ATE457265T1 - Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff - Google Patents

Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff

Info

Publication number
ATE457265T1
ATE457265T1 AT04028829T AT04028829T ATE457265T1 AT E457265 T1 ATE457265 T1 AT E457265T1 AT 04028829 T AT04028829 T AT 04028829T AT 04028829 T AT04028829 T AT 04028829T AT E457265 T1 ATE457265 T1 AT E457265T1
Authority
AT
Austria
Prior art keywords
fiber composite
flange
male tool
composite laminate
contact
Prior art date
Application number
AT04028829T
Other languages
English (en)
Inventor
Mikael Petersson
Bjoern Weidmann
Max Krogager
Claes Rudqvist
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Application granted granted Critical
Publication of ATE457265T1 publication Critical patent/ATE457265T1/de

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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1036—Bending of one piece blank and joining edges to form article
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1043—Subsequent to assembly
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Catalysts (AREA)
AT04028829T 2004-12-06 2004-12-06 Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff ATE457265T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP04028829A EP1666353B1 (de) 2004-12-06 2004-12-06 Verfahren zur Herstellung eines gekrümmten Trägers aus Verbundwerkstoff

Publications (1)

Publication Number Publication Date
ATE457265T1 true ATE457265T1 (de) 2010-02-15

Family

ID=34927663

Family Applications (1)

Application Number Title Priority Date Filing Date
AT04028829T ATE457265T1 (de) 2004-12-06 2004-12-06 Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff

Country Status (5)

Country Link
US (2) US7670525B2 (de)
EP (1) EP1666353B1 (de)
AT (1) ATE457265T1 (de)
DE (1) DE602004025482D1 (de)
ES (1) ES2338551T3 (de)

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7943076B1 (en) * 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
US8632653B2 (en) * 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
DE102005028765B4 (de) * 2005-06-22 2016-01-21 Airbus Operations Gmbh Verfahren zur Herstellung eines Verstärkungsprofils
DE602005025490D1 (de) * 2005-10-17 2011-02-03 Saab Ab Verfahren zur Herstellung eines gekrümmten Gegenstands aus Verbundwerkstoff sowie durch dieses Verfahren hergestellter Gegenstand
US8691137B2 (en) 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US9102103B2 (en) 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
US8333858B2 (en) 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US7807005B2 (en) 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
WO2008132252A1 (es) * 2007-04-30 2008-11-06 Airbus España, S.L. Geometrías complejas en material compuesto y procedimiento de conformado de las mismas
US8118959B2 (en) 2007-06-27 2012-02-21 The Boeing Company Method and apparatus for contouring composite pre-preg articles
CN101910493B (zh) * 2008-01-11 2013-07-24 东丽株式会社 弯曲形状强化纤维基材、及使用其的层合体、预成型体、纤维强化树脂复合材料和它们的制造方法
FR2928295B1 (fr) * 2008-03-07 2017-12-08 Duqueine Rhone Alpes Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante.
US8349105B2 (en) 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
US8932423B2 (en) 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9090028B2 (en) 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US10821653B2 (en) 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
GB2484476B (en) * 2010-10-11 2012-12-12 Gkn Aerospace Services Ltd Composite structure
US9387657B2 (en) 2010-11-12 2016-07-12 The Boeing Company Method of fabricating a curved composite structure using composite prepreg tape
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
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
ITTO20110421A1 (it) * 2011-05-12 2012-11-13 Alenia Aeronautica Spa Elemento strutturale con ala avente bordo netto, e suo processo di fabbricazione
US9545757B1 (en) * 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
US9314974B2 (en) 2013-01-07 2016-04-19 The Boeing Company Method and apparatus for fabricating contoured laminate structures
US10828846B2 (en) 2013-01-07 2020-11-10 The Boeing Company Method and apparatus for fabricating contoured laminate structures
US10399284B2 (en) 2014-05-16 2019-09-03 The Boeing Company Method and apparatus for forming contoured composite laminates
US9782937B1 (en) 2014-05-16 2017-10-10 The Boeing Company Apparatus for forming contoured composite laminates
EP3000586B1 (de) 2014-09-26 2019-03-20 Airbus Operations, S.L. Verfahren zur Herstellung eines Verbundstoffmaterialteils mit einer Bahn und mindestens einem Flansch
FR3034704B1 (fr) 2015-04-08 2019-12-13 Cotesa Gmbh Couche de fibres pour stratifies courbes en materiau composite a base de fibres et procede de depose de couches de fibres ouvertes en eventail
DE102015110195A1 (de) 2015-06-24 2016-12-29 Airbus Operations Gmbh Vorrichtung und Verfahren zum Umformen eines Faserhalbzeugs
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
WO2018168202A1 (ja) * 2017-03-17 2018-09-20 株式会社Subaru 繊維材の賦形装置及び繊維材の賦形方法
FR3081369B1 (fr) 2018-05-28 2020-05-08 Stelia Aerospace Dispositif et procede de mise en forme d'une piece d'ebauche pour la formation d'une piece thermoplastique structurelle
US11014314B2 (en) 2018-06-28 2021-05-25 The Boeing Company End effector for forming prepreg plies on highly contoured surfaces
US11305498B2 (en) 2018-12-21 2022-04-19 The Boeing Company System and method for fabricating a composite ply layup
US11318689B2 (en) 2018-12-21 2022-05-03 The Boeing Company Ply transporting and compacting apparatus and method therefor
ES2958761T3 (es) * 2019-11-13 2024-02-14 Airbus Operations Slu Dispositivo y método de formación de un laminado compuesto para obtener un perfil en forma de Z
WO2021157082A1 (ja) * 2020-02-07 2021-08-12 三菱重工業株式会社 複合材構造体の製造方法及び積層体の製造方法並びに積層体及び積層型
US11824938B1 (en) 2022-10-28 2023-11-21 Splunk Inc. External sensor integration at edge device for delivery of data to intake system
US12617162B2 (en) * 2022-11-14 2026-05-05 Rohr, Inc. Forming thermoplastic structure stamping blank using automated fiber placement device

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2593714A (en) * 1943-06-30 1952-04-22 Roy H Robinson Method of making cellular structures
GB1258456A (de) * 1969-03-27 1971-12-30
US3913290A (en) * 1974-03-25 1975-10-21 Avco Corp Fire insulation edge reinforcements for structural members
DE3003552C2 (de) * 1980-01-31 1982-06-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flächenbauteil, insbesondere für ein Luftfahrzeug
GB2105254B (en) * 1981-06-24 1984-05-10 Permabond Adhesives Top-hat stiffeners for grp and other panels of synethetic plastics materials
IT1218709B (it) * 1981-06-30 1990-04-19 Boeing Co Metodo di fabbricazione di un preformato utilizzando un materiale composito rinforzato con fibre
FR2544050A1 (fr) * 1983-04-11 1984-10-12 Lombard Gerard Profile leger en plastique arme avec armature interne rigidificatrice
DK92684D0 (da) 1983-04-20 1984-02-23 Itt Profil eller konstruktionselement af et armeret kompositmateriale samt maskine og fremgangsmade til fremstilling heraf
US4576849A (en) * 1983-06-06 1986-03-18 Hercules Incorporated Curved composite beam
US4512835A (en) * 1983-06-06 1985-04-23 Hercules Incorporated Method of making a curved composite beam
US4475976A (en) * 1983-12-23 1984-10-09 The Boeing Company Method and apparatus for forming composite material articles
US4955803A (en) * 1986-02-03 1990-09-11 The Board Of Trustees Of The Leland Stanford Junior University Apparatus for forming fiber composite materials
FR2635484B1 (fr) * 1988-08-18 1991-04-05 Aerospatiale Procede et dispositifs de fabrication de pieces planes incurvees en materiau composite
FR2635714B1 (fr) * 1988-08-26 1991-02-01 Brisard Machines Outils Dispositif de nappage pour la mise en place automatique d'une nappe de fibres sur un moule et machine comportant un tel dispositif
JP2554063Y2 (ja) * 1989-10-17 1997-11-12 財団法人日本航空機開発協会 胴体壁内装板
US5223067A (en) * 1990-02-28 1993-06-29 Fuji Jukogyo Kabushiki Kaisha Method of fabricating aircraft fuselage structure
DE4137649C2 (de) * 1991-11-15 1997-11-20 Gerhard Dingler Bauelement
US6017048A (en) * 1992-06-05 2000-01-25 Fritschen; Thomas M. Aero bicycle frame
US5648109A (en) * 1995-05-03 1997-07-15 Massachusetts Institute Of Technology Apparatus for diaphragm forming
FR2766407B1 (fr) * 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US6054197A (en) * 1997-09-19 2000-04-25 State University Of New York At Albany Structural elements
GB9828368D0 (en) * 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
US6655633B1 (en) * 2000-01-21 2003-12-02 W. Cullen Chapman, Jr. Tubular members integrated to form a structure
US7056402B2 (en) * 2000-11-21 2006-06-06 Eads Deutschland Gmbh Technical production method, tension module and sewing material holder for creating textile preforms for the production of fibre-reinforced plastic components
KR100427405B1 (ko) * 2001-03-07 2004-04-17 박재만 피에스에스씨 합성거더
EP1342553B1 (de) * 2002-03-08 2016-05-18 Airbus Operations GmbH Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens
US20050210820A1 (en) * 2004-03-24 2005-09-29 Shinmaywa Industries, Ltd. Frame and method for fabricating the same
US7434366B2 (en) * 2005-01-11 2008-10-14 A. Zahner Company I-beam with curved flanges
AT501521B1 (de) * 2005-01-27 2013-07-15 Krestel Stefan Trägerartiges, aus einzelteilen zusammengesetztes bauelement sowie verfahren zur herstellung des bauelements
US7673433B2 (en) * 2005-04-29 2010-03-09 The Boeing Company Damage-tolerant monolithic structures
US8632653B2 (en) * 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements

Also Published As

Publication number Publication date
EP1666353B1 (de) 2010-02-10
US7670525B2 (en) 2010-03-02
US8151529B2 (en) 2012-04-10
US20060216480A1 (en) 2006-09-28
US20100148005A1 (en) 2010-06-17
DE602004025482D1 (de) 2010-03-25
ES2338551T3 (es) 2010-05-10
EP1666353A1 (de) 2006-06-07

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