DE60100821D1 - Verfahren zur Herstellung einer Verbundstruktur und damit hergestellte Verbundstruktur - Google Patents

Verfahren zur Herstellung einer Verbundstruktur und damit hergestellte Verbundstruktur

Info

Publication number
DE60100821D1
DE60100821D1 DE60100821T DE60100821T DE60100821D1 DE 60100821 D1 DE60100821 D1 DE 60100821D1 DE 60100821 T DE60100821 T DE 60100821T DE 60100821 T DE60100821 T DE 60100821T DE 60100821 D1 DE60100821 D1 DE 60100821D1
Authority
DE
Germany
Prior art keywords
composite structure
producing
method
produced therewith
structure produced
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
DE60100821T
Other languages
English (en)
Other versions
DE60100821T2 (de
Inventor
Toru Fujihira
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
Priority to JP2000113439 priority Critical
Priority to JP2000113439A priority patent/JP4425422B2/ja
Application filed by Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Application granted granted Critical
Publication of DE60100821D1 publication Critical patent/DE60100821D1/de
Publication of DE60100821T2 publication Critical patent/DE60100821T2/de
Application status is Active legal-status Critical
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
    • B29C70/30Shaping 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
    • B29C70/342Shaping 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 isostatic pressure
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2007/00Flat articles, e.g. films or sheets
    • B29L2007/002Panels; Plates; Sheets
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • Y02T50/42Airframe
    • Y02T50/43Composites
DE60100821T 2000-04-14 2001-04-17 Verfahren zur Herstellung einer Verbundstruktur und damit hergestellte Verbundstruktur Active DE60100821T2 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2000113439 2000-04-14
JP2000113439A JP4425422B2 (ja) 2000-04-14 2000-04-14 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

Publications (2)

Publication Number Publication Date
DE60100821D1 true DE60100821D1 (de) 2003-10-30
DE60100821T2 DE60100821T2 (de) 2004-04-08

Family

ID=18625401

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60100821T Active DE60100821T2 (de) 2000-04-14 2001-04-17 Verfahren zur Herstellung einer Verbundstruktur und damit hergestellte Verbundstruktur

Country Status (4)

Country Link
US (1) US6802931B2 (de)
EP (1) EP1145828B1 (de)
JP (1) JP4425422B2 (de)
DE (1) DE60100821T2 (de)

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JP4425424B2 (ja) * 2000-05-01 2010-03-03 本田技研工業株式会社 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
JP2005231618A (ja) * 2004-01-23 2005-09-02 Toray Ind Inc 自動車用外板部材
US7134629B2 (en) 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7159822B2 (en) * 2004-04-06 2007-01-09 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
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
US7335012B2 (en) * 2004-12-22 2008-02-26 General Electric Company Apparatus for fabricating reinforced composite materials
US7332049B2 (en) * 2004-12-22 2008-02-19 General Electric Company Method for fabricating reinforced composite materials
US7431978B2 (en) * 2004-12-22 2008-10-07 General Electric Company Reinforced matrix composite containment duct
US8920594B2 (en) * 2005-08-03 2014-12-30 Sikorsky Aircraft Corporation Composite thermoplastic matrix airframe structure and method of manufacture therefore
DE602005025490D1 (de) 2005-10-17 2011-02-03 Saab Ab Verfahren zur Herstellung eines gekrümmten Gegenstands aus Verbundwerkstoff sowie durch dieses Verfahren hergestellter Gegenstand
FR2906785B1 (fr) * 2006-10-10 2009-12-04 Airbus France Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage
DE102007003275B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Schalenelement als Teil eines Flugzeugrumpfes
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8043458B2 (en) * 2007-06-21 2011-10-25 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
ITMI20071448A1 (it) * 2007-07-18 2009-01-19 Alenia Aermacchi Spa Procedimento di realizzazione di un pannello fonoassorbente per veicoli
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
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.
DE102009013585B4 (de) 2009-03-17 2012-01-26 Airbus Operations Gmbh Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise
CN102019592B (zh) 2009-09-10 2012-07-04 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料加筋壁板成形的定位装置
US8608884B2 (en) * 2009-09-14 2013-12-17 Joel A. Stanley Method and system for mounting objects to polymeric membranes
US9121180B2 (en) * 2009-09-14 2015-09-01 Bwdt, Llc System for mounting objects to polymeric membranes
US8499524B2 (en) 2009-09-14 2013-08-06 Joel A. Stanley System for mounting objects to polymeric membranes
US7935202B2 (en) * 2009-09-14 2011-05-03 Stanley Joel A System for mounting objects to polymeric membranes
US9175479B2 (en) 2009-09-14 2015-11-03 Bwdt, Llc System for mounting objects to polymeric membranes
US8557070B2 (en) 2009-09-14 2013-10-15 Joel A. Stanley Method of mounting objects to polymeric membranes
US8623158B2 (en) 2009-09-14 2014-01-07 Joel A. Stanley System for mounting objects to polymeric membranes
US9121545B2 (en) 2009-09-14 2015-09-01 Bwdt, Llc System for mounting objects to polymeric membranes
DE102009057006A1 (de) * 2009-12-04 2011-06-09 Eads Deutschland Gmbh Vorrichtung und Verfahren zur Herstellung eines gekrümmten Verbundbauteils sowie Verbundbauteil
US8491743B2 (en) * 2009-12-15 2013-07-23 The Boeing Company Composite ply stabilizing method
JP5550370B2 (ja) * 2010-02-05 2014-07-16 本田技研工業株式会社 航空機翼構造の製造方法
CN101791821B (zh) * 2010-04-08 2011-09-14 中国航空工业集团公司北京航空制造工程研究所 一种大尺寸复合材料长桁的成形装置
CN103249542A (zh) 2010-07-13 2013-08-14 里尔喷射机公司 复合结构及其形成方法
US20120199292A1 (en) * 2011-02-03 2012-08-09 Sikorsky Aircraft Corporation Ply locking for honeycomb panels
CN103341987B (zh) * 2013-06-17 2015-09-09 沈阳飞机工业(集团)有限公司 Ω长桁纵横加筋复合材料整体壁板共固化工艺
EP2865516B1 (de) 2013-10-28 2016-03-09 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Oberflächeversteifte Verbundplatte und Verfahren zu deren Herstellung
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
EP3272640B1 (de) 2016-07-21 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hubschrauber mit einem rumpf und einem verbundstoffheckausleger

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JPS5942621B2 (de) * 1981-01-12 1984-10-16 Fuji Heavy Ind Ltd
US4416349A (en) 1981-09-30 1983-11-22 The Boeing Company Viscoelastically damped reinforced skin structures
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
US5451377A (en) 1993-09-29 1995-09-19 Rockwell International Corp. Composite structures and methods of manufacturing such structures
US5580502A (en) 1995-03-23 1996-12-03 Sikorsky Aircraft Corporation Method of fabricating a composite article having an integral, co-cured composite stiffening member
FR2771330B1 (fr) 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
GB9802597D0 (en) * 1998-02-07 1998-04-01 Hurel Dubois Uk Ltd Panels and structures
BR9911045B1 (pt) * 1998-05-22 2009-08-11 uso de um tecido tratado quanto à rigidez, método para produzir um tecido tratado quanto à rigidez, tecido tratado quanto à rigidez, uso de uma matéria-prima de tecido tratado quanto à rigidez, método para produzir uma matéria-prima de tecido tratado quanto à rigidez, uso de uma camada pré-impregnada tratada quanto à rigidez, método para produzir uma camada pré-impregnada tratada quanto à rigidez para um precursor de estrutra em sanduìche alveolada tratada quanto à rigidez, estrutura em sanduìche alveolada tratada quanto à rigidez, método de produzir um precursor de estrutura em sanduìche alveolada tratada quanto à rigidez e método de produzir uma estrutura em sanduìche alveolada tratada quanto à rigidez.
US6197146B1 (en) * 1998-12-21 2001-03-06 Sikorsky Aircraft Corporation Method and apparatus for forming airfoil structures
US6523246B1 (en) * 1999-11-26 2003-02-25 Honda Giken Kogyo Kabushiki Kaisha Jig used for formation of fiber-reinforced composite structure and method for formation of fiber-reinforced composite structure using jig
JP4191343B2 (ja) * 1999-11-26 2008-12-03 本田技研工業株式会社 ハニカムサンドイッチパネルの製造方法

Also Published As

Publication number Publication date
US6802931B2 (en) 2004-10-12
EP1145828B1 (de) 2003-09-24
DE60100821T2 (de) 2004-04-08
EP1145828A2 (de) 2001-10-17
US20010030380A1 (en) 2001-10-18
JP4425422B2 (ja) 2010-03-03
EP1145828A3 (de) 2002-03-20
JP2001293738A (ja) 2001-10-23

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