CA2223779C - Production of large composite structures - Google Patents

Production of large composite structures Download PDF

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Publication number
CA2223779C
CA2223779C CA002223779A CA2223779A CA2223779C CA 2223779 C CA2223779 C CA 2223779C CA 002223779 A CA002223779 A CA 002223779A CA 2223779 A CA2223779 A CA 2223779A CA 2223779 C CA2223779 C CA 2223779C
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CA
Canada
Prior art keywords
core
resin
feeder channel
tool
mold
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
Application number
CA002223779A
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French (fr)
Other versions
CA2223779A1 (en
Inventor
George C. Tunis, Iii
William H. Seemann, Iii
Andrew P. Perrella
Rikard K. Haraldsson
William E. Everitt
Everett A. Pearson
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Scrimp Systems LLC
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Scrimp Systems LLC
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Application filed by Scrimp Systems LLC filed Critical Scrimp Systems LLC
Publication of CA2223779A1 publication Critical patent/CA2223779A1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/36Shaping 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 and impregnating by casting, e.g. vacuum casting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/0061Moulds or cores; Details thereof or accessories therefor characterised by the configuration of the material feeding channel
    • B29C33/0066Moulds or cores; Details thereof or accessories therefor characterised by the configuration of the material feeding channel with a subdivided channel for feeding the material to a plurality of locations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/021Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles characterised by the shape of the surface
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3642Bags, bleeder sheets or cauls for isostatic pressing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/544Details of vacuum bags, e.g. materials or shape
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure
    • B29C70/547Measures for feeding or distributing the matrix material in the reinforcing structure using channels or porous distribution layers incorporated in or associated with the product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure
    • B29C70/548Measures for feeding or distributing the matrix material in the reinforcing structure using distribution constructions, e.g. channels incorporated in or associated with the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3642Bags, bleeder sheets or cauls for isostatic pressing
    • B29C2043/3644Vacuum bags; Details thereof, e.g. fixing or clamping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/76Cores
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/23Sheet including cover or casing
    • Y10T428/233Foamed or expanded material encased
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/23Sheet including cover or casing
    • Y10T428/239Complete cover or casing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24496Foamed or cellular component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24521Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface
    • Y10T428/24537Parallel ribs and/or grooves
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/2457Parallel ribs and/or grooves
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612Composite web or sheet
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249994Composite having a component wherein a constituent is liquid or is contained within preformed walls [e.g., impregnant-filled, previously void containing component, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249994Composite having a component wherein a constituent is liquid or is contained within preformed walls [e.g., impregnant-filled, previously void containing component, etc.]
    • Y10T428/249999Differentially filled foam, filled plural layers, or filled layer with coat of filling material
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30Woven fabric [i.e., woven strand or strip material]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3325Including a foamed layer or component

Abstract

Large composite structures are produced using a vacuum assisted resin transfer molding process incorporating a resin distribution network. The resin distribution network is provided by a textured sheet (104) of metal formed as an integral vacuum bag and mold. The texture is formed by upraised portions (108) on one side of the sheet which correspond with depressions on the other side. Valleys between the upraised portions form the resin distribution network. A fiber lay up is placed against the textured sheet (104) with the upraised portions facing the lay up. Main feeder grooves (114) are also formed directly in the sheet (104). Resin is supplied under vacuum to the main feeder grooves, from where it travels through the valleys of the textured sheet (104) to impregnate the lay up.

Description

- Production of Large Composite Structures T'IELD OF THE INVENTION ' This invention relates to the production of fiber reinforced resin composite structures, and in particular to processes for vacuum assisted resin transfer molding of large composite structures.
BACKGROUND OF THE INVENTION

Vacuum assisted resin transfer molding (VA-RTM) has been used to produce a number of large, fiber reinforced composite structures such as boat hulls which incorporate materials such as foam.and balsa cores. The cores are covered with a fiber reinforced resin. In the VA-RTM process, the reinforcement fiber, such as a fabric or mat, is arranged in a single sided mold in a dry condition along with the desired core materials according to the form of the desired finished part. The lay-up is then encapsulated in a vacuum bag and impregnated with resin under vacuum. The resin is allowed to cure.

Various methods have been utilized to introduce and enhance the distribution of resin through the reinforcement fiber. These methods include the placement of a disposable distribution media over the outside layer of fabric and the incorporation of holes and/or slots penetrating through the core to allow resin to flow from the outer to the inner layer of reinforcement fiber. See, for example, U.S. Patent Nos.

5,316,462 and 4,560,523. A supply groove in a foam core has also been used in a closed mold resin injection process to facilitate resin flow. See, for example, U. S. Patent No.

5,096,651.

WO 96/40488 fCT/US96/09171 SUINB~iARY OF THE INVENTION

The present invention relates' to- a method for distributing resin during the manufacture of large composite structures using a vacuum assisted resin transfer molding (VA-RTM) process and the composite structure produced by this method. The composite structure is formed from internal cores surrounded by fiber reinforced resin. In one embodiment of the invention, resin is supplied directly into a network of main feeder grooves which are interconnected to a series of smaller microgrooves formed in the surface of the internal cores. From the feeder grooves and microgrooves, the resin flows outwardly from the core to penetrate the reinforcement fiber. In a second embodiment of the invention, a separate distribution medium is interposed between the internal core and the fiber reinforcement. The resin is supplied directly to one or more main feeder grooves in the core surface and penetrates the reinforcement fiber via the distribution medium. Also, the main feeder grooves can extend around the cores to form supply loops, allowing impregnation of transverse structural members.

In a further embodiment, an integrated vacuum bag and mold are formed from a textured sheet of metal. The texture is formed by closely spaced upraised portions on one side of the sheet which correspond with depressions on the other side of the sheet. The closely spaced upraised portions define valleys therebetween which form a resin distribution network.

Main feeder grooves are formed directly in the sheet. The textured sheet can also be used as a mold from which other tools are made.

With this method, large composite structures which require multiple cores can be formed quickly prior to the gel time of typical vinyl ester or polyester resins, and the amount of resin used can be minimized. By supplying the resin directly through the vacuum bag into the feeder grooves, the supply is not limited to a part edge or inlet in a tool. Adjacent cores can be supplied via a single resin inlet. The resin distribution network can remain in the finished part, eliminating disposal of distribution ~ materials. In this case, the microgrooves are filled with resin after curing, thereby increasing interlaminar shear strength and delamination strength. Structural features such as shear ties, compression webs, or beams can be incorporated directly into the composite part during the molding process.
DESCRIPTION OF THE DRAWINGS

to The invention will be more fully understood from the following detailed description taken in conjunction with the accompanying drawings in which:

Fig. 1 is a perspective view of a core for a composite structure according to a first embodiment of the present invention;

Fig. 2 is a schematic cross-sectional view of a composite structure being formed according to the first embodiment of the present invention;

Fig. 3 is a schematic perspective view of a further composite structure being formed according to the present invention;

Fig. 4 is a perspective view of a composite structure being formed according to the present invention;

Fig. 5 is a perspective view of a further core for a composite structure according to the present invention;

Fig. 6 is a perspective view of a core for a composite structure according to a second embodiment of the present invention;

Fig. 7 is a schematic cross-sectional view of a composite structure being formed according to the second embodiment of the present invention;

' Fig. 8 is a schematic cross-sectional view of a composite structure being formed using an integrated mold and vacuum structure;

Fig. 9 is a schematic cross-sectional view of a rigid mold and flexible lid for forming a composite structure;
Fig. 10 is a perspective view of a core for a composite structure having multiple main feeder grooves;

Fig. 11 is a schematic cross-sectional view of an integrated mold and vacuum bag for forming a composite structure according to a further embodiment of the present invention;

Fig. 12 is a perspective view of one side of a textured sheet of material forming the integrated mold and vacuum bag of Fig. il; and Fig. 13 is a perspective view of the other side of the textured sheet of Fig. 12.

RETAILED DESCRIPTION OF THE INVENTION

A large composite part made according to the present invention includes a core 12, shown in Fig. 1. The core is made from a material able to support the pressure of a vacuum. Typical materials include foams, such as a polyurethane or a polyvinyl chloride, or balsa wood. The core can be solid or hollow, such as a blown polyethylene.

Concrete may also be used. The core is shown as a rectangular block, although other configurations are possible, as discussed further below.

One or more main feeder grooves or channels 14 are provided in the surface 16 of the core. The main feeder groove may circumscribe the entire core to form a loop. A

resin distribution network comprising channels of a smaller cross-sectional area than the main feeder groove is provided in contact with the surface of the core for fluid communication with the main feeder groove.

In a first embodiment of the present invention, the resin distribution network is provided in the form of a plurality of microgrooves 18 machined in the surface 16 of the core 12, as shown in Fig. 1. The microgrooves 18 are generally arranged transversely to the main feeder groove 14.

Some of the microgrooves may circumscribe the entire core to create a resin flow loop beginning and ending at the main feeder groove. The actual relation of the microgrooves to the main feeder groove depends on the geometry of the core and the optimization of the resin impregnation, as discussed further below.

. 5 The core 14 with the network of grooves is covered with' one or more layers of a fiber material 20, illustrated schematically in Fig. 2. The fiber material may be a cloth or mat formed from fibers of glass, carbon, or other suitable material. Depending on the structural requirements of the desired finished part, the core may be completely surrounded with fiber material, or one or more surfaces of the core may be left free of fiber material. The fiber material may be wrapped in a sheet around the core, or individual pieces of fiber material may be applied to the desired. core faces. The fiber may also be supplied in a tubular form into which the core is inserted.

A plurality of fiber wrapped cores are arranged to form the desired finished part. Although two cores are shown in Fig. 2, the actual number and arrangement of cores is determined by the desired finished part. One or more layers of a fiber material can be wrapped around a plurality of cores to form an outer skin 22, shown schematically in Fig.

2. The particular number of layers of fiber material, the type, and the arrangement depend on the desired finished part and can be readily determined by those of skill in the art.

A bleeder layer is generally provided in the form of a tab 23 extending from an outer fiber layer to a vacuum outlet 25.

Peel plies, typically required with prior art vacuum processes, are generally not needed with the process of the present invention.

The fiber material 24 surrounding and between the cores ' creates structural members such as shear ties, compression webs, and beams. For example, referring to Fig. 4, a plurality of triangular cores 40 are used to form a deck.

The fiber material between adjacent triangular cores forms diagonal structural members 41 that support both compression and shear forces.

During the lay-up, suitable fittings 26, such as plastic or copper tees, are positioned in the main feeder grooves 14 ' to facilitate the subsequent insertion of resin supply tubes 28. One or more fittings may be positioned in each feeder groove, to accommodate the desired resin flow. The lay-up is placed against a mold 29, and a vacuum bag 30 is then placed over the lay-up, including the plastic fittings, and sealed to the mold in a manner known in the art, as shown schematically in Fig. 2. The vacuum bag is then punctured and the supply tubes 28 are inserted through the vacuum bag directly into their respective fittings 26. The supply tubes are sealed to the bag to retain vacuum integrity. In this manner, the main feeder grooves are supplied directly with resin by penetrating the outer vacuum bag with a supply tube that is inserted directly into the groove.

Referring to Fig. 8, the vacuum bag and mold may also be integrated into a single structure 80 which is rigid enough to retain its shape as a mold but flexible enough to collapse against the part upon application of a vacuum. For example, the integrated structure 80 may comprise a thin gauge steel sheet, such as 0.25 inch or thinner. The cores 82 and fiber material 84, 86, as described above, are encapsulated in the steel sheet. Holes are drilled through the sheet to access the fittings. Resin impregnation occurs as described above. The integrated structure may be formed of other suitable materials, such as rubber or silicone or a thin composite sheet material such as a plastic laminated metal.

Fig. 9 illustrates a further mold embodiment in which a rigid mold 90 is sealed with a flexible lid 92 formed, for example, from a steel or plastic material. A part, ' comprising the cores and fiber material as described above, is placed in the recess 94 defined by the rigid mold. A

vacuum groove 96 in the lid surrounds the part. Holes are provided through the lid or mold to access fittings for resin impregnation as described above. During impregnation of the resin under vacuum, the lid flexes at the edge of the vacuum ~ groove, to allow compaction of the part.

The resin, such as a polyester, vinyl ester, epoxy, - 5 phenolic, acrylic, or bismaleimide, travels relatively quickly through the main feeder grooves 14 and into the microgrooves 18. From the microgrooves, the resin penetrates the fiber material 20, 22. Impregnation results from resin infusion originating at the core surface 16 and migrating outwardly to the exterior of the part. The fiber material on adjacent core surfaces may be impregnated via a main feeder groove in one of the adjacent cores, as indicated in Figs. 3 and 4.

The cross-sectional area of the main feeder groove and the cross-sectional area and spacing of the microgrooves are optimized to provide a suitable time to allow the resin to impregnate all of the fiber material before curing without leaving unimpregnated areas. A typical main feeder groove may have a depth of 0.5 inch and a width of 0.5 inch for a cross-sectional area of 0.25 square inches. Typical microgrooves may have a depth of 0.125 inch and a width of, 0.125 inch for_a cross-sectional area of approximately 0.016 square inches. The microgrooves may be spaced 1.0 inch on center. These dimensions may be modified to accommodate reinforcement fiber materials of different types and/or thicknesses. Also, the cross-sectional area of the main feeder grooves may be increased if the part is particularly large to more rapidly distribute the resin to all sections of the part. Similarly, multiple main feeder grooves 14 may be provided in a core 12, as indicated in Fig. 10.

In addition, the cross-sectional area of the main feeder ' grooves or the microgrooves may be reduced to create flow restrictions to increase resin dwell time at a particular ' area. Resin dwell time may also be increased by placing a resin ''fuse' in the feeder groove which temporarily blocks the resin flow. The fuse dissolves after contact with the _ g _ resin after a known period of time, which may be set by the length of the fuse. For example, with a vinyl ester resin, a Styrofoam fuse has been used successfully. The feeder grooves may also terminate to redirect resin flow.

The main feeder grooves 14 allow passage of resin from -one core to an adjacent core. Holes may be provided through the cores to connect main feeder grooves. Each main feeder groove may be supplied with resin simultaneously, creating parallel circuits, or in a prescribed sequence, creating series circuits, depending on the geometry and size of the part to be impregnated. Additionally, the main feeder grooves may be independent of each other, creating separate circuits.

After impregnation, the resin is allowed sufficient time to cure. Once cured, the microgrooves 18 are filled with solid resin. This resin provides a lateral locking mechanism which improves the interlaminar shear strength of the bond between the fiber reinforced composite and the core. The resin remaining in the groove network also increases the forces necessary to delaminate the fiber reinforced face skins from the core.

The actual arrangement and shape and number of cores depends on the desired finished part. For example, triangular cores 40 are shown in Fig. 3. The triangular cores may have main feeder grooves 42 provided in at least two surfaces. A central triangular core 44 may have main feeder grooves in three surfaces. Microgrooves are provided in the surfaces as described above. A plurality of triangular cores may be arranged in, for example, a row to form a deck. In this example, resin, supplied through tubes 46, is impregnated sequentially beginning at the central core and progressing toward the edges, as shown by the shaded region 48 in Fig. 4.

An arcuate core 50 is shown in Fig. 5. The arcuate core 50 may have a main feeder groove 52 in one surface and a network of microgrooves 54 radiating from the feeder groove _g_ to circumscribe the core. The arcuate cores may be used to form curved structures such as boat hulls or arches.
In another embodiment of the present invention, illustrated in Figs. 6 and 7, a core 60 is provided with a main feeder groove 62 as described above. A distribution medium 64 is then provided adjacent the core faces. The medium comprises a network of open passageways formed by a structure capable of maintaining the passageways in an open condition during application of the vacuum. For example, the medium may comprise intersecting filaments held in spaced relation from the core surface by post-like members located at each filament intersection, a grid-like structure of aligned strips, or an open weave fabric. Suitable distribution media are known for example, from U.S. Patents Nos. 4,902,215 and 5,052,906. A fiber material 66 is then wrapped over the distribution media, as described above. A
plurality of cores are arranged to form the desired finished part, and a vacuum bag 68 is placed over the cores and fiber material, as described above. Resin supply tubes 70 leading from a resin source are inserted through the bag 68 and fiber material 66 to fittings 72 in the main feeder grooves 62. The supply tubes 70 are sealed to the vacuum bag in a manner known in the art . Resin is fed through the supply tubes to the main feeder grooves. The resin travels relatively quickly through the main feeder grooves and into the distribution media. From the distribution media, the resin penetrates the fiber material. A suitable time interval is provided to allow the resin to cure.
Resin distribution media presents a more uniform resin flow front than the microgrooves. For this reason, resin distribution media are generally preferred for more complicated parts, whereas microgrooves are preferred to conserve resin, since less resin flows through the microgrooves.
In a further embodiment, illustrated in Figs. 11 through 13, the vacuum bag and mold are integrated into a single tool 102 formed from a textured sheet 104 of metal, such as a thin gauge steel sheet. The sheet is rigid enough to retain its shape as a mold, but flexible enough to collapse or be pulled against the part under the vacuum applied during a resin impregnation process, discussed further below. A sheet thickness of 0.25 inch or less has been found suitable. A
plastic or a composite material such as a metal and plastic laminate formed as a textured sheet may also be used.
Preferably, the texture is formed by closely spaced upraised portions 108 formed on one side of the sheet 104 which correspond to depressions 106 on the other side of the sheet. The closely spaced upraised portions 108 define valleys 110 therebetween which form a resin distribution network. For example, the upraised portions may have a generally hexagonal shape having a longest dimension of between 3/8 inch and 7/16 inch. A depth of the valleys of approximately 30 thousandths of an inch has been found to be suitable. Such a textured sheet is readily formable and is commercially available from Ardmore Textured Metal of Edison, New Jersey. Alternatively, the texture could be provided on a single side of the sheet if desired, such that the upraised portions do not make corresponding depressions on the other side.
The sheet is shaped into the desired form of a mold 112 having a mold cavity 118 with the upraised portions of the sheet forming the interior walls of the cavity, thereby facing the part to be impregnated. Main feeder grooves 114 are formed directly in the sheet 104 in the desired locations, rather than in the cores as described above. The main feeder grooves may have dimensions as discussed above.
Vacuum outlet channels 116 are formed around the perimeter ' of the tool.
To form a composite part, a fiber lay up is placed within the cavity 118 adjacent the textured surfaces of the tool, and the tool is sealed as with a tacky tape or other seal as is known in the art. A peel ply may be used if the texture is not to be retained on the part. Alternatively, - a peel ply may be omitted if the texture is desired to be retained on the surface of the part. Forming the texture on . 5 the part imparts some further stiffness to the part and may be desired for esthetic reasons as well. The fiber lay up may comprise cores wrapped with fiber material as discussed above. Fittings are inserted into the main feeder grooves through punctures made in the sheet as discussed above. A

vacuum is applied to the interior of the tool, and the sheet of textured material is pulled adjacent the fiber lay up such that the tops of the upraised portion contact the fiber lay up, but the valleys remain open to form a network of narrow, interconnected passageways through which resin is able to flow. Under the vacuum, resin is drawn first into the main feeder grooves and then into the valleys. From the valleys, the resin is able to fully impregnate the filter material, flowing finally to the vacuum outlet channels around the perimeter. The resin is allowed sufficient i:ime to cure.

After curing, the part is removed from the tool.

In an alternative embodiment, the textured sheet can be used as a lid in conjunction with a conventional mold. The fiber lay up is placed against the mold surface. The textured sheet is placed over the fiber lay up and sealed to the mold in any suitable manner. Additional resin distribution media may need to be used adjacent the conventional mold surfaces. Resin impregnation occurs as discussed above.

The textured sheet can also be used as a master mold which is used to make tools from other materials, such as ceramics. The tool is then used as a mold in the resin ' impregnation process. In this case, the sheet comprises a negative of the tool; that is, the side of the sheet having ' the indentations is used to form the tool. The resulting tool has the configuration of the upraised portions separated by the valleys, which form a resin distribution medium as discussed above. A ceramic mold generally does not flex to collapse against the part under vacuum. In this case, a separate vacuum bag is used in conjunction with the mold, as -is known in the art.
The invention is not to be limited by what has been particularly shown and described, except as indicated by the appended claims.

Claims (86)

1. A tool for forming a composite structure by vacuum assisted resin transfer molding, said tool comprising:
a mold surface and a vacuum bag arranged with said mold surface to form a mold cavity for receiving a structure to be impregnated with resin;
at least a portion of said vacuum bag formed from a sheet material having a texture formed by upraised portions on a first side of said sheet material, said upraised portions being closely spaced and having valleys therebetween, said valleys forming a resin distribution network of interconnected channels; and a main feeder channel having a cross-sectional area larger than a cross-sectional area of said valleys being provided in fluid communication with said valleys and extending along a portion of said tool to provide resin to said resin distribution network.
2. The tool of claim 1, wherein said vacuum bag and said mold are unitary.
3. The tool of claim 1, wherein said portion of said vacuum bag forms said mold surface, whereby said vacuum bag and said mold are unitary.
4. The tool of claim 1, wherein said valleys have a depth of approximately 30 thousandths of an inch.
5. The tool of claim 1, wherein said upraised portions are generally hexagonal in shape and have a longest dimension between 3/8 inch and 7/16 inch.
6. The tool of claim 1, wherein said sheet of material forming said portion of said vacuum bag comprises a sheet of thin gauge steel.
7. The tool of claim 1, wherein said portion of said vacuum bag is formed of a sheet rigid enough to retain its shape but flexible enough to collapse against a structure under a vacuum applied during a resin transfer molding process.
8. The tool of claim 1, wherein said sheet of material forming said portion of said vacuum bag has a thickness of 0.25 inch or less.
9. The tool of claim 1, wherein said sheet material further comprises depressions corresponding to said upraised portions formed on the other side of said sheet material.
10. The tool of claim 1, further comprising a vacuum outlet channel formed in said vacuum bag around a perimeter of said tool.
11. The tool of claim 1, wherein said vacuum bag and said mold are sealable to form said mold cavity.
12. A method of forming a composite structure comprising:
providing a tool for forming a composite structure by vacuum assisted resin transfer molding, said tool comprising:
a mold surface and a vacuum bag arranged with said mold surface to form a mold cavity for receiving a part to be impregnated with resin;
at least a portion of said vacuum bag formed from a sheet material having a texture formed by upraised portions on a first side of said sheet material, said upraised portions being closely spaced and having valleys therebetween, said valleys forming a resin distribution network; and a main feeder channel having a cross-sectional area larger than a cross-sectional area of said valleys being provided in fluid communication with said valleys and extending along a portion of said tool to provide resin to said resin distribution network;
providing the part to be molded in said mold cavity;
sealing said mold cavity;
connecting a source of uncured resin to said main feeder channel;
connecting the interior of said mold cavity to a vacuum outlet;
forcing said uncured resin through said main feeder channel and said resin distribution network to said vacuum outlet to fill said part in said mold cavity to impregnate said part; and curing said resin to form a composite structure.
13. The method of claim 12, wherein, in said tool providing step, said vacuum bag and said mold are unitary.
14. The method of claim 12, wherein, in said tool providing step, said portion of said vacuum bag forms said mold surface, whereby said vacuum bag and said mold are unitary.
15. The method of claim 12, wherein, in said tool providing step, said valleys have a depth of approximately 30 thousandths of an inch.
16. The method of claim 12, wherein, in said tool providing step, said upraised portions are generally hexagonal in shape and have a longest dimension between 3/8 inch and 7/16 inch.
17. The method of claim 12, wherein, in said tool providing step, said sheet of material forming said portion of said vacuum bag comprises a sheet of thin gauge steel.
18. The method of claim 12, wherein, in said tool providing step, said portion of said vacuum bag is formed of a sheet rigid enough to retain its shape but flexible enough to collapse against a structure under a vacuum applied during a resin transfer molding process.
19. The method of claim 12, wherein, in said tool providing step, said sheet of material forming said portion of said vacuum bag has a thickness of 0.25 inch or less.
20. The method of claim 12, wherein, in said tool providing step, said sheet material further comprises depressions corresponding to said upraised portions formed on the other side of said sheet material.
21. The method of claim 12, wherein in said tool providing step, said tool further comprises a vacuum outlet channel formed in said vacuum bag around a perimeter of said tool.
22. The method of claim 12, wherein said step of connecting said source of uncured resin to said feeder channel comprises forming a hole in said vacuum bag and inserting a supply tube from said source into said feeder channel.
23. A method of forming a composite structure comprising:
providing a core having a peripheral surface and a feeder channel formed to lie across at least a portion of said peripheral surface of said core;
providing a resin distribution network adjacent at least a portion of said core peripheral surface in fluid communication with said feeder channel in said core peripheral surface;
covering at least a portion of said core and said resin distribution network with a fiber material;
sealing said covered core in a forming structure, at least a first portion of said forming structure comprising a mold and at least a further portion of said forming structure comprising a flexible portion collapsible under vacuum against an adjacent portion of said covered core;
connecting a source of uncured resin to said feeder channel through said forming structure;
connecting the interior of said forming structure to a vacuum outlet;
forcing said uncured resin through said feeder channel and said resin distribution network to said vacuum outlet to fill said forming structure between said core and said forming structure to impregnate said fiber material; and curing said resin to form a composite structure.
24. The method of claim 23, wherein said resin distribution network comprises a network of grooves formed in said surface of said core extending from said feeder channel, said grooves having a smaller cross-sectional area than said feeder channel.
25. The method of claim 24, wherein said grooves are arranged transversely to said feeder channel.
26. The method of claim 24, wherein at least a portion of said grooves circumscribe said core to form a loop beginning and terminating at said feeder channel.
27. The method of claim 23, wherein said resin distribution network comprises a resin distribution medium laid adjacent to said surface of said core.
28. The method of claim 27, wherein said resin distribution medium comprises a structure forming a network of intersecting open passageways.
29. The method of claim 27, wherein said resin distribution medium comprises intersecting filaments held in spaced relation from the core surface by post-like members located at each filament intersection, a grid-like structure of aligned strips, or an open weave fabric.
30. The method of claim 23, further comprising placing at least one connection fitting in said feeder channel prior to covering said core and said resin distribution network with a fiber material.
31. The method of claim 30, wherein said step of connecting said source of uncured resin to said channel comprises forming a hole in said forming structure at said connection fitting and inserting a supply tube from said source into said connection fitting.
32. The method of claim 23, further comprising providing a plurality of said cores, each having a peripheral surface and a feeder channel formed in said surface extending throughout a length of said core, and arranging said cores adjacent to each other to form a desired finished part.
33. The method of claim 32, wherein said cores are arranged adjacent to each other with each of said feeder channels generally aligned.
34. The method of claim 33, further comprising covering said adjacently arranged cores with a further fiber material prior to said step of placing in said mold.
35. The method of claim 23, wherein said forming structure comprises a thin steel sheet.
36. The method of claim 23, wherein said forming structure comprises a rigid mold and a flexible bag.
37. The method of claim 23, wherein said forming structure comprises a rubber bag.
38. The method of claim 23, wherein said forming structure comprises a silicone bag.
39. The method of claim 23, wherein said forming structure comprises a thin composite sheet material.
40. The method of claim 23, wherein said forming structure comprises a rigid mold and a flexible lid.
41. The method of claim 40, wherein said lid includes a vacuum groove therein to surround a periphery of said core covered with said fiber material.
42. The method of claim 23, wherein said feeder channel and said distribution network are sized and arranged to allow the resin to completely fill the fiber material covering the core prior to curing.
43. The method of claim 23, wherein said core comprises a foam material.
44. The method of claim 23, wherein said core comprises balsa wood.
45. The method of claim 23, wherein said core comprises concrete.
46. The method of claim 23, wherein said core comprises a block having a generally rectangular cross-section.
47. The method of claim 23, wherein said core comprises a block having a generally triangular cross-section.
48. The method of claim 23, wherein said core comprises a block having an arcuate face.
49. The method of claim 23, wherein a plurality of feeder channels are formed to lie across at least a portion of said peripheral surface of said core.
50. The method of claim 23, further comprising causing a delay in filling said forming structure with said uncured resin.
51. The method of claim 50, wherein said step of causing a delay comprises providing a material dissolvable by said uncured resin in a portion of said feeder channel.
52. The method of claim 50, wherein said step of causing a delay comprises narrowing a portion of said feeder channel.
53. A method of forming a composite structure comprising:
providing a core having a peripheral surface and a feeder channel formed to lie across at least a portion of said peripheral surface of said core;
providing a resin distribution network adjacent at least a portion of said core peripheral surface in fluid communication with said feeder channel in said core peripheral surface;
covering at least a portion of said core and said resin distribution network with a fiber material;
placing said covered core in a mold;
sealing said covered core in a bag against said mold;
connecting a source of uncured resin to said feeder channel through said bag;
connecting the interior of said bag to a vacuum outlet;
forcing said uncured resin through said feeder channel and said resin distribution network to said vacuum outlet to fill said mold between said core and said mold and said bag to impregnate said fiber material; and curing said resin to form a composite structure.
54. The method of claim 53, wherein said resin distribution network comprises a network of grooves formed in said surface of said core extending from said feeder channel, said grooves having a smaller cross-sectional area than said feeder channel.
55. The method of claim 54, wherein said grooves are arranged transversely to said feeder channel.
56. The method of claim 54, wherein at least a portion of said grooves circumscribe said core to form a loop beginning and terminating at said feeder channel.
57. The method of claim 53, wherein said resin distribution network comprises a resin distribution medium laid adjacent to said surface of said core.
58. The method of claim 57, wherein said resin distribution medium comprises a structure forming a network of intersecting open passageways.
59. The method of claim 57, wherein said resin distribution medium comprises intersecting filaments held in spaced relation from the core surface by post-like members located at each filament intersection, a grid-like structure of aligned strips, or an open weave fabric.
60. The method of claim 53, further comprising placing at least one connection fitting in said feeder channel prior to covering said core and said resin distribution network with a fiber material.
61. The method of claim 60, wherein said step of connecting said source of uncured resin to said channel comprises puncturing said bag at said connection fitting and inserting a supply tube from said source into said connection fitting.
62. The method of claim 53, further comprising providing a plurality of said cores, each having a peripheral surface and a feeder channel formed in said surface extending throughout a length of said core, and arranging said cores adjacent to each other to form a desired finished part.
63. The method of claim 62, wherein said cores are arranged adjacent to each other with each of said feeder channels generally aligned.
64. The method of claim 62, further comprising covering said adjacently arranged cores with a further fiber material prior to said step of placing in said mold.
65. The method of claim 53, wherein said feeder channel and said distribution network are sized and arranged to allow the resin to completely fill the fiber material covering the core prior to curing.
66. The method of claim 53, wherein said core comprises a foam material.
67. The method of claim 53, wherein said core comprises balsa wood.
68. The method of claim 53, wherein said core comprises concrete.
69. The method of claim 53, wherein said core comprises a block having a generally rectangular cross-section.
70. The method of claim 53, wherein said core comprises a block having a generally triangular cross-section.
71. The method of claim 53, wherein said core comprises a block having an arcuate face.
72. The method of claim 53, wherein a plurality of feeder channels are formed to lie across at least a portion of said peripheral surface of said core.
73. A unitary composite structure comprising:
a core having a peripheral surface and a feeder channel formed to lie across at least a portion of said peripheral surface of said core;
a resin distribution network adjacent said core peripheral surface and said feeder channel in said core peripheral surface;
a fiber material covering said core, said feeder channel, and said resin distribution network; and a cured resin impregnating said fiber material, said feeder channel, and said resin distribution network.
74. The structure of claim 73, wherein said resin distribution network comprises a network of grooves formed in said surface of said core extending from said feeder channel, said grooves having a smaller cross-sectional area than said feeder channel.
75. The structure of claim 74, wherein said grooves are arranged transversely to said feeder channel.
76. The structure of claim 74, wherein at least a portion of said grooves circumscribe said core to form a loop beginning and terminating at said feeder channel.
77. The structure of claim 74, wherein said resin distribution network comprises a resin distribution medium laid adjacent to said peripheral surface of said core.
78. The structure of claim 77, wherein said resin distribution medium comprises intersecting filaments held in spaced relation from the core surface by post-like members located at each filament intersection, a grid-like structure of aligned strips, or an open weave fabric.
79. The structure of claim 74, further comprising a plurality of said cores, each having a peripheral surface and a feeder channel formed in said surface extending throughout a length of said core, and arranging said cores adjacent to each other.
80. The structure of claim 79, wherein said cores are arranged adjacent to each other with each of said feeder channels generally aligned.
81. The structure of claim 74, wherein said core comprises a foam material.
82. The structure of claim 74, wherein said core comprises balsa wood.
83. The structure of claim 74, wherein said core comprises concrete.
84. The structure of claim 74, wherein said core comprises a block having a generally rectangular cross-section.
85. The structure of claim 74, wherein said core comprises a block having a generally triangular cross-section.
86. The structure of claim 74, wherein said core comprises a block having an arcuate face.
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US08/475,849 US5958325A (en) 1995-06-07 1995-06-07 Large composite structures and a method for production of large composite structures incorporating a resin distribution network
US08/475,849 1995-06-07
US08/612,251 1996-03-07
US08/612,251 US6773655B1 (en) 1995-06-07 1996-03-07 Large composite structures and a method for production of large composite structures incorporating a resin distribution network
PCT/US1996/009171 WO1996040488A1 (en) 1995-06-07 1996-06-04 Production of large composite structures

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Families Citing this family (149)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5904972A (en) * 1995-06-07 1999-05-18 Tpi Technology Inc. Large composite core structures formed by vacuum assisted resin transfer molding
US6558608B2 (en) * 1995-06-28 2003-05-06 Tpi Technology, Inc. Method for molding fiber reinforced composite container
US6203749B1 (en) * 1996-02-15 2001-03-20 David Loving Process for fiberglass molding using a vacuum
US6000243A (en) * 1998-04-27 1999-12-14 The Regents Of The University Of California Vacuum pull down method for an enhanced bonding process
AU749594B2 (en) 1998-08-11 2002-06-27 Daimlerchrysler Ag People mover carshells
KR20010075455A (en) * 1998-09-30 2001-08-09 히라이 가쯔히꼬 Hollow Structure of Fiber-Reinforced Resin and Method of Manufacturing The Same
US6945987B2 (en) * 2002-11-08 2005-09-20 Kci Licensing, Inc. Patient cooling system
US6482497B1 (en) * 1998-11-30 2002-11-19 Rocky Mountain Composites Inc. Pressure-cycled, packet-transfer infusion of resin-stitched preforms
US6090335A (en) * 1999-01-08 2000-07-18 Northrop Grumman Corporation Process of forming fiber reinforced composite articles using an insitu cured resin infusion port
US6656411B1 (en) 1999-01-11 2003-12-02 Northrop Grumman Corporation Grooved core pattern for optimum resin distribution
US6555045B2 (en) * 1999-01-11 2003-04-29 Northrop Grumman Corporation Grooved mold apparatus and process for forming fiber reinforced composite structures
KR20010102186A (en) * 1999-02-16 2001-11-15 히라이 가쯔히꼬 Frp structure body and production method therefor
JP2000238140A (en) * 1999-02-17 2000-09-05 Toray Ind Inc Frp cylinder and its manufacture
DE19911267A1 (en) * 1999-03-13 2000-09-14 Basf Ag Azoxy dyes and their Cu complexes
US6216752B1 (en) 1999-03-31 2001-04-17 Northrop Grumman Corporation Gravity feed resin delivery system for VARTM fabrication
US6367406B1 (en) * 1999-09-24 2002-04-09 Larson/Glastron Boats, Inc. Boat and method for manufacturing using resin transfer molding
US20030186038A1 (en) * 1999-11-18 2003-10-02 Ashton Larry J. Multi orientation composite material impregnated with non-liquid resin
US7681835B2 (en) * 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
AU3789801A (en) * 1999-12-07 2001-06-18 Boeing Company, The Double bag vacuum infusion process and system for low cost, advanced composite fabrication
AU2459101A (en) 1999-12-28 2001-07-09 Webcore Technologies, Inc. Fiber reinforced composite cores and panels
US6386131B1 (en) 2000-08-28 2002-05-14 Roshdy George S. Barsoum Hybrid ship hull
US6649002B2 (en) 2000-11-09 2003-11-18 Patent Holding Company Method of manufacturing articles utilizing a composite material having a high density of small particles in a matrix material
US8419883B2 (en) 2000-12-27 2013-04-16 Milliken & Company Fiber reinforced composite cores and panels
WO2002058915A1 (en) * 2001-01-26 2002-08-01 Kaneka Corporation Core material for fiber-reinforced resin composite structure and method for producing fiber-reinforced resin composite structure using the same
US6518330B2 (en) 2001-02-13 2003-02-11 Board Of Trustees Of University Of Illinois Multifunctional autonomically healing composite material
US6723271B2 (en) 2001-04-16 2004-04-20 W. Scott Hemphill Method and apparatus for making composite parts
US6565792B2 (en) 2001-05-11 2003-05-20 Hardcore Composites Apparatus and method for use in molding a composite structure
US6750272B2 (en) 2001-06-25 2004-06-15 Board Of Trustees Of University Of Illinois Catalyzed reinforced polymer composites
US7048985B2 (en) * 2001-07-23 2006-05-23 Vrac, Llc Three-dimensional spacer fabric resin infusion media and reinforcing composite lamina
US7060156B2 (en) * 2001-07-23 2006-06-13 Vrac, Llc Three-dimensional spacer fabric resin interlaminar infusion media process and vacuum-induced reinforcing composite laminate structures
CN100381272C (en) * 2001-07-24 2008-04-16 北京航空工艺研究所 Technological process resulting in improved structural quality of vacuum permeation formed composite material
DK176335B1 (en) * 2001-11-13 2007-08-20 Siemens Wind Power As Process for manufacturing wind turbine blades
US6964561B2 (en) * 2002-04-23 2005-11-15 V System Composites, Inc. High-performance infusion system for VARTM fabrication
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
FR2843933B1 (en) * 2002-08-27 2005-05-20 Gen Trailers France BODY FOR COMPOSITE MATERIALS FOR AN INDUSTRIAL VEHICLE, PROCESS FOR PRODUCING THE SAME, AND MOLD ASSEMBLY AND COUNTER-MOLD FOR IMPLEMENTING THE METHOD
US6918985B2 (en) * 2002-12-12 2005-07-19 The Boeing Company Method for making a radome
US7300894B2 (en) * 2002-12-30 2007-11-27 University Of Maine Composites pressure resin infusion system (ComPRIS)
CN100406239C (en) * 2003-03-13 2008-07-30 东邦泰纳克丝株式会社 Method of resin transfer molding
CA2519866C (en) * 2003-03-28 2012-05-22 Webcore Technologies, Inc. Fiber reinforced composite cores and panels
NL1023425C2 (en) * 2003-05-14 2004-11-16 Tno Method and device for the manufacture of a fiber-reinforced plastic product.
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US8262823B2 (en) * 2003-09-04 2012-09-11 The Boeing Company Window skin panel and method of making same
US7299552B2 (en) * 2003-09-08 2007-11-27 Hewlett-Packard Development Company, L.P. Methods for creating channels
US7029267B2 (en) 2003-10-23 2006-04-18 Saint- Gobain Technical Fabrics Canada, Ltd Reusable vacuum bag and methods of its use
US6941888B2 (en) * 2003-12-16 2005-09-13 Roshdy George S. Barsoum Hybrid ship hull
US7160498B2 (en) 2004-03-08 2007-01-09 Tracker Marine, L.L.C. Closed molding tool
DE102004013742A1 (en) * 2004-03-18 2005-10-13 Ge Bayer Silicones Gmbh & Co. Kg Shaping process using a silicone rubber composition
US7566747B2 (en) * 2004-05-07 2009-07-28 The Board Of Trustees Of The University Of Illinois Wax particles for protection of activators, and multifunctional autonomically healing composite materials
CN100395096C (en) * 2004-07-28 2008-06-18 上特技材有限公司 Method for fabricating composite structure of plastic strengthened by fiberglass
US7959058B1 (en) 2005-01-13 2011-06-14 The United States Of America As Represented By The Secretary Of The Navy Hybrid composite welded joint
US8047798B2 (en) 2005-02-03 2011-11-01 Vestas Wind Systems A/S Method of manufacturing a wind turbine blade shell member
US7612152B2 (en) * 2005-05-06 2009-11-03 The Board Of Trustees Of The University Of Illinois Self-healing polymers
US7744974B2 (en) * 2005-07-19 2010-06-29 Pearson Pilings, Llc Composite structure and method of manufacture
US20070108646A1 (en) * 2005-11-15 2007-05-17 Louderback Michael J Method of fabricating a composite structure with details
US20070256599A1 (en) * 2005-12-16 2007-11-08 Jack Rigsby Inorganic Composite Material And Manufacturing Process
CN101351603A (en) * 2005-12-16 2009-01-21 21世纪结构有限责任公司 Inorganic composite building panel
US7758800B2 (en) * 2005-12-22 2010-07-20 Comtek Advanced Structures Limited System and method for resin infusion
US7723405B2 (en) 2006-01-05 2010-05-25 The Board Of Trustees Of The University Of Illinois Self-healing coating system
US8741198B2 (en) * 2006-03-08 2014-06-03 Toray Industries, Inc. Process for producing fiber reinforced resin
GB2436616A (en) 2006-03-29 2007-10-03 Inverness Medical Switzerland Assay device and method
US7569625B2 (en) * 2006-06-02 2009-08-04 The Board Of Trustees Of The University Of Illinois Self-healing elastomer system
US7749424B2 (en) 2006-08-31 2010-07-06 Milgard Manufacturing, Inc. Vacuum-infused fiberglass-reinforced fenestration framing member and method of manufacture
US7897097B2 (en) 2006-08-31 2011-03-01 Milgard Manufacturing Incorporated Vacuum-infused fiberglass-reinforced fenestration framing member and method of manufacture
US7849729B2 (en) * 2006-12-22 2010-12-14 The Boeing Company Leak detection in vacuum bags
WO2008089334A2 (en) 2007-01-19 2008-07-24 Vec Industries, L.L.C. Method and apparatus for molding composite articles
US9770871B2 (en) 2007-05-22 2017-09-26 The Boeing Company Method and apparatus for layup placement
US8568551B2 (en) * 2007-05-22 2013-10-29 The Boeing Company Pre-patterned layup kit and method of manufacture
US20080299391A1 (en) * 2007-05-31 2008-12-04 White Scott R Capsules, methods for making capsules, and self-healing composites including the same
WO2009003477A1 (en) 2007-06-29 2009-01-08 Lm Glasfiber A/S A method for producing a composite structure and a composite structure
DK2160286T4 (en) 2007-06-29 2019-03-18 Lm Glasfiber As Process for using a moldable core block for a resin impregnation process, a method for preparing a composite structure and a composite structure thus obtained
US8333864B2 (en) * 2008-09-30 2012-12-18 The Boeing Company Compaction of prepreg plies on composite laminate structures
US8936695B2 (en) 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US8707766B2 (en) 2010-04-21 2014-04-29 The Boeing Company Leak detection in vacuum bags
US20090155521A1 (en) * 2007-08-07 2009-06-18 Rodman William L Composite structures and methods of making same
US20090039566A1 (en) * 2007-08-07 2009-02-12 Rodman William L Composite structures and methods of making same
US8834782B2 (en) * 2007-08-07 2014-09-16 William L. Rodman Composite structures and methods of making same
US7754045B2 (en) * 2007-11-14 2010-07-13 The Boeing Company Method and tools for fabricating composite beams
US7926407B1 (en) * 2007-11-16 2011-04-19 Gerald Hallissy Armor shielding
US8916010B2 (en) * 2007-12-07 2014-12-23 The Boeing Company Composite manufacturing method
US8752293B2 (en) 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
US20090181254A1 (en) * 2008-01-15 2009-07-16 The Board Of Trustees Of The University Of Illinois Multi-capsule system and its use for encapsulating active agents
KR100941096B1 (en) * 2008-02-01 2010-02-10 현대자동차주식회사 Molding method of bumper back beam for vehicle
US7851048B2 (en) 2008-02-12 2010-12-14 Milliken & Co. Fiber reinforced core panel
DE102008013759B4 (en) * 2008-03-12 2012-12-13 Airbus Operations Gmbh Process for producing an integral fiber composite component and core mold for carrying out the process
US20090309260A1 (en) 2008-06-12 2009-12-17 Kenneth Herbert Keuchel Method of delivering a thermoplastic and/or crosslinking resin to a composite laminate structure
US8480393B2 (en) * 2008-06-13 2013-07-09 Lockheed Martin Corporation Vacuum-assisted resin transfer molding process with reusable resin distribution line
WO2010039547A2 (en) * 2008-09-23 2010-04-08 Invision Technology, Llc Reinforced internal composite structures
US20100135817A1 (en) * 2008-10-22 2010-06-03 Wirt John C Wind turbine blade and method for manufacturing thereof
US20100308515A1 (en) * 2009-06-05 2010-12-09 Astoria Industries Of Iowa, Inc. Apparatus and process for manufacturing a vacuum molded fiberglass chipper body
US20100310886A1 (en) * 2009-06-05 2010-12-09 Astoria Industries Of Iowa, Inc. apparatus and process for manufacturing a vacuum molded fiberglass service body
GB2470618B (en) * 2009-09-14 2011-08-24 Alexander Fergusson An improved method of and apparatus for making a composite material
US8158245B2 (en) 2009-09-24 2012-04-17 Cytec Technology Corp. Thermoplastic composites and methods of making and using same
US8529818B2 (en) * 2009-09-30 2013-09-10 General Electric Company Automated fiber placement in female mold
DK2483076T3 (en) * 2009-10-01 2016-10-24 Milliken & Co Composite cores and panels
US8389104B2 (en) 2009-10-02 2013-03-05 Milliken & Company Composite cores and panels
DE102009060699B4 (en) * 2009-12-29 2014-07-03 Airbus Operations Gmbh Infusion method and flow aid
CN102917869B (en) * 2010-05-13 2014-11-12 贝尔直升机泰克斯特龙公司 Method of making a composite article having an internal passageway
IT1410977B1 (en) * 2010-06-14 2014-10-03 Automobili Lamborghini Spa PROCESS AND DEVICES FOR MANUFACTURING PRODUCTS IN COMPOSITE MATERIALS
JP5927183B2 (en) * 2010-07-02 2016-06-01 ヘクセル ホールディング ゲーエムベーハー Fiber reinforced composite molded product
GB201012293D0 (en) * 2010-07-22 2010-09-08 Advanced Composites Group Ltd Mould tools
US8551380B2 (en) 2010-11-12 2013-10-08 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
US9387657B2 (en) 2010-11-12 2016-07-12 The Boeing Company Method of fabricating a curved composite structure using composite prepreg tape
US9701067B2 (en) 2010-11-12 2017-07-11 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
US8646183B2 (en) 2011-03-14 2014-02-11 Milliken & Company Process for forming a fiber reinforced core panel able to be contoured
US8641848B2 (en) 2011-03-14 2014-02-04 Milliken & Company Method and apparatus for combining elongated strips
US8663791B2 (en) 2011-04-04 2014-03-04 Milliken & Company Composite reinforced cores and panels
EP2511083A1 (en) * 2011-04-14 2012-10-17 Siemens Aktiengesellschaft Method for manufacturing a work piece by vacuum assisted resin transfer moulding
US8728374B1 (en) 2011-08-02 2014-05-20 Crane Composites Inc. Method of manufacturing a foundation wall panel
EP2750852B1 (en) 2011-08-30 2018-06-27 Johnson Controls Technology Company Method for manufacturing a vehicle trim component via compression forming and injection molding and trim component produced thereby
US10464280B2 (en) 2011-08-30 2019-11-05 Shanghai Yanfeng Jinqiao Automotive Trim Systems Co. Ltd. Trim component for vehicle interior
DE102011111452A1 (en) * 2011-08-30 2013-02-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Production of a fiber composite component
KR20130028561A (en) 2011-09-09 2013-03-19 현대자동차주식회사 Large tow carbon fiber composite with improved flexural property and surface property
JP6066331B2 (en) * 2012-02-15 2017-01-25 東レ株式会社 Manufacturing method of fiber reinforced resin
EP2639050B1 (en) 2012-03-14 2014-05-14 Siemens Aktiengesellschaft Method of manufacturing an article by molding
US9566742B2 (en) * 2012-04-03 2017-02-14 Massachusetts Institute Of Technology Methods and apparatus for computer-assisted spray foam fabrication
CN102745307B (en) * 2012-06-29 2015-02-18 深圳市海斯比船艇科技股份有限公司 Manufacturing method of ship
US10093268B2 (en) 2012-08-27 2018-10-09 Shanghai Yanfeng Jinqiao Automotive Trim Systems Co. Ltd. Trim component for vehicle interior
WO2014062900A1 (en) 2012-10-18 2014-04-24 Cytec Industries Inc. Surface engineering of thermoplastic materials and tooling
US8973871B2 (en) 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
DE102013201728A1 (en) * 2013-02-04 2014-08-07 Bayerische Motoren Werke Aktiengesellschaft Core and process for producing fiber-reinforced plastic semi-finished products
US11052619B1 (en) 2013-04-29 2021-07-06 Plastics Unlimited, Inc. Fabrication apparatuses and methods
US9574349B2 (en) * 2013-05-13 2017-02-21 Hawkeye Pedershaab Concrete Technologies, Inc. Post-tensioning concrete pipe wrap
CN103587130B (en) * 2013-10-15 2016-04-06 南京航空航天大学 The method of microwave curing fiber-reinforced resin matrix compound material component and device
CN106132673B (en) 2014-03-04 2018-03-16 庞巴迪公司 The method and apparatus that composite laminate stacking is formed using breathable polyethylene vacuum diaphragm
CN103878994B (en) * 2014-04-14 2016-12-28 北京建筑大学 FRP air entrained concrete composite plate and preparation method thereof
CN104044277B (en) * 2014-05-04 2016-12-07 中北大学 The vacuum assisted resin transfer molding integral forming technique of composite fuel tank
DE102014209400A1 (en) * 2014-05-19 2015-11-19 Bayerische Motoren Werke Aktiengesellschaft mold
CN104070684A (en) * 2014-06-04 2014-10-01 洛阳双瑞风电叶片有限公司 Pipeline-free vacuum infusion forming method of sandwiched composite material
DE102014213187A1 (en) * 2014-07-08 2016-01-14 Bayerische Motoren Werke Aktiengesellschaft Press tool with optimized resin flow
DE102014222560A1 (en) * 2014-11-05 2016-05-12 Bayerische Motoren Werke Aktiengesellschaft Manufacturing core and method for producing a fiber composite component and fiber composite component
DE102015225467B4 (en) * 2015-12-16 2019-12-19 Airbus Defence and Space GmbH Coated composite component and method for producing a coated composite component
DE102016218076A1 (en) 2016-09-21 2018-03-22 Bayerische Motoren Werke Aktiengesellschaft RTM tool with resin injection system
GB2554870A (en) * 2016-10-06 2018-04-18 Forward Composites Fabricating a composite article
DE102016220588A1 (en) 2016-10-20 2018-04-26 Bayerische Motoren Werke Aktiengesellschaft Distributed system adapted to semi-finished fiber properties
WO2018100152A1 (en) * 2016-12-01 2018-06-07 Lm Wind Power International Technology Ii Aps Method and system for manufacturing a shear web for a wind turbine blade
USD887926S1 (en) 2017-01-17 2020-06-23 Angel Armor, Llc Transparent armor
US11225942B2 (en) * 2017-07-05 2022-01-18 General Electric Company Enhanced through-thickness resin infusion for a wind turbine composite laminate
EP3476561B1 (en) * 2017-10-31 2020-02-26 Airbus Operations, S.L. Modular mould and method for manufacturing a panel of fibre reinforced material
US10759124B2 (en) * 2017-11-21 2020-09-01 The Boeing Company Apparatus and method for manufacturing liquid molded composites using a discrete network of tool surface resin distribution grooves
GB2570104B (en) * 2017-12-18 2021-12-29 Composite Integration Ltd Improved system and method for resin transfer moulding
CN109986722B (en) * 2017-12-29 2024-01-02 尹军华 Processing device for carbon fiber composite material cascade and cascade
EP3814176B1 (en) 2018-06-28 2024-02-21 Shanghai Yanfeng Jinqiao Automotive Trim Systems Co. Ltd Vehicle trim component
US11318689B2 (en) 2018-12-21 2022-05-03 The Boeing Company Ply transporting and compacting apparatus and method therefor
US11305498B2 (en) 2018-12-21 2022-04-19 The Boeing Company System and method for fabricating a composite ply layup
ES2910045T3 (en) 2019-10-24 2022-05-11 Diab Int Ab Composite sandwich components
FR3106295B1 (en) * 2020-01-17 2023-05-05 Alstom Transp Tech Method of manufacturing a section, in particular of a vehicle, preferably of a railway vehicle, associated section
WO2022130459A1 (en) * 2020-12-14 2022-06-23 三菱重工業株式会社 Fiber-reinforced composite material shaping device and fiber-reinforced composite material shaping method
CN114311745B (en) * 2021-12-23 2023-06-02 大连理工大学 Forming system and preparation method of composite material sandwich structure

Family Cites Families (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1217157A (en) 1916-10-21 1917-02-27 American Gum Products Company Rubber composition and process of making the same.
US2913036A (en) * 1956-08-10 1959-11-17 Anthony Bros Fibre Glass Pool Process and apparatus for molding large plastic structures
US3146148A (en) * 1957-11-08 1964-08-25 Gen Dynamics Corp Apparatus for fabricating composite structures
GB1024582A (en) * 1961-07-05 1966-03-30 Rodgers William A method of manufacturing a synthetic resin moulding reinforced with fibrous material
FR1504274A (en) * 1966-12-09 1967-12-01 Elastic punch improved for forming, particularly of impregnated fibrous materials
US3666600A (en) * 1969-03-10 1972-05-30 North American Rockwell Apparatus for forming layup laminate
US3855029A (en) * 1969-03-12 1974-12-17 E Sabel Method for re-inforcing cast-metal objects, particularly thin plates of hard and brittle cast steel
BE769501A (en) * 1970-07-22 1971-11-16 Camus Raymond ELEMENT OF CONSTRUCTION
US3710733A (en) * 1971-03-02 1973-01-16 Plasteel Ind Inc Integrated reinforced plastic unit and method and apparatus for making the same
US4125526A (en) * 1973-01-02 1978-11-14 Goodyear Aerospace Corporation Vacuum blanket curing method
JPS503098A (en) * 1973-05-16 1975-01-13
JPS53117079A (en) * 1977-03-24 1978-10-13 Nippon Hardboard Decorative plate and its production method
US4132755A (en) * 1977-07-22 1979-01-02 Jay Johnson Process for manufacturing resin-impregnated, reinforced articles without the presence of resin fumes
DE2736842A1 (en) * 1977-08-16 1979-03-01 Wolf & Sohn Kg Peter PANEL ELEMENT
GB1604872A (en) * 1978-03-29 1981-12-16 Rohm & Haas Reinforcing a layer of plastics material
US4238437A (en) * 1978-08-02 1980-12-09 Rolston John A Method for producing fiber reinforced product
US4217157A (en) * 1978-11-20 1980-08-12 United Technologies Corporation Method of fabricating fiber-reinforced articles
US4312829A (en) * 1979-12-10 1982-01-26 Fourcher Fredric J Molding method
NL178761C (en) * 1980-03-11 1986-05-16 Le Comte Holland B V METHOD FOR MANUFACTURING ARTICLE RESIN ARTICLES
US4560523A (en) * 1984-04-30 1985-12-24 A&M Engineered Composites Corporation Intrusion molding process for forming composite structures
US4622091A (en) * 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
US4676041A (en) * 1985-11-19 1987-06-30 Warminster Fiberglass Co. Corrosion-resistant door and its method of manufacture
US4822436A (en) * 1986-03-07 1989-04-18 Northrop Corporation Apparatus for debulking and autoclaving laminates of complex shapes
US5123985A (en) * 1986-09-02 1992-06-23 Patricia Evans Vacuum bagging apparatus and method including a thermoplastic elastomer film vacuum bag
US5045251A (en) * 1987-06-15 1991-09-03 Ford Motor Company Method of resin transfer molding a composite article
JP2802430B2 (en) 1987-07-10 1998-09-24 3−ディ コンポジッツ リミテッド Molding method
US5132069A (en) * 1987-07-10 1992-07-21 Newton John R Method of injection molding composite articles
US4902215A (en) * 1988-06-08 1990-02-20 Seemann Iii William H Plastic transfer molding techniques for the production of fiber reinforced plastic structures
US4975311A (en) * 1988-12-20 1990-12-04 Itt Corporation Vacuum lamination station
US4942013A (en) * 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
US5052906A (en) * 1989-03-30 1991-10-01 Seemann Composite Systems, Inc. Plastic transfer molding apparatus for the production of fiber reinforced plastic structures
GB8915369D0 (en) * 1989-07-04 1989-08-23 3 D Composites Moulding method
JPH03162933A (en) * 1989-11-21 1991-07-12 Yamaha Motor Co Ltd Method of molding plastic and structure of mold for molding plastic
US5593633A (en) * 1990-05-03 1997-01-14 Dull; Kenneth M. Edge and surface breather for high temperature composite processing
US5096651A (en) * 1990-05-23 1992-03-17 Le Comte Adolf Method for manufacturing an object of synthetic resin
US5304339A (en) * 1990-05-23 1994-04-19 Le Comte Adolf Method for manufacturing a large-sized object of fiber reinforced synthetic resin
US5242651A (en) * 1990-07-25 1993-09-07 Vought Aircraft Company Pressure balanced processing of composite structures
US5087193A (en) * 1990-08-09 1992-02-11 Herbert Jr Kenneth H Apparatus for forming a composite article
CA2056224A1 (en) * 1990-12-19 1992-06-20 Terry Martin Boustead Conformal composite molding
US5256366A (en) * 1991-01-08 1993-10-26 Richard Wejrock Method of molding fiberglass
US5129813A (en) * 1991-02-11 1992-07-14 Shepherd G Maury Embossed vacuum bag, methods for producing and using said bag
GB9111817D0 (en) 1991-06-01 1991-07-24 British Aerospace Composite resin flow
US5266249A (en) * 1992-01-02 1993-11-30 Fusion Composites, Inc. Method of forming a fiber reinforced plastic structure
US5316462A (en) * 1993-02-18 1994-05-31 William Seemann Unitary vacuum bag for forming fiber reinforced composite articles
US5439635A (en) * 1993-02-18 1995-08-08 Scrimp Systems, Llc Unitary vacuum bag for forming fiber reinforced composite articles and process for making same
US5433165A (en) * 1994-03-30 1995-07-18 Outboard Marine Corporation Method of manufacturing a boat hull
US5500164A (en) * 1994-05-02 1996-03-19 Synergistic Composite Systems Inc. Method and apparatus for producing large fiber reinforced structures
US5576030A (en) * 1995-10-02 1996-11-19 Lockheed Corporation Apparatus for fabricating composite parts

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