DE60101819D1 - Verfahren zur Herstellung eines halbgehärteten faserverstärkten Verbundteils mit einem Stufenrand, und Verfahren zur Herstellung eines mit diesem Verbundteil vorgeformter Struktur - Google Patents

Verfahren zur Herstellung eines halbgehärteten faserverstärkten Verbundteils mit einem Stufenrand, und Verfahren zur Herstellung eines mit diesem Verbundteil vorgeformter Struktur

Info

Publication number
DE60101819D1
DE60101819D1 DE60101819T DE60101819T DE60101819D1 DE 60101819 D1 DE60101819 D1 DE 60101819D1 DE 60101819 T DE60101819 T DE 60101819T DE 60101819 T DE60101819 T DE 60101819T DE 60101819 D1 DE60101819 D1 DE 60101819D1
Authority
DE
Germany
Prior art keywords
producing
composite part
semi
fiber reinforced
step edge
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
DE60101819T
Other languages
English (en)
Other versions
DE60101819T2 (de
Inventor
Junichi Kondo
Nobuo Matsui
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor Co Ltd
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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Publication of DE60101819D1 publication Critical patent/DE60101819D1/de
Application granted granted Critical
Publication of DE60101819T2 publication Critical patent/DE60101819T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • 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
    • 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
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Reinforced Plastic Materials (AREA)
DE60101819T 2000-05-01 2001-05-01 Verfahren zur Herstellung eines halbgehärteten faserverstärkten Verbundteils mit einem Stufenrand, und Verfahren zur Herstellung eines mit diesem Verbundteil vorgeformter Struktur Expired - Lifetime DE60101819T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2000132681 2000-05-01
JP2000132681A JP4425424B2 (ja) 2000-05-01 2000-05-01 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法

Publications (2)

Publication Number Publication Date
DE60101819D1 true DE60101819D1 (de) 2004-02-26
DE60101819T2 DE60101819T2 (de) 2004-07-01

Family

ID=18641327

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60101819T Expired - Lifetime DE60101819T2 (de) 2000-05-01 2001-05-01 Verfahren zur Herstellung eines halbgehärteten faserverstärkten Verbundteils mit einem Stufenrand, und Verfahren zur Herstellung eines mit diesem Verbundteil vorgeformter Struktur

Country Status (4)

Country Link
US (1) US6730184B2 (de)
EP (1) EP1151850B1 (de)
JP (1) JP4425424B2 (de)
DE (1) DE60101819T2 (de)

Families Citing this family (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0122050D0 (en) 2001-09-13 2001-10-31 Bae Systems Plc Composite material structure
US7229513B2 (en) * 2003-10-31 2007-06-12 The Boeing Company Method for an integral composite forward flange in a composite
JP4218519B2 (ja) * 2003-12-26 2009-02-04 戸田工業株式会社 磁界アンテナ、それを用いて構成したワイヤレスシステムおよび通信システム
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US8920594B2 (en) * 2005-08-03 2014-12-30 Sikorsky Aircraft Corporation Composite thermoplastic matrix airframe structure and method of manufacture therefore
ATE409577T1 (de) 2005-12-20 2008-10-15 Saab Ab Versteifungselement und verfahren zu dessen herstellung
ES2311937T3 (es) * 2005-12-20 2009-02-16 Saab Ab Elemento de rigidizacion y procedimiento para la fabricacion de elemento de rigidizacion.
JP2008055609A (ja) 2006-08-29 2008-03-13 Jamco Corp 複合材の未硬化連続予備成形方法
US7963483B2 (en) * 2006-10-31 2011-06-21 Airbus Operations Gmbh Stiffening element carbon-glass layered foot section
US7686251B2 (en) * 2006-12-13 2010-03-30 The Boeing Company Rib support for wing panels
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
FR2909919B1 (fr) * 2006-12-13 2012-12-07 Eads Ccr Procede de fabrication d'une piece complexe en materiau composite a fibres longues et a matrice thermodurcissable
FR2924378B1 (fr) * 2007-03-29 2010-01-01 Carbone Forge Procede de fabrication par moulage d'une piece composite thermoplastique.
EP2156943A4 (de) * 2007-04-30 2013-11-27 Airbus Operations Sl Aus verbundmaterial hergestellte komplexe geometrien und verfahren zur herstellung der geometrien
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
DE102007032819B4 (de) * 2007-07-13 2014-08-28 Airbus Operations Gmbh Verfahren und Werkzeug zur Herstellung eines T-Stringers
US7968169B2 (en) 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
ITTO20070659A1 (it) * 2007-09-20 2009-03-21 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento strutturale curvilineo in materiale composito avente una sezione aperta complessa.
US7871553B2 (en) * 2007-09-21 2011-01-18 The Boeing Company Process for forming curved thermoplastic composite material
JP2009234046A (ja) 2008-03-27 2009-10-15 Jamco Corp 複合材の未硬化連続予備成形方法
US8079549B2 (en) * 2008-06-30 2011-12-20 EMBRAER—Empresa Brasileira de Aeronautica S.A. Monolithic integrated structural panels especially useful for aircraft structures
JP5322594B2 (ja) * 2008-11-12 2013-10-23 株式会社ジャムコ 断面の異なる複合材型材の連続成形方法
FR2949208B1 (fr) * 2009-08-18 2014-02-21 Eads Europ Aeronautic Defence Procede de fabrication de pieces composites permettant une reparabilite desdites pieces
DE102009057009B4 (de) * 2009-12-04 2015-01-08 Airbus Defence and Space GmbH Vorrichtung und Verfahren zur Herstellung eines schalenförmigen Verbundbauteils
DE102010062871A1 (de) * 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Infusionsverfahren und Aufbau eines Infusionsverfahrens
CA2804960A1 (en) 2010-07-13 2012-01-19 Learjet Inc. Composite structure and method of forming same
CN102092135A (zh) * 2010-12-13 2011-06-15 中国航空工业集团公司北京航空材料研究院 一种提高复合材料翼面结构刚度的方法
US20130119191A1 (en) * 2011-11-10 2013-05-16 General Electric Company Load-bearing structures for aircraft engines and processes therefor
EP2922685B1 (de) * 2012-11-26 2019-04-17 Cytec Industries Inc. Bonding von verbundstoffen
US9440401B1 (en) * 2012-12-10 2016-09-13 The Boeing Company Method for producing composite laminated parts with non-ruled surfaces
ES2626352T3 (es) * 2013-05-30 2017-07-24 Airbus Operations S.L. Herramienta híbrida para curar piezas de material compuesto
JP6239272B2 (ja) * 2013-06-04 2017-11-29 三菱航空機株式会社 繊維強化プラスチック部材の成形方法および成形装置
JP6220162B2 (ja) * 2013-06-07 2017-10-25 三菱航空機株式会社 繊維強化プラスチック構造体の製造装置および製造方法
US9840041B2 (en) 2013-12-20 2017-12-12 Saab Ab Stiffening element and reinforced structure
FR3020780B1 (fr) * 2014-05-09 2017-01-13 Airbus Operations Sas Procede de fabrication d'une piece en materiau composite pour structure d'aeronef par pultrusion et cocuisson
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
US9849967B2 (en) * 2015-04-01 2017-12-26 The Boeing Company Composite rib for an aircraft
JP6581875B2 (ja) * 2015-10-06 2019-09-25 三菱重工業株式会社 複合材の成形方法
WO2018170314A1 (en) 2017-03-16 2018-09-20 The Boeing Company Systems and methods of curing a thermoset composite to a target state of cure
JP2020511334A (ja) 2017-03-16 2020-04-16 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 第１の熱硬化性複合材と第２の熱硬化性複合材を共接合して硬化複合材部品を構成する方法
US10773430B2 (en) * 2017-04-25 2020-09-15 The Boeing Company Thermoplastic composite part manufacturing system and method
EP3647035B1 (de) * 2017-08-10 2021-10-27 Mitsubishi Heavy Industries, Ltd. Verbundstoffmaterialformgestell und verbundstoffmaterialformverfahren
US11390045B2 (en) * 2018-09-07 2022-07-19 Textron Innovations Inc. Molding assembly and method of co-curing stiffener with panel
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
DE102019114710A1 (de) * 2019-05-31 2020-12-03 Airbus Operations Gmbh Vorrichtung und Verfahren
US11897074B2 (en) 2020-02-20 2024-02-13 The Boeing Company Needle arrays for forming ultrasonic perforations, and methods of making the same
US11840362B2 (en) 2020-03-19 2023-12-12 Mitsubishi Heavy Industries, Ltd. Support body and support body mounting method
US20230100087A1 (en) * 2020-06-17 2023-03-30 Mitsubishi Heavy Industries, Ltd. Jig and composite material processing method
US11752708B2 (en) 2021-09-10 2023-09-12 The Boeing Company Uncured composite structures, cured composite structures, and methods of curing uncured composite structures

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4151031A (en) 1977-07-05 1979-04-24 General Dynamics Corporation Apparatus for continuously forming composite shapes
JPS59129119A (ja) * 1983-01-17 1984-07-25 Mitsubishi Heavy Ind Ltd 繊維強化プラスチック製品
JPH01109378U (de) * 1988-01-14 1989-07-24
JPH03253309A (ja) * 1990-03-02 1991-11-12 Tonen Corp 繊維強化樹脂プリプレグ
JPH058316A (ja) * 1991-07-05 1993-01-19 Mitsubishi Heavy Ind Ltd 複合材製構造体の製造方法
US5242523A (en) 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
JPH07115412B2 (ja) * 1993-05-21 1995-12-13 日機装株式会社 格子状構造物およびその製造方法
JP3796778B2 (ja) * 1995-09-22 2006-07-12 いすゞ自動車株式会社 シェアージョイント構造体及びその接着方法
JP4076241B2 (ja) * 1996-10-30 2008-04-16 本田技研工業株式会社 繊維強化プラスチック成形品の製造方法
JP2000015710A (ja) * 1998-07-03 2000-01-18 Nissan Motor Co Ltd Ｆｒｐ製構造体の製造方法
GB9828368D0 (en) * 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
JP4425422B2 (ja) * 2000-04-14 2010-03-03 本田技研工業株式会社 複合材製構造体の製造方法、及びそれにより製造される複合材製構造体

Also Published As

Publication number Publication date
EP1151850A3 (de) 2002-02-06
US20010035249A1 (en) 2001-11-01
JP4425424B2 (ja) 2010-03-03
JP2001315149A (ja) 2001-11-13
EP1151850A2 (de) 2001-11-07
EP1151850B1 (de) 2004-01-21
DE60101819T2 (de) 2004-07-01
US6730184B2 (en) 2004-05-04

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