AU2006220368A1 - Metal containing diamond like carbon coating compositions - Google Patents
Metal containing diamond like carbon coating compositions Download PDFInfo
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- AU2006220368A1 AU2006220368A1 AU2006220368A AU2006220368A AU2006220368A1 AU 2006220368 A1 AU2006220368 A1 AU 2006220368A1 AU 2006220368 A AU2006220368 A AU 2006220368A AU 2006220368 A AU2006220368 A AU 2006220368A AU 2006220368 A1 AU2006220368 A1 AU 2006220368A1
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- 229910052799 carbon Inorganic materials 0.000 title claims description 37
- 229910052751 metal Inorganic materials 0.000 title claims description 31
- 239000002184 metal Substances 0.000 title claims description 31
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims description 15
- 239000008199 coating composition Substances 0.000 title claims description 14
- 229910003460 diamond Inorganic materials 0.000 title description 2
- 239000010432 diamond Substances 0.000 title description 2
- 238000000576 coating method Methods 0.000 claims description 62
- 239000000758 substrate Substances 0.000 claims description 42
- 239000011248 coating agent Substances 0.000 claims description 41
- 229910052723 transition metal Inorganic materials 0.000 claims description 20
- 150000003624 transition metals Chemical class 0.000 claims description 20
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 15
- 238000005513 bias potential Methods 0.000 claims description 12
- 239000011651 chromium Substances 0.000 claims description 12
- 239000010936 titanium Substances 0.000 claims description 12
- 239000010955 niobium Substances 0.000 claims description 11
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 11
- 229910052721 tungsten Inorganic materials 0.000 claims description 10
- 239000010937 tungsten Substances 0.000 claims description 10
- 229910052719 titanium Inorganic materials 0.000 claims description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 8
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 8
- 229910052804 chromium Inorganic materials 0.000 claims description 5
- 239000000470 constituent Substances 0.000 claims 2
- 239000010410 layer Substances 0.000 description 34
- 239000007789 gas Substances 0.000 description 19
- 239000000203 mixture Substances 0.000 description 19
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 18
- 238000000034 method Methods 0.000 description 12
- 238000000151 deposition Methods 0.000 description 10
- 229910052786 argon Inorganic materials 0.000 description 9
- 230000008021 deposition Effects 0.000 description 9
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 8
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 8
- 238000012986 modification Methods 0.000 description 5
- 230000004048 modification Effects 0.000 description 5
- 239000004215 Carbon black (E152) Substances 0.000 description 4
- 230000004075 alteration Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 238000001755 magnetron sputter deposition Methods 0.000 description 4
- 238000005137 deposition process Methods 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 239000011261 inert gas Substances 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000013034 coating degradation Methods 0.000 description 2
- 238000007373 indentation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 229910003481 amorphous carbon Inorganic materials 0.000 description 1
- 239000007900 aqueous suspension Substances 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- -1 chromium Chemical class 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 239000002019 doping agent Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 239000002346 layers by function Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000010705 motor oil Substances 0.000 description 1
- RJSRQTFBFAJJIL-UHFFFAOYSA-N niobium titanium Chemical compound [Ti].[Nb] RJSRQTFBFAJJIL-UHFFFAOYSA-N 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 238000004549 pulsed laser deposition Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 238000000992 sputter etching Methods 0.000 description 1
- 238000005477 sputtering target Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 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 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
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- Physical Vapour Deposition (AREA)
- Chemical Vapour Deposition (AREA)
Description
P001 Section 29 Regulation 3.2(2))
AUSTRALIA
Patents Act 1990 COMPLETE SPECIFICATION STANDARD PATENT Application Number: Lodged: Invention Title: Metal containing diamond like carbon coating compositions The following statement is a full description of this invention, including the best method of performing it known to us: METAL-CONTAINING DIAMOND-LIKE-CARBON COATING COMPOSITIONS CROSS-REFERENCE TO RELATED APPLICATIONS [0001] Not Applicable.
U9 FEDERALLY SPONSORED RESEARCH [0002] The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require 00 DO the patent owner to license others on reasonable terms as provided for by the terms of DAAH10-98-2-0004 awarded by the C< U.S. Army.
C- BACKGROUND OF THE INVENTION [0003] Field of Invention. The present invention relates to metal diamond-like carbon coating compositions, and more particularly, to metal diamond-like-carbon coating compositions containing an intermediate layer of a transition metal, such as chromium, or transition-metal carbide, and an exterior layer of carbon and a transition metal such as titanium, tungsten or niobium and method of making the same.
[0004] For many years, it has been known that diamond-like carbon (DLC) films are hard and have low friction coefficients especially against steel. These low A values were revealed for amorphous hydrogenated (abbreviated as a-C:H or DLC) as well as for metal containing hydrocarbon (Me-C:H or Me-DLC) films. Today, for both types of coatings, several applications, above all in the field of machine elements and of tools, are known. Besides the coating properties, it is an important aspect that DLC as well as Me-DLC coatings can be deposited at low substrate temperatures (<200C).
[0005] A comparison of DLC and Me-DLC shows that there are advantages and disadvantages to both coating materials as well as to the corresponding deposition techniques. Hard DLC EH-11239 (05-13 coatings, consisting of a highly cross-linked network of IND carbon atoms, have high compressive stress (a few GPa). The mentioned high stress values often lead to poor adhesion with the substrate, especially on steel and, therefore, limit its use in practical applications.
[0006] Many methods for the preparation of DLC films have been developed. The most commonly applied method is the radio 00 -0 frequency glow discharge of hydrocarbon gases with c n negatively self-biased substrates. However, there are several problems in the scaling up of this r.f. technique to
\O
industrially relevant dimensions and geometries.
[0007] Commonly Me-DLC films having low metal content (atomic ratios of Me/C up to approximately 0.3) have markedly lower compressive stress than a-C:H GPa). Such films consist of a network of amorphous carbon (DLC) with incorporated metal carbides. The friction coefficients of such coatings are rather similar to those of DLC coatings. However, the wear resistance of Me-DLC coatings generally is lower than that of DLC. At one time, the lowest abrasive wear rates reported for Me-DLC coatings were at least a factor of 2 higher than those reported for metal-free DLC coatings.
[0008] Generally, Me-C:H (Me-DLC) coatings are prepared in industrial batch coaters by reactive magnetron sputtering in argon-hydrocarbon gas mixtures using metal or metal carbide targets. When comparing the two types of coatings, it should be noted that the electrical resistivity of DLC coatings (>106 Q cm) is much higher than that of Me-DLC (10- 3 1 n cm) [0009] For example, a magnetron-sputtering assisted pulsed laser deposition technique was used to prepare titanium carbide and tungsten carbide containing amorphous diamond-like Eh-1123 (Ub-1 3 carbon films in an article by Voevodin et al. In another IND article, Wei et al. used a pulsed laser technique with a special target configuration, which allowed to ablate graphite and a dopant (Cu, Ti, Si). A few percent of these elements Sincorporated into the carbon matrix caused markedly improved adhesion. However, it seems to be difficult to compare the properties of the mentioned composite films to Me-DLC films containing hydrogen and prepared using different preparation 00 -0 techniques as discussed in an article entitled "Effect of target material on deposition and properties of metalcontaining DLC (Me-DLC) coatings", by K. Bewilogua, C. V.
Cooper, C. Specht, J. Schroder, R. Wittorf and M. Grischke, C- Surface Coatings Technology 127, 224-232, Elsevier (2000), which is incorporated by reference herein in its entirety.
[0010] Consequently, there exists a need for a metal diamond-like-carbon coating composition having a superior hardness and resistance to failure in pure rolling compared to commercially available metal diamond-like-carbon coating compositions.
SUMMARY OF THE INVENTION (0011] In accordance with the present invention, a metal-containing diamond-like-carbon coating composition broadly including a first layer having a first transition metal composition, and having a first surface and a second surface in contact with a substrate is provided. The coating also includes a second layer having carbon and a second transition metal selected from the group consisting of tungsten, niobium, titanium and combinations thereof, and having a first surface and a second surface in contact with the first surface of the first layer. Preferably, the thickness of coating is about 0.5 micrometer to micrometers. In addition, the composition can optionally kuz)-ij possess a low abrasive wear rate. Such low abrasive wear rate I\N should not exceed more than about 1 x 10 10 m 3 mi 'N Such a coating may be deposited using substrate bias potential having a bias potential range of about -50 to -750 volts DC.
cu t00121 It may therefore be seen that the present invention teaches a metal-containing coating having an intermediate layer comprising a transition metal and an exterior, 00 I\ functional layer comprising a transition metal and carbon.
(cN [0013] The details of one or more embodiments of the invention Sare set forth in the accompanying drawings and the description below. Other features, objects, and advantages of the invention will be apparent from the description and drawings, and from the claims.
BRIEF DESCRIPTION OF THE DRAWINGS [0014] FIG. 1 is a representation of a metal diamond-like-carbon coating having an intermediate layer and an exterior layer deposited upon a substrate comprising a rolling-contact-fatigue rod; [0015] FIG. 2 is a graph showing the relationship between metal concentration and abrasive wear rate for metal diamondlike-coating compositions containing intermediate layers of chromium and exterior layers of carbon and metals such as tungsten, titanium and niobium; [0016] FIG. 3 is a bar graph representing the adherence performance of metal diamond-like-coatings as a function of substrate bias potential; [0017] FIG. 4A is a representation of a rolling-contact-fatigue (RCF) experiment depicting a top view of the arrangement of three roughened balls positioned in I\O contact with a rotating rod coated with the compositions of Samples 1-7 as described in the Examples; and
(N
S[0018] FIG. 4B is a representation of the rolling-contact-fatigue (RCF) experiment of FIG. 4A depicting a side view of the roughened balls positioned in contact with the rotating rod.
00
NO
[0019] Like reference numbers and designations in the various (CN drawings indicate like elements.
NO
DETAILED DESCRIPTION [0020] Me-DLC coatings are deposited via magnetron sputtering, in which four targets composed of the metal of interest are installed into the interior of the deposition chamber, activated, and sputtered with Argon (Ar) and acetylene (C 2
H
2 gases. Deposition substrates, comprising rolling-contact-fatigue rods, or substrates 10, composed of a through-hardened ferrous alloy, AISI M50, are placed into the deposition chamber and negatively biased using a direct current (DC) potential ranging from about -50 to -750 volts DC. Sputtering target compositions include elemental titanium niobium and tungsten [0021] Metal hydrocarbon (Me-DLC) coatings are prepared by reactive dc magnetron sputtering in unbalanced mode housing HTC 1000/4 (ABS) coater commercially available from Hauzer Techno Coating, Venlo, The Netherlands. Before initializing the deposition runs, the residual pressure in the vacuum chamber is set at less than about 10 3 Pascal (Pa) During the deposition runs, the total gas pressure in the vacuum chamber is between about 0.3 Pa to 0.6 Pa. The substrates mentioned herein are supported within the vacuum chamber using substrate ~kJD~LJ~ holders maintained at temperatures up to about 2000C. These NO substrate holders permitted the substrate to be rotated at a rate of about twelve revolutions per minute of planetary, two-fold rotation. Throughout the entire process, the e( Sdeposition rates are typically about 2 to 3 micrometers per hour.
[0022] The Me-DLC deposition process generally comprises four 00 NO steps. First, the substrates are cleaned using an Argon etching process at a pressure of about 0.3 Pa as known to one C-i of ordinary skill in the art. For this step, argon gas is
\O
admitted to the chamber until the achievement of the desired C-i gas flow rate and/or chamber pressure, generally about 300 standard cubic centimeters per minute (sccm) and 0.3 Pa, respectively, and ionized to produce Ar+ ions for sputter cleaning the substrate surface.
[0023] Second, an intermediate layer 12 composed of a transition metal, in this case chromium is then sputter deposited upon the Ar-ion-etched substrates. During this second stage of the deposition process, the DC current applied to one or more targets composed of chromium metal is held constant at the target value. For this process step, argon gas is introduced into the chamber and held constant until the intermediate layer had grown to achieve its target thickness.
As for the Ar-ion-etching stage, the flow rate and partial pressure of argon for this second process step are, respectively, approximately 300 sccm and 0.3-0.6 Pa, respectively. As these deposition conditions are maintained, chromium metal is sputter deposited onto the substrate surface until the achievement of a desired thickness. Typically, the deposited transition-metal intermediate layer possesses a thickness of at least about 10 nanometers (0.01 micrometers) and no more than about 2000 nanometers (2.0 micrometers) and
UD-_L_'
preferably about 100 nanometers (0.1 micrometers) to 300 NO nanometers (0.3 micrometers).
[0024] Third, the dc current applied to the chromium metal Stargets is decreased until reaching zero. The mixture of reactive gases is flushed from the vacuum chamber in preparation for the sputter deposition of the exterior layer.
A quantity of argon gas is again introduced into the chamber, 00 O and a quantity of acetylene gas is then introduced until the ratio of argon gas to acetylene gas is approximately 1:1 or a 50/50 mixture. Generally, the amount of acetylene gas present Nin the reactive gas mixture is about fifteen percent to forty-five percent by volume of the chamber.
[0025] Fourth, an exterior layer 14 of the metal diamond-like-carbon coating composition is then sputter deposited upon the intermediate layer of the substrates. The DC current is applied gradually, that is, starting from zero and gradually increasing in intensity, to one or more targets composed of a metal such as tungsten, niobium, titanium and combinations thereof. Again, a quantity of argon gas is initially introduced into the chamber and then a quantity of acetylene gas is introduced until the ratio of argon gas to acetylene gas is approximately 1:1. Again, the amount of acetylene gas generally present in the mixture is about fifteen percent to forty-five percent by volume of the chamber. During the transition from pure inert gas to a combination of inert gas and acetylene or following the achievement of final acetylene-inert gas mixture, target metal begins being sputter deposited upon a first surface, that is, the exterior surface, of the intermediate layer of transition metal on each substrate until a desired thickness is achieved.
These processing conditions result in the deposition of a Me-DLC coating containing an atomic metal-to-carbon (Me/C) Thfl~LLZ.)Y \~JD±2 ratio in the range of 0.1 to 0.8. For purposes of illustration and not to be taken in a limiting sense, the deposited exterior layer may possess a thickness of about 0.1 micrometer to 10 micrometers. The resulting metal-containing diamondlike-carbon coating composition deposited upon the substrate material is illustrated in FIG. 1. As depicted, a second surface, that is, the interior surface, of the exterior layer is in contact with the first surface or exterior surface of the intermediate layer whose second surface, that is, the interior surface is in contact with the exterior surface of the substrate.
[0026] EXPERIMENTAL RESULTS [0027] Abrasive Wear Rate [0028] Referring now to FIG. 2, an abrasive wear rate was determined for several planar samples of substrates having various metal diamond-like-carbon coating compositions deposited thereupon in accordance with the method described herein and compared to a substrate coated with a vendor-supplied metal diamond-like-carbon coating (Balzerso Balinit [0029] A Calo tester operating with an aluminum oxide (A1 2 03) and water suspension was utilized to calculate the abrasive wear rate for Samples 1-7. To quantify the results, the volume of coating removed by the Calo device, generated by a rotating ball, was divided by the normal force and the track length of the rotating ball.
[0030] Sample 1, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited thereupon an intermediate layer of chromium metal (Cr) having Cn-IILjY iU~-i~ a thickness of 0.1 micrometers and an exterior layer of \D titanium (Ti) diamond-like-carbon composition having a thickness of 1 micrometer.
[0031] Sample 2, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited thereupon an intermediate layer of chromium metal (Cr) having a thickness of 0.3 micrometers and an exterior layer of 00 \D titanium (Ti) diamond-like-carbon composition having a Sthickness of 3 micrometers.
(N
S[0032] Sample 3, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited thereupon an intermediate layer of chromium metal (Cr) having a thickness of 0.1 micrometers and an exterior layer of tungsten diamond-like-carbon composition having a thickness of 1 micrometer.
[0033] Sample 4, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited thereupon an intermediate layer of chromium metal (Cr) having a thickness of 0.3 micrometers and an exterior layer of tungsten diamond-like-carbon composition having a thickness of 3 micrometers.
[0034] Sample 5, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited thereupon an intermediate layer of chromium metal (Cr) having a thickness of 0.1 micrometers and an exterior layer of niobium (Nb) diamond-like-carbon composition having a thickness of 1 micrometer.
[0035] Sample 6, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 having deposited hEh-112J (Ub-1 thereupon an intermediate layer of chromium metal (Cr) having \D a thickness of 0.3 micrometers and an exterior layer of niobium (Nb) diamond-like-carbon composition having a thickness of 3 micrometers.
[0036] Sample 7, representative of substrate 10, is a rolling-contact-fatigue rod made of AISI M50 coated with an intermediate layer of chromium metal (Cr) having a thickness 00 \D of 0.3 micrometers and an exterior layer of Balinit from SBalzers Inc. of Elgin, Illinois, whose international headquarters is located in the Principality of Liechtenstein,
IO
Sa tungsten diamond-like-carbon coating having a thickness C( of 3 micrometers, deposited using a floating potential.
[0037] The abrasive wear rate of samples 3 and 4 (W-DLC) is significantly lower than the abrasive wear rate for other compositions. The metal-to-carbon ratio of both samples 3 and 4 is much lower than for the metal-to-carbon ratios of the other samples. For the deposition of samples 3 and 4, the resulting abrasive wear rate was strongly independent of the bias potential over a range of -100 to -120 V DC, showing an abrasive wear rate-of less than or equal to 1 x 10 15 m 3 m- N Given the metal-to-carbon ratios of about 0.1 to 0.3 and resulting high metal content, in the same range as the metal content of the Balzers@ Balinit C® coating, the resulting W-DLC coatings of samples 3 and 4 demonstrate unexpected results in light of prior documented research by the inventors of record.
Moreover, these abrasive wear rate results constitute a distinct advantage over the other compositions investigated.
When compared to the standard, vendor-supplied W-DLC coating (Balzersa Balinit C) samples 3 and 4 are also superior to sample 7. The abrasive wear rates of samples 3 and 4 are greater than one order of magnitude to the abrasive wear rate range of 15-20 x 10 15 m 3 m' 1 N measured for sample 7. As demonstrated, a Me-DLC coating, and more specifically a W-DLC ND coating, applied using a negative bias potential as opposed to a floating bias potential, for example, sample 7, Balinit C from Balzers Inc., exhibits far superior abrasive wear rate e( Sresults.
[0038] Adherence Performance 00 ID [0039] Referring now to FIG. 3, an adherence performance value was determined for Samples 1-6.
IND
(0040] The adherence performance of the coatings was carried C-i out by means of static Rockwell indentation at a 150 kilogram load. According to the well known VDI classification, a value of HF-l indicates excellent adherence, and a value of HF-6 indicates complete delamination around the indentation.
[0041] Samples 3 and 4 demonstrate superior adherence over a substrate bias potential range of -100 volts to -500 volts when compared to both the Ti-containing DLC and Nb-containing DLC coatings. Moreover, the results indicate that the adherence is essentially invariant with the substrate bias potential, which is an advantage in the processing of larger parts.
[0042] Generally, as the distance from target-to-substrate increases, as may be the case for the processing of large parts, for example, the atoms sputtered from the metal targets lose kinetic energy as they traverse the distance from target to substrate. This argues in favor of applying a higher substrate bias potential when coating large parts. However, with other compositions and deposition processes parameters, the use of higher substrate bias potentials leads to coating degradation; for example, the coating adherence becomes EH-1123 kOb-13 inferior. As shown in FIG. 3, the W-DLC coatings of samples 3 \D and 4 do not exhibit coating degradation.
[0043] Rolling-Contact-Fatigue cu [0044] Finally, this family of W-DLC coatings exhibits a dramatic improvement in rolling-contact-fatigue (RCF) performance compared to the standard, vendor-supplied W-DLC 00 ND coating (Balzers Balinit C) ci C( [0045] A representation of an RCF experiment performed in I accordance with the present invention is illustrated in FIGS.
C- 4A and 4B. Three roughened balls (B 1
B
2
B
3 0.5 inches (12.7 mm) in diameter, are radially loaded within a pair of bearing cups (Bc 1 and Be2) against the rolling-contact-fatigue rod (R 1 0.375 inches (9.525 mm) in diameter, of sample 1 (as described above). A clamping force is applied to the bearing cups (Bc 1 Bc2) causing a radial load to be applied between the roughened balls and the rod. The rod is rotated at three thousand six hundred revolutions per minute (3,600 rpm) in a direction (DI) on its longitudinal axis (L 1 while being drip lubricated with oil conforming to MIL-L-23699, a synthetic turbine engine lubricant employed by the United States military.
[0046] Each rolling-contact-fatigue rod of samples 1-7 was subjected to 5 x 106 cycles to determine the highest amount of applied contact stress, or the rolling-contact stress limit (RCSL), required to induce failure. The RCSL for the standard, vendor-supplied W-DLC coating (Balzers® Balinit was determined to be 400 Ksi (2.76 GPa). The RCSL for the W-DLC coating was 700 Ksi (4.83 GPa). The RCSL for the Ti-DLC coating was 800 Ksi (5.52 GPa). The RCSL for the Nb-DLC coating was 400 Ksi (2.76 GPa).
i h-iI23_9 Ub-12 ID [0047] When translated into a constant contact stress level of approximately 400 Ksi (2.76 GPa), it is estimated that the increase in RCSL for a W-DLC or Ti-DLC coated part would e( Sresult in an increase in the rolling-contact-fatigue life of the part of between about 10 and 15 times greater than the rolling-contact-fatigue life delivered by the standard, vendor-supplied W-DLC coating (BalzersD Balinit C®) 00
\O
[0048] Although an exemplary embodiment of the present C-i invention has been shown and described with reference to
\O
Iparticular embodiments and applications thereof, it will be apparent to those having ordinary skill in the art that a number of changes, modifications, or alterations to the invention as described herein may be made, none of which depart from the spirit or scope of the present invention. All such changes, modifications, and alterations should therefore be seen as being within the scope of the present invention.
[0049] Although the foregoing description of the present invention has been shown and described with reference to particular embodiments and applications thereof, it has been presented for purposes of illustration and description and is not intended to be exhaustive or to limit the invention to the particular embodiments and applications disclosed. It will be apparent to those having ordinary skill in the art that a number of changes, modifications, variations, or alterations to the invention as described herein may be made, none of which depart from the spirit or scope of the present invention. The particular embodiments and applications were chosen and described to provide the best illustration of the principles of the invention and its practical application to thereby enable one of ordinary skill in the art to utilize the invention in various embodiments and with various t'ki-112jj UD-Ij modifications as are suited to the particular use I\ contemplated. All such changes, modifications, variations, and alterations should therefore be seen as being within the scope of the present invention as determined by the appended Sclaims when interpreted in accordance with the breadth to which they are fairly, legally, and equitably entitled.
00
IND
ND
0q
Claims (14)
- 2. The coating according to Claim 1, wherein said second transition metal is selected from the group consisting of tungsten, niobium, titanium and combinations thereof.
- 3. The coating according to Claim 1, wherein said first transition metal is chromium.
- 4. The coating according to Claim 1, wherein said second layer has a thickness of about 0.5 micrometers to micrometers. The coating according to Claim 1, wherein said first layer has a thickness of about 0.01 micrometers to 2.0 micrometers.
- 6. The coating according to Claim 1, wherein said second layer has a low abrasive wear rate.
- 7. The coating according to Claim 6, wherein said low abrasive wear rate is less than 1 x 10 1 m 3 m- 'N Eh-1239 (Ob-13
- 8. The coating according to Claim 1, wherein said second layer is deposited using a substrate bias potential having a range of about -50 volts to -750 volts. e(
- 9. The coating according to Claim 1, wherein said second layer has a metal to carbon ratio of about 0.1 to 0.8. The coating according to Claim 1, wherein said first 00 layer and second layer possess a rolling-contact stress limit of at least 4 gigapascals. \O
- 11. A diamond-like-carbon coating composition having a transition-metal constituent, comprising: a substrate; a first layer comprising a first transition metal, and having a first surface and a second surface in contact with said substrate, wherein said first layer and second layer possess a rolling-contact stress limit of at least 4 gigapascals; and a second layer comprising carbon and a second transition metal.
- 12. The coating according to Claim 11, wherein said second transition metal is selected from the group consisting of tungsten, niobium, titanium and combinations thereof.
- 13. The coating according to Claim 11, wherein said first transition metal is chromium.
- 14. The coating according to Claim 11, wherein said second layer has a thickness of about 0.5 micrometers to micrometers. Vh 112 j O k U b 13 The coating according to Claim 11, wherein said first ks0 layer has a thickness of about 0.01 micrometers to micrometers. S16. The coating according to Claim 11, wherein said second layer has a low abrasive wear rate.
- 17. The coating according to Claim 16, wherein said low 00 \0 abrasive wear rate is less than 1 x 10-10 m 3 m-'N 1 (Nc
- 18. The coating according to Claim 11, wherein said second \O layer is deposited using a substrate bias potential having a C- range of about -50 volts to -750 volts.
- 19. The coating according to Claim 11, wherein said second layer has a metal to carbon ratio of about 0.1 to 0.8. A diamond-like-carbon coating composition having a transition-metal constituent, comprising: a substrate; a first layer comprising a first transition metal, and having a first surface and a second surface in contact with said substrate, wherein said first layer and second layer possess a rolling-contact stress limit of at least 4 gigapascals; and a second layer comprising carbon and a second transition metal, wherein said second layer has a low abrasive wear rate.
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| AU2006220368A AU2006220368A1 (en) | 2006-09-14 | 2006-09-14 | Metal containing diamond like carbon coating compositions |
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| Application Number | Priority Date | Filing Date | Title |
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| AU2006220368A AU2006220368A1 (en) | 2006-09-14 | 2006-09-14 | Metal containing diamond like carbon coating compositions |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117904581A (en) * | 2024-03-15 | 2024-04-19 | 中南大学 | High-strength and high-toughness nano multilayer metal composite material and gradient interface design method thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117904581A (en) * | 2024-03-15 | 2024-04-19 | 中南大学 | High-strength and high-toughness nano multilayer metal composite material and gradient interface design method thereof |
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