US20030066256A1 - Hurricane door light - Google Patents
Hurricane door light Download PDFInfo
- Publication number
- US20030066256A1 US20030066256A1 US09/974,264 US97426401A US2003066256A1 US 20030066256 A1 US20030066256 A1 US 20030066256A1 US 97426401 A US97426401 A US 97426401A US 2003066256 A1 US2003066256 A1 US 2003066256A1
- Authority
- US
- United States
- Prior art keywords
- frame
- film
- window assembly
- assembly
- panel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000011521 glass Substances 0.000 claims abstract description 25
- 230000002787 reinforcement Effects 0.000 claims description 27
- 239000000853 adhesive Substances 0.000 claims description 12
- 230000001070 adhesive effect Effects 0.000 claims description 12
- 238000010276 construction Methods 0.000 claims description 11
- 125000006850 spacer group Chemical group 0.000 claims description 6
- -1 polyethylene terephthalate Polymers 0.000 claims description 4
- 229920000139 polyethylene terephthalate Polymers 0.000 claims description 4
- 239000005020 polyethylene terephthalate Substances 0.000 claims description 4
- 239000005357 flat glass Substances 0.000 claims 1
- 230000035515 penetration Effects 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 description 8
- 239000004033 plastic Substances 0.000 description 4
- 229920003023 plastic Polymers 0.000 description 4
- 239000004793 Polystyrene Substances 0.000 description 3
- 239000005340 laminated glass Substances 0.000 description 3
- 229920002223 polystyrene Polymers 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000005336 safety glass Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
- B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
- B32B17/10009—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets
- B32B17/10036—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising two outer glass sheets
- B32B17/10045—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising two outer glass sheets with at least one intermediate layer consisting of a glass sheet
- B32B17/10055—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising two outer glass sheets with at least one intermediate layer consisting of a glass sheet with at least one intermediate air space
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
- B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
- B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
- B32B17/10009—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets
- B32B17/10036—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising two outer glass sheets
- B32B17/10045—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing characterized by the number, the constitution or treatment of glass sheets comprising two outer glass sheets with at least one intermediate layer consisting of a glass sheet
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/06—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
- B32B17/10—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
- B32B17/10005—Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
- B32B17/10165—Functional features of the laminated safety glass or glazing
- B32B17/10293—Edge features, e.g. inserts or holes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2367/00—Polyesters, e.g. PET, i.e. polyethylene terephthalate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1407—Doors; surrounding frames
- B64C1/1469—Doors between cockpit and cabin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0021—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems means for restricting access to flight deck
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
- E06B3/54—Fixing of glass panes or like plates
- E06B3/58—Fixing of glass panes or like plates by means of borders, cleats, or the like
- E06B3/5892—Fixing of window panes in openings in door leaves
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B5/00—Doors, windows, or like closures for special purposes; Border constructions therefor
- E06B5/10—Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes
- E06B5/12—Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes against air pressure, explosion, or gas
Definitions
- the present invention relates to windows and more particularly to impact-resistant and pressure-resistant windows.
- Exterior building windows are part of the “building envelope” comprising the exterior of the building. As part of the building envelope, exterior windows are subjected to a variety of weather extremes.
- An increasing number of building code standards and regulations have been, and continue to be, developed for such windows.
- many building codes include strenuous impact standards, which require a window to withstand impacts similar to those of a missile driven by high winds, as in a hurricane or a tornado. These building codes may also require the windows to withstand a variety of extreme cyclical pressure changes.
- an insulated glass (IG) assembly includes a flexible impact-resistant sheet incorporated into the laminated glass, extending beyond the laminated glass, and secured between the frame and the structure to which it is mounted (e.g. a door or a building).
- the frame is injection molded of plastic and is reinforced with high-strength inserts extending between the frame and the glass.
- the window unit is extremely strong and is believed to meet all current building code requirements. Further, the window unit is relatively simple and inexpensive.
- FIG. 1 is a perspective view of the doorlight of the present invention mounted within a door
- FIG. 2 is a fragmentary exploded sectional view taken along line 2 - 2 in FIG. 1;
- FIG. 3 is a fragmentary assembled sectional view taken along line 2 - 2 in FIG. 1;
- FIG. 4 is a perspective view of the window in an aircraft
- FIG. 5 is a sectional view taken along line 5 - 5 in FIG. 4;
- FIG. 6 is a fragmentary cross sectional view similar to FIG. 3 showing a first alternative embodiment of the invention.
- FIG. 7 is a fragmentary cross sectional view similar to FIG. 3 showing a second alternative embodiment of the invention.
- FIGS. 1 - 3 a doorlight constructed in accordance with a preferred embodiment of the invention is illustrated in FIGS. 1 - 3 and generally designated 10 .
- the doorlight 10 includes an IG assembly 16 and a frame assembly 8 .
- the frame assembly 8 supports the IG assembly 16 within a door 100 or other supporting structure.
- the IG assembly 16 in turn includes a laminated assembly 28 , a first glass panel 26 and a spacer frame 29 . If a non-insulated construction is desired, both the spacer frame 29 and the first glass panel 26 may be eliminated.
- the laminated assembly 28 includes a second glass panel 24 , a third glass panel 22 and a flexible impact resistant film 20 .
- the glass panels 24 and 22 forming the laminated assembly 28 include a perimeter edge 122 .
- the second glass panel 24 and the third glass panel 22 are laminated to the opposite sides of the film 20 using techniques well known to those skilled in the art.
- the film 20 includes a peripheral margin portion 21 that extends beyond the glass panels 22 and 24 in all directions. Alternatively, the film 20 could extend beyond the panels only in selected areas.
- the first, second and third glass panels 26 , 24 , and 22 are 1 ⁇ 8 inch tempered safety glass that meets ANSI Z97.1 and U.S. C.P.S.C. 16 CFR 1201 CI and CII.
- the film 20 is 7 mil thick polyethylene terephthalate (P.E.T.), although other thicknesses and/or materials may be readily used.
- the film 20 is flexible, although it may be semi-rigid depending on the thickness.
- the spacer frame 29 holds the laminated assembly 28 and the first glass panel 26 apart in an insulated construction. The fabrication of the spacer frame 29 and its attachment to the glass panels are well known to those skilled in the art.
- the frame assembly 8 includes an inner frame half 12 , an outer frame half 14 , and a reinforcement frame insert 18 .
- the frame halves are generally well known to those skilled in the art of doorlights and windows.
- the inner frame half 12 and the outer frame half 14 are fabricated of a high-performance UV-stable plastic or an injection-molded polystyrene.
- the inner frame half 12 and the outer frame half 14 are fastened together with a first fastening means for interconnecting the frame halves, such as screws 41 to secure the IG assembly 16 within the supporting structure 100 .
- the inner frame half 12 includes a door-engagement flange 30 , an IG-assembly-engagement flange 32 and a main-body portion 34 .
- the door-engagement flange 30 extends from the main-body portion 34 to the door 100 or support structure, and defines a first recess 76 .
- the first recess 76 allows the second fastening means 70 , discussed below, to be hidden from sight.
- the first recess 76 also receives a structural adhesive 38 a to seal the door-engagement flange 30 to the door 100 .
- the IG-engagement flange 32 extends from the main-body portion 34 to contact the IG assembly 16 .
- the IG-engagement flange 32 defines a groove 40 extending along the length of the inner frame half 12 for receiving a structural adhesive 38 b.
- the main-body portion 34 is located between the IG-engagement flange 32 and the door-engagement flange 30 .
- the main-body portion 34 includes a plurality of screw bosses spaced about the inner frame half 12 . Each screw boss 60 extends and defines a hole 42 through which a screw (not shown) passes.
- the outer frame half 14 is somewhat of a mirror image of the inner frame half 12 .
- the outer frame half 14 includes a door-engagement flange 46 , a window-engagement flange 48 and a main-body portion 50 .
- the door-engagement flange 46 defines a groove 52 in which a traditional gasket material 80 a is placed.
- the window-engagement flange 48 defines a groove 54 in which a traditional gasket material 80 b is placed. These grooves 52 and 54 extend around the perimeter of the entire outer frame 14 .
- the main body portion 50 also includes a plurality of screw bosses 62 to receive the screws 41 . One boss 62 is aligned with each boss 60 when the frame halves are aligned with one another.
- the reinforcement frame 18 (FIGS. 2 and 3) is uniform in cross section throughout its length and includes a secured leg 64 , a supporting leg 66 and a U-shaped channel 68 .
- the channel 68 connects the supporting leg 66 and the secured leg 64 .
- the secured leg 68 contacts the door or other supporting structure 100
- the supporting leg 66 contacts the IG assembly 16 .
- the channel 68 includes a plurality of holes 88 to allow the screws (not shown) to pass through.
- the screws 70 secure the secured leg 68 to the door 100 .
- the reinforcement frame 18 is 24 gauge steel, but may be any suitable thickness or material. To reduce materials, costs, and disposal issues, the reinforcement frame 18 can be made out of the skin of the door 100 .
- the reinforcement frame 18 is located under the interior frame half 12 and on top of the supporting structure 100 and the IG assembly 16 .
- the present invention is adopted for installation within an opening of a supporting structure 100 , such as a door.
- the IG assembly 10 may come in various sizes and shapes to fit within nearly any opening.
- the glass panels 22 , 24 and 26 are cut to the desired dimension and shape.
- the glass panels 22 and 24 are laminated to the film 20 forming the laminated assembly 28 .
- the margin portion 21 of the film extends beyond the glass in all directions.
- the film 20 may be trimmed if necessary.
- the laminated assembly 28 and first glass panel 26 are sealed to opposite sides of the spacer frame 29 forming the IG assembly 16 .
- the reinforcement frame 18 is rollformed or stamped out of steel or aluminum.
- the frame halves 12 and 14 are injection molded out of polystyrene or another plastic.
- the frame halves 12 and 14 and the reinforcement frame 18 are assembled and packaged with the IG assembly 16 to create a product ready for shipping to the installer.
- the installer cuts or otherwise forms an opening in the supporting structure or door 100 .
- Conventional gaskets 80 a - b are installed within the grooves 52 and 54 on the exterior frame half 14 .
- the door 100 is oriented horizontally and the exterior frame half 14 is placed under the door aligned with the opening.
- the door-engagement flange 46 is sealed to the door 100 and the IG-engagement flange 48 is sealed to the IG assembly 16 .
- the IG assembly 16 is placed within the formed opening and on top of the exterior frame half 14 with the film 20 overlapping the edges of the perimeter of the formed opening.
- the reinforcement frame 18 is then installed so that the secured leg 64 sandwiches the film 20 to the door 100 around the perimeter of the formed opening.
- the film 20 extends from the edges of the laminated glass panels 22 and 24 around the channel 68 and beyond the edges of the secured leg 64 .
- a structural adhesive 38 a - b such as Dow #995 structural silicone is applied to the inner frame half 12 in the first recess 76 and the groove 36 (FIG. 2).
- the installer may be instructed to apply the adhesive 38 liberally to ensure a good seal.
- the inner frame half 12 is then inserted around the opening formed in the door 100 .
- the door-engagement flange 30 is adhered to the door 100 , and the secured leg 64 and the IG-engagement flange 32 are adhered to the IG assembly 16 and the supporting leg 66 .
- the screw bosses 60 on the inner frame half 12 fit within the channel 68 of the reinforcement frame 18 .
- the holes 42 on the inner frame half 12 are aligned with the holes 88 on the reinforcement frame 20 and the holes 58 on the outer frame half 14 to allow the screws 41 to pass through and secure the frame halves 12 and 14 together.
- the head of the screw 41 rests on the shoulder 43 in the screw boss 60 , and the screw is anchored in the boss 62 .
- the screws 41 draw the frame halves 12 and 14 together to sandwich (a) the door 100 , secured leg 64 and security film 20 between the door engagement flanges 30 and 46 , (b) the IG assembly 16 and the supporting leg 66 between the window engagement flanges 32 and 49 and (c) the reinforcement frame 18 and security film 20 between the bosses 60 and 62 .
- the film 20 is secured in two locations. First, the film is secured between the reinforcement frame 18 and the bosses 62 , with the screws 41 passing through all three elements. Second, the film is secured between the reinforcement frame 18 and the door 100 , with the screws 70 passing through all three elements. Consequently, the film 20 is securely retained in position so as to enable the window assembly to meet all current building code requirements. Any or all of the glass panels 22 , 24 , and 26 may break, but the film will remain intact and in position.
- a second reinforcement frame 84 is added to the doorlight 10 to provide extra security, especially against sudden pressure changes.
- a fastening means 71 such as a screw secures the second reinforcement frame 84 to the door 100 .
- the traditional gaskets 80 a - b on the outer frame half 14 are replaced with a structural adhesive 38 c - d.
- the outer frame half 14 also defines a recess 52 instead of the groove 52 .
- the remaining construction and assembly of the doorlight 10 is generally identical to the corresponding elements described above in connection with the preferred embodiment.
- the first glass panel 26 is replaced with a second laminated assembly 86 identical to the first laminated assembly 28 .
- the second film 92 also extends beyond the perimeter of the glass panels in the second laminated assembly 28 .
- the second film 92 is stretched around the second reinforcement frame 84 to be secured to the door 100 just as the first film 20 was as described above in connection with the preferred embodiment.
- the remaining construction and assembly of this doorlight 10 is generally identical to the corresponding elements described above in connection with the preferred embodiment and the second embodiment.
- the present invention is shown as a window 10 of an aircraft 100 .
- the window 10 includes a window assembly 16 and a frame assembly 8 as described above with various modifications to fit within the opening on an aircraft.
- the skin of the aircraft provides the outer frame half 15 .
- an additional piece (not shown) may be secured around the perimeter edge of the opening to act as an outer frame half.
- the window assembly 16 constructed as disclosed above, is placed in the opening with the film 20 overlapping the inner edge of the formed opening.
- the window assembly 16 may be made in a variety of ways such as including a laminated assembly 29 , two laminated assemblies (not shown), or using any of the alternative embodiments above.
- the reinforcement frame 18 is then placed around the perimeter of the opening sandwiching the film 20 to the supporting structure 100 with the secured leg 64 and the supporting leg 60 sandwiching the window assembly 16 against the outer skin 15 .
- the inner frame half 13 has structural adhesive 38 b applied to a groove 94 .
- Structural adhesive 38 a is applied around the indentation 96 so that it oozes into a first recess 102 and a second recess 104 defined by the inner frame half 13 .
- Structural adhesive 38 e is applied between the outer skin 15 of the aircraft 100 and the IG assembly 16 .
- a fastening means 44 such as a screw then is tightened to draw the inner frame half 13 together with the outer skin 15 .
- the outer skin 15 and the inner frame half 13 sandwich the supporting structure 100 , reinforcement frame 18 , film 20 and IG assembly 16 .
- the structural adhesive 38 a, b, and e may be a variety of materials used to fasten or secure parts together.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Securing Of Glass Panes Or The Like (AREA)
Abstract
Description
- I. Field of the Invention
- The present invention relates to windows and more particularly to impact-resistant and pressure-resistant windows.
- II. Description of the Art
- Exterior building windows are part of the “building envelope” comprising the exterior of the building. As part of the building envelope, exterior windows are subjected to a variety of weather extremes. An increasing number of building code standards and regulations have been, and continue to be, developed for such windows. In particular, many building codes include strenuous impact standards, which require a window to withstand impacts similar to those of a missile driven by high winds, as in a hurricane or a tornado. These building codes may also require the windows to withstand a variety of extreme cyclical pressure changes.
- One such standard may be found in
Chapters - Window manufacturers have developed, and continue to develop a variety of constructions in an effort to meet the evolving building code requirements. Examples of two such constructions are disclosed in U.S. Pat. 5,636,484 issued Jun. 10, 1997 to DeBlock and 5,765,325 issued Jun. 16, 1998 to DeBlock, which share a common disclosure of two embodiments. Both embodiments include a high-strength polycarbonate sheet (1) in the insulated glass assembly and (2) structurally and/or mechanically secured to the window frame. While a significant advance in the art, the development of even-stronger constructions has continued. For example, the most recent code requirements causes the polystyrene window frame to be the likely failure point in the prior construction.
- The aforementioned problems are overcome by the present invention wherein an insulated glass (IG) assembly includes a flexible impact-resistant sheet incorporated into the laminated glass, extending beyond the laminated glass, and secured between the frame and the structure to which it is mounted (e.g. a door or a building).
- In a preferred embodiment, the frame is injection molded of plastic and is reinforced with high-strength inserts extending between the frame and the glass.
- The window unit is extremely strong and is believed to meet all current building code requirements. Further, the window unit is relatively simple and inexpensive.
- These and other objects, advantages and features of the invention will be more fully understood and appreciated by reference to the detailed description of the preferred embodiments and the drawings.
- FIG. 1 is a perspective view of the doorlight of the present invention mounted within a door;
- FIG. 2 is a fragmentary exploded sectional view taken along line2-2 in FIG. 1;
- FIG. 3 is a fragmentary assembled sectional view taken along line2-2 in FIG. 1;
- FIG. 4 is a perspective view of the window in an aircraft;
- FIG. 5 is a sectional view taken along line5-5 in FIG. 4;
- FIG. 6 is a fragmentary cross sectional view similar to FIG. 3 showing a first alternative embodiment of the invention; and
- FIG. 7 is a fragmentary cross sectional view similar to FIG. 3 showing a second alternative embodiment of the invention.
- I. First Embodiment
- By way of disclosure and not by way of limitation, a doorlight constructed in accordance with a preferred embodiment of the invention is illustrated in FIGS.1-3 and generally designated 10. The
doorlight 10 includes anIG assembly 16 and aframe assembly 8. Theframe assembly 8 supports theIG assembly 16 within adoor 100 or other supporting structure. - The
IG assembly 16 in turn includes a laminatedassembly 28, afirst glass panel 26 and aspacer frame 29. If a non-insulated construction is desired, both thespacer frame 29 and thefirst glass panel 26 may be eliminated. - The laminated
assembly 28 includes asecond glass panel 24, athird glass panel 22 and a flexible impactresistant film 20. Theglass panels assembly 28 include aperimeter edge 122. Thesecond glass panel 24 and thethird glass panel 22 are laminated to the opposite sides of thefilm 20 using techniques well known to those skilled in the art. Thefilm 20 includes aperipheral margin portion 21 that extends beyond theglass panels film 20 could extend beyond the panels only in selected areas. In the preferred embodiment, the first, second andthird glass panels film 20 is 7 mil thick polyethylene terephthalate (P.E.T.), although other thicknesses and/or materials may be readily used. Thefilm 20 is flexible, although it may be semi-rigid depending on the thickness. Thespacer frame 29 holds the laminatedassembly 28 and thefirst glass panel 26 apart in an insulated construction. The fabrication of thespacer frame 29 and its attachment to the glass panels are well known to those skilled in the art. - The
frame assembly 8 includes aninner frame half 12, anouter frame half 14, and a reinforcement frame insert 18. The frame halves are generally well known to those skilled in the art of doorlights and windows. Theinner frame half 12 and theouter frame half 14 are fabricated of a high-performance UV-stable plastic or an injection-molded polystyrene. Theinner frame half 12 and theouter frame half 14 are fastened together with a first fastening means for interconnecting the frame halves, such asscrews 41 to secure theIG assembly 16 within the supportingstructure 100. - The
inner frame half 12 includes a door-engagement flange 30, an IG-assembly-engagement flange 32 and a main-body portion 34. The door-engagement flange 30 extends from the main-body portion 34 to thedoor 100 or support structure, and defines afirst recess 76. Thefirst recess 76 allows the second fastening means 70, discussed below, to be hidden from sight. Thefirst recess 76 also receives astructural adhesive 38 a to seal the door-engagement flange 30 to thedoor 100. The IG-engagement flange 32 extends from the main-body portion 34 to contact theIG assembly 16. The IG-engagement flange 32 defines a groove 40 extending along the length of theinner frame half 12 for receiving astructural adhesive 38 b. The main-body portion 34 is located between the IG-engagement flange 32 and the door-engagement flange 30. The main-body portion 34 includes a plurality of screw bosses spaced about theinner frame half 12. Eachscrew boss 60 extends and defines ahole 42 through which a screw (not shown) passes. - The
outer frame half 14 is somewhat of a mirror image of theinner frame half 12. Theouter frame half 14 includes a door-engagement flange 46, a window-engagement flange 48 and a main-body portion 50. The door-engagement flange 46 defines agroove 52 in which atraditional gasket material 80 a is placed. The window-engagement flange 48 defines agroove 54 in which atraditional gasket material 80 b is placed. Thesegrooves outer frame 14. Themain body portion 50 also includes a plurality ofscrew bosses 62 to receive thescrews 41. Oneboss 62 is aligned with eachboss 60 when the frame halves are aligned with one another. - The reinforcement frame18 (FIGS. 2 and 3) is uniform in cross section throughout its length and includes a
secured leg 64, a supportingleg 66 and a U-shaped channel 68. The channel 68 connects the supportingleg 66 and thesecured leg 64. The secured leg 68 contacts the door or other supportingstructure 100, and the supportingleg 66 contacts theIG assembly 16. The channel 68 includes a plurality ofholes 88 to allow the screws (not shown) to pass through. Thescrews 70 secure the secured leg 68 to thedoor 100. In the preferred embodiment, thereinforcement frame 18 is 24 gauge steel, but may be any suitable thickness or material. To reduce materials, costs, and disposal issues, thereinforcement frame 18 can be made out of the skin of thedoor 100. In the preferred embodiment, thereinforcement frame 18 is located under theinterior frame half 12 and on top of the supportingstructure 100 and theIG assembly 16. - II. Manufacture and Installation of the First Embodiment
- The present invention is adopted for installation within an opening of a supporting
structure 100, such as a door. TheIG assembly 10 may come in various sizes and shapes to fit within nearly any opening. - The
glass panels glass panels film 20 forming thelaminated assembly 28. Themargin portion 21 of the film extends beyond the glass in all directions. Thefilm 20 may be trimmed if necessary. Thelaminated assembly 28 andfirst glass panel 26 are sealed to opposite sides of thespacer frame 29 forming theIG assembly 16. - The
reinforcement frame 18 is rollformed or stamped out of steel or aluminum. The frame halves 12 and 14 are injection molded out of polystyrene or another plastic. The frame halves 12 and 14 and thereinforcement frame 18 are assembled and packaged with theIG assembly 16 to create a product ready for shipping to the installer. - The installer cuts or otherwise forms an opening in the supporting structure or
door 100. Conventional gaskets 80 a-b are installed within thegrooves exterior frame half 14. Thedoor 100 is oriented horizontally and theexterior frame half 14 is placed under the door aligned with the opening. The door-engagement flange 46 is sealed to thedoor 100 and the IG-engagement flange 48 is sealed to theIG assembly 16. TheIG assembly 16 is placed within the formed opening and on top of theexterior frame half 14 with thefilm 20 overlapping the edges of the perimeter of the formed opening. Thereinforcement frame 18 is then installed so that thesecured leg 64 sandwiches thefilm 20 to thedoor 100 around the perimeter of the formed opening. Thefilm 20 extends from the edges of thelaminated glass panels secured leg 64. - A
structural adhesive 38 a-b such as Dow #995 structural silicone is applied to theinner frame half 12 in thefirst recess 76 and the groove 36 (FIG. 2). Of course other adhesives and materials may be used to secure theinner frame half 12 to thedoor 100. The installer may be instructed to apply the adhesive 38 liberally to ensure a good seal. Theinner frame half 12 is then inserted around the opening formed in thedoor 100. The door-engagement flange 30 is adhered to thedoor 100, and thesecured leg 64 and the IG-engagement flange 32 are adhered to theIG assembly 16 and the supportingleg 66. - The
screw bosses 60 on theinner frame half 12 fit within the channel 68 of thereinforcement frame 18. Theholes 42 on theinner frame half 12 are aligned with theholes 88 on thereinforcement frame 20 and theholes 58 on theouter frame half 14 to allow thescrews 41 to pass through and secure the frame halves 12 and 14 together. The head of thescrew 41 rests on theshoulder 43 in thescrew boss 60, and the screw is anchored in theboss 62. - The
screws 41 draw the frame halves 12 and 14 together to sandwich (a) thedoor 100,secured leg 64 andsecurity film 20 between thedoor engagement flanges IG assembly 16 and the supportingleg 66 between thewindow engagement flanges 32 and 49 and (c) thereinforcement frame 18 andsecurity film 20 between thebosses IG assembly 16 and thedoor 100. - The
film 20 is secured in two locations. First, the film is secured between thereinforcement frame 18 and thebosses 62, with thescrews 41 passing through all three elements. Second, the film is secured between thereinforcement frame 18 and thedoor 100, with thescrews 70 passing through all three elements. Consequently, thefilm 20 is securely retained in position so as to enable the window assembly to meet all current building code requirements. Any or all of theglass panels - III. Alternative Embodiments
- A. Second Embodiment
- In the second embodiment illustrated in FIG. 6, a
second reinforcement frame 84 is added to thedoorlight 10 to provide extra security, especially against sudden pressure changes. A fastening means 71 such as a screw secures thesecond reinforcement frame 84 to thedoor 100. The traditional gaskets 80 a-b on theouter frame half 14 are replaced with astructural adhesive 38 c-d. Theouter frame half 14 also defines arecess 52 instead of thegroove 52. The remaining construction and assembly of thedoorlight 10 is generally identical to the corresponding elements described above in connection with the preferred embodiment. - B. Third Embodiment
- In the third embodiment illustrated in FIG. 7, the
first glass panel 26 is replaced with a secondlaminated assembly 86 identical to the firstlaminated assembly 28. Thesecond film 92 also extends beyond the perimeter of the glass panels in the secondlaminated assembly 28. Thesecond film 92 is stretched around thesecond reinforcement frame 84 to be secured to thedoor 100 just as thefirst film 20 was as described above in connection with the preferred embodiment. The remaining construction and assembly of thisdoorlight 10 is generally identical to the corresponding elements described above in connection with the preferred embodiment and the second embodiment. - C. Fourth Embodiment
- In the fourth embodiment illustrated in FIGS.4-5, the present invention is shown as a
window 10 of anaircraft 100. Thewindow 10 includes awindow assembly 16 and aframe assembly 8 as described above with various modifications to fit within the opening on an aircraft. As shown in FIG. 5, the skin of the aircraft provides theouter frame half 15. Alternatively, an additional piece (not shown) may be secured around the perimeter edge of the opening to act as an outer frame half. Thewindow assembly 16, constructed as disclosed above, is placed in the opening with thefilm 20 overlapping the inner edge of the formed opening. Thewindow assembly 16 may be made in a variety of ways such as including alaminated assembly 29, two laminated assemblies (not shown), or using any of the alternative embodiments above. Thereinforcement frame 18 is then placed around the perimeter of the opening sandwiching thefilm 20 to the supportingstructure 100 with thesecured leg 64 and the supportingleg 60 sandwiching thewindow assembly 16 against theouter skin 15. Theinner frame half 13 has structural adhesive 38 b applied to agroove 94. Structural adhesive 38 a is applied around theindentation 96 so that it oozes into afirst recess 102 and asecond recess 104 defined by theinner frame half 13. Structural adhesive 38 e is applied between theouter skin 15 of theaircraft 100 and theIG assembly 16. A fastening means 44 such as a screw then is tightened to draw theinner frame half 13 together with theouter skin 15. Theouter skin 15 and theinner frame half 13 sandwich the supportingstructure 100,reinforcement frame 18,film 20 andIG assembly 16. The structural adhesive 38 a, b, and e may be a variety of materials used to fasten or secure parts together. - While this invention has been described in conjunction with doorlights and aircraft windows, it should be readily apparent that the present invention has a variety of uses in other applications such as building windows, skyscraper windows, mobile home windows, residential home windows and many more applications where glazing panels need to be impact resistant and resistant to pressure changes.
- The above descriptions are those of preferred embodiments of the invention. Various alterations and changes can be made without departing from the spirit and broader aspects of the invention as set forth in the appended claims, which are to be interpreted in accordance with the principles of patent law including the doctrine of equivalents.
- The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
Claims (13)
Priority Applications (1)
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US09/974,264 US6546682B1 (en) | 2001-10-10 | 2001-10-10 | Hurricane door light |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US09/974,264 US6546682B1 (en) | 2001-10-10 | 2001-10-10 | Hurricane door light |
Publications (2)
Publication Number | Publication Date |
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US20030066256A1 true US20030066256A1 (en) | 2003-04-10 |
US6546682B1 US6546682B1 (en) | 2003-04-15 |
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Application Number | Title | Priority Date | Filing Date |
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US09/974,264 Expired - Fee Related US6546682B1 (en) | 2001-10-10 | 2001-10-10 | Hurricane door light |
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US (1) | US6546682B1 (en) |
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