Classifications

• • 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
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
  • C23C16/30—Deposition of compounds, mixtures or solid solutions, e.g. borides, carbides, nitrides
  • C23C16/40—Oxides
  • C23C16/401—Oxides containing silicon
• • 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
• • 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
  • C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
  • C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
  • C23C16/46—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating characterised by the method used for heating the substrate
• • 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
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
  • Y02T50/00—Aeronautics or air transport
  • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Definitions

• the present invention relates to plastic glazing. Their interest is for example linked to a search for lightening on various types of vehicles or to obtaining complex shapes.
• Various transparent plastics can be used, such as polycarbonate, polymethyl methacrylate, polypropylene, polyurethane, polyvinyl butyral, poly (ethylene glycol terephthalate), poly (butylene glycol terephthalate), ionomer resin such as ethylene / neutralized (meth) acrylic acid copolymer with a polyamine, cycloolefinic copolymer such as ethylene / norbornene or ethylene / cyclopentadiene, polycarbonate / polyester copolymer, ethylene / vinyl acetate copolymer and the like, alone or in mixtures.
• the relative scratchability of plastic substrates justifies the almost generalized formation of anti-scratch protective coatings in applications such as glazing.
• the coatings consisting for example of carbon, hydrogen, silicon and oxygen, can be formed according to any known process for depositing thin layers, in particular exothermic deposition techniques, under vacuum, at more or less reduced or atmospheric pressure; in this regard, the PECVD (Plasma Enhanced Chemical Vapor Deposition) processes can be cited hereinafter referred to as plasma CVD, electron beam evaporation, sputtering magnetron, ionically assisted CVD, ion source CVD, etc.
• These layers may contain anti-UV agents and / or be associated with one or more other functional layers.
• the inventors have noted the creation of particularly sensitive microcracks for layers with good abrasion and scratch resistance and all the more important that the glazing is used at high temperature, the ranges of use generally accepted for motor vehicles. being from -30 ° C to 90 ° C, or more generally -40 ° C to 100 ° C, and from -70 ° C to 100 ° C for aircraft.
• application EP 1 022 354 A2 describes the heating of the plastic substrate prior to the formation of a layer by plasma CVD without even mentioning any possible creation of cracks.
• the inventors have now defined the criteria making it possible to delay considerably, if not to suppress the formation of cracks, even when the plastic glazing is used at relatively high temperatures, of the order of 100 ° C. for example.
• the subject of the invention is a process for forming a coating on at least part of a plastic substrate, distinguished by the fact of being carried out at a temperature at least equal to the maximum temperature of use of the coated substrate minus 20 ° C.
• This temperature is that at which the substrate itself is stabilized from the start of the actual formation of the coating.
• the creation of microcracks is considerably delayed even when the coated substrate is used at high temperature, of the order of 100 ° C. and more in particular.
• the method implements a plasma CVD.
• a coating based on silicon, oxygen, carbon, hydrogen among others, and with adjustable properties is obtained from one or more precursors such as silane, hexamethyldisiloxane, tetramethyldisiloxane ...
• This technique also makes it easy to form stacks of layers.
• the process is carried out at a temperature at least equal to the maximum temperature for using the coated substrate.
• the coating is formed at a temperature generally not exceeding 125 ° C, or up to 135 ° C for particular grades.
• the process is carried out at a temperature as close as possible to this degradation temperature of the plastic.
• cooling means are used to avoid reaching the degradation temperature of the plastic.
• This use is then particularly advantageous when proceeding according to the previous embodiment, as close as possible to this degradation temperature. It can provide sufficient deposition time to obtain the required thicknesses, in several or even all at once.
• an advantageous embodiment consists in forming the coating in several stages.
• the method comprises the operations consisting successively of a) stabilizing the substrate to be coated at a temperature at least equal to its maximum operating temperature minus 20 ° C., b) forming the coating while ensuring that the temperature of the substrate does not reach the degradation temperature of the plastic, c) repeat operations a) and b) if necessary, depending on the thickness and other characteristics desired for the coating.
• the substrate is made of polycarbonate, the coating being formed at a temperature at least equal to 120 ° C.
• the subject of the invention is also a product comprising a plastic substrate provided with a coating formed according to the method described above, the average thickness of the coating being at least 2 ⁇ m, preferably at least 4 ⁇ m, and particularly preferably at least 6 ⁇ m.
• Another object of the invention is the application of this product as a piece of plastic material which is not necessarily transparent such as a bodywork (door, fender, bonnet, deflector or equivalent in applications other than automotive), as glazing, in particular for land, water or air vehicle, in particular for motor vehicle, safety glazing for helmet or of the type requiring resistance in the heat.
• a bodywork door, fender, bonnet, deflector or equivalent in applications other than automotive
• glazing in particular for land, water or air vehicle, in particular for motor vehicle, safety glazing for helmet or of the type requiring resistance in the heat.
• the application of glazing of the invention for buildings or urban furniture - advertising billboards, bus shelters, etc. - is also interesting.
• the invention is illustrated by the following embodiment.
• EXAMPLE A polycarbonate sheet 300 X 850 mm and 4 mm thick, sold by the Bayer Company under the registered trademark Makrolon, is subjected to the deposition of a coating by plasma CVD.
• the deposit chamber is equipped with a microwave plasma source of 350
• the coating is formed according to the following four steps:
• the temperature reached by the substrate at the end of steps 2 and 4 is 124-125 ° C, that is to say just below the softening temperature of the polycarbonate.
• it omits to act on the temperature of the substrate: 5 ⁇ m of coating is deposited in a single operation.
• the substrate temperature ranges from around 20 ° C (room temperature) to 85 ° C.
• the substrate is initially heated to 120 ° C, but a thickness of 5 ⁇ m of coating is deposited “at once”.
• the substrate is at a temperature of 130-132 ° C, higher than the degradation temperature of the polycarbonate; its deformation makes it incompatible with an application as a transparent product in which even minimal optical quality is required.
• the glazings resulting from the first and second tests are subjected to 500 rounds of the Taber cycle with a CS 10 F grinding wheel under a load of 500 g; the haze measured is less than 10% in both cases, which indicates satisfactory abrasion resistance.
• the distances between the cracks observed in the coatings are of the order of 100 ⁇ m to 1 mm. Their appearance often precedes delamination of the coating.
• the specific deposition process of the invention therefore makes it possible to avoid or delay the appearance of microcracks; the beneficial consequences on the adhesion of the coating to the substrate, as well as on the optical quality of the product, are obvious.

Landscapes

• Chemical & Material Sciences (AREA)
• Chemical Kinetics & Catalysis (AREA)
• Engineering & Computer Science (AREA)
• Materials Engineering (AREA)
• Mechanical Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• General Chemical & Material Sciences (AREA)
• Inorganic Chemistry (AREA)
• Laminated Bodies (AREA)
• Coating Of Shaped Articles Made Of Macromolecular Substances (AREA)
• Chemical Vapour Deposition (AREA)
• Application Of Or Painting With Fluid Materials (AREA)

Applications Claiming Priority (3)

Publications (1)

Family

ID=30470974

Family Applications (1)

Country Status (11)

Families Citing this family (2)

Family Cites Families (10)

• 2002
  • 2002-08-06 FR FR0210021A patent/FR2843408B1/fr not_active Expired - Fee Related
• 2003
  • 2003-08-04 MX MXPA05001438A patent/MXPA05001438A/es unknown
  • 2003-08-04 CN CNA038187442A patent/CN1675405A/zh active Pending
  • 2003-08-04 AU AU2003274222A patent/AU2003274222A1/en not_active Abandoned
  • 2003-08-04 US US10/523,032 patent/US20060013965A1/en not_active Abandoned
  • 2003-08-04 CA CA002494631A patent/CA2494631A1/fr not_active Abandoned
  • 2003-08-04 KR KR1020057002122A patent/KR20050042473A/ko not_active Ceased
  • 2003-08-04 BR BR0313236-6A patent/BR0313236A/pt not_active IP Right Cessation
  • 2003-08-04 JP JP2004526972A patent/JP2005534813A/ja active Pending
  • 2003-08-04 WO PCT/FR2003/002458 patent/WO2004015166A2/fr not_active Ceased
  • 2003-08-04 EP EP03758205A patent/EP1534876A2/de not_active Withdrawn

Non-Patent Citations (1)

Also Published As

Similar Documents

Legal Events