ATE262408T1 - Verfahren zur herstellung von vorgehärteten teilen aus verbundwerkstoff mit in frischem zustand angewandten versteifern - Google Patents

Verfahren zur herstellung von vorgehärteten teilen aus verbundwerkstoff mit in frischem zustand angewandten versteifern

Info

Publication number
ATE262408T1
ATE262408T1 AT00500167T AT00500167T ATE262408T1 AT E262408 T1 ATE262408 T1 AT E262408T1 AT 00500167 T AT00500167 T AT 00500167T AT 00500167 T AT00500167 T AT 00500167T AT E262408 T1 ATE262408 T1 AT E262408T1
Authority
AT
Austria
Prior art keywords
base part
composite parts
stiffeners
composite material
producing pre
Prior art date
Application number
AT00500167T
Other languages
English (en)
Inventor
Pancorbo Carlos Cerezo
Casado Rafael Dominguez
Castro Nodal Manuel De
Pastor Augusto Perez
Garcia Aquilino Garcia
Garcia Manuel Huertas
Original Assignee
Airbus Espana Sl
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 Espana Sl filed Critical Airbus Espana Sl
Application granted granted Critical
Publication of ATE262408T1 publication Critical patent/ATE262408T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/182Stringers, longerons
    • 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
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/24Moulded or cast structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/246Uncured, e.g. green
    • 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
    • B29L2031/00Other particular articles
    • B29L2031/001Profiled members, e.g. beams, sections
    • B29L2031/003Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • 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
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/42Processes of molding involving cross linking

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
AT00500167T 2000-03-07 2000-07-26 Verfahren zur herstellung von vorgehärteten teilen aus verbundwerkstoff mit in frischem zustand angewandten versteifern ATE262408T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200000551A ES2185443B1 (es) 2000-03-07 2000-03-07 Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco.

Publications (1)

Publication Number Publication Date
ATE262408T1 true ATE262408T1 (de) 2004-04-15

Family

ID=8492610

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00500167T ATE262408T1 (de) 2000-03-07 2000-07-26 Verfahren zur herstellung von vorgehärteten teilen aus verbundwerkstoff mit in frischem zustand angewandten versteifern

Country Status (6)

Country Link
US (1) US6508909B1 (de)
EP (1) EP1134070B1 (de)
AT (1) ATE262408T1 (de)
CA (1) CA2315541C (de)
DE (1) DE60009259T2 (de)
ES (1) ES2185443B1 (de)

Families Citing this family (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4448242B2 (ja) * 2000-09-05 2010-04-07 本田技研工業株式会社 スティフンドパネル用成形補助治具
ES2205961B2 (es) * 2001-02-13 2005-03-01 Eads Construcciones Aeronauticas, S.A. Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.
US6649006B2 (en) 2001-10-09 2003-11-18 Lockheed Martin Corporation Method of making a waffle stiffener
EP1336469A1 (de) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Verfahren zur Herstellung eines Versteifungselementes für ein Flugzeugaussenblech und mit dem Versteifungselement versehenes Aussenblech
US7374715B2 (en) * 2002-05-22 2008-05-20 Northrop Grumman Corporation Co-cured resin transfer molding manufacturing method
US7419627B2 (en) * 2002-09-13 2008-09-02 Northrop Grumman Corporation Co-cured vacuum-assisted resin transfer molding manufacturing method
US7052573B2 (en) 2003-11-21 2006-05-30 The Boeing Company Method to eliminate undulations in a composite panel
EP1543941B1 (de) * 2003-12-16 2006-06-28 Airbus Espana, S.L. Prozess und Werkzeuge zum reduzieren von thermisch induzierten Restspannungen und Formverzerrungen bei monolithischen Verbundstrukturen
ES2246675B1 (es) * 2003-12-30 2007-05-01 Airbus España S.L. Metodo y aparato para la formacion de una bolsa de vacio en la fabricacion de estructuras de material compuesto de gran superficie.
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
US7134629B2 (en) * 2004-04-06 2006-11-14 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
ATE493253T1 (de) * 2005-03-30 2011-01-15 Eads Constr Aeronauticas Sa Verfahren zur herstellung einer monolithischen lüfterhaube
WO2006112823A1 (en) * 2005-04-13 2006-10-26 The Boeing Company Method to eliminate undulations in a composite panel
DE102005026010B4 (de) * 2005-06-07 2010-12-30 Airbus Deutschland Gmbh Verfahren zur Herstellung einer verstärkten Schale zur Bildung von Teilkomponenten für Luftfahrzeuge
WO2007074179A1 (es) * 2005-12-29 2007-07-05 Airbus España, S.L. Procedimiento y útiles para la fabricación de cuadernas de material compuesto
RU2390417C2 (ru) * 2005-12-29 2010-05-27 Айрбус Эспанья, С.Л. Способ и оснастка для производства композитных кольцевых рам
CN101370643B (zh) * 2005-12-30 2011-02-02 空客西班牙公司 具有u-型加强构件的复合面板的制备方法
RU2392121C2 (ru) * 2005-12-30 2010-06-20 Айрбус Эспанья, С.Л. Способ изготовления композитных панелей с u-образными элементами жесткости
FR2902689B1 (fr) * 2006-06-22 2008-08-22 Airbus France Sas Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee
GB0614087D0 (en) 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
GB0616121D0 (en) * 2006-08-14 2006-09-20 Airbus Uk Ltd Moulding tool and method of manufacturing a part
US20080070665A1 (en) * 2006-09-19 2008-03-20 Cyberscan Technology, Inc. Regulated gaming - compartmented freelance code
DE102007015518A1 (de) * 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung von Profilteilen
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
GB0712552D0 (en) 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
GB0712549D0 (en) 2007-06-29 2007-08-08 Airbus Uk Ltd Improvements in elongate composite structural members
GB0712553D0 (en) 2007-06-29 2007-08-08 Airbus Uk Ltd Composite panel stiffener
ITTO20070557A1 (it) * 2007-07-27 2009-01-28 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento curvo in materiale composito
US8016970B2 (en) * 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
AU2008326228B2 (en) 2007-11-09 2013-05-02 Bae Systems Plc Improvements relating to methods of fabricating structural elements
DE102008001498B3 (de) 2008-04-30 2009-08-27 Airbus Deutschland Gmbh Verfahren und Umformvorrichtung zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
CN102112063A (zh) * 2008-06-06 2011-06-29 瓦里克斯医疗公司 静脉治疗装置和方法
GB0813161D0 (en) 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
GB0813146D0 (en) 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
GB0813149D0 (en) * 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
ES2364112B1 (es) * 2008-12-22 2012-07-04 Airbus Operations, S.L. Sistema de posicionamiento, manipulación y desmontaje de útiles para la fabricación de piezas aeronáuticas.
EP2379312B1 (de) * 2009-01-21 2019-04-03 Vestas Wind Systems A/S Verfahren zur herstellung einer windturbinenschaufel und vorform für eine windturbinenschaufel
US20100198209A1 (en) * 2009-01-30 2010-08-05 Tartaglia Joseph M Hemorrhoid Therapy and Method
AT508169A1 (de) * 2009-04-16 2010-11-15 Facc Ag Spant und verfahren zur herstellung eines solchen spants
ES2382065B1 (es) * 2009-09-14 2013-07-01 Airbus Operations, S.L. Método de localización de pérdidas de presión en bolsas de vacio
DE102009060706B4 (de) * 2009-12-29 2014-12-04 Airbus Operations Gmbh Verfahren sowie Vorrichtung zur Herstellung einer Versteifungsstruktur für ein Flugzeugrumpfsegment sowie eine Versteifungsstruktur
ES2378682B1 (es) 2010-06-18 2013-02-28 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" para un avión y herramienta de curado usada en el mismo.
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
ES2378015B1 (es) * 2010-09-08 2013-04-15 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" que reduce el efecto de sombrero mexicano y herramienta de curado usada en el mismo.
ES2397727B1 (es) * 2010-10-28 2014-01-17 Airbus Operations, S.L. Retenedores reutilizables para coencolado de larguerillos no curados.
ITTO20110421A1 (it) * 2011-05-12 2012-11-13 Alenia Aeronautica Spa Elemento strutturale con ala avente bordo netto, e suo processo di fabbricazione
ES2400129B1 (es) * 2011-05-30 2014-06-18 Airbus Operations, S.L. Método de fabricación de larguerillos con forma de "t" con un ángulo diferente de 90� entre el alma y el pie
DE102011079943A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
ES2415773B1 (es) * 2011-12-29 2014-09-02 Airbus Operations S.L. Método de fabricación de piezas de material compuesto con cambios de espesor
EP2889211B1 (de) * 2013-12-31 2018-10-24 Airbus Operations S.L. Flugzeugstruktur aus Verbundmaterial
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
USD777014S1 (en) * 2014-08-12 2017-01-24 Servi-Sure, LLC Integrated stiffener
EP3088171B1 (de) * 2015-04-30 2022-06-29 Airbus Operations, S.L. Herstellungsverfahren von verbundstrukturen mit ausserhalb des vakuumbeutels angeordneten härtungswerkzeugen
ES2671185T3 (es) * 2015-05-28 2018-06-05 Airbus Operations, S.L. Métodos y sistemas de inspección para detectar fugas en ensamblajes con bolsa de vacío
US10272658B2 (en) * 2015-07-08 2019-04-30 The Boeing Company System and method for forming a composite part
EP3272640B1 (de) * 2016-07-21 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hubschrauber mit einem rumpf und einem verbundstoffheckausleger
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
CN111844812A (zh) * 2020-08-17 2020-10-30 沈阳飞机工业(集团)有限公司 分体式复合材料成型工装及其使用方法
CN113338331A (zh) * 2021-07-13 2021-09-03 浙江交工集团股份有限公司 一种用于锚栓型装配式挡墙的螺栓精确连接体系及其施工方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2440831A1 (fr) * 1978-11-07 1980-06-06 Dassault Avions Panneaux a base de fibres a haute resistance, particulierement applicables a la construction des avions
GB8508419D0 (en) * 1985-04-01 1985-05-09 Short Brothers Ltd Moulding fibre reinforced resin
DE3739753A1 (de) * 1987-11-24 1989-06-08 Dornier Gmbh Verfahren zum herstellen von bauteilen aus faserverstaerkten kunststoffen
US5593633A (en) * 1990-05-03 1997-01-14 Dull; Kenneth M. Edge and surface breather for high temperature composite processing
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
DE19832441C1 (de) * 1998-07-18 2000-01-05 Daimler Chrysler Aerospace Verfahren zur Herstellung einer stringerversteiften Schale in Faserverbundbauweise
US6245275B1 (en) * 1999-05-13 2001-06-12 Vought Aircraft Industries, Inc. Method for fabricating composite structures

Also Published As

Publication number Publication date
CA2315541A1 (en) 2001-09-07
ES2185443A1 (es) 2003-04-16
EP1134070A1 (de) 2001-09-19
CA2315541C (en) 2007-10-23
EP1134070B1 (de) 2004-03-24
DE60009259T2 (de) 2004-12-30
DE60009259D1 (de) 2004-04-29
ES2185443B1 (es) 2004-09-01
US6508909B1 (en) 2003-01-21

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