DE60239773D1 - Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik - Google Patents

Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik

Info

Publication number
DE60239773D1
DE60239773D1 DE60239773T DE60239773T DE60239773D1 DE 60239773 D1 DE60239773 D1 DE 60239773D1 DE 60239773 T DE60239773 T DE 60239773T DE 60239773 T DE60239773 T DE 60239773T DE 60239773 D1 DE60239773 D1 DE 60239773D1
Authority
DE
Germany
Prior art keywords
bonding
tool
vacuum bag
skin
beams
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
DE60239773T
Other languages
English (en)
Inventor
Vines Pedro Nogueroles
Garcia Aquilino Garcia
Pancorbo Carlos Cerezo
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 Defence and Space SA
Original Assignee
EADS Construcciones Aeronauticas SA
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 EADS Construcciones Aeronauticas SA filed Critical EADS Construcciones Aeronauticas SA
Application granted granted Critical
Publication of DE60239773D1 publication Critical patent/DE60239773D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B29C70/40Shaping 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
    • 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
    • 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
    • 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
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/38Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • 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
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49623Static structure, e.g., a building component
    • Y10T29/49629Panel
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49801Shaping fiber or fibered material
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49863Assembling or joining with prestressing of part
    • Y10T29/49867Assembling or joining with prestressing of part of skin on frame member
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49885Assembling or joining with coating before or during assembling
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49892Joining plate edge perpendicularly to frame
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982Coating

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Ceramic Products (AREA)
DE60239773T 2001-02-13 2002-02-13 Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik Expired - Lifetime DE60239773D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200100317A ES2205961B2 (es) 2001-02-13 2001-02-13 Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.

Publications (1)

Publication Number Publication Date
DE60239773D1 true DE60239773D1 (de) 2011-06-01

Family

ID=8496708

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60239773T Expired - Lifetime DE60239773D1 (de) 2001-02-13 2002-02-13 Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik

Country Status (5)

Country Link
US (1) US6735866B2 (de)
EP (1) EP1231046B1 (de)
AT (1) ATE506172T1 (de)
DE (1) DE60239773D1 (de)
ES (1) ES2205961B2 (de)

Families Citing this family (78)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6510601B1 (en) * 2000-03-20 2003-01-28 The Boeing Company Invar forming method for making tooling
US6956084B2 (en) 2001-10-04 2005-10-18 Bridgestone Corporation Nano-particle preparation and applications
US6609879B2 (en) * 2001-11-14 2003-08-26 General Electric Company Method and apparatus for vacuum bagging a component having a partial flange
US7249943B2 (en) * 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
ES2271513T3 (es) 2003-12-16 2007-04-16 Airbus España, S.L. Proceso y utillaje para reducir las tensiones residuales y las distorsiones de la forma inducidas termicamente en estructuras de composite monoliticas.
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.
US7205370B2 (en) 2004-01-12 2007-04-17 Bridgestone Corporation Polymeric nano-particles of flower-like structure and applications
US8063142B2 (en) 2004-03-02 2011-11-22 Bridgestone Corporation Method of making nano-particles of selected size distribution
US7718737B2 (en) 2004-03-02 2010-05-18 Bridgestone Corporation Rubber composition containing functionalized polymer nanoparticles
US20050282956A1 (en) 2004-06-21 2005-12-22 Xiaorong Wang Reversible polymer/metal nano-composites and method for manufacturing same
US7998554B2 (en) 2004-07-06 2011-08-16 Bridgestone Corporation Hydrophobic surfaces with nanoparticles
ES2276569B1 (es) 2004-12-30 2008-06-16 Airbus España S.L. Util hibrido para el curado de piezas de material compuesto.
US7659342B2 (en) 2005-02-03 2010-02-09 Bridgestone Corporation Polymer nano-particle with polar core and method for manufacturing same
ES2356319T3 (es) * 2005-03-30 2011-04-06 Eads Construcciones Aeronáuticas S.A. Proceso de fabricación de un capot de motor monolítico.
US20060266472A1 (en) * 2005-05-06 2006-11-30 Kipp Michael D Vacuum bagging methods and systems
DE102005057907B4 (de) 2005-12-02 2012-03-22 Eurocopter Deutschland Gmbh Luftfahrzeug-Druckkabinentür aus Faserverbundwerkstoff
US9061900B2 (en) 2005-12-16 2015-06-23 Bridgestone Corporation Combined use of liquid polymer and polymeric nanoparticles for rubber applications
US8288473B2 (en) 2005-12-19 2012-10-16 Bridgestone Corporation Disk-like nanoparticles
US7884160B2 (en) 2005-12-19 2011-02-08 Bridgestone Corporation Non-spherical nanoparticles made from living triblock polymer chains
US8877250B2 (en) 2005-12-20 2014-11-04 Bridgestone Corporation Hollow nano-particles and method thereof
US8697775B2 (en) 2005-12-20 2014-04-15 Bridgestone Corporation Vulcanizable nanoparticles having a core with a high glass transition temperature
CN101448629B (zh) * 2005-12-29 2011-08-17 空客西班牙公司 用于制造复合环形框架的方法和工具
DE102006005252B4 (de) * 2006-02-02 2010-10-28 Thyssenkrupp Vdm Gmbh Formbauteil aus einer Eisen-Nickel-Kobalt-Legierung
US20080008836A1 (en) * 2006-05-01 2008-01-10 Kipp Michael D Method for extending the useful life of mold type tooling
US7935184B2 (en) 2006-06-19 2011-05-03 Bridgestone Corporation Method of preparing imidazolium surfactants
GB0614087D0 (en) 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
KR101445405B1 (ko) 2006-07-28 2014-09-26 가부시키가이샤 브리지스톤 상간 영역을 갖는 중합체성 코어-쉘 나노입자
BRPI0621913B1 (pt) * 2006-07-28 2018-12-18 Airbus Espana Sl procedimento para fabricar uma peça de um material composto para estrutura aeronáutica
US20080106007A1 (en) * 2006-10-17 2008-05-08 Kipp Michael D Resin infusion process utilizing a reusable vacuum bag
WO2008048657A2 (en) * 2006-10-17 2008-04-24 American Consulting Technology & Research, Inc. Method for enhancing the sealing potential of formable, disposable tooling materials
US7588711B2 (en) * 2006-11-21 2009-09-15 The Boeing Company Method for forming a composite support beam
WO2008070110A1 (en) * 2006-12-04 2008-06-12 American Consulting Technology & Research, Inc. Shrinkable film barrier for mandrel tooling members
US7597959B2 (en) 2006-12-19 2009-10-06 Bridgestone Corporation Core-shell fluorescent nanoparticles
US7649049B2 (en) 2006-12-20 2010-01-19 Bridgestone Corporation Rubber composition containing a polymer nanoparticle
ATE501835T1 (de) * 2007-01-22 2011-04-15 Saab Ab Verfahren und vorrichtung zur herstellung eines tragflächenholmprofilelements
EP2153979B1 (de) * 2007-04-30 2016-10-19 Airbus Operations S.L. Aus verbundwerkstoff hergestellter torsionskasten mit mehreren holmen
ITTO20070423A1 (it) * 2007-06-14 2008-12-15 Alenia Aeronautica Spa Procedimento ed attrezzatura di polimerizzazione per la fabbricazione di travi di materiale composito aventi una sezione trasversale a forma di j.
US7829624B2 (en) 2007-06-29 2010-11-09 Bridgestone Corporation One-pot synthesis of nanoparticles and liquid polymer for rubber applications
US7828246B2 (en) * 2007-09-14 2010-11-09 Spectrum Aeronautical, Llc Wing with sectioned tubular members
US8268107B2 (en) 2007-09-21 2012-09-18 The Boeing Company Fly away caul plate
US7754045B2 (en) 2007-11-14 2010-07-13 The Boeing Company Method and tools for fabricating composite beams
US9656450B2 (en) * 2008-01-02 2017-05-23 Tpk Touch Solutions, Inc. Apparatus for laminating substrates
WO2009097514A1 (en) 2008-01-31 2009-08-06 Alliant Techsystems Inc. A stiffener tool positioning apparatus
US8373657B2 (en) 2008-08-15 2013-02-12 Qualcomm Incorporated Enhanced multi-touch detection
DE102008062477B3 (de) * 2008-12-16 2010-03-25 Airbus Deutschland Gmbh Verfahren, System und Formwerkzeug zum Herstellen von Bauteilen aus Faserverbundwerkstoffen
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.
ES2527600T3 (es) 2008-12-31 2015-01-27 Bridgestone Corporation Procedimiento de formación de nanopartículas formando primero el núcleo, nanopartícula y composición
US9062144B2 (en) 2009-04-03 2015-06-23 Bridgestone Corporation Hairy polymeric nanoparticles with first and second shell block polymer arms
US8165702B2 (en) * 2009-05-08 2012-04-24 Accudyne Systems Inc. Article manufacturing process
US8282757B2 (en) 2009-11-10 2012-10-09 Alliant Techsystems Inc. Automated composite annular structure forming
US9662841B2 (en) 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
US9115222B2 (en) 2009-12-29 2015-08-25 Bridgestone Corporation Well defined, highly crosslinked nanoparticles and method for making same
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.
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
DE102011079928A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
DE102011079943A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
FR2987779A1 (fr) * 2012-03-12 2013-09-13 Airbus Operations Sas Procede de realisation d'une piece en materiau composite et outillage pour sa mise en oeuvre
US8978536B2 (en) * 2012-04-30 2015-03-17 Future Force Innovation, Inc. Material for providing blast and projectile impact protection
US8758879B2 (en) 2012-06-24 2014-06-24 The Boeing Company Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same
CN102909866A (zh) * 2012-10-24 2013-02-06 中国航空工业集团公司北京航空材料研究院 一种复合材料加筋壁板长桁轴线成型控制方法
US9797257B2 (en) 2012-12-10 2017-10-24 General Electric Company Attachment of composite article
US9777579B2 (en) 2012-12-10 2017-10-03 General Electric Company Attachment of composite article
CN105014987A (zh) * 2014-04-29 2015-11-04 哈尔滨飞机工业集团有限责任公司 一种复合材料共固化盒段结构加强肋r角的成型方法
CN104290336A (zh) * 2014-08-14 2015-01-21 航天海鹰(镇江)特种材料有限公司 一种开放式软性工装成型j形梁结构复合材料制件的方法
DE102014116848B4 (de) 2014-11-18 2023-06-15 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Anlage zum automatisierten Herstellen eines Vakuumaufbaus
EP3088171B1 (de) * 2015-04-30 2022-06-29 Airbus Operations, S.L. Herstellungsverfahren von verbundstrukturen mit ausserhalb des vakuumbeutels angeordneten härtungswerkzeugen
GB201518284D0 (en) * 2015-10-15 2015-12-02 Composite Technology & Applic Ltd A method of generating a movement profile for a layup procedure
CN105437536B (zh) * 2015-12-11 2017-12-12 昌河飞机工业(集团)有限责任公司 一种带加强筋的复合材料壁板成形工装
US10525683B2 (en) * 2016-11-08 2020-01-07 The Boeing Company Heated double diaphragm tool for decorative laminate application
CN109624355A (zh) * 2018-12-10 2019-04-16 西安航空职业技术学院 高性能vari工艺成型复合材料的出胶结构及方法
IT202000027287A1 (it) * 2020-11-13 2022-05-13 Leonardo Spa Metodo e attrezzatura per l'integrazione di longheroni continui aventi sezione a j in pannelli allungati di materiale composito
CN113459540B (zh) * 2021-06-25 2022-05-10 成都飞机工业(集团)有限责任公司 一种细长带闭角的零件成型装置及成型方法
CN114013066B (zh) * 2021-11-19 2024-07-12 浙江美洲豹特种设备有限公司 一种立式热压罐
GB2615755A (en) * 2022-02-15 2023-08-23 Airbus Operations Ltd Fuel tank stringer with flow passage
CN115303443B (zh) * 2022-09-27 2024-08-02 湖北三江航天万峰科技发展有限公司 一种舱体复合成型工艺

Family Cites Families (9)

* 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
US4411380A (en) * 1981-06-30 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Metal matrix composite structural panel construction
US4502200A (en) * 1982-03-08 1985-03-05 Atlantic Richfield Company Method of preparing lightweight mirror module
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5622733A (en) * 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US5850722A (en) * 1996-09-27 1998-12-22 Mcdonnell Douglas Corporation Lightweight superplastically formed, diffusion bonded panel structure and process of manufacture
JP3647612B2 (ja) * 1997-07-24 2005-05-18 富士重工業株式会社 航空機の前縁構造及びその製造方法
ES2185443B1 (es) * 2000-03-07 2004-09-01 Airbus España S.L. Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco.

Also Published As

Publication number Publication date
US20020144401A1 (en) 2002-10-10
ES2205961B2 (es) 2005-03-01
EP1231046A2 (de) 2002-08-14
ATE506172T1 (de) 2011-05-15
ES2205961A1 (es) 2004-05-01
EP1231046A3 (de) 2002-10-30
EP1231046B1 (de) 2011-04-20
US6735866B2 (en) 2004-05-18

Similar Documents

Publication Publication Date Title
DE60239773D1 (de) Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik
US9156240B2 (en) Automated production and installation of patches for reworking structures
CN1098152C (zh) 两用敷层工具
Raspall et al. Fabrication of complex 3D composites by fusing automated fiber placement (AFP) and additive manufacturing (AM) technologies
US7544261B1 (en) Process and tools for manufacturing composite ring frames
US6620369B1 (en) Net molding of resin composite parts
US11772339B2 (en) Three-dimensional printing of composite repair patches and structures
JPH04301410A (ja) 複雑な形状の複合材製品の製造方法
JP6971882B2 (ja) 3d形状に成形するためのレイアップ特異部を有するフラットな複合材
CN107283868A (zh) 一种成型碳纤维复合材料加筋壁板的筋条整体定位方法
US6261395B1 (en) Manufacture of stiffened composite structures
US20210094240A1 (en) Method and apparatus for fabrication of composite tooling
US20240075697A1 (en) Caul plates for preforms that undergo pick and placement
JPH05193025A (ja) 複合形成工具の製作方法
EP3670160B1 (de) System und verfahren zur herstellung einer verbundlagenlaminierung
US11981839B2 (en) Method and apparatus for fabrication of composite tooling
GB2254820A (en) Tooling for composite component manufacture
RU2390417C2 (ru) Способ и оснастка для производства композитных кольцевых рам
US20240308159A1 (en) Composite parts, and methods of manufacturing
US11872780B2 (en) Methods and tool for cutting an uncured composite material
JP2947879B2 (ja) 成形治具の製造方法
CN102615915B (zh) 一种嵌入式无卤玻纤增强板的制备方法
US20210094246A1 (en) Method and apparatus for fabrication of composite tooling