APPARATUS AND METHODS FOR DEFINING A PLASMA

Abstract

Apparatus comprising: a support arranged to transport a moving substrate; a plasma generator arranged to generate plasma; and an electrode arranged to bias ions within the plasma towards the moving substrate to form an ion flux. The ion flux has an energy level between 3.6 eV and 250 eV. Alternatively, apparatus for defining plasma having a plurality of spaced race track portions.

Claims

1-28. (canceled)

29. An apparatus for curing a radiation curable material on a substrate, the apparatus comprising: a cylindrical drum arranged to rotate to transport a moving substrate; a plasma generator arranged to generate plasma; a radiation curable material delivery device arranged to deliver radiation curable material towards the cylindrical drum such that the radiation curable material will, in use, condense on the substrate; and one or more electrodes arranged to bias positive ions within the plasma towards the cylindrical drum to form a positive ion flux for curing radiation curable material condensed on the substrate, the ion flux having an energy level between 3.6 eV and 250 eV, the cylindrical drum defining one of the one or more electrodes.

30. An apparatus according to claim 29, further comprising a magnet array arranged to spatially define the plasma.

31. An apparatus according to claim 29 arranged to provide a unit energy dose which is no greater than 15 J/cm.sup.2.

32. An apparatus according to claim 29, wherein the cylindrical drum is arranged to move the substrate at a speed through the ion flux such that the dwell time is no greater than 5 minutes.

33. An apparatus according to claim 29, further comprising a gas delivery system arranged to deliver a primary gas from which the plasma is generated and one or more further gases that are distinct from the primary gas.

34. An apparatus for defining a plasma comprising: a drum arranged to transport a moving substrate; a plasma generator arranged to generate a plasma; and a magnet array comprising: single magnet arranged to define a magnetic field configured to influence the generated plasma to form a closed loop race track having: a first race track portion that is adjacent to a first surface region of the drum; and a second race track portion that is adjacent to a second surface region of the drum, wherein the first and second surface regions are circumferentially spaced from one another.

35. An apparatus according to claim 34, wherein the first and second surface regions are circumferentially spaced from one another by at least 20 mm.

36. An apparatus according to claim 34, wherein the magnet array comprising further magnets arranged to define one or more further race track portions, each race track portion being adjacent to the surface of the drum and circumferentially spaced from each other race track portion by at least 20 mm.

37. An apparatus according to claim 34, wherein the magnet array is disposed within the drum.

38. An apparatus according to claim 34, wherein the drum defines an electrode arranged to generate the plasma.

39. An apparatus according to claim 34, further comprising an electrode arranged to bias ions within the plasma towards the drum to form an ion flux, wherein the ion flux has an energy level between 3.6 eV and 250 eV and/or arranged to define the first race track portion on a first side of the substrate and the second race track portion on the opposite side of the substrate and/or further comprising a gas delivery system arranged to deliver a primary gas from which the plasma is generated and one or more further gases that are distinct from the primary gas and/or further comprising a delivery device arranged to deliver radiation curable material to the substrate, the apparatus being arranged such that the radiation curable material condenses on the substrate.

40. An apparatus comprising: a substrate; a support arranged to support and move the substrate; a plasma generator arranged to generate plasma; an anode; and a cathode, at least one of the anode and cathode arranged to bias ions within the plasma towards the moving substrate to form a positive ion flux, the ion flux having an energy level between 3.6 eV and 250 eV, the substrate being located between the anode and cathode.

Description

DESCRIPTION OF THE DRAWINGS

[0098] By way of example only, certain embodiments of the invention will now be described by reference to the accompanying drawings, in which:

[0099] FIG. 1 is a schematic drawing of apparatus for carrying out a process according to a first embodiment of the invention;

[0100] FIG. 2 is a schematic drawing of apparatus for carrying out a process according to a second embodiment of the invention;

[0101] FIG. 3 is a schematic drawing that illustrates radiation and vapour flows;

[0102] FIG. 4 is a schematic drawing showing configuration for sequential delivery and cure;

[0103] FIG. 5 is a schematic drawing showing a further configuration for sequential delivery and cure;

[0104] FIG. 6 is a schematic drawing that illustrates a plasma source for use in FIGS. 1 to 5;

[0105] FIG. 7 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0106] FIG. 8 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0107] FIG. 9 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0108] FIG. 10 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0109] FIG. 11 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0110] FIG. 12 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0111] FIG. 13 is a schematic drawing of apparatus according to a further embodiment of the invention;

[0112] FIG. 14 is a diagram illustrating a narrow racetrack; and

[0113] FIG. 15 is a diagram illustrating a wide racetrack.

EMBODIMENTS OF THE INVENTION

[0114] The apparatus in FIG. 1 is housed in a vacuum chamber 1. A web 2 to be treated is fed over idle rollers 3, 7 between web unwind and rewind stations (not shown). The web is fed past a deposition station 4 defined by an enclosure 4 in which is housed a device 5 that generates a directional beam 5 of a radiation curable material, and a low pressure gas plasma source 6 that generates a directed ion flux 6. The flux 6 may comprise cations and other positively charged or non-charged particles and species, but the positively charged ions are the primary curing or processing initiator. The ionisation fraction of the plasma might typically be 10.sup.5 to 10.sup.1. The beam of radiation curable material, such as a polymer precursor vapour or atomised liquid, is directed at the web 2 as it passes below device 5, and the plasma source 6 simultaneously directs the ion flux 6 at the web 2 to be incident on the web generally concurrently with the beam 5. The beam 5 and flux 6 overlap so that the overlap region is exposed to the ion radiation during delivery, thereby to initiate curing as the vapour is delivered to the web 2. The enclosure 4 serves to support a differential pressure between the inside of the enclosure and the vacuum chamber 1 so as to control escape of the precursor vapour and process gases outside of the enclosure. The apparatus can optionally have surface treatment stations 8 and 9 to enhance the properties of the web prior to and after the deposition station 4.

[0115] An alternative embodiment of the invention is illustrated in FIG. 2 in which the linear feed of the web 2 between rollers 3, 7 is supplemented by a rotating drum feed 10. The rotating drum 10 allows additional treatment processes to take place, e.g., further depositing stations 11, 12 for coating metallic or non-metallic compounds before and after the deposition station 4, and treatment stations 13, 14 to enhance the properties of the film before and after the optional depositing stations 11 and 12.

[0116] As shown in FIGS. 1 and 2, the radiation curable material deposition device 5 may be relocated to 5a, which indicates an alternative spatial configuration for delivery relative to the radiation source 6 so that it is downstream rather than upstream of the radiation 6 in the movement of the web 2. However, the precursor beam 5 would still be angled to overlap the ion flux 6 in a similar manner shown in FIG. 3. This shows the pattern of the precursor beam 5 and ion flux 6, and how these beams overlap in space and are incident concurrently on the web 2 so that a coating is progressively deposited and cured as the web passes the deposition station 4. Such an overlapping configuration may be used in embodiments of the invention.

[0117] FIG. 4 shows an embodiment of the invention in which the deposition device 5 has been repositioned away from the ion flux source 6. In FIGS. 1 to 3, the deposition and curing occurs concurrently in space and time onto the web 2, whereas in the illustrated embodiment, the web 2 first passes the deposition beam 5 and transports the uncured deposited material to the ion flux 6 to be cured. Although the deposition device 5 and ion flux source 6 are active concurrently in time, they are acting sequentially upon the web 2, and so the respective beams 5 and 6 are not spatially concurrent.

[0118] FIG. 5 shows a further embodiment of the invention in which the deposition device 5 is repositioned to deliver the vapour stream 5 onto a free span portion of the moving web 2. The ion flux source 6 is arranged to cure in a free span position after a roller 10. This configuration is similar to that referred to in Example 1 below.

[0119] FIG. 6 shows a plasma generator 6 suitable for use in embodiments of the invention described herein. In the illustrated example, the plasma generator 6 is a low pressure gas plasma. The pressure of this process will determine not only the mean free path of any molecule within the plasma zone, but also the ion energy distribution dependent upon the electric field used. Reference Handbook of Plasma Processing Technology pages 38-43 (ISBN0-8155-1220-1). The plasma is generated between a cathode 15, which is water cooled, and a reaction plate 16. An outer core 17 is insulated from an anodic inner core 18, which is also water cooled, by an insulating layer 19. Spatial separation between the anode and cathode is supplied by insulators 20. A magnet array 21 of a magnetron is arranged with an outer set of magnets in opposite polarity to a centre set of magnets on a yoke plate 22 to which they are magnetically attached to create a magnetic field to trap the ionised gas. A plasma gas is supplied to the plasma area from a gas inlet pipe 23. The magnet array 21 operates as a magnetron to enhance ionisation of the plasma in the glow discharge in the region of the reaction plate 16. A driving voltage is applied to the anode 18 and is electrically connected to the reaction plate 16, which is positive relative to the web 2 so as to direct the ion flux 6 towards the web 2.

[0120] In other embodiments, any suitable ion flux source may be provided, and different means may be employed to direct the ion flux towards the substrate. For example, as will be described in more detail below with reference to FIGS. 7 to 13, the support for transporting the substrate may define a cathode to attract the ion flux towards the web. Moreover, although the ion flux has been illustrated as being extracted from a plasma and directed towards the web, in other embodiments the plasma may be defined adjacent to the substrate and the electrons and other negatively charged particles and species may be extracted from the plasma away from the substrate and web.

[0121] FIG. 7 shows an embodiment of the invention in which the rotating drum 10 defines a cathode arranged to attract the ion flux 6 towards the web 2. The system is housed in a vacuum chamber (not shown). The housing enables the operating pressure to be set to an appropriate level observed to be ranging between 10-4 and 10-0 millibar (mbar), but preferentially ranging between 10.sup.3 and 10.sup.1 milibar (mbar). The housing may also define an anode for the generation of plasma between the anode and the cathodic drum 10. The plasma is formed from a gas, such as Argon, supplied via a gas inlet 23. As with the embodiments illustrated in FIGS. 4 and 5, the precursor is applied to the web 2 upstream with respect to the curing zone by a device 5 that generates a directional beam 5 of a radiation curable material.

[0122] The drum 10 has an interior space 26, which may be water cooled. The drum 10 is rotatably mounted on a stationary yoke 22 disposed within the interior space 26. The stationary yoke 22 supports a magnet array 21. The magnet array 21 is arranged to produce closed loop magnetic flux lines that interact with the ion flux 6 to define relatively narrow race track of high density ion flux having portions 6a, 6b that are located in close proximity to the web 2. The inventors have discovered that the position of the magnet relative to the outer surface of the drum 10 affects the configuration, in including the separation, of the discrete race track portions. Generally speaking, the discrete race track portions are relative close together when the magnet is relatively close to the drum surface, and relative widely spaced when the magnet is located away from the drum surface, closer to the central axis of the drum.

[0123] In the illustrated embodiment, the web 2 shields the cathode roller 10 from the ion flux 6; this is advantageous because it inhibits oxidisation and fouling of the cathode 10. In such embodiments, the radiation source 6 should be powered by an AC supply, preferably operating within the radio frequency (RF) range; for example, 40-320 kHz. In some embodiments the voltage source may be an AC source having any suitable frequency, such as 50 Hz.

[0124] FIG. 8 shows an alternative embodiment of the invention that is similar to the embodiment of FIG. 7, but in which the precursor is applied to the web 2 through the curing zone by a device 5 that generates a directional beam 5 of a radiation curable material. As such, the curing in this embodiment occurs concurrently with the delivery of precursor material.

[0125] FIGS. 9 to 12 show alternative embodiments of the invention in which the magnet array 21 is arranged and configured to produce a plurality of discrete race track regions or portions around the surface of the roller 10. Put another way, the magnet array 21 is arranged to define a closed loop race track that has a number of distinct portions that each pass close to, or contact, the surface of the drum 10, and each of the distinct race track portions are spatially separated from one another by a distance defined by the magnetic array 21 which in some embodiments can be 20-40 mm. This advantageously enables the discrete race track portions to be used for different purposes, such as the treatment or curing of opposite faces of the web 2, or pre-treating the web 2 prior to the delivery of precursor followed by curing thereof.

[0126] In the embodiment of FIG. 9, the magnet array 21 consists of a single magnet assembly arranged to define a relatively wide race track that is in close proximity to the drum 10 at two circumferentially spaced portions 6a, 6b. A magnet assembly of embodiments of the present invention may comprise one or more magnets. The centre points of the race track portions 6a, 6b are rotationally spaced about the drum axis by approximately 135. The pathway of the web 2 is arranged such that the first race track portion 6a acts upon a first face of the web 2, and the second race track portion 6b acts upon the opposite face of the web 2. In the first example, in which the web 2 is shown in solid line, the top surface of the web 2 is exposed to the first race track portion 6a, due to the first race track portion 6a being positioned at a location where the web 2 is supported by the drum 10, and the bottom surface of the web 2 is exposed to the second race track portion 6b, due to the second race track portion 6b being located in close proximity to the drum 10 at a location where the web 2 is no longer supported by the drum 10, but is still close to the second race track portion 6b. The second example, shown with the web 2a in dashed line, shows the opposite configuration in which the web 2 has the underside surface exposed before the top surface to the respective regions of high density ion flux.

[0127] The embodiment of FIG. 10 is similar to that shown in FIG. 9. However, in the embodiment of FIG. 10, the race track portions 6a, 6b are each positioned at a location where the web 2 is supported by the drum 10 so as to be exposed to the top surface of the web 2. A pair of tensioning rollers 3,7 may be provided to wrap the web 2 around approximately 270 of the drum. The first race track portion 6a is arranged to pre-treat the top surface of the web 2 to improve surface adhesion. The second race track portion 6b is arranged to define a curing zone adjacent the top surface of the web 2. Precursor is applied to the top surface of the web 2, between the race track portions 6a, 6b, upstream of the curing zone, by a device 5 that generates a directional beam 5 of a radiation curable material.

[0128] The embodiment of FIG. 11 is similar to that shown in FIG. 10. However, the magnet array 21a, 21b of the embodiment shown in FIG. 11 consists of two magnet assemblies, each arranged to define relatively narrow race track portions 6a, 6b and 6c, 6d. The first magnet assembly 21a is located on a first side of the yoke 22 and arranged to define a first racetrack 6a, 6b adjacent to the drum surface 10 on a first side thereof. The second magnet assembly 21b is located on a second side of the yoke 22 and arranged to define a second racetrack 6c, 6d adjacent to the drum surface 10 and centred at a location that is rotationally spaced around the drum surface 10 with respect to the centre of the first race track portion as defined by 6a, 6b by approximately 180. Precursor is applied to the top surface of the web 2, between the race track portions 6a, 6b and 6c, 6d, upstream of the curing zone define by the second race track portion 6c, 6d, by a device 5 that generates a directional beam 5 of a radiation curable material.

[0129] The embodiment of FIG. 12 is similar to that shown in FIG. 11. However, the magnet arrays 21a, 21b and 21c of the embodiments shown in FIG. 12 are each arranged to define a race track portion at 6a, 6b, at 6c, 6d and at 6e, 6f. The first and second magnet assemblies 21a, 21b are identical to those described with reference to FIG. 11. The third magnet assembly 21c is disposed between the first and second magnets 21a, 21b, in place of the device 5, and arranged to define a third race track portion at 6e, 6f adjacent to the drum surface 10 and centred at a location that is rotationally spaced around the drum surface 10 with respect to the centre first race track portion 6a, 6b by approximately 90. In addition to the gas inlet 23, the illustrated embodiment includes second gas inlet 23a that is spaced from the first gas inlet 23. This may be advantageous if the drum 10 is particularly large and it is derisible to perform plasma processing around the drum 10, or if different gases are to be used to generate distinct, different plasmas.

[0130] The embodiment of FIG. 13 is similar to that shown in FIGS. 7 & 8. However the device 5 that generates a directional beam 5 of a radiation curable material has been omitted. Such an embodiment may be used to pre-treat the web 2 prior to subsequent processing steps.

[0131] The race track portions of embodiments of the invention such as those described with reference to FIGS. 7 to 13 preferably extend so as to act upon a significant portion of the height of the circumferential face of the drum 10, as illustrated in FIGS. 14 and 15.

[0132] FIG. 14 shows a narrow race track comprising race track portions 6a and 6b. Thus, race track portions both 6a and 6b are two parts of the same high density ion flux. The circumferential separation 24 and the rotational separation 25 are small. The circumferential separation 24 can be a low as 20 mm on the drum surface and the rotational separation 25 is dependent on the roller 10 diameter.

[0133] FIG. 15 describes a wide race track comprising race track portions 6a and 6b. However, the magnet array (not shown) inside the drum 10 has been arranged and configured such that the circumferential separation 24 and the rotational separation 25 are relatively large. The rotational separation can be as much as 180 (greater than 180 being simply a mirror image of the reflectionally symmetrical smaller angle) and the circumferential separation is dependent on the roller 10 diameter.

[0134] Embodiments of the invention having a magnet array 21 disposed within the drum cavity 26 advantageously enable a magnetically enhanced plasma to be defined with a small mechanical footprint, due to the magnets being contained inside the drum 10. This lends itself to retrofitting such a drum in existing plasma processing devices. In some embodiments, separate processing functions can be achieved with a magnet array consisting of a single magnet assembly that is conveniently housed within the drum 10. In some embodiments, such as those described with reference to FIGS. 9 and 10, race track portions can be defined at a plurality of discreet positions around the drum using a single magnet assembly.

[0135] Embodiments of the invention having a magnet array 21 disposed within the drum cavity 26 can use any suitable means of plasma curing i.e. these embodiments are not limited to using an ion flux having an energy level between 3.6 eV and 250 eV for curing and/or processing.

[0136] Embodiments of the invention may include a magnet array arranged to form one or more race tracks having any suitable configuration.

[0137] Thus, embodiments of the invention provide a low energy ion flux that can be used for curing or processing steps. An advantage to using an ion flux having an energy level between 3.6 eV and 250 eV for the curing, rather than an electron flux having an energy level between 6.5 eV and 300 eV, is that any overspray of radiation curable material or re-evaporate thereof will also be cured due to species generated at earthed surfaces inside the process chamber.

[0138] The functional element of the radiation curable precursor is any saturated or unsaturated material capable of being vaporised or atomised and sprayed onto the substrate, and also capable of being polymerised by the ion flux. Precursors can be organic or inorganic and include unsaturated organic materials, silicon-based materials, halogen-based materials, organo-metallic composites etc, with acrylates such as tripropylene glycol diacrylate or isobornyl acrylate being preferred. Most polymerisable materials described in the art can be used in the process. The vaporised or atomised material may optionally include other radiation curable or non-curable components to provide functionality such as adhesion promotion, dimensional stability, mechanical properties, colour, antibacterial properties, hydrophillia, hydrophobia, electrical conductivity etc.

[0139] The thickness of the precursor film or the cured polymer coating can be any suitable value. For example, in some embodiments the value may be at least 0.001 m. In some embodiments, the value is in the range 0.001 m-50 m, and preferably 0.01 m to 1 m, the preferred thickness largely being decided on the basis of the function of the polymer layer in the intended application, and cost constraints, rather than constraints arising from the process. For example, for barrier packaging applications, the function of the polymer layer is to protect the barrier coating (i.e. the aluminium or aluminium oxide) against physical damage or abrasion. In this case, the lower limit of thickness of the polymer layer may be around 0.02 m, as below this there is insufficient protection. The upper limit may be subjective, as above about 1 m, the benefit of mechanical protection will begin to be outweighed by the risk of delamination.

[0140] Any web substrate which can be handled by the equipment can be used in the invention. Substrates can include a wide variety of commercially available thermoplastic films (including polyesters such as polyethylene terephthalate (PET) or polyethylene naphthalate (PEN) or blends or coextrusions thereof), polyamides (including nylon 6 and nylon 6.6), polyolefines (including polypropylene and high and low density polyethylene) and other thermoplastic films known in the art. Non-thermoplastic films, including biodegradable films and films derived from renewable resources, such as polylactic acid or cellulose-based materials including cellulose diacetate, also known as cellulose acetate, may also be used. Thermoset polymer films, such as polyimides may also be used. Fibrous, non-woven or woven substrates (such as paper or textiles) may also be used. The invention is not limited by this list of web substrates.

[0141] The process of embodiments of the invention may be a high speed process, meaning that the web substrate is moving at a speed of at least 50 m/min. It is preferred that the web is moving at a speed of at least 5 m/s, and more preferably that that the web is moving at a speed of at least 7 m/s. In some embodiments of the invention, the web may form part of a reel to reel process.

[0142] Embodiments of the invention may use any easily ionisable inert gases to generate the plasma; for example argon, helium and neon, or other non-reactive gases or reactive gases including nitrogen or oxygen. Combinations of gases could be used to tailor the gas to specific applications. The gas used to generate the plasma is distinct from the radiation curable monomer. This may provide a more controllable and practicable method compared to generating a plasma using the monomer itself, due to the quantities involved. For example, the high flow rates, such as 25 ml per minute, used in embodiments of the invention would cause considerable vacuum problems if ionised in a plasma.

[0143] One or more further gases may be added to the primary gas used to create the plasma, the further gas(es) being arranged to perform one or more additional functions such as removing unwanted species from the web, or including certain species in the developing polymer film on the web substrate. The use of an ion flux as the primary curing initiator has a further advantage over the use of an electron flux in that the ion flux may contain ionised species from both the primary plasma gas and the further plasma gas, meaning that, even with the plasma spaced from the web substrate, the further gas can act upon the web or polymer film though migration of its ions. In one example, hydrogen could be used to passivate the surface. In an other example, nitrogen could be introduced as the further gas in order to introduce a reactive bonding species aimed at increasing or changing the cross-linking within the film.

[0144] The moving substrate is exposed to the ion flux for a period of time inversely proportional to the web speed. This period of time shall be referred to as the dwell time and this can be influenced by the web speed and the length of web being exposed to the flux, which shall be referred to as the dwell length. It is preferred that the dwell length be as short as is reasonably practicable. A unit power dose measured in W/cm.sup.2 experienced by the web can be calculated by dividing the operating power of the plasma generator by the cross sectional area of the ion flux. The unit power dose can be used with the dwell time to establish a unit energy dose on the web, measured in J/cm.sup.2. With a known flow rate of radiation curable precursor and width of delivery the energy dose per unit precursor can be attained.

[0145] The plasma generator used in embodiments of the present invention may be connected to a an AC or a DC power supply. Depending on the power supply used, it is possible to create and control an ion flux having the stated energy ranges, such as an energy level that is no greater than 250 eV or an energy level that is no greater than 100 eV. For example, the voltage applied to the plasma generator may define the maximum energy level and as such applying 250V results in an ion flux having a maximum energy level of 250 eV.

[0146] In embodiments of the invention it is preferred that the unit energy dose, described above, is no greater than 15 J/cm.sup.2, more preferably no greater than 13 J/cm.sup.2, and in some embodiments the unit power may be no greater than 0.1 J/cm.sup.2. It is preferred that the dwell length, as described above is between 5-50 cm and even more preferred to be 10 cm. A short flux may undesirably limit the line speed of the web, whereas a long flux length may lead to undesirably high power consumption and impracticability of space. It is preferred that the dwell time be as low as possible whilst still giving full cure to ensure a high process efficiency.

[0147] The substrate can optionally be pre-coated or post-coated, vacuum deposited or printed with a wide variety of metals, metallic or non-metallic compounds and other materials, in order to achieve desired properties or effects. For non-transparent barrier applications, for example, substrates such as polyester films coated with a metal such as aluminium are especially preferred. For transparent barrier applications, substrates such as polyester films coated with a transparent metallic or non-metallic oxide, nitride or other compound (e.g. oxide of aluminium or oxide of silicon) are especially preferred. For electrical or electronic applications, the web substrate may be optionally pre-coated with a metal such as copper or another conductive inorganic or organic material, which however may be transparent or non-transparent. However, the invention is not limited to these specified coatings.

[0148] For very high barrier applications, a plurality of barrier layers, separated by polymer layers, is used, as this extends the diffusion pathway for gas or vapour between the permeable defects in each barrier layer. In this case, since the polymer layer is functioning as a separating layer between two metal or ceramic layers, and has little or no inherent barrier of its own, it should preferably be as thin as practicable, conducive with the requirements that it should be continuous, i.e. with no voids or defects, and have good surface smoothness to maximise the barrier of the second or subsequent barrier layer.

[0149] For optically variable devices, the function of the polymer layer is to generate light interference, and thus produce a colour shift. For such applications, a coating thickness of approximately a quarter to half of the wavelength of the incident light is preferred but the invention is not limited by this thickness.

[0150] Materials manufactured by the invention are suitable for use in multiple different applications including: packaging applications; abrasion-resistant material or intermediate (in which the polymer coating prevents abrasion damage to any underlying functional layers during conversion or use); security or anti-counterfeit applications, including continuously optically variable devices; decorative applications, including continuously optically variable devices; functional industrial applications; and electrical or electronic applications (inclusive of static electricity dissipation).

[0151] Some more specific examples of embodiments of the invention will now be set out.

Example 1

[0152] A planar magnetron such as that shown in FIG. 4 was electrically connected to a DC power source such that the reaction plate 16 and inner core 18 were anodic and held at a power of 1 kW. The voltage applied did not deviate beyond the range 220-240V throughout the experiment. The approximate energy dose on the web during this trial was 12 J/cm.sup.2. The surrounding electrode 15 and outer case 17 were connected to earth. An argon and oxygen gas mixture was delivered through the delivery 23. This curing plasma was positioned downstream of an acrylate delivery system. The delivery flow rate of the acrylate system was set to 15 ml/min distributing an acrylate vapour over a 12 m thick PET substrate of 400 mm width travelling at approximately 1 m/min. The process was run for approximately 10 minutes before venting. Upon checking the material, it was found to have excellent adhesion and resistant to flexing.

Example 2

[0153] A roller magnetron similar to FIG. 9 where the high density plasma (race track) zones 6a, 6b were rotationally spaced by approximately 135 was connected to an RF power source such that the entire roller surface was held at a power of 0.3 kW over a magnetron area of 500100 mm. This plasma dose was therefore 0.6 W/cm.sup.2. The voltage applied stayed within the range of 180-220V during the experiment. The roller assembly was floated from earth. The delivery flow rate of the acrylate system was set to 10 ml/min distributing an acrylate vapour over a 12 m thick PET substrate of 400 mm width travelling at approximately 100 m/min. This gave a 0.06 s dwell time in the plasma, hence the approximate energy dose on the web during this trial was 3.610.sup.2 J/cm.sup.2. The substrate subsequently traveled to a metallisation zone for an aluminium coating of between 2.0-2.5 optical density within the same machine. Both the acrylate system and metallisation processes occurred concurrently in time. The processes were run for approximately 5 minutes before venting. Upon checking the material, it was found to have excellent adhesion and oxygen and moisture barrier.

Example 3

[0154] In this example, a simulated small roller magnetron similar FIG. 12, was setup in a Bell Jar vacuum and utilised three magnetic arrays 21, space equally around the roller (rotationally spaced by 120). The roller surface was connected to an RF power source running at a frequency of 175 kHz and an approximate power of 100 W. When in operation, three distinct race tracks formed on the surface of the roller with the race track zone centres rotationally spaced by 120 around the surface in the same manner as the magnet arrays. This was sustained for approximately 5 minutes and was stable.

Example 4

[0155] In this example, a roller magnetron similar to FIG. 13 was used to plasma pre-treat a substrate prior to metallising. The roller surface was connected to an RF power source running at a frequency of 40 kHz sustaining 0.3 kW with a voltage 200V. The approximate energy dose on the substrate was 3.610.sup.2 J/cm.sup.2. The substrate was subsequently exposed to a metallisation zone for an aluminium coating of between 2.0-2.5 optical density. The process was run for approx 10 minutes at a line speed of 100 m/min before venting. The material was checked and found to have excellent metal adhesion and oxygen and moisture barrier.

Example 5

[0156] In a further experiment following the above example 4, the substrate line speed was reduced in stages to observe the level the substrate could endure before thermal degradation. Carbonisation of the web was observed at a web speed of 0.25 m/min. At 0.5 m/min some film distortion was noted, above 1 m/min no damage was observed on the substrate. The roller surface was connected to an RF power source running at a frequency of 40 kHz sustaining 0.3 kW with a voltage 200V. At the point of observed thermal degradation, when run at approximately 0.25 m/min line speed, giving a 24 second dwell time in the plasma, the energy dose to the substrate was 14.4 J/cm.sup.2.