거 TiCN층(3)을 코팅하고 그 상면에는 900~1100℃ 온도인 고온화학증착법에 의거 Al2O3층(5)을 코팅한 기술을 국내 특허출원 96~1603호(이하 선기술이라함)로 출원한 바 있다.In order to improve the above-mentioned defects, the present inventors coat the TiCN layer 3 on the surface of the base material 1 according to the chemical vapor deposition method, which is 700 to 900 ° C, and a high temperature of 900 to 1100 ° C on the upper surface thereof. Based on the chemical vapor deposition method, the technology of coating the Al 2 O 3 layer (5) has been filed in the domestic patent application No. 96 ~ 1603 (hereinafter referred to as the prior art).

그러나 상기한 선기술은 두 코팅층의 열전도도 및 열팽창 계수의 차이가 커서 코팅층 내부의 잔류응력이 존재하므로 인한 밀착성의 결여로 절삭공구 수명에 영향을 미치고 있다.However, the above-described technology has a large difference in thermal conductivity and coefficient of thermal expansion between the two coating layers, and thus has a residual stress inside the coating layer, thereby affecting the cutting tool life due to the lack of adhesion.

본 발명은 상기한 종래의 문제점을 개선하기 위해 안출한 것으로, 선기술의 두 코팅층 사이에 또 다른 코팅층을 삽입하므로써 코팅층 내부의 잔류응력을 제거하여 밀착성이 높고, 내마모성이 우수한 적층구조를 갖는 합금공구를 얻는데 그 목적이 있다.The present invention has been made in order to improve the above-mentioned conventional problems, by inserting another coating layer between the two coating layers of the prior art by removing the residual stress in the coating layer of the alloy tool having a high adhesiveness, laminated structure excellent in wear resistance To get that purpose.

도 1은 종래에 따른 피복 적층 구조의 단면도.1 is a cross-sectional view of a conventional laminated structure.

도 2a는 본 발명에 따른 피복 적층 구조의 단면도.2A is a cross-sectional view of a clad laminate structure according to the present invention.

도 2b는 본 발명의 타실시예에 따른 피복 적층 구조를 나타낸 단면도.Figure 2b is a cross-sectional view showing a coating laminated structure according to another embodiment of the present invention.

도 3a는 본 발명을 이용한 피삭재(SKT4)를 건식 절삭한 경우의 내마모성 시험을 나타낸 그래프.Figure 3a is a graph showing the wear resistance test in the case of dry cutting the workpiece (SKT4) using the present invention.

도 3b는 본 발명을 이용한 피삭재(SKT4)를 습식 절삭한 경우의 내마모성 시험을 나타낸 그래프.3B is a graph showing abrasion resistance test in the case of wet cutting the workpiece (SKT4) using the present invention.

도 4는 본 발명을 이용한 피삭재(SKT4)를 건식 절삭한 경우의 내결손성 시험을 나타낸 그래프.Figure 4 is a graph showing the fracture resistance test in the case of dry cutting the workpiece (SKT4) using the present invention.

도면의 주요부분에 대한 부호의 설명Explanation of symbols for main parts of the drawings

1 : 모재 2 : TiN층1: Base material 2: TiN layer

3 : TiCN층 4 : TiC층3: TiCN layer 4: TiC layer

5 : Al2O35: Al 2 O 3 layer

이와 같은 목적을 달성하기 위한 본 발명은 그 실시예를 나타낸 도 2a와 같이, 모재(1)의 표면에 TiCN층(2)과 TiN층(3)과 Al2O3층(4)이 형성되거나 도 2b와 같이 모재(1)와 TiCN(3) 사이에 TiN층 또는 TiCN층(2)이 형성된 구조로 이루어 진다.In order to achieve the above object, in the present invention, as shown in FIG. 2A, the TiCN layer 2, the TiN layer 3, and the Al 2 O 3 layer 4 are formed on the surface of the base material 1. As shown in FIG. 2B, the TiN layer or the TiCN layer 2 is formed between the base material 1 and the TiCN 3.

상기한 적층구조에서 각각의 두께는 TiCN을 0.1~15㎛, TiN층을 0.5~5.0㎛, 금속산화합물층을 0.1~3.0㎛ 범위로 함이 바람직하다.In the above laminated structure, each thickness is preferably in the range of 0.1 to 15 μm of TiCN, 0.5 to 5.0 μm of the TiN layer, and 0.1 to 3.0 μm of the metal acid compound layer.

본 발명에 이용되는 모재는 WC, TaC, TiC, CO 등으로 조성된 여타의 초경합금을 대상으로 할 수 있는 것으로, 모재 표면에 티타늄 화합물을 피복할 수 있는 대상이면 모두 적용가능하다.The base material used in the present invention can be applied to other cemented carbides composed of WC, TaC, TiC, CO, etc., and any applicable material can be applied as long as it can coat the titanium compound on the surface of the base material.

따라서 모재 조성을 어느 하나에 국한하지 않는다.Therefore, the base material composition is not limited to any one.

티타늄 화합물층에 적층되는 금속산화물은 일예로써 Al2O3를 들 수 있다.The metal oxide laminated on the titanium compound layer may include Al 2 O 3 as an example.

상기한 적층구조를 갖도록 코팅처리함에 있어서는, 먼저 모재(1)의 표면에 증온화학증착법(약 700~900℃ 부근)을 이용하여 0.1~15㎛ 두께의 TiCN층(3)이 되게 코팅하고, 고온화학증착법(약 900~1100℃ 부근)을 이용하여 0.5~5㎛ 두께의 TiC층(4)과, 0.1~3.0㎛ 두께의 금속 산화물층(5)이 되게 순차적으로 코팅한다.In the coating treatment to have the laminate structure described above, first, the surface of the base material 1 is coated to a TiCN layer 3 having a thickness of 0.1 to 15 μm by using a chemical vapor deposition method (around 700 to 900 ° C.), and a high temperature. The chemical vapor deposition (approximately 900 to 1100 ° C) is used to coat the TiC layer 4 having a thickness of 0.5 to 5 µm and the metal oxide layer 5 having a thickness of 0.1 to 3.0 µm.

또한 본 발명은 도 2b와 같이 모재(1)와 TiCN층(3) 사이에 TiN층(2) 또는 TiCN층을 고온화학증착법으로 0.1~1.0㎛ 두께로 형성시킬 수 있다.In addition, the present invention can form a TiN layer (2) or TiCN layer between 0.1 to 1.0㎛ thickness between the base material (1) and the TiCN layer (3) by a high temperature chemical vapor deposition method.

다음은 실시예에 따라 설명한다.The following is described according to the embodiment.

밀링 절삭용 공구의 규격이 SPKN 1203DETR인 초경합금 모재를 하기의 표 1, 2, 3과 같은 조건으로 코팅하였다.The cemented carbide cutting material, the specification of SPKN 1203DETR, was coated under the conditions shown in Tables 1, 2, and 3 below.

표 1은 기존의 고온화학증착법을 이용한 코팅(TiCN층, Al2O3층)조건을 나타낸 것이고(시편 1), 표 2는 기존의 중온화학증착법에 따른 코팅(TiCN)조건 및 고온화학증착법에 따른 코팅(Al2O3) 조건을 나타낸 것이고(시편 2), 표 3은 본 발명으로써, 중온화학증착법에 따른 코팅(TiCN) 및 고온화학증착법에 따른 코팅(TiC층, Al2O3층)조건을 나타낸 것이다.Table 1 shows the coating (TiCN layer, Al 2 O 3 layer) conditions using the conventional high temperature chemical vapor deposition method (Sample 1), Table 2 shows the coating (TiCN) conditions and high temperature chemical vapor deposition method according to the conventional medium temperature chemical vapor deposition method According to the coating (Al 2 O 3 ) conditions (Sample 2), Table 3, the present invention, the coating according to the medium temperature chemical vapor deposition (TiCN) and the coating according to the high temperature chemical vapor deposition (TiC layer, Al 2 O 3 layer) The condition is shown.

표 4는 상기 조건에 따른 코팅층 두께를 나타낸 것이다.Table 4 shows the coating layer thickness according to the above conditions.

이들 코팅조건에서는 상호 대비를 위하여 중요단계만 제시하였고, 각 단계 사이의 짧은 전이단계들은 생략하고 단순화하였다.In these coating conditions, only important steps are presented for mutual contrast, and short transition steps between each step are omitted and simplified.

모재는 WC, TaC, TiC, CO 로 구성된 초경합금으로 각 조건에 대하여 모두 동일한 것으로 하였다.The base material is a cemented carbide composed of WC, TaC, TiC, and CO, and all were the same for each condition.

상기 피복된 세가지 종류의 시편 표 1~표 3에 대하여 밀링 절삭시험을 실시하여 성능을 비교하였다.Milling cutting test was performed on the three coated specimens Tables 1 to 3 to compare the performance.

성능비교는 일반적으로 밀링절삭방법에 의하여 내마모성 시험을 하였고, 공구에 충격이 심하게 걸리는 조건으로 내결손성 시험도 하였다.In general, the performance comparison was performed by the milling cutting method, and the fracture resistance test was performed under the condition that the tool was severely impacted.

[표 1]TABLE 1

종래의 고온화학증착법(TiCN층, Al2O3층)(시편 1)Conventional High Temperature Chemical Vapor Deposition (TiCN Layer, Al 2 O 3 Layer) (Sample 1)

[표 2]TABLE 2

종래의 중온 및 고온화학증착법(시편 2)Conventional Medium and High Temperature Chemical Vapor Deposition (Psalm 2)

[표 3]TABLE 3

본 발명에 따른 증착법Deposition method according to the invention

[표 4]TABLE 4

각 조건에서의 코팅층 두께Coating layer thickness at each condition

내마모 시험Abrasion resistance test

비교시험에서 절삭조건은 피삭재가 SKT 4 재질의 강한 경우에 절삭속도를 180mm/min, 이송량을 0.1mm/tooth, 절삭깊이를 2.0mm로 하여 각각 건식과 습식에서 절삭을 실시하였다.In the comparative test, the cutting conditions were cut dry and wet with the cutting speed of 180mm / min, feed rate of 0.1mm / tooth and depth of cut of 2.0mm when the workpiece was made of SKT 4 material.

공구 측면의 최대 마모(프랭크 마모)량을 Vb max로 표시하였으며, 이 마모량이 적을수록 내마모성이 우수함을 나타낸다.The maximum amount of wear (Frank wear) on the side of the tool is expressed as Vb max, indicating that the lower the amount of wear, the better the wear resistance.

도 3a 및 도 3b는 시험 결과를 나타낸 것인데, 전자는 건식으로 절삭한 결과이고, 후자는 습식으로 절삭한 결과이다.3A and 3B show the test results, the former being a dry cut and the latter being a wet cut.

도 3a 및 도 3b에서와 같이 시편 1(종래)보다 시편 2(선 기술)와 시편 3(본 발명)의 내마모성이 우수한 것을 알 수 있는데, 이는 종래의 고온 화학증착법에 의한 코팅시편이 코팅층의 직하에 취약한 금속간 화합물인 에타(η)상이 형성되어 절삭시험시에 모재와 코팅층사이의 부착력을 감소시키는 요인임을 알 수 있다.3A and 3B, it can be seen that specimens 2 (linear technology) and specimens 3 (invention) have better abrasion resistance than specimens 1 (conventional), which are coated under the high temperature chemical vapor deposition method under the coating layer. It can be seen that the eta (η) phase, which is a weak intermetallic compound, is formed to reduce adhesion between the base material and the coating layer during the cutting test.

시편 3을 시편 2와 비교하면 본 발명이 우수함을 알 수 있다.Comparing specimen 3 with specimen 2, it can be seen that the present invention is excellent.

이는, 시편 2의 단점인 코팅층내부의 잔류응력을 제거하여 밀착성을 높이며, 또한 Al2O3층와 유사한 TiC에 의한 것임을 알 수 있다.This can be seen that it is due to the TiC similar to the Al 2 O 3 layer to increase the adhesion by removing the residual stress in the coating layer, which is a disadvantage of the specimen 2.

내결손 시험A defect test

내결손 시험은 상기 내마모성 시험과 동일한 SKT 4 피삭재로 절삭속도를 90m/min, 절삭깊이를 2.0mm로 실시하였으며, 이송량을 0.14mm/tooth에서 부터 몇단계 증가시키면서 건식으로 4회 실시하였다.The fracture resistance test was performed with the same SKT 4 workpiece as the abrasion resistance test with a cutting speed of 90 m / min and a depth of cut of 2.0 mm, and was carried out dry four times while increasing the feed amount from 0.14 mm / tooth to several steps.

그 결과 도 4와 같이 본 발명(시편 3)이 우수함을 알 수 있었다.As a result, it was found that the present invention (Psalm 3) is excellent as shown in FIG.

이상에서와 같이 본 발명은 공구 모재표면의 중온 화학 증착에 따른 TiC층과 고온 화학증착에 따른 TiC층 및 Al2O3층을 형성시키므로써, 코팅층간의 내부 잔류응력을 제거하여 밀착성을 좋게하고, 내마모성증대 등에 따라 사용수명이 형성된 효과를 갖는 절삭용 피복 초경합금 공구를 확보할 수 있다.As described above, the present invention forms a TiC layer according to the medium temperature chemical vapor deposition of the tool base material surface, a TiC layer according to the high temperature chemical vapor deposition, and an Al 2 O 3 layer, thereby improving the adhesion by removing the internal residual stress between the coating layers. It is possible to secure a cutting coated cemented carbide tool having an effect of forming a service life according to increased wear resistance.

Claims (8)

초경합금 공구모재 표면에 TiCN층, TiC층, 금속산화물층이 순차적으로 적층 피복된 것임을 특징으로 하는 절삭용 피복 초경합금 공구.A cemented carbide tool for cutting, characterized in that the TiCN layer, the TiC layer, and the metal oxide layer are sequentially laminated on the cemented carbide tool surface. 제1항에 있어서, TiCN층 두께가 0.1~15.0㎛, TiC층 두께가 0.5~5.0㎛, 금속산화물층 두께가 0.1~3.0㎛임을 특징으로 하는 절삭용 피복 초경합금 공구.The coated cemented carbide tool according to claim 1, wherein the TiCN layer has a thickness of 0.1-15.0 µm, the TiC layer has a thickness of 0.5-5.0 µm, and the metal oxide layer has a thickness of 0.1-3.0 µm. 제1항 또는 제2항에 있어서, 모재 표면과 TiCN층 사이에 TiN층 또는 TiCN층이 형성된 것임을 특징으로 하는 절삭용 피복 초경합금 공구.The coated cemented carbide tool according to claim 1 or 2, wherein a TiN layer or a TiCN layer is formed between the base material surface and the TiCN layer. 제1항 또는 제2항에 있어서, 금속산화물층이 Al2O3임을 특징으로 하는 절삭용 피복 초경합금 공구. 3. The coated cemented carbide tool according to claim 1 or 2, wherein the metal oxide layer is Al 2 O 3 . 초경합금 공구 모재표면에 중온 화학증착법을 이용하여 TiCN층을 코팅하고, 고온 화학증착법을 이용하여 TiC층과 금속산화물층을 순차적으로 코팅함을 특징으로 하는 절삭용 피복 초경합금 공구의 제조방법.Cemented carbide tool The method of manufacturing a coated cemented carbide tool characterized in that the coating of the TiCN layer on the surface of the base metal substrate by using a medium temperature chemical vapor deposition method, and sequentially coating the TiC layer and the metal oxide layer using a high temperature chemical vapor deposition method. 제5항에 있어서, TiCN층 두께가 0.1~15.0㎛, TiC층 두께가 0.5~5.0㎛, 금속산화물층 두께가 0.1~3.0㎛되게 코팅함을 특징으로 하는 절삭용 피복 초경합금 공구의 제조방법.The method of claim 5, wherein the TiCN layer is coated with a thickness of 0.1 to 15.0 µm, the TiC layer is 0.5 to 5.0 µm, and the metal oxide layer is 0.1 to 3.0 µm. 제5항에 있어서, 모재 표면에 고온 화학증착법을 이용하여 TiN층 또는 TiCN층을 코팅한 후 중온 화학증착법에 의해 TiCN층을 코팅함을 특징으로 하는 절삭용 피복 초경합금 공구의 제조방법.The method of claim 5, wherein the surface of the base material is coated with a TiN layer or a TiCN layer by using a high temperature chemical vapor deposition method, and then coated with a TiCN layer by a medium temperature chemical vapor deposition method. 제5항 또는 제6항에 있어서, 금속산화물이 Al2O3임을 특징으로 하는 절삭용 피복 초경합금 공구의 제조방법.7. The method of claim 5 or 6, wherein the metal oxide is Al 2 O 3 .
KR1019960079327A 1996-12-31 1996-12-31 Cutting coated carbide tool and manufacturing method thereof KR19980059980A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101381639B1 (en) * 2013-06-05 2014-04-04 주식회사 인팩 The bush for dispersing thrust

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101381639B1 (en) * 2013-06-05 2014-04-04 주식회사 인팩 The bush for dispersing thrust

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