WO2000066358A2 - Reinforced structural foam article and method for making same - Google Patents
Reinforced structural foam article and method for making same Download PDFInfo
- Publication number
- WO2000066358A2 WO2000066358A2 PCT/US2000/011007 US0011007W WO0066358A2 WO 2000066358 A2 WO2000066358 A2 WO 2000066358A2 US 0011007 W US0011007 W US 0011007W WO 0066358 A2 WO0066358 A2 WO 0066358A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- article
- foam layer
- layer
- skin
- reinforcing
- Prior art date
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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
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/02—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C41/04—Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
- B29C41/06—Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould about two or more axes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/02—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C41/20—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. moulding inserts or for coating articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
- B29C70/323—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core on the inner surface of a rotating mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
- B29C70/323—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core on the inner surface of a rotating mould
- B29C70/326—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core on the inner surface of a rotating mould by rotating the mould around its axis of symmetry
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/065—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
- B29K2105/043—Skinned foam
-
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- 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
- B32B2323/00—Polyalkenes
- B32B2323/04—Polyethylene
Definitions
- the present invention relates generally to field of reinforced foam or sheet structures, particularly to articles which may be used for structural, transportation, container, armor and similar purposes made of a reinforced shock and energy absorbing material. Still more particularly, the invention relates to a structural foam article including a reinforcing layer or members imbedded therein.
- tough support material examples include containers, mechanical supports, and transport or material handling components.
- stretchers, cargo handling articles, and the like must typically offer good load support and durability in relatively light-weight structures.
- Many such structures are presently made of wood or an assembly of different materials which, when combined, provide the needed mechanical properties with reduced weight.
- existing structures often do not provide a desired degree of structural stiffness and toughness to resist loading, impact, and marring during use. Moreover, the strength-to-weight properties of materials such as plywood, used in many material handling applications, may be less than desired, ultimately reducing the net load which can be handled.
- existing composite structures and assemblies including plastics, metal, cloth, and molded or assembled resinous articles, often require timely manufacturing, assembly and finishing operations, and offer only limited design flexibility in terms of contours, integral handles, and similar features.
- the present invention provides a technique for forming a reinforced structural foam article designed to respond to these needs.
- the article may take any suitable form, and the technique is particularly well suited to the creation of tough, load-bearing and impact- resistant articles.
- the invention is useful for fashioning body armor, vehicle armor, protective clothing, protective and energy absorbing clothing inserts, and so forth.
- the inventive technique provides tough, light-weight transport articles (e.g. stretchers, load spreaders), protective shelters, and so forth.
- Articles fabricated in accordance with the invention may be based upon reinforcement by a variety of means, such as rigid structural members or a strong fabric layer embedded in a structural foam composite.
- the structural foam may be formed by a variety of techniques, such as rotational molding.
- the articles may be conformed to specific desired contours to respect space and configuration constraints of specific applications. In the case of personal armor, the articles may follow body contours of users.
- the forms may be designed to facilitate their assembly in vehicles or containers, or their integration with other elements of a container or material handling system.
- the technique allows for the formation of articles including at least one outer skin layer, and a foam layer extending from the skin layer.
- the reinforcing elements, members or layer is embedded in the article, at least partially in the foam layer.
- the articles may include outer skin layers on both sides of the foam layer, or skin layers that completely envelope the foam layer.
- the reinforcement may be partially or completely embedded in the article.
- Figure 1 is a sectional perspective view of a reinforced structural foam article illustrating the various layers of the article in one exemplary configuration
- Figure 2 is a sectional illustration of a pair of molds used to form an article such as that illustrated in Figure 1 ;
- Figure 3 is a detailed view of the interior of the molds shown in Figure 2 during the molding process used to form the article;
- Figure 4 is a detailed view like that of Figure 3, showing the growth of a structural foam layer which will embed the reinforcing layer of the structure;
- Figure 5 is a flow chart illustrating exemplary steps in the creation of an article such as that shown in Figure 1 through the progressive steps illustrated in Figures 3 and
- Figure 6 is a sectional view of a further embodiment of a reinforced article in which a rigid framework is embedded within a molded body
- Figure 7 is a partial sectional view of a reinforced structural article in which a fitting or similar connector element is received.
- Figure 8 is a partial sectional view through an alternative configuration of a reinforced article in which structures are provided for receiving fasteners used to attach the article into an assembly or subassembly.
- a reinforced structural foam article designated generally by the reference numeral 10
- a reinforced structural foam article is illustrated as including a first skin layer 12, a second skin layer 14, and first and second portions 16 and 18 of a structural foam layer therebetween.
- a reinforcing layer 20 is embedded in the article in contact with the first and second structural foam layer portions 16 and 18.
- the article thus presents an inner surface 22 along the exterior of skin layer 12 and an outer surface 24 defining layer 14.
- the internal surfaces of skin layers 12 and 14, namely surfaces 26 and 28, respectively, are integral with the portions 16 and 18 of the structural foam layer to provide good adherence of the structural foam layer to the skin layers.
- the article 10 includes outer skin layers 12 and 14 which bound the foam layer on both sides thereof, the skin layers need not be identical to one another, and where desired, one of the skin layers may be eliminated entirely.
- the reinforcing layer 20, which may include various structures, members, fabrics, and so forth as described in greater detail below, is then embedded in the foam layer either completely or partially (e.g., the reinforcing layer or elements may extend to the outer surface of the article, such as through a skin layer).
- Skin layers 12 and 14, and the structural foam layer defined by portions 16 and 18 may be made of any suitable moldable material, such as polyethylene.
- the skin layers and the structural foam layer are made of similar materials to facilitate their processing and homogeneous bonding and, where appropriate, recycling.
- these layers may be made of a non-crosslinked polyethylene available commercially from various sources, such as Exxon Chemical Canada, under the designation Escorene.
- the structural foam layer includes a blowing or foaming agent in admixture with the moldable plastic material to produce the structural foam body. Any suitable blowing agent may be employed for this purpose, such as an agent commercially available from Bayer Corp. of Pittsburgh, Pennsylvania or Uniroyal Chemical Co.
- any suitable material may be used for reinforcing layer 20.
- flexible materials are preferred, such as fabrics made of high tensile strength, tough materials, such as materials available under the commercial designations Kevlar and Spectra.
- the reinforcing layer may include rigid or substantially rigid structural members, such as plates, beams, standoffs, and so forth. Such reinforcing elements may be linked to one another to form a grid work or framework for adding the desired mechanical properties to the composite article. Where desired, both rigid and flexible reinforcing elements may be provided. It should also be noted that, while in the described embodiment a single reinforcing layer is illustrated, multiple plies of such materials may be employed. Moreover, where the materials have directional properties, the plies may vary in orientation to provide additional resistance to puncture and enhanced energy absorption. Similarly, such layers may be spaced or offset from a center line of the article, as illustrated in the figures, or may lie generally along the center line. Where appropriate, the layers may be positioned adjacent to one or both of the skin layers.
- Figure 2 illustrates an exemplary configuration for molds or dies used to form the article of Figure 1.
- the mold assembly designated generally by reference numeral 30, includes first and second mold halves 32 and 34, which may be brought together and joined to surround a mold cavity 36.
- the mold cavity is bounded by interior surfaces 38 and 40 which, in the illustrated embodiment, define the contours of inner and outer surfaces 22 and 24 (see Figure 1) of the resulting article.
- surfaces 38 and 40 may define a partial or full chest plate such that the molded article fits a generalized or customized contour of a wearer of a resulting body armor article.
- the contours defined by these surfaces may define panels for use in such applications as vehicle armor, helmets, load bearing members, stretchers, shields, shelter components, and so forth.
- mold halves 32 and 34 are brought together and the reinforcing layer is held within the mold by any acceptable manner.
- mold halves 32 and 34 present retention surfaces 42 which are brought to bear on a reinforcing sheet material or fabric 20 to hold the material within the mold.
- the material preferably only partially divides the cavity 36 to prevent the free flow of moldable plastic material around the reinforcing material during the molding process.
- Alternative arrangements for enabling such material flow might include openings in the reinforcing material, openings adjacent to the edges of the mold, and so forth.
- Figure 1 When the material is fixed within the mold, force is exerted on the mold halves, as illustrated by arrows 44 in Figure 2, to hold the reinforcing layer securely within the mold during the molding process.
- force may be exerted by any appropriate clamp, fastener assembly, and so forth.
- the article of Figure 1 may be formed by any suitable molding process, in a presently preferred embodiment, the article is formed by rotational molding to create a skin-foam-skin cross-sectional structure in which the reinforcing layer, fabric or rigid framework is embedded.
- Figures 3 and 4 illustrate the progressive formation of the structural foam material with the embedded reinforcing layer. This process may be carried out through exemplary steps in Figure 5.
- the molding process represented generally by the reference numeral 100 in Figure 5, begins at step 102 where the reinforcing layer is secured in the mold. Again, this may be accomplished in any suitable manner, such as by retaining the peripheral edge of the reinforcing layer as shown in Figure 2.
- the mold is closed and secured.
- a skin layer charge of moldable plastic material is injected into the mold cavity 36. This charge will generally include a sufficient quantity of material to form the inner and outer skin layers as the mold and forming article are heated and rotated. Thus, the particular composition and volume of the charge will depend upon the configuration and size of the article being molded.
- the mold along with the reinforcing material and the skin layer charge, is heated and rotated.
- this rotational molding process includes insertion of the mold into a rotational molding oven which is heated to a sufficient temperature to melt the plastic charge within the mold.
- the mold is rotated during such heating, generally along three orthogonal axes to promote flow of the plastic material around the mold cavity to form the skin layers.
- the speed of rotation, the combination of rotation about the orthogonal axes, dwell times, and so forth, will depend upon such factors as the geometry of the article, the desired thickness of the skin layers, and so forth.
- FIG 3 illustrates in section the growth of skin layers 12 and 14 during the heating and rotating of step 108.
- the plastic charge is melted along the interior surfaces 38 and 40 of the mold, and begins to accumulate, filling the mold cavity from these surfaces in an inward direction.
- the skin layers continue to grow as indicated by arrows 46 in Figure 3, until substantially all of the first charge is fused.
- the foam layer charge is then injected into the mold.
- this foam layer charge may include any suitable plastic material, which may be identical to the plastic material used to form the skin layers.
- the foam layer charge includes a blowing agent which promotes the creation of a structural foam during the molding process.
- the mold is then heated and rotated as indicated at step 112.
- step 112 the particular rotation, temperatures, dwell times, and so forth, involved in step 112 will vary depending upon the type and configuration of the article being formed.
- the structural foam layers continue to form along the skin layers until the entire mold cavity 36 is filled, as indicated by arrows 48 in Figure 4.
- the structural foam layer surrounds, secures and embeds the reinforcing layer in place within the article.
- the mold is cooled and the article is removed from the mold as indicated at step 114 in Figure 5. Finally, the article may be trimmed and assembled with other materials, subassemblies, structures, and the like, as indicated at step 116.
- the reinforced structural foam article of the present invention may include rigid or semi-rigid members provided either independently or in a grid work or framework.
- Figure 6 illustrates a configuration in accordance with this aspect of the present technique.
- a reinforced article 120 includes a first skin layer 12, a second skin layer 14, and first and second portions of a foam layer 16 and 18, formed in accordance with the foregoing discussion.
- a reinforcing member, designated generally by reference numeral 122, is provided within the article, at least partially embedded within the foam layer defined by portions 16 and 18.
- the reinforcing member includes a series of reinforcing elements
- standoffs 126 space the members from the skin layer 14, while intermediate standoffs 128 space the members from one another.
- standoffs may be provided on one or both sides of the article, or may be eliminated where sufficient positioning is obtained through other means (e.g., support within the mold, fusible standoffs, etc.).
- reinforcing member 122 along with other such members, where desired, is supported within a mold, and the mold is closed to receive charges of moldable plastic material.
- the mold receives a charge for forming skin layers 12 and 14, followed by a rotation and heating of the mold to create the skin layers.
- interstices between the components forming the reinforcing member 122 are substantially filled by either the skin layers or by the structural foam layer.
- the article is then removed from the mold after the desired cure period.
- FIG. 7 For integration of the reinforced structural foam article of the present technique into larger assemblies or structures, various reinforcing and assembly fittings may be provided as illustrated in Figures 7 and 8.
- a reinforced article 130 including a fastener system
- the fastener system of Figure 7 is specifically adapted for providing secure passage of an attachment article through the reinforced structure following molding.
- Article 130 of Figure 7 thus includes, by way of example, a bushing 132 which is molded within the article in accordance with the foregoing procedure. That is, the bushing is fitted into the mold and remains in place through formation of the skin layers 12 and 14, and the first and second portions of the foam layers 16 and 18.
- a reinforcing layer 20 is provided, although rigid frameworks such as that illustrated in Figure 6 may also be included, or may replace the layer 20 of Figure 7.
- bushing 132 includes a flange 134 at one end thereof, and a threaded sleeve 136 extending from the flange. Internal threads
- sleeve 136 are provided on sleeve 136 for receiving an insert 140 which, itself, has a threaded outer surface 142.
- FIG. 8 A further alternative fastening system is illustrated in Figure 8 for a reinforced article 144.
- Figure 8 illustrates two exemplary external fastener types, designed specifically to receive fasteners which do not extend fully through the article.
- a winged insert system 146 is provided, while in a further alternative, a flanged insert system 148 is used. Either system is designed to receive a threaded fastener such as a screw or bolt 150.
- winged system 148 a series of radially-extending wings 152 are provided for preventing rotational displacement of a sleeve 154 embedded within the reinforced article.
- Sleeve 154 is supported within the mold and embedded within the article as described above with respect to the system of Figure 7. Thereafter, fastener 150 may be secured within the sleeve and substantial torque applied to the fastener without displacement or pull out of the sleeve from the article.
- a front flange 156 is formed on an insert sleeve 158, in addition to a rear flange 160.
- Front and rear flanges 156 and 160 offer substantial resistance to pull out of the insert during assembly of the article with other components.
- the features of the winged system 146 and flange system 148 may be combined to provide enhanced resistance to rotation and pull out.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU67463/00A AU6746300A (en) | 1999-04-30 | 2000-04-24 | Reinforced structural foam article and method for making same |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13204399P | 1999-04-30 | 1999-04-30 | |
US60/132,043 | 1999-04-30 | ||
US54134600A | 2000-04-03 | 2000-04-03 | |
US09/541,346 | 2000-04-03 |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2000066358A2 true WO2000066358A2 (en) | 2000-11-09 |
WO2000066358A3 WO2000066358A3 (en) | 2001-03-15 |
WO2000066358A9 WO2000066358A9 (en) | 2002-02-21 |
Family
ID=26830042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2000/011007 WO2000066358A2 (en) | 1999-04-30 | 2000-04-24 | Reinforced structural foam article and method for making same |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU6746300A (en) |
WO (1) | WO2000066358A2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1358988A1 (en) * | 2002-04-30 | 2003-11-05 | Gesikat Ltd. | Making parts by rotational moulding |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1729108A1 (en) * | 1967-11-28 | 1971-06-03 | Thermovox Gmbh | Process for the production of closed and open containers and molded parts from plastics and containers and molded parts produced in this way |
FR2091333A5 (en) * | 1970-05-13 | 1972-01-14 | Langmatz Hans | Lamp post - of reinforced plastics |
GB1365341A (en) * | 1971-11-29 | 1974-09-04 | Raleigh Industries Ltd | Moulding of annular foamed material articles |
US4178406A (en) * | 1977-12-29 | 1979-12-11 | Rohm And Haas Company | Three-layered fiberglass construction |
EP0286058A2 (en) * | 1987-04-08 | 1988-10-12 | FERRARI ENGINEERING S.p.A. | Composite load-bearing structural element and relative manufacturing process |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07125082A (en) * | 1993-11-08 | 1995-05-16 | Sekisui Chem Co Ltd | Manufacture of fiber reinforced molded product |
-
2000
- 2000-04-24 AU AU67463/00A patent/AU6746300A/en not_active Abandoned
- 2000-04-24 WO PCT/US2000/011007 patent/WO2000066358A2/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1729108A1 (en) * | 1967-11-28 | 1971-06-03 | Thermovox Gmbh | Process for the production of closed and open containers and molded parts from plastics and containers and molded parts produced in this way |
FR2091333A5 (en) * | 1970-05-13 | 1972-01-14 | Langmatz Hans | Lamp post - of reinforced plastics |
GB1365341A (en) * | 1971-11-29 | 1974-09-04 | Raleigh Industries Ltd | Moulding of annular foamed material articles |
US4178406A (en) * | 1977-12-29 | 1979-12-11 | Rohm And Haas Company | Three-layered fiberglass construction |
EP0286058A2 (en) * | 1987-04-08 | 1988-10-12 | FERRARI ENGINEERING S.p.A. | Composite load-bearing structural element and relative manufacturing process |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 1995, no. 08, 29 September 1995 (1995-09-29) & JP 07 125082 A (SEKISUI CHEM CO LTD), 16 May 1995 (1995-05-16) * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1358988A1 (en) * | 2002-04-30 | 2003-11-05 | Gesikat Ltd. | Making parts by rotational moulding |
Also Published As
Publication number | Publication date |
---|---|
WO2000066358A9 (en) | 2002-02-21 |
WO2000066358A3 (en) | 2001-03-15 |
AU6746300A (en) | 2000-11-17 |
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