Classifications

• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B5/00—Optical elements other than lenses
  • G02B5/08—Mirrors
  • G02B5/0808—Mirrors having a single reflecting layer
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
  • B29C37/0025—Applying surface layers, e.g. coatings, decorative layers, printed layers, to articles during shaping, e.g. in-mould printing
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
  • B29D11/00—Producing optical elements, e.g. lenses or prisms
  • B29D11/00596—Mirrors
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B5/00—Optical elements other than lenses
  • G02B5/08—Mirrors
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B5/00—Optical elements other than lenses
  • G02B5/08—Mirrors
  • G02B5/10—Mirrors with curved faces
• • G—PHYSICS
  • G02—OPTICS
  • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
  • G02B5/00—Optical elements other than lenses
  • G02B5/20—Filters
  • G02B5/26—Reflecting filters

Definitions

• This invention relates to reflective mirrors and fab ⁇ rication methods therefore, and more particularly to mir- rors with a composite resin structure and a precipitated reflective coating.
• Mirrors are conventionally formed from glass or plas- tic coated with a reflective surface. Another technique involves stretching a thin film of aluminized mylar over the opening of a pressurized chamber. In this practice, a partial vacuum or positive pressure is used to shape the aluminized mylar surface to the desired contour. All three types of mirrors can be quite expensive when large dimen ⁇ sions and/or a high quality surface are required.
• Glass mirrors require lengthy grinding and polishing to obtain a high quality surface; this is not only time- consuming but also difficult when aspheric curved shapes are required, such as for parabolic reflectors. Glass mir ⁇ rors are quite fragile, and accidents during handling, in ⁇ stallation and maintenance cause major economic losses. Also, when it is desired to edge-butt a number of mirrors together to form a larger overall reflective surface, the edges of the glass segments are very susceptible to chip ⁇ ping. This results either in noticeable gaps between adja- cent segments, or the necessity to stagger or inset and overlap adjacent segments; both of these approaches are visually distracting. For complicated surface geometries, very expensive specialized grinding and polishing equipment that is not widely available is required. In addition, glass mirrors are relatively heavy for a given reflective area.
• the thermal forming of a plastic sheet involves heating and stretching the sheet over a non-optical quality forming tool and then glu ⁇ ing a ribbed support structure onto its opposite side to provide rigidity.
• the surface of the stretched sheet must next be extensively ground and polished.
• the plastic mir ⁇ ror surface is not particularly durable, which can result in a limited lifetime for this type of mirror. Further ⁇ more, since the thermal forming process is not consistently uniform over the full mirror surface, producing a curved plastic mirror without grinding and polishing has not been technically or economically successful to date. Vacuum formed aluminized mylar requires an active pump, sensor and servo system to maintain the proper shape. The surface of this film is much less durable than either glass or plastic mirrors.
• the process for forming reflective mirror coatings also has significant limitations.
• Conventional coating processes require vacuum chambers and the use of special protective overcoats that are also generally vacuum depos ⁇ ited over the metallized surface to prevent oxidation, tar ⁇ nishing or damage during cleaning.
• the present invention seeks to provide a new mirror structure and related fabrication method that allows for the rapid replication of high quality mirrors of any de ⁇ sired shape, with a large reduction in processing time and cost compared to existing fabrication techniques.
• the in ⁇ vention also seeks to provide an efficient method for ap- plying a reflective coating to the new mirror structure.
• a new type of mirror that has a composite resin structure and is fabricated on a shaped forming tool.
• the forming tool has an optical quality surface, and a shape that is complimentary to the desired mirror shape.
• a mold release agent is applied to the tool surface, followed by a mirror resin coating which assumes the shape and optical quality of the tool surface.
• a rigid composite backing is formed over it.
• the composite backing together with the mirror resin coating are then removed as an integral unit from the forming tool, and a reflective metallic coating is applied and protected with a clear lacquer. At most only a minor amount of polishing of the resin surface prior to applying the metal coating will allow the metallic surface to basically replicate the optical quality of the original tool surface.
• the formation of the reflective coating can also be inte- grated into the mirror fabrication while still on the tool. This is accomplished by first applying a transparent pre ⁇ liminary resin coating over the mold release agent on the tool, forming a metallized reflective coating on the pre ⁇ liminary resin coating, and then completing the composite mirror with the mirror resin coating and composite backing as described above.
• the transparent preliminary resin coating protects the metallic surface after the mirror has been removed from the tool.
• the metallic coating is preferably formed with a pro- cess that is similar to the Brashear glass silvering pro ⁇ cess described above.
• the microporous surface of the resin is first thoroughly degreased and cleaned, preferably with a cerum oxide solution followed by a diluted nitric acid cleansing. This allows the stannous chloride to enter the resin pores and act as a bonding agent for the metal.
• a cotton pile that does not scratch the optical quality resin surface is preferably employed for the degreaser and stannous chlo- ride.
• the result contrary to expectations, is that the metal coating successfully adheres to the mirror's resin surface.
• This metallization technique is particularly use ⁇ ful for large mirrors, but can also be used for smaller mirrors in lieu of the conventional vacuum metallization coating process.
• FIG. 1 is a sectional view, not to scale, of a compos ⁇ ite mirror as fabricated on a forming tool in accordance with the invention
• FIG. 2 is a sectional view, not to scale, showing the mirror or FIG. 1 after it has been removed from the forming tool;
• FIGs. 3a-3f are fragmentary respective views, not to scale, showing successive steps in the formation of a re ⁇ flective metallic coating on a composite resin mirror sur ⁇ face, in accordance with the invention.
• FIG. 4 is a sectional view, not to scale, showing the integrated fabrication of a composite mirror along with a metallic reflective coating and protective resin coat on a forming tool.
• the present invention uses a forming tool that has an optical quality surface and a shape that is complimentary to the desired mirror shape to provide the mirror geometry and surface quality. Mirrors can then be quickly and inexpensively replicated from a common forming tool.
• a forming tool is indicated by reference number 2 in FIG. 1.
• Its outer surface 4 has a spherical convex shape that is used to form mirrors with a complimentary spherical concave shape.
• Other mirror shapes can also be provided with an appropriate forming tool surface, includ ⁇ ing flat, elliptical and other aspherical geometries.
• the tool 2 can be fabricated by establishing a concave cutout in a block of metal to the desired tool shape, heat ⁇ ing a mass of glass within the cutout so that it assumes the cutout shape, mounting the glass to a rigid framework, and then grinding and polishing its outer surface to an optical quality.
• optical quality is generally understood as referring to a surface that, when supporting a metallized reflective coating, reflects incident light with little or no noticeable defects.
• a conventional mold release agent 6 is first applied to the forming tool's optical quality surface, followed by a layer of gel coat resin ma ⁇ terial 8.
• the resin is preferably a vinylester because of its dimensional stability resulting from its low coeffi ⁇ cient of thermal expansion as it cures, but other di en- sionally stable resin materials could also be used.
• the resin layer 8 is applied in a conventional manner at room temperature, and allowed to cure and outgas.
• the mold re- lease agent 4 prevents the resin from sticking to the tool.
• a resinous gel coat layer 10, preferably vinylester, is then applied over the lower resin layer 8 to add stiff ⁇ ness and rigidity.
• a veil which is a fine weave cloth commonly used in the fiber glass indus- try, to hold the resin at the surface adjacent the forming tool; the veil does not print through to the resin surface adjacent the tool that will eventually provide the mirror surface.
• Layer 8 is typically about 2-10mm thick, and the total thickness of layers 8 and 10 is typically about 10- 20mm.
• the gel coat layer 10 is followed by a layer of resin and chopped random fiber mat 12, typically about 30-40mm thick.
• a vacuum formed closed cell foam 14 is sandwiched between the layer 12 and an outer resin/chopped random fi- ber mat layer 16; the foam layer 14 is typically about 1cm thick or more, while the outer resin/chopped random fiber mat layer 16 is generally about 3 mm thick or greater.
• the combination of the three layers 12, 14 and 16 provides a light weight structure with high rigidity, the basic con- cept of which is well known in the field of composites.
• the gel coat 10 prevents the pattern of the random fiber mat in layer 12 from printing through to the first resin layer 8.
• each of the resin layers 8, 10, 12 and 16 is allowed to cure and outgas upon application to the composite struc ⁇ ture.
• the com ⁇ posite mirror structure 18 is lifted off the forming tool 2, as illustrated in FIG. 2.
• the exposed surface 20 of the first resin layer 8 either has the de- sired degree of optical quality as replicated from the tool surface 4, or can acquire the desired optical quality with only a small amount of polishing, similar to compounding the painted finish on an automobile.
• the resin layer 8 is typically not reflective enough to serve as a mirror surface. A metallized reflective sur ⁇ face is therefore applied over resin layer 8 at this point.
• the metal deposition is performed so that the metal surface essentially replicates the optical quality of the surface of resin layer 8.
• the metal layer can be added with a con- ventional vacuum deposition process. However, particularly for larger mirrors, a unique process that is particularly suited for a resinous surface is preferably employed.
• the new process for applying a metal coating is illus ⁇ trated in FIGs. 3a-3f. It incorporates the Brashear pro- cess described above that is used for glass silvering, but modifies it with a preliminary treatment that has been found to cause the metal to adhere to the resinous sub ⁇ strate without scratching or damaging the optical surface of the resin part. Without this preliminary treatment, the metal would not adhere and could be easily removed, as when the Brashear process is attempted on a plastic surface.
• the outer surface 20 of the resin coating 8 has a i- croporous characteristic, with an array of micropores 22 in the surface.
• the first step of the metallization process is to thoroughly degrease and clean the resin surface 20. This is preferably accomplished with a degreasing agent such as cerum oxide that is dissolved in a liquid solution so that no abrasive particles are present to scratch the optical surface of the composite mirror.
• a degreasing agent such as cerum oxide that is dissolved in a liquid solution so that no abrasive particles are present to scratch the optical surface of the composite mirror.
• the solution is applied with a non-abrasive material such as a cotton pile, which may be a common cotton ball, rubbed onto the resin surface in a swirling manner.
• the solution should not be rubbed on too hard, so as to avoid scratches that are visi- ble after the metallization has been applied.
• the resin surface is rinsed with distilled water, cleansed with a diluted nitric acid and then thoroughly rinsed again with distilled water.
• the de ⁇ greasing, cleansing and rinsing steps are then preferably repeated to assure a properly prepared surface.
• the cleansing and rinsing of the resin surface is indicated by arrows 26 in FIG. 3b.
• a metal coating can be added with a conventional Brashear process.
• a solution of a bonding agent 28 (FIG. 3c) , preferably stannous chloride, is first sprayed onto the surface of the resin coating 8, which is then rinsed with distilled water. When the surface is properly de- greased and cleaned, the stannous chloride enters the mi- cropores and bonds to the resin surface.
• a twin noz ⁇ zle is used to spray silver suspended in a solution 30 onto the surface.
• the solution typically consists of distilled water, nitric acid, alcohol and silver nitrate.
• the silver precipitates from the solution (as indicated by arrows 32) and establishes a silver coating 34 on the stannous chlo ⁇ ride film.
• the surface is then rinsed again with distilled water, and any residual moisture is blown off with filtered com- pressed air, as indicated by arrows 36 in FIG. 3e.
• the remaining silver layer 34 at this point will generally rep ⁇ licate the optical quality surface of the resin layer 8, which in turn is a complimentary replication of the forming tool's surface.
• a thin protective coating of clear lacquer 38 (FIG. 3f) is then sprayed on over the silver layer and allowed to dry. At this point the mirror is completed.
• FIG. 4 An alternate fabrication technique, in which the pro ⁇ vision of metallic and protective coatings are integrated into the composite layup process, is illustrated in FIG. 4.
• a substan ⁇ tially transparent gel coat resin layer 40 is applied over the mold release agent 6 and allowed to cure and outgas.
• a reflective metal layer 42 is then formed over the trans ⁇ parent resin layer 40, either by vacuum deposition or with the new technique described above in connection with FIGs. 3a-3f.
• the remainder of the composite structure is then fabricated over the metal layer 42.
• the inner surface of the reflective metal layer 42 replicates the optical quali ⁇ ty of the forming tool via the transparent resin layer 40, while the resin layer 40 provides a protective coating for the mirror in lieu of a lacquer coat.
• the new composite mirror structure is particu ⁇ larly useful for large mirrors, it offers significant cost and weight advantages for smaller mirrors also.
• Applica- tions for the new mirror structure include architectural decorative exterior mirrors, design and large floor-to- ceiling mirrors for building interiors, side and rear view mirrors for automobiles, trucks and buses, flat light ⁇ weight mirrors for simulator visual optical systems, and high optical quality laser reflectors and visible light reflectors used in the electronics industry.
• the coated surface of the composite mirror is many times more durable than the coated surface of a stretched mylar mirror, and less brittle than a glass mirror.
• the shape and optical quality of the composite mirror surface are very accurate and repeatable (to better than 0.25mm), and the mirror is not subject to the problem of localized differences in ma- ' terial stretch that is inherent with stretched mylar mir ⁇ rors.

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• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Optics & Photonics (AREA)
• Engineering & Computer Science (AREA)
• Health & Medical Sciences (AREA)
• Manufacturing & Machinery (AREA)
• Ophthalmology & Optometry (AREA)
• Mechanical Engineering (AREA)
• Optical Elements Other Than Lenses (AREA)

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• 1994
  • 1994-07-08 EP EP94923467A patent/EP0659281A1/de not_active Withdrawn
  • 1994-07-08 WO PCT/US1994/007883 patent/WO1995002199A1/en not_active Application Discontinuation

Non-Patent Citations (1)

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