GB2306389A - Composite wood panel - Google Patents
Composite wood panel Download PDFInfo
- Publication number
- GB2306389A GB2306389A GB9611554A GB9611554A GB2306389A GB 2306389 A GB2306389 A GB 2306389A GB 9611554 A GB9611554 A GB 9611554A GB 9611554 A GB9611554 A GB 9611554A GB 2306389 A GB2306389 A GB 2306389A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wood
- layers
- panel
- layer
- pressure
- 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.)
- Withdrawn
Links
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
- B32B21/00—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
- B32B21/14—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood board or veneer
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/10—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of wood
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- 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
- B32B21/00—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
- B32B21/04—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B21/042—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood as the main or only constituent of a layer, which is next to another layer of the same or of a different material of wood
-
- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/26—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
-
- 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
- B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
- B32B2309/02—Temperature
- B32B2309/022—Temperature vs pressure profiles
-
- 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
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/12—Copper
-
- 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
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/24—Aluminium
-
- 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
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/30—Iron, e.g. steel
-
- 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
- B32B2605/00—Vehicles
- B32B2605/003—Interior finishings
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Wood Science & Technology (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
A composite wood panel includes a plurality of wood layers (12, 16) formed from medium density tropical hardwoods and one or more metal layers (14). Sheets of thermosetting phenolic adhesive interleave the wood and metal layers (12-16). The assembled board has considerably higher strength and less weight than corresponding wood boards.
Description
COMPOSITE WOOD PANEL
The present invention relates to a composite wood panel and to a method of producing such a panel.
Composite wood panels have been used for some time in applications which require high strength and durability.
However, in cases where the panelling is to be subjected to large stresses and wear, such as in railway carriage applications and the like, the panelling must be thick to provide reasonable performance. Thick panelling has inherent disadvantages of high weight and large volume.
The present invention seeks to provide improved wood panelling.
According to an aspect of the present invention, there is provided, a composite wood panel comprising a plurality of wood veneer layers and one or more metal layers, at least one of the wood layers being formed from a medium density tropical hardwood or similar wood. Preferably all the wood layers are formed from a medium density tropical hardwood or similar wood. Other species of wood may be used in applications which do not require chemical impregnation before manufacture of the panel.
According to another aspect of the present invention, there is provided a method of producing a composite wood panel including the steps of forming a balanced assembly of layers and binding the assembly under high heat and pressure.
According to another aspect of the present invention, there is provided a method of producing a composite wood panel including the steps of forming a balanced assembly of layers and interleaving the layers with sheets of phenolic thermosetting adhesive.
The preferred embodiment provides a composite structural panel which can combine the advantages of medium density wood fibre, metals, chemicals and phenolics to provide a panel with additional strength, stability and durability, and which has improved thermal/heat reflection insulation properties, and including improved sound insulation. By reducing the thickness of individual veneer layers and the quantity of metal and chemicals, the panel can be made light-weight and approximately twice the strength of equivalent base panels without reinforcement.
The panel is preferably fire and rot-proof treated to improve its properties and durability.
Typical applications for the panel include internal walls, bulkheads, ceilings, body side linings, seats, doors and floors and external doors for railway carriages and locomotives and also for other public transport vehicles such as buses and the like.
An embodiment of the present invention is described below, by way of example only, with reference to the accompanying drawing, in which the sole Figure is a cross-sectional view of an embodiment of composite wood board.
Referring to the Figure, the embodiment of panel shown is formed of five layers, four of which can be said to be matching layers. The relative thicknesses of the layers will vary in dependence upon the application and will vary from the indications given in the Figure.
The central layer 16 is a wood veneer layer which may be formed from a single sheet of veneer or from a plurality of sheets, in accordance with requirements for the application in question. The preferred veneer is obtained from medium density tropical hardwoods, for example of mahogany type, or from similar woods. Woods from Africa and South America have been found to have the most desirable properties. The preferred woods are of medium density of certain texture so as to have reasonable flexibility and have relatively short grain. This combination retains the flexibility of the panel and facilitates impregnation of the wood with phenolic adhesive, fire retardants, rot-proofing chemicals, as is described in further detail below.
Each veneer layer preferably has a thickness of between 1.2 millimetres and 3.2 millimetres. The metal layers 14 may have similar thicknesses.
The preferred woods have a density preferably between 600 kg/m3 and 670 kg/m3 (between 38 and 42 lb/ft3), although woods with a density between 560 kg/m3 and 720 kg/m3 (between 35 and 45 lb/ft3) could also be used. These figures are given at 12 moisture content.
Each side of the central layer 16 is covered by a thin metal layer 14 of, for example, aluminium, stainless steel, copper or the like. The metal layers 14 are in turn covered by wood veneer outer layers 12 which may or may not be of the same wood as the central layer 16, in dependence upon the application.
The metal layers 14 can also be applied on the exterior surfaces of the panel or in certain applications in an unbalanced construction with a metal layer 14 exposed on one surface and the opposite side metal layer 14 overlaid by veneer to allow for bonding of other surface materials, decorative laminates or other layers. Also for the purposes of applying sound proofing suitable chemicals may be bonded or sprayed on the wood veneer surface on one side thereof.
The metal layers 16 and the wood layers 12, 16 are substantially matched for flexibility such that the wood layers 12, 16 can retain the flexibility of the metal layers 14 in expansion and contraction.
The strength and integrity of the panel is obtained by careful manufacture. In the preferred embodiment, after careful selection of the raw wood, which is of the type mentioned above, veneers are produced by cutting on the basis of a loosely rotary cut. The cutting knife is preferably set at an angle to separate the wood fibres slightly, which enhances flexibility of the veneer, and absorption of adhesives such as phenolic adhesives and impregnation of fire retardant and rot-proofing chemicals, thereby bonding of the various layers to one another. All of the veneer layers of the panel are preferably produced in this manner.
The veneer layers are then pressure impregnated with chemicals either in the body or glue-line of the veneer so as to rot-proof and fire-proof the wood. The preferred fire retardant properties are ignition "nil" and "nil" spread of flame for up to 20 minutes, which would meet the specifications for public transport vehicles.
The thin metallic sheets 14 are then assembled under the face veneer layers 12, each layer being interlaid with a thermosetting adhesive, preferably a phenolic thermosetting impregnated paper adhesive. This adhesive is produced in the form of thin flexible sheets which have the appearance of
Bakelite (TM) and can be rolled onto the veneer layers and pressed onto them at high temperatures for bonding.
Alternatively, thin metallic sheets 14 or decorative and plain finish melamine laminates can be provided on the outer face of the panel for particular exterior finishes.
In the preferred embodiment, the layers of the panel are in balance through the panel, that is symmetrical about the central plane of the panel, to maintain equal stresses on each side, both during and after manufacture.
The assembled layers are then loaded into hot presses and compressed at a pressure of, for example, around 1.7 bar (around 250 psi) at a temperature preferably not less than around 1370C (around 2800F) and most preferably between around 1370C to around 1490C (around 280 to around 3000F).
The adhesive forms a gel and is fused into the fibres of the veneer layers, while the paper carrier acts as a web to assist in binding the layers together. At the same time, the adhesive bonds the metal layers 14 under the extreme heat and pressure of the presses all in one operation.
Adhesive impregnation, hence binding, can be improved by ensuring that the veneers have a moisture content of not less than about 6% and not more than about 8%.
In order to maintain even strength across the whole of a panel, should the size of the panel be too large to be able to be made from single sheets of material for each layer, a plurality of sheets are used but without scarf joints.
Splice joints are preferably used.
The thermosetting phenol impregnated paper adhesive used in the preferred embodiment provides fire retardant qualities to the panel and is thus advantageously also to be used as a covering over the outer veneer layers 12. It can also serve as a finishing product for the panel, to receive by exterior application, painted or glued, other materials such as rubber or vinyl, floor covering for railway carriages, locomotives and buses.
Where other exterior finishes are desired and liquid adhesives are applied to secure the bonding of plain finish or decorative laminates unsuitable for hot thermosetting bonding, the outer veneers of the panel are left exposed as raw-wood fibre to provide a key for bonding purposes.
Before application and fixing of the manufactured panel, all edges and holes are sealed with water repellent preservative liquid to prevent absorption of moisture and weakening of wood fibre.
Claims (17)
1. A composite wood panel comprising a plurality of wood veneer layers and one or more metal layers, at least one of the wood layers being formed from a medium density tropical hardwood or similar wood.
2. A panel according to claim 1, wherein all the wood layers are formed from a medium density tropical hardwood or similar wood.
3. A panel according to claim 1 or 2, wherein each wood layer has a thickness between 1.2 and 3.2 millimetres.
4. A panel according to any preceding claim, wherein each wood layer is formed from a wood having a density between 560 and 720 kg/m3, measured at 12 moisture content.
5. A panel according to claim 1, 2 or 3, wherein each wood layer is formed from a wood having a density between 600 and 670 kg/m3, measured at 12 moisture content.
6. A panel according to any preceding claim, wherein the metal layer or layers are formed of aluminium, stainless steel or copper.
7. A panel according to any preceding claim, comprising a thermosetting adhesive sheet bonding each pair of facing layers to one another.
8. A panel according to claim 7, wherein the thermosetting sheet is a phenolic adhesive sheet.
9. A method of producing a composite wood panel including the steps of forming a balanced assembly of layers and binding the assembly under high heat and pressure.
assembly under high heat and pressure.
10. A method of producing a composite wood panel including the steps of forming a balanced assembly of layers and interleaving the layers with sheets of phenolic thermosetting adhesive.
11. A method according to claim 9 or 10, comprising the step of forming the or each wood layer by a loosely rotary cut.
12. A method according to claim 11, wherein the or each wood layer is cut at an angle which separates the wood fibres at the surface of the wood layer.
13. A method according to any one of claims 9 to 12, wherein the assembled layers are treated in hot presses at a pressure of around 1.7 bar.
14. A method according to claim 13, wherein the assembled layers are treated in hot presses at a pressure not less than around 1370C.
15. A method according to claim 13 or 14, wherein the assembled layers are treated in hot presses at a pressure between 1370C and 1490C.
16. A composite wood panel substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings.
17. A method of forming a composite wood panel substantially as hereinbefore described with reference to the accompanying drawing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9521117.3A GB9521117D0 (en) | 1995-10-16 | 1995-10-16 | Composite wood panel |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9611554D0 GB9611554D0 (en) | 1996-08-07 |
GB2306389A true GB2306389A (en) | 1997-05-07 |
Family
ID=10782338
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB9521117.3A Pending GB9521117D0 (en) | 1995-10-16 | 1995-10-16 | Composite wood panel |
GB9611554A Withdrawn GB2306389A (en) | 1995-10-16 | 1996-06-03 | Composite wood panel |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB9521117.3A Pending GB9521117D0 (en) | 1995-10-16 | 1995-10-16 | Composite wood panel |
Country Status (2)
Country | Link |
---|---|
GB (2) | GB9521117D0 (en) |
ZA (1) | ZA966990B (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001040598A1 (en) * | 1999-12-03 | 2001-06-07 | Cambridge Building Technology Limited | A structural component |
GB2358372A (en) * | 2000-01-24 | 2001-07-25 | Chia Shun Liu | Laminated plywood structure |
WO2002007938A1 (en) * | 2000-07-11 | 2002-01-31 | Votteler Lackfabrik Gmbh & Co. Kg | Method for producing veneered compressed parts |
WO2004071764A1 (en) * | 2003-02-14 | 2004-08-26 | Kronotec Ag | Building board |
EP1621332A1 (en) * | 2004-07-30 | 2006-02-01 | Fritz Egger GmbH & Co | Laminate, building material with a laminate and manufacturing method thereof |
FR2883798A1 (en) * | 2005-04-04 | 2006-10-06 | Skywoods Sarl | Decorative panel for e.g. interior fitting of cabin of e.g. executive jet airplane, has two layers with facing side made up of wood and central core made up of aluminum provided between facing side and back layer made up of peeled wood |
EP1958765A1 (en) * | 2007-02-15 | 2008-08-20 | Julien Waumans | Floor for sports facilities |
ITMO20080330A1 (en) * | 2008-12-24 | 2010-06-25 | Mariano Paganelli | PROCEDURE FOR REALIZING HIGH RESISTANCE TILES FOR THE COATING OF FLOORS AND WALLS, INSIDE OR OUTSIDE. |
ITUD20100032A1 (en) * | 2010-02-22 | 2011-08-23 | Mattellone S R L | MULTILAYERED MATERIAL AND RELATIVE PROCEDURE OF REALIZATION |
EP2256265A3 (en) * | 2009-05-22 | 2012-02-15 | Silvestri & associati-Studio Tecnico | Insulated multilayer sandwich panel |
US8877319B1 (en) * | 2013-07-29 | 2014-11-04 | Po Ming Huang | Multi-layer composite structure |
FR3011505A1 (en) * | 2013-10-09 | 2015-04-10 | Jean-Luc Chanel | STRUCTURAL PANEL, IN PARTICULAR, FOR CARRYING OUT VEHICLES AND HABITATS |
US20160311194A1 (en) * | 2015-04-23 | 2016-10-27 | Goodrich Corporation | Flexible veneer panel with metal mesh layer |
US11525226B2 (en) * | 2019-07-01 | 2022-12-13 | Goodrich Corporation | Thermally layered fire treated veneer panel |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB433824A (en) * | 1934-07-07 | 1935-08-21 | Venesta Ltd | Improvements in or relating to composite sheets |
GB1043851A (en) * | 1962-02-05 | 1966-09-28 | Union Carbide Corp | Improvements in and relating to resins |
GB1460570A (en) * | 1973-03-20 | 1977-01-06 | Laser Eng Ltd | Musical percussion instruments |
-
1995
- 1995-10-16 GB GBGB9521117.3A patent/GB9521117D0/en active Pending
-
1996
- 1996-06-03 GB GB9611554A patent/GB2306389A/en not_active Withdrawn
- 1996-08-16 ZA ZA9606990A patent/ZA966990B/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB433824A (en) * | 1934-07-07 | 1935-08-21 | Venesta Ltd | Improvements in or relating to composite sheets |
GB1043851A (en) * | 1962-02-05 | 1966-09-28 | Union Carbide Corp | Improvements in and relating to resins |
GB1460570A (en) * | 1973-03-20 | 1977-01-06 | Laser Eng Ltd | Musical percussion instruments |
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001040598A1 (en) * | 1999-12-03 | 2001-06-07 | Cambridge Building Technology Limited | A structural component |
GB2358372A (en) * | 2000-01-24 | 2001-07-25 | Chia Shun Liu | Laminated plywood structure |
WO2002007938A1 (en) * | 2000-07-11 | 2002-01-31 | Votteler Lackfabrik Gmbh & Co. Kg | Method for producing veneered compressed parts |
US7037401B2 (en) | 2000-07-11 | 2006-05-02 | Votteler Lackfabrik Gmbh & Co. Kg | Method for producing veneered compressed parts |
WO2004071764A1 (en) * | 2003-02-14 | 2004-08-26 | Kronotec Ag | Building board |
US7651751B2 (en) | 2003-02-14 | 2010-01-26 | Kronotec Ag | Building board |
EP1621332A1 (en) * | 2004-07-30 | 2006-02-01 | Fritz Egger GmbH & Co | Laminate, building material with a laminate and manufacturing method thereof |
FR2883798A1 (en) * | 2005-04-04 | 2006-10-06 | Skywoods Sarl | Decorative panel for e.g. interior fitting of cabin of e.g. executive jet airplane, has two layers with facing side made up of wood and central core made up of aluminum provided between facing side and back layer made up of peeled wood |
WO2006106232A2 (en) * | 2005-04-04 | 2006-10-12 | Skywoods (Sarl) | Novel decorative panel based on wood, for interior design |
WO2006106232A3 (en) * | 2005-04-04 | 2007-01-11 | Skywoods Sarl | Novel decorative panel based on wood, for interior design |
EP1958765A1 (en) * | 2007-02-15 | 2008-08-20 | Julien Waumans | Floor for sports facilities |
WO2008099011A1 (en) * | 2007-02-15 | 2008-08-21 | Julien Waumans | Floor for sports facilities |
ITMO20080330A1 (en) * | 2008-12-24 | 2010-06-25 | Mariano Paganelli | PROCEDURE FOR REALIZING HIGH RESISTANCE TILES FOR THE COATING OF FLOORS AND WALLS, INSIDE OR OUTSIDE. |
US8557083B2 (en) | 2008-12-24 | 2013-10-15 | Mariano Paganelli | Process for realising high-resistance slabs or tiles, destined for covering internal or external floors or walls |
RU2533794C2 (en) * | 2008-12-24 | 2014-11-20 | Мариано ПАГАНЕЛЛИ | Production of high-durability boards or tiles for coating of indoor or outdoor floors or walls and high-durability hardness |
EP2650454A1 (en) * | 2008-12-24 | 2013-10-16 | Mariano Paganelli | A process for realising high-resistance slabs or tiles, destined for covering internal or external floors or walls |
WO2010072704A1 (en) * | 2008-12-24 | 2010-07-01 | Mariano Paganelli | A process for realising high-resistance slabs or tiles, destined for covering internal or external floors or walls |
EP2256265A3 (en) * | 2009-05-22 | 2012-02-15 | Silvestri & associati-Studio Tecnico | Insulated multilayer sandwich panel |
CN102844180A (en) * | 2010-02-22 | 2012-12-26 | 马特洛尼有限责任公司 | Multi-layer material and relative method of production |
WO2011101735A1 (en) | 2010-02-22 | 2011-08-25 | Mattelone Srl | Multi-layer material and relative method of production |
ITUD20100032A1 (en) * | 2010-02-22 | 2011-08-23 | Mattellone S R L | MULTILAYERED MATERIAL AND RELATIVE PROCEDURE OF REALIZATION |
US9296181B2 (en) | 2010-02-22 | 2016-03-29 | Mattellone Srl | Multi-layer material and relative method of production |
US8877319B1 (en) * | 2013-07-29 | 2014-11-04 | Po Ming Huang | Multi-layer composite structure |
FR3011505A1 (en) * | 2013-10-09 | 2015-04-10 | Jean-Luc Chanel | STRUCTURAL PANEL, IN PARTICULAR, FOR CARRYING OUT VEHICLES AND HABITATS |
US20160311194A1 (en) * | 2015-04-23 | 2016-10-27 | Goodrich Corporation | Flexible veneer panel with metal mesh layer |
US10814582B2 (en) * | 2015-04-23 | 2020-10-27 | Goodrich Corporation | Flexible veneer panel with metal mesh layer |
US11525226B2 (en) * | 2019-07-01 | 2022-12-13 | Goodrich Corporation | Thermally layered fire treated veneer panel |
Also Published As
Publication number | Publication date |
---|---|
GB9521117D0 (en) | 1995-12-20 |
ZA966990B (en) | 1997-02-24 |
GB9611554D0 (en) | 1996-08-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |