Hard titanium aluminum nitride coating, hard-coated tool, and their production methods
10767258 ยท 2020-09-08
Assignee
Inventors
Cpc classification
B23B27/148
PERFORMING OPERATIONS; TRANSPORTING
C23C16/45514
CHEMISTRY; METALLURGY
C23C28/044
CHEMISTRY; METALLURGY
International classification
B23B27/14
PERFORMING OPERATIONS; TRANSPORTING
C23C16/455
CHEMISTRY; METALLURGY
Abstract
A titanium aluminum nitride coating having a columnar crystal structure, which is formed on a substrate, comprises high-Al TiAlN having an fcc structure, which has a composition represented by (Tix.sub.1, Aly.sub.1)N, wherein x.sub.1 and y.sub.1 are numbers meeting x.sub.1=0.005-0.1, and y.sub.1=0.995-0.9 by atomic ratio, and network-like, high-Ti TiAlN having an fcc structure, which has a composition represented by (Tix.sub.2, Aly.sub.2)N, wherein x.sub.2 and y.sub.2 are numbers meeting x.sub.2=0.5-0.9, and y.sub.2=0.5-0.1 by atomic ratio; the high-Al TiAlN being surrounded by the network-like, high-Ti TiAlN.
Claims
1. A hard titanium aluminum nitride coating having a columnar crystal structure, and comprising high-Al TiAlN having an fcc structure, which has a composition represented by (Tix.sub.1, Aly.sub.1)N, wherein x.sub.1 and y.sub.1 are numbers meeting x.sub.1=0.005-0.1, and y.sub.1=0.995-0.9 by atomic ratio, and network-like, high-Ti TiAlN having an fcc structure, which has a composition represented by (Tix.sub.2, Aly.sub.2)N, wherein x.sub.2 and y.sub.2 are numbers meeting x.sub.2=0.5-0.9, and y.sub.2=0.5-0.1 by atomic ratio; said high-Al TiAlN being surrounded by said network-like, high-Ti TiAlN, wherein said network-like means that said high-Ti TiAlN is distributed in a network form in a photomicrograph.
2. The hard titanium aluminum nitride coating according to claim 1, wherein said high-Al TiAlN has an average longitudinal cross section diameter of 2-50 nm and an average transverse cross section diameter of 10-300 nm.
3. The hard titanium aluminum nitride coating according to claim 1, wherein said columnar crystal has an average lateral cross section diameter of 0.1-1.2 m.
4. A hard-coated tool having a hard titanium aluminum nitride coating formed on a substrate, wherein said hard titanium aluminum nitride coating has a columnar crystal structure, and comprises high-Al TiAlN having an fcc structure, which has a composition represented by (Tix.sub.1, Aly.sub.1)N, wherein x.sub.1 and y.sub.1 are numbers meeting x.sub.1=0.005-0.1, and y.sub.1=0.995-0.9 by atomic ratio, and network-like, high-Ti TiAlN having an fcc structure, which has a composition represented by (Tix.sub.2, Aly.sub.1)N, wherein x.sub.2 and y.sub.2 are numbers meeting x.sub.2=0.5-0.9, and y.sub.2=0.5-0.1 by atomic ratio; said high-Al TiAlN being surrounded by said network-like, high-Ti TiAlN, wherein said network-like means that said high-Ti TiAlN is distributed in a network form in a photomicrograph.
5. The hard-coated tool according to claim 4, wherein said high-Al TiAlN has an average longitudinal cross section diameter of 2-50 nm and an average transverse cross section diameter of 10-300 nm.
6. The hard-coated tool according to claim 4, wherein said columnar crystal has an average lateral cross section diameter of 0.1-1.2 m.
7. A method for producing a hard titanium aluminum nitride coating by chemical vapor deposition, comprising (1) using a mixture gas A comprising a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas, and a mixture gas B comprising an NH.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas as starting material gases; (2) rotating first and second nozzles arranged with different distances from a rotation axis; and (3) ejecting said mixture gas A and said mixture gas B separately from said first and second nozzles.
8. The method for producing a hard titanium aluminum nitride coating according to claim 7, wherein with the total amount of said mixture gases A and B as 100% by volume, the composition of said mixture gas A comprises 0.02-0.31% by volume of a TiCl.sub.4 gas, 0.15-0.8% by volume of an AlCl.sub.3 gas, and 3-40% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, and the composition of said mixture gas B comprises 0.4-1.9% by volume of an NH.sub.3 gas, and 2-26% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas; and wherein a volume ratio H.sub.2(A)/H.sub.2(B) of the H.sub.2 gas in said mixture gas A to the H.sub.2 gas in said mixture gas B is 1-5.
9. The method for producing a hard titanium aluminum nitride coating according to claim 7, wherein the distance H.sub.1 from an opening of said first nozzle to said rotation axis is longer than the distance H.sub.2 from an opening of said second nozzle to said rotation axis; and wherein said mixture gas A is ejected from said first nozzle, and said mixture gas B is ejected from said second nozzle.
10. The method for producing a hard titanium aluminum nitride coating according to claim 7, wherein the distance H.sub.1 from an opening of said first nozzle to said rotation axis is longer than the distance H.sub.2 from an opening of said second nozzle to said rotation axis; and wherein said mixture gas B is ejected from said first nozzle, and said mixture gas A is ejected from said second nozzle.
11. The method for producing a hard titanium aluminum nitride coating according to claim 9, wherein a ratio H.sub.1/H.sub.2 of the distance H.sub.1 from an opening of said first nozzle to said rotation axis to the distance H.sub.2 from an opening of said second nozzle to said rotation axis is in a range of 1.5-3.
12. The method for producing a hard titanium aluminum nitride coating according to claim 7, wherein the reaction pressure is 3-6 kPa, and the reaction temperature is 750-830 C.
13. A method for producing a hard-coated tool having a hard titanium aluminum nitride coating by chemical vapor deposition, comprising (1) using a mixture gas A comprising a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas, and a mixture gas B comprising an NH.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas as starting material gases; (2) rotating first and second nozzles arranged with different distances from a rotation axis; (3) disposing a tool substrate around said first and second nozzles; and (4) ejecting said mixture gas A and said mixture gas B separately from said first and second nozzles.
14. The method for producing a hard-coated tool according to claim 13, wherein with the total amount of said mixture gases A and B as 100% by volume, the composition of said mixture gas A comprises 0.02-0.31% by volume of a TiCl.sub.4 gas, 0.15-0.8% by volume of an AlCl.sub.3 gas, and 3-40% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, and the composition of said mixture gas B comprises 0.4-1.9% by volume of an NH.sub.3 gas, and 2-26% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas; and wherein a volume ratio H.sub.2(A)/H.sub.2(B) of the H.sub.2 gas in said mixture gas A to the H.sub.2 gas in said mixture gas B is 1-5.
15. The method for producing a hard-coated tool according to claim 13, wherein the distance H.sub.1 from an opening of said first nozzle to said rotation axis is longer than the distance H.sub.2 from an opening of said second nozzle to said rotation axis; and wherein said mixture gas A is ejected from said first nozzle, and said mixture gas B is ejected from said second nozzle.
16. The method for producing a hard-coated tool according to claim 13, wherein the distance H.sub.1 from an opening of said first nozzle to said rotation axis is longer than the distance H.sub.2 from an opening of said second nozzle to said rotation axis; and wherein said mixture gas B is ejected from said first nozzle, and said mixture gas A is ejected from said second nozzle.
17. The method for producing a hard-coated tool according to claim 15, wherein a ratio H.sub.1/H.sub.2 of the distance H.sub.1 from an opening of said first nozzle to said rotation axis to the distance H.sub.2 from an opening of said second nozzle to said rotation axis is in a range of 1.5-3.
18. The method for producing a hard-coated tool according to claim 13, wherein the reaction pressure is 3-6 kPa, and the reaction temperature is 750-830 C.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DESCRIPTION OF THE PREFERRED EMBODIMENTS
(18) [1] Hard-Coated Tool
(19) The hard-coated tool of the present invention has a hard titanium aluminum nitride coating having a columnar crystal structure, which is formed on a tool substrate by chemical vapor deposition, the hard titanium aluminum nitride coating having a structure comprising high-Al TiAlN having an fcc structure, which has a composition represented by (Tix.sub.1, Aly.sub.1)N, wherein x.sub.1 and y.sub.1 are numbers meeting x.sub.1=0.005-0.1, and y.sub.1=0.995-0.9 by atomic ratio, and network-like, high-Ti TiAlN having an fcc structure, which has a composition represented by (Tix.sub.2, Aly.sub.2)N, wherein x.sub.2 and y.sub.2 are numbers meeting x.sub.2=0.5-0.9, and y.sub.2=0.5-0.1 by atomic ratio; the high-Al TiAlN being surrounded by the network-like, high-Ti TiAlN.
(20) (A) Substrate
(21) The substrate should be a material having high heat resistance, to which chemical vapor deposition can be applied, for example, WC-based cemented carbide, cermet, high-speed steel, tool steel, ceramics such as cubic-boron-nitride-based sintered boron nitride (cBN) and sialon, etc. From the aspect of strength, hardness, wear resistance, toughness and thermal stability, WC-based cemented carbide, cermet and ceramics are preferable. In the case of WC-based cemented carbide, for example, the hard titanium aluminum nitride coating of the present invention may be formed on its as-sintered surfaces, but preferably on its worked surfaces (ground surface, cutting edge surface, etc.) to increase dimension precision.
(22) (B) Hard Titanium Aluminum Nitride Coating
(23) (1) Composition
(24) The hard titanium aluminum nitride coating of the present invention formed by chemical vapor deposition has a columnar crystal structure, and comprises Ti, Al and N as indispensable components. The composition of indispensable components in the hard titanium aluminum nitride coating of the present invention preferably comprises 4-22 atomic % of Ti, 48-23 atomic % of Al, and 48-55 atomic % of N, with the total amount of Ti, Al and N as 100 atomic %. Outside the above composition range, the desired microstructure cannot be obtained. The composition of indispensable components more preferably comprises 8-18 atomic % of Ti, 42-29 atomic % of Al, and 50-53 atomic % of N. 30 atomic % or less of N may be substituted by C or B. Though the hard titanium aluminum nitride coating of the present invention may contain Cl as an inevitable impurity, the Cl content is preferably 1.5 atomic % or less, more preferably 0.8 atomic % or less. The composition of the hard titanium aluminum nitride coating can be measured by EPMA.
(25) (a) Composition of High-Al TiAlN
(26) The high-Al TiAlN has a composition represented by the general formula of (Tix.sub.1, Aly.sub.1)N, wherein x.sub.1 and y.sub.1 are numbers meeting x.sub.1=0.005-0.1, and y.sub.1=0.995-0.9 by atomic ratio. The percentage x.sub.1 of Ti of less than 0.005 leading to too much Al causes the precipitation of an hcp structure, resulting in low hardness, and poor wear resistance at high temperatures. When x.sub.1 is more than 0.1, the hard titanium aluminum nitride coating has a fine granular crystal structure, having reduced oxidation resistance. For higher performance, the atomic ratio of (Tix.sub.1, Aly.sub.1) to N is preferably 0.3/0.7 to 0.7/0.3, more preferably 0.4/0.6 to 0.6/0.4.
(27) (b) Composition of High-Ti TiAlN
(28) The high-Ti TiAlN has a composition represented by the general formula of (Tix.sub.2, Aly.sub.2)N, wherein x.sub.2 and y.sub.2 are numbers meeting x.sub.2=0.5-0.9, and y.sub.2=0.5-0.1 by atomic ratio. The percentage x.sub.2 of Ti of less than 0.5 leading to too much Al causes the precipitation of an hcp structure, resulting in low hardness and wear resistance. The x.sub.2 of more than 0.9 leads to too little Al, resulting in drastically reduced oxidation resistance. For higher performance, the atomic ratio of (Tix.sub.2, Aly.sub.2) to N is preferably 0.3/0.7 to 0.7/0.3, more preferably 0.4/0.6 to 0.6/0.4.
(29) The compositions of high-Al TiAlN and high-Ti TiAlN can be determined by the measurement results of EDS described later.
(30) (2) High-Al TiAlN and High-Ti TiAlN
(31) (a) Structure
(32) As is clear from
(33) Though not necessarily clear, a reason why the hard titanium aluminum nitride coating of the present invention has higher performance than those of conventional hard titanium aluminum nitride coatings is considered as follows: Hard titanium aluminum nitride coatings formed by conventional chemical vapor deposition methods have structures in which TiAlN having different Al contents or TiN and AlN are alternately laminated. Because each layer in the laminate has fine granular crystal grains, there are a high percentage of crystal grain boundaries. When cutting is conducted by a tool having such hard titanium aluminum nitride coating, crystal grain boundaries act as paths for oxygen intrusion at cutting edges of the tool at elevated temperatures, so that oxidation is accelerated to drastically reduce wear resistance and oxidation resistance at high temperatures. Also, the fcc structure of high-Al TiAlN layers in the laminate is transformed to an hcp structure at high temperatures, causing interlayer delamination and thus resulting in a shorter life.
(34) On the other hand, in the hard titanium aluminum nitride coating of the present invention, high-Al TiAlN is surrounded by network-like, high-Ti TiAlN. Because the high-Al TiAlN surrounded by the network-like, high-Ti TiAlN acts as starting portions of coating growth, titanium aluminum nitride crystal grains grow predominantly in one direction, resulting in columnar crystals. Accordingly, even when the high-Al TiAlN having an fcc structure shrinks by transformation to an hcp structure at a temperature elevated by cutting, the breakage of the coating is suppressed by the surrounding network-like, high-Ti TiAlN having an fcc structure. Such characteristic microstructure is not owned by conventional hard titanium aluminum nitride coatings. Thus, the hard titanium aluminum nitride coating of the present invention has much higher high-temperature hardness than those of conventional hard titanium aluminum nitride coatings, resulting in excellent wear resistance. Also, because the hard titanium aluminum nitride coating of the present invention has a large Al content, and a columnar crystal structure having fewer crystal grain boundaries than a granular crystal structure, it is less oxidized (having excellent oxidation resistance). The microstructure having high-Al TiAlN surrounded by network-like, high-Ti TiAlN can be identified by the measurement results of nanobeam diffraction (see
(35) (b) Average Transverse and Longitudinal Cross Section Diameters of High-Al TiAlN
(36) The average transverse cross section diameter is an average of the maximum diameters of high-Al TiAlN portions in columnar crystal grains of the hard titanium aluminum nitride coating, in a TEM photograph of a cross section perpendicular to a substrate surface. The average longitudinal cross section diameter is an average of the maximum lengths of the high-Al TiAlN portions in directions perpendicular to the maximum diameters, in a TEM photograph of a cross section perpendicular to the substrate surface. Specifically, the average transverse cross section diameter of high-Al TiAlN is determined by arbitrarily selecting five high-Al TiAlN portions surrounded by network-like, high-Ti TiAlN in the TEM photograph (magnification: 200,000 times) of
(37) The high-Al TiAlN generally has a flat shape (see
(38) (3) Average Lateral Cross Section Diameter of Columnar Crystals in Hard Titanium Aluminum Nitride Coating
(39) The hard titanium aluminum nitride coating of the present invention has a columnar crystal structure. The average lateral cross section diameter of columnar crystals is an average diameter of cross sections of columnar crystal grains in a plane perpendicular to the substrate surface. To have high hardness and excellent wear resistance, the average lateral cross section diameter of columnar crystals is preferably 0.1-1.2 m, more preferably 0.2-1.0 m. At the average lateral cross section diameter of less than 0.1 m, a percentage of crystal grain boundaries to titanium aluminum nitride crystal grains is high, resulting in drastically reduced oxidation resistance at high temperatures. On the other hand, when the average lateral cross section diameter is more than 1.2 m, cracking occurs in crystal grains, resulting in the breakage of the coating. Specifically, the average lateral cross section diameter is determined by measuring the lateral cross section diameters of 10 arbitrary columnar crystal grains in a thickness-direction immediate portion of the hard titanium aluminum nitride coating on the SEM photograph of
(40) (4) Thickness of Hard Titanium Aluminum Nitride Coating
(41) To prevent peeling from the substrate while exhibiting excellent wear resistance and oxidation resistance, the thickness of the hard titanium aluminum nitride coating of the present invention is preferably 1-15 m, more preferably 2-12 m. The thickness of less than 1 m does not provide sufficient coating effects, and the thickness of more than 15 m likely causes cracking in the coating because of too much thickness. The thickness of the hard titanium aluminum nitride coating can be properly controlled by coating time. Because the hard coating and each layer constituting it are not completely flat, what is simply called thickness means an average thickness.
(42) (5) Hardness
(43) The hardness of the hard titanium aluminum nitride coating of the present invention measured by a nanoindentation method is preferably 33 GPa or more. When the hardness is less than 33 GPa, the hard titanium aluminum nitride coating has insufficient wear resistance. By industrial production, the hardness of 35-42 GPa can be achieved.
(44) (C) Underlayer
(45) Though not particularly restrictive, a Ti(CN) coating, a TiN coating or a TiZr(CN) coating is preferably formed by chemical vapor deposition as an underlayer for the hard titanium aluminum nitride coating of the present invention. A Ti(CN) coating has poor heat resistance at high temperatures despite excellent wear resistance, but its disadvantage of heat resistance can be overcome by forming the hard titanium aluminum nitride coating of the present invention thereon.
(46) The temperature of forming a Ti(CN) coating by chemical vapor deposition is 750-950 C., substantially equal to the preferred coating temperature (750-830 C.) of the hard titanium aluminum nitride coating of the present invention, resulting in high industrial productivity. In the hard-coated tool of the present invention, an adhesion-increasing intermediate layer may be formed between the hard titanium aluminum nitride coating and the Ti(CN) coating. The intermediate layer is preferably a TiN coating or a TiAl(CN) coating.
(47) (d) Upper Layer
(48) Though not particularly restrictive, a single- or multi-layer hard coating indispensably comprising at least one element selected from the group consisting of Ti, Al, Cr, B and Zr, and at least one element selected from the group consisting of C, N and O may be formed by chemical vapor deposition, as an upper layer on the hard titanium aluminum nitride coating of the present invention. The upper layer is a single- or multi-layer coating of, for example, TiC, CrC, SiC, VC, ZrC, TiN, AlN, CrN, Si.sub.3N.sub.4, VN, ZrN, Ti(CN), (TiSi) N, (TiB)N, TiZrN, TiAl(CN), TiSi(CN), TiCr(CN), TiZr(CN), Ti(CNO), TiAl(CNO), Ti(CO), TiB.sub.2, etc.
(49) [2] Chemical Vapor Deposition Apparatus
(50) The hard titanium aluminum nitride coating of the present invention can be formed by chemical vapor deposition, using a thermal or plasma-enhanced chemical vapor deposition apparatus (CVD furnace). As shown in
(51) [3] Production Method
(52) The production method of the hard titanium aluminum nitride coating of the present invention will be explained in detail below, taking a case of using a thermal vapor deposition method for example, but it should be noted that the present invention is not restricted thereto, and that other chemical vapor deposition methods can be used.
(53) (A) Formation of Underlayer (Titanium Carbonitride Coating)
(54) An H.sub.2 gas, an N.sub.2 gas, and/or an Ar gas are introduced into a CVD furnace in which substrates are set, and after heated to the coating temperature, a starting material gas comprising a TiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas (or a CH.sub.3CN gas and a C.sub.2H.sub.6 gas), and an H.sub.2 gas are introduced into the CVD furnace to form a titanium carbonitride underlayer.
(55) (1) Starting Material Gas for l-Ti(CN) Coating
(56) The composition of a starting material gas for forming an l-Ti(CN) coating having a columnar crystal structure as an example of the underlayers preferably comprises 0.8-3% by volume of a TiCl.sub.4 gas, 10-30% by volume of an N.sub.2 gas, and 0.1-1.2% by volume of a CH.sub.3CN gas, the balance being an H.sub.2 gas, their total amount being 100% by volume. With the amounts of a TiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas and an H.sub.2 gas outside the above ranges, the resultant titanium carbonitride coating has too high a carbon concentration, or contains too large columnar crystal grains, resulting in low adhesion to an upper hard titanium aluminum nitride layer.
(57) (B) Formation of Hard Titanium Aluminum Nitride Coating
(58) (1) Starting Material Gases for Hard Titanium Aluminum Nitride Coating
(59) As starting material gases for forming the hard titanium aluminum nitride coating, a mixture gas A comprising a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas, and a mixture gas B comprising an NH.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas are used. It is preferable that with the total amount of a TiCl.sub.4 gas, an AlCl.sub.3 gas, an NH.sub.3 gas, an N.sub.2 gas, and an H.sub.2 gas as 100% by volume, the composition of the mixture gas A comprises 0.02-0.31% by volume of a TiCl.sub.4 gas, 0.15-0.8% by volume of an AlCl.sub.3 gas, and 3-40% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, and the composition of the mixture gas B comprises 0.4-1.9% by volume of an NH.sub.3 gas, and 2-26% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, a volume ratio H.sub.2(A)/H.sub.2(B) of the H.sub.2 gas in the mixture gas A to the H.sub.2 gas in the mixture gas B being 1-5. At any volume ratio H.sub.2(A)/H.sub.2(B) of less than 1 or more than 5, the reaction speed of the starting material gas is uneven, providing hard titanium aluminum nitride coatings formed on substrates set in the CVD furnace with poor thickness distributions. In the mixture gases A, B, part of the H.sub.2 gas as a carrier gas may be substituted by an Ar gas. More preferably, the composition of the mixture gas A comprises 0.02-0.31% by volume of a TiCl.sub.4 gas, 0.15-0.8% by volume of an AlCl.sub.3 gas, and 4.9-21.8% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, and the composition of the mixture gas B comprises 0.7-1.9% by volume of an NH.sub.3 gas, and 3-16.5% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas. Further preferably, the composition of the mixture gas A comprises 0.1-0.2% by volume of a TiCl.sub.4 gas, 0.3-0.5% by volume of an AlCl.sub.3 gas, and 4.9-21.8% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas, and the composition of the mixture gas B comprises 0.8-1.3% by volume of an NH.sub.3 gas, and 3-16.5% by volume of an N.sub.2 gas, the balance being an H.sub.2 gas. The volume ratio H.sub.2(A)/H.sub.2(B) is more preferably 1.5-4.8.
(60) (a) Mixture Gas A
(61) When the TiCl.sub.4 gas is less than 0.02% by volume, the amount of Al is too large in the mixture gas A, so that an hcp structure is precipitated, resulting in a hard titanium aluminum nitride coating having low hardness. On the other hand, when the TiCl.sub.4 gas is more than 0.31% by volume, the resultant hard titanium aluminum nitride coating does not have the microstructure of the present invention.
(62) When the AlCl.sub.3 gas is less than 0.15% by volume, the hard titanium aluminum nitride coating contains too small an amount of Al, having low oxidation resistance. When the AlCl.sub.3 gas is more than 0.8% by volume, the hard titanium aluminum nitride coating contains too large an amount of Al, having an hcp structure precipitated, and thus low wear resistance.
(63) When the N.sub.2 gas is either less than 3% by volume or more than 40% by volume, the reaction speed of starting material gases is uneven, so that hard titanium aluminum nitride coatings having a poor thickness distribution are formed on substrates set in a CVD furnace.
(64) (b) Mixture Gas B
(65) When the NH.sub.3 gas is either less than 0.4% by volume or more than 1.9% by volume in the mixture gas B, the reaction speed is uneven, failing to obtain a microstructure peculiar to the present invention.
(66) When the N.sub.2 gas is either less than 2% by volume or more than 26% by volume, the reaction speed of starting material gases is uneven, so that hard titanium aluminum nitride coatings having a poor thickness distribution are formed on substrates set in a CVD furnace.
(67) (2) Method of Introducing Starting Material Gases
(68) To form a microstructure in which high-Al TiAlN having an fcc structure is surrounded by network-like, high-Ti TiAlN having an fcc structure, by mixing highly reactive mixture gases A and B to control their reaction speed, the mixture gases A and B should be introduced into a CVD furnace 1 without contact. For this purpose, for example, a CVD furnace 1 comprising a pipe assembly 30, in which three pipes 11, 11, 12 in total are fixed as shown in
(69) The mixture gases A and B should be separately introduced into the CVD furnace 1, without hindering the flow of the mixture gases A, B ejected from each nozzle. To this end, as exemplified in
(70) To obtain the characteristic microstructure of the present invention, the nozzles 11a, 12a introducing the mixture gases A, B are preferably rotated at a speed of 2-4 rpm. The rotation directions of the first and second nozzles 11a, 12a are not restricted.
(71)
(72) To obtain the characteristic microstructure of the present invention, a ratio H.sub.1/H.sub.2 of the distance H.sub.1 from an opening of a first nozzle 11a to the rotation axis O to the distance H.sub.2 from an opening of a second nozzle 12a to the rotation axis O is preferably in a range of 1.5-3.
(73) (a) First Pipe Assembly
(74)
(75) The first pipe 11 has a radius R.sub.1, and the second pipe 12 has a radius R.sub.2. The center axis O.sub.1 of the first pipe 11 is positioned on a circle C.sub.1 having a first diameter D.sub.1 around the rotation axis O. Accordingly, two first pipes 11, 11 are positioned at equal distance from the rotation axis O. A center angle of the center axes O.sub.1, O.sub.1 of the first pipes 11, 11 to the rotation axis O is preferably 90-180. The center axis O.sub.2 of the second pipe 12 is at the same position as that of the rotation axis O, and an outer periphery of the second pipe 12 is on a circle C.sub.2 having a second diameter D.sub.2 (=2R.sub.2) around the rotation axis O.
(76) The nozzles (first nozzles) 11a, 11a of the first pipes 11, 11 are directed outward in a just opposite direction (180 direction). Though each first pipe 11 has a vertical line of nozzles (first nozzles) 11a in the depicted example, it is not restrictive, but the first nozzles 11a may be aligned along plural lines. The second pipe 12 has two vertical lines of nozzles (second nozzles) 12a, 12a arranged in a diametrical direction (180 direction). Of course, the second nozzles 12a are not restricted to two lines, but may be in one line. Because the first diameter D.sub.1 is larger than the second diameter D.sub.2 [D.sub.12 (R.sub.1+R.sub.2)], the first nozzles 11a, 11a are located outside, and the second nozzles 12a, 12a are located inside, when the pipe assembly 30 is rotated around the rotation axis O.
(77) When the second pipe 12 has a line of second nozzles 12a, and the center angle of the center axes O.sub.1, O.sub.1 of the first pipes 11, 11 is less than 180, the second nozzles 12a are directed preferably in a distant direction (opposite to the center angle ) from the first nozzles 11a, 11a. In this case, the ejection direction of the first nozzles 11a is preferably perpendicular to the ejection direction of the second nozzles 12a.
(78) It is preferable that when the center axes O.sub.1, O.sub.1 of the first pipes 11, 11 and the center axis O.sub.2 of the second pipe 12 are on the same line, and when the second pipe 12 has two lines of second nozzles 12a, 12a, the first nozzles 11a, 11a are directed outward oppositely (180 direction), and the second nozzles 12a are directed oppositely and perpendicularly to the first nozzles 11a, 11a (at a center angle of 90).
(79) (b) Second Pipe Assembly
(80)
(81) The center axis O.sub.2 of the second pipe 12 is at the same position as that of the rotation axis O of the pipe assembly 40, with the first pipe 11 positioned near the second pipe 12. The first pipe 11 has a radius R.sub.1, and the second pipe 12 has a radius R.sub.2. The center axis O.sub.1 of the first pipe 11 is positioned on a circle C.sub.1 having a first diameter D.sub.1 around the rotation axis O. The second pipe 12 has a center axis O.sub.2 at the same position as that of the rotation axis O, and its periphery coincides a circle C.sub.2 having a second diameter D.sub.2 (=2R.sub.2) around the rotation axis O. Because the first diameter D.sub.1 is larger than the second diameter D.sub.2 [D.sub.12 (R.sub.1+R.sub.2)], the first nozzle 11a is located outside, while the second nozzle 12a is located inside, when the pipe assembly 40 is rotated around the rotation axis O.
(82) Though the nozzles (first nozzles) 11a of the first pipe 11 and the second nozzles 12a of the second pipe 12 are directed oppositely (180 direction) in the depicted example, it is of course not restricted as long as a center angle of the first nozzle 11a and the second nozzle 12a is within 90-180.
(83) (c) Third Pipe Assembly
(84)
(85) The first pipe 11 has a radius R.sub.1, and the second pipe 12 has a radius R.sub.2. The center axis O.sub.1 of each first pipe 11 is positioned on a circle C.sub.1 having a first diameter D.sub.1 around the rotation axis O. Accordingly, four first pipes 11, 11, 11, 11 are located at equal distance from the rotation axis O. The center axis O.sub.2 of the second pipe 12 is at the same position as that of the rotation axis O, with its periphery located on a circle C.sub.2 having a second diameter D.sub.2 (=2R.sub.2) around the rotation axis O. Because the first diameter D.sub.1 is larger than the second diameter D.sub.2 [D.sub.12 (R.sub.1+R.sub.2)], the first nozzles 11a, 11a, 11a, 11a are outside, while the second nozzles 12a, 12a, 12a, 12a are inside, when the pipe assembly 50 is rotated around the rotation axis O. Though a center angle of the center axes O.sub.1, O.sub.1 of the adjacent first pipes 11, 11 to the rotation axis O is 90 in the depicted example, it is not restricted but may be 60-120.
(86) (3) Coating-Forming Temperature
(87) The temperature of forming the hard titanium aluminum nitride coating is preferably 750-830 C. When the coating-forming temperature is lower than 750 C., the resultant hard titanium aluminum nitride coating has too high a chlorine content, resulting in low hardness. On the other hand, when the coating-forming temperature exceeds 830 C., the reaction is too accelerated, forming a granular crystal structure, and thus resulting in poor oxidation resistance.
(88) (3) Reaction Pressure
(89) The reaction pressure of forming the hard titanium aluminum nitride coating is preferably 3-6 kPa. When the reaction pressure is less than 3 kPa, the above characteristic microstructure cannot be obtained. On the other hand, when the reaction pressure exceeds 6 kPa, the resultant hard titanium aluminum nitride coating has a granular crystal structure, and thus poor oxidation resistance.
(90) (C) Formation of Upper Layers (Hard Coatings)
(91) Though not particularly restrictive, upper layers may be formed on the hard titanium aluminum nitride coating by a known chemical vapor deposition method. The upper-layer-forming temperature may be 700-830 C. Starting material gases used for forming the upper layers are exemplified as follows:
(92) 1. TiC coating: a TiCl.sub.4 gas, a CH.sub.4 gas, and an H.sub.2 gas.
(93) 2. CrC coating: a CrCl.sub.3 gas, a CH.sub.4 gas, and an H.sub.2 gas.
(94) 3. SiC coating: a SiCl.sub.4 gas, a CH.sub.4 gas, and an H.sub.2 gas.
(95) 4. VC coating: a VCl gas, a CH.sub.4 gas, and an H.sub.2 gas.
(96) 5. ZrC coating: a ZrCl.sub.4 gas, a CH.sub.4 gas, and an H.sub.2 gas.
(97) 6. TiN coating: a TiCl.sub.4 gas, an N.sub.2 gas, and an H.sub.2 gas.
(98) 7. AN coating: an AlCl.sub.3 gas, an NH.sub.3 gas, and an H.sub.2 gas.
(99) 8. CrN coating: a CrCl.sub.3 gas, an NH.sub.3 gas, and an H.sub.2 gas.
(100) 9. Si.sub.3N.sub.4 coating: a SiCl.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas.
(101) 10. VN coating: a VCl.sub.3 gas, an NH.sub.3 gas, and an H.sub.2 gas.
(102) 11. ZrN coating: a ZrCl.sub.4 gas, an N.sub.2 gas, and an H.sub.2 gas.
(103) 12. Ti(CN) coating: a TiCl.sub.4 gas, a CH.sub.4 gas, an N.sub.2 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a CH.sub.3CN gas, an N.sub.2 gas, and an H.sub.2 gas.
(104) 13. (TiSi)N coating: a TiCl.sub.4 gas, a SiCl.sub.4 gas, an N.sub.2 gas, and an NH.sub.3 gas.
(105) 14. (TiB)N coating: a TiCl.sub.4 gas, an N.sub.2 gas, and a BCl.sub.3 gas.
(106) 15. TiZr(CN) coating: a TiCl.sub.4 gas, a ZrCl.sub.4 gas, an N.sub.2 gas, a CH.sub.4 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a ZrCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(107) 16. TiAl(CN) coating: a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, a CH.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(108) 17. TiSi(CN) coating: a TiCl.sub.4 gas, a SiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a SiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(109) 18. TiCr(CN) coating: a TiCl.sub.4 gas, a CrCl.sub.3 gas, an N.sub.2 gas, a CH.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a CrCl.sub.3 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(110) 19. TiV(CN) coating: a TiCl.sub.4 gas, a VCl.sub.3 gas, an N.sub.2 gas, a CH.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a VCl.sub.3 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(111) 20. TiZr(CN) coating: a TiCl.sub.4 gas, a ZrCl.sub.4 gas, an N.sub.2 gas, a CH.sub.4 gas, an NH.sub.3 gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, a ZrCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas, and an H.sub.2 gas.
(112) 21. Ti(CNO) coating: a TiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.4 gas, a CO gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.3CN gas, a CO gas, and an H.sub.2 gas.
(113) 22. TiAl(CNO) coating: a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, a CH.sub.4 gas, a CO gas, and an H.sub.2 gas, or a TiCl.sub.4 gas, an AlCl.sub.3 gas, an N.sub.2 gas, a CH.sub.3CN gas, a CO gas, and an H.sub.2 gas.
(114) 23. Ti(CO) coating: a TiCl.sub.4 gas, an N.sub.2 gas, a CH.sub.4 gas, a CO gas, a CO.sub.2 gas, and an H.sub.2 gas.
(115) 24. TiB.sub.2 coating: a TiCl.sub.4 gas, a BCl.sub.3 gas, and an H.sub.2 gas.
(116) (D) Treatment of Cutting Edge after Forming Hard Coating
(117) The hard titanium aluminum nitride coating formed on the substrate is smoothed by brushing, buffing, blasting, etc., to achieve a surface state having excellent chipping resistance. Particularly when a hard-coated cutting edge is treated by wet or dry blasting using ceramic powder of alumina, zirconia, silica, etc., the hard coating is provided with smoothed surface and reduced residual tensile stress, thereby getting improved chipping resistance.
(118) The present invention will be explained in further detail by Examples below, of course without intention of restricting the present invention thereto. In Examples and Comparative Examples below, the flow rate (L/minute) is expressed by L per every minute at 1 atom and 25 C., and the thickness is expressed by an average value.
Example 1
(119) (1) Formation of Hard Coating
(120) Milling insert substrates (WDNW140520-B) of WC-based cemented carbide comprising 11.5% by mass of Co, 2.0% by mass of TaC, and 0.7% by mass of CrC, the balance being WC and inevitable impurities, which are schematically shown in
(121) Introduced into the CVD furnace 1 using the pipe assembly 30 shown in
(122) (2) Measurement of Thickness
(123) The thicknesses of the titanium carbonitride coating and the hard titanium aluminum nitride coating of each hard-coated tool were measured by the following procedure. Each coating surface was lapped slantingly at an angle of 5 to obtain a lapped surface, and the lapped surface exposing the thickness-direction cross sections of the hard coatings was observed by an optical microscope of 1,000 times at five arbitrary points to measure the thickness of each layer, and the measured thicknesses were arithmetically averaged. The results are shown in Table 2.
(124) (3) Identification of Crystal Structure
(125) To identify the crystal structure, CuK.sub.1 rays (wavelength : 0.15405 nm) were projected onto a hard coating surface on a rake face of the property-evaluating insert (SNMN120408) at tube voltage of 45 kV and tube current of 40 mA, by an X-ray diffraction apparatus (EMPYREAN available from PANalytical). The X-ray diffraction pattern obtained in a 2 range of 20-80 is shown in
(126) (4) Microstructure (High-Al TiAlN and High-Ti TiAlN) of Hard Titanium Aluminum Nitride Coating
(127) On the fractured surface (hard titanium aluminum nitride coating, etc.) of each hard-coated tool, microstructure observation was conducted by SEM (S-4200 available from Hitachi, Ltd.) and a field-emission transmission electron microscope FE-TEM (JEM-2010F available from JEOL Ltd.), and mapping analysis was conducted by an energy-dispersive X-ray spectrometer EDS (UTW-type Si (Li) semiconductor detector available from NORAN) attached to JEM-2010F.
(128)
(129)
(130)
(131)
(132) It was found from
(133) (6) Measurement of Composition
(134) In a cross section of the property-evaluating insert (SNMN120408), the composition of the hard titanium aluminum nitride coating was measured at five arbitrary points at its thickness-direction center by an electron probe microanalyzer EPMA (JXA-8500F available from JEOL, Ltd.), under the conditions of acceleration voltage of 10 kV, irradiation current of 0.05 A, and a beam diameter of 0.5 m. The measured values were arithmetically averaged to determine the composition of the hard titanium aluminum nitride coating. The results are shown in Table 2.
(135) In a cross section of the hard coating of the property-evaluating insert (SNMN120408), the compositions of high-Al TiAlN grains and high-Ti TiAlN grains in the hard titanium aluminum nitride coating were analyzed at five arbitrary points at a thickness-direction center of the above coating, by an energy-dispersive X-ray spectrometer EDS [UTW-type Si (Li) semiconductor detector available from NORAN, beam diameter: about 1 nm] attached to FE-TEM (JEM-2010F), and the measured values were arithmetically averaged. The results are shown in Table 3.
(136) (7) Measurement of Hardness
(137) The surface hardness of the hard coating was measured 5 times by a nanoindentation method using a nanoindentation hardness tester (ENT-1100 available from Elionix Inc.) with a Si single crystal as a standard sample, at a maximum load of 4900 mN, and a load speed of 49 mN/second, for a keeping time of 1 second, and arithmetically averaged. The results are shown in Table 2.
(138) (8) Evaluation of Performance
(139) Each milling insert 60 was fixed to a tip portion 72 of a tool body 71 of the indexable rotary cutting tool (ASRT5063R-4) 70 shown in
(140) Work: SCM440 having hardness of 32HRC,
(141) Machining method: Milling,
(142) Insert shape: WDNT140520-B,
(143) Cutting speed: 175 m/minute,
(144) Number of revolution: 885 rpm,
(145) Feed speed per one tooth: 1.50 mm/tooth,
(146) Feed speed: 5310 mm/minute,
(147) Axial cutting depth: 1.0 mm,
(148) Radial cutting depth: 40 mm, and
(149) Cutting method: Dry cutting.
Examples 2-18
(150) Each hard-coated tool (milling insert) was produced in the same manner as in Example 1 except for changing the coating conditions of the hard titanium aluminum nitride coating as shown in Tables 1-1 and 1-2, and its properties and tool lives were evaluated. With respect to the hard titanium aluminum nitride coating of each Example, the measurement results of composition, crystal structure and form, thickness and hardness, as well as an average lateral cross section diameter of columnar crystals are shown in Table 2. The measurement results of composition, crystal structure, Dav and Daw of high-Al TiAlN and the composition and crystal structure of high-Ti TiAlN in each Example are shown in Table 3. The observation results of microstructure of high-Al TiAlN, etc. and the tool life in each Example are shown in Table 4. It is clear from Tables 2-4 that each hard titanium aluminum nitride coating of Examples 2-18 has a columnar crystal structure in which high-Al TiAlN having an fcc structure is surrounded by network-like, high-Ti TiAlN having an fcc structure, as well as a good tool life, as in Example 1.
Example 19
(151) With the same milling insert substrates of WC-based cemented carbide as in Example 1 set in the CVD furnace 1, a mixture gas comprising 0.37% by volume of a TiCl.sub.4 gas, 54.34% by volume of an N.sub.2 gas and 45.29% by volume of an H.sub.2 gas at a flow rate of 55.2 L/minute was flown into the CVD furnace at 800 C. and 16 kPa, to form a titanium nitride coating having an average thickness of 0.2 m on the insert substrate.
(152) A 5-m-thick hard titanium aluminum nitride coating having a composition represented by Ti.sub.0.10Al.sub.0.40N.sub.0.50 (atomic ratio) was formed in the same manner as in Example 1, except for introducing the mixture gas A through the second nozzles 12a of the second pipe 12 and the mixture gas B through the first nozzles 11a, 11a of the first pipes 11, 11 into the CVD furnace 1, thereby producing the hard-coated tool of the present invention (milling insert).
(153) The properties and tool lives of the hard-coated tools were evaluated in the same manner as in Example 1. The measurement results of the composition, crystal structure and form, thickness and hardness of the hard titanium aluminum nitride coating, and the average lateral cross section diameter of columnar crystals are shown in Table 2. The measurement results of the composition, crystal structure, Dav and Daw of high-Al TiAlN, and the composition and crystal structure of high-Ti TiAlN are shown in Table 3. The observed microstructure of high-Al TiAlN, etc. and the tool life are shown in Table 4. It is clear from Tables 2-4 that the hard titanium aluminum nitride coating of Example 19 had a columnar crystal structure, in which high-Al TiAlN having an fcc structure was surrounded by network-like, high-Ti TiAlN having an fcc structure, as well as a good tool life, as in Example 1.
Comparative Example 1
(154) After forming a titanium carbonitride coating in the same manner as in Example 1, the nozzles 11a, 12a shown in
Comparative Example 2
(155) After forming a titanium carbonitride coating in the same manner as in Example 1, the nozzles 11a, 12a shown in
Comparative Example 3
(156) A hard titanium aluminum nitride coating was formed in the same manner as in Example 1, except that the nozzles 11a, 12a shown in
(157) As shown in Table 4, in any hard titanium aluminum nitride coatings of Comparative Examples 1-3, high-Al TiAlN was not surrounded by network-like, high-Ti TiAlN. The hard titanium aluminum nitride coatings of Comparative Examples 1-2 had granular crystal structures, though they had an fcc structure. The hard titanium aluminum nitride coating of Comparative Example 3 had a granular crystal structure in which hard titanium aluminum nitride layers having an fcc structure and hard titanium aluminum nitride layers having an fcc+hcp structure were alternately laminated.
(158) TABLE-US-00001 TABLE 1-1 Reaction Pressure Mixture-Gas-Ejecting Nozzle No. Temp. ( C.).sup.(1) (kPa) Apparatus Mixture Gas A Mixture Gas B Example 1 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 2 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 3 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 4 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 5 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 6 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 7 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 8 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 9 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 10 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 11 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 12 800 3 FIG. 12(a) First Nozzle Second Nozzle Example 13 800 5 FIG. 12(a) First Nozzle Second Nozzle Example 14 750 4 FIG. 12(a) First Nozzle Second Nozzle Example 15 830 4 FIG. 12(a) First Nozzle Second Nozzle Example 16 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 17 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 18 800 4 FIG. 12(a) First Nozzle Second Nozzle Example 19 800 4 FIG. 12(a) Second Nozzle First Nozzle Com. Ex. 1 850 6 FIG. 13 First Nozzle Second Nozzle Com. Ex. 2 800 1 FIG. 13 First Nozzle Second Nozzle Com. Ex. 3 800 1 FIG. 13 First Nozzle Second Nozzle Note: .sup.(1)Coating-forming temperature.
(159) TABLE-US-00002 TABLE 1-2 Starting Material Gas Composition (% by volume) Mixture Gas A Mixture Gas B H.sub.2(A)/ No. H.sub.2 N.sub.2 Ar TiCl.sub.4 AlCl.sub.3 H.sub.2 N.sub.2 NH.sub.3 H.sub.2(B).sup.(2) Example 1 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Example 2 60.26 6.28 0.00 0.13 0.38 25.74 6.28 0.93 2.34 Example 3 58.75 12.77 0.00 0.26 0.77 12.77 12.77 1.91 4.60 Example 4 38.19 21.82 0.00 0.11 0.33 22.37 16.37 0.81 1.71 Example 5 56.77 4.87 0.00 0.17 0.49 33.25 3.24 1.21 1.71 Example 6 52.58 7.51 0.00 0.02 0.45 30.80 7.51 1.13 1.71 Example 7 52.43 7.49 0.00 0.31 0.45 30.71 7.49 1.12 1.71 Example 8 52.67 7.52 0.00 0.15 0.15 30.85 7.52 1.14 1.71 Example 9 52.49 7.50 0.00 0.15 0.50 30.74 7.50 1.12 1.71 Example 10 52.32 7.47 0.00 0.15 0.45 30.64 7.47 1.50 1.71 Example 11 52.71 7.53 0.00 0.15 0.45 30.87 7.53 0.76 1.71 Example 12 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Example 13 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Example 14 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Example 15 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Example 16 27.43 35.78 0.00 0.12 0.29 11.93 23.85 0.60 2.30 Example 17 39.36 23.85 0.00 0.12 0.29 11.93 23.85 0.60 3.30 Example 18 27.47 35.82 0.00 0.12 0.29 11.94 23.88 0.48 2.30 Example 19 52.51 7.50 0.00 0.15 0.45 30.76 7.50 1.13 1.71 Com. Ex. 1 40.00 25.00 0.00 0.35 1.00 11.65 20.00 2.00 3.43 Com. Ex. 2 65.93 0.00 18.84 0.16 0.94 0.00 9.42 4.71 Com. Ex. 3 58.20 20.10 0.00 0.50 1.30 0.00 18.10 1.80 Note: .sup.(2)A volume ratio of an H.sub.2 gas in the mixture gas A to an H.sub.2 gas in the mixture gas B.
(160) TABLE-US-00003 TABLE 2 Hard Titanium Aluminum Nitride Coating Composition (atomic %) Crystal Crystal Daw.sup.(1) Thickness Hardness No. Ti Al N Structure Form (m) (m) (GPa) Example 1 15 33 52 fcc Columnar 0.66 5 39 Example 2 10 39 51 fcc Columnar 0.40 5 40 Example 3 7 41 52 fcc Columnar 0.98 5 35 Example 4 8 41 51 fcc Columnar 0.25 5 40 Example 5 18 32 50 fcc Columnar 0.28 5 40 Example 6 4 44 52 fcc Columnar 0.10 5 42 Example 7 22 26 52 fcc Columnar 1.00 5 35 Example 8 22 27 51 fcc Columnar 0.24 5 41 Example 9 17 33 50 fcc Columnar 0.88 5 38 Example 10 13 35 52 fcc Columnar 0.75 5 37 Example 11 14 35 51 fcc Columnar 1.20 5 35 Example 12 12 38 50 fcc Columnar 0.25 5 39 Example 13 13 35 52 fcc Columnar 0.96 5 38 Example 14 14 38 48 fcc Columnar 0.15 5 35 Example 15 18 27 55 fcc Columnar 1.12 5 35 Example 16 15 37 48 fcc Columnar 0.85 5 37 Example 17 19 30 51 fcc Columnar 0.95 5 36 Example 18 12 35 53 fcc Columnar 0.52 5 34 Example 19 10 40 50 fcc Columnar 0.54 5 38 Com. Ex. 1 12 38 50 fcc Granular .sup.(2) 5 34 Com. Ex. 2 6 44 50 fcc Granular .sup.(2) 5 33 Com. Ex. 3 4.5 45.5 50 fcc + hcp Granular .sup.(2) 5 32 Note: .sup.(1)Daw means an average transverse cross section diameter of columnar crystals. .sup.(2)Not measured.
(161) TABLE-US-00004 TABLE 3 High-Al TiAlN High-Ti TiAlN (Ti.sub.x1, Al.sub.y1)N (Ti.sub.x2, Al.sub.y2)N (atomic ratio) Crystal Dav.sup.(1) Daw.sup.(2) (atomic ratio) Crystal No. x.sub.1 y.sub.1 Structure (nm) (nm) x.sub.2 y.sub.2 Structure Example 1 0.02 0.98 fcc 12 40 0.67 0.33 fcc Example 2 0.01 0.99 fcc 10 32 0.72 0.28 fcc Example 3 0.08 0.92 fcc 48 262 0.85 0.15 fcc Example 4 0.01 0.99 fcc 28 85 0.52 0.48 fcc Example 5 0.04 0.96 fcc 26 93 0.82 0.18 fcc Example 6 0.005 0.995 fcc 2 30 0.50 0.50 fcc Example 7 0.10 0.90 fcc 32 162 0.90 0.10 fcc Example 8 0.09 0.91 fcc 21 62 0.86 0.14 fcc Example 9 0.03 0.97 fcc 28 84 0.60 0.40 fcc Example 10 0.02 0.98 fcc 26 75 0.63 0.37 fcc Example 11 0.08 0.92 fcc 30 150 0.88 0.12 fcc Example 12 0.02 0.98 fcc 8 22 0.61 0.39 fcc Example 13 0.03 0.97 fcc 22 80 0.75 0.25 fcc Example 14 0.06 0.94 fcc 5 20 0.80 0.20 fcc Example 15 0.07 0.93 fcc 50 300 0.82 0.18 fcc Example 16 0.03 0.97 fcc 18 56 0.70 0.30 fcc Example 17 0.09 0.91 fcc 25 68 0.62 0.38 fcc Example 18 0.08 0.92 fcc 43 132 0.55 0.45 fcc Example 19 0.01 0.99 fcc 38 212 0.71 0.29 fcc Com. Ex. 1 .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) Com. Ex. 2 .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) Com. Ex. 3 .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) .sup.(3) Note: .sup.(1)Dav means an average longitudinal cross section diameter. .sup.(2)Daw means an average transverse cross section diameter. .sup.(3)No.
(162) TABLE-US-00005 TABLE 4 Tool Life No. Microstructure (m).sup.(1) Example 1 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 60 Example 2 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 3 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 4 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 50 Example 5 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 50 Example 6 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 7 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 8 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 9 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 10 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 11 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 12 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 13 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 14 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 15 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 16 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Example 17 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 50 Example 18 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 40 Example 19 High-Al TiAlN surrounded by network-like, high-Ti TiAlN 55 Com. Ex. 1 TiAlN having different Al contents alternately laminated 15 Com. Ex. 2 TiAlN having different Al contents alternately partially 10 laminated Com. Ex. 3 TiAlN having different Al contents alternately laminated 10 Note: .sup.(1)Expressed by the cutting distance.
(163) Each hard-coated tool (milling insert) of Examples 1-19 had a tool life of 40 m or more (expressed by cutting distance), as long as 2 times or more those of Comparative Examples 1-3. Such high performance appears to be achieved by excellent wear resistance and oxidation resistance of each hard-coated tool (milling insert) of Examples 1-19, which were obtained by the above characteristic microstructure of the hard titanium aluminum nitride coating.
(164) On the other hand, the hard titanium aluminum nitride coating of Comparative Example 1 having a granular structure, in which TiAlN layers having different Al contents were alternately laminated, suffered rapid oxidation because oxygen intruded through crystal grain boundaries at high temperatures. As a result, the hard-coated tool of Comparative Example 1 suffered rapid crater wear, resulting in a short life. The tool of Comparative Example 2 having a hard titanium aluminum nitride coating having a granular structure, in which TiAlN layers having different Al contents were partially laminated, had poor oxidation resistance at high temperatures as in Comparative Example 1, resulting in a short life. Because the fcc structure was rapidly converted to the hcp structure in the hard titanium aluminum nitride coating of Comparative Example 3 at high temperatures, the coating had lower hardness with interlayer delamination, so that the tool having such coating had a short life.
DESCRIPTION OF REFERENCE NUMERALS
(165) 1: CVD furnace 2: Chamber 3: Heater 4: Shelf 4a: Center opening of shelve 5: Reaction vessel 6: First crystal phase (pale gray portion) 7: Second thin-film-like (network-like) crystal phase (dark gray or black portion) 11: First pipe 11a: Nozzle of first pipe 12: Second pipe 12a: Nozzle of second pipe 13: Discharge pipe 20: Insert substrate 30, 40, 50, 80: Assembly of first and second pipes 60: Milling insert 70: Indexable rotary cutting tool 71: Tool body 72: Tip portion 73: Setscrew