NL2000115C2 - Wear resistant assembly comprising layers of tungsten carbide and tungsten carbide stabilized diamond like carbon, has specific thickness for two adjacent layers - Google Patents
Wear resistant assembly comprising layers of tungsten carbide and tungsten carbide stabilized diamond like carbon, has specific thickness for two adjacent layers Download PDFInfo
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- NL2000115C2 NL2000115C2 NL2000115A NL2000115A NL2000115C2 NL 2000115 C2 NL2000115 C2 NL 2000115C2 NL 2000115 A NL2000115 A NL 2000115A NL 2000115 A NL2000115 A NL 2000115A NL 2000115 C2 NL2000115 C2 NL 2000115C2
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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
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
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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
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
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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
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/3492—Variation of parameters during sputtering
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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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
- C23C28/044—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
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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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
- C23C28/046—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material with at least one amorphous inorganic material layer, e.g. DLC, a-C:H, a-C:Me, the layer being doped or not
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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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/40—Coatings including alternating layers following a pattern, a periodic or defined repetition
- C23C28/42—Coatings including alternating layers following a pattern, a periodic or defined repetition characterized by the composition of the alternating layers
Abstract
Description
Meerlaags WC-WC gestabiliseerd DLCMulti-layer WC-WC stabilized DLC
De onderhavige uitvinding heeft betrekking op een slijtvast meerlaags samenstel omvattende afwisselend wolfraamcarbide-wolfraamcarbide gestabiliseerd diamantach-5 tige koolstoflagen. Meerlaagse structuren omvattende wolfraamcarbide, wolfraam-carbide gestabiliseerde diamantachtige koolstof zijn in de stand der techniek bekend en worden op een substraat gesputterd, dat bij voorkeur een stalen substraat omvat. Op deze wijze kunnen slijtvaste lagen verkregen worden. Dergelijke slijtvaste en wrijving verminderende bekledingen zijn voor allerlei soorten toepassingen van belang en kun-10 nen onder de meeste omstandigheden smering ten minste gedeeltelijk vervangen. Wolfraamcarbide gestabiliseerd diamantachtige koolstof heeft een lage wrijvingscoëffi-ciënt, is chemisch inert, heeft hoge slijtvastheid en hoge hardheid in vergelijking met algemeen bekende conventionele beschermende bekledingen.The present invention relates to a wear-resistant multi-layer assembly comprising alternately tungsten carbide-tungsten carbide stabilized diamond-like carbon layers. Multi-layer structures comprising tungsten carbide, tungsten carbide-stabilized diamond-like carbon are known in the art and are sputtered onto a substrate, which preferably comprises a steel substrate. Wear-resistant layers can be obtained in this way. Such wear-resistant and friction-reducing coatings are important for all kinds of applications and can at least partially replace lubrication under most circumstances. Tungsten carbide stabilized diamond-like carbon has a low coefficient of friction, is chemically inert, has high abrasion resistance and high hardness compared to well-known conventional protective coatings.
Hechting tussen het substraat en het meerlaagse samenstel is van wezenlijk be-15 lang en gebleken is dat in het bijzonder bij de wisselende temperatuur aanzienlijke spanningen aanwezig zijn tussen het substraat en het meerlaags samenstel.Adhesion between the substrate and the multilayer assembly is of substantial importance and it has been found that considerable stresses are present between the substrate and the multilayer assembly, in particular at the varying temperature.
Om de hechting te vergroten tussen het meerlaags samenstel en het substraat wordt het gebruik van hechtingslagen voorgesteld.To increase the adhesion between the multi-layer assembly and the substrate, the use of adhesive layers is proposed.
In de stand der techniek wordt aangenomen dat door het verminderen van de 20 dikte van de lagen van het meerlaags samenstel de totale spanning in de richting van drukspanning verschuift, omdat elk scheidingsvlak tussen twee lagen verdere druk-spanning zal geven. Bij het verminderen van de behandelingstijd om elk van de lagen aan te brengen, zullen vanaf een bepaald punt niet langer afzonderlijke lagen ontstaan maar zal een gemengde structuur verkregen worden. Een dergelijke gemengde structuur 25 voldoet echter niet aan de eisen van dichtheid, hardheid en drukspanning.It is assumed in the prior art that by reducing the thickness of the layers of the multi-layer assembly, the total stress shifts in the direction of compressive stress, because each interface between two layers will give further compressive stress. When reducing the treatment time to apply each of the layers, separate layers will no longer arise from a certain point, but a mixed structure will be obtained. However, such a mixed structure does not meet the requirements of density, hardness and compressive stress.
Gezien het bovenstaande is het doel van de uitvinding in een wolfraamcarbide-wolfraamcarbide gestabiliseerd diamantachtige koolstof meerlaagse structuur te voorzien die geoptimaliseerde sterkte-eigenschappen heeft.In view of the above, the object of the invention is to provide a tungsten carbide-tungsten carbide stabilized diamond-like carbon multilayer structure that has optimized strength properties.
Volgens de uitvinding wordt een slijtvast meerlaags samenstel voorgesteld zoals 30 hierboven beschreven, waarbij de dikte van twee aangrenzende lagen van dat meerlaagse samenstel ligt tussen 5 en 10 nm.According to the invention, a wear-resistant multi-layer assembly is described as described above, wherein the thickness of two adjacent layers of said multi-layer assembly is between 5 and 10 nm.
Verrassenderwijs is gebleken dat indien de dikte van de laag verhoudingsgewijs dichtbij het mengpunt van de lagen gekozen wordt, de spanning in de meerlaagse 2 00 0 1 15 2 structuur aanzienlijk minder compressief zal zijn. Gebaseerd op proeven uitgevoerd in de stand der techniek werd aangenomen dat de druksterkte in een meerlaagse constructie langzaam zou afhemen naar het punt waar mengen van de structuren ontstaat. Echter bleek uit proeven van aanvraagster dat dit niet juist is en dat 5 verrassenderwijs een minimum in drukspanning bestaat nabij het punt waar het mengen van de structuren plaatsvindt.Surprisingly, it has been found that if the thickness of the layer is chosen relatively close to the mixing point of the layers, the tension in the multilayer structure will be considerably less compressive. Based on tests conducted in the prior art, it was believed that the compressive strength in a multilayer construction would slow down to the point where mixing of the structures occurs. However, tests by the applicant showed that this is not correct and that surprisingly a minimum pressure pressure exists near the point where the mixing of the structures takes place.
Volgens een voorkeursuitvoering van de uitvinding heeft de dunste van de aangrenzende lagen van de meerlaagse structuur een dikte van ten minste 2,5 nm. Bij voorkeur hebben beide aangrenzende lagen dezelfde dikte.According to a preferred embodiment of the invention, the thinnest of the adjacent layers of the multilayer structure has a thickness of at least 2.5 nm. Both adjacent layers preferably have the same thickness.
10 De uitvinding heeft eveneens betrekking op een werkwijze voor het vervaardigen van een dergelijk slijtvast meerlaags samenstel. Bij voorkeur wordt dit door sputteren verwezenlijkt en tijdens het sputteren wordt een wijziging in omstandigheden verwezenlijkt om de meerlaagse structuur voort te brengen. Dit kan bijvoorbeeld verwezenlijkt worden door het toevoegen van acetyleen, dat periodiek aan- en uitgeschakeld 15 wordt. Een andere mogelijkheid is het plaatsen van het substraat op een draaiende tafel waarbij het substraat periodiek aan het effect van sputteren onderworpen wordt. Sputteren kan met een of twee targets verwezenlijkt worden. Volgens de uitvinding wordt de verandering in sputteromstandigheden elke 30 sec -1 min verwezenlijkt. Dit betekent dat elke sputterperiode van een of twee lagen van de meerlaagse constructie 30 sec - 1 20 min duurt.The invention also relates to a method for manufacturing such a wear-resistant multi-layer assembly. This is preferably achieved by sputtering and during sputtering a change in circumstances is realized to produce the multilayer structure. This can be achieved, for example, by adding acetylene, which is periodically switched on and off. Another possibility is to place the substrate on a rotating table whereby the substrate is periodically subjected to the effect of sputtering. Sputtering can be achieved with one or two targets. According to the invention, the change in sputtering conditions is realized every 30 seconds -1 minutes. This means that each sputtering period of one or two layers of the multi-layer construction lasts 30 seconds - 1 20 minutes.
Volgens een verdere voorkeursuitvoering van de uitvinding wordt een op chroom gebaseerde hechting bevorderende laag aangebracht op het (stalen) substraat alvorens het meerlaags samenstel neer te slaan.According to a further preferred embodiment of the invention, a chromium-based adhesion promoting layer is applied to the (steel) substrate before depositing the multi-layer assembly.
De uitvinding zal verder verduidelijkt worden verwijzend naar de grafieken ge-25 toond in de figuren, waarbij:The invention will be further clarified with reference to the graphs shown in the figures, wherein:
Fig. 1 de resultaten van proeven toont om meerlaagse structuren te verkrijgen met wisselende acetyleenstroommodulaties in minuten;FIG. 1 shows the results of tests to obtain multi-layer structures with varying acetylene flow modulations in minutes;
Fig. 2 dezelfde grafiek toont waarbij de dikte van de ontstaande lagen is weergegeven; en 30 Fig. 3 een experimentele opstelling voor het sputteren toont.FIG. 2 shows the same graph showing the thickness of the layers formed; and FIG. 3 shows an experimental arrangement for sputtering.
Uit fig. 1 en 2 kan geconcludeerd worden dat de druksterkte niet geleidelijk daalt vanaf lagen met grotere dikte in een meerlaagse constructie naar -1,6 GPa bij volledig mengen maar een onverwachte piek heeft die een lagere drukspanning tot gevolg heeft.It can be concluded from Figs. 1 and 2 that the compressive strength does not gradually decrease from layers of greater thickness in a multi-layered structure to -1.6 GPa with full mixing, but has an unexpected peak that results in a lower compressive stress.
33
Nabij deze piek kan steeds duidelijk onderscheid gemaakt worden tussen wolffaamcar-bide en met wolffaamcarbide gestabiliseerde diamantachtige koolstoflagen. De spanning werd gemeten zoals beschreven in het artikel "Measurement and Interpretation of Stress in Aluminium-Based Metallization as a Function of Thermal History in IEEE 5 Transactions on Electron Devices, Vol. ED-34, nr. 3, maart 1987.Near this peak, a clear distinction can always be made between wolffaam carbide and wolffaam carbide stabilized diamond-like carbon layers. The voltage was measured as described in the article "Measurement and Interpretation of Stress in Aluminum-Based Metallization as a Function of Thermal History in IEEE 5 Transactions on Electron Devices, Vol. ED-34, No. 3, March 1987.
Dergelijke lagen of bekledingen kunnen bijvoorbeeld vervaardigd worden via niet gebalanceerd reactief magnetronsputteren in het ATC 1500 F sputterstelsel (AJA Int.).Such layers or coatings can be made, for example, via unbalanced reactive microwave sputtering in the ATC 1500 F sputtering system (AJA Int.).
In fig. 3 is schematisch een experimentele opstelling getoond gebruikt bij het 10 vervaardigen van de monsters volgens grafiek 1 en 2. Een lagedrukkamer heeft verwij-zingscijfer 1 terwijl een wolfraamcarbidetarget 2 en chroomtarget 3 aanwezig zijn. Het substraat moet geplaatst worden op een draaitafel 4, waarbij een gasinlaat voor acetyleen met 5 aangegeven is.Fig. 3 schematically shows an experimental arrangement used in the production of the samples according to graphs 1 and 2. A low-pressure chamber has reference numeral 1 while a tungsten carbide target 2 and chromium target 3 are present. The substrate must be placed on a turntable 4, with a gas inlet for acetylene indicated by 5.
Proeven werden uitgevoerd waarbij als substraat een siliciumwafer gebruikt 15 wordt. Een dergelijke siliciumwafer is zeer gevoelig voor spanningen en kan gemakkelijk gebogen worden. De kromming is een maat voor de daarin ingebrachte spanning. Een 4 inch wafer werd gebruikt tijdens de beproevingen en de totale sputtertijd was 2 uur. De druk in de kamer voor neerslag was 10 maal 10'5 Pa en het wafersubstraat werd verwarmd tot een temperatuur van 160aC gedurende 90 min. Tijdens de neerslag werd 20 de temperatuur op ongeveer 160eC gehandhaafd en het HF-vermogen op het wolfraamcarbidetarget is 148 W. De diameter van het target was 5,04 cm. Om hechting te bevorderen werd eerst een chroomlaag neergeslagen op de siliciumwafer met een dikte van ongeveer 300 nm. De argongasflow werd constant op 35 sccm gehouden, terwijl 5 sccm acetyleengasstroming tussen 4 sec en 10 min gemoduleerd werd. Benadrukt moet 25 worden dat de juistheid van de theorie achter het waargenomen verschijnsel met de onderhavige uitvinding als gevolg niet doorslaggevend is met betrekking tot de geldigheid van de bijgevoegde conclusies. Bovendien is het duidelijk dat de omvang van de bescherming van de onderhavige aanvrage zich uitbreidt tot de conclusies en combinatie van de conclusies met andere uit de stand der techniek bekende maatregelen, die 30 voor de hand liggend zijn gezien het bovenstaande voor degene bekwaam in de stand der techniek.Tests were carried out using a silicon wafer as substrate. Such a silicon wafer is very sensitive to stresses and can easily be bent. The curvature is a measure of the voltage introduced therein. A 4 inch wafer was used during the tests and the total sputtering time was 2 hours. The pressure in the precipitation chamber was 10 times 10 -5 Pa and the wafer substrate was heated to a temperature of 160 ° C for 90 minutes. During the precipitation, the temperature was maintained at approximately 160 ° C and the HF power on the tungsten carbide target is 148 W The diameter of the target was 5.04 cm. To promote adhesion, a chromium layer was first deposited on the silicon wafer with a thickness of approximately 300 nm. The argon gas flow was kept constant at 35 sccm, while 5 sccm acetylene gas flow was modulated between 4 sec and 10 min. It should be emphasized that the accuracy of the theory behind the observed phenomenon with the present invention is consequently not decisive with regard to the validity of the appended claims. Moreover, it is clear that the scope of the protection of the present application extends to the claims and combination of claims with other measures known from the prior art, which are obvious in view of the above for those skilled in the art. engineering.
2 00 0 1 152 00 0 1 15
Claims (11)
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NL2000115A NL2000115C2 (en) | 2006-06-27 | 2006-06-27 | Wear resistant assembly comprising layers of tungsten carbide and tungsten carbide stabilized diamond like carbon, has specific thickness for two adjacent layers |
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NL2000115A NL2000115C2 (en) | 2006-06-27 | 2006-06-27 | Wear resistant assembly comprising layers of tungsten carbide and tungsten carbide stabilized diamond like carbon, has specific thickness for two adjacent layers |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN108611613A (en) * | 2018-06-09 | 2018-10-02 | 中国科学院兰州化学物理研究所 | A kind of preparation method of nano-multilayered structures carbon-base film |
Citations (2)
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US5947710A (en) * | 1995-12-07 | 1999-09-07 | Carrier Corporation | Rotary compressor with reduced lubrication sensitivity |
EP1123989A2 (en) * | 2000-02-09 | 2001-08-16 | Hauzer Techno Coating Europe Bv | Method for producing coatings as well as object |
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2006
- 2006-06-27 NL NL2000115A patent/NL2000115C2/en not_active IP Right Cessation
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US5947710A (en) * | 1995-12-07 | 1999-09-07 | Carrier Corporation | Rotary compressor with reduced lubrication sensitivity |
EP1123989A2 (en) * | 2000-02-09 | 2001-08-16 | Hauzer Techno Coating Europe Bv | Method for producing coatings as well as object |
Non-Patent Citations (3)
Title |
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PAULEAU Y ET AL: "Structure and mechanical properties of hard W-C coatings deposited by reactive magnetron sputtering", SURFACE AND COATINGS TECHNOLOGY SWITZERLAND, vol. 54-55, no. 1-3, 16 November 1992 (1992-11-16), pages 324 - 328, XP002420460, ISSN: 0257-8972 * |
PUJADA B R ET AL: "Density, stress, hardness and reduced Young's modulus of W-C:H coatings", SURF. COAT. TECHNOL.; SURFACE AND COATINGS TECHNOLOGY DEC 20 2006, vol. 201, no. 7 SPEC. ISS., 20 December 2006 (2006-12-20), pages 4284 - 4288, XP002420461 * |
RINCON C ET AL: "Effects of carbon incorporation in tungsten carbide films deposited by r.f. magnetron sputtering: single layers and multilayers", SURFACE & COATINGS TECHNOLOGY ELSEVIER SWITZERLAND, vol. 163-164, 30 January 2003 (2003-01-30), pages 386 - 391, XP002420459, ISSN: 0257-8972 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108611613A (en) * | 2018-06-09 | 2018-10-02 | 中国科学院兰州化学物理研究所 | A kind of preparation method of nano-multilayered structures carbon-base film |
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