US3900592A - Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate - Google Patents
Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate Download PDFInfo
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- US3900592A US3900592A US382308A US38230873A US3900592A US 3900592 A US3900592 A US 3900592A US 382308 A US382308 A US 382308A US 38230873 A US38230873 A US 38230873A US 3900592 A US3900592 A US 3900592A
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- 239000000758 substrate Substances 0.000 title claims abstract description 67
- 238000000576 coating method Methods 0.000 title claims abstract description 42
- 239000011248 coating agent Substances 0.000 title claims abstract description 39
- 238000000034 method Methods 0.000 title claims abstract description 36
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims description 18
- 239000010936 titanium Substances 0.000 title claims description 18
- 229910052719 titanium Inorganic materials 0.000 title claims description 18
- ZVWKZXLXHLZXLS-UHFFFAOYSA-N zirconium nitride Chemical compound [Zr]#N ZVWKZXLXHLZXLS-UHFFFAOYSA-N 0.000 title abstract description 7
- 230000008021 deposition Effects 0.000 claims abstract description 16
- 239000000203 mixture Substances 0.000 claims abstract description 8
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 26
- 239000007789 gas Substances 0.000 claims description 15
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 13
- 229910052757 nitrogen Inorganic materials 0.000 claims description 13
- 229910052726 zirconium Inorganic materials 0.000 claims description 12
- 239000000376 reactant Substances 0.000 claims description 10
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 8
- 150000004767 nitrides Chemical class 0.000 claims description 8
- 238000001704 evaporation Methods 0.000 claims description 6
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 claims description 4
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 claims description 4
- 230000008859 change Effects 0.000 claims description 2
- 238000000151 deposition Methods 0.000 abstract description 16
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 abstract description 11
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 abstract description 6
- 229910026551 ZrC Inorganic materials 0.000 abstract description 4
- OTCHGXYCWNXDOA-UHFFFAOYSA-N [C].[Zr] Chemical compound [C].[Zr] OTCHGXYCWNXDOA-UHFFFAOYSA-N 0.000 abstract description 4
- 238000005240 physical vapour deposition Methods 0.000 abstract description 4
- 239000000463 material Substances 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 238000005520 cutting process Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 229920006384 Airco Polymers 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 238000005137 deposition process Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010894 electron beam technology Methods 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000001351 cycling effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000002905 metal composite material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000007740 vapor deposition Methods 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/027—Graded interfaces
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/0021—Reactive sputtering or evaporation
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/24983—Hardness
Definitions
- a method for coating a substrate with titanium nitride or titanium carbide or zirconium nitride or zirconium carbide is described wherein physical vapor deposition in a vacuum is used, and wherein the substrate is biased by an electrical potential and the composition of the deposit is changed by introducing a gas during the deposition to produce a hardness gradient in the deposit which increases outwardly from the substrate.
- Titanium Nitride #1100, 325x Vickers Pneumatic Hardness Tests Kglmm 100 qram load 50 gram load 100 qram load 10 gram load METHOD FOR COATING A SUBSTRATE TO PROVIDE A TITANIUM OR ZIRCONIUM NITRIDE OR CARBIDE DEPOSIT HAVING A HARDNESS GRADIENT WHICH INCREASES OUTWARDLY FROM THE SUBSTRATE
- This invention relates to coated substrates and, more particularly, to the coating of a substrate to produce a high hardness coating.
- the production of high hardness coatings on substrates may be desired in a wide variety of applications.
- a titasium carbide coating on the surface of tungsten carbide cutting tools or wear parts produces significantly longer cutting or wear life than is possible with the uncoated tools or parts.
- Another example is the coating of wear surfaces in the combustion chambers of internal combustion engines, particularly those of the rotary type, with high hardness coatings of titanium nitride or titanium carbide.
- Another object of the invention is to provide a method for coating a substrate in which very high hardness of the coating is obtained.
- lt is another object of the invention to provide a method for coating a substrate in which relatively higher deposition rates may be achieved than in many prior art methods.
- 7 V v A further object of the invention is to provide a method for coating a substrate in which a very strong mechanical bond between a high hardness coating and a relatively softer substrate is achieved.
- the method of the invention comprises placing the substrate in an evacuated environment and evaporating titanium or zirconium metal in the evacuated environment to produce a vapor and causing the vapor to deposit on the substrate.
- the composition of the vapor is changed by reacting it with a gas during deposition to produce a hardness gradient in the deposit which increases outwardly from the substrate.
- an electrical potential is applied to the substrate during the deposition process sufficient to produce a voltage difference of at least 200 volts between the substrate and the crucible.
- the method is applicable to coating a variety of substrates, including metals such as aluminum, magnesium, iron, and alloys thereof, and to coating metal composites such as tungsten carbide.
- substrates including metals such as aluminum, magnesium, iron, and alloys thereof
- metal composites such as tungsten carbide.
- the particular materials used depends upon the use of the product being manufactured. For example, a coating of titanium nitride on a titanium carbide substrate will produce a very hard product suitable for use in cutting tools and wear parts.
- Coatings deposited in accordance with the invention may comprise titanium nitride, titanium carbide, zirconium nitride or zirconium carbide for wear parts, cutting tools, or corrosion resistance, etc.
- the invention is applicable to any situation wherein it is desirable to produce a hard coating on a relatively softer substrate.
- the equipment utilized to carry out the method of the invention may be of any suitable type in which a vapor of the material to be deposited is produced in a vacuum. Heating of the coating material in order to vaporize same may be accomplished by such means as resistance heating, induction heating, or preferably electron beam heating. Equipment for accomplishing high vacuum vapor deposition is known in the art andis commercially available on the market from the Airco Temescal Division of Airco, 'lnc., Berkeley, Calif. The particular structure of the equipment is not critical to the invention and therefore will not be further de-' the initial pressure in the chamber is of the order of 1 millitorr or less.
- an electrical potential is applied to the substrate during deposition.
- the electrical potential is sufficient to produce a glow discharge.
- an electrical bias of negative 200 volts or greater will produce the desired glow I discharge.
- the electrical biasing will also tend to heat the substrate, which is desirable in most cases to enhance the quality of the deposit.
- the titanium or zirconium of which a nitride or carbide is to be deposited is evaporated within the evacuated environment.
- the term titanium is meant to include pure titanium and titanium base alloys as well.
- the tenn zirconium is meant to include pure zirconium and zirconium base alloys as well.
- the metal thusevaporated will pass in the vapor form within the evacuated environment and when vapor particles thereof strike the substrate, they will condense on the substrate and thereby form a deposit on the surface thereof. The particular conditions under which this occurs are well known to those skilled in the art and therefore will not be further detailed herein.
- the respective dimensional responses of the substrate and the coating to thermal or mechanical forces may be substantially different. As a result, very high shear forces may concentrate at the interface between the coating and the substrate. If this interface is weak for any reason, such as poor adhesion or the presence of discontinuities or foreign substances, failure can result.
- the method of the invention creates a hardness gradient in the coating. Ideally, this is accomplished by making the mechanical and thermal properties of the coating and the substrate at the interface identical. Transition from the mechanical and thermal properties at the interface to the higher strength properties on the outer surface of the deposit are made to occur gradually from the interface to the outersurface.
- the elimination of thermal and mechani cal property discontinuities distributes shear stresses over a volume, rather than concentrating them at a surface plane at the interface, thus rendering the resultant product more resistant to thermal or mechanical cycling.
- the composition of the vapor produced in the evacuated environment is changed gradually during the deposition process to produce a hardness gradient in the deposit which increases outwardly from the substrate.
- This is accomplished by the introduction of a reactant gas to the vapor gradually increasing the gas pressure, such as from about one micron to about 50 microns.
- the reactant gas may such as to produce a nitride or carbide, and may be acetylene, nitrogen, methane, etc., for example.
- the photomicrograph enlarged 325 times illustrates the cross section of a substrate coated in accordance with the invention and illustrating the results of Vickers Pneumatic hardness tests in kilograms per square millimeter taken across the cross section.
- the substrate is indicatedv at the very bottom of the illustration and five regions of the coating are indicated at A, B, C, .Dand E in the photograph. These regions represent different partial pressures of nitrogen present during the evaporation process.
- Region A in which no nitrogen bleed was used, is pure titanium.
- Region B was deposited at 3 to 4 microns partial pressure nitrogen, region C at 4 to 6.5 microns partial pressure of nitrogen, region D at microns partial pressure of nitrogen, and region E at 12 microns partial pressure of nitrogen. Deposition rates for all regions was 0.0008 inch per minute except for region. E, in which the rate was 0.0003 inch.
- Evaporation 'occurred from a pure titanium ingot with a 25 kilowatt electron beam at'a starting pressure of 0.01 micron in the vacuum chamber.
- the temperature of the substrate was l600F.
- Pressure of the nitrogen was increased to the 12 micron maximum in a time period of 40 minutes and then was held constant in the region E.
- pure titanium deposited at the substrate surface in the region A offered relatively low hardness values, and the Vickers hardness values increased substantially in the regions B through D.
- the outer surface offered the maximum Vickers hardness of 2,450 kilograms per square millimeter under a 100 gram load.
- the illustration indicates that the surface hardness is substantially increased by depositing titanium nitride in accordance with the invention.
- TITANIUM-NITRIDE HARDNESS AS A FUNCTION OF BIAS AND NITROGEN PRESSURE
- the substrate temperature was l,600F and the deposition rate was 1 i 0.3 mils per minute in all cases.
- Zirconium has been deposited in accordance with the invention and similar results have been achieved. Hardness values of zirconium nitride deposited by evaporating zirconium with a N bleed were as follows:
- Zirconium carbide may be produced in a similar manner.
- the invention provides an improved method for coating a substrate in which very high hardness of the coating is obtained. Relatively high deposition rates may also be achieved in comparison with many prior art methods. A very strong mechanical bond is obtained between the high hardness coating and the relatively softer substrate.
- a method for coating a substrate with a nitride or carbide of titanium or zirconium comprising, placing the substrate in an evacuated environment, evaporating titanium or zirconium from a crucible in the evacuated environment to produce a vapor and causing the vapor to deposit on the substrate initially as titanium or zirconium, applying an electrical potential during deposition sufficient to produce a voltage difference of at least 200 volts between the substrate and the crucible, and introducing a reactant gas with a gradually increasing partial pressure to the vapor to change the composition of the deposit from its initial composition to increasing nitride or carbide in the direction outwardly from the substrate to produce a hardness gradient in the deposit which increases outwardly from the substrate.
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- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physical Vapour Deposition (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Ceramic Products (AREA)
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Abstract
A method for coating a substrate with titanium nitride or titanium carbide or zirconium nitride or zirconium carbide is described wherein physical vapor deposition in a vacuum is used, and wherein the substrate is biased by an electrical potential and the composition of the deposit is changed by introducing a gas during the deposition to produce a hardness gradient in the deposit which increases outwardly from the substrate.
Description
United Sttes Patent Kennedy et al.
[451 Aug. 19, 1975 METHOD FOR COATING A SUBSTRATE TO PROVIDE A TITANIUM OR ZIRCONIUM NITRIDE OR CARBIDE DEPOSIT HAVING A HARDNESS GRADIENT WHICH INCREASES OUTWARDLY FROM THE SUBSTRATE Inventors: Kurt D. Kennedy, Berkeley; Glen R.
Scheuermann, Novato, both of Calif.
Assignee: Airco, Inc., Montvale, NJ.
Filed: July 25, 1973 Appl. No.: 382,308
US. Cl. 427/39; 427/249; 428/217; 428/212 Int. Cl. C23c 11/08 Field of Search 117/93, 93.1 GD, 106 R, 117/107, 131
References Cited UNITED STATES PATENTS 5/1958 Munster et al 117/106 R T 1 tan i um Ni tr i de #1 100 2,972,556 2/1961 Vrahiotes et a1 117/106 R 3,108,900 10/1963 Papp 3,437,511 4/1969 Hough 3,492,152 1/1970 Cariou et al. 117/106 R Primary Examiner-William D. Martin Assistant ExaminerJohn H. Newsome Attorney, Agent, or F irmFitch, Even, Tabin & Luedeka A method for coating a substrate with titanium nitride or titanium carbide or zirconium nitride or zirconium carbide is described wherein physical vapor deposition in a vacuum is used, and wherein the substrate is biased by an electrical potential and the composition of the deposit is changed by introducing a gas during the deposition to produce a hardness gradient in the deposit which increases outwardly from the substrate.
. ABSTRACT 6 Claims, 1 Drawing Figure Vickers Pneumatic ardness ests 100 qram load 50 gram load l I -lO f. into lOO qram load 50 gram load 4 100 qram load 10 gram load PATENTED M161 91975 3, 900.592
Titanium Nitride #1100, 325x Vickers Pneumatic Hardness Tests (Kglmm 100 qram load 50 gram load 100 qram load 10 gram load METHOD FOR COATING A SUBSTRATE TO PROVIDE A TITANIUM OR ZIRCONIUM NITRIDE OR CARBIDE DEPOSIT HAVING A HARDNESS GRADIENT WHICH INCREASES OUTWARDLY FROM THE SUBSTRATE This invention relates to coated substrates and, more particularly, to the coating of a substrate to produce a high hardness coating.
The production of high hardness coatings on substrates may be desired in a wide variety of applications. For example, it is well known that the production of a titasium carbide coating on the surface of tungsten carbide cutting tools or wear parts produces significantly longer cutting or wear life than is possible with the uncoated tools or parts. Another example is the coating of wear surfaces in the combustion chambers of internal combustion engines, particularly those of the rotary type, with high hardness coatings of titanium nitride or titanium carbide.
In order to accomplish this deposition, much work has been done in the area of physical vapor deposition processes, hollow cathode sputtering processes, chemical vapor deposition processes, and reactive physical vapor deposition processes. Prior art applications of such processes, however, have failed to produce hardness values as high as may be required in many instances. Moreover, in many instances of prior art deposition processes, the rate of deposition has been lower than that desirable for high production techniques. In other cases of prior art deposition techniques, mechanical failure of the coating at the interface with the substrate has occurred.
It is an object of the present invention to provide an improved method for coating a substrate.
Another object of the invention is to provide a method for coating a substrate in which very high hardness of the coating is obtained.
lt is another object of the invention to provide a method for coating a substrate in which relatively higher deposition rates may be achieved than in many prior art methods. 7 V v A further object of the invention is to provide a method for coating a substrate in which a very strong mechanical bond between a high hardness coating and a relatively softer substrate is achieved.
Other objects of the invention will become apparent to those skilled in the art from the followingdescription, taken in connection with the accompanying illustration which is a photomicrograph enlarged 325 times of the cross section of a substrate coated with titanium nitride in accordance with the invention,
Very generally, the method of the invention comprises placing the substrate in an evacuated environment and evaporating titanium or zirconium metal in the evacuated environment to produce a vapor and causing the vapor to deposit on the substrate. The composition of the vapor is changed by reacting it with a gas during deposition to produce a hardness gradient in the deposit which increases outwardly from the substrate. To improve deposition rate and hardness, an electrical potential is applied to the substrate during the deposition process sufficient to produce a voltage difference of at least 200 volts between the substrate and the crucible.
Referring now in greater detail to the method of the invention, the method is applicable to coating a variety of substrates, including metals such as aluminum, magnesium, iron, and alloys thereof, and to coating metal composites such as tungsten carbide. The particular materials used depends upon the use of the product being manufactured. For example, a coating of titanium nitride on a titanium carbide substrate will produce a very hard product suitable for use in cutting tools and wear parts.
As was the case in connection with the substrates, the nature of the deposit put down will also depend upon the end use for the product being manufactured. Coatings deposited in accordance with the invention may comprise titanium nitride, titanium carbide, zirconium nitride or zirconium carbide for wear parts, cutting tools, or corrosion resistance, etc. Generally speaking, the invention is applicable to any situation wherein it is desirable to produce a hard coating on a relatively softer substrate.
The equipment utilized to carry out the method of the invention may be of any suitable type in which a vapor of the material to be deposited is produced in a vacuum. Heating of the coating material in order to vaporize same may be accomplished by such means as resistance heating, induction heating, or preferably electron beam heating. Equipment for accomplishing high vacuum vapor deposition is known in the art andis commercially available on the market from the Airco Temescal Division of Airco, 'lnc., Berkeley, Calif. The particular structure of the equipment is not critical to the invention and therefore will not be further de-' the initial pressure in the chamber is of the order of 1 millitorr or less.
In order to enhance the deposition rate, the quality of the deposit, and the hardness of the deposit, an electrical potential is applied to the substrate during deposition. The electrical potential is sufficient to produce a glow discharge. Typically, an electrical bias of negative 200 volts or greater will produce the desired glow I discharge. The electrical biasing will also tend to heat the substrate, which is desirable in most cases to enhance the quality of the deposit.
The titanium or zirconium of which a nitride or carbide is to be deposited is evaporated within the evacuated environment. As used herein, the term titanium is meant to include pure titanium and titanium base alloys as well. The tenn zirconium is meant to include pure zirconium and zirconium base alloys as well. As is known in the art, the metal thusevaporated will pass in the vapor form within the evacuated environment and when vapor particles thereof strike the substrate, they will condense on the substrate and thereby form a deposit on the surface thereof. The particular conditions under which this occurs are well known to those skilled in the art and therefore will not be further detailed herein.
If the hard coating deposited on the substrate has a substantially higher strength than the substrate material, the respective dimensional responses of the substrate and the coating to thermal or mechanical forces may be substantially different. As a result, very high shear forces may concentrate at the interface between the coating and the substrate. If this interface is weak for any reason, such as poor adhesion or the presence of discontinuities or foreign substances, failure can result. 1
To avoid such failure, the method of the invention creates a hardness gradient in the coating. Ideally, this is accomplished by making the mechanical and thermal properties of the coating and the substrate at the interface identical. Transition from the mechanical and thermal properties at the interface to the higher strength properties on the outer surface of the deposit are made to occur gradually from the interface to the outersurface. The elimination of thermal and mechani cal property discontinuities distributes shear stresses over a volume, rather than concentrating them at a surface plane at the interface, thus rendering the resultant product more resistant to thermal or mechanical cycling.
To this end, the composition of the vapor produced in the evacuated environment is changed gradually during the deposition process to produce a hardness gradient in the deposit which increases outwardly from the substrate. This is accomplished by the introduction of a reactant gas to the vapor gradually increasing the gas pressure, such as from about one micron to about 50 microns. Typically, all that is necessary is to turn on a bleed source and allow a gradual build-up of the partial pressure of the bleed gas in the vapor. The reactant gas may such as to produce a nitride or carbide, and may be acetylene, nitrogen, methane, etc., for example. A reduction of damaging stress concentrations at the interface between the coating and the substrate results.
Referring now to the illustration, the photomicrograph enlarged 325 times illustrates the cross section of a substrate coated in accordance with the invention and illustrating the results of Vickers Pneumatic hardness tests in kilograms per square millimeter taken across the cross section. The substrate is indicatedv at the very bottom of the illustration and five regions of the coating are indicated at A, B, C, .Dand E in the photograph. These regions represent different partial pressures of nitrogen present during the evaporation process.
Region A, in which no nitrogen bleed was used, is pure titanium. Region B was deposited at 3 to 4 microns partial pressure nitrogen, region C at 4 to 6.5 microns partial pressure of nitrogen, region D at microns partial pressure of nitrogen, and region E at 12 microns partial pressure of nitrogen. Deposition rates for all regions was 0.0008 inch per minute except for region. E, in which the rate was 0.0003 inch.
Evaporation" 'occurred from a pure titanium ingot with a 25 kilowatt electron beam at'a starting pressure of 0.01 micron in the vacuum chamber. The temperature of the substrate was l600F. Pressure of the nitrogen was increased to the 12 micron maximum in a time period of 40 minutes and then was held constant in the region E. As may be seen, pure titanium deposited at the substrate surface in the region A offered relatively low hardness values, and the Vickers hardness values increased substantially in the regions B through D. Finally, the outer surface offered the maximum Vickers hardness of 2,450 kilograms per square millimeter under a 100 gram load.
The illustration indicates that the surface hardness is substantially increased by depositing titanium nitride in accordance with the invention.
The following table set forth below illustrates titanium nitride hardness as a function of electrical substrate bias and nitrogen pressure. As ma be seen, there is a general tendency in the range set out for hardness to increase as a function of gas pressure and as a function of a negative bias voltage.
TITANIUM-NITRIDE HARDNESS AS A FUNCTION OF BIAS AND NITROGEN PRESSURE The substrate temperature was l,600F and the deposition rate was 1 i 0.3 mils per minute in all cases.
Other titanium base materials which have been successfully deposited include Ti3Al-2.5V on aluminum substrates with a nitrogen bleed to form titanium nitride. The same material has been coated with the use of a methane and an acetylene bleed to form titanium carbide in each case.
Zirconium has been deposited in accordance with the invention and similar results have been achieved. Hardness values of zirconium nitride deposited by evaporating zirconium with a N bleed were as follows:
Vickers Hardness N Pressure Number-kg/mm Microns 494 .0 l 5 750 .03 494 .05 i625 .3 1950 l 1 000 l .3 2325 l .6 23 l .9
As may be seen, in the range shown, a general tendency toward increased hardness with increasing partial pressure of N exists. Zirconium carbide may be produced in a similar manner.
It may therefore be seen that the invention provides an improved method for coating a substrate in which very high hardness of the coating is obtained. Relatively high deposition rates may also be achieved in comparison with many prior art methods. A very strong mechanical bond is obtained between the high hardness coating and the relatively softer substrate.
Various modifications of the invention in addition to those shown and described herein will become apparent to those skilled in the art from the foregoing description and accompanying illustration. Such modifi- What is claimed is:
1. A method for coating a substrate with a nitride or carbide of titanium or zirconium, comprising, placing the substrate in an evacuated environment, evaporating titanium or zirconium from a crucible in the evacuated environment to produce a vapor and causing the vapor to deposit on the substrate initially as titanium or zirconium, applying an electrical potential during deposition sufficient to produce a voltage difference of at least 200 volts between the substrate and the crucible, and introducing a reactant gas with a gradually increasing partial pressure to the vapor to change the composition of the deposit from its initial composition to increasing nitride or carbide in the direction outwardly from the substrate to produce a hardness gradient in the deposit which increases outwardly from the substrate.
2. A method according to claim 1 wherein the reactant gas is nitrogen in order to produce a nitride coating.
3. A method according to claim 1 wherein the reactant gas is methane in order to produce a carbide coating.
4. A method according to claim 1 wherein the reactant gas is acetylene in order to produce a carbide coating.
5. A method according to claim 1 wherein the substrate is biased negative with respect to ground.
6. A method according to claim 1 wherein the substrate is heated during deposition.
Claims (6)
1. A METHOD FOR COATING A SUBSTRATE WITH A NITRIDE OR CARBIDE OF TITANIUM OR ZIRCONIUM, COMPRISING, PLACING THE SUBSTRATE IN AN EVACUATED ENVIRONMENT, EVAPORATING TITANIUM OR ZIRCONIUM FROM A CRUCIBLE IN THE EVACUATED ENVIRONMENT TO PRODUCE A VAPOR AND CAUSING THE VAPOR TO DEPOSIT ON THE SUBSTRATE INITIALLY AS TITANIUM OR ZIRCONIUM, APPLYING AN ELECTRICAL POTENTIAL DURING DEPOSITION SUFFICIENT TO PRODUCE A VOLTAGE DIFFERENCE OF AT LEAST 200 VOLTS BETWEEN THE SUBSTRATE AND THE CRUCIBLE, AND INTRODUCING A REACTANT GAS WITH A GRADUALLY INCREASING PARTIAL PRESSURE TO THE VAPOR TO CHANGE THE COMPOSITION OF THE DEPOSIT FROM ITS INITIAL COMPOSITION TO INCREASING NITRIDE OR CARBIDE IN THE DIRECTION OUTWARDLY FROM THE SUBSTRATE TO PRODUCE A HARDNESS GRADIENT IN THE DEPOSIT WHICH INCREASES OUTWARDLY FROM THE SUBSTRATE.
2. A method according to claim 1 wherein the reactant gas is nitrogen in order to produce a nitride coating.
3. A method according to claim 1 wherein the reactant gas is methane in order to produce a carbide coating.
4. A method according to claim 1 wherein the reactant gas is acetylene in order to produce a carbide coating.
5. A method according to claim 1 wherein the substrate is biased negative with respect to ground.
6. A method according to claim 1 wherein the substrate is heated during deposition.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US382308A US3900592A (en) | 1973-07-25 | 1973-07-25 | Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate |
| DE19742431448 DE2431448B2 (en) | 1973-07-25 | 1974-07-01 | PROCESS FOR COATING A SUBSTRATE WITH A NITRIDE OR CARBIDE OF TITANIUM OR ZIRCONIUM BY REACTIVE EVAPORATION |
| JP8555474A JPS5319325B2 (en) | 1973-07-25 | 1974-07-25 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US382308A US3900592A (en) | 1973-07-25 | 1973-07-25 | Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3900592A true US3900592A (en) | 1975-08-19 |
Family
ID=23508397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US382308A Expired - Lifetime US3900592A (en) | 1973-07-25 | 1973-07-25 | Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3900592A (en) |
| JP (1) | JPS5319325B2 (en) |
| DE (1) | DE2431448B2 (en) |
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| US4035541A (en) * | 1975-11-17 | 1977-07-12 | Kennametal Inc. | Sintered cemented carbide body coated with three layers |
| US4107352A (en) * | 1977-01-13 | 1978-08-15 | Westinghouse Canada Limited | Chemical vapor deposition |
| US4109061A (en) * | 1977-12-08 | 1978-08-22 | United Technologies Corporation | Method for altering the composition and structure of aluminum bearing overlay alloy coatings during deposition from metallic vapor |
| US4226082A (en) * | 1976-06-07 | 1980-10-07 | Nobuo Nishida | Ornamental part for watches and method of producing the same |
| US4254159A (en) * | 1977-12-23 | 1981-03-03 | Balzers Aktiengesellschaft Fur Hochvakuumtechnik Und Dunne Schichten | Method of producing gold-color coatings |
| US4260658A (en) * | 1979-06-21 | 1981-04-07 | Kobe, Inc. | Erosion resistant surface |
| US4333962A (en) * | 1979-09-04 | 1982-06-08 | Balzers Aktiengesellschaft | Method for producing gold color coatings |
| US4346123A (en) * | 1979-08-02 | 1982-08-24 | Balzers Aktiengesellschaft | Method of depositing hard wear-resistant coatings on substrates |
| US4415602A (en) * | 1981-07-24 | 1983-11-15 | Canadian Industrial Innovation Centre/Waterloo | Reactive plating method and product |
| US4466991A (en) * | 1946-07-17 | 1984-08-21 | Vsesojuzny Nauchno-Issledovatelsky Instrumentalny Institut | Cutting tool hardening method |
| US4514240A (en) * | 1980-10-30 | 1985-04-30 | Societe Europeenne De Propulsion | Method for adhesively bonding parts made of refractory materials |
| DE3515807A1 (en) * | 1984-05-04 | 1985-11-07 | Diesel Kiki Co. Ltd., Tokio/Tokyo | METHOD FOR PRODUCING A THIN FILM |
| DE3535022A1 (en) * | 1985-02-08 | 1986-08-14 | Citizen Watch Co., Ltd., Tokio/Tokyo | METHOD FOR PRODUCING COATING LAYERS BY ION RADIATION PLATING |
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| US4758451A (en) * | 1985-12-19 | 1988-07-19 | Fried. Krupp Gmbh | Process for producing coated molded bodies |
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| WO1990012125A1 (en) * | 1989-04-06 | 1990-10-18 | Institut Strukturnoi Makrokinetiki Akademii Nauk Sssr | Method for obtaining a refractory inorganic coating on the surface of an article |
| US4973388A (en) * | 1986-02-04 | 1990-11-27 | Preci-Coat S.A. | Method of depositing a decorative wear-resistant coating layer on a substrate |
| DE3936550C1 (en) * | 1989-11-03 | 1991-04-18 | Arthur Klink Gmbh, 7530 Pforzheim, De | Substrate coating for wear resistance - with titanium nitride in vacuum chamber contg. titanium evaporator and heater with rotary substrate holder |
| WO1991014017A1 (en) * | 1990-03-09 | 1991-09-19 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
| GB2242442A (en) * | 1990-03-09 | 1991-10-02 | Allan Matthews | Modulated composition composites produced by vapour deposition |
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| US5137772A (en) * | 1987-03-27 | 1992-08-11 | Nihon Sinku Gijutsu Kabusiki Kaisha | Body coated with cubic boron nitride and method for manufacturing the same |
| US5185211A (en) * | 1991-07-11 | 1993-02-09 | Praxair S.T. Technology, Inc. | Non-stoichiometric titanium nitride coating |
| US5229193A (en) * | 1989-11-10 | 1993-07-20 | Shin-Etsu Chemical Co., Ltd. | Silicon carbide member |
| US5242753A (en) * | 1991-07-11 | 1993-09-07 | Praxair S.T. Technology, Inc. | Substoichiometric zirconium nitride coating |
| US5264297A (en) * | 1990-03-09 | 1993-11-23 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
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| US5626920A (en) * | 1991-10-04 | 1997-05-06 | Tulip Memory Systems, Inc. | Method for coating metal disc substrates for magnetic-recording media |
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| US5681635A (en) * | 1994-01-20 | 1997-10-28 | Tulip Memory Systems, Inc. | Magnetic recording medium having a ceramic substrate, an underlayer having a dense fibrous zone T structure, and a magnetic layer |
| US5707748A (en) * | 1993-07-21 | 1998-01-13 | Balzers Ag | Coated tool with increased service life |
| US5707705A (en) * | 1993-09-08 | 1998-01-13 | Tulip Memory Systems, Inc. | Titanium or titanium-alloy substrate for magnetic-recording media |
| US5928977A (en) * | 1996-12-23 | 1999-07-27 | Smh Management Services Ag | Zirconia based ceramic article as wear-resistant exterior part for wristwatch |
| US6162500A (en) * | 1996-06-27 | 2000-12-19 | Vaw Motor Gmbh | Method of treating a casting having a casting surface |
| US6360423B1 (en) | 1997-12-16 | 2002-03-26 | Clad Metals Llc | Stick resistant coating for cookware |
| US6432022B1 (en) | 1998-05-15 | 2002-08-13 | Alpha Getriebebau Gmbh | Low-play planetary gear mechanism |
| US20040157066A1 (en) * | 2003-02-07 | 2004-08-12 | Arzoumanidis G. Alexis | Method of applying a hardcoating typically provided on downhole tools, and a system and apparatus having such a hardcoating |
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| US6797335B1 (en) * | 1999-08-16 | 2004-09-28 | Paderov Anatol Y Nikolaevich | Method for deposition of wear-resistant coatings and for increasing the lifespan of parts |
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| JPS5221283A (en) * | 1975-08-13 | 1977-02-17 | Seiko Instr & Electronics Ltd | Constituting element of works for clock parts etc. |
| JPS5334027U (en) * | 1976-08-31 | 1978-03-25 | ||
| GB1579999A (en) * | 1977-09-12 | 1980-11-26 | Gen Electric | Annular metal cutting die of titanium carbide coating tool steel and method of shaving metal rods |
| ES494779A0 (en) * | 1979-08-09 | 1981-03-16 | Mitsubishi Metal Corp | PROCEDURE FOR THE MANUFACTURE OF BLADES EQUIPPED WITH COATING, FOR CUTTING TOOLS |
| FR2483848A1 (en) * | 1980-06-06 | 1981-12-11 | Stephanois Rech Mec | PROCESS FOR THE PRODUCTION OF A COMPOSITE LAYER RESISTING BOTH IN GRIPPING, ABRASION, CORROSION AND FATIGUE BY ALTERNATE STRESSES, AND COMPOSITE LAYER THUS OBTAINED |
| SE8300910L (en) * | 1983-02-18 | 1984-08-19 | Santrade Ltd | COMPOSITION BODY CONSISTS OF A SUBSTRATE COATED WITH HEART, Wear-resistant finish |
| DE3431330A1 (en) * | 1984-08-25 | 1986-03-06 | Battelle-Institut E.V., 6000 Frankfurt | Shear blade for an electric shaver |
| JPS61288062A (en) * | 1985-06-17 | 1986-12-18 | エヌ・ベ−・フイリツプス・フル−イランペンフアブリケン | Improvement of abrasion resistance of titanium matter |
| DE4232429A1 (en) * | 1992-09-28 | 1994-03-31 | Bosch Gmbh Robert | Tool for the treatment of surfaces of components and carrier material for this tool |
| US5384201A (en) * | 1991-05-31 | 1995-01-24 | Robert Bosch Gmbh | Tool for treating surfaces of structural parts and carrier material for the same |
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Cited By (93)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4466991A (en) * | 1946-07-17 | 1984-08-21 | Vsesojuzny Nauchno-Issledovatelsky Instrumentalny Institut | Cutting tool hardening method |
| US4035541A (en) * | 1975-11-17 | 1977-07-12 | Kennametal Inc. | Sintered cemented carbide body coated with three layers |
| US4226082A (en) * | 1976-06-07 | 1980-10-07 | Nobuo Nishida | Ornamental part for watches and method of producing the same |
| US4107352A (en) * | 1977-01-13 | 1978-08-15 | Westinghouse Canada Limited | Chemical vapor deposition |
| US4109061A (en) * | 1977-12-08 | 1978-08-22 | United Technologies Corporation | Method for altering the composition and structure of aluminum bearing overlay alloy coatings during deposition from metallic vapor |
| US4254159A (en) * | 1977-12-23 | 1981-03-03 | Balzers Aktiengesellschaft Fur Hochvakuumtechnik Und Dunne Schichten | Method of producing gold-color coatings |
| US4260658A (en) * | 1979-06-21 | 1981-04-07 | Kobe, Inc. | Erosion resistant surface |
| US4346123A (en) * | 1979-08-02 | 1982-08-24 | Balzers Aktiengesellschaft | Method of depositing hard wear-resistant coatings on substrates |
| US4333962A (en) * | 1979-09-04 | 1982-06-08 | Balzers Aktiengesellschaft | Method for producing gold color coatings |
| US4514240A (en) * | 1980-10-30 | 1985-04-30 | Societe Europeenne De Propulsion | Method for adhesively bonding parts made of refractory materials |
| US4415602A (en) * | 1981-07-24 | 1983-11-15 | Canadian Industrial Innovation Centre/Waterloo | Reactive plating method and product |
| DE3515807A1 (en) * | 1984-05-04 | 1985-11-07 | Diesel Kiki Co. Ltd., Tokio/Tokyo | METHOD FOR PRODUCING A THIN FILM |
| DE3535022A1 (en) * | 1985-02-08 | 1986-08-14 | Citizen Watch Co., Ltd., Tokio/Tokyo | METHOD FOR PRODUCING COATING LAYERS BY ION RADIATION PLATING |
| DE3535022C2 (en) * | 1985-02-08 | 1994-07-14 | Citizen Watch Co Ltd | Metallic article with coating layers and method for the production by ion vapor deposition |
| US4966789A (en) * | 1985-02-12 | 1990-10-30 | Masco Corporation Of Indiana | Process of manufacturing seal members having a low friction coefficient |
| GB2187537B (en) * | 1985-02-12 | 1989-06-14 | Masco Corp | Seal members for valves and faucets |
| US4935313A (en) * | 1985-02-12 | 1990-06-19 | Masco Corporation Of Indiana | Process of manufacturing seal members having a low friction coefficient |
| WO1986004548A1 (en) * | 1985-02-12 | 1986-08-14 | Masco Corporation | Process of manufacturing seal members having a low friction coefficient |
| GB2187537A (en) * | 1985-02-12 | 1987-09-09 | Masco Corp | Process of manufacturing seal members having a low friction coefficient |
| US4758451A (en) * | 1985-12-19 | 1988-07-19 | Fried. Krupp Gmbh | Process for producing coated molded bodies |
| US4973388A (en) * | 1986-02-04 | 1990-11-27 | Preci-Coat S.A. | Method of depositing a decorative wear-resistant coating layer on a substrate |
| DE3731127A1 (en) * | 1987-03-12 | 1988-09-22 | Vac Tec Syst | Process and device for the vacuum plasma arc deposition of decorative and wear-resistant coatings |
| US5137772A (en) * | 1987-03-27 | 1992-08-11 | Nihon Sinku Gijutsu Kabusiki Kaisha | Body coated with cubic boron nitride and method for manufacturing the same |
| US5141776A (en) * | 1989-04-06 | 1992-08-25 | Merzhanov Alexandr G | Method of depositing a refractory inorganic coating on the surface of a workpiece |
| WO1990012125A1 (en) * | 1989-04-06 | 1990-10-18 | Institut Strukturnoi Makrokinetiki Akademii Nauk Sssr | Method for obtaining a refractory inorganic coating on the surface of an article |
| US5075181A (en) * | 1989-05-05 | 1991-12-24 | Kennametal Inc. | High hardness/high compressive stress multilayer coated tool |
| US5304417A (en) * | 1989-06-02 | 1994-04-19 | Air Products And Chemicals, Inc. | Graphite/carbon articles for elevated temperature service and method of manufacture |
| DE3936550C1 (en) * | 1989-11-03 | 1991-04-18 | Arthur Klink Gmbh, 7530 Pforzheim, De | Substrate coating for wear resistance - with titanium nitride in vacuum chamber contg. titanium evaporator and heater with rotary substrate holder |
| US5229193A (en) * | 1989-11-10 | 1993-07-20 | Shin-Etsu Chemical Co., Ltd. | Silicon carbide member |
| AU648781B2 (en) * | 1990-03-09 | 1994-05-05 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
| US5264297A (en) * | 1990-03-09 | 1993-11-23 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
| GB2242442B (en) * | 1990-03-09 | 1994-02-02 | Allan Matthews | Modulated composition composites produced by vapour deposition |
| GB2242442A (en) * | 1990-03-09 | 1991-10-02 | Allan Matthews | Modulated composition composites produced by vapour deposition |
| WO1991014017A1 (en) * | 1990-03-09 | 1991-09-19 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
| US5858181A (en) * | 1990-03-09 | 1999-01-12 | Kennametal Inc. | Physical vapor deposition of titanium nitride on a nonconductive substrate |
| US5288543A (en) * | 1990-09-17 | 1994-02-22 | Tdk Corporation | Protective film on sliding members and method of forming same |
| US6139964A (en) | 1991-04-22 | 2000-10-31 | Multi-Arc Inc. | Plasma enhancement apparatus and method for physical vapor deposition |
| US5458754A (en) | 1991-04-22 | 1995-10-17 | Multi-Arc Scientific Coatings | Plasma enhancement apparatus and method for physical vapor deposition |
| US5242753A (en) * | 1991-07-11 | 1993-09-07 | Praxair S.T. Technology, Inc. | Substoichiometric zirconium nitride coating |
| US5185211A (en) * | 1991-07-11 | 1993-02-09 | Praxair S.T. Technology, Inc. | Non-stoichiometric titanium nitride coating |
| US5811182A (en) * | 1991-10-04 | 1998-09-22 | Tulip Memory Systems, Inc. | Magnetic recording medium having a substrate and a titanium nitride underlayer |
| US5626920A (en) * | 1991-10-04 | 1997-05-06 | Tulip Memory Systems, Inc. | Method for coating metal disc substrates for magnetic-recording media |
| US6103367A (en) * | 1991-10-04 | 2000-08-15 | Tulip Memory Systems, Inc. | Coating of metal substrate for magnetic recording medium |
| US5308707A (en) * | 1991-10-07 | 1994-05-03 | Nitruvid | Treatment process for depositing a layer of carbon in vapour phase on the surface of a metal article and article thus obtained |
| US5635269A (en) * | 1992-04-15 | 1997-06-03 | Tulip Memory Systems, Inc. | Precision-etched textured stop/start zone for magnetic-recording disks |
| US5443892A (en) * | 1993-03-19 | 1995-08-22 | Martin Marietta Energy Systems, Inc. | Coated graphite articles useful in metallurgical processes and method for making same |
| US5707748A (en) * | 1993-07-21 | 1998-01-13 | Balzers Ag | Coated tool with increased service life |
| US5707705A (en) * | 1993-09-08 | 1998-01-13 | Tulip Memory Systems, Inc. | Titanium or titanium-alloy substrate for magnetic-recording media |
| US5961792A (en) * | 1993-09-08 | 1999-10-05 | Tulip Memory Systems, Inc. | Method for making titanium or titanium-alloy substrate for magnetic-recording media |
| US5681635A (en) * | 1994-01-20 | 1997-10-28 | Tulip Memory Systems, Inc. | Magnetic recording medium having a ceramic substrate, an underlayer having a dense fibrous zone T structure, and a magnetic layer |
| US6162500A (en) * | 1996-06-27 | 2000-12-19 | Vaw Motor Gmbh | Method of treating a casting having a casting surface |
| US6555241B1 (en) | 1996-06-27 | 2003-04-29 | Vaw Motor Gmbh | Cast aluminum part having a casting surface |
| US5928977A (en) * | 1996-12-23 | 1999-07-27 | Smh Management Services Ag | Zirconia based ceramic article as wear-resistant exterior part for wristwatch |
| US6827975B2 (en) * | 1997-06-16 | 2004-12-07 | Tdy Industries, Inc. | Method of coating cutting tools |
| US7093340B2 (en) | 1997-12-16 | 2006-08-22 | All-Clad Metalcrafters Llc | Stick resistant ceramic coating for cookware |
| US6360423B1 (en) | 1997-12-16 | 2002-03-26 | Clad Metals Llc | Stick resistant coating for cookware |
| US6432022B1 (en) | 1998-05-15 | 2002-08-13 | Alpha Getriebebau Gmbh | Low-play planetary gear mechanism |
| US6797335B1 (en) * | 1999-08-16 | 2004-09-28 | Paderov Anatol Y Nikolaevich | Method for deposition of wear-resistant coatings and for increasing the lifespan of parts |
| US20040157066A1 (en) * | 2003-02-07 | 2004-08-12 | Arzoumanidis G. Alexis | Method of applying a hardcoating typically provided on downhole tools, and a system and apparatus having such a hardcoating |
| US20040170872A1 (en) * | 2003-02-27 | 2004-09-02 | Henderer Willard E. | Coated carbide tap |
| US7147939B2 (en) * | 2003-02-27 | 2006-12-12 | Kennametal Inc. | Coated carbide tap |
| US20070154715A1 (en) * | 2003-07-16 | 2007-07-05 | Sandvik Intellectual Property Ab | Support pad for long hole drill |
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| US20050025928A1 (en) * | 2003-07-16 | 2005-02-03 | Sandvik Ab | Support pad for long hole drill |
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Also Published As
| Publication number | Publication date |
|---|---|
| DE2431448B2 (en) | 1977-07-07 |
| JPS5034610A (en) | 1975-04-03 |
| JPS5319325B2 (en) | 1978-06-20 |
| DE2431448A1 (en) | 1975-03-06 |
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