DE602004002262D1 - Verfahren zum Auflegen von Prepregteile für eine selbstverstärkte Platte - Google Patents

Verfahren zum Auflegen von Prepregteile für eine selbstverstärkte Platte

Info

Publication number
DE602004002262D1
DE602004002262D1 DE602004002262T DE602004002262T DE602004002262D1 DE 602004002262 D1 DE602004002262 D1 DE 602004002262D1 DE 602004002262 T DE602004002262 T DE 602004002262T DE 602004002262 T DE602004002262 T DE 602004002262T DE 602004002262 D1 DE602004002262 D1 DE 602004002262D1
Authority
DE
Germany
Prior art keywords
plungers
layers
inverted
carbon fiber
self
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.)
Active
Application number
DE602004002262T
Other languages
English (en)
Other versions
DE602004002262T2 (de
Inventor
Georges Navas
Jean-Paul Petetin
Michel Fontayne
Pierre Lafon
Guy Hellard
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602004002262D1 publication Critical patent/DE602004002262D1/de
Application granted granted Critical
Publication of DE602004002262T2 publication Critical patent/DE602004002262T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • B29C70/04Shaping 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
    • 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
    • B29C70/34Shaping 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
    • B29C70/345Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • 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
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1028Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
    • Y10T156/1031Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith with preshaping of lamina
    • 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
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1043Subsequent to assembly
    • Y10T156/1044Subsequent to assembly of parallel stacked sheets only
    • Y10T156/1048Subsequent to assembly of parallel stacked sheets only to form dished or receptacle-like product
    • 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
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1043Subsequent to assembly
    • Y10T156/1049Folding only

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
DE602004002262T 2003-12-04 2004-11-22 Verfahren zum Anordnen von vormprägnierten Teilen für eine selbstversteifende Verbundplatte Active DE602004002262T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0314253A FR2863197B1 (fr) 2003-12-04 2003-12-04 Procede de mise en place des elements d'un panneau auto-raidi en composite preimpregne
FR0314253 2003-12-04

Publications (2)

Publication Number Publication Date
DE602004002262D1 true DE602004002262D1 (de) 2006-10-19
DE602004002262T2 DE602004002262T2 (de) 2007-04-05

Family

ID=34451721

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004002262T Active DE602004002262T2 (de) 2003-12-04 2004-11-22 Verfahren zum Anordnen von vormprägnierten Teilen für eine selbstversteifende Verbundplatte

Country Status (7)

Country Link
US (1) US7270722B2 (de)
EP (1) EP1537981B1 (de)
AT (1) ATE338630T1 (de)
CA (1) CA2487049C (de)
DE (1) DE602004002262T2 (de)
ES (1) ES2271786T3 (de)
FR (1) FR2863197B1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2863198B1 (fr) * 2003-12-04 2006-03-03 Airbus France Panneaux auto-raidis en composite pre-impregne et procedes de mise en place des elements de tels panneaux
WO2007077265A1 (es) * 2005-12-30 2007-07-12 Airbus España, S.L. Procedimiento para la fabricación de paneles de materiales compuestos con elementos rigidizadores en forma de u
DE102007015517A1 (de) 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Strukturbauteils
FR2942165B1 (fr) * 2009-02-16 2016-01-29 Airbus France Procede de fabrication d'un panneau raidi en materiau composite
FR2986990B1 (fr) * 2012-02-17 2014-10-03 Airbus Operations Sas Panneau auto-raidi en materiau composite et procede de realisation d'un tel panneau
FR2997955B1 (fr) 2012-11-13 2015-07-03 Structil Materiau de comblement de structure composite
US9409348B2 (en) 2013-02-04 2016-08-09 The Boeing Company Fabrication of stiffened composite panels
US9511520B1 (en) 2014-08-20 2016-12-06 The Boeing Company Method, apparatus and device for preventing vacuum bag wrinkling
ES2926668T3 (es) * 2015-04-30 2022-10-27 Airbus Operations Sl Método de fabricación de estructuras de material compuesto con útiles de curado por fuera de la bolsa de vacío
GB201507519D0 (en) * 2015-05-01 2015-06-17 Vestas Wind Sys As Reinforcing Structure for a Wind Turbine Blade
US10035300B2 (en) 2015-06-23 2018-07-31 The Boeing Company System and method for manufacturing a stiffened composite structure
JP6719495B2 (ja) * 2018-03-06 2020-07-08 株式会社Subaru プリフォーム賦形方法、複合材成形方法及び複合材
CN112512926B (zh) 2018-08-08 2023-04-04 克里奥瓦克公司 用于产品的真空贴体包装的设备和方法
US11390045B2 (en) 2018-09-07 2022-07-19 Textron Innovations Inc. Molding assembly and method of co-curing stiffener with panel
CN110480884B (zh) * 2019-08-22 2022-06-24 中国商用飞机有限责任公司北京民用飞机技术研究中心 模具、组装预成型结构的制造方法和壁板结构的制造方法
FR3121383A1 (fr) * 2021-04-01 2022-10-07 Airbus Operations Outil pour la fabrication d’un panneau auto-raidi et procédé de fabrication d’un panneau auto-raidi utilisant un tel outil
FR3130189B1 (fr) * 2021-12-14 2024-04-12 Airbus Operations Sas Dispositif de fabrication d’un panneau raidi permettant de maîtriser la géométrie dudit panneau raidi et procédé de fabrication d’un panneau raidi utilisant ledit dispositif

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2105254B (en) * 1981-06-24 1984-05-10 Permabond Adhesives Top-hat stiffeners for grp and other panels of synethetic plastics materials
US5538589A (en) * 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine

Also Published As

Publication number Publication date
CA2487049A1 (fr) 2005-06-04
CA2487049C (fr) 2013-01-08
US7270722B2 (en) 2007-09-18
FR2863197B1 (fr) 2006-03-03
FR2863197A1 (fr) 2005-06-10
EP1537981A1 (de) 2005-06-08
EP1537981B1 (de) 2006-09-06
ATE338630T1 (de) 2006-09-15
DE602004002262T2 (de) 2007-04-05
US20050166501A1 (en) 2005-08-04
ES2271786T3 (es) 2007-04-16

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