Classifications

• • C—CHEMISTRY; METALLURGY
  • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
  • C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
  • C09D179/00—Coating compositions based on macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing nitrogen, with or without oxygen, or carbon only, not provided for in groups C09D161/00 - C09D177/00
  • C09D179/04—Polycondensates having nitrogen-containing heterocyclic rings in the main chain; Polyhydrazides; Polyamide acids or similar polyimide precursors
  • C09D179/08—Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
• • 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
• • 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
  • C23C16/453—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 passing the reaction gases through burners or torches, e.g. atmospheric pressure CVD
• • 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
  • C23C16/50—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 using electric discharges
  • C23C16/513—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 using electric discharges using plasma jets
• • 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
  • Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
  • Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
  • Y10T428/264—Up to 3 mils
  • Y10T428/265—1 mil or less

Definitions

• the presently disclosed subject matter relates to high-temperature polymer composites including at least one silicon-oxy-carbide film deposited by atmospheric plasma deposition.
• high-temperature polymeric materials can be limited at elevated temperatures (e.g., greater than about 350°F) in applications that require long exposures (e.g., greater than 1000 hours) because the polymeric materials may react with oxygen under these conditions. This interaction of the polymeric materials with oxygen can result in undesirable degradation and diminishing material properties that can be difficult to predict.
• Figure 2 shows a depiction of such increased surface degredation.
• thermo-oxidative stability Intuitively it would seem that protecting a material's surface from oxygen diffusion would improve its thermo-oxidative stability and, indeed, some studies verify this supposition.
• aluminum foil was used to coat Celion 6000/PMR-15 composites and did find that a thin coating did provide significant protection from oxidation.
• the use of an expanded graphite barrier reduced the rate of oxidative degradation of PMR-15 resin such that the thermo-oxidative stability increased by up to 25%.
• high-temperature barrier coatings e.g., oxygen-barrier
• adhesion-promoting coatings e.g., interlay ers
• One or more aspects of the present disclosure may address one or more of the
• thermo-oxidative coating comprises a silicon-oxy-carbide (SOC) layer generally having a thickness from about 50 nm to about 12 microns and covering at least one surface of the polymeric substrate.
• SOC silicon-oxy-carbide
• the SOC layer is formed by atmospheric plasma deposition.
• the SOC layer can be tailored for specific polymeric matrix substrates and/or specific applications for the composite.
• Other technologies to create barrier layers e.g., oxygen- barrier layers
• Certain aspects provide composites that beneficially demonstrate an increased level of thermo-oxidative stability relative of composites of the same polymeric substrate being devoid of a thermo-oxidative barrier coating according to aspects of the present disclosure.
• a composite comprising: a polymeric substrate and a thermo-oxidative barrier coating comprising a silicon-oxy-carbide (SOC) layer having a thickness from about 100 to about 900 nm and covering at least one surface of the polymeric substrate.
• SOC silicon-oxy-carbide
• the SOC layer is formed by atmospheric plasma deposition.
• the SOC layer includes a carbon content ranging from about 3% to about 50%.
• the SOC layer includes a silicon content ranging from about 3% to about 50%.
• the SOC layer includes an oxygen content ranging from about 3% to about 50%.
• the SOC layer reduces oxygen diffusion into the polymeric substrate.
• the composite comprises a thermo-oxidative stability (TOS) of less than about 5.0% weight loss relative to a composite comprising the same polymeric substrate and being devoid of the SOC layer.
• the composite comprises a thermo-oxidative stability (TOS) of less than about 2.0% weight loss relative to a composite comprising the same polymeric substrate and being devoid of the SOC layer.
• the polymeric substrate comprises a polymeric matrix selected from a polyimide, an epoxy, bismaleimide, and a cyanate ester.
• the present disclosure provides composites including an adhesion- promoting layer comprising a silicon-oxy-carbide (SOC) layer having a thickness generally from about 50 nm to about 12 microns deposited onto at least one surface of a polymeric matrix substrate.
• SOC silicon-oxy-carbide
• the SOC layer is formed by atmospheric plasma deposition.
• the adhesion-promoting layer can be used to bind a known (or prospective) oxygen-barrier layer (OBL) onto the composite. That is, the OBL can be deposited in a manner substantially (or fully) overlying the adhesion-promoting layer such that the adhesion-promoting layer is sandwiched between the polymeric matrix substrate and the OBL.
• the adhesion-promoting layer functions at least in one respect as a tailorable tie-layer for the polymeric matrix substrate and the OBL.
• the adhesion-promoting layer increases the degree to which the OBL is attached to the composite.
• the adhesion-promoting layer according to aspects of the present disclosure can increase the bond strength of the OBL to the polymeric substrate relative to the bond strength of the same OBL directly deposited onto the same polymeric substrate.
• a composite comprising: (i) a polymeric substrate; (ii) an adhesion-promoting layer comprising a silicon- oxy-carbide (SOC) layer having a thickness from about 100 to about 900 nm and covering at least one surface of the polymeric substrate; and (iii) an oxygen-barrier layer (OBL) deposited and substantially overlying the adhesion-promoting layer.
• SOC silicon- oxy-carbide
• OBL oxygen-barrier layer
• the SOC layer is formed by atmospheric plasma deposition.
• the SOC layer includes a carbon content ranging from about 3% to about 30%; a silicon content ranging from about 10% to about 50%; and an oxygen content ranging from about 10% to about 50%.
• the OBL reduces oxygen diffusion into the polymeric substrate, said OBL comprising metallic materials, ceramic materials, or combinations thereof.
• the adhesion-promoting layer increases the bond strength of the OBL to the polymeric substrate relative to the bond strength of the same OBL directly deposited onto the same polymeric substrate.
• said composite comprises a first bond strength between the polymeric substrate and the SOC layer and a second bond strength between the SOC layer and the OBL, the first and second bond strengths each being greater than that of a comparative bond strength directly between the same OBL and the same polymeric substrate.
• Preferably composite comprises a thermo-oxidative stability (TOS) of less than about 2.0% weight loss.
• TOS thermo-oxidative stability
• the polymeric substrate comprises a polymeric matrix selected from a polyimide, an epoxy, a bismaleimide, and a cyanate ester.
• the polymeric substrate comprises a polyimide matrix.
• thermo-oxidative barrier coating comprising a SOC layer, preferably having a thickness from about 50 nm to about 12 microns, onto at least one surface of a polymeric matrix substrate via atmospheric plasma deposition.
• the thermo-oxidative barrier coating beneficially reduces the level and/or rate of oxygen diffusion into the polymeric matrix resin. Consequently, certain aspects of the present disclosure demonstrate an increased level of thermo-oxidative stability relative of composites of the same polymeric substrate being devoid of a thermo-oxidative barrier coating according to aspects of the present disclosure.
• thermo-oxidative barrier coating comprising a silicon- oxy-carbide (SOC) layer having a thickness from about 100 to about 900 nm onto at least one surface of a polymeric substrate.
• the depositing step comprises the deposition of the SOC layer via atmospheric plasma deposition (APDP).
• APDP atmospheric plasma deposition
• the APDP comprises the use of a chemical precursor of the SOC layer comprising a silane, organosilane, or combination thereof.
• the APDP comprises the use of a chemical precursor of the SOC layer comprising tetramethylcyclotetrasiloxane, octamethylcyclotetrasiloxane, or a combination thereof.
• the SOC layer inhibits the diffusion of oxygen into the polymeric substrate.
• the composite comprises a thermo-oxidative stability (TOS) of less than about 2.0% weight loss relative to a composite comprising the same polymeric substrate and being devoid of the SOC layer.
• TOS thermo-oxidative stability
• composites are produced by depositing an adhesion-promoting layer comprising a SOC, preferably having a thickness from about 50 nm to about 12 microns, onto at least one surface of a polymeric matrix substrate followed by depositing an OBL substantially overlying the adhesion- promoting layer.
• the adhesion-promoting layer in at least one respect, functions as a tie- layer to facilitate a stronger and longer-lasting bond of the OBL to the polymeric matrix substrate.
• the adhesion-promoting layer can be specifically tailored to tie dissimilar materials (e.g., the OBL layer being dissimilar to the polymeric matrix substrate as realized by a relatively weak or non-existent direct bond between the two components).
• the SOC layer is formed by atmospheric plasma deposition, which enables a high level of tailoring for specific polymeric matrix substrates, OBL, and/or specific applications for the resulting composite.
• a method of forming a composite comprising: (i) depositing an adhesion-promoting layer comprising a silicon-oxy- carbide (SOC) layer having a thickness from about 100 to about 900 nm onto at least one surface of a polymeric substrate; and (ii) depositing an oxygen-barrier layer (OBL) substantially overlying the adhesion-promoting layer.
• SOC silicon-oxy- carbide
• OBL oxygen-barrier layer
• the step of depositing the SOC layer comprises the deposition of the SOC layer via atmospheric plasma deposition (APDP).
• APDP atmospheric plasma deposition
• the APDP comprises the use of a chemical precursor of the SOC layer comprising a silane, organosilane, or combination thereof.
• the APDP comprises the use of a chemical precursor of the SOC layer comprising tetramethylcyclotetrasiloxane, octamethylcyclotetrasiloxane, or a combination thereof.
• the OBL reduces oxygen diffusion into the polymeric substrate, said OBL comprising metallic materials, ceramic materials, or combinations thereof.
• the adhesion-promoting layer increases the bond strength of the OBL to the polymeric substrate relative to the bond strength of the same OBL directly deposited onto the same polymeric substrate.
• Figure 1 shows a schematic of oxygen diffusion into a composite and resulting near- surface degradation after long-term, thermo-oxidative exposure
• Figure 2 shows a schematic of surface degradation due to thermo-oxidative aging.
• Figure 3 illustrates a composite aspect comprising a thermo-oxidative barrier coating comprising a silicon-oxy-carbide (SOC) layer deposited onto a polymeric matrix substrate;
• SOC silicon-oxy-carbide
• Figure 4 illustrates a composite aspect comprising an adhesion-promoting layer comprising a silicon-oxy-carbide (SOC) layer sandwiched between at least one surface of a polymeric matrix substrate and an oxygen-barrier layer;
• SOC silicon-oxy-carbide
• FIG 5 illustrates a general flow diagram for a method of forming a composite aspect in which an SOC layer is provided as an oxygen-barrier layer (OBL);
• OLB oxygen-barrier layer
• Figure 6 illustrates a general flow diagram for a method of forming a composite aspect in which an SOC layer is provided as an adhesion-promoting layer;
• Figure 7A provides a general schematic of atmospheric plasma deposition that can be employed in forming SOC coating aspects
• Figure 7B provides a general schematic of an atmospheric plasma deposition device including a showerhead-type discharge head aspect
• Figures 8A-8I are Fourier transform infrared spectroscopy (FTIR) spectra for SOC layers (i) prior to aging, (ii) after about 3432 hours of aging, and (iii) after about 7752 hours of aging.
• FTIR Fourier transform infrared spectroscopy
• aspects of the present disclosure comprise high-temperature polymer composites including at least one SOC coating or layer deposited onto a polymeric matrix substrate by atmospheric plasma deposition as well as systems and methods of applying SOC layers on polymeric matrix substrates to form composites demonstrating an improved level of thermo-oxidative stability.
• the use of atmospheric plasma deposition beneficially enables the tailoring of the resulting SOC layers so that they can function either (or both) (i) as a thermo-oxidative barrier coating preventing or significantly mitigating the level of oxygen that diffuses into the polymeric matrix substrate or (ii) an adhesion-promoting layer increasing the degree of adherence or bonding of an oxygen-barrier layer (OBL) to the polymeric matrix substrate.
• OBL oxygen-barrier layer
• a composite can include a SOC layer sandwiched between the polymeric matrix substrate and a commercially known or viable OBL in which the SOC layer functions both as a "tie-layer" to attach two dissimilar components (e.g., substrate and OBL) and also as a secondary oxygen- barrier to prevent oxygen diffusion into the polymeric matrix substrate.
• the SOC layers are preferably capable of withstanding high-temperature (e.g., 350- 700°F) exposures that are either non-porous, strain-resistant, or a combination thereof.
• the SOC layers can beneficially enhance a composite's thermo-oxidative stability.
• Composites including one or more SOC layers according to certain aspects of the present disclosure exhibit a substantially reduced level of oxygen diffusion into the polymeric matrix substrate. That is, the one or more SOC layers significantly retard thermo-oxidative degradation. In this regard, the one or more SOC layers prevents or substantially reduces the level of oxygen diffusing into the polymeric matrix substrate.
• the SOC layers can be deposited onto the polymeric matrix substrate utilizing atmospheric plasma deposition.
• Utilization of atmospheric plasma deposition enables the creation of tailorable, thermo-oxidative stable, strain-resistant coatings to improve the in-service durability and useful service temperature of high-temperature polymeric composites.
• the use of atmospheric plasma deposition enables the formation of a dense and durable thin film or coating directly onto substrates and to complex (e.g., contoured) shapes as compared to other approaches.
• certain aspects of the present disclosure enable the use of high-performance materials to produce durable, non- permeable, strain-resistant oxygen-barriers or adhesion-promoting layers.
• aspects of the present disclosure provide for the formation of tailored coatings below the micron scale to obtain desired features.
• a further advantage of aspects of the present disclosure lies in the ability to directly apply an SOC coating to complex shapes to form composite of such complex shapes.
• atmospheric plasma deposition can be provided as a mobile system so that coatings can be applied on site rather than in a lab or factory, if so desired.
• SOC coatings according to aspects of the present disclosure can comprise a thickness of at least any of the following: 10, 50, 100, 200, 300, 400, and 500nm; and at most about any of the following: 12000, 10000, 50000, 1000, 900, 800, 700, 600, 500, and 400nm (e.g., 10- 12000nm, 10-lOOOOnm, 50-800nm, 50-500nm, 10-200nm, etc.).
• SOC coatings according to certain aspects of the present disclosure can comprise a thickness from about 50 nm to about 12 microns.
• the respective carbon, silicon, and oxygen content of SOC coatings can be varied in view of a particularly intended application.
• the SOC layers can include a carbon content comprising at least any of the following: 3, 5, 10, 20, 30, 40, 50, and 60%; and at most about any of the following: 70, 60, 50, 40, 30, 25%, 20%, ands 10% (e.g., 5-70%, 20-70%, 10-40%, 50-70%, 3-50%, 3-25%, 3- 10%, etc.).
• the SOC coatings can include a silicon content comprising at least any of the following: 3, 5, 10, 20, 30, 40, 50, and 60%; and at most about any of the following: 70, 60, 50, 40, 30, 25%, 20%, ands 10% (e.g., 5-70%, 20-70%, 10-40%, 50-70%, 3-50%, 3-25%, 3- 10%, etc.).
• the SOC coatings can include an oxygen content comprising at least any of the following: 3, 5, 10, 20, 30, 40, 50, and 60%; and at most about any of the following: 70, 60, 50, 40, 30, 25%, 20%, ands 10% (e.g., 5-70%, 20-70%, 10-40%, 50-70%, 3-50%, 3-25%, 3- 10%,etc).
• the SOC coating or layers according to aspects of the present disclosure are created via atmospheric plasma deposition.
• a variety of chemical precursors can be used in atmospheric plasma deposition for creating SOC layers according to aspects of the present disclosure.
• siloxanes and organosilanes can be employed in certain aspects.
• a few exemplary chemical precursors can include
• octamethylcyclotetrasiloxane OCTS
• TCTS tetramethylcyclotetrasiloxane
• HMDSO hexamethyldisiloxane
• BTESE l,2-bis(triethoxysilyl)ethane
• TEOS tetraethyl orthosilicate
• HDSN hexametbyldisilizane
• TMDSO tetramethyldisiloxane
• the polymeric matrix substrate can comprise a polyimide, a bismaleimide, a benzoxazine, a thermoplastic (e.g., a polyetheretherketone, polyetherketoneketone, etc.), an epoxy, a cyanate ester, or combinations thereof.
• the polymeric matrix substrate comprises a polyimide, preferably a polyimide recognized as being suitable for high-performance and/or high-temperature applications.
• polyimides suitable for composite fabrication according to certain aspects of the present disclosure include those disclosed in U.S. Patent Numbers 3,745,149 (Serafini et al), 5,338,827 (Serafini et al), 5, 171,822 (Pater), 5,081, 198 (Pater et al), 7,041,778 (Curliss et al), 6,958, 192 (Hergenrother et al), 5,412,066
• polyimide matrix resins include PMR-15 (described in U.S. Patent No. 3,745,149), PMR-II-50, RP-46, phenylethynyl end-capped polyimides such as PETI-5 and PETI-330, HFPE-52- ⁇ , and AFR-PE-4, the contents of each are hereby incorporated in their entireties by reference.
• the present disclosure provides composites comprising a polymeric matrix substrate and a thermo-oxidative barrier coating.
• the thermo-oxidative coating comprises a SOC layer created by atmospheric plasma deposition.
• the SOC layer has a thickness from about 100 to about 900 nm and covers at least one surface of the polymeric substrate.
• the SOC layer beneficially can reduce (or virtually eliminate) the amount of oxygen that diffuses into the polymeric matrix substrate.
• thermo-oxidative stability test can include placing samples (e.g., SOC-coated polymeric matrix substrates) in a chamber through which a constant flow of air travels at a rate sufficient to refresh the chamber volume at a rate of 5 times/hour.
• the test temperature, pressure, and time can be selected to result in a measurable degradation of an unprotected (uncoated) polymeric matrix substrate for direct comparison.
• the oxygen-barrier capability of the SOC coating can be determined by the weight loss of protected composite samples relative to unprotected composite samples.
• Thermo-oxidative Stability is the ability of the composite to withstand elevated temperatures in an oxygen-containing environment, such as air, with minimal loss of weight and/or properties. Since, in a composite, compression strength is a resin-dominated property, the retention of compression strength after long-time exposures to high temperatures is monitored as a measure of TOS. Weight loss over time can also be used as a measure.
• Polymers can degrade through mechanisms, such as volatilization, resulting in a composite having reduced mass due to this loss of polymer.
• One test used herein to measure TOS includes placing a plaque of polymeric or composite material in a chamber, increasing the temperature and pressure within the chamber to a predetermined temperature and pressure, and holding these conditions for up to several thousand hours with multiple atmospheric changes over the course of the test. The plaques are then removed and tested for weight loss and retention of compression and/or shear strength. The weight loss and retention of compression strength reflect service conditions in high-performance environments and provide a measure of the longer-term stability of the polymeric material. A higher TOS is important for material that will be used at a high temperature in air for long periods of time.
• Composites in accordance with certain aspects of the present disclosure, can comprise a TOS comprising less than at least any of the following: 10%, 7%, 5%, 4%, 3%, 2%, 1%, 0.5%, 0.1%, and 0% weight loss (e.g., 0.1-10%, 0.1-7%, etc.) relative to a composite comprising the same polymeric substrate and being devoid of a thermo-oxidative barrier layer comprising an SOC layer in accordance with aspects of the present disclosure.
• a TOS comprising less than at least any of the following: 10%, 7%, 5%, 4%, 3%, 2%, 1%, 0.5%, 0.1%, and 0% weight loss (e.g., 0.1-10%, 0.1-7%, etc.) relative to a composite comprising the same polymeric substrate and being devoid of a thermo-oxidative barrier layer comprising an SOC layer in accordance with aspects of the present disclosure.
• FIG. 3 illustrates a composite according to one aspect of the present disclosure comprising a thermo-oxidative barrier coating 15 comprising a SOC layer deposited onto a polymeric matrix substrate 10.
• the present disclosure provides composites including an adhesion- promoting layer comprising a SOC layer deposited via atmospheric plasma deposition onto at least one surface of a polymeric matrix substrate.
• the adhesion-promoting layer can be used to bind a known (or prospective) oxygen-barrier layer (OBL) onto the composite. That is, the OBL can be deposited in a manner substantially (or fully) overlying the adhesion-promoting layer such that the adhesion-promoting layer is sandwiched between the polymeric matrix substrate and the OBL.
• OBL oxygen-barrier layer
• the adhesion-promoting layer functions at least in one respect as a tailorable tie-layer for the polymeric matrix substrate and the OBL.
• the adhesion-promoting layer increases the degree to which the OBL is attached to the composite.
• the adhesion-promoting layer according to aspects of the present disclosure can increase the bond strength of the OBL to the polymeric substrate relative to the bond strength of the same OBL directly deposited onto the same polymeric substrate.
• the OBL can include currently known (or OBL materials developed in the future) OBL materials that reduce (or virtually eliminates) oxygen diffusion into the polymeric matrix substrate.
• OBL materials can comprise metallic materials, ceramic materials, or combinations thereof.
• Exemplary materials that may be used to form the OBL layer can include known oxygen-barriers such as silicon oxides, aluminum, and aluminum oxides.
• the adhesion-promoting layer increases the bond strength of the OBL to the polymeric substrate relative to the bond strength of the same OBL directly deposited onto the same polymeric substrate.
• composites can comprise a first bond strength between the polymeric substrate and the SOC layer and a second bond strength between the SOC layer and the OBL.
• the first and second bond strengths each being greater than that of a comparative bond strength directly between the same OBL and the same polymeric substrate.
• the incorporation of the adhesion- promoting layer helps ensure that an OBL material stays attached to the polymeric matrix substrate to improve the thermo-oxidative stability of the composite.
• a composite can include a SOC layer sandwiched between the polymeric matrix substrate and a commercially known or viable OBL in which the SOC layer functions both as a "tie-layer" to attach two dissimilar components (e.g., substrate and OBL) and also as a secondary oxygen-barrier to prevent oxygen diffusion into the polymeric matrix substrate.
• Figure 4 illustrates a composite according to one aspect of the present disclosure comprising an adhesion-promoting layer 20 comprising a SOC layer deposited onto at least one surface of a polymeric matrix substrate 10.
• the adhesion-promoting layer 20 is sandwiched between at least one surface of a polymeric matrix substrate 10 and an OBL 30.
• the present disclosure provides methods of fabricating composites according to aspects of the present disclosure.
• methods of forming composites include a step of depositing a thermo-oxidative barrier coating comprising a SOC layer directly onto at least one surface of a polymeric matrix substrate via atmospheric plasma deposition.
• the thermo-oxidative barrier coating beneficially reduces the level and/or rate of oxygen diffusion into the polymeric matrix resin. Consequently, certain aspects of the present disclosure demonstrate an increased level of thermo-oxidative stability relative of composites of the same polymeric substrate being devoid of a thermo-oxidative barrier coating according to aspects of the present disclosure.
• certain aspects of the present disclosure can include a step of providing one or more polymeric substrates 100 followed by depositing a thermo- oxidative barrier coating comprising a SOC layer 150 directly onto at least one surface of the polymeric substrate to provide a composite.
• the polymeric substrates can be pre-cleaned by traditional physical or chemical methods and/or plasma pretreated prior to depositing an SOC layer onto the polymeric substrate.
• the SOC layer can provide adequate thermo-oxidative stability to the resulting composite that a traditionally employed thermo-oxidative barrier layer can be avoided if desired.
• composites are produced by depositing an adhesion-promoting layer comprising a SOC onto at least one surface of a polymeric matrix substrate followed by depositing an OBL substantially overlying the adhesion-promoting layer.
• the adhesion-promoting layer in at least one respect, functions as a tie-layer to facilitate a stronger and longer- lasting bond of the OBL to the polymeric matrix substrate.
• the adhesion-promoting layer can be specifically tailored to tie dissimilar materials (e.g., the OBL layer being dissimilar to the polymeric matrix substrate as realized by a relatively weak or non-existent direct bond between the two components).
• the SOC layer is formed by atmospheric plasma deposition, which enables a high level of tailoring for specific polymeric matrix substrates, OBL, and/or specific applications for the resulting composite.
• the OBL reduces oxygen diffusion into the polymeric substrate and can comprise known OBL materials such as various metallic materials, ceramic materials, or combinations thereof.
• the OBL can be deposited on top (e.g., overlying) the adhesion-promoting layer by any technique known for depositing such materials.
• the adhesion-promoting layer beneficially increases the bond strength of the OBL to the polymeric matrix substrate relative to the bond strength of the same OBL when directly deposited onto the same polymeric substrate.
• the SOC layer functions as an interlayer over which a different layer (e.g., a traditional OBL) can be deposited.
• certain aspects of the present disclosure in which the SOC layer is sandwiched between the polymeric substrate and a traditional OBL can include a step of providing one or more polymeric substrates 200 followed by depositing an adhesion- promoting layer comprising a SOC 250 onto at least one surface of the polymeric substrate.
• the SOC coated polymeric substrate can then be subjected to an OBL deposition step 275 in which a traditional OBL is deposited over the top of the SOC layer such that the SOC layer is sandwiched between the OBL and the polymeric substrate to provide a composite according to certain aspects of the present disclosure.
• OBL deposition step 275 in which a traditional OBL is deposited over the top of the SOC layer such that the SOC layer is sandwiched between the OBL and the polymeric substrate to provide a composite according to certain aspects of the present disclosure.
• the polymeric substrates can be pre-cleaned by traditional physical or chemical methods and/or plasma pretreated prior to depositing an SOC layer onto the polymeric substrate.
• the SOC coatings / layers are created by atmospheric plasma deposition.
• One of the benefits of using atmospheric plasma deposition is that the relatively large production of chemically reactive species, such as atomic oxygen, enables the precursor to be mixed downstream in the plasma afterglow where it can react with the reactive neutrals from the plasma to produce a coating on the substrate.
• Atmospheric plasma deposition beneficially generates much greater reactive species concentrations than more traditional deposition techniques and can be used in a remote or downstream mode.
• One suitable atmospheric plasma deposition system suitable for deposited an SOC coating onto a polymeric matrix substrate is ATOMFLOTM Model 400 with Precursor Delivery System from Surfx® Technologies LLC (USA).
• Chemical precursor materials for creation of SOC layers in accordance with aspects of the present disclosure can generally comprise silanes, organosilanes, or combination thereof.
• a few exemplary chemical precursors suitable for certain aspects include
• octamethylcyclotetrasiloxane OCTS
• TCTS tetramethylcyclotetrasiloxane
• HMDSO hexamethyldisiloxane
• BTESE l,2-bis(triethoxysilyl)ethane
• TEOS tetraethyl orthosilicate
• HMDN hexametbyldisilazane
• TMDSO tetramethyldisiloxane
• atmospheric plasma deposition has several parameters that can be adjusted in unison or independently of each other to tailor the resulting SOC coating for a desired application.
• the height of the plasma applicator head from the substrate being coated can be adjusted as desired, for example, from about 1 mm to 1 cm (e.g., 2-7mm, 3-6mm).
• the helium or argon (as the primary gas) flow rate can be varied from about 20 to 50 liters per minute (LPM) (e.g., 20-40, 25-35LPM).
• the plasma power can be varied from about 80W to 180W (e.g, 100-150W, 120-150W).
• Oxygen gas flow can range, for example, from 0.1 to 1 LPM.
• the bubbler flow rate of the inert gas can range from about 0.1 to 2 LPM.
• the dilution flow rate of inert gas can range from about 0.5 to 5.0 LPM.
• the temperature of the chemical precursor can vary from room temperature up to the boiling point of the particular chemical being utilized as the chemical precursor.
• the plasma applicator head is typically attached to a robotic arm that has been programmed to apply the SOC coating onto a given space of the substrate.
• the speed at which the robotic arm moves can be varied as well. For instance, the speed at which the robotic arm moves can range from 10-100 mm/s.
• FIG. 7A provides a general schematic of an atmospheric deposition device in accordance with certain aspects of the present disclosure.
• the atmospheric-plasma deposition device 50 includes an outer electrode 52 which is electrically grounded and an inner electrode 54 to which an external voltage is applied.
• the external voltage can be supplied by a high- frequency, high-voltage generator 57.
• the generator 57 can supply the inner electrode 54 with a voltage in the order of, for example, 5 to 30 kV and the frequency of the voltage can range, for example, from 10 to 20 kHz.
• the atmospheric plasma deposition device 50 includes a plasma gas / working gas inlet stream 56 entering a first end of the device 50.
• the plasma gas / working gas inlet stream 56 comprises helium gas, oxygen gas, or a mixture thereof.
• a plasma discharge 58 is generally located at an end of the device 50 opposite to the plasma gas / working gas inlet stream 56.
• a plasma stream 60 exits the plasma discharge 58 of the device 50.
• One or more chemical precursors 62 such as those discussed in the present specification, can be introduced into the plasma steam 60 via precursor inlets 64.
• an SOC layer 15 can be deposited onto the surface of a polymeric substrate 10.
• Figure 7A illustrates a device 50 providing a single discharge steam (e.g., plasma discharge 58 in Figure 7A)
• certain preferred aspects utilize a device comprising a showerhead-type configuration in which multiple plasma discharges are provided.
• Figure 7B illustrates a device comprising a showerhead-type configuration in which multiple plasma discharges are provided.
• an atmospheric -plasma deposition device 50 can comprise a showerhead-type discharge head 152 including multiple discharge orifices 158.
• the power supply 157 and the chemical precursors 162 can be connected to the top of the device 50.
• the chemical precursors can be delivered inside the head to the plasma and the afterglow region 160 is where the chemical reactions and film deposition occur.
• One commercially available device including a showerhead-type configuration in which multiple plasma discharges are provided includes ATOMFLOTM Model 400 from Surfx® Technologies LLC (USA).
• a total of eight panels had a SOC layer, ranging from about 200 - 500nm thick, deposited thereon by atmospheric plasma deposition utilizing ATOMFLOTM Model 400 with Precursor Delivery System from Surfx® Technologies LLC (USA) to form the SOC layers in each of these examples.
• the chemical precursors utilized were TMCTS and OMCTS.
• a pretreatment step was conducted prior to deposition of the SOC layer onto the polyimide substrate.
• the polyimide substrate was pretreated at a 50% power rating for 4 minutes March Plasmod GCM-200 with air as the plasma gas.
• a ninth panel ( Figure 81) was prepared and tested to provide a comparison to the eight panels having a SOC deposited thereon by atmospheric plasma deposition.
• the ninth panel was provided coated with a vacuum CVD film.
• Table 1 The operating variables that were modified from run to run, as well as respective values, are summarized in Table 1 below.
• Table 2 provides a summary of the operating parameters of atmospheric plasma deposition that were held as fixed conditions during all runs. It should be noted, however, that the operating parameters that were selected to be fixed conditions among the eight run need not necessarily be fixed or set at these particular values.
• the height between the plasma-deposition source and the closest surface of the polyimide substrate can readily be varied from the 5-mm height employed in the exemplary runs discussed herein.
• the height of the deposition source above the substrate can be varied from 1 mm to 1 cm.
• Table 3 provides a quick summary of the times used to coat a SOC layer onto a 100mm X 138.5mm polyimide substrate. It should be noted, however, that the deposition rates and /or density of the resulting SOC layer can be tailored by adjusting one or more of the operating parameters of the atmospheric plasma deposition.
• each of the samples was subjected to testing for oxygen-barrier functionality at 450°F for about 7,752 hours with weight loss data obtained after about 3,432 hours of exposure. These tests were conducted to illustrate the ability of the respective SOC coatings to stay attached to the polyimide substrate and the ability to prevent weight loss due to oxidation. As discussed above, the SOC layers were deposited using OMCTS and TMCTS precursors with atmospheric plasma and the "CVD" sample was deposited with OMCTS in a vacuum chamber. The results of this additional testing are summarized in Table 4.
• FTIR Fourier transform infrared spectroscopy
• FTIR spectrum representative of the unaged (e.g., no aging) panel and subsequent FTIR spectra representative of aged panel should not change significantly.
• the SOC coatings can be considered stable when only minor (or preferably no) changes in the FTIR spectra from unaged to aged are compared. In such instances, the SOC layers can be considered stable and not oxidizing or thermally degrading during the test period. To the contrary, FTIR spectra that show large differences from the unaged to the aged are not particularly desirable as they are chemically changing as they age.

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