DE602007010760D1 - Vorrichtung und verfahren zur herstellung einer strukturellen faser-verbund-komponente mit grosser fläche - Google Patents

Vorrichtung und verfahren zur herstellung einer strukturellen faser-verbund-komponente mit grosser fläche

Info

Publication number
DE602007010760D1
DE602007010760D1 DE602007010760T DE602007010760T DE602007010760D1 DE 602007010760 D1 DE602007010760 D1 DE 602007010760D1 DE 602007010760 T DE602007010760 T DE 602007010760T DE 602007010760 T DE602007010760 T DE 602007010760T DE 602007010760 D1 DE602007010760 D1 DE 602007010760D1
Authority
DE
Germany
Prior art keywords
shaping body
controllable
unit
placing
reception
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
DE602007010760T
Other languages
English (en)
Inventor
Joerg Schendel
Bernd Ostermeier
Thomas Konsolke
Ralf-Peter Dittmann
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
Publication of DE602007010760D1 publication Critical patent/DE602007010760D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C70/30—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]
    • 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
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/0094—Geometrical properties
    • 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
    • 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
    • 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
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1788—Work traversing type and/or means applying work to wall or static structure
    • 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
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1788—Work traversing type and/or means applying work to wall or static structure
    • Y10T156/1795—Implement carried web supply
DE602007010760T 2006-05-05 2007-05-04 Vorrichtung und verfahren zur herstellung einer strukturellen faser-verbund-komponente mit grosser fläche Active DE602007010760D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US79807106P 2006-05-05 2006-05-05
DE102006021110A DE102006021110B4 (de) 2006-05-05 2006-05-05 Vorrichtung und Verfahren zum Herstellen eines großflächigen Faserverbund-Strukturbauteils
PCT/EP2007/054337 WO2007128788A1 (en) 2006-05-05 2007-05-04 Apparatus and method for producing a large-area fibre-composite structural component

Publications (1)

Publication Number Publication Date
DE602007010760D1 true DE602007010760D1 (de) 2011-01-05

Family

ID=38564911

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102006021110A Expired - Fee Related DE102006021110B4 (de) 2006-05-05 2006-05-05 Vorrichtung und Verfahren zum Herstellen eines großflächigen Faserverbund-Strukturbauteils
DE602007010760T Active DE602007010760D1 (de) 2006-05-05 2007-05-04 Vorrichtung und verfahren zur herstellung einer strukturellen faser-verbund-komponente mit grosser fläche

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102006021110A Expired - Fee Related DE102006021110B4 (de) 2006-05-05 2006-05-05 Vorrichtung und Verfahren zum Herstellen eines großflächigen Faserverbund-Strukturbauteils

Country Status (11)

Country Link
US (1) US8088236B2 (de)
EP (1) EP2015922B1 (de)
JP (1) JP5027215B2 (de)
CN (1) CN101426636B (de)
AT (1) ATE489221T1 (de)
BR (1) BRPI0712293A2 (de)
CA (1) CA2649070C (de)
DE (2) DE102006021110B4 (de)
ES (1) ES2356095T3 (de)
RU (1) RU2438874C2 (de)
WO (1) WO2007128788A1 (de)

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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
DE102010040970A1 (de) 2010-09-17 2012-03-22 Airbus Operations Gmbh Verfahren und Vorrichtung zur Bereitstellung eines trockenen textilen Vorformlings
DE102012219267A1 (de) * 2012-10-22 2014-04-24 Wobben Properties Gmbh Verfahren und Vorrichtung zur Herstellung von Vorformlingen zum Herstellen eines Rotorblattes
CA2895564C (en) * 2012-12-21 2020-03-24 Short Brothers Plc Fabric handling apparatus
CN103507277B (zh) * 2013-10-23 2015-06-17 连云港中复连众复合材料集团有限公司 一种风力发电机叶片根部铺层的改良方法
EP3083459B1 (de) 2013-12-19 2020-09-23 Short Brothers Plc Gewebepositionierungsvorrichtung
DE102014107290A1 (de) * 2014-05-23 2015-11-26 Ssc Swiss Shielding Corporation Ag Thermisches Isolierelement und Verfahren zur Montage eines thermischen Isolierelements an eine Innenraumoberfläche eines Schienenfahrzeugs
US10112348B2 (en) 2015-03-02 2018-10-30 Ingersoll Machine Tools, Inc. Fiber placement system
RU2632864C2 (ru) * 2015-06-25 2017-10-11 Владимир Николаевич Фетисов Способ изготовления оболочек пневмоконструкций и полотен большой площади из пленочного материала
DE102016002844B3 (de) * 2016-03-10 2017-08-10 Premium Aerotec Gmbh Strukturbauteil, Verfahren zur Herstellung eines Strukturbauteils, Druckrumpf für ein Fahrzeug mit Strukturbauteil
CN109591323B (zh) * 2018-12-05 2020-10-20 中航复合材料有限责任公司 一种适用于z形复合材料机身隔框毛坯的铺放装置
NL2027433B1 (en) * 2021-01-26 2022-08-19 Boeing Co Contour enforcement for line assembled fuselage segments
JP2022081434A (ja) * 2020-11-18 2022-05-31 ザ・ボーイング・カンパニー 航空機用の大型複合部品の脱型
JP2022080863A (ja) 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー ラインで組み立てられる胴体セグメントのための輪郭強化
EP4001128A1 (de) 2020-11-18 2022-05-25 The Boeing Company Konturendurchsetzung für bandmontierte rumpfsegmente
US20230364867A1 (en) * 2022-05-11 2023-11-16 Airbus Operations Sl Device and method for manufacturing composite parts for an aircraft bulkhead

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US3574040A (en) * 1967-06-29 1971-04-06 Gen Dynamics Corp Apparatus for making laminated structural shapes by the controlled detrusive placement and polymerization of tectonic filamentous tapes
US3810805A (en) * 1972-04-14 1974-05-14 Goldsworthy Eng Inc Geodesic path length compensator for composite-tape placement head
EP0062991B1 (de) * 1981-04-11 1986-09-17 Gkn Technology Limited Herstellung von Gegenständen aus zusammengesetztem Material
GB8305749D0 (en) * 1983-03-02 1983-04-07 British Aerospace Tape laying apparatus
US4588466A (en) * 1983-04-08 1986-05-13 Vektronics Manufacturing, Inc. Tape laying method and apparatus
FR2548084B1 (fr) 1983-06-28 1985-12-13 Ato Chimie Procede de fabrication d'objets composites et objets composites obtenus
DE3507720C2 (de) 1985-03-05 1997-08-14 Rieter Automotive Int Ag Verfahren und Vorrichtung zum Herstellen eines Rohlings aus glasfaserverstärktem Kunststoff
JPS63114608A (ja) * 1986-10-31 1988-05-19 Mazda Motor Corp Ｆｒｐ製ホイ−ルデイスクの製造方法
FR2617468B1 (fr) * 1987-06-30 1989-12-15 Coopelin Procede et machine de formation d'un empilage a plat de feuilles de format predetermine
JPH04344225A (ja) * 1991-05-22 1992-11-30 Mitsubishi Heavy Ind Ltd 複合材自動積層装置
GB2268704B (en) * 1992-07-16 1996-01-10 British Aerospace Layup preparation for fibre reinforced composites
US5746553A (en) * 1996-04-08 1998-05-05 The Boeing Company Dual purpose lay-up tool
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JP3632177B2 (ja) * 2002-11-29 2005-03-23 川崎重工業株式会社 プリプレグ幅変更自動積層方法及びその装置
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Also Published As

Publication number Publication date
DE102006021110B4 (de) 2011-04-21
CN101426636A (zh) 2009-05-06
RU2438874C2 (ru) 2012-01-10
JP5027215B2 (ja) 2012-09-19
ES2356095T3 (es) 2011-04-04
US20100006202A1 (en) 2010-01-14
WO2007128788A1 (en) 2007-11-15
US8088236B2 (en) 2012-01-03
DE102006021110A1 (de) 2007-11-08
ATE489221T1 (de) 2010-12-15
JP2009536129A (ja) 2009-10-08
EP2015922A1 (de) 2009-01-21
EP2015922B1 (de) 2010-11-24
RU2008142970A (ru) 2010-06-10
BRPI0712293A2 (pt) 2012-01-10
CA2649070A1 (en) 2007-11-15
CN101426636B (zh) 2012-09-05
CA2649070C (en) 2012-11-20

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