Articles consisting of metal, hard metal, cermet or ceramic and coated with a hard material, and method for producing such articles
11459660 · 2022-10-04
Assignee
Inventors
Cpc classification
C23C16/30
CHEMISTRY; METALLURGY
C23C28/044
CHEMISTRY; METALLURGY
C23C28/048
CHEMISTRY; METALLURGY
International classification
Abstract
Articles containing metal, hard metal, cermet or ceramic and coated with a hard material, and a method for producing same. The hard material layers can be used as anti-wear layers for cutting tools, as protective layers for turbine blades, or as diffusion barriers in microelectronics. The hard material layers exhibit a high hardness, high oxidation resistance, and excellent wear resistance. The articles are coated with a single- or multi-layer layer system by a thermal CVD method without plasma excitation, where the single- or multi-layer layer system includes at least one nanocomposite layer with a first nanocrystalline phase of cubic titanium oxycarbonitride and a second, amorphous phase of silicon oxycarbonitride or silicon oxycarbide.
Claims
1. Articles consisting of metal, hard metal, cermet or ceramic and coated with a hard material, Which articles are coated with a single- or multi-layer layer system by means of a thermal CVD method without plasma excitation, wherein the single- or multi-laver layer system contains at least one nanocomposite layer with an overall composition of (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) with 0.7<x≤0.99 and 0.01≤y<0.3 and 0.4<a<0.9 and 0.1<b<0.6 and 0.01<c≤0.1, with x+y=1 and a+b+c=1, wherein the nanocomposite layer comprises a first nanocrystalline phase of cubic titanium oxycarbonitride with a crystallite size of 10 nm to 20 nm and a second, amorphous phase of silicon oxycarbonitride or silicon oxycarbide, wherein Ti—O bonds and Si—O bonds are formed; and wherein the nanocomposite layer has a chlorine content between 0.001 and 1 at. %.
2. The articles coated with a hard material according to claim 1 in which multiple nanocomposite layers are arranged.
3. The articles coated with a hard material according to claim 1 in which the one or more nanocomposite layers have a gradient with respect to the Si/Ti atomic ratio.
4. The articles coated with a hard material according to claim 1 in which at least one nanocomposite layer has a lamellar structure.
5. The articles coated with a hard material according to claim 4 in which the layer having the lamellar structure comprises lamellae with a thickness between 50 nm and 500 nm.
6. The articles coated with a hard material according to claim 4 in which the layer having the lamellar structure comprises lamellae with different Si/Ti atomic ratios.
7. The articles coated with a hard material according to claim 1 in whiCh the nanocomposite layer has a hardness of 3000 HV to 4000 HV.
8. The articles coated with a hard material according to claim 1 in which the nanocomposite layer has a layer thickness of 1 μm to 10 μm.
9. The articles coated with a hard material according to claim 1 in which one or more cover layers and/or bonding layers are present.
10. The articles coated with a hard material according, to claim 9 in which the cover layers and/or bonding layers are composed of one or more nitrides, carbides, carbonitrides, oxynitrides, oxycarbides, oxycarbonitrides, oxides of Ti, Hf, Zr, Cr and/or Al or mixed phases of these elements.
11. The articles coated with a hard material according to claim 1 in which the nanocomposite layer has a hardness of 3300 HV to 3600 HV.
12. The articles coated with a hard material according to claim 1 in which the nanocomposite layer has a layer thickness of 4 μm to 7 μm.
13. A method for producing articles consisting of metal, hard metal, cermet or ceramic and coated with a hard material, according to claim 1, said method comprising: depositing at least one (TixSiy)(CaNbOc) nanocomposite layer by a thermal CVD method without plasma excitation in a gas mixture of TiCl.sub.4 one or more silicon chlorides, CH.sub.3CN, H.sub.2, using a gas admixture from CO or CO.sub.2 and at temperatures between 700° C. and 950° C. and at pressures between 0.1 kPa and 0.1 MPa, wherein an Si/Ti atomic ratio of greater than 1 is chosen for the silicon chloride and titanium chloride in the gas phase.
14. The method according to claim 13 further comprising: adding in which N.sub.2 is added to the gas mixture.
15. Articles consisting of metal, hard metal, cermet or ceramic and coated with a hard material, which articles are coated with a single- or multi-layer layer system by means of a thermal CVD method without plasma excitation from a gas mixture of TiCl.sub.4 one or more silicon chlorides, CH.sub.3CN, H.sub.2, using a gas admixture from CO or CO.sub.2 and at temperatures between 700° C. and 950° C. and at pressures between 0.1 kPa and 0.1 MPa, wherein the single- or multi-layer layer system contains at least one nanocomposite layer with an overall composition of (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) with 0.7<x≤0.99 and 0.01≤y<0.3 and 0.4<a<0.9 and 0.1<b<0.6 and 0.01<c≤0.1, with x+y=1 and a+b+c=1, wherein the at least one nanocomposite layer has a lamellar structure with different Si/Ti atomic ratios, wherein the nanocomposite layer comprises a first nanocrystalline phase of cubic titanium oxycarbonitride with a crystallite size of 10 nm to 20 nm and a second, amorphous phase of silicon oxycarbonitride or silicon oxycarbide, wherein Ti—O bonds and Si—O bonds are formed; and wherein the nanocomposite layer has a chlorine content between 0.001 and 1 at. %.
Description
(1) The invention is explained below in greater detail with the aid of exemplary embodiments and figures. The figures show:
(2)
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EXEMPLARY EMBODIMENT 1
(8) A high-silicon (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer is deposited as a cover layer by means of a thermal CVD method on WC/Co indexable hard metal inserts that are pre-coated with a 5-μm thick TiN/TiCN/TiN layer system. The coating process is carried out in a hot wall CVD reactor with an inner diameter of 75 mm. The CVD coating takes place with a gas mixture of 0.09 vol. % TiCl.sub.4, 0.58 vol. % SiCl.sub.4, 0.23 vol. % CH.sub.3CN, 0.31 vol. % CO and 98.79 vol. % H.sub.2. The deposition temperature is 850° C. and the process pressure is 6 kPa. After a coating time of 90 min, a 4.5-μm thick (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) layer is obtained.
(9) From the X-ray diffractogram in
(10) By means of Rietveld analysis, a crystallite size of 18.3±1.8 nm was determined for the nanocrystalline titanium oxycarbonitride phase.
(11) The elemental analysis by means of WDX found the following element content:
(12) 39.5 at. % Ti,
(13) 9.7 at. % Si,
(14) 27.2 at. % C,
(15) 21.0 at. % N,
(16) 2.1 at. % O,
(17) and 0.5 at. % Cl.
(18) For this (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer, there results a y value of 0.2, which is calculated from the concentrations in at. % in accordance with y=Si/(Si+Ti). From the WDX elemental analysis, there results an overall composition for C, N, O with a=0.54, b=0.42 and c=0.04. By means of a Vickers indenter, a microhardness of 3590 HV [0.01] was measured.
Exemplary Embodiment 2
(19) A low-silicon (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer is deposited as a cover layer by means of a thermal CVD method on WC/Co indexable hard metal inserts that are pre-coated with a 5-μm thick TiN/TiCN/TiN layer system. The coating process is carried out in a hot wall CVD reactor with an inner diameter of 75 mm. The CVD coating takes place with a gas mixture of 0.18 vol. % TiCl.sub.4, 0.57 vol. % SiCl.sub.4, 0.22 vol. % CH.sub.3CN, 0.78 vol. % CO, 71.38 vol. % H.sub.2, and 26.87 vol. % N.sub.2. The deposition temperature is 850° C. and the process pressure is 6 kPa. After a coating time of 90 min, a 6.9-μm thick (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) layer is obtained.
(20) In the X-ray thin layer analysis conducted with grazing incidence, only a cubic TiC.sub.xN.sub.1-x phase is identified, as the X-ray diffractogram presented in
(21) As an additional phase, the nanocomposite layer contains amorphous silicon oxycarbonitride, which was also identified by means of XPS analysis. By means of Rietveld analysis, a crystallite size of 16.8±2.1 nm was determined for the nanocrystalline titanium oxycarbonitride phase.
(22) The elemental analysis by means of WDX found the following element content:
(23) 43.2 at. % Ti,
(24) 1.7 at. % Si,
(25) 26.0 at. % C,
(26) 25.4 at. % N,
(27) 3.4 at. % O, and
(28) 0.3 at. % Cl.
(29) For this (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer, there results a y value of 0.04, which is calculated from the concentrations in at. % in accordance with y=Si/(Si+Ti). From the WDX elemental analysis, there results an overall composition for C, N, O with a=0.47, for b=0.46 and for c=0.06. By means of a Vickers indenter, a microhardness of 3330 HV [0.01] was measured.
Exemplary Embodiment 3
(30) A (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer is deposited as a cover layer by means of the thermal CVD method according to the invention on WC/Co indexable hard metal inserts that are pre-coated with a 5-μm thick TiN/TiCN/TiN layer system. The coating process is carried out in a hot wall CVD reactor with an inner diameter of 75 mm. The CVD coating takes place with a gas mixture of 0.09 vol. % TiCl.sub.4, 0.58 vol. % SiCl.sub.4, 0.22 vol. % CH.sub.3CN, 0.31 vol. % CO, 71.5 vol. % H.sub.2, and 27.3 vol. % N.sub.2. The deposition temperature is 850° C. and the process pressure is 6 kPa.
(31) After a coating time of 90 min, a 4.1-μm thick (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer is obtained.
(32)
(33) The elemental analysis by means of WDX found the following element content:
(34) 42.1 at. % Ti,
(35) 4.7 at. % Si,
(36) 26.7 at. % C,
(37) 23.7 at. % N,
(38) 2.7 at. % O, and
(39) 0.1 at. % Cl.
(40) For this (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer, there results a y value of 0.1, which is calculated from the concentrations in at % in accordance with y=Si/(Si+Ti). From the WDX elemental analysis, there results an overall composition for C, N, O with a=0.50, for b=0.45 and for c=0.05. By means of a Vickers indenter, a microhardness of 3410 HV [0.01] was measured.
Exemplary Embodiment 4
(41) A (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer is deposited as a cover layer by means of a thermal CVD method on WC/Co indexable hard metal inserts that are pre-coated with a 5-μm thick TiN/TiCN/TiN layer system. The coating process is carried out in a hot wall CVD reactor with an inner diameter of 75 mm. The CVD coating takes place with a gas mixture of 0.12 vol. % TiCl.sub.4, 0.58 vol. % SiCl.sub.4, 0.22 vol. % CH.sub.3CN, 0.59 vol. % CO, 71.36 vol. % H.sub.2, and 27.13 vol. % N.sub.2. The deposition temperature is 850° C. and the process pressure is 6 kPa. After a coating time of 90 min, a 4.4-μm thick (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) layer is obtained.
(42) In the X-ray thin layer analysis conducted with grazing incidence, only a cubic TiC.sub.xN.sub.1-x phase is identified. XPS analyses found that the cubic TiC.sub.xN.sub.1-x phase is composed of titanium oxycarbonitride. As an additional phase, the nanocomposite layer contains amorphous silicon oxycarbide that was identified by the XPS analysis shown in
(43) The elemental analysis by means of WDX found the following element content:
(44) 42.5 at. % Ti,
(45) 2.7 at. % Si,
(46) 25.5 at. % C,
(47) 26.2 at. % N,
(48) 2.9 at. % O, and
(49) 0.2 at. % Cl.
(50) For this (Ti.sub.xSi.sub.y)(C.sub.aN.sub.bO.sub.c) nanocomposite layer, there results a y value of 0.06, which is calculated from the concentrations in at % in accordance with y=Si/(Si+Ti). From the WDX elemental analysis, there results an overall composition for C, N, O with a=0.47, for b=0.48 and for c=0.05. By means of a Vickers indenter, a microhardness of 3410 HV [0.01] was measured.