DE60239773D1 - Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding Technik - Google Patents
Verfahren zur Herstellung von Elementen aus Verbundmaterial durch Co-Bonding TechnikInfo
- 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
Links
- 238000000034 method Methods 0.000 title abstract 4
- 239000002131 composite material Substances 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 229910001374 Invar Inorganic materials 0.000 abstract 1
- 238000009786 automated tape laying Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
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
- B29C70/44—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
-
- 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
-
- 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
- B29C70/342—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 isostatic pressure
-
- 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
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
-
- 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
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
-
- 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
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/246—Uncured, e.g. green
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49623—Static structure, e.g., a building component
- Y10T29/49629—Panel
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
- Y10T29/49867—Assembling or joining with prestressing of part of skin on frame member
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49885—Assembling or joining with coating before or during assembling
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49892—Joining plate edge perpendicularly to frame
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
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)
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)
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)
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. |
-
2001
- 2001-02-13 ES ES200100317A patent/ES2205961B2/es not_active Expired - Fee Related
-
2002
- 2002-02-12 US US10/074,269 patent/US6735866B2/en not_active Expired - Lifetime
- 2002-02-13 DE DE60239773T patent/DE60239773D1/de not_active Expired - Lifetime
- 2002-02-13 AT AT02380034T patent/ATE506172T1/de not_active IP Right Cessation
- 2002-02-13 EP EP02380034A patent/EP1231046B1/de not_active Expired - Lifetime
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 |
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