Patent Document

BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     This invention relates to a method of applying an electric conductive layer to selected portions of a mounting frame or foam mount, and to the foam mount, and more particularly, to applying the electric conductive layer to inner surface of one side of the foam mount, and applying a non-electric conductive layer to inner surface of opposite side of the foam mount. 
     2. Discussion of the Technical Problem 
     At the present time there is a desire to provide electronic shielding around the body of commercial aircrafts such that electronic signals to and from electronic equipment of the passengers, e.g. cell phones and computers within the commercial aircraft, are only transmitted by and received through the antenna of the aircraft. One of the advantages of this arrangement is the elimination of uncontrolled transmission of signals through the windows of the aircraft, which transmitted signals can interfere with transmitted signals required to operate the aircraft. As is appreciated by those skilled in the art, to attain this goal it becomes necessary to prevent transmission of the signals through the cabin windows and through the door windows of the aircraft. 
     In one approach to accomplish this goal, a window pane having an electric conductive layer is mounted in a foam mount having an electric conductive layer. The window pane can be an electro-chromic window, or one or more glass sheets having an electric conductive layer or film over the major surface of one or more of the sheets. More particularly and as is known in the art, the electro chromic window includes an electro chromic medium between two spaced electrodes. Each of the electrodes include an electric conductive layer or film on a major surface of a glass sheet. The electric conductive layer or film provides a radio frequency (“RF”) shielding. 
     The outboard surface of the foam mount has an electric conductive layer, e.g. an RF shielding layer or coating. The inboard surface of the foam mount is coated with a non-electrical conductive decorative paint to compliment the decor of the aircraft interior. The foam mount having the window pane is positioned in the window opening of the aircraft between an outboard structural ply and an inboard protective overlay sheet. The conductive layer on the foam mount is electrically connected with the aircraft wall to connect the electric conductive layer of the foam mount to the electric ground of the aircraft. With this arrangement, the electric conductive layers of the electro-chromic window and the electric conductive layer of the foam mount provide an RF shielding over the window opening in the body of the aircraft. 
     As is appreciated by those skilled in the art, applying two different layers, or coatings on a foam mount can be time consuming and labor intensive. It would be advantages, therefore, to provide a method of coating selected portions of a foam mount with an electric conductive layer, and other selected portions of the foam mount with a non-electric conductive decorative layer that minimizes the time and the labor to apply the two layers to a foam mount. 
     SUMMARY OF THE INVENTION 
     This invention relates to a method of applying an electric conductive layer to selected portions of a foam mount; the foam mount in a shape having an enclosed frame surrounding an open area. The frame in cross section includes, among other things, a peripheral surface; an inner surface opposite to the peripheral surface, the inner surface defining the open area; a first side extending from the peripheral surface to first portion of the inner surface, and an opposite second side extending from the peripheral surface to second portion of the inner surface, wherein the inner surface of the foam mount includes open end of a groove facing the open area of the foam mount and the first portion is on one side of the open end of the groove and the second portion is on the other side of the open end of the groove. The method includes, among other things, applying a first electric conductive coating over inner surfaces of the groove; inserting peripheral edge of a substrate in the groove to completely cover the open area of the foam mount to separate the foam mount into a first section and a second section. The first section includes the first side of the foam mount and a portion of the inner surface connected to the first side defined as a first portion, and the second half includes the second side of the foam mount, and a portion of the inner surface connected to the second side defined as a second portion. A second electric conductive coating is applied over the first section, wherein the coating on the first section and the coating on the inner surface of the groove contact one another, and a non-electric conductive coating is applied over the second section of the foam mount. 
     Further, this invention relates to a method of making an RF shielded window by, among other things, providing a foam mount in a shape having an enclosed frame surrounding an open area, the frame in cross section having, among other things, a peripheral surface; an inner surface opposite to the peripheral surface, the inner surface defining the open area; a first side extending from the peripheral surface to first portion of the inner surface, and an opposite second side extending from the peripheral surface to second portion of the inner surface, wherein the inner surface of the foam mount includes open end of a groove facing the open area of the foam mount, and the first portion is on one side of the open end of the groove and the second portion is on the other side of the open end of the groove. A transparency having an electric conductive layer over a major surface of the transparency is shaped and sized to fit within the groove of the foam mount and completely cover the open area of the foam mount. A substrate having a peripheral shape and a thickness similar to peripheral shape and thickness of the transparency is provided. A first electric conductive coating is applied over inner surfaces of the groove, afterward, peripheral edge of the substrate is inserted in the groove to completely cover the open area of the foam mount and to separate the foam mount into a first section and a second section. The first section includes the first side and a portion the inner surface connected to the first side defined as a first portion, and the second half includes the second side, and a portion of the inner surface connected to the second side defined as a second portion. A second electric conductive coating is applied over the first section, wherein the second coating on the first section of the foam mount and the first coating on the inner surfaces of the groove contact one another. A non-electric conductive coating is applied over the second section of the foam mount. The substrate is removed from the foam mount, and the transparency is placed in the groove of the foam mount. 
     Still further, this invention relates to an aircraft window mounted in a foam mount made by the above methods. 
     In addition, this invention relates to a coating mask including, among other things, a base; a wall mounted on the base and extending upward from the base; a first shim mounted on the base between perimeter of the base and the upright wall; a second shim mounted on the base between the perimeter of the base and the wall, the first and the second shims spaced from on another, and a cover mounted to the first shim to move in a first direction to a closed position, wherein the cover in the closed position is over the base and on the second shim, and to move the cover in an opposite second direction to an open position to expose surface of the base within the wall. The cover has an opening, which is sized such that when the cover is in the closed position, the cover overlays the wall and the base within the wall is viewed. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWING 
         FIG. 1  is a fragmented side view of an aircraft showing outboard view of a cabin window. 
         FIG. 2 . Is a view taken along lines  2 - 2  of  FIG. 1 . 
         FIG. 3  is a cross sectional view of the foam mount shown in  FIG. 2 . 
         FIG. 4  is a plan elevated top view of a blank used in the practice of the invention to prevent coating overlap. 
         FIG. 5  is a prospective view of a mask in the open position; the mask can be used in the practice of the invention to prevent coating overlap. 
         FIG. 6 . Is a view similar to the view of  FIG. 5  showing a foam mount positioned on the base of the mask. 
         FIG. 7  is a view similar to the view of  FIG. 6  showing the mask in the closed position. 
         FIG. 8  is a fragmented side view of one non-limited embodiment of a mask cover on one side of the foam mount in accordance to the teachings of the invention. 
         FIG. 9  is a view similar to the view of  FIG. 8  showing another non-limited embodiment of a mask cover on the other side of the foam mount in accordance to the teachings of the invention. 
     
    
    
     DESCRIPTION OF THE INVENTION 
     As used herein, spatial or directional terms, such as “inner”, “outer”, “left”, “right”, “up”, “down”, “horizontal”, “vertical”, and the like, relate to the invention as it is shown in the drawing figures. However, it is to be understood that the invention can assume various alternative orientations and, accordingly, such terms are not to be considered as limiting. Further, all numbers expressing dimensions, physical characteristics, and so forth, used in the specification and claims are to be understood as being modified in all instances by the term “about”. Accordingly, unless indicated to the contrary, the numerical values set forth in the following specification and claims can vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques. Moreover, all ranges disclosed herein are to be understood to encompass any and all subranges subsumed therein. For example, a stated range of “1 to 10” should be considered to include any and all subranges between (and inclusive of) the minimum value of 1 and the maximum value of 10; that is, all subranges beginning with a minimum value of 1 or more and ending with a maximum value of 10 or less, e.g., 1 to 6.7, or 3.2 to 8.1, or 5.5 to 10. Also, as used herein, the terms “sprayed over”, “applied over”, or “provided over” mean sprayed, applied, or provided on but not necessarily in surface contact with. For example, a material “applied over” a substrate does not preclude the presence of one or more other materials of the same or different composition located between the deposited material and the substrate. 
     Before discussing non-limiting embodiments of the invention, it is understood that the invention is not limited in its application to the details of the particular non-limiting embodiments shown and discussed herein since the invention is capable of other embodiments. Further, the terminology used herein to discuss the invention is for the purpose of description and is not of limitation. Still further, unless indicated otherwise in the following discussion, like numbers refer to like elements. 
     Non-limiting embodiments of the invention will be directed to the practice of the invention to make a cabin window of an aircraft; the invention, however, is not limited to any particular type of aircraft cabin window, and the invention contemplates the practice of the invention on door windows of an aircraft. Further, the invention can be practiced on windows for commercial and residential buildings, e.g. but not limited to type disclosed in U.S. Pat. No. 5,675,944, which patent in its entirety is hereby incorporated by reference; on a window for any type of vehicle; e.g. air and space vehicles, and above or below water vessels, and on a window for a viewing side or door for any type of containers, for example but not limited to a refrigerator, cabinet and/or oven door. 
     With reference to  FIGS. 1 and 2  as needed, a section  20  of an aircraft  22  has a cabin window  24 . The cabin window  24  (see  FIG. 2 ) includes a frame mount  26 , which includes features of the invention and is coated according to the invention. In the preferred practice of the invention the frame mount  26  is made of foam and will hereinafter also be referred to as “frame mount” or “foam mount.” A pane  28 , e.g. an electro-chromic window  28  is mounted in a groove  30  of the foam mount  26 . The electro-chromic window  28  includes an electro-chromic medium  31  between a pair of electrodes  32  and  33 . Each of the electrodes  32  and  33  includes an electric conductive layer or film  34  on inner surface  35  of a glass sheet  36 . The marginal edges  37  of the sheets  36  of the electrodes  32  and  33  are sealed to provide a sealed cell  38  having the electro-chromic medium  31 . Outer surface  39  of the glass sheet  36  of the electrode  32  faces the exterior of the aircraft  22 , and outer surface  40  of the glass sheet  36  of the electrode  33  faces the interior of the aircraft  22 . Electro-chromic windows are well known in the art and no further discussion of the construction of the electro-chromic window  24  is deemed necessary. 
     The electro conductive film  34  of the electrodes  32  and  33  provides an RF shielding to prevent transmission of electric signals through the pane  28 . The inboard inner surface  41  of the foam mount  26  faces the interior of the aircraft  22 , and outboard inner surface  42  of the foam mount  26  faces the exterior of the aircraft  22 . An inboard protective overlay sheet  43  is between inboard side  44  of the foam mount  26  and interior window frame  46 , and a structural ply  48  is between outboard side  50  of the foam mount  26  and body  52  of the aircraft  22 . Optionally a gasket  54  is provided between outboard surface  56  of the structural ply  48  and the body  52  of the aircraft  22  to minimize, if not eliminate, the ingress of moisture between the aircraft body  52  and the structural ply  48 . 
     The invention is not limited to the manner in which, or the components used, to securely mount the cabin window  24  in the aircraft body  52 , and any of the techniques or fasteners, e.g. bolts, nuts, screws, clips and latches known in the art can be used in the practice of the invention to secure the cabin window  24  to the aircraft body. As is appreciated by those skilled in the art, the manner of using the fasteners, and the type of fasteners used, to secure the cabin window to the aircraft body  52  is dictated by the designer and/or builder of the aircraft and is therefore not limiting to the invention. Further, the invention contemplates unitizing the components of the cabin window, e.g. the structural ply  48 , the foam mount  26  having the pane  28 , and the inboard protective layer  24 , and securing the unitized cabin window in the aircraft body  52 , and thereafter securing the inboard window frame  46  to the aircraft body. The invention also contemplates individually mounting and securing the components of the cabin window  24  in the aircraft body  52 , e.g. securing the structural ply  56  and gasket  54 , if used, in position; securing the frame mount  26  having the pane  28  in position against the structural ply  48 , and securing the inboard protective sheet  42  in position against the frame mount  26 , and thereafter, securing the inboard window frame  46  to the aircraft body. 
     The structural ply  48  is not limited to the invention and can be a single glass or plastic sheet, or a pair of glass and plastic sheets, and combinations thereof laminated together by a interlayer material as is known in the art, e.g. as described in U.S. Patent Application Publication 2007/0002422A1. When the sheets are made of glass, the glass is preferably chemically tempered, heat tempered or heat strengthen. The materials of the sheets and the number of sheets of the structural ply  48  is not limiting to the invention. 
     The inboard protective overly sheet  43  is not limiting to the invention and can be any of the types used in the art, e.g. a plastic sheet to protect the underlying pane  28  from surface scratches caused by passenger curiosity, cleaning solutions, and/or abrasive cleaning materials. 
     In the preferred practice of the invention, the pane  28  is an electro chromic device or window  28  having the medium  31  changing percent of light transmission as a function of changes in voltage applied to the medium. The invention is not limited to the construction of the electro chromic window and any of the types known in the art, e.g. U.S. Pat. Nos. 5,215,821, 6,471,360 and 6,783,099 and U.S. Patent Application Publication 2007/0002422A1 can be used in the practice of the invention. The invention also contemplates the pane  28  being a photo chromic device having a pair of glass sheets spaced from one another and a medium between the sheets that changes percent of light transmission as a function of light intensity on the medium. The invention is not limited to the construction of the photo chromic window and any of the types known in the art, e.g. U.S. Pat. Nos. 4,720,350, 5,973,039 and 7,393,101 can be used in the practice of the invention. The invention further contemplates the pane  28  being a glass or plastic sheet, or one or more glass or plastic sheets or combinations thereof, laminated together or spaced from one another by a spacer frame, e.g. of the type disclosed in U.S. Pat. No. 5,675,944. The above mentioned documents are hereby incorporated by reference. 
     As can now be appreciated by those skilled in the art, the invention contemplates the window  28  having an electric conductive layer or film on at least one of the major surfaces of the window to act as an RF shielding. For example and not limiting to the invention, in the instance when the window  28  is a photo chromic window, an electric conductive layer or film is provided on the outer surface of a sheet, or the inner surface of a sheet, e.g. the surface  35  of the glass sheet  36  of the electrode  32  and/or  33 . 
     In another non-limiting embodiment of the invention, the pane  28  includes a substrate, e.g. a glass or plastic sheet having an electrically conductive layer or film over a major surface of the substrate. The electric conductive layer or film, e.g. the electric conductive layer  34  of the electrodes  32  and  33  of the pane  28  (see  FIG. 2 ) provides a barrier to the transmission of electronic signals, e.g. but not limited to signals received and transmitted by electronic equipment, e.g. but not limited to cell phones and wireless computers. The invention is not limited to the conductive layer  36 , and the layer can be any of the types known in the art. Non-limiting embodiments of conductive coatings that can be used in the practice of the invention include, but are not limited to, a pyrolytic deposited fluorine doped tin oxide film of the type sold by PPG Industries, Inc. under the registered trademark NESA®; a magnetron sputter deposited tin doped indium oxide film of the type sold by PPG Industries, Inc under the registered trademark NESATRON®; a coating made up of one or more magnetron sputter deposited films, the films including, but not limited to a metal film, e.g. silver between metal oxide films (dielectric films), e.g. zinc oxide and/or zinc stannate, each of which may be applied sequentially by magnetron sputtering, e.g. as disclosed in U.S. Pat. Nos. 4,610,771; 4,806,220 and 5,821,001, the disclosures of which are hereby incorporated by reference. 
     The foam mount  26  can be made of any material that is compressible, flexible and is electrically non-conductive. The material is preferably compressible and flexible so that the pane  28  can be mounted in the groove  30  of the foam mount  26 . The foam mount  26  is electrically non-conductive in order that only selected surface portions of the foam mount can be made electrically conductive by an application of an electrically conductive coating. More particularly and with reference to  FIGS. 2 and 3  as needed, in one non-limiting embodiment of the invention, an electrically conductive layer or coating  60  is applied or provided over inner walls  61  of the groove  30 , the outboard side  50 , and the outboard inner surface  42  of the foam mount  26 , and a decorative coating  62 , preferably a non-electric conductive coating, is applied or provided over the inboard inner surface  41  of the foam mount  26 . Outer peripheral surface  64  of the foam mount  26  is not intentionally covered with either the conductive coating  62 , or with the decorative coating  62 , because the outer surface  64  of the foam mount  26  is not visible when viewing through the cabin window and not coating the surface  64  realizes a reduction in the cost of the coatings; however, overspray or over paint onto the outer surface  64  of the foam mount is acceptable. In one non-limiting embodiment of the invention, the invention was practiced on Zote Foam mounts made by Technifab, Inc having an office in Avon, Ohio. 
     In the practice of the invention, the foam mount  26  is coated with the electric conductive layers  60  and  61  to prevent electronic signals from moving through the foam mount. The inboard inner surface  38  of the foam mount is painted with a decorative paint for aesthetic reasons. With reference to  FIG. 3 , interface  63  is the end of the conductive layer  61  and the beginning of the decorative coating  62 . As is appreciated, the invention is not limited to the location of the interface  63 , however, the conductive layers  60  and  61  and the conductive layer of the pane  28  should provide an RF shielding without any gaps or separations between the conductive layers  60  and  61  of the foam mount and conductive layer of the pane  28 . Further, as is appreciated, the invention is not limited to the types of paint used in the practice of the invention. In one non-limiting embodiment of the invention, the electrically conductive coating  60  was 102-32/B507 Silver RF paint of the type sold by Creative Materials, and the decorative coating  62  was 1050 HF BAC70913 topcoat sold by HSH Interplan, Inc. 
     In one non-limiting embodiment of the invention, the foam mount was painted in the manner described in PROCESS A. 
     PROCESS A 
     1. HSH Interplan, inc. EED non-crazed cleaner for composites was applied to the inner walls  61  of the groove  30  of the foam mount  26  with a lint free Kimberly-Clark WypAII L30 wipe followed by a stream of low pressure compressed air to remove lint and foreign particles from the groove  30 ; 
     2. 102-32/B507 Silver RF paint (hereinafter also referred to as “Silver RF paint”) was prepared per directions provided by the manufacturer of the Silver RF paint; 
     3. A paint stick or a swab was used to apply a layer  60  of the Silver RF paint to the inner walls  61  of the groove  30  of the foam mount  26  (see  FIG. 3 ). Care was exercised not to apply any of the Silver RF paint to the inboard inner surface  41  of the foam mount  26 . 
     4. The layer  60  of the Silver RF paint applied over the inner walls  61  of the groove  30  was cured per instructions provided by the manufacturer of the Silver RF paint. 
     5. After the curing of the layer  60  of the Silver RF paint on the walls of the groove, a blank  70  (see  FIG. 4 ) having a shape similar to the shape of the pane  28  to be mounted in the groove  30  was provided. In one non-limited embodiment of the invention, the blank was a cardboard blank, however, the invention is not limited thereto, and the blank can be made of any material, e.g. but not limited to wood, metal, glass or plastic. The thickness of the blank  70  is not limiting to the invention, and the thickness is preferably 80-90% of the thickness of the pane  28  to be mounted in the groove  30  of the foam mount  26  for the reason discussed below. As mentioned above, the blank  70  has a shape similar to the shape of the pane  28 , however, in this non-limiting embodiment of the invention, the shape of the blank is 5-10% smaller than the shape of the pane  28  to be mounted in the groove  30 . By providing a blank  70  that is thinner and smaller than the pane  28  to be mounted in the groove  30 , the groove  30  of the foam mount  26  is not excessively flexed when the blank  70  was inserted in the groove  30  to partition the inboard inner surface  36 , from the outboard inner surface  38 , of the foam mount  26  to prevent coating overlap. 
     6. The layer  60  of the Silver RF paint was sprayed onto the outboard inner surface  42 , and the outboard side  50 , of the foam mount  26  (see  FIG. 3 ). Care was taken not to spay the outer surface  64  of the foam mount, however, overspray of the Silver RF paint onto the outer surface  64  was noted. In this non-limiting embodiment of the invention, overspray of the Silver RF paint onto the outer surface  64  is acceptable. 
     7. The layer  60  of the Silver RF paint on the outboard inner surface  42 , and the outboard side  50 , of the foam mount  26  was cured per directions provided by the manufacturer of the Silver RF paint. The blank  70  remained in the groove  30  of the foam mount during the curing of the Silver RF paint. 
     8. After the curing of the layer  60  of the Silver RF paint on the outboard inner surface  40 , and the outboard side  50 , of the foam mount  26  was completed, the inboard inner surface  41  of the foam mount  26  was cleaned using HSH Interplan, Inc. EED cleaner. Thereafter, HSH Interplan, Inc 1025 primer/sealer was painted on the inboard inner surface  41  of the foam mount  26 . The sealer was cured in one of the following manners: heated at 95° Fahrenheit for 15 minutes or cured at room temperature for one hour. After the sealer was cured, the layer  62  of the decorative paint was sprayed over the sealer. Care was taken not to spay the sealer or the decorative paint on the outer surface  64  of the foam mount  26 , however, overspray of the sealer and the decorative paint onto the outer surface  64  was noted. In this non-limiting embodiment of the invention, overspray of the sealer and the decorative paint onto the outer surface  64  of the foam mount  26  is acceptable. 
     9. The layer  62  of the decorative paint on the inboard inner surface  41  of the foam mount  26  was cured per directions provided by the manufacturer of the decorative paint. 
     The term “overspray” as used herein is defined as a coating or layer having a decreasing thickness as the distance from the coating area increases. In the practice of the invention, the overspray of the Silver RF paint has a thickness that decreases as the distance from the intersection of the outboard side  50 , and the outer surface  64 , of the foam mount  26  increases (see  FIG. 3 ), and the overspray of the Silver RF paint terminates short of the intersection of the inboard side  44 , and the outer surface  64 , of the foam mount  26 . The overspray of the decorative paint  62  has a thickness that decreases as the distance from the intersection of the inboard side  44 , and the outer surface  64 , of the foam mount  26  increases (see  FIG. 3 ), and the overspray of the decorative paint terminates short of the intersection of the outboard side  50 , and the outer surface  64 , of the foam mount  26 . Further, the overspray of the decorative paint and the overspray of Silver RF paint preferably do not overlap. 
     After the layers or coatings applied to the foam mount were cured or dried, the blank  70  was removed and the electro chromic window  28  was mounted in the groove  30  of the foam mount  26 . The conductive layer  60  on the foam mount  26  is electrically connected with the aircraft wall to connect the electric conductive layer of the foam mount to the electric ground of the aircraft. With this arrangement, the electric conductive layers of the window  28  and the electric conductive layer  60  of the foam mount  26  provide an RF shielding over the window opening in the body of the aircraft. Covering the walls  61  of the groove  30  of the foam mount assures that there is no break in the RF shield provided by the electrodes  32  and  33  of the pane  28  and the electric conductive layer  60  of the foam mount  26 . With reference to  FIG. 2 , wires  72  (see  FIG. 2 ) contacting the electrodes  32  and  33  of the pane  28  and wire  74  contacting the Silver RF paint  60  were arranged in groove  76  (see  FIGS. 2 and 3 ) in the outboard side  50  of the foam mount  26  to meet at tab  78  formed on outer surface  64  of the foam mount  26 . The wires were provided with connectors (not shown) to connect to the electro chromic window  28  and the layer  60  of the Silver RF paint to the electrical system of the aircraft  22 . 
     As can now be appreciated, the practice of PROCESS A does not provide for the prevention of overspray onto the outer surface  64 , and the inboard side  44 , of the foam mount  26  (see  FIG. 3 ). The invention contemplates preventing the painting or covering the outer surface  64 , and/or the inboard side  44 , of the foam mount  26  with the electric conductive layer  60  and the decorative paint layer  62 , respectively. In one non-limiting embodiment of the invention, the decorative paint and the electrically conductive paint are applied with a paint brush or with a paint roller to prevent the covering of the outer surface  64 , and the inboard side  44 , of the foam mount  26 . In another non-limiting embodiment of the invention, the foam mount  26  is positioned in a mask designed to prevent or minimize the covering of the outer surface  64 , and/or the inboard side  44 , of the foam mount  26  with the conductive paint and the decorative paint, respectively. 
     With reference to  FIG. 5 , there is shown a non-limiting embodiment of a mask  90  of the invention to prevent or minimize the covering of the outer surface  64 , and/or the inboard side  44 , of the foam mount  26  with the conductive paint and/or the decorative paint, respectively. The coating mask  90  includes a base  92  having a plurality of spaced upright pins  94  secured on the base  92  in any convenient manner, and positioned on the base  92  to contain the foam mount  26  as shown in  FIG. 6  and to prevent sideway motion of the foam mount  26  without compressing the outer surface  64  of the foam mount. The height of the pins  94  as measured from surface  96  of the base  92  of the mask  90  is equal to, or slightly greater, e.g. greater than 0 to 10% greater than the thickness of the foam mount  26  as measured between the outboard side  50  and the inboard side  44  (see  FIG. 3 ) to avoid compression of the foam mount  26  when the mask cover  98  is positioned over the foam mount  26  and engages the pins  94 . As can be appreciated, as the percent difference between the height of the pins  92  and the thickness of the foam mount  26  increases, the greater the probably of over spray of the conductive paint and the decorative paint passing through the space between the mask cover  98  and the foam mount  26 , and depositing over the outside surface  64 , and/or the inboard side  44 , of the foam mount  26 . 
     With continued reference to  FIG. 5 , the base (hereinafter also referred to as the “mask base”)  92  includes support plates  100  and  102 . A shim  104  is secured to the support plate  100  in any convenient manner, e.g. by screws or welding. One plate  106  of a hinge  108  is secured to side  110  of the shim  104 , and the other plate  112  of the hinge  108  is secured to outer surface  113  of the mask cover  98  at hinge support  114  (clearly shown in  FIG. 7 ) so that inner surface  116  of the mask cover  98  and the surface  96  of the mask base  92  can be pivoted toward and away from one another to position the inner surface  116  of the mask cover  98  on the pins  94  (the mask cover  98  in the closed position as shown in  FIG. 7 ), and to move the inner surface  116  of the mask cover  98  away from the pins  94  toward the open position (mask cover  98  shown in the open position in  FIGS. 5 and 6 ). Preferably, but not limiting to the invention, the thickness of the shim  104  as measured between the inner surface  116  of the mask cover  98  and the surface  96  of the mask base  92  is equal to the height of the pins  94 . As is appreciated, the invention contemplates a solid endless or continuous wall in place of the pins  94 . A piece of the sold continuous wall  119  is shown only in  FIG. 5  and shown only in phantom. 
     With reference to  FIG. 8 , in one non-limiting embodiment of the invention, one mask cover  98 A is provided with a cut out center portion  120  sized such that with the mask  90  in the closed position, the inner surface  116  of the mask cover  98 A overlays the inboard side  44  of the foam mount  26 . With reference to  FIG. 9 , in the non-limiting embodiment of the invention under discussion, another mask cover  98 B is provided with a cut out center portion  120  sized such that with the mask  90  in the closed position, the inner surface  116  of the mask cover  98 B overlays the outboard side  50  of the foam mount  26  adjacent the intersection of the outboard side  50 , and the outer surface  64 , of the foam mount  26  as shown in  FIG. 9 . As can be appreciated, when the cut out portions  120  are the same size, one size mask cover  98  can be used in the practice of the invention. 
     With reference to  FIGS. 5-7  as needed, the mask cover  98  further includes a fastener support  120  that is aligned with the support  102  of the base  92  when the mask cover  98  is in the closed position (see  FIG. 7 ). The mask cover  98  is preferably maintained in the closed position when the masks  90  are moved into and out of the cure chamber (not shown). The invention is not limited to the type of fastener  122  used in the practice of the invention to maintain the mask in the closed position. In one non-limiting embodiment of the invention, the fastener was a magnetic fastener  122  having magnetic bar  124  secured to the support plate  102  of the base  92  of the mask  90 , and a magnetic bar  126  secured to fastener support  120  of the mask cover  98 . The positive side of the magnetic bar  124  faces the magnetic bar  126 , and the negative surface of the magnetic bar  126  faces the magnetic bar  124 . The magnetic bars are secured to their respective support in any convenient manner, e.g. by screws  128  (see  FIGS. 6 and 7 ). The thickness of the magnetic bars  124  and  126  as measured between the surface  96  of the mask base  92  and the inner surface  116  of the mask cover is equal to the thickness of the shim  104 , or the height of the pins  94 . 
     In another non-limiting embodiment of the invention, the mask  90  was used to apply the conductive layer  60  and the decorative layer  62  to selected portions of the foam mount  26  in the manner described in PROCESS B. 
     PROCESS B 
     A. Steps 1-5 of PROCESS A were practiced. 
     B. The foam mount  26  having the blank  70  was placed within the pins  94  of the mask  90  (see  FIG. 6 ) with the inboard side  44  of the foam mount  26  on the surface  96  of the base  92  of the mask  90 . The mask cover  98 B was positioned in the closed position such that the mask cover  98 B overlaid a portion of the outboard side  50  of the foam mount  26  adjacent the intersection of the outboard side  50 , and the outer surface  64 , of the foam mount  26  (see  FIG. 9 ). 
     C. The layer  60  of the Silver RF paint was sprayed onto the outboard inner surface  42 , and the uncovered portion of the outboard side  50  of the foam mount  26  (see  FIG. 9 ). 
     D. Step  7  of PROCESS A was practiced. 
     E. The inboard inner surface  41  of the foam mount  26  was cleaned as described in Step 8 of PROCESS A above. 
     F. The foam mount  26  having the blank  70  was placed within the pins  94  of the mask  90  (see  FIG. 6 ) with the outboard side  50  of the foam mount  26  on the surface  96  of the base  92  of the mask  90 . The mask cover  98 A was positioned in the closed position such that the mask cover  98 A overlaid the inboard side  44  of the foam mount  26  (see  FIG. 8 ). 
     G. The sealer identified in Step 8 of PROCESS A was applied over the inboard inner surface  38  of the foam mount  26  and cured according to Step 8 of Process A. 
     H. After the sealer was cured, the layer  62  of the decorative paint was sprayed over the sealer to apply the decorative paint over the inboard inner surface  38  of the foam mount  26 . 
     I. Step 9 of PROCESS A was practiced. 
     The mask cover  98 A prevented overspray of the sealer and decorative coating  62  over the outer surface  64 , and the outer surface  64 , of the foam mount  26 , and the mask cover  98 B prevented overspray of the conductive coating  60  over the outer surface  64  of the foam mount  26 . As is appreciate the invention is not limited to the sequence in which the inboard surfaces  44  and  50  of the foam mount  26  are painted. 
     After the groove  30 , the inner surfaces  41  and  42 , and the outboard side  50 , of the foam mount  28  are covered, and the conductive paint and the decorative paint have cured, the blank  70  was removed and the electro chromic window  29  having the conductive layer  36  was mounted in the groove  30  of the foam mount  26  as discussed above. 
     It is readily appreciated by those skilled in the art that modifications can be made to the non-limiting embodiments of the invention without departing from the concepts disclosed in the foregoing description. It is understood that various changes can be made without departing from the spirit of the invention as defined by the claimed subject matter which follows.

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