US2679467A - Pressure blowout safety closure - Google Patents
Pressure blowout safety closure Download PDFInfo
- Publication number
- US2679467A US2679467A US237957A US23795751A US2679467A US 2679467 A US2679467 A US 2679467A US 237957 A US237957 A US 237957A US 23795751 A US23795751 A US 23795751A US 2679467 A US2679467 A US 2679467A
- Authority
- US
- United States
- Prior art keywords
- unit
- glass
- closure
- interlayer
- segments
- 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.)
- Expired - Lifetime
Links
- 239000011229 interlayer Substances 0.000 claims description 20
- 238000004880 explosion Methods 0.000 claims description 15
- 229920003023 plastic Polymers 0.000 claims description 11
- 239000004033 plastic Substances 0.000 claims description 9
- 229920001169 thermoplastic Polymers 0.000 claims description 7
- 239000004416 thermosoftening plastic Substances 0.000 claims description 7
- 239000011521 glass Substances 0.000 description 19
- 239000005357 flat glass Substances 0.000 description 11
- BZHJMEDXRYGGRV-UHFFFAOYSA-N Vinyl chloride Chemical compound ClC=C BZHJMEDXRYGGRV-UHFFFAOYSA-N 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 238000000926 separation method Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 3
- DHKHKXVYLBGOIT-UHFFFAOYSA-N acetaldehyde Diethyl Acetal Natural products CCOC(C)OCC DHKHKXVYLBGOIT-UHFFFAOYSA-N 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000005340 laminated glass Substances 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 239000013521 mastic Substances 0.000 description 2
- -1 vinyl acetal Chemical class 0.000 description 2
- 229920002554 vinyl polymer Polymers 0.000 description 2
- 229920000298 Cellophane Polymers 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 239000002390 adhesive tape Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000009432 framing Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000002650 laminated plastic Substances 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000003566 sealing material Substances 0.000 description 1
Images
Classifications
-
- 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
-
- 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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
- Y10T156/1092—All laminae planar and face to face
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31551—Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
- Y10T428/31645—Next to addition polymer from unsaturated monomers
- Y10T428/31649—Ester, halide or nitrile of addition polymer
Definitions
- This invention relates to. transparent closures and it has particular relation to safety closures adapted to rupture under. predetermined explosion pressure and then can be substantially restored to function as an effective closure.
- One object of the invention is to provide an improved explosion closure so designed as to rupture along predetermined areas under pressure resulting from an explosion, or from other pressures, and also so designed that the ruptured segments can be restored substantially to their original position.
- Another object of the invention is to provide an improved laminated transparent unit capable of being ruptured and the resulting segments replaced and secured substantially in the original plane of the unit in the form of an effective closure.
- Another object of the invention is to provide an improved method of making a laminated unit having predetermined rupturing characteristics.
- Another object of the invention is to provide an improved method of making a laminated unit having characteristics which cause it to rupture along predetermined areas under pressure resulting from explosions, and to render it restorable to an eifective closure unit after it has been ruptured.
- window units may shatter, or large segments may be blown out bodily.
- the invention described herein is directed to the problem of providing a transparent window closure that responds to pressures in such manner that the window is breakable along predetermined areas to define segments which can move inwardly or outwardly from the plane of the original closure unit and which can be restored to the plane of such original unit a short time after it has been ruptured.
- Laminated glass or plastic can be employed as Window elements for the purposes of this invention.
- a rectangular laminated unit. is manufactured in such manner that an interlayer of plastic material extends beyond the edges of the outside plates so as to be mountable upon. frame members which are clamped upon opposite sides" thereof. In this way the: unit is flexibly mounted in the frame defining the window. Examples of this general type of closure structure are found in U. S. Patents 2,427,557, dated September: 16,: 1947, and 2,293,656,. dated August 18, 1942.
- Both of the outer plates, or only one of them, can be scored or splitdiagonally whilev themarginal edge portions of the plastic interlayer remain intact and upon mounting in the frame support as described, the window can. be: forced" outwardly from its plane and ruptured alongthe diagonal lines.
- the segments resulting from: the broken unit swing outwardly upon the flexible mounting edges in a hinging action. Since the marginal portions are flexible and the rupture is effected along the diagonal-areas, the segments can be swung back into substantially their original position and fastened in this position.
- the joints along the diagonal lines of breakage can be filled with mastic, or putty, or: other material which will serve to seal the joints.
- Fig. 1 is a fragmentary front elevation of a closure unit in which the invention has been incorporated;
- Fig. 2 is a fragmentary cross sec-; tion on a larger scale taken substantially along the line II-II of Fig. 1;
- Fig. 3 is a fragmentary perspective of a closure unit which has been subjected to pressure breakage;
- Fig. 4 is a front elevation of a closure unit with segments thereof restored to their original position after they have been displaced;
- Fig. 5 is a fragmentary cross section on a larger scale taken substantially along the line V--V of Fig. 4;
- Fig. dis a front elevation: of another form of structure similar to that shown in Fig. 1;
- Fig. 9 is a. crosssection on a larger scale taken substantially along the line IX-IX of Fig. 8;
- Fig. 10' is a cross-section of another form similar to Fig. 9.
- a rectangular laminated closure unit it which is composed of a sheet interlayer 12 of transparent plastic such as vinyl acetal resinand plate glass' I3 and I4 adhered upon opposite sides thereof;
- the composite elements l2, l3, and M are laminated in a conventional manner so that the plate glass structure and plastic interlayer form a unitary closure member adapted to be installed as a window or other similarrstructure.
- Marginal edges 15 of the plastic extend beyond the edges of the plate glass around the four edges thereof and provide a flexible connection between the glass plates and a surrounding supporting framework 16.
- the fiexible edges l are clamped between the marginal portions of the framework and suitable framing strips l9 by means of bolts which extend through the marginal portions of the plastic as well as through the frame members 16 and I9.
- the plate glass 13 on one side of the unit is split diagonally to form diagonal splitting areas 2
- Such splitting of the unit divides it into four triangular segments 24 each normally having one of its angular portions pointing toward the area 23 where the splitting lines intersect.
- the segments 24 are slightly separated, for example approximately .04 of an inch, before the final lamination of the glass is accomplished; that is, before the unit is placed in an autoclave.
- the interlayer sheet [2 is also split, as indicated at 25, along areas substantially coextensive with the areas of splitting of the glass plate.
- suitable spacing material for example, vinyl chloride 25, to maintain proper spacing between the segments during the pressing operation which is incidental to the lamination of plate glass.
- suitable spacing material for example, vinyl chloride 25
- the unit ill will rupture under the explosive force and the glass segments 24 will define the area of breakage of the plate glass [4 which has not been split but which will rupture substantially along the lines of the splitting areas 2
- the laminated glass segments then assume the position indicated in Fig. 3. That is, they are forced outwardly. It has been found that the unit will break and the segments of the unit will assume the angular position indicated in this figure regardless of whether the force of the explosion is applied on the side of the unit having the splitting areas or on the other side of the unit where the plate glass was continuous in its original laminated form.
- the flexible marginal portions [5 can bend more or less freely to permit the broken segments of the glass to swing outwardly. lhe unit can be repaired, at least to an effective degree and to the extent of substantially closing the unit, by moving the segments back to substantially a common plane corresponding to the plane of the original unit. Then by applying a bolt 29 at the central intersecting area 23, together with washers engaging opposite sides of the unit in overlapping relation to th segments 24, these elements can be reassembled.
- the areas of separation between adjacent segments 24 after restoration to their original common plane can be filled with sealing material such as putty or mastic, or covered with strips of adhesive tape, or so-called cellophane tape, which will maintain a substantial closure against entrance of air or gases.
- a unit Illa similar to the unit I0 is mounted in the same manner in plosion.
- frame structure elements l6a and 19a that are clamped by means of bolts 20a on opposite sides of the interlayer margins 15a.
- the plate glass 1311 and Ma on both sides of the interlayer 12a was continuous.
- Only the plastic interlayer 12a is split diagonally, as indicated at 2511, from the four corners of the unit.
- the areas 250. of splitting intersect, as indicated at 23a, at the central portion of the unit in substantially the same manner as the areas of splitting 25 intersect at 23 in the arrangement described with reference to Figs. 1 and 2.
- the areas of splitting of the plastic interlayer will define the lines of breakage of the unit under the force of an exthe glass itself is not split, the unit will be stronger. In a unit of this type the glass can be thinner.
- a filler of more or less non-adherent spacing material such as vinyl chloride, can be applied in the areas 25a to maintain proper sep-. aration of the interlayer sections in the manner shown at 26 in Fig. 2.
- the glass plate structure on both sides, or on one side, of the unit can be cut or scored as indicated at 2la, to facilitate splitting thereof along the lines defined diagonally across the unit when it is subjected to the forces of an explosion.
- the cut or scored portions Hi) can be designated as splitting areas.
- a unit lllb similar to the unit It! is mountable along its marginal portions l5b in the same manner as that described with reference to the mounting of the unit I0 between elements It and I9.
- the plate glass elements I31) and Nb on opposite sides of the vinyl acetal interlayer 12b are split only in one direction. That is, the plate glass l3b is split along one diagonal area 2 lb while the plate glass on the other side of the interlayer is split along a similar diagonal area 2 la which is transverse to the splitting area 21b.
- the splitting area 2lb extends diagonally from the upper right hand corner of the unit [0b to the lower left hand corner thereof, whereas the splitting area 2Ic extends diagonally from the upper left hand corner to the lower right hand corner of the unit lllb.
- the interlayer l2b is split diagonally in both directions as indicated at 2519 and 250 and that suitable spacing material 26c, such as vinyl chloride, is applied in the same manner as the vinyl chloride 26 is applied in the construction described above.
- a transparent laminated closure member comprising glass sheets adhered to opposite faces. of a thermoplastic interlayer which projects beyond the edges of the sheets to provide for fiexible mounting of the member within a structure opening, one of the glass sheets being formed of four triangular sections disposed in spaced relation to define intersecting diagonal splitting lines upon which the continuous glass sheet and the plastic of the closure member can rupture without separation from the structure when one face of the closure member is exposed to a sudden force as from a nearby explosion.
- a laminated closure member for a structure opening comprising superposed glass sheets adbored to opposite faces of a thermoplastic interlayer which projects beyond the edges of the closure member to provide a flexible mounting means to the adjacent structure, one of the glass sheets and the interlayer being cut alOng intersecting diagonal lines extending between opposite corners of the cut glass sheet to provide four spaced triangular segments adhered to the uncut glass sheet, the uncut glass sheet normally forming a continuous glass member suspended Within the structure opening by the uncut extensions of the thermoplastic layer and breaking along the cut lines of the glass sheet and interlayer without separation from the uncut portions of the interlayer upon application of an unusual force as by a nearby explosion.
- a transparent closure member for a structure opening and adapted for rupturing along predetermined lines without separation from the supporting structure upon application of an unusual force comprising a continuous transparent normally rigid and brittle member substantially corresponding to the shape of the structure opening but smaller in size, a flexible member adhered to one face of the continuous member and extending beyond the edges thereof to form a flexible mounting means for the continuous member within the structure opening, a lurality of substantially triangularly shaped spaced transparent members adhered to the flexible member and overlying the continuous member to define lines of rupture of the continuous mom-- her, the continuous member forming the sole means spanning the spaces between the spaced members.
- a transparent closure for a structure opening and adapted for rupturing along predetermined lines without separation from the supporting structure upon application of an unusual force comprising two superposed continuous transparent normally rigid and brittle members substantially corresponding to the shape of the structure opening but smaller in size, a thermoplastic member disposed between and adhered to adjacent faces of the superposed members, the thermoplastic member extending beyond the edges of the superposed members for flexibly suspending them upon the structure and within the structure opening, and predetermined lines of rupture of the superposed members formed in the thermoplastic member by cutting thin strips from the latter member along intersecting diagonal lines disposed within the area defined by the perimeter of the superposed members.
Description
J. H. SHERTS PRESSURE BLOWOUT SAFETY CLOSURE May 25, 1954 s Sheeis-Sheet 1 Filed July 21, 1951 INVENTOR. JAMES HERVE! SHERTS 94cm A y25,1954 J. H. SHERTS 2,679,467
PRESSURE BLOWOUT SAFETY CLOSURE Filed July 21 1951 3 Sheets-Sheet 2 INVENTOR.
JAMES HERVEY susms l5 (0 BY (9m K m May 25, 1954 J. H. SHERTS PRESSURE BLOWOUT SAFETY CLOSURE Filed July 21 1951 3 Sheets-Sheet 3 [ 4b 25b 26b //vv=w Toe JAMES HERVE! snags 94m: flTTOeA/EK lob Patented May 25, 1954 PRESSURE BLOWOUT SAFETY CLOSURE James Hervey Sherts, Pittsburgh, Pa., assignor to Pittsburgh Plate Glass Company, Allegheny County, Pa., a corporation of Pennsylvania Application July 21, 1951, Serial No. 237,957 4 Claims. (01. 1542.73)
This invention relates to. transparent closures and it has particular relation to safety closures adapted to rupture under. predetermined explosion pressure and then can be substantially restored to function as an effective closure.
One object of the invention is to provide an improved explosion closure so designed as to rupture along predetermined areas under pressure resulting from an explosion, or from other pressures, and also so designed that the ruptured segments can be restored substantially to their original position.
Another object of the invention is to provide an improved laminated transparent unit capable of being ruptured and the resulting segments replaced and secured substantially in the original plane of the unit in the form of an effective closure.
Another object of the invention is to provide an improved method of making a laminated unit having predetermined rupturing characteristics.
Another object of the invention is to provide an improved method of making a laminated unit having characteristics which cause it to rupture along predetermined areas under pressure resulting from explosions, and to render it restorable to an eifective closure unit after it has been ruptured.
In locations Where explosions may occur, for example at arsenals, explosive manufacturing plants, and in numerous areas in time of war, the effect of the pressures exerted by explosions upon windows may involve breakage that cannot be repaired except by replacement of the glazing unit. Under the impact of the explosion pressures, window units may shatter, or large segments may be blown out bodily.
Also the problem of replacement of windows in the wake of a destructive explosion isa serious one. It is very important under certain circumstances that the windows be closed and/or replaced immediately.
The invention described herein is directed to the problem of providing a transparent window closure that responds to pressures in such manner that the window is breakable along predetermined areas to define segments which can move inwardly or outwardly from the plane of the original closure unit and which can be restored to the plane of such original unit a short time after it has been ruptured. Laminated glass or plastic can be employed as Window elements for the purposes of this invention. In one type of window, a rectangular laminated unit. is manufactured in such manner that an interlayer of plastic material extends beyond the edges of the outside plates so as to be mountable upon. frame members which are clamped upon opposite sides" thereof. In this way the: unit is flexibly mounted in the frame defining the window. Examples of this general type of closure structure are found in U. S. Patents 2,427,557, dated September: 16,: 1947, and 2,293,656,. dated August 18, 1942.
Both of the outer plates, or only one of them, can be scored or splitdiagonally whilev themarginal edge portions of the plastic interlayer remain intact and upon mounting in the frame support as described, the window can. be: forced" outwardly from its plane and ruptured alongthe diagonal lines. The segments resulting from: the broken unit swing outwardly upon the flexible mounting edges in a hinging action. Since the marginal portions are flexible and the rupture is effected along the diagonal-areas, the segments can be swung back into substantially their original position and fastened in this position. The joints along the diagonal lines of breakage can be filled with mastic, or putty, or: other material which will serve to seal the joints.
In the drawings:
Fig. 1 is a fragmentary front elevation of a closure unit in which the invention has been incorporated; Fig. 2 is a fragmentary cross sec-; tion on a larger scale taken substantially along the line II-II of Fig. 1; Fig. 3 is a fragmentary perspective of a closure unit which has been subjected to pressure breakage; Fig. 4 is a front elevation of a closure unit with segments thereof restored to their original position after they have been displaced; Fig. 5 is a fragmentary cross section on a larger scale taken substantially along the line V--V of Fig. 4; Fig. dis a front elevation: of another form of structure similar to that shown in Fig. 1; Fig. '7 is a cross section on a larger scale taken substantially along the line VII-VII of Fig. 6; Fig. 8 is a front elevation of another form of closure unit in which the inven-- tion ha been incorporated; Fig. 9 is a. crosssection on a larger scale taken substantially along the line IX-IX of Fig. 8; Fig. 10'is a cross-section of another form similar to Fig. 9.
In practicing the invention, there is provided a rectangular laminated closure unit it which is composed of a sheet interlayer 12 of transparent plastic such as vinyl acetal resinand plate glass' I3 and I4 adhered upon opposite sides thereof; The composite elements l2, l3, and M are laminated in a conventional manner so that the plate glass structure and plastic interlayer form a unitary closure member adapted to be installed as a window or other similarrstructure.
As shown in Figs. 1 and 2, the plate glass 13 on one side of the unit is split diagonally to form diagonal splitting areas 2| intersecting in the central portion of the unit at a location indicated at 23. Such splitting of the unit divides it into four triangular segments 24 each normally having one of its angular portions pointing toward the area 23 where the splitting lines intersect.
The segments 24 are slightly separated, for example approximately .04 of an inch, before the final lamination of the glass is accomplished; that is, before the unit is placed in an autoclave. The interlayer sheet [2 is also split, as indicated at 25, along areas substantially coextensive with the areas of splitting of the glass plate. The spaces along the splitting areas between adjacent segments 24 and the corresponding splitting areas of the interlayer sheet are filled with suitable spacing material, for example, vinyl chloride 25, to maintain proper spacing between the segments during the pressing operation which is incidental to the lamination of plate glass. Well known examples of laminating glass are disclosed in U. S. Patents 1,781,084, dated November 11, 1930 and 1,870,693, dated August 9, 1932. After the 1aminating operations have been completed, the vinyl chloride spacing elements 26 can be removed.
In the event of an explosion in the neighborhood where closure units of the type described above are installed, the unit ill will rupture under the explosive force and the glass segments 24 will define the area of breakage of the plate glass [4 which has not been split but which will rupture substantially along the lines of the splitting areas 2| adjacent thereto. The laminated glass segments then assume the position indicated in Fig. 3. That is, they are forced outwardly. It has been found that the unit will break and the segments of the unit will assume the angular position indicated in this figure regardless of whether the force of the explosion is applied on the side of the unit having the splitting areas or on the other side of the unit where the plate glass was continuous in its original laminated form.
As a result of the explosion, the flexible marginal portions [5 can bend more or less freely to permit the broken segments of the glass to swing outwardly. lhe unit can be repaired, at least to an effective degree and to the extent of substantially closing the unit, by moving the segments back to substantially a common plane corresponding to the plane of the original unit. Then by applying a bolt 29 at the central intersecting area 23, together with washers engaging opposite sides of the unit in overlapping relation to th segments 24, these elements can be reassembled.
The areas of separation between adjacent segments 24 after restoration to their original common plane can be filled with sealing material such as putty or mastic, or covered with strips of adhesive tape, or so-called cellophane tape, which will maintain a substantial closure against entrance of air or gases.
As shown in Figs. 6 and '7, a unit Illa similar to the unit I0 is mounted in the same manner in plosion. However, since frame structure elements l6a and 19a that are clamped by means of bolts 20a on opposite sides of the interlayer margins 15a. However, in this arrangement, the plate glass 1311 and Ma on both sides of the interlayer 12a was continuous. Only the plastic interlayer 12a is split diagonally, as indicated at 2511, from the four corners of the unit. The areas 250. of splitting intersect, as indicated at 23a, at the central portion of the unit in substantially the same manner as the areas of splitting 25 intersect at 23 in the arrangement described with reference to Figs. 1 and 2. In an installation of this type, the areas of splitting of the plastic interlayer will define the lines of breakage of the unit under the force of an exthe glass itself is not split, the unit will be stronger. In a unit of this type the glass can be thinner.
If desired a filler of more or less non-adherent spacing material, such as vinyl chloride, can be applied in the areas 25a to maintain proper sep-. aration of the interlayer sections in the manner shown at 26 in Fig. 2.
The installation shown in Figs. 3 and 4 can be repaired in the same manner as that described above with reference to the use of bolt and washer elements corresponding to the bolt 29 and washers 30.
If desired, the glass plate structure on both sides, or on one side, of the unit can be cut or scored as indicated at 2la, to facilitate splitting thereof along the lines defined diagonally across the unit when it is subjected to the forces of an explosion. The cut or scored portions Hi) can be designated as splitting areas.
In another form of the invention as illustrated in Figs. 8, 9, and 10, a unit lllb similar to the unit It! is mountable along its marginal portions l5b in the same manner as that described with reference to the mounting of the unit I0 between elements It and I9. In this arrangement, the plate glass elements I31) and Nb on opposite sides of the vinyl acetal interlayer 12b are split only in one direction. That is, the plate glass l3b is split along one diagonal area 2 lb while the plate glass on the other side of the interlayer is split along a similar diagonal area 2 la which is transverse to the splitting area 21b. In other words,
the splitting area 2lb extends diagonally from the upper right hand corner of the unit [0b to the lower left hand corner thereof, whereas the splitting area 2Ic extends diagonally from the upper left hand corner to the lower right hand corner of the unit lllb. It is to be noted that the interlayer l2b is split diagonally in both directions as indicated at 2519 and 250 and that suitable spacing material 26c, such as vinyl chloride, is applied in the same manner as the vinyl chloride 26 is applied in the construction described above.
Although more than one form of the invention has been shown and described in detail, it will be apparent to those skilled in the art that the invention is not so limited but that various changes can be made therein without departing from the spirit and/or scope of the invention as exemplified in the appended claims.
What is claimed is:
1. A transparent laminated closure member comprising glass sheets adhered to opposite faces. of a thermoplastic interlayer which projects beyond the edges of the sheets to provide for fiexible mounting of the member within a structure opening, one of the glass sheets being formed of four triangular sections disposed in spaced relation to define intersecting diagonal splitting lines upon which the continuous glass sheet and the plastic of the closure member can rupture without separation from the structure when one face of the closure member is exposed to a sudden force as from a nearby explosion.
2. A laminated closure member for a structure opening comprising superposed glass sheets adbored to opposite faces of a thermoplastic interlayer which projects beyond the edges of the closure member to provide a flexible mounting means to the adjacent structure, one of the glass sheets and the interlayer being cut alOng intersecting diagonal lines extending between opposite corners of the cut glass sheet to provide four spaced triangular segments adhered to the uncut glass sheet, the uncut glass sheet normally forming a continuous glass member suspended Within the structure opening by the uncut extensions of the thermoplastic layer and breaking along the cut lines of the glass sheet and interlayer without separation from the uncut portions of the interlayer upon application of an unusual force as by a nearby explosion.
3. A transparent closure member for a structure opening and adapted for rupturing along predetermined lines without separation from the supporting structure upon application of an unusual force, comprising a continuous transparent normally rigid and brittle member substantially corresponding to the shape of the structure opening but smaller in size, a flexible member adhered to one face of the continuous member and extending beyond the edges thereof to form a flexible mounting means for the continuous member within the structure opening, a lurality of substantially triangularly shaped spaced transparent members adhered to the flexible member and overlying the continuous member to define lines of rupture of the continuous mom-- her, the continuous member forming the sole means spanning the spaces between the spaced members.
4. A transparent closure for a structure opening and adapted for rupturing along predetermined lines without separation from the supporting structure upon application of an unusual force, comprising two superposed continuous transparent normally rigid and brittle members substantially corresponding to the shape of the structure opening but smaller in size, a thermoplastic member disposed between and adhered to adjacent faces of the superposed members, the thermoplastic member extending beyond the edges of the superposed members for flexibly suspending them upon the structure and within the structure opening, and predetermined lines of rupture of the superposed members formed in the thermoplastic member by cutting thin strips from the latter member along intersecting diagonal lines disposed within the area defined by the perimeter of the superposed members.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,121,777 Bailey June 29, 1938 2,202,690 Fix May 28, 1940 2,300,506 Kamerer Nov. 3, 1942 2,382,963 Dodge Aug. 21, 1945 FOREIGN PATENTS Number Country Date 513,426 Great Britain Oct. 12, 1939
Claims (1)
1. A TRANSPARENT LAMINATED CLOSURE MEMBER COMPRISING GLASS SHEETS ADHERED TO OPPOSITE FACES OF A THERMOPLASTIC INTERLAYER WHICH PROJECTS BEYOND THE EDGES OF THE SHEETS TO PROVIDE FOR FLEXIBLE MOUNTING OF THE MEMBER WITHIN A STRUCTURE OPENING, ONE OF THE GLASS SHEETS BEING FORMED OF FOUR TRIANGULAR SECTIONS DISPOSED IN SPACED RELATION TO DEFINED INTERSECTING DIAGONAL SPLITTING LINES UPON WHICH THE CONTINUOUS GLASS SHEET AND THE PLASTIC OF THE CLOSURE MEMBER CAN RUPTURE WITHOUT SEPARTION FROM THE STRUCTURE WHEN ONE FACE OF THE CLOSURE MEMBER IS EXPOSED TO A SUDDEN FORCE AS FROM A NEARBY EXPLOSION.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US237957A US2679467A (en) | 1951-07-21 | 1951-07-21 | Pressure blowout safety closure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US237957A US2679467A (en) | 1951-07-21 | 1951-07-21 | Pressure blowout safety closure |
Publications (1)
Publication Number | Publication Date |
---|---|
US2679467A true US2679467A (en) | 1954-05-25 |
Family
ID=22895928
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US237957A Expired - Lifetime US2679467A (en) | 1951-07-21 | 1951-07-21 | Pressure blowout safety closure |
Country Status (1)
Country | Link |
---|---|
US (1) | US2679467A (en) |
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2721157A (en) * | 1953-01-05 | 1955-10-18 | Pittsburgh Plate Glass Co | Explosion resisting window |
US2758042A (en) * | 1952-12-09 | 1956-08-07 | Pittsburgh Plate Glass Co | Safety glass construction |
US2784926A (en) * | 1953-03-30 | 1957-03-12 | Lockheed Aircraft Corp | Protected aircraft enclosures |
US2851388A (en) * | 1954-04-26 | 1958-09-09 | Mine Safety Appliances Co | Protective shield |
US3078201A (en) * | 1960-03-21 | 1963-02-19 | Midwest Research Inst | Seam structure for a flexible bag |
US3401976A (en) * | 1965-07-21 | 1968-09-17 | Renault | Sun visors for vehicles |
US3630812A (en) * | 1968-01-29 | 1971-12-28 | Saint Gobain | Windshield for motor vehicles |
US3797167A (en) * | 1972-03-07 | 1974-03-19 | F Gomboc | Fire escape window |
US3807106A (en) * | 1973-04-16 | 1974-04-30 | Eastman Kodak Co | Explosion relief wall supporting fastener |
US3938764A (en) * | 1975-05-19 | 1976-02-17 | Mcdonnell Douglas Corporation | Frangible aircraft floor |
US4049221A (en) * | 1975-12-24 | 1977-09-20 | Lockheed Aircraft Corporation | Relief of inter-compartment differential pressure in aircraft |
US4067154A (en) * | 1975-02-20 | 1978-01-10 | Fike Metal Products Corporation | Instantaneous venting, non-frangible burst panel structure |
US4089140A (en) * | 1976-09-24 | 1978-05-16 | Mcdonnell Douglas Corporation | Carpet installation for frangible aircraft floors |
US4248610A (en) * | 1978-08-09 | 1981-02-03 | Metallgesellschaft Aktiengesellschaft | Dust collector with pressure-relief opening |
US4390152A (en) * | 1976-05-13 | 1983-06-28 | Lockheed Corporation | Aircraft decompression vent assembly |
US4432514A (en) * | 1976-09-23 | 1984-02-21 | The Boeing Company | Decompression equalization relief valve |
US4498261A (en) * | 1981-12-07 | 1985-02-12 | Continental Disc Corporation | Low pressure venting panel |
EP0306836A2 (en) * | 1987-09-05 | 1989-03-15 | Flachglas Aktiengesellschaft | Window for buildings protected against explosion effect |
US5035182A (en) * | 1984-03-28 | 1991-07-30 | The United States Of America As Represented By The Secretary Of The Navy | Bending type ordnance venting device |
US5069401A (en) * | 1989-11-15 | 1991-12-03 | The Boeing Company | Compartment partition and pressure relief door therefor |
US5118053A (en) * | 1989-09-27 | 1992-06-02 | The Boeing Company | Pressure equalization systems |
WO1993002269A1 (en) * | 1991-07-17 | 1993-02-04 | Chaddesley Investments Pty. Ltd. | Transparent laminates and monolithic transparencies |
US5194688A (en) * | 1992-01-31 | 1993-03-16 | Hughes Missile Systems Company | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
US5201830A (en) * | 1990-03-15 | 1993-04-13 | Braswell Marion M | System for controlling ambient pressure within an enclosed environment |
AU659864B2 (en) * | 1991-07-17 | 1995-06-01 | Chaddesley Investments Pty Ltd | Transparent laminates and monolithic transparencies |
US5937611A (en) * | 1995-09-28 | 1999-08-17 | Howes; Stephen E. | Method of making an impact resistant window |
US5967170A (en) * | 1995-08-03 | 1999-10-19 | Imi Marston Limited | Pressure relief panels |
EP0867686A3 (en) * | 1997-03-27 | 2000-05-10 | Lockheed Martin Corporation | Device and method for sealing a munition within a canister until munition launch |
US6101783A (en) * | 1995-09-28 | 2000-08-15 | Howes; Stephen E. | Impact resistant window |
EP1065329A2 (en) * | 1999-07-02 | 2001-01-03 | Glas Trösch Holding AG | Covering element for suspended ceilings |
EP1065330A1 (en) * | 1999-07-02 | 2001-01-03 | Glas Trösch Holding AG | Cladding panel for covering a part of a building |
US6213426B1 (en) * | 1999-07-09 | 2001-04-10 | The Boeing Company | Monolithic structure with redundant load paths |
US6264141B1 (en) * | 1997-02-19 | 2001-07-24 | Mcdonnell Douglas Corporation | Aircraft decompression protection panel |
US6715245B2 (en) * | 2002-04-03 | 2004-04-06 | Signature Door Co., Inc. | Impact resistant pane and mounting |
WO2005014964A1 (en) * | 2003-07-18 | 2005-02-17 | Hamilton Erskine Limited | Improvements relating to impact-resistant structures and assemblies |
US20050224647A1 (en) * | 2004-03-23 | 2005-10-13 | Tubbs Gregory A | Insulating baffle for a floor shear truss |
US20060022088A1 (en) * | 2003-12-19 | 2006-02-02 | Francis Dazet | Aircraft nose with shield |
US20070194177A1 (en) * | 2006-02-21 | 2007-08-23 | Coak Craig E | Aircraft window assembly |
US20090159748A1 (en) * | 2007-12-20 | 2009-06-25 | Airbus Deutschland Gmbh | Decompression Device With Adjustable Release Pressure |
US8584569B1 (en) * | 2011-12-06 | 2013-11-19 | The United States Of America As Represented By The Secretary Of The Navy | Plume exhaust management for VLS |
US20140227959A1 (en) * | 2006-06-07 | 2014-08-14 | Wozair Limited | Blast Protection Damper |
US20180361833A1 (en) * | 2017-06-14 | 2018-12-20 | Gloria O. Davila | Temporary automotive window covering |
US20200180748A1 (en) * | 2018-12-11 | 2020-06-11 | Airbus Helicopters Deutschland GmbH | Foreign object impact proof windshield assembly |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2121777A (en) * | 1936-03-02 | 1938-06-28 | Bailey & Sharp Co Inc | Windowpane and method of making same |
GB513426A (en) * | 1938-04-05 | 1939-10-12 | Harry Da Costa | Improvements in pressure release devices for fluid-pressure apparatus |
US2202690A (en) * | 1938-07-07 | 1940-05-28 | Pittsburgh Plate Glass Co | Safety glass |
US2300506A (en) * | 1940-11-05 | 1942-11-03 | Pittsburgh Plate Glass Co | Window construction |
US2382963A (en) * | 1942-01-10 | 1945-08-21 | Libbey Owens Ford Glass Co | Windshield or window construction |
-
1951
- 1951-07-21 US US237957A patent/US2679467A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2121777A (en) * | 1936-03-02 | 1938-06-28 | Bailey & Sharp Co Inc | Windowpane and method of making same |
GB513426A (en) * | 1938-04-05 | 1939-10-12 | Harry Da Costa | Improvements in pressure release devices for fluid-pressure apparatus |
US2202690A (en) * | 1938-07-07 | 1940-05-28 | Pittsburgh Plate Glass Co | Safety glass |
US2300506A (en) * | 1940-11-05 | 1942-11-03 | Pittsburgh Plate Glass Co | Window construction |
US2382963A (en) * | 1942-01-10 | 1945-08-21 | Libbey Owens Ford Glass Co | Windshield or window construction |
Cited By (57)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2758042A (en) * | 1952-12-09 | 1956-08-07 | Pittsburgh Plate Glass Co | Safety glass construction |
US2721157A (en) * | 1953-01-05 | 1955-10-18 | Pittsburgh Plate Glass Co | Explosion resisting window |
US2784926A (en) * | 1953-03-30 | 1957-03-12 | Lockheed Aircraft Corp | Protected aircraft enclosures |
US2851388A (en) * | 1954-04-26 | 1958-09-09 | Mine Safety Appliances Co | Protective shield |
US3078201A (en) * | 1960-03-21 | 1963-02-19 | Midwest Research Inst | Seam structure for a flexible bag |
US3401976A (en) * | 1965-07-21 | 1968-09-17 | Renault | Sun visors for vehicles |
US3630812A (en) * | 1968-01-29 | 1971-12-28 | Saint Gobain | Windshield for motor vehicles |
US3797167A (en) * | 1972-03-07 | 1974-03-19 | F Gomboc | Fire escape window |
US3807106A (en) * | 1973-04-16 | 1974-04-30 | Eastman Kodak Co | Explosion relief wall supporting fastener |
US4067154A (en) * | 1975-02-20 | 1978-01-10 | Fike Metal Products Corporation | Instantaneous venting, non-frangible burst panel structure |
US3938764A (en) * | 1975-05-19 | 1976-02-17 | Mcdonnell Douglas Corporation | Frangible aircraft floor |
US4049221A (en) * | 1975-12-24 | 1977-09-20 | Lockheed Aircraft Corporation | Relief of inter-compartment differential pressure in aircraft |
US4390152A (en) * | 1976-05-13 | 1983-06-28 | Lockheed Corporation | Aircraft decompression vent assembly |
US4432514A (en) * | 1976-09-23 | 1984-02-21 | The Boeing Company | Decompression equalization relief valve |
US4089140A (en) * | 1976-09-24 | 1978-05-16 | Mcdonnell Douglas Corporation | Carpet installation for frangible aircraft floors |
US4248610A (en) * | 1978-08-09 | 1981-02-03 | Metallgesellschaft Aktiengesellschaft | Dust collector with pressure-relief opening |
US4498261A (en) * | 1981-12-07 | 1985-02-12 | Continental Disc Corporation | Low pressure venting panel |
US5035182A (en) * | 1984-03-28 | 1991-07-30 | The United States Of America As Represented By The Secretary Of The Navy | Bending type ordnance venting device |
EP0306836A3 (en) * | 1987-09-05 | 1990-08-29 | Flachglas Aktiengesellschaft | Window for buildings protected against explosion effect |
EP0306836A2 (en) * | 1987-09-05 | 1989-03-15 | Flachglas Aktiengesellschaft | Window for buildings protected against explosion effect |
US5118053A (en) * | 1989-09-27 | 1992-06-02 | The Boeing Company | Pressure equalization systems |
US5069401A (en) * | 1989-11-15 | 1991-12-03 | The Boeing Company | Compartment partition and pressure relief door therefor |
US5201830A (en) * | 1990-03-15 | 1993-04-13 | Braswell Marion M | System for controlling ambient pressure within an enclosed environment |
WO1993002269A1 (en) * | 1991-07-17 | 1993-02-04 | Chaddesley Investments Pty. Ltd. | Transparent laminates and monolithic transparencies |
AU659864B2 (en) * | 1991-07-17 | 1995-06-01 | Chaddesley Investments Pty Ltd | Transparent laminates and monolithic transparencies |
US5194688A (en) * | 1992-01-31 | 1993-03-16 | Hughes Missile Systems Company | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
EP0553970A2 (en) * | 1992-01-31 | 1993-08-04 | Hughes Aircraft Company | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
EP0553970A3 (en) * | 1992-01-31 | 1994-06-15 | Hughes Aircraft Co | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
US5967170A (en) * | 1995-08-03 | 1999-10-19 | Imi Marston Limited | Pressure relief panels |
US5937611A (en) * | 1995-09-28 | 1999-08-17 | Howes; Stephen E. | Method of making an impact resistant window |
US6101783A (en) * | 1995-09-28 | 2000-08-15 | Howes; Stephen E. | Impact resistant window |
US6264141B1 (en) * | 1997-02-19 | 2001-07-24 | Mcdonnell Douglas Corporation | Aircraft decompression protection panel |
EP0867686A3 (en) * | 1997-03-27 | 2000-05-10 | Lockheed Martin Corporation | Device and method for sealing a munition within a canister until munition launch |
EP1065329A2 (en) * | 1999-07-02 | 2001-01-03 | Glas Trösch Holding AG | Covering element for suspended ceilings |
EP1065330A1 (en) * | 1999-07-02 | 2001-01-03 | Glas Trösch Holding AG | Cladding panel for covering a part of a building |
EP1065329A3 (en) * | 1999-07-02 | 2001-02-21 | Glas Trösch Holding AG | Covering element for suspended ceilings |
US6213426B1 (en) * | 1999-07-09 | 2001-04-10 | The Boeing Company | Monolithic structure with redundant load paths |
US6443392B2 (en) | 1999-07-09 | 2002-09-03 | The Boeing Company | Monolithic structure with redundant load paths |
US6715245B2 (en) * | 2002-04-03 | 2004-04-06 | Signature Door Co., Inc. | Impact resistant pane and mounting |
US20070011962A1 (en) * | 2003-07-18 | 2007-01-18 | Erskine James H | Relating to impact-resistant structures and assemblies |
US7793581B2 (en) | 2003-07-18 | 2010-09-14 | Hamilton Erskine Limited | Relating to impact-resistant structures and assemblies |
WO2005014964A1 (en) * | 2003-07-18 | 2005-02-17 | Hamilton Erskine Limited | Improvements relating to impact-resistant structures and assemblies |
US20060022088A1 (en) * | 2003-12-19 | 2006-02-02 | Francis Dazet | Aircraft nose with shield |
US7384015B2 (en) * | 2003-12-19 | 2008-06-10 | Airbus France Sa | Aircraft nose with shield |
US7007892B2 (en) * | 2004-03-23 | 2006-03-07 | The Boeing Company | Insulating baffle for a floor shear truss |
US20050224647A1 (en) * | 2004-03-23 | 2005-10-13 | Tubbs Gregory A | Insulating baffle for a floor shear truss |
US20070194177A1 (en) * | 2006-02-21 | 2007-08-23 | Coak Craig E | Aircraft window assembly |
US7552896B2 (en) * | 2006-02-21 | 2009-06-30 | The Boeing Company | Aircraft window assembly |
US20140227959A1 (en) * | 2006-06-07 | 2014-08-14 | Wozair Limited | Blast Protection Damper |
US9920871B2 (en) * | 2006-06-07 | 2018-03-20 | Wozair Limited | Blast protection damper |
US20090159748A1 (en) * | 2007-12-20 | 2009-06-25 | Airbus Deutschland Gmbh | Decompression Device With Adjustable Release Pressure |
US8201775B2 (en) * | 2007-12-20 | 2012-06-19 | Airbus Deutschland Gmbh | Improved decompression device with adjustable release pressure |
US8584569B1 (en) * | 2011-12-06 | 2013-11-19 | The United States Of America As Represented By The Secretary Of The Navy | Plume exhaust management for VLS |
US20180361833A1 (en) * | 2017-06-14 | 2018-12-20 | Gloria O. Davila | Temporary automotive window covering |
US10414249B2 (en) * | 2017-06-14 | 2019-09-17 | Gloria O. Davila | Temporary automotive window covering |
US20200180748A1 (en) * | 2018-12-11 | 2020-06-11 | Airbus Helicopters Deutschland GmbH | Foreign object impact proof windshield assembly |
US11827332B2 (en) * | 2018-12-11 | 2023-11-28 | Airbus Helicopters Deutschland GmbH | Foreign object impact proof windshield assembly |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2679467A (en) | Pressure blowout safety closure | |
US2358143A (en) | Vented panel | |
US2356878A (en) | Vehicular glazing construction | |
CN101282835B (en) | Laminated glass pane having an integrated retaining element | |
FR2447273B1 (en) | ||
IE39350B1 (en) | Fire resistant panels | |
GB882003A (en) | Laminated parts | |
US2721157A (en) | Explosion resisting window | |
US5885714A (en) | Laminated safety glass | |
EP1500537B1 (en) | Glass pane for vehicles | |
ATE253168T1 (en) | FIRE-RESISTANT SURFACE ELEMENT WITH AT LEAST TWO TRANSLUCENT FIRE PROTECTION GLASS PANELS | |
US3112535A (en) | Explosion venting construction for buildings | |
US5853835A (en) | Laminated and beveled safety glass panel | |
AU748032B2 (en) | Collapsible panel and method for controlled collapsing thereof | |
JPH0840747A (en) | Fireproof glass | |
WO2013091876A1 (en) | Bursting element for an explosion-prone installation | |
EP0692601B1 (en) | Improved wing particularly designed for application to boxes and casings for fire extinguishers, fire plugs and antifire and antiaccident items | |
GB756170A (en) | Improvements in or relating to laminated transparent structure adapted to function as a safety closure rupturable under shock | |
US20020011541A1 (en) | Collapsible panel and method for controlled collapsing thereof | |
JPH03506056A (en) | bulletproof glass | |
US6454038B2 (en) | Collapsible panel and method for controlled collapsing thereof | |
US2301365A (en) | Pressure relief vent | |
US2137439A (en) | Window assembly | |
DE718405C (en) | Polarizing filter | |
US2741306A (en) | Window panel storm covering for doors and the like |