DE102007060029A1 - Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile - Google Patents

Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile Download PDF

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Publication number
DE102007060029A1
DE102007060029A1 DE102007060029A DE102007060029A DE102007060029A1 DE 102007060029 A1 DE102007060029 A1 DE 102007060029A1 DE 102007060029 A DE102007060029 A DE 102007060029A DE 102007060029 A DE102007060029 A DE 102007060029A DE 102007060029 A1 DE102007060029 A1 DE 102007060029A1
Authority
DE
Germany
Prior art keywords
carrier
mold
pressure
tubular
support surface
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.)
Ceased
Application number
DE102007060029A
Other languages
German (de)
English (en)
Inventor
Hauke Lengsfeld
Volker Reye
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 GmbH
Original Assignee
Airbus Operations GmbH
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 GmbH filed Critical Airbus Operations GmbH
Priority to DE102007060029A priority Critical patent/DE102007060029A1/de
Priority to EP08860048.1A priority patent/EP2229273B1/de
Priority to BRPI0821246-5A priority patent/BRPI0821246A2/pt
Priority to CA2707802A priority patent/CA2707802A1/en
Priority to RU2010122662/05A priority patent/RU2488488C2/ru
Priority to PCT/EP2008/065355 priority patent/WO2009074419A1/de
Priority to JP2010537352A priority patent/JP2011506136A/ja
Priority to CN200880120453.0A priority patent/CN101896329B/zh
Publication of DE102007060029A1 publication Critical patent/DE102007060029A1/de
Priority to US12/794,487 priority patent/US20100276069A1/en
Priority to US14/285,704 priority patent/US9180628B2/en
Priority to US14/928,389 priority patent/US20160129647A1/en
Ceased 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
    • B29C70/42—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
    • B29C70/48—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 and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
    • B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
    • 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
    • B29C70/30—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
    • B29C70/36—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 impregnating by casting, e.g. vacuum casting
    • 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
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • 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
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • 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
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D23/00—Producing tubular articles
    • B29D23/001—Pipes; Pipe joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B30—PRESSES
    • B30B—PRESSES IN GENERAL
    • B30B5/00—Presses characterised by the use of pressing means other than those mentioned in the preceding groups
    • B30B5/02—Presses characterised by the use of pressing means other than those mentioned in the preceding groups wherein the pressing means is in the form of a flexible element, e.g. diaphragm, urged by fluid pressure
    • 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
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0872—Prepregs
    • B29K2105/089—Prepregs fabric
    • 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
    • B29K2307/00—Use of elements other than metals as reinforcement
    • B29K2307/04—Carbon
    • 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
    • B29L2023/00—Tubular articles
    • B29L2023/22—Tubes or pipes, i.e. rigid
    • 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
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
DE102007060029A 2007-12-13 2007-12-13 Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile Ceased DE102007060029A1 (de)

Priority Applications (11)

Application Number Priority Date Filing Date Title
DE102007060029A DE102007060029A1 (de) 2007-12-13 2007-12-13 Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile
PCT/EP2008/065355 WO2009074419A1 (de) 2007-12-13 2008-11-12 Verfahren und vorrichtung zur herstellung röhrenförmiger strukturbauteile
BRPI0821246-5A BRPI0821246A2 (pt) 2007-12-13 2008-11-12 Método e dispositivo para produção de componentes estruturais em formato de tubo
CA2707802A CA2707802A1 (en) 2007-12-13 2008-11-12 Method and device for producing tube-shaped structural components
RU2010122662/05A RU2488488C2 (ru) 2007-12-13 2008-11-12 Способ и устройство для производства цилиндрических конструктивных компонентов
EP08860048.1A EP2229273B1 (de) 2007-12-13 2008-11-12 Verfahren und vorrichtung zur herstellung röhrenförmiger strukturbauteile
JP2010537352A JP2011506136A (ja) 2007-12-13 2008-11-12 筒状の構造部材を製造する方法およびデバイス
CN200880120453.0A CN101896329B (zh) 2007-12-13 2008-11-12 生产管状结构部件的方法和设备
US12/794,487 US20100276069A1 (en) 2007-12-13 2010-06-04 Method and device for the production of tubular structural components
US14/285,704 US9180628B2 (en) 2007-12-13 2014-05-23 Method and device for the production of tubular structural components
US14/928,389 US20160129647A1 (en) 2007-12-13 2015-10-30 Method and device for the production of tubular structural components

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102007060029A DE102007060029A1 (de) 2007-12-13 2007-12-13 Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile

Publications (1)

Publication Number Publication Date
DE102007060029A1 true DE102007060029A1 (de) 2009-06-18

Family

ID=40679895

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102007060029A Ceased DE102007060029A1 (de) 2007-12-13 2007-12-13 Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile

Country Status (9)

Country Link
US (3) US20100276069A1 (https=)
EP (1) EP2229273B1 (https=)
JP (1) JP2011506136A (https=)
CN (1) CN101896329B (https=)
BR (1) BRPI0821246A2 (https=)
CA (1) CA2707802A1 (https=)
DE (1) DE102007060029A1 (https=)
RU (1) RU2488488C2 (https=)
WO (1) WO2009074419A1 (https=)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102029708A (zh) * 2009-09-30 2011-04-27 通用电气公司 阴模中的纤维自动放置
WO2011070002A1 (de) * 2009-12-07 2011-06-16 Airbus Operations Gmbh Vorrichtung und verfahren zur herstellung einer aus einem faserverbundwerkstoff bestehenden rumpfschale für ein luftfahrzeug
DE102010051739B3 (de) * 2010-11-19 2011-12-29 Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg Verfahren und Vorrichtung zum Herstellen von zylindrischen Großstrukturen
DE102010043415A1 (de) * 2010-11-04 2012-05-10 Airbus Operations Gmbh Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung
WO2013075775A3 (de) * 2011-11-22 2013-07-18 Daimler Ag Verfahren zum herstellen eines hohlprofils sowie hohlprofilbauteil
EP2626194A1 (en) * 2012-02-07 2013-08-14 Siemens Aktiengesellschaft Method of manufacturing a turbine blade, system for manufacturing a turbine blade and intermediate member for manufacturing a turbine blade
ITTO20120317A1 (it) * 2012-04-12 2013-10-13 Alenia Aermacchi Spa Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito
DE102012010271A1 (de) * 2012-05-25 2013-11-28 Premium Aerotec Gmbh Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues, sowie Verwendung hierfür
DE102012210043A1 (de) * 2012-06-14 2013-12-19 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung einer Leichtbaustruktur sowie Leichtbaustruktur
DE102012112939A1 (de) * 2012-12-21 2014-06-26 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung und Verfahren zur Infiltration einer Faserpreform
DE102013205089A1 (de) * 2013-03-22 2014-09-25 Supertex Composites Gmbh Verfahren und Herstellungssystem zur Herstellung eines faserverstärkten Strukturbauteils
DE102013209143A1 (de) * 2013-05-16 2014-11-20 Zf Friedrichshafen Ag Verfahren zum Herstellen eines rotationssymmetrischen Faser-Kunststoff-Verbund-Bauteils, Vorrichtung zur Durchführung eines derartigen Verfahrens und rotationssym-metrisches Faser-Kunststoff-Verbund-Bauteil
DE102014217486A1 (de) * 2014-09-02 2016-03-03 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Herstellen von FKV-Bauteilen mit lokaler Verstärkung
EP3278966A1 (en) * 2016-08-02 2018-02-07 The Boeing Company Tubular structure and a method of manufacturing thereof
EP3552773A1 (en) * 2018-04-13 2019-10-16 The Boeing Company System and method for removing a workpiece from a manufacturing fixture
DE102014112311B4 (de) 2014-08-27 2025-06-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Formwerkzeug zur Infusion eines Matrixmaterials

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009057009B4 (de) * 2009-12-04 2015-01-08 Airbus Defence and Space GmbH Vorrichtung und Verfahren zur Herstellung eines schalenförmigen Verbundbauteils
JP6214300B2 (ja) 2012-10-29 2017-10-18 キヤノン株式会社 定着用部材の製造方法及び製造装置
DE102014217039A1 (de) * 2014-08-27 2016-03-03 Bayerische Motoren Werke Aktiengesellschaft Verfahren für die Herstellung eines mit wenigstens einem Verstärkungsschott verstärkten geschlossenen Hohlprofils aus Faserverbundmaterial
CN104494160B (zh) * 2014-11-25 2017-01-25 中联重科股份有限公司 折叠臂架、纤维增强树脂基复合材料臂节及其制造方法
GB2554218A (en) * 2015-03-17 2018-03-28 Harvard College Automated membrane fabrication system
EP3312083B1 (en) * 2015-11-05 2021-10-20 Airbus Operations, S.L.U. Forming tool for manufacturing an aperture surrounding frame for an aircraft fuselage
GB2555089A (en) * 2016-10-11 2018-04-25 Jaguar Land Rover Ltd A Method of moulding a composite structure
ES2954328T3 (es) * 2017-07-25 2023-11-21 Subaru Corp Plantilla de moldeo de materiales compuestos y método de moldeo de materiales compuestos
US11523750B2 (en) 2018-08-06 2022-12-13 Biosense Webster (Israel) Ltd. Assessing tissue contact with catheter using pairs of electrodes and common reference ground established using designed circuit-board capacitance
DE102019007784B4 (de) * 2019-11-09 2021-07-01 Diehl Aviation Laupheim Gmbh Hohlkanal-Herstellung im Sandwich-Panel mit Platzhalter und Sandwich-Panel
CN116442565B (zh) * 2023-04-25 2026-03-10 哈尔滨工程大学 复合材料波纹夹芯圆柱耐压壳一体成型模具及其制备方法
CN117287623A (zh) * 2023-09-08 2023-12-26 浙江大学 用于低温绝热容器外壳的筒体、低温绝热容器及制造设备

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69109642T2 (de) * 1990-12-19 1995-09-21 United Technologies Corp Anpassungsfähige Formgebung von Verbundwerkstoffen.
DE19913079A1 (de) * 1999-03-23 2000-09-28 Bayerische Motoren Werke Ag Bauteil aus einem thermoplastischen Faserverbundwerkstoff und Verfahren zu dessen Herstellung
DE102004006615A1 (de) * 2004-02-10 2005-10-20 Eurocopter Deutschland Verfahren zur Herstellung eines Faserverbundwerkstoff-Hohlbauteils sowie Zwischenprodukt dafür

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2739350A (en) * 1952-01-28 1956-03-27 Northrop Aircraft Inc Method and means of molding
US2815534A (en) * 1954-07-12 1957-12-10 Ising George Earl Process for making a closed one-piece reinforced plastic tank
US2995781A (en) * 1957-11-19 1961-08-15 Clarence L Sipler Method of making tubular conduits
US3049901A (en) * 1960-04-01 1962-08-21 Singer Fidelity Inc Flexible hose
DE3923416A1 (de) * 1989-07-12 1991-01-24 Mecron Med Prod Gmbh Verfahren zur herstellung eines ein hohlprofil aufweisenden koerpers
JP2935722B2 (ja) * 1990-02-28 1999-08-16 富士重工業株式会社 航空機の胴体構造およびその成形方法
FR2704898B1 (fr) 1993-05-03 1995-08-04 Drillflex Structure tubulaire de preforme ou de matrice pour le tubage d'un puits.
FR2769866B1 (fr) * 1997-10-20 2000-01-14 Sarma Procede de moulage, moule de fabrication d'une piece globalement cylindrique a profil creux en matiere composite et piece obtenue grace a ce procede
DE19803909A1 (de) 1998-02-02 1999-08-05 Ver Foerderung Inst Kunststoff Verfahren zur Herstellung von endlosfaserverstärkten Hohlkörpern im Harzinjektionsverfahren
CA2347717A1 (en) 1998-09-30 2000-04-06 Toray Industries, Inc. A fibre-reinforced resin structure having hollow cross section and manufacturing method thereof
JP4346143B2 (ja) * 1999-02-24 2009-10-21 社団法人日本航空宇宙工業会 複合樹脂製品の成形方法及びその装置
US6510961B1 (en) 1999-04-14 2003-01-28 A&P Technology Integrally-reinforced braided tubular structure and method of producing the same
RU2156397C1 (ru) * 1999-06-30 2000-09-20 Государственное предприятие "Производственное объединение "Авангард" Способ ремонта трубопровода (варианты)
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
US20040219855A1 (en) * 2003-05-02 2004-11-04 Tsotsis Thomas K. Highly porous interlayers to toughen liquid-molded fabric-based composites
US20080289743A1 (en) * 2003-05-02 2008-11-27 Tsotsis Thomas K Highly porous interlayers to toughen liquid-molded fabric-based composites
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
JP4826176B2 (ja) * 2005-08-31 2011-11-30 東レ株式会社 強化繊維プリフォームおよびｒｔｍ成形方法
US7824171B2 (en) * 2005-10-31 2010-11-02 The Boeing Company Corner-consolidating inflatable apparatus and method for manufacturing composite structures
WO2008092971A1 (es) * 2007-01-30 2008-08-07 Airbus España, S.L. Estructura de material compuesto para fuselaje de aeronave y su procedimiento de fabricación

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69109642T2 (de) * 1990-12-19 1995-09-21 United Technologies Corp Anpassungsfähige Formgebung von Verbundwerkstoffen.
DE19913079A1 (de) * 1999-03-23 2000-09-28 Bayerische Motoren Werke Ag Bauteil aus einem thermoplastischen Faserverbundwerkstoff und Verfahren zu dessen Herstellung
DE102004006615A1 (de) * 2004-02-10 2005-10-20 Eurocopter Deutschland Verfahren zur Herstellung eines Faserverbundwerkstoff-Hohlbauteils sowie Zwischenprodukt dafür

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102029708A (zh) * 2009-09-30 2011-04-27 通用电气公司 阴模中的纤维自动放置
CN102029708B (zh) * 2009-09-30 2016-01-20 通用电气公司 阴模中的纤维自动放置
US8911585B2 (en) 2009-12-07 2014-12-16 Airbus Operations Gmbh Device and method for manufacturing a fiber-reinforced composite fuselage shell for an aircraft
WO2011070002A1 (de) * 2009-12-07 2011-06-16 Airbus Operations Gmbh Vorrichtung und verfahren zur herstellung einer aus einem faserverbundwerkstoff bestehenden rumpfschale für ein luftfahrzeug
CN102686381A (zh) * 2009-12-07 2012-09-19 空中客车德国运营有限责任公司 用于制造用于飞行器的由纤维复合材料制成的机身外壳的装置和方法
DE102010043415A1 (de) * 2010-11-04 2012-05-10 Airbus Operations Gmbh Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung
US9120274B2 (en) 2010-11-04 2015-09-01 Airbus Operations Gmbh Method for producing a hollow component and device
DE102010043415B4 (de) * 2010-11-04 2015-04-09 Airbus Operations Gmbh Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung
DE102010051739B3 (de) * 2010-11-19 2011-12-29 Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg Verfahren und Vorrichtung zum Herstellen von zylindrischen Großstrukturen
WO2012066017A1 (de) 2010-11-19 2012-05-24 Siempelkamp Maschinen- Und Anlagenbau Gmbh & Co. Kg VERFAHREN UND VORRICHTUNG ZUM HERSTELLEN VON ZYLINDRISCHEN GROßSTRUKTUREN
WO2013075775A3 (de) * 2011-11-22 2013-07-18 Daimler Ag Verfahren zum herstellen eines hohlprofils sowie hohlprofilbauteil
EP2626194A1 (en) * 2012-02-07 2013-08-14 Siemens Aktiengesellschaft Method of manufacturing a turbine blade, system for manufacturing a turbine blade and intermediate member for manufacturing a turbine blade
ITTO20120317A1 (it) * 2012-04-12 2013-10-13 Alenia Aermacchi Spa Procedimento per la fabbricazione di barili integrali di fusoliera in materiale composito
WO2013153537A3 (en) * 2012-04-12 2013-12-05 Alenia Aermacchi S.P.A. A method of manufacturing single piece fuselage barrels in composite material
US9962917B2 (en) 2012-04-12 2018-05-08 Alenia Aermacchi S.P.A. Method of manufacturing single piece fuselage barrels in composite material
US10005243B2 (en) 2012-05-25 2018-06-26 Premium Aerotec Gmbh Method for producing a fibre composite component by means of a vacuum build-up, and use therefor
DE102012010271B4 (de) * 2012-05-25 2017-10-12 Premium Aerotec Gmbh Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues
DE102012010271A1 (de) * 2012-05-25 2013-11-28 Premium Aerotec Gmbh Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues, sowie Verwendung hierfür
DE102012210043A1 (de) * 2012-06-14 2013-12-19 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung einer Leichtbaustruktur sowie Leichtbaustruktur
US10479031B2 (en) 2012-12-21 2019-11-19 ThyssenKrupp Federn und Stabilisatoren GmbH Device and method for infiltrating a fiber preform
DE102012112939A1 (de) * 2012-12-21 2014-06-26 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung und Verfahren zur Infiltration einer Faserpreform
WO2014147230A3 (de) * 2013-03-22 2014-11-20 Supertex Composites Gmbh Verfahren und herstellungssystem zur herstellung eines faserverstärkten strukturbauteils
DE102013205089A1 (de) * 2013-03-22 2014-09-25 Supertex Composites Gmbh Verfahren und Herstellungssystem zur Herstellung eines faserverstärkten Strukturbauteils
DE102013209143A1 (de) * 2013-05-16 2014-11-20 Zf Friedrichshafen Ag Verfahren zum Herstellen eines rotationssymmetrischen Faser-Kunststoff-Verbund-Bauteils, Vorrichtung zur Durchführung eines derartigen Verfahrens und rotationssym-metrisches Faser-Kunststoff-Verbund-Bauteil
DE102014112311B4 (de) 2014-08-27 2025-06-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Formwerkzeug zur Infusion eines Matrixmaterials
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CN101896329A (zh) 2010-11-24
US20100276069A1 (en) 2010-11-04
US20160129647A1 (en) 2016-05-12
US20140346715A1 (en) 2014-11-27
CN101896329B (zh) 2014-04-09
WO2009074419A1 (de) 2009-06-18
EP2229273A1 (de) 2010-09-22
RU2010122662A (ru) 2012-01-20
EP2229273B1 (de) 2016-01-27
RU2488488C2 (ru) 2013-07-27
US9180628B2 (en) 2015-11-10
JP2011506136A (ja) 2011-03-03

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