Coated cutting tool
US-2024287680-A1 · Aug 29, 2024 · US
US9976213B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9976213-B2 |
| Application number | US-201414781622-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 16, 2014 |
| Priority date | Apr 26, 2013 |
| Publication date | May 22, 2018 |
| Grant date | May 22, 2018 |
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A tool having a base body of carbide, cermet, ceramic, steel or high speed steel and a single-layer or multi-layer wear-protection coating applied thereto in a CVD process, wherein the wear-protection coating has at least one Ti 1-x Al x C y N z layer having stoichiometry coefficients 0.70≤x<1.0≤y<0.25 and 0.75≤z<1.15 wherein the Ti 1-x Al x C y N z layer is of a thickness of 1 μm to 25 μm and has a crystallographic preferential orientation, which is characterized by a ratio of the intensities of the X-ray diffraction peaks of the crystallographic {111} plane and the {200} plane, wherein I{111}/I{200}>1+h (ln h) 2 , wherein h is the thickness of the Ti 1-x Al x C y N z layer in micrometer.
Opening claim text (preview).
The invention claimed is: 1. A process for the production of a tool having a base body of carbide, cermet, ceramic, steel or high speed steel and a single-layer or multi-layer wear-protection coating applied thereto in a CVD process, wherein the wear-protection coating has at least one Ti 1-x Al x C y N z layer having stoichiometry coefficients 0.70<x<1, 0<y<0.25 and 0.75≤z<1.15 and of a thickness in the range of 1 μm to 25 μm, wherein for production of the Ti 1-x Al x C y N z layer a) the bodies to be coated are placed in a substantially cylindrical CVD reactor designed for an afflux flow on the bodies to be coated with the process gases in a direction substantially radially relative to the longitudinal axis of the reactor, b) two precursor gas mixtures (VG1) and (VG2) are provided, wherein the first precursor gas mixture (VG1) contains 0.005% to 0.2 vol-% TiCl 4 , 0.025% to 0.5 vol-% AlCl 3 and as a carrier gas hydrogen (H 2 ) or a mixture of hydrogen and nitrogen (H 2 /N 2 ), and wherein the second precursor gas mixture (VG2) contains 0.1 to 3.0 vol-% of at least one N-donor selected from ammonia (NH 3 ) and hydrazine (N 2 H 4 ), and as a carrier gas hydrogen (H 2 ) or a mixture of hydrogen and nitrogen (H 2 /N 2 ), and wherein the first precursor gas mixture (VG1) and/or the second precursor gas mixture (VG2) optionally contains a C-donor selected from acetonitrile (CH 3 CN), ethane (C 2 H 6 ), ethene (C 2 H 4 ) and ethyne (C 2 H 2 ) and mixtures thereof, wherein the total vol-% proportion of N-donor and C-donor in the precursor gas mixtures (VG1, VG2) is in the range of 0.1 to 3.0 vol-%, c) the two precursor gas mixtures (VG1, VG2) are kept separate before passing into the reaction zone and are introduced substantially radially relative to the longitudinal axis of the reactor at a process temperature in the CVD reactor in the range of 600° C. to 850° C. and a process pressure in the CVD reactor in the range of 0.2 to 18 kPa, wherein the ratio of the volume gas flows ({dot over (V)}) of the precursor gas mixtures (VG1, VG2){dot over (V)}(VG1)/{dot over (V)}(VG2) is less than 1.5. 2. A process according to claim 1 , wherein the process includes at least one of: the process temperature in the CVD reactor is in the range of 650° C. to 800° C. and the process pressure in the CVD reactor is in the range of 0.2 to 7 kPa. 3. A process according to claim 1 , wherein the ratio of the volume gas flows ({dot over (V)}) of the precursor gas mixtures (VG1, VG2){dot over (V)}(VG1)/{dot over (V)}(VG2) is less than 1.25. 4. A process according to claim 1 , wherein the concentration of TiCl 4 in the precursor gas mixture (VG1) and the concentration of N-donor in the precursor gas mixture (VG2) are so set that the molar ratio of Ti to N in the volume gas flows {dot over (V)}(VG1) and {dot over (V)}(VG2) introduced into the reactor in stage c) is ≤0.25. 5. A process according to claim 1 , wherein the second precursor gas mixture (VG2) contains ≤1.0 vol-% of the N-donor. 6. A process according to claim 1 , wherein the N-donor is ammonia (NH 3 ). 7. A process according to claim 1 , wherein the wear-protection coating is subjected to a blasting treatment with a particulate blasting agent under conditions such that the Ti 1-x Al x C y N z layer after the blasting treatment has residual stresses in the range of +300 to −5000 MPa. 8. A tool having a base body of carbide, cermet, ceramic, steel or high speed steel and a single-layer or multi-layer wear-protection coating applied thereto in a CVD process, wherein the wear-protection coating includes at least one Ti 1-x Al x C y N z layer having stoichiometry coefficients 0.70≤x<1, 0<y<0.25 and 0.75≤z<1.15, and wherein the Ti 1-x Al x C y N z layer is of a thickness of 1 μm to 25 μm and has a crystallographic preferential orientation, which is characterised by a ratio of the intensities of the X-ray diffraction peaks of the crystallographic {111} plane and the {200} plane, wherein I{111}/I{200}>1+h (ln h) 2 , wherein h is the thickness of the Ti 1-x Al x C y N z layer in micrometers. 9. A tool according to claim 8 , wherein the full-width half-maximum (FWHM) of the X-ray diffraction peak of the {111} plane of the Ti 1-x Al x C y N z layer is <1%. 10. A tool according to claim 8 , wherein the Ti 1-x Al x C y N z layer has at least 90 vol-% Ti 1-x Al x C y N z phase with a cubically face-centred (fcc) lattice. 11. A tool according to claim 8 , wherein the Ti 1-x Al x C y N z layer has stoichiometry coefficients 0.70≤x<1, y=0 and 0.95≤z<1.15. 12. A tool according to claim 8 , wherein the Ti 1-x Al x C y N z layer has a thickness in the range of 3 μm to 20 μm. 13. A tool according to claim 8 , wherein the ratio of the intensities of the X-ray diffraction peaks of the crystallographic {111} plane and the {200} plane of the Ti 1-x Al x C y N z layer is >1+(h+3)x(ln h) 2 . 14. A tool according to claim 8 , wherein the Ti 1-x Al x C y N z layer has a Vickers hardness (HV)>2300 HV. 15. A tool according to claim 8 , wherein the wear-protection coating includes at least one of: arranged between the base body and the Ti 1-x Al x C y N z layer, at least one layer selected from a TiN layer, a TiCN layer deposited by means of high temperature CVD (CVD) or medium temperature CVD (MT-CVD), an Al 2 O 3 layer and combinations thereof, and arranged over the Ti 1-x Al x C y N z layer, at least one hard material layer. 16. A tool according to claim 8 , wherein an absolute maximum, measured radiographically or by means of EBSD, of the diffraction intensity of the crystallographic {111} planes of the fcc Ti 1-x Al x C y N z layer is within an angle range of α=±10°, starting from the normal direction of the sample surface. 17. A tool including a base body of carbide, cermet, ceramic, steel or high speed steel and a single-layer or multi-layer wear-protection coating applied thereto in a CVD process, wherein the wear-protection coating includes at least one Ti 1-x Al x C y N z layer having stoichiometry coefficients 0.70<x<1, 0<y<0.25 and 0.75<z<1.15, and wherein the Ti 1-x Al x C y N z layer is of a thickness of 1 μm to 25 μm and has a crystallographic preferential orientation, which is characterised by a ratio of the intensities of the X-ray diffraction peaks of the crystallographic {111} plane and the {200} plane, wherein l{111}/l{200}>1+h (ln h) 2 , wherein h is the thickness of the Ti 1-x Al x C y N z layer in micrometers, produced according to claim 1 . 18. A process according to claim 2 , wherein the process includes at least one of: the process temperature in the CVD reactor is in the range of 657° C. to 750° C. and the process pressure in the CVD reactor is in the range of 0.4 to 1.8 kPa. 19. A process according to claim 5 , wherein the second precursor gas mixture (VG2) contains <0.6 vol-% of the N-donor. 20. A process according to claim 7 , wherein the Ti 1-x Al x C y N z layer after the blasting treatment has residual stresses in the range of −1 to −3500 MPa. 21. A tool according to claim 9 , wherein the full-width half-maximum (FWHM) of the X-ray diffraction peak of the {111} plane of the Ti 1-x Al x C y N z layer is <0.6%. 22. A tool according to claim 10 , wherein the Ti 1-x Al x C y N z layer has at least 98 vol-% Ti 1-x Al x C y N z phase with a cubically face-centred (fcc) lattice. 23. A tool according to claim 14 , wherein the Ti 1-x Al x C y N z layer has a Vickers hardness (HV) in the range of 27
characterised by the method of coating (C23C16/04 takes precedence) · CPC title
Nitrides {(C23C16/303 takes precedence)} · CPC title
Radial flow · CPC title
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