FR2565894B1 - Procede de fabrication de lamines composites renforces par fibres - Google Patents

Procede de fabrication de lamines composites renforces par fibres

Info

Publication number
FR2565894B1
FR2565894B1 FR8504151A FR8504151A FR2565894B1 FR 2565894 B1 FR2565894 B1 FR 2565894B1 FR 8504151 A FR8504151 A FR 8504151A FR 8504151 A FR8504151 A FR 8504151A FR 2565894 B1 FR2565894 B1 FR 2565894B1
Authority
FR
France
Prior art keywords
fiber reinforced
reinforced composite
composite laminates
manufacturing fiber
manufacturing
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
Application number
FR8504151A
Other languages
English (en)
French (fr)
Other versions
FR2565894A1 (fr
Inventor
Peter Sappl
Franz Nowak
Peter Auer
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2565894A1 publication Critical patent/FR2565894A1/fr
Application granted granted Critical
Publication of FR2565894B1 publication Critical patent/FR2565894B1/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/28—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
    • 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
    • B29C2791/00—Shaping characteristics in general
    • B29C2791/001—Shaping in several steps
    • 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
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • 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
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/243—Partially cured
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00—Layered products

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Thermal Sciences (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
FR8504151A 1984-03-27 1985-03-20 Procede de fabrication de lamines composites renforces par fibres Expired FR2565894B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3411270 1984-03-27
DE19843445462 DE3445462A1 (de) 1984-03-27 1984-12-13 Verfahren zum herstellen von faserverbund-laminaten

Publications (2)

Publication Number Publication Date
FR2565894A1 FR2565894A1 (fr) 1985-12-20
FR2565894B1 true FR2565894B1 (fr) 1989-10-27

Family

ID=25819757

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8504151A Expired FR2565894B1 (fr) 1984-03-27 1985-03-20 Procede de fabrication de lamines composites renforces par fibres

Country Status (2)

Country Link
DE (1) DE3445462A1 (enrdf_load_stackoverflow)
FR (1) FR2565894B1 (enrdf_load_stackoverflow)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62257839A (ja) * 1986-05-06 1987-11-10 町田　輝史 繊維強化プラスチツク複合薄板及びその成形方法
EP0392226A1 (en) * 1989-03-23 1990-10-17 Mitsubishi Gas Chemical Company, Inc. Vacuum, continuous batch process for producing laminates and apparatus for such process
DE4033438C1 (enrdf_load_stackoverflow) * 1990-10-20 1992-05-14 Saar-Federn Gmbh, 6620 Voelklingen, De
US5759325A (en) * 1996-03-29 1998-06-02 Sikorsky Aircraft Corporation Method for controlling thickness during lay-up and fabrication of press-cured composite articles
DE19949318A1 (de) * 1999-09-11 2001-03-15 Menzolit Fibron Gmbh Kohlenstoffaserverstärktes SMC für multiaxial verstärkte Bauteile
RU2421334C2 (ru) * 2006-07-28 2011-06-20 Айрбус Эспанья, С.Л. Способ изготовления деталей, сделанных из композитных материалов с двумя циклами термоотверждения
CA2659371C (en) * 2006-07-28 2014-08-26 Airbus Espana, S.L. Process for the manufacture of parts made of composite materials with two curing cycles
DE102014209815A1 (de) * 2014-03-07 2015-09-10 Leichtbau-Zentrum Sachsen Gmbh Verfahren zur Verbindung von faserverstärkten Kunststoffbauteilen mit duroplastischer Matrix
DE102014215964A1 (de) 2014-08-12 2016-02-18 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Herstellen eines mit einem unidirektionalen Fasergelege versehenen SMC-Bauteiles
AT517696B1 (de) * 2015-09-04 2017-04-15 Röchling Leripa Papertech Gmbh & Co Kg Faserverstärkter Kunststoffkörper

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1047314A (enrdf_load_stackoverflow) * 1900-01-01
FR464064A (fr) * 1913-10-01 1914-03-12 Alfred George Spencer Procédé de fabrication de ressorts-tampons, ressorts de traction, de portée ou autres, ainsi que de diaphragmes élastiques, en caoutchouc, et produits en résultant
US1386722A (en) * 1919-06-24 1921-08-09 Western Electric Co Diaphragm
GB527906A (en) * 1939-02-11 1940-10-18 Ebonestos Ind Ltd Improvements in and relating to the moulding of articles from synthetic resins
US3334001A (en) * 1963-06-03 1967-08-01 Certain Teed Prod Corp Process for forming a laminated plastic structure
US3530212A (en) * 1967-02-16 1970-09-22 Gen Motors Corp Method of making glass resin laminates
IT999823B (it) * 1973-11-26 1976-03-10 Mispa Snc Procedimento per la fabbricazione di un manufatto comprendente strati di tessuto impregnati di resine
US4065340A (en) * 1977-04-28 1977-12-27 The United States Of America As Represented By The National Aeronautics And Space Administration Composite lamination method
DE2722262B2 (de) * 1977-05-17 1979-07-19 Kurt 7218 Trossingen Held Verfahren und Vorrichtung zur kontinuierlichen Herstellung von Laminaten
GB2108038B (en) * 1981-10-06 1985-07-24 Advanced Composite Components Moulding and curing prepregs at reduced temperature
DE3200877C2 (de) * 1982-01-14 1985-09-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und Vorrichtung zum Herstellen von Blattfedern aus faserverstärkten Werkstoffen

Also Published As

Publication number Publication date
DE3445462A1 (de) 1985-10-10
DE3445462C2 (enrdf_load_stackoverflow) 1989-05-18
FR2565894A1 (fr) 1985-12-20

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