Process for transferring microstructures to a final substrate

Information

  • Patent Grant
  • 10899120
  • Patent Number
    10,899,120
  • Date Filed
    Friday, November 23, 2018
    5 years ago
  • Date Issued
    Tuesday, January 26, 2021
    3 years ago
Abstract
A process for transferring microstructures to a flexible or rigid final substrate that offers advantages in both speed and precision is provided. The inventive process involves subjecting a transfer film in a continuous roll-to-roll process to the following operations: either forming microstructures on, or transferring microstructures to a surface of the transfer film; and then transferring the microstructures from the transfer film onto a surface of the final substrate. The microstructures are single or multi-layer structures that are made up of: voids in a substantially planar surface, the voids optionally filled or coated with another material; raised areas in a substantially planar surface; or combinations thereof.
Description
TECHNICAL FIELD

The present invention generally relates to a continuous roll-to-roll process for producing and transferring security devices in the form of microstructures from a transfer film to a final substrate.


BACKGROUND AND SUMMARY OF THE INVENTION

Security threads as well as security patches may be mounted on a surface of a security document (e.g., currency or banknote paper) or label either during or post manufacture. Mounting of these devices may be achieved by any number of known techniques including: applying a pressure-sensitive adhesive to the backside of the device and pressing the device to the surface of the document or label; and applying a heat activated adhesive to the backside of the device and applying the device using thermal transfer techniques, to the surface of the document or label.


The production of these security devices and the application of these devices to security documents or labels take place in separate operations. Combining these operations in a continuous roll-to-roll process for producing and transferring these security devices to a final substrate would realize advantages in both speed and precision.


The present invention fulfills this need by providing a continuous roll-to-roll process for producing and transferring security devices in the form of microstructured elements or microstructures from a transfer film to a final substrate.


More specifically, the present invention provides a transfer film for transferring microstructures to a final substrate. The microstructures transferred by the transfer film to a final substrate are single or multi-layer structures that comprise: voids in a substantially planar surface, the voids optionally filled or coated with another material; raised areas in a substantially planar surface; or combinations thereof.


In a first exemplary embodiment, the transfer film comprises a carrier film and one or more thermal release adhesive layers on a surface of the carrier film, wherein the thermal release adhesive layer(s) is made up of a plurality of expandable microspheres and one or more pressure sensitive adhesives.


The term “thermal release adhesive”, as used herein, means an adhesive that decreases its adhesion to a surface when heated to temperatures higher than about 60° C., while the term “expandable microspheres”, as used herein, means polymer microspheres that start expansion and/or foaming when heated to temperatures higher than about 60° C.


Thermal release adhesives (e.g., thermal release tapes) are known in the art and have been used in semiconductor wafer processing and other electronic component manufacturing processes. Suppliers of thermal release products used for electronic applications include Nitto Denko Corporation, 1-2, Shimohozumi 1-chome Ibaraki-shi, Osaka Japan (Nitto Denko), which sells REVALPHA® thermal release adhesive tapes and sheets, and Haeun Chemtec Co., Ltd., Shingil-dong, Danwon-gu, Ansan, Kyungki-do, 425-839, Korea, which sells REXPAN™ heat release film. However, the thickness and cost of these products are prohibitive for anything other than small scale samples, and are not suitable for volume production as described herein.


The term “pressure sensitive adhesive”, as used herein, means an adhesive that needs only minimal pressure to adhere or stick to a surface.


In an exemplary embodiment, the one or more thermal release adhesive layers are prepared from a formulation comprising from about 25 to about 99% by wt. (preferably, from about 75 to about 97% by wt., more preferably, from about 90 to about 96% by wt.) of an energy (e.g., ultraviolet (UV) radiation) curable pressure sensitive adhesive (PSA) formulation, and from about 1 to about 75% by wt. (preferably, from about 3 to about 25% by wt., more preferably, from about 4 to about 10% by wt.) of expandable microspheres.


In this exemplary embodiment, the energy curable PSA formulation generally comprises:

    • from about 5 to about 95% by wt. (preferably, from about 10 to about 70% by wt., more preferably, from about 30 to about 60% by wt.) of one or more elastomeric oligomers;
    • from about 1 to about 75% by wt. (preferably, from about 5 to about 60% by wt., more preferably, from about 10 to about 40% by wt.) of one or more tackifying resins;
    • from about 0.5 to about 75% by wt. (preferably, from about 5 to about 60% by wt., more preferably, from about 20 to about 50% by wt.) of one or more reactive monomeric diluents; and
    • from about 0.1 to about 15% by wt. (preferably, from about 1 to about 8% by wt., more preferably, from about 3 to about 6% by wt.) of one or more photoinitiators.


In a second exemplary embodiment, the transfer film comprises a carrier film and one or more cured binder layers. In this embodiment, the microstructures have one or more cured conformal release coating layers on a surface thereof, and are bonded to the transfer film by way of the one or more cured binder layers. Heat is not required to initiate release during transfer of the microstructures.


The present invention further provides a method of using the transfer films described above, which method comprises using the transfer films (a) to transfer the above-described microstructures in a continuous roll-to-roll process to a final substrate, or (b) as manufacturing substrates during production of the microstructures and then to transfer the microstructures in a continuous roll-to-roll process to a final substrate.


Also provided is a process for transferring microstructures to a final substrate. In a first exemplary embodiment, the process comprises subjecting the transfer film first described above in a continuous roll-to-roll process to the following operations: either forming microstructures on, or transferring microstructures to a surface of the thermal release adhesive layer(s) of the transfer film, wherein the microstructures are single or multi-layer structures that comprise: voids in a substantially planar surface, wherein the voids are optionally filled or coated with another material; raised areas in a substantially planar surface; or combinations thereof; and then transferring the microstructures from the transfer film onto a surface of the final substrate.


In a first preferred embodiment, the process comprises: forming the microstructures on a surface of a disposable manufacturing substrate; bringing the formed microstructures into contact with a surface of the transfer film while applying pressure thereto, thereby activating the pressure sensitive adhesive in the thermal release adhesive layer(s) of the transfer film, adhering the microstructures to its surface; stripping away the disposable manufacturing substrate; applying one or more heat and/or pressure activated adhesives to the microstructures on the transfer film; bringing the adhesive coated microstructures on the transfer film into contact with a surface of the final substrate while applying both heat and pressure to the transfer film, thereby causing the microspheres in the thermal release adhesive layer(s) to expand (or foam) and deactivate the pressure sensitive adhesive, allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, allowing the microstructures to adhere to the surface of the final substrate.


This embodiment is particularly suited for microstructures having so-called “up/down non-parity” (e.g., refractive optical systems). As will be readily appreciated by those skilled in the art, such structures are intended to be viewed from a top or upper side rather than a bottom or lower side. The inventive process allows the microstructures on the disposable manufacturing substrate to be visually inspected for quality assurance purposes before transferring the microstructures to the transfer film, and further allows the microstructures to be properly positioned in an upright position on a surface of the final substrate.


In a second preferred embodiment, the process comprises: forming the microstructures on a surface of the thermal release adhesive layer(s) of the transfer film; applying one or more heat and/or pressure activated adhesives to the formed microstructures on the transfer film; bringing the adhesive coated microstructures into contact with a surface of the final substrate while applying both heat and pressure to the transfer film, thereby causing the microspheres in the thermal release adhesive layer(s) to expand (or foam) and deactivate the pressure sensitive adhesive, allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, allowing the microstructures to adhere to the surface of the final substrate.


This embodiment is particularly suited for microstructures that do not require an upper/lower surface inspection (e.g., conductive circuit elements or structures). Such structures could be symmetrical in cross section and are not necessarily intended to be viewed from a top or upper side rather than a bottom or lower side.


In a second exemplary embodiment, the process is a continuous roll-to-roll process that comprises:

    • forming the microstructures on a surface of a disposable manufacturing substrate;
    • applying one or more release coating layers to a surface of the microstructures, the release coating layer(s) conforming to the microstructure surface, and then curing the release coating layer(s);
    • applying one or more binder layers to a surface of a carrier film and optionally also to the cured release coated surface of the microstructures, and while these surfaces are in contact with each other, curing the binder layer(s);
    • mechanically removing the disposable manufacturing substrate from the microstructures now bonded to the carrier film; and then
    • transferring the microstructures from the carrier film onto a surface of the final substrate.


In a preferred embodiment, the microstructures are transferred from the carrier film onto a surface of the final substrate by: applying one or more heat and/or pressure activated adhesives to the microstructures on the carrier film; bringing the adhesive coated microstructures on the carrier film into contact with a surface of the final substrate; applying both heat and pressure to the carrier film and then lifting the carrier film from the microstructures causing separation between the microstructures and the release coating layer(s), thereby allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, thereby allowing the microstructures to adhere to the surface of the final substrate.


Other features and advantages of the invention will be apparent to one of ordinary skill from the following detailed description and accompanying drawings.


Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. All publications, patent applications, patents and other references mentioned herein are incorporated by reference in their entirety. In case of conflict, the present specification, including definitions, will control. In addition, the materials, methods/processes, and examples are illustrative only and not intended to be limiting.





BRIEF DESCRIPTION OF THE DRAWINGS

Particular features of the disclosed invention are illustrated by reference to FIG. 1, which is a schematic flow diagram of the second exemplary embodiment of the inventive process for transferring microstructures to a final substrate. Components in this drawing are not necessarily to scale, emphasis instead being placed upon clearly illustrating the principles of the present disclosure.





DETAILED DESCRIPTION OF THE INVENTION

The subject invention provides methods or processes for producing microstructures (e.g., precision cast microstructures) on a continuous roll-to-roll substrate or film in ways that allow these microstructures to be subsequently transferred to a final substrate. Advantages in speed and precision are realized by using roll-to-roll processes to produce microstructures, while providing a means for transferring the microstructures to a final surface that is not necessarily compatible with or suitable for flexible web processing (e.g., rigid final substrates such as glass). In this way, final substrates may have precision microstructures applied to their surface, without being subjected to all of the conditions which are necessary for the production of, for example, precision cast microstructures.


The present invention is useful in the production of passport security laminates, the application of security patches or seals on value documents, labels on products, thin films or foils to banknotes, conductors or insulating circuit components onto rigid substrates, and other general applications of microstructured elements or microstructures to a surface.


For avoidance of doubt, nanostructures are also contemplated by the present invention, as are (as alluded to above) end-use applications outside of the security field.


Exemplary embodiments of the inventive system will now be disclosed. There is no intent, however, to limit the present disclosure to the embodiments disclosed herein. On the contrary, the intent is to cover all alternatives, modifications and equivalents.


The microstructures used in the present invention are single or multi-layer structures that comprise: voids in a substantially planar surface, the voids optionally filled or coated with another material; raised areas in a substantially planar surface; or combinations thereof. In an exemplary embodiment, the microstructures (e.g., optical or physical structures) are precision cast microstructures that include any and all types of structures whose form may be produced by backfilling a negative void in a cured or hardened matrix on a flexible substrate.


Examples of such contemplated precision cast microstructures include multilayer optical systems such as refractive, reflective, diffractive, and hybrid micro-optic structures, as well as other single or multilayer structures such as conductive traces, circuit patterns, microlenses, waveguides, negative space air lenses, insulating ceramic structures, icon image elements, microtext, anti-reflective structures, light refracting prisms, micromirror structures, patterned semiconductors, patterned or unpatterned metallization, fluorescent security print, porous filtration structures, chemical or electronic sensor elements, photoresist masking structures, ruled gratings, periodic or aperiodic arrays, structures for increasing surface area, tactility altering structures, structures for facilitating mechanical bonding, etc.


Generally speaking, the size of these microstructures (i.e., width or depth) is limited only by that which is achievable by casting from an embossing tool onto a flexible substrate. The size may range from tens of nanometers (a few atomic layers thick) in depth in some cases to a few micrometers in most cases, and up to millimeter scale structures.


Precision casting of microstructures in a roll-to-roll form on a flexible substrate or film has many advantages, particularly when considered together with a transferrable process, as will be described. The term “precision casting”, as used herein, means the replication of a microstructured surface having a predesigned pattern of voids and/or raised areas, or negative and positive features.


By using radiation cured polymers on film, or hot embossable films, for example, the surface of the master is copied continuously, and a precise pattern of voids and/or raised areas may be formed in a cured matrix, resulting in precisely formed microstructures or “icon elements.” Exemplary processes are described in U.S. Pat. No. 7,333,268 to Steenblik et al., U.S. Pat. No. 7,468,842 to Steenblik et al., U.S. Pat. No. 7,738,175 to Steenblik et al., U.S. patent application Ser. No. 12/820,320 to Steenblik et al., and U.S. patent application Ser. No. 13/360,017 to Samuel M. Cape et al., which are all incorporated herein by reference in their entirety. By casting these structures, each negative space results in a voluminous region that can be backfilled with a second material that can be much different than the material used to cast the matrix. For example, slurries, pastes, dispersions, gels, powders, liquids, and flakes may all be used to fill the voids, resulting in a precision element that is contained within the volume of the matrix. This allows for the formation of shapes using materials that would be difficult or impossible to cast without using this matrix backfilling technique. The backfilled material may be further cured, washed, etc. to ensure desired properties such as degree of crosslinking, etc.


Once a first layer of such backfilled embossed matrix has been formed, any practical number of additional layers may be added thereafter, such as a second layer of backfilled precision elements, or precision elements that are not backfilled such as a microlens layer, or a polymer spacer layer followed by a microlens layer, a metallization layer, or other functional coatings. Additionally, it is possible and often desirable to apply a coating to the flexible substrate before the first microstructured layer is cast, in order to facilitate replication from the embossing master and for removal of the microstructured elements at a later time. This coating may be tailored to provide adhesion or release properties between the flexible substrate and the microstructured layer. For example, such a coating may be prepared from polymers having low surface energy, such as UV curable silicone-modified polyacrylates.


In an example of the first exemplary embodiment of the inventive process for transferring microstructures having “up/down non-parity”, the precision cast single or multi-layer microstructures are formed on a flexible disposable manufacturing substrate, and then the microstructures are transferred away from the manufacturing substrate and onto a new carrier film having one or more thermal release adhesive layers. The thermal release adhesive layer(s) is used to provide a strong bond between the new carrier film and the microstructures and to allow for the release of these microstructures at a later time upon the application of heat. To summarize, the inventive process:

    • a) Enables the removal of the flexible disposable manufacturing substrate (i.e., base film) from the precision cast microstructures, which lack any significant strength, body or structural integrity when taken by themselves;
    • b) Enables the conversion and handling of the microstructured elements using traditional web or sheet based equipment such that further coatings and adhesives may be applied, and so that the otherwise fragile structures may be slit, die-cut, perforated, sheeted, etc.; and
    • c) Enables the transfer of the microstructures from the thermal release adhesive coated carrier film (i.e., the TRA transfer film) to a final substrate without suffering from damaging effects of the transfer process such as heat, pressure, and tension, while allowing the carrier film to be rewound and discarded after the transfer process is complete.


The thermal release adhesive layer(s) of the transfer film provides a strong bond between the precision cast microstructures and the new carrier film yet has a mechanism for decisive, predictable release at a later time when the microstructures are transferred to the final substrate.


The formulation used to prepare the thermal release adhesive layer(s) of the present invention is made specifically to have strong bonding at room temperatures, and significantly reduced bond strength when elevated temperatures are applied. The adhesive formulation may be said to be ‘activated’ when it is in the low temperature, high bond strength state, and ‘deactivated’ when it is in an elevated temperature, diminished bond strength state.


As noted above, the inventive thermal release adhesive formulation, in a more preferred embodiment, comprises from about 90 to about 96% by weight of an energy curable PSA formulation, and from about 4 to about 10% by weight of expandable microspheres.


The energy curable PSA formulation used in the inventive thermal release adhesive formulation, in a more preferred embodiment, comprises:

    • from about 30 to about 60% by wt. of one or more elastomeric oligomers, which provide high elongation and structure to the formulation;
    • from about 10 to about 40% by wt. of one or more tackifying resins, which impart elasticity, flexibility and adhesion to the formulation;
    • from about 20 to about 50% by wt. of one or more reactive monomeric diluents, which serve to modify the degree of crosslinking and the glass transition temperature of the formulation; and
    • from about 3 to about 6% by wt. of one or more photoinitiators.


Specific examples of suitable PSA formulations include, but are not limited to, the following:


PSA Formulation 1:















30 wt. %
trimethylolpropane triacrylate, which is sold



under the trade designation SR-351 by



Sartomer Company of Exton, PA., USA.



(Sartomer)


33 wt. %
aromatic urethane/tackifier oligomer, which



is sold under the trade designation CN3000



by Sartomer


33 wt. %
isobornyl acrylate, which is sold under the



trade designation SR-506 NS by Sartomer


 4 wt. %
liquid mixture of two photoinitiators, sold



under the trade designation OMNIRAD



1000 by IGM Resins Inc. of St. Charles, IL,



USA (IGM)









PSA Formulation 2:















19 wt. %
urethane acrylate oligomer, which is sold



under the trade designation CN973H85 by



Sartomer


32 wt. %
tackifier resin, which is sold under the trade



designation S115 by Sartomer


45 wt. %
2(2-ethoxyethoxy) ethyl acrylate



(EOEOEA), a reactive monomeric diluent,



which is sold under the trade designation



SR256 by Sartomer


 4 wt. %
2-hydroxy-2-methyl-1-phenyl-1-propanone



photoinitiator, which is sold under the trade



designation OMNIRAD 73 by IGM









Specific examples of suitable expandable microspheres, which start expansion and/or foaming when heated to temperatures higher than about 60° C., include:

    • expandable plastic microspheres, sold under the trade designation EXPANCEL® by Casco Adhesives AB, P.O. Box 11538, Stockholm, Sweden 100 01 (Casco);
    • dry thermoplastic microspheres, sold under the trade designation DUALITE® by Henkel Corporation, One Henkel Way, Rocky Hill, Conn. 06067 (Henkel);
    • thermal expandable microsphere, sold under the trade designation ADVANCELL EM by Sekisui Kagaku Kogyo Kabushiki Kaisha (dba Sekisui Chemical Co. Ltd.), 4-4, Nishitemma 2-chome, Kita-ku Osaka-shi, Osaka, Japan 530-8565 (Sekisui); and
    • expandable microspheres available from Matsumoto Yushi-Seiyaku Co., Ltd., 2-1-3 Shibukawa-cho Yao-shi, Osaka, Japan (Matsumoto), Kureha Corporation, 3-3-2, Nihonbashi-Hamacho, Chuo-ku, Tokyo, Japan 103-8552 (Kureha), and Hangzhou Hi-Tech Fine Chemical Co., Ltd., Haihong Technical and Industrial Area, Liangzhu Town, Yuhang District, Hangzhou, Zhejiang, China (Haihong Group).


A specific example of a suitable TRA formulation is set forth below:


TRA Formulation:















90 wt. %
a radiation curable PSA formulation, which



is sold under the trade designation



AROCURE ™ by Ashland Inc., 50 E.



RiverCenter Blvd., P.O. Box 391,



Covington, KY 41012-0391 (Ashland)


10 wt. %
expandable microspheres, which are sold



under the trade designation EXPANCEL ™



by Akzo Nobel Inc., 525 West Van Buren,



Chicago, IL 60607, USA (Akzo Nobel).









The TRA works through the mechanism of microsphere expansion, allowing for precise control of release. During the release process, the adhesive bond strength declines dramatically. In one example, the bond strength of the activated TRA was found to be between 5.3 to 9.6 Newtons/inch (N/in), while the heat-deactivated strength was measured to be approximately 0.9 to 0.1 N/in. Typical microspheres for this use will start expanding at 80-180° C. and continue to expand up to 125-220° C. Once the adhesive has been heated in this way, the tack and bond strength are permanently reduced.


Before expansion, the microspheres preferably range from 5 to 50 microns in diameter, and after heating they preferably expand to 15 to 150 microns in diameter. More preferably, the microspheres range from 6 to 20 microns in diameter before expansion.


Prior to heating, preferable thermal release adhesive layer thicknesses range from 3 to 100 microns and more preferably from 5 to 25 microns. After heating, this layer will typically double in thickness.


Preparation of the TRA formulation may be accomplished by combining premixed energy curable PSA in its liquid state with the weighed quantity of polymeric microspheres (e.g., polymeric microsphere powder), followed by blending with a high shear mixer. The resulting suspension of powder with energy curable PSA will remain stable in its liquid form for an extended period of time as long as exposure to sources of heat and UV radiation are avoided.


The TRA formulation is applied to a carrier film. Suitable carrier films may be any flexible material that is capable of receiving a coating and being conveyed through production equipment. For example, polymeric materials such as biaxially oriented polyethylene terephthalate (PET), polypropylene (PP), nylon 6 polyamide (PA), polyethylene napthalate (PEN), cellulose acetate or other film materials, as well as non-polymeric materials such as paper constitute suitable carrier films.


Methods suitable for liquid adhesive application may be used to apply the TRA formulation to a carrier film as long as the microsphere activation temperature is not exceeded. For example, a suitable layer thickness of TRA formulation may be achieved by drawing down onto a carrier film with a wire wrapped rod (e.g., a #14 Meyers rod), or by means of a flexographic printing unit or gravure cylinder. The liquid TRA formulation may be heated above room temperature in order to reduce the viscosity for ease of application (i.e., to facilitate pumping or pouring) as long as the microsphere activation temperature is not exceeded. When a thin layer has been applied to the carrier film with the desired thickness (e.g., 15 micron thickness), the TRA may be cured by UV radiation, for example, by passing the coated carrier film beneath a 300 Watts/in Hg lamp at 40 fpm. Alternatively, the TRA may be electron beam cured by passing the uncured resin through an e-beam curing unit. In addition, both methods may be used in combination.


Once cured, the TRA becomes activated so that it has high tack and peel strength (e.g., peel strength values ranging from about 5 to about 50 N/in (ASTM D903-98)), and is ready to be brought into contact with the desired bonding surface. For example, a flexible micro-optic security film may be brought into contact with the TRA and carrier film (i.e., the TRA transfer film), forming a laminated structure that remains bonded until it is desirable to release the bond by application of heat.


The entire laminated structure thus formed may then be rewound and handled as a single flexible film, allowing further processing such as: stripping away the base manufacturing film, applying adhesives on the exposed side of the micro-optic film, die cutting, printing, metalizing, or other film converting operations. The adhesive bond of the TRA may then be deactivated by heating (e.g., 80-220° C.) at a point in time when it is advantageous to transfer the microstructure from the TRA transfer film (e.g., TRA/60 gauge PET carrier film) onto the final substrate. As noted above, such a process may be useful in the production of passport security laminates, the application of security patches or seals on value documents, labels on products, thin films or foils to banknotes, conductors or insulating circuit components onto rigid substrates, and other general applications of microstructured elements or microstructures to a surface.


Deactivation of the TRA occurs whenever the softening temperature of the polymeric shell of the microspheres has been reached or exceeded, causing volume expansion (or foaming) and a significant decrease in the adhesive bond strength compared to its preheated state. Heating methods suitable for causing deactivation of the TRA include forced hot air, heated roller, infrared heating, oven or hotplate heating, heated foil stamping roller, passport laminator, heated shoe, heated platen, heated bath, and the like.


In a preferred process for transferring microstructures having “up/down non-parity” to a final substrate, the continuous roll-to-roll process comprises:

    • forming microstructures on a disposable flexible manufacturing substrate;
    • optionally, backfilling the microstructures with a curable material;
    • applying an energy curable TRA in liquid form to a separate carrier film and curing by application of UV light, e-beam radiation, or both, thereby forming a “TRA transfer film”;
    • nipping together the formed microstructures on the flexible manufacturing substrate to the TRA layer of the TRA transfer film, thereby activating the pressure sensitive adhesive in the TRA layer and allowing the adhesive to adhere the microstructures to the TRA layer;
    • stripping away the disposable flexible manufacturing substrate;
    • converting the microstructure/TRA transfer film using methods known in the art, including, but not limited to, applying other heat and/or pressure activated adhesives (e.g., tack-free, heat-activated adhesives), primers or coatings, to the transfer film, followed by slitting or die cutting the film to desired final dimensions, and sheeting the cut film into stacks or rewinding onto reels or spools, thereby forming a “transfer ready system”;
    • transferring the adhesive-coated microstructures to a final substrate by bringing the microstructures on the transfer ready system into contact with the final substrate for thermal lamination, whereby heat and pressure are applied to the transfer ready system, thereby causing the microspheres in the TRA layer to expand (or foam) and deactivate the pressure sensitive adhesive, thereby allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, allowing the microstructures to adhere to the surface of the final substrate; and
    • rewinding and discarding the transfer film with deactivated TRA, leaving the final substrate with newly affixed microstructures on its surface, ready for further processing or printing as desired.


In an exemplary embodiment, the microstructure is a multi-layer optical system in the form of a security thread or foil, and the final substrate is banknote paper. In this exemplary embodiment, the heat and pressure of lamination causes the thread/foil to securely bond to the banknote paper, while at the same time exceeding the deactivation temperature of the TRA, thereby causing the TRA and carrier film to separate from the thread/foil. This process provides an advantageous means of delivering a security thread/foil to banknote paper, following by rewinding and discarding the carrier film containing deactivated TRA.


In another exemplary embodiment, the microstructure is a die-cut, heat-seal label, and the final substrate is product packaging.


In an exemplary embodiment of the inventive process for transferring microstructures having “up/down parity” (i.e., cross-sectional symmetry), the precision cast single or multi-layer microstructures are formed directly on the TRA transfer film, and then the microstructures are transferred away from the TRA transfer film onto the final substrate. In this configuration, care must be taken to avoid overheating the TRA during the microstructure casting step. Casting resins with low viscosities (resins that do not need additional heat to flow freely such as neopentyl glycol diacrylate (available from Sartomer under the trade designation SR247)), combined with an internally water cooled casting surface (comparable to a flexographic chill drum) allow microstructures to be UV cured against the TRA without overheating the expandable microspheres or causing premature expansion.


In a preferred process, the continuous roll-to-roll process comprises:

    • applying an energy curable TRA in liquid form to a separate carrier film and curing by application of UV light, e-beam radiation, or both, thereby forming a “TRA transfer film”;
    • forming microstructures on the TRA transfer film;
    • optionally, backfilling the microstructures with a curable material;
    • converting the microstructure/TRA transfer film by applying other heat and/or pressure activated adhesives (e.g., tack-free, heat-activated adhesives), primers or coatings, to the transfer film, followed by slitting or die cutting the film to desired final dimensions, and sheeting the cut film into stacks or rewinding onto reels or spools, thereby forming a “transfer ready film”;
    • transferring the adhesive-coated microstructures to a final substrate by bringing the microstructures on the transfer ready system into contact with the final substrate for thermal lamination, whereby heat and pressure are applied to the transfer ready system, thereby causing the microspheres in the TRA layer to expand (or foam) and deactivate the pressure sensitive adhesive, thereby allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, allowing the microstructures to adhere to the surface of the final substrate; and
    • rewinding and discarding the transfer film with deactivated TRA, leaving the final substrate with newly affixed microstructures on its surface, ready for further processing or printing as desired.


In an exemplary embodiment, the microstructure is an embedded lens array structure, and the final substrate is a laser engravable polycarbonate substrate. Here, the embedded lens array structure is made up of a low refractive index (RI) (e.g., n=1.35-1.45) concave polymeric matrix backfilled with high RI (e.g., n=1.5-1.8) polymer, the applied adhesive is a heat-activated adhesive, and the embedded lens array structure of the transfer ready film is brought into contact with a surface of the laser engravable polycarbonate substrate and heated under pressure to a point in which the embedded lens array structure is thermally laminated to the surface of the polycarbonate substrate. In this embodiment, the heat and pressure of lamination causes the embedded lens structure to securely bond to the intended polycarbonate final substrate, while at the same time exceeding the deactivation temperature of the TRA, causing the TRA transfer film to separate from the embedded lens structure. This process provides an advantageous means of delivering a lens structure to a surface of a laser engravable polycarbonate surface, such that further processing steps may occur, such as laser writing through the lens structure into the polycarbonate, providing an optically variable laser written effect.


In another exemplary embodiment, the microstructure is a reflective optical system, and the final substrate is currency or banknote paper. In this embodiment, the reflective optical system is cast against the TRA transfer film. It is suitable to form such a multi-layer microstructure directly onto the TRA transfer film that will be used to transfer the optics to the final substrate (rather than onto a flexible disposable manufacturing substrate followed by transferring onto the TRA transfer film). This is so because a reflective optical system operates with the reflector side against the final substrate and so is compatible and advantageous to use with this method.


To produce this reflective optical system, the following method may be used. A thin layer (e.g., 5 microns) of TRA is coated onto a 60 gauge film of PET and cured by application of UV light. Next, icons are formed as voids in a radiation cured liquid polymer (e.g., acrylated urethane) that is cast from an icon mold, then the icon voids are filled with a submicron particle pigmented coloring material by gravure-like doctor blading against the polymeric icon surface, then the fill is solidified by suitable means (e.g., solvent removal, radiation curing, or chemical reaction), then the reflective lens elements are cast against the filled icons by bringing the icon side of the film against a lens mold filled with radiation curable polymer, and the polymer is solidified by application of UV light or other actinic radiation. Next the lens elements are metalized (e.g., with aluminum) using a physical vapor deposition process, which is known in the art of holographic foil manufacture. Following metallization, an optional sealing layer may be applied to further protect the metal coating, followed by the application and drying of an adhesive, for example, a tack-free, heat-activated polyurethane foiling adhesive. Next, the entire structure (i.e., TRA transfer film with optical microstructure (icon layer/reflective lens elements/metal reflecting layer/sealing layer/adhesive layer)) may be converted into its final form by undergoing slitting and rewinding onto reels that are compatible with holographic foil transfer equipment. In this form, the micro-optic system may be transferred away from the TRA transfer film and onto the final substrate by the application of heat and pressure. For example, the structure may be brought into contact with currency or banknote paper while a foiling die applies pressure at 140° C. At this temperature, the foiling adhesive bonds the structure (by the side having reflector elements) to the final paper substrate, while the TRA provides the mechanism for release of the micro-optic system from the TRA transfer film. Then the desired final product (paper with surface applied reflective micro-optics) is rewound and the waste TRA transfer film is rewound and discarded or recycled.


In yet another exemplary embodiment, the microstructures are conductive circuit traces, and the final substrate is a glass substrate, which constitutes a subassembly of a touch screen display. In this embodiment, heat and pressure causes the conductive circuit traces to bond to the glass substrate, while releasing from the TRA transfer film. This process provides a means of producing the microstructure conductive circuit traces in high volume on a roll-to-roll basis, and subsequent delivery to an inflexible final substrate, resulting in an economically produced subassembly of a touch screen display.


In a further exemplary embodiment, the microstructure is in the form of a regular array of microstructured pre-ceramic polymers, and the final substrate is a quartz substrate, which forms a temperature sensing diffraction grating. In this embodiment, heat and pressure allows the ‘green cured’ array of pre-ceramic polymers (referring to a ceramic that is yet to be fired) to transfer away from the TRA transfer film and onto the quartz substrate. Next, the quartz and pre-ceramic are fired in a kiln at high temperatures (e.g., 1400-1600° C.), resulting in a sintered ceramic microstructure fused to a quartz substrate.


This process provides a means of producing a microstructured diffraction grating using ceramic precursors in high volume and at low temperatures on a roll-to-roll basis, and subsequent transfer to an inflexible final substrate. In this way, further processes incompatible with a flexible web can occur such as high temperature firing, resulting in the formation of a microstructured ceramic surface that can survive extremes in temperature exposure, but is produced using economical flexible web processes. In this example, the microstructured ceramic grating on quartz substrate finds use as a temperature monitor or a strain gauge. By reflecting a laser off of its surface and measuring the distance between the reflected bright zones (areas of constructive interference), highly accurate changes in groove spacing due to temperature or strain can be detected and calculated.


An alternative process for transferring microstructures to a final substrate will now be described. This alternative process provides improvements in overall system thickness, transfer speed, stability over time, and elimination of residue on the transferred microstructures.


The alternative process does not require the use of heat to initiate release of the microstructures from the carrier film (and thus is compatible with cold foiling methods), although it is still compatible and may be used with thermally activated adhesives. This process is also compatible with a cast spacer between focusing elements (e.g., lenses) and icons, and as such is not limited to the “spacer-less” structure shown in FIG. 1. Additionally, where the release layer(s) and binder layer(s) are ‘fully cured’ and stable, temperatures encountered during, for example, heated foiling, may facilitate removal of the carrier, but do so without leaving a residue on the microstructures.


As mentioned above, the alternative process for transferring microstructures employs:

    • 1) one or more release coatings, which are applied to (and conform to) an upper surface of the microstructures, and are cured; and
    • 2) one or more binder layers, which are cured in contact with the carrier film and the cured release coating(s) on the upper surface of the microstructures.


      Together, these layers serve to bind the microstructures firmly to the carrier film until a later time when it is desirable to transfer the microstructures to a final substrate such as currency paper and to discard the carrier film. Moreover, by employing a fully cured binder, temperature and pressure instability is avoided.


The one or more binder layers, in a preferred embodiment, are prepared from an energy curable (e.g., UV curable) binder formulation generally comprising:

    • (a) from about 0 to about 99.8% by wt. (preferably, from about 10 to about 50% by wt.) of an energy curable polyacrylate oligomer;
    • (b) from about 0 to about 99.8% by wt. (preferably, from about 20 to about 80% by wt.) of an energy curable acrylate monomer; and
    • (c) from about 0.2 to about 35% by wt. (preferably, from about 1 to about 12% by wt.) of a free radical photoinitiator.


      The binder formulation may be applied between the carrier film and microstructures (when still attached to the manufacturing substrate) during the continuous roll-to-roll process. The formulation is applied at thicknesses ranging from about 0.5 to about 25 microns (preferably, from about 2 to about 10 microns), and the layers bonded using, for example, a traditional wet lamination process where the two layers are brought together with uncured resin between the layers and then cured together. A relatively strong bond to the carrier film is realized such that release never occurs at the interface between the binder layer(s) and the carrier film. In a preferred embodiment, a carrier film having ‘print receptive’ surface treatment is used, while in another preferred embodiment, the surface energy of the carrier film is modified during production using, for example, corona or plasma pretreatment.


In a more preferred embodiment, the one or more binder layers are prepared from a formulation comprising:

    • (a) 40 wt. % of an energy curable polyacrylate oligomer sold under the trade designation CN293 by Sartomer;
    • (b) 60 wt. % of an energy curable acrylate monomer sold under the trade designation CD420 by Sartomer; and
    • (c) 4 wt. % of a liquid mixture of two photoinitiators sold under the trade designation OMNIRAD 1000 by IGM.


In order to prevent a permanent bond between the binder and microstructures (e.g., a microlens-based film structure), the microstructures are first treated with a ‘release’ formulation that has low bond strength (i.e., peel strength of less than 1 N/in (ASTM D903-98)). In this way, the cured binder bonds strongly to the carrier film and also bonds strongly to the cured release coating layer(s). This combination provides a bond which is strong under one set of conditions (favorable for removal of the manufacturing substrate) as well as a bond that is easily broken under another set of conditions (favorable for transfer of the microstructures to final substrate).


The one or more conformal release coating layers, in a preferred embodiment, are prepared from an energy curable (e.g., UV curable) formulation generally comprising:

    • (a) from about 1 to about 98 wt. % (preferably, from about 5 to about 20 wt. %) of isodecyl acrylate;
    • (b) from about 2 to about 50 wt. % (preferably, from about 10 to about 35 wt. %) of a free radical photoinitiator; and
    • (c) from about 0 to about 90 wt. % (preferably, from about 10 to about 80 wt. %) of 2-propanol (isopropyl alcohol).


      The formulation, which has been found to work over a range of dilutions with isopropyl alcohol, is applied by roll coating, or other suitable method for applying a fluid to a flexible substrate (e.g., flexo coating, anilox coating, gravure coating, metering rod (Meyer bar), curtain coating, rotary screen, silk screen, immersion, reverse roll, knife-over-roll, gap coating, or air knife) at thicknesses ranging from about 0.1 to about 10 microns, preferably, from about 0.5 to about 2 microns. The viscosity of the formulation ranges from about 2 to about 50 centipoise (cps) (preferably, from about 5 to about 15 cps), allowing the formulation to conform to the surface of the microstructures. The release coating layer(s), both before and after full cure, have a sufficiently low interfacial bond strength. In particular, the interfacial bond strength is low enough that when the microstructures are bonded to the final substrate by an adhesive and the carrier film is peeled away, separation will occur at the interface of the microstructures and the release coating layer(s). The ease of separation is controlled by the component properties of the release coating. For example, a monofunctional component such as isodecyl acrylate with a low glass transition temperature (Tg=−60° C.) will have a much lower bond strength than a higher functionality component such as trimethylolpropane ethoxy triacrylate (TMPEOTA) (Tg=37° C.), which has a larger number of reactive sites per polymer molecule. During hot or cold foiling operations, the necessary force for breaking this bond is supplied as tension when the carrier film is pulled away from the microstructures and rewound on a waste reel.


In a more preferred embodiment, the release formulation comprises:

    • (a) 10 wt. % of isodecyl acrylate;
    • (b) 30 wt. % of a liquid mixture of two photoinitiators sold under the trade designation OMNIRAD 1000 by IGM; and
    • (c) 60 wt. % of isopropyl alcohol.


The conditions that provide either a strong bond or weak bond using this construction are determined by the geometry of separation (i.e., by the angle at which the manufacturing substrate is peeled away relative to the carrier film). With a low angle of peel (i.e., obtuse angles greater than 90 to about 180°), the bond is high between the carrier and the microstructures, due to the distribution of force over a larger area (similar to the difficulty of separating two flat plates of glass with a layer of water between). With a high angle of peel (i.e., acute angles less than 90 to about 0°), the stress is concentrated to a smaller region, breaking bonds at the interface closest to the source of stress, allowing the manufacturing substrate to be removed without disrupting the bond between the microstructures and the carrier film. Once the manufacturing substrate has been removed and the adhesive applied, the microstructures may be applied to the final substrate such as paper on a commercial foiling unit (e.g., a Leonard Kurz MHS foiling machine), or passport booklet laminating machine. This equipment is designed to lift away carrier films to rewind and discard, and this lifting process easily breaks the bond between the microstructures and the film at the release coating interface.


Referring now to FIG. 1 in detail, a schematic flow diagram of one embodiment of this alternative process for transferring microstructures to a final substrate is shown generally at 10. The inventive process is a continuous roll-to-roll process that in this exemplary embodiment comprises:

    • forming the microstructures on a surface of a disposable manufacturing substrate (shown generally in process steps (A) and (B) in FIG. 1);
    • applying one or more release coating layers to a surface of the microstructures, the release coating layer(s) conforming to the microstructure surface, and then curing the release coating layer(s) (shown generally in process step (C) in FIG. 1);
    • applying one or more binder layers to a surface of a carrier film and optionally also to the cured release coated surface of the microstructures, and while these surfaces are in contact with each other, curing the binder layer(s) (shown generally in process step (D) in FIG. 1);
    • mechanically removing the disposable manufacturing substrate from the microstructures now bonded to the carrier film (shown generally in process step (E) in FIG. 1);
    • converting the bonded or laminated film structure using methods known in the art, including, but not limited to, applying other heat and/or pressure activated adhesives (e.g., tack-free, heat-activated adhesives), primers or coatings, to the film structure (shown generally in process step (F) in FIG. 1), followed by slitting or die cutting the structure to desired final dimensions (shown generally in process step (G) in FIG. 1), and sheeting the cut film into stacks or rewinding onto reels or spools, thereby forming a “transfer ready system”;
    • transferring the adhesive-coated microstructures to a final substrate by bringing the microstructures on the transfer ready system into contact with the final substrate (shown generally in process step (H) in FIG. 1) for thermal lamination, whereby heat and pressure are applied to the transfer ready system and then the carrier film is lifted from the microstructures causing separation between the microstructures and the release coating layer(s), thereby allowing transfer of the microstructures onto the surface of the final substrate, while simultaneously activating the adhesive on the microstructures, thereby allowing the microstructures to adhere to the surface of the final substrate; and
    • rewinding and discarding the carrier film (shown generally in process step (I) in FIG. 1), leaving the final substrate with newly affixed microstructures on its surface, ready for further processing or printing as desired.


As noted above, this alternative process provides improvements in overall system thickness and transfer speed. The binder layer(s) is cured between films allowing the binder to be rolled out to a very thin layer between the films, which reduces overall system caliper. This reduction in caliper translates into run speed improvements because the conductance of heat through the system is faster when there is less material acting as a thermal mass to slow down the melting of the adhesive.


Other features and advantages of the invention will be apparent to one of ordinary skill from the following detailed description and accompanying drawings. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. All publications, patent applications, patents and other references mentioned herein are incorporated by reference in their entirety. In case of conflict, the present specification, including definitions, will control. In addition, the materials, methods, and examples are illustrative only and not intended to be limiting.

Claims
  • 1. A process for transferring microstructures to a final substrate, the process comprising: subjecting a transfer film to a continuous roll-to-roll process, the continuous roll-to-roll process comprising: casting focusing microstructures on a surface of a disposable manufacturing substrate, wherein the focusing microstructures comprise voids in a substantially planar surface, or raised areas in a substantially planar surface;transferring the focusing microstructures from the disposable manufacturing substrate to a surface of a carrier film comprising an adhesive layer or a binder layer; andapplying heat and pressure to the carrier film to release the focusing microstructures from the carrier film; andtransferring the focusing microstructures from the transfer film onto a surface of the final substrate,wherein the focusing microstructures comprise refractive or reflective focusing microstructures.
  • 2. The process of claim 1, wherein the binder layer comprises one or more energy curable polyacrylates and a free radical photoinitiator.
  • 3. The process of claim 1, further comprising: prior to transferring the focusing microstructures to the carrier film, applying a release coating layer to a surface of the focusing microstructures, the release coating layer conforming to the surface of the focusing microstructures,curing the release coating layer,applying the binder layer to a surface of the carrier film, andwhile the surface of the carrier film and the surface of the focusing microstructures are in contact with each other, curing the binder layer.
  • 4. The process of claim 3, wherein the focusing microstructures are cast in a continuous process from a microstructured surface having a predesigned pattern onto the surface of the disposable manufacturing substrate, the predesigned pattern comprising a pattern of at least one of voids or raised areas.
  • 5. The process of claim 3, wherein the release coating layer comprises an isodecyl acrylate, a free radical photoinitiator, or an isopropyl alcohol.
  • 6. The process of claim 3, which further comprises: applying a heat activated adhesive or a pressure activated adhesive to coat the focusing microstructures on the carrier film;bringing the adhesive coated focusing microstructures on the carrier film into contact with a surface of the final substrate;lifting the carrier film from the focusing microstructures, causing separation between the focusing microstructures and the release coating layer, thereby allowing transfer of the focusing microstructures onto the surface of the final substrate; andsimultaneously activating the heat activated adhesive on the focusing microstructures, thereby allowing the focusing microstructures to adhere to the surface of the final substrate.
  • 7. The process of claim 3, further comprising, applying the binder layer to the cured release coating layer, the binder layer conforming to the surface of the focusing microstructures.
CROSS REFERENCE TO RELATED APPLICATION AND CLAIM OF PRIORITY

The present application claims priority under 35 U.S.C. § 120 as a divisional of U.S. patent application Ser. No. 14/421,394, filed Feb. 12, 2015, which claims priority under 35 U.S.C. § 365 and is a 371 National Stage of International Application No. PCT/US2012/051395, filed Aug. 17, 2012, the contents of which are herein incorporated by reference.

US Referenced Citations (292)
Number Name Date Kind
992151 Berthon May 1911 A
1824353 Jensen Sep 1931 A
1849036 Ernst Mar 1932 A
1942841 Shimizu Jan 1934 A
2268351 Tanaka Dec 1941 A
2355902 Berg Aug 1944 A
2432896 Hotchner Dec 1947 A
2888855 Tanaka Jun 1959 A
2992103 Land et al. Jul 1961 A
3122853 Koonz et al. Mar 1964 A
3241429 Rice et al. Mar 1966 A
3264164 Jerothe et al. Aug 1966 A
3312006 Rowland Apr 1967 A
3357772 Rowland Dec 1967 A
3357773 Rowland Dec 1967 A
3463581 Clay Aug 1969 A
3609035 Ataka Sep 1971 A
3643361 Eaves Feb 1972 A
3704068 Waly Nov 1972 A
3801183 Sevelin et al. Apr 1974 A
3811213 Eaves May 1974 A
3887742 Reinnagel Jun 1975 A
4025673 Reinnagel May 1977 A
4073650 Yevick Feb 1978 A
4082426 Brown Apr 1978 A
4185191 Stauffer Jan 1980 A
4345833 Siegmund Aug 1982 A
4417784 Knop et al. Nov 1983 A
4498736 Griffin Feb 1985 A
4507349 Fromson et al. Mar 1985 A
4519632 Parkinson et al. May 1985 A
4534398 Crane Aug 1985 A
4634220 Hockert et al. Jan 1987 A
4645301 Orensteen et al. Feb 1987 A
4662651 Mowry, Jr. May 1987 A
4688894 Hockert Aug 1987 A
4691993 Porter et al. Sep 1987 A
4756972 Kloosterboer et al. Jul 1988 A
4765656 Becker et al. Aug 1988 A
4814594 Drexler Mar 1989 A
4892336 Kaule et al. Jan 1990 A
4892385 Webster, Jr. et al. Jan 1990 A
4920039 Fotland et al. Apr 1990 A
4935335 Fotland Jun 1990 A
4988126 Heckenkamp et al. Jan 1991 A
5044707 Mallik Sep 1991 A
5074649 Hamanaka Dec 1991 A
5085514 Mallik et al. Feb 1992 A
5135262 Smith et al. Aug 1992 A
5142383 Mallik Aug 1992 A
5211424 Bliss May 1993 A
5215864 Laakmann Jun 1993 A
5232764 Oshima Aug 1993 A
5254390 Lu Oct 1993 A
5282650 Smith et al. Feb 1994 A
5359454 Steenblik et al. Oct 1994 A
5384861 Mattson et al. Jan 1995 A
5393099 D'Amato Feb 1995 A
5393590 Caspari Feb 1995 A
5413839 Chatwin et al. May 1995 A
5433807 Heckenkamp et al. Jul 1995 A
5438928 Chatwin et al. Aug 1995 A
5449200 Andric et al. Sep 1995 A
5460679 Abdel-Kader Oct 1995 A
5461495 Steenblik et al. Oct 1995 A
5464690 Boswell Nov 1995 A
5468540 Lu Nov 1995 A
5479507 Anderson Dec 1995 A
5492370 Chatwin et al. Feb 1996 A
5503902 Steenblik et al. Apr 1996 A
5538753 Antes et al. Jul 1996 A
5543942 Mizuguchi et al. Aug 1996 A
5555476 Suzuki et al. Sep 1996 A
5567276 Boehm et al. Oct 1996 A
5568313 Steenblik et al. Oct 1996 A
5574083 Brown et al. Nov 1996 A
5575507 Yamauchi et al. Nov 1996 A
5598281 Zimmerman et al. Jan 1997 A
5623347 Pizzanelli Apr 1997 A
5623368 Calderini et al. Apr 1997 A
5626969 Joson May 1997 A
5631039 Knight et al. May 1997 A
5639126 Dames et al. Jun 1997 A
5642226 Rosenthal Jun 1997 A
5643678 Boswell Jul 1997 A
5670003 Boswell Sep 1997 A
5670096 Lu Sep 1997 A
5674580 Boswell Oct 1997 A
5688587 Burchard et al. Nov 1997 A
5695346 Sekiguchi et al. Dec 1997 A
5712731 Drinkwater et al. Jan 1998 A
5723200 Oshima et al. Mar 1998 A
5731064 Süss Mar 1998 A
5737126 Lawandy Apr 1998 A
5753349 Boswell May 1998 A
5759683 Boswell Jun 1998 A
5763349 Zandona Jun 1998 A
5783017 Boswell Jul 1998 A
5783275 Mück et al. Jul 1998 A
5800907 Yumoto Sep 1998 A
5810957 Boswell Sep 1998 A
5812313 Johansen et al. Sep 1998 A
5886798 Staub et al. Mar 1999 A
5933276 Magee Aug 1999 A
5949420 Terlutter Sep 1999 A
5995638 Amidror et al. Nov 1999 A
6030691 Burchard et al. Feb 2000 A
6036230 Farber Mar 2000 A
6036233 Braun et al. Mar 2000 A
6060143 Tompkin et al. May 2000 A
6084713 Rosenthal Jul 2000 A
6089614 Howland et al. Jul 2000 A
6106950 Searle et al. Aug 2000 A
6176582 Grasnick Jan 2001 B1
6177953 Vachette et al. Jan 2001 B1
6179338 Bergmann et al. Jan 2001 B1
6195150 Silverbrook Feb 2001 B1
6249588 Amidror et al. Jun 2001 B1
6256149 Rolfe Jul 2001 B1
6256150 Rosenthal Jul 2001 B1
6283509 Braun et al. Sep 2001 B1
6288842 Florczak et al. Sep 2001 B1
6297911 Nishikawa et al. Oct 2001 B1
6301363 Mowry, Jr. Oct 2001 B1
6302989 Kaule Oct 2001 B1
6328342 Belousov et al. Dec 2001 B1
6329040 Oshima et al. Dec 2001 B1
6329987 Gottfried et al. Dec 2001 B1
6345104 Rhoads Feb 2002 B1
6348999 Summersgill et al. Feb 2002 B1
6350036 Hannington et al. Feb 2002 B1
6369947 Staub et al. Apr 2002 B1
6373965 Liang Apr 2002 B1
6381071 Dona et al. Apr 2002 B1
6404555 Nishikawa Jun 2002 B1
6405464 Gulick, Jr. et al. Jun 2002 B1
6414794 Rosenthal Jul 2002 B1
6424467 Goggins Jul 2002 B1
6433844 Li Aug 2002 B2
6450540 Kim Sep 2002 B1
6467810 Taylor et al. Oct 2002 B2
6473238 Daniell Oct 2002 B1
6483644 Gottfried et al. Nov 2002 B1
6500526 Hannington Dec 2002 B1
6521324 Debe Feb 2003 B1
6542646 Bar-Yona Apr 2003 B1
6558009 Hannington et al. May 2003 B2
6587276 Daniell Jul 2003 B2
6616803 Isherwood et al. Sep 2003 B1
6618201 Nishikawa et al. Sep 2003 B2
6641270 Hannington et al. Nov 2003 B2
6671095 Summersgill et al. Dec 2003 B2
6712399 Drinkwater et al. Mar 2004 B1
6721101 Daniell Apr 2004 B2
6724536 Magee Apr 2004 B2
6726858 Andrews Apr 2004 B2
6751024 Rosenthal Jun 2004 B1
6761377 Taylor et al. Jul 2004 B2
6795250 Johnson et al. Sep 2004 B2
6803088 Kaminsky et al. Oct 2004 B2
6819775 Amidror et al. Nov 2004 B2
6833960 Scarbrough et al. Dec 2004 B1
6856462 Scarbrough et al. Feb 2005 B1
6870681 Magee Mar 2005 B1
6900944 Tomczyk May 2005 B2
6935756 Sewall et al. Aug 2005 B2
7030997 Neureuther et al. Apr 2006 B2
7058202 Amidror Jun 2006 B2
7068434 Florczak et al. Jun 2006 B2
7114750 Alasia et al. Oct 2006 B1
7194105 Hersch et al. Mar 2007 B2
7246824 Hudson Jul 2007 B2
7254265 Naske et al. Aug 2007 B2
7255911 Lutz et al. Aug 2007 B2
7288320 Steenblik et al. Oct 2007 B2
7333268 Steenblik et al. Feb 2008 B2
7336422 Dunn et al. Feb 2008 B2
7372631 Ozawa May 2008 B2
7389939 Jones et al. Jun 2008 B2
7422781 Gosselin Sep 2008 B2
7457038 Dolgoff Nov 2008 B2
7457039 Raymond et al. Nov 2008 B2
7468842 Steenblik et al. Dec 2008 B2
7504147 Hannington Mar 2009 B2
7545567 Tomczyk Jun 2009 B2
7609450 Niemuth Oct 2009 B2
7630954 Adamczyk et al. Dec 2009 B2
7686187 Pottish et al. Mar 2010 B2
7712623 Wentz et al. May 2010 B2
7719733 Schilling et al. May 2010 B2
7738175 Steenblik et al. Jun 2010 B2
7751608 Hersch et al. Jul 2010 B2
7762591 Schilling et al. Jul 2010 B2
7763179 Levy et al. Jul 2010 B2
7812935 Cowbum et al. Oct 2010 B2
7820269 Staub et al. Oct 2010 B2
7830627 Commander et al. Nov 2010 B2
7849993 Finkenzeller et al. Dec 2010 B2
8027093 Commander et al. Sep 2011 B2
8057980 Dunn et al. Nov 2011 B2
8111463 Endle et al. Feb 2012 B2
8149511 Kaule et al. Apr 2012 B2
8241732 Hansen et al. Aug 2012 B2
8284492 Crane et al. Oct 2012 B2
8514492 Schilling et al. Aug 2013 B2
8528941 Dörfler et al. Sep 2013 B2
8537470 Endle et al. Sep 2013 B2
8557369 Hoffmüller et al. Oct 2013 B2
8693101 Tomczyk et al. Apr 2014 B2
8867134 Steenblik et al. Oct 2014 B2
8908276 Holmes Dec 2014 B2
20010048968 Cox et al. Dec 2001 A1
20020014967 Crane et al. Feb 2002 A1
20020114078 Halle et al. Aug 2002 A1
20020185857 Taylor et al. Dec 2002 A1
20030031861 Reiter et al. Feb 2003 A1
20030112523 Daniell Jun 2003 A1
20030157211 Tsunetomo et al. Aug 2003 A1
20030179364 Steenblik et al. Sep 2003 A1
20030183695 Labrec et al. Oct 2003 A1
20030228014 Alasia et al. Dec 2003 A1
20030232179 Steenblik et al. Dec 2003 A1
20030234294 Uchihiro et al. Dec 2003 A1
20040020086 Hudson Feb 2004 A1
20040022967 Lutz et al. Feb 2004 A1
20040065743 Doublet Apr 2004 A1
20040100707 Kay et al. May 2004 A1
20040140665 Scarborough et al. Jul 2004 A1
20040209049 Bak Oct 2004 A1
20050094274 Souparis May 2005 A1
20050104364 Keller et al. May 2005 A1
20050161501 Giering et al. Jul 2005 A1
20050180020 Steenblik et al. Aug 2005 A1
20050247794 Jones et al. Nov 2005 A1
20060003295 Hersch et al. Jan 2006 A1
20060011449 Knoll Jan 2006 A1
20060017979 Goggins Jan 2006 A1
20060018021 Tompkins et al. Jan 2006 A1
20060061267 Yamasaki Mar 2006 A1
20060227427 Dolgoff Oct 2006 A1
20070058260 Steenblik et al. Mar 2007 A1
20070092680 Chathns et al. Apr 2007 A1
20070164555 Mang et al. Jul 2007 A1
20070183045 Shilling et al. Aug 2007 A1
20070183047 Phillips et al. Aug 2007 A1
20070237938 Ouderkirk Oct 2007 A1
20070273143 Crane et al. Nov 2007 A1
20070284546 Ryzi et al. Dec 2007 A1
20070291362 Hill et al. Dec 2007 A1
20080130018 Steenblik et al. Jun 2008 A1
20080143095 Isherwood et al. Jun 2008 A1
20080160226 Kaule et al. Jul 2008 A1
20080182084 Tompkin et al. Jul 2008 A1
20090008923 Kaule et al. Jan 2009 A1
20090061159 Staub Mar 2009 A1
20090243278 Camus et al. Oct 2009 A1
20090290221 Hansen et al. Nov 2009 A1
20090310470 Yrjonen Dec 2009 A1
20090315316 Staub et al. Dec 2009 A1
20100001508 Tompkin et al. Jan 2010 A1
20100018644 Sacks et al. Jan 2010 A1
20100045024 Attner et al. Feb 2010 A1
20100068459 Wang et al. Mar 2010 A1
20100084851 Schilling Apr 2010 A1
20100109317 Huffmuller et al. May 2010 A1
20100177094 Kaule et al. Jul 2010 A1
20100182221 Kaule et al. Jul 2010 A1
20100194532 Kaule Aug 2010 A1
20100208036 Kaule Aug 2010 A1
20100308571 Steenblik et al. Dec 2010 A1
20100328922 Peters et al. Dec 2010 A1
20110017498 Lauffer et al. Jan 2011 A1
20110019283 Steenblik et al. Jan 2011 A1
20110056638 Rosset Mar 2011 A1
20110179631 Gates et al. Jul 2011 A1
20120019607 Dunn et al. Jan 2012 A1
20120033305 Moon et al. Feb 2012 A1
20120091703 Maguire et al. Apr 2012 A1
20120098249 Rahm et al. Apr 2012 A1
20120194916 Cape et al. Aug 2012 A1
20120243744 Camus et al. Sep 2012 A1
20130003354 Meis et al. Jan 2013 A1
20130010048 Dunn et al. Jan 2013 A1
20130038942 Holmes Feb 2013 A1
20130044362 Commander et al. Feb 2013 A1
20130154250 Dunn et al. Jun 2013 A1
20140174306 Wening et al. Jun 2014 A1
20140175785 Kaule et al. Jun 2014 A1
20140353959 Lochbihler Dec 2014 A1
20140367957 Jordan Dec 2014 A1
20160176221 Holmes Jun 2016 A1
20160257159 Attner et al. Sep 2016 A1
Foreign Referenced Citations (130)
Number Date Country
2009278275 Jul 2012 AU
2741298 Apr 2010 CA
1102865 May 1995 CN
1126970 Nov 2003 CN
1950570 Apr 2007 CN
101678664 Mar 2010 CN
19804858 Aug 1999 DE
19932240 Jan 2001 DE
10100692 Aug 2004 DE
0090130 Oct 1983 EP
0092691 Nov 1983 EP
0118222 Sep 1984 EP
0156460 Oct 1985 EP
0203752 Dec 1986 EP
0253089 Jan 1988 EP
0318717 Jun 1989 EP
0415230 Mar 1991 EP
0319157 Jul 1992 EP
0801324 Oct 1997 EP
0887699 Dec 1998 EP
0930174 Jul 1999 EP
0997750 May 2000 EP
1002640 May 2000 EP
1356952 Oct 2003 EP
1002640 May 2004 EP
1354925 Apr 2006 EP
1659449 May 2006 EP
1743778 Jan 2007 EP
1876028 Jan 2008 EP
1897700 Mar 2008 EP
1931827 Apr 2009 EP
2335937 Jun 2011 EP
2338682 Jun 2011 EP
2162294 Mar 2012 EP
2803939 Jul 2001 FR
2952194 May 2011 FR
1095286 Dec 1967 GB
2103669 Feb 1983 GB
2362493 Nov 2001 GB
2395724 Jun 2004 GB
2433470 Jun 2007 GB
2490780 Nov 2012 GB
41-004953 Mar 1966 JP
46-022600 Aug 1971 JP
04-234699 Aug 1992 JP
H05-508119 Nov 1993 JP
10-035083 Feb 1998 JP
10-039108 Feb 1998 JP
11-501590 Feb 1999 JP
11-189000 Jul 1999 JP
2000-056103 Feb 2000 JP
2000-233563 Aug 2000 JP
2000-256994 Sep 2000 JP
2001-055000 Feb 2001 JP
2001-516899 Oct 2001 JP
2001-324949 Nov 2001 JP
2003-039583 Feb 2003 JP
2003-165289 Jun 2003 JP
2003-528349 Sep 2003 JP
2003-326876 Nov 2003 JP
2004-262144 Sep 2004 JP
2004-317636 Nov 2004 JP
2005-193501 Jul 2005 JP
2009-274293 Nov 2009 JP
2011-502811 Jan 2011 JP
10-0194536 Jun 1999 KR
2002170350000 Mar 2001 KR
2003119050000 May 2003 KR
1005443000000 Jan 2006 KR
1005613210000 Mar 2006 KR
2111125 May 1998 RU
2245566 Jan 2005 RU
2010101854 Jul 2011 RU
575740 Feb 2004 TW
WO 2011051669 May 2011 WF
WO 1992008998 May 1992 WO
WO 1992019994 Nov 1992 WO
WO 1993024332 Dec 1993 WO
WO 1996035971 Nov 1996 WO
WO 1997019820 Jun 1997 WO
WO 1997044769 Nov 1997 WO
WO 1998013211 Apr 1998 WO
WO 1998015418 Apr 1998 WO
WO 1998026373 Jun 1998 WO
WO 1999014725 Mar 1999 WO
WO 1999023513 May 1999 WO
WO 1999026793 Jun 1999 WO
WO 1999066356 Dec 1999 WO
WO 2001007268 Feb 2001 WO
WO 2001011591 Feb 2001 WO
WO 2001039138 May 2001 WO
WO 2001053113 Jul 2001 WO
WO 2001063341 Aug 2001 WO
WO 2001071410 Sep 2001 WO
WO 2002040291 May 2002 WO
WO 2002043012 May 2002 WO
WO 2002101669 Dec 2002 WO
WO 2003005075 Jan 2003 WO
WO 2003007276 Jan 2003 WO
WO 2003022598 Mar 2003 WO
WO 2003053713 Jul 2003 WO
WO 2003061980 Jul 2003 WO
WO 2003061983 Jul 2003 WO
WO 2003082598 Oct 2003 WO
WO 2003098188 Nov 2003 WO
WO 2004022355 Mar 2004 WO
WO 2004036507 Apr 2004 WO
WO 2004087430 Oct 2004 WO
WO 2005106601 Nov 2005 WO
WO 2006029744 Mar 2006 WO
WO 2007076952 Jul 2007 WO
WO 2007133613 Nov 2007 WO
WO 2009000527 Dec 2008 WO
WO 2009000528 Dec 2008 WO
WO 2009000529 Dec 2008 WO
WO 2009000530 Dec 2008 WO
WO 2009121784 Oct 2009 WO
WO 2010015383 Feb 2010 WO
WO 2010094691 Dec 2010 WO
WO 2010136339 Dec 2010 WO
WO 2011015384 Feb 2011 WO
WO 2011019912 Feb 2011 WO
WO 2011044704 Apr 2011 WO
WO 2011107793 Sep 2011 WO
WO 2011122943 Oct 2011 WO
WO 2012027779 Mar 2012 WO
WO 2012103441 Aug 2012 WO
WO 2013028534 Feb 2013 WO
WO 2013093848 Jun 2013 WO
WO 2013098513 Jul 2013 WO
Non-Patent Literature Citations (35)
Entry
Egyptian Patent Office, “Technical Report,” Application No. EG2015020243, Feb. 12, 2019, 7 pages.
Office Action dated Dec. 20, 2018 in connection with Korean Patent Application No. 10-2015-7006374, 4 pages.
Article: “Spherical Lenses” (Jan. 18, 2009); pp. 1-12; retrieved from the Internet: URL:http://www.physicsinsights.org/simple_optics_spherical_lenses-1.html.
Drinkwater, K. John, et al., “Development and applications of Diffractive Optical Security Devices for Banknotes and High Value Documents”, Optical Security and Counterteit Deterrence Techniques III, 2000, pp. 66-79, SPIE vol. 3973, San Jose, CA.
Fletcher, D.A., et al., “Near-field infrared imaging with a microfabricated solid immersion lens”, Applied Physics Letters, Oct. 2, 2000, pp. 2109-2111, vol. 77, No. 14.
Gale, M. T., et al., Chapter 6—Replication, Micro Optics: Elements, Systems and Applications, 1997, pp. 153-177.
Hardwick, Bruce and Ghioghiu Ana, “Guardian Substrate as an Optical Medium for Security Devices”, Optical Security and Counterfeit Deterrence Techniques III, 2000, pp. 176-179, SPIE vol. 3973, San Jose, CA.
Hutley, M.C., et al., “The Moiré Magnifier”, Pure Appl. Opt. 3, 1994, pp. 133-142, IOP Publishing Ltd., UK.
Hutley, M.C., “Integral Photography, Superlenses and the Moiré Magnifier”, European Optical Society, 1993, pp. 72-75, vol. 2, UK.
Hutley, M., et al., “Microlens Arrays”, Physics World, Jul. 1991, pp. 27-32.
Kamal, H., et al., “Properties of Moiré Magnifiers”, Opt. Eng., Nov. 1998, pp. 3007-3014, vol. 37, No. 11.
Leech, Patrick W., et al., Printing via hot embossing of optically variable images in thermoplastic acrylic lacquer, Microelectronic Engineering, 2006, pp. 1961-1965, vol. 83, No. 10, Elsevier Publishers BV, Amsterdam, NL.
Lippmann, G., “Photgraphie—Épreuves Réversibles, Photographies Intégrals”, Académie des Sciences, 1908, pp. 446-451, vol. 146, Paris.
Liu, S., et al., “Artistic Effects and Application of Moiré Patterns in Security Holograms”, Applied Optics, Aug. 1995, pp. 4700-4702, vol. 34, No. 22.
Phillips, Roger W., et al., Security Enhancement of Holograms with Interference Coatings, Optical Security and Counterfeit Deterrence Techniques III, 2000, pp. 304-316, SPIE vol. 3973, San Jose, CA.
Steenblik, Richard A., et al., Unison Micro-optic Security Film, Optical Security and Counterfeit Deterrence Techniques V, 2004, pp. 321-327, SPIE vol. 5310, San Jose, CA.
Van Renesse, Rudolf L., Optical Document Security, 1994, Artech House Inc., Norwood, MA.
Van Renesse, Rudolf L., Optical Document Security, 1998, 2nd edition, pp. 232-235, 240-241 and 320-321, Artech House Inc., Norwood, MA (ISBN 0-89006-982-4).
Van Renesse, Rudolf L., Optical Document Security, 2005, 3rd edition, pp. 62-169, Artech House Inc., Norwood, MA (ISBN 1-58053-258-6).
Wolpert, Gary R., Design and development of an effective optical variable device based security system incorporating additional synergistic security technologies, Optical Security and Counterfeit Deterrence Techniques III, 2000, pp. 55-61, SPIE vol. 3973, San Jose, CA.
Zhang, X., et al., “Concealed Holographic Coding for Security Applications by Using a Moire Technique”, Applied Optics, Nov. 1997, pp. 8096-8097, vol. 36, No. 31.
Office Action dated Sep. 10, 2018 in connection with Australian Application No. AU2017235929, 3 pages.
Amidror, “A Generalized Fourier-Based Method for the Analysis of 2D Moiré Envelope-Forms in Screen Superpositions”, Journal of Modern Optics (London, GB), vol. 41, No. 9, Sep. 1, 1994, pp. 1837-1862, ISSN: 0950-0340.
Dunn, et al., “Three-Dimensional Virtual Images for Security Applications”, Optical Security and Counterfeit Deterrence Techniques V, (published Jun. 3, 2004), pp. 328-336, Proc. SPIE 5310.
Muke, “Embossing of Optical Document Security Devices”, Optical Security and Counterfeit Deterrence Techniques V, (published Jun. 3, 2004), pp. 341-349, Proc. SPIE 5310.
Intellectual Property India, “Examination report under sections 12 & 13 of the Patents Act, 1970 and the Patents Rules, 2003,” Application No. IN 1934/DELNP/2015, dated Jul. 29, 2019, 6 pages.
IMPI Mexican Institute Industrial Property, “Notification of 1st in-depth requirement,” Application No. MX/a/2015/002072, dated May 8, 2019, 8 pages.
IP Australia, “Examination report No. 2 for standard patent application,” Application No. AU2017235929, dated Aug. 14, 2019, 3 pages.
IP Australia, “Examination report No. 3 for standard patent application,” Application No. AU2017235929, dated Sep. 10, 2019, 3 pages.
Canadian Intellectual Property Office, Office Action in connection with Application No. CA 2,881,826, dated Oct. 3, 2019, 4 pages.
Brazil Instituto Nacionalda Propriedade Industrial, Office Action in connection with Application No. BR112015003455-1, dated Oct. 11, 2019, 5 pages.
European Patent Office, “Communication pursuant to Article 94(3) EPC,” Application No. EP12766740.0, dated Sep. 23, 2019, 4 pages.
Office Action in connection with Mexican Application No. MX/a/2015/002072 dated Dec. 17, 2019, 6 pages.
Examination report No. 1 in connection with Australian Application No. 2019229332 dated Sep. 12, 2020, 4 pages.
Examination report No. 2 in connection with Australian Application No. 2019229332 dated Oct. 6, 2020, 4 pages.
Related Publications (1)
Number Date Country
20190105887 A1 Apr 2019 US
Divisions (1)
Number Date Country
Parent 14421394 US
Child 16198952 US