FR2773514B1 - METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE - Google Patents

METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE

Info

Publication number
FR2773514B1
FR2773514B1 FR9800213A FR9800213A FR2773514B1 FR 2773514 B1 FR2773514 B1 FR 2773514B1 FR 9800213 A FR9800213 A FR 9800213A FR 9800213 A FR9800213 A FR 9800213A FR 2773514 B1 FR2773514 B1 FR 2773514B1
Authority
FR
France
Prior art keywords
strongly
resin
manufacturing
composite panel
panel core
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 - Fee Related
Application number
FR9800213A
Other languages
French (fr)
Other versions
FR2773514A1 (en
Inventor
Olivier Brun
Claude Bonnebat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sollac SA
Original Assignee
Sollac SA
Lorraine de Laminage Continu SA SOLLAC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sollac SA, Lorraine de Laminage Continu SA SOLLAC filed Critical Sollac SA
Priority to FR9800213A priority Critical patent/FR2773514B1/en
Publication of FR2773514A1 publication Critical patent/FR2773514A1/en
Application granted granted Critical
Publication of FR2773514B1 publication Critical patent/FR2773514B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • 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
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
    • B29C70/506—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands and impregnating by melting a solid material, e.g. sheet, powder, fibres
    • 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
    • B29K2101/00—Use of unspecified macromolecular compounds as moulding material
    • B29K2101/10—Thermosetting resins
    • 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
    • B29K2105/25—Solid
    • B29K2105/253—Preform
    • B29K2105/256—Sheets, plates, blanks or films
FR9800213A 1998-01-13 1998-01-13 METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE Expired - Fee Related FR2773514B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9800213A FR2773514B1 (en) 1998-01-13 1998-01-13 METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9800213A FR2773514B1 (en) 1998-01-13 1998-01-13 METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE

Publications (2)

Publication Number Publication Date
FR2773514A1 FR2773514A1 (en) 1999-07-16
FR2773514B1 true FR2773514B1 (en) 2000-02-11

Family

ID=9521670

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9800213A Expired - Fee Related FR2773514B1 (en) 1998-01-13 1998-01-13 METHOD FOR MANUFACTURING A FLEXIBLE TABLECLOTH AND A STRONGLY RESIN-LOADED COMPOSITE PANEL CORE

Country Status (1)

Country Link
FR (1) FR2773514B1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE410185A (en) *
FR2656340B1 (en) * 1989-12-22 1994-05-06 Isofran TEXTILE CORE, MANUFACTURING METHOD, AND COMPOSITE PRODUCT OBTAINED WITH SUCH A TEXTILE CORE.
DE4129190A1 (en) * 1991-09-03 1993-03-04 Held Kurt METHOD AND DEVICE FOR THE CONTINUOUS PRODUCTION OF RESIN IMPREGNATED MATERIALS
US5340520A (en) * 1992-06-10 1994-08-23 Beech Aircraft Corp. Non-woven mat surface ply for woven fabric
EP0686494A3 (en) * 1994-06-06 1996-06-05 Owens Corning Fiberglass Corp Polymer coated glass fiber mat

Also Published As

Publication number Publication date
FR2773514A1 (en) 1999-07-16

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20140930