ATE493333T1 - Einstückiger co-aushärtender verbundflügel - Google Patents
Einstückiger co-aushärtender verbundflügelInfo
- Publication number
- ATE493333T1 ATE493333T1 AT03739169T AT03739169T ATE493333T1 AT E493333 T1 ATE493333 T1 AT E493333T1 AT 03739169 T AT03739169 T AT 03739169T AT 03739169 T AT03739169 T AT 03739169T AT E493333 T1 ATE493333 T1 AT E493333T1
- Authority
- AT
- Austria
- Prior art keywords
- wing
- spars
- cured
- single piece
- structural members
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/006—Degassing moulding material or draining off gas during moulding
- B29C37/0064—Degassing moulding material or draining off gas during moulding of reinforced material
-
- 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
- B29C70/40—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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/24—Moulded or cast structures
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/8016—Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/8066—Impregnating
-
- 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
- B29L2031/3085—Wings
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/90—Direct application of fluid pressure differential to shape, reshape, i.e. distort, or sustain an article or preform and heat-setting, i.e. crystallizing of stretched or molecularly oriented portion thereof
- Y10S264/904—Maintaining article in fixed shape during heat-setting
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Textile Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Macromonomer-Based Addition Polymer (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/175,722 US6889937B2 (en) | 1999-11-18 | 2002-06-20 | Single piece co-cure composite wing |
PCT/US2003/019100 WO2004000643A2 (en) | 2002-06-20 | 2003-06-19 | Single piece co-cure composite wing |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE493333T1 true ATE493333T1 (de) | 2011-01-15 |
Family
ID=29999053
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03739169T ATE493333T1 (de) | 2002-06-20 | 2003-06-19 | Einstückiger co-aushärtender verbundflügel |
Country Status (8)
Country | Link |
---|---|
US (2) | US6889937B2 (de) |
EP (1) | EP1585664B1 (de) |
JP (1) | JP4607583B2 (de) |
CN (1) | CN100575189C (de) |
AT (1) | ATE493333T1 (de) |
AU (1) | AU2003245544A1 (de) |
DE (1) | DE60335576D1 (de) |
WO (1) | WO2004000643A2 (de) |
Families Citing this family (121)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1495859B1 (de) * | 2003-07-08 | 2008-09-03 | Airbus Deutschland GmbH | Leichtbaustruktur |
FI118122B (fi) * | 2004-10-08 | 2007-07-13 | Patria Aerostructures Oy | Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale |
EP1666354B1 (de) * | 2004-12-01 | 2010-09-29 | Airbus Operations GmbH | Strukturbauteil, Verfahren zum Herstellen eines Strukturbauteils und Verwendung eines Strukturbauteils für eine Flugzeugschale |
GB0426944D0 (en) * | 2004-12-08 | 2005-01-12 | Airbus Uk Ltd | A trussed structure |
FR2879496B1 (fr) * | 2004-12-16 | 2008-12-12 | Eurocopter France | Procede et dispositif de fabrication d'une carene de rotor d'helicoptere, et carene obtenue |
FR2882681B1 (fr) * | 2005-03-03 | 2009-11-20 | Coriolis Composites | Tete d'application de fibres et machine correspondante |
DE102006031491B4 (de) | 2005-07-19 | 2010-09-30 | Eurocopter Deutschland Gmbh | Verfahren zur Herstellung eines dreidimensional gekrümmten Faserverbundwerkstoff-Strukturbauteils |
EP1764307A1 (de) * | 2005-09-14 | 2007-03-21 | EADS Construcciones Aeronauticas, S.A. | Herstellungsverfahren einer monolithischen Flügelvorderkante |
US7402269B2 (en) * | 2005-10-25 | 2008-07-22 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
GB2435457B (en) * | 2006-02-28 | 2011-03-09 | Hal Errikos Calamvokis | Aircraft wings and their assembly |
WO2007126405A2 (en) * | 2006-03-30 | 2007-11-08 | University Of Florida Research Foundation Inc. | Airfoil for micro air vehicle |
US7487937B2 (en) * | 2006-03-30 | 2009-02-10 | University Of Florida Research Foundation, Inc. | Airfoil for micro air vehicle |
GB0611875D0 (en) * | 2006-06-15 | 2006-07-26 | Airbus Uk Ltd | A stringer for an aircraft wing and a method of forming thereof |
DE102006031326B4 (de) * | 2006-07-06 | 2010-09-23 | Airbus Deutschland Gmbh | Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031325B4 (de) * | 2006-07-06 | 2010-07-01 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031334A1 (de) * | 2006-07-06 | 2008-01-10 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031323B4 (de) * | 2006-07-06 | 2010-07-15 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031335B4 (de) | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
WO2008003733A1 (en) * | 2006-07-06 | 2008-01-10 | Airbus Deutschland Gmbh | Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby |
DE102006031336B4 (de) | 2006-07-06 | 2010-08-05 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt |
GB0616121D0 (en) * | 2006-08-14 | 2006-09-20 | Airbus Uk Ltd | Moulding tool and method of manufacturing a part |
US7753313B1 (en) * | 2006-09-19 | 2010-07-13 | The Boeing Company | Composite wing slat for aircraft |
US7713021B2 (en) * | 2006-12-13 | 2010-05-11 | General Electric Company | Fan containment casings and methods of manufacture |
EP2128018A4 (de) * | 2007-01-29 | 2013-09-18 | Airbus Operations Sl | Flugzeuglastrahmen aus verbundmaterial |
FR2912680B1 (fr) * | 2007-02-21 | 2009-04-24 | Coriolis Composites Sa | Procede et dispositif de fabrication de pieces en materiau composite, en particulier de troncons de fuselage d'avion |
WO2008121005A1 (en) * | 2007-03-29 | 2008-10-09 | Falcomposite Limited | Aircraft component manufacture and assembly |
US8490362B2 (en) | 2007-04-05 | 2013-07-23 | The Boeing Company | Methods and systems for composite structural truss |
US7954763B2 (en) * | 2007-04-05 | 2011-06-07 | The Boeing Company | Methods and systems for composite structural truss |
BRPI0721604B1 (pt) * | 2007-04-30 | 2018-06-26 | Airbus Operations, S.L. | Método para a fabricação de uma estrutura de caixa de torção de multilongarinas integradas de material compósito para aeronave |
US7861969B2 (en) * | 2007-05-24 | 2011-01-04 | The Boeing Company | Shaped composite stringers and methods of making |
ES2335837B1 (es) * | 2007-06-29 | 2011-02-18 | Airbus España, Sl. | Cubierta para boca de acceso de aeronave. |
ITTO20070507A1 (it) | 2007-07-11 | 2009-01-12 | Alenia Aeronautica Spa | Procedimento di fabbricazione di una struttura d'ala monolitica a profilo integrale |
US8042315B2 (en) * | 2007-09-14 | 2011-10-25 | Spectrum Aeronautical, Llc | Reinforced composite panel |
US8668858B2 (en) * | 2007-09-14 | 2014-03-11 | Spectrum Aeronautical, Llc | Method for manufacturing a reinforced panel of composite material |
US7828246B2 (en) * | 2007-09-14 | 2010-11-09 | Spectrum Aeronautical, Llc | Wing with sectioned tubular members |
FR2921899B1 (fr) * | 2007-10-04 | 2011-04-15 | Airbus France | Procede de renforcement local d'un element en materiau composite, et caisson central de voilure pour aeronef renforce |
US7879276B2 (en) * | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
DE102008013759B4 (de) * | 2008-03-12 | 2012-12-13 | Airbus Operations Gmbh | Verfahren zur Herstellung eines integralen Faserverbundbauteils sowie Kernform zur Durchführung des Verfahrens |
DE102008029058A1 (de) * | 2008-06-18 | 2009-12-24 | GKN Aerospace Services Limited, East Cowes | Verfahren und Formwerkzeug zur Herstellung von Bauteilen aus faserverstärktem Verbundwerkstoff mit Mikrowellen |
ES2371401B1 (es) * | 2008-06-27 | 2012-11-07 | Airbus Operations, S.L. | Estructura de superficie sustentadora de aeronave. |
US9327467B2 (en) | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | Mandrel for autoclave curing applications |
US8540921B2 (en) | 2008-11-25 | 2013-09-24 | The Boeing Company | Method of forming a reinforced foam-filled composite stringer |
GB0900494D0 (en) | 2009-01-14 | 2009-02-11 | Airbus Uk Ltd | Aerofoil Structure |
FR2943943A1 (fr) * | 2009-04-02 | 2010-10-08 | Coriolis Composites | Procede et machine pour l'application d'une bande de fibres sur des surfaces convexes et/ou avec aretes |
DE102009017644B4 (de) * | 2009-04-16 | 2018-05-24 | Airbus Defence and Space GmbH | Vorrichtung zur Verhinderung des Durchtritts von Gasen und/oder Fluiden aus einem Flügelkasten in eine Rumpfzelle eines Flugzeugs |
FR2954269B1 (fr) * | 2009-12-18 | 2012-12-28 | Lorraine Construction Aeronautique | Pannneau structurant composite de bord de fuite pour element d'aeronef |
US8500066B2 (en) * | 2009-06-12 | 2013-08-06 | The Boeing Company | Method and apparatus for wireless aircraft communications and power system using fuselage stringers |
FR2948059B1 (fr) * | 2009-07-17 | 2011-08-05 | Coriolis Composites | Machine d'application de fibres avec rouleau de compactage transparent au rayonnement du systeme de chauffage |
FR2948058B1 (fr) * | 2009-07-17 | 2011-07-22 | Coriolis Composites | Machine d'application de fibres comprenant un rouleau de compactage souple avec systeme de regulation thermique |
US8570152B2 (en) | 2009-07-23 | 2013-10-29 | The Boeing Company | Method and apparatus for wireless sensing with power harvesting of a wireless signal |
US8617687B2 (en) * | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
US8424805B2 (en) * | 2009-10-07 | 2013-04-23 | Donald Smith | Airfoil structure |
US20110117231A1 (en) * | 2009-11-19 | 2011-05-19 | General Electric Company | Fiber placement system and method with inline infusion and cooling |
DE102009060693A1 (de) * | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement |
ES2391102B1 (es) * | 2010-01-14 | 2013-10-09 | Airbus Operations, S.L. | Disposicion de union de dos cajones de material compuesto con una pieza intermedia y procedimiento de fabricacion de dicha pieza intermedia |
ITTO20100175A1 (it) | 2010-03-08 | 2011-09-09 | Alenia Aeronautica Spa | Procedimento per la fabbricazione di longheroni alari e travi di fusoliera a doppio t in materiale composito a sezione variabile |
DE102010002720A1 (de) * | 2010-03-10 | 2011-09-15 | Aloys Wobben | Windenergieanlagen-Rotorblatt |
DE102010043850A1 (de) * | 2010-11-12 | 2012-05-16 | Airbus Operations Gmbh | Strukturelement für ein Luft- und/oder Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes |
FR2972387B1 (fr) * | 2011-03-09 | 2013-04-26 | Latecoere | Procede de realisation d'une preforme comportant au moins deux troncons presentant des epaisseurs differentes. |
US20130048134A1 (en) * | 2011-08-25 | 2013-02-28 | The Boeing Company | Stagnant Fuel Thermal Insulation System |
WO2013078646A1 (en) * | 2011-11-30 | 2013-06-06 | Airbus S.A.S. | Airplane component having a box structure |
GB201120707D0 (en) * | 2011-12-01 | 2012-01-11 | Airbus Operations Ltd | Leading edge structure |
EP2791003A4 (de) * | 2011-12-12 | 2016-01-06 | Saab Ab | Flugzeugstruktur mit struktureller faserfreier verstärkender bindeharzschicht |
EP2814732B1 (de) * | 2012-02-17 | 2017-04-05 | Saab Ab | Verfahren und formsystem zur netzformung einer cogehärteten, integrierten struktur |
FR2992890B1 (fr) * | 2012-07-04 | 2015-04-10 | Heol Composites | Procede de fabrication d'une piece creuse en materiaux composites et piece creuse mettant en oeuvre ledit procede |
US9415858B2 (en) | 2012-08-28 | 2016-08-16 | The Boeing Company | Bonded and tailorable composite assembly |
ES2799904T3 (es) | 2012-10-03 | 2020-12-22 | Airbus Operations Sl | Carena de extremo de una superficie sustentadora horizontal |
US9333713B2 (en) | 2012-10-04 | 2016-05-10 | The Boeing Company | Method for co-curing composite skins and stiffeners in an autoclave |
ES2623044T3 (es) | 2012-11-22 | 2017-07-10 | Airbus Operations S.L. | Método de fabricación de una estructura altamente integrada incluyendo costillas de borde de ataque y de salida para una superficie de elevación de una aeronave |
US9527575B2 (en) * | 2012-11-26 | 2016-12-27 | The Boeing Company | Multi-box wing spar and skin |
US9145197B2 (en) * | 2012-11-26 | 2015-09-29 | The Boeing Company | Vertically integrated stringers |
RU2522725C1 (ru) * | 2012-12-07 | 2014-07-20 | Российская Федерация от имени которой выступает Министерство промышленности и торговли Российской Федерации | Способ изготовления полых конструкций с внутренними стенками |
US9096324B2 (en) * | 2013-03-19 | 2015-08-04 | The Boeing Company | Joint assembly to form a sealed flow conduit |
EP2996866B1 (de) * | 2013-05-17 | 2019-12-11 | Leonardo S.P.A. | Verfahren zur herstellung einer einstückigen schachtel mit mehreren holmen aus verbundstoff in einer geschlossenen form |
GB2515044A (en) * | 2013-06-12 | 2014-12-17 | Airbus Operations Ltd | Aircraft wing arrangement |
ES2674659T3 (es) * | 2013-09-23 | 2018-07-03 | Airbus Operations S.L. | Método para fabricar una caja de torsión aeronáutica, caja de torsión y herramienta para fabricar una caja de torsión aeronáutica |
US9738375B2 (en) | 2013-12-05 | 2017-08-22 | The Boeing Company | One-piece composite bifurcated winglet |
EP2910365B1 (de) * | 2014-02-21 | 2017-04-26 | Airbus Operations GmbH | Verbundstrukturelement und Torsionskasten |
US9981735B2 (en) * | 2014-04-01 | 2018-05-29 | The Boeing Company | Structural arrangement and method of fabricating a composite trailing edge control surface |
CN104192292B (zh) * | 2014-09-17 | 2017-01-18 | 中航通飞华南飞机工业有限公司 | 一种复合材料整体共固化机身及加工方法 |
ES2784499T3 (es) * | 2014-10-08 | 2020-09-28 | Salver S P A | Procedimiento de ensamblaje de superficies de control de aeronaves |
RU2582506C1 (ru) * | 2014-12-15 | 2016-04-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" (КНИТУ-КАИ) | Консоль складной аэродинамической поверхности из полимерного композиционного материала |
ES2727473T3 (es) * | 2014-12-22 | 2019-10-16 | Magna Steyr Fahrzeugtechnik Ag & Co Kg | Procedimiento para fabricar componentes de vehículo/componentes estructurales a base de un material plástico y componente de vehículo o componente estructural fabricado de esa manera |
FR3034338B1 (fr) | 2015-04-01 | 2017-04-21 | Coriolis Composites | Tete d'application de fibres avec rouleau d'application particulier |
GB201509142D0 (en) | 2015-05-28 | 2015-07-15 | Blade Dynamics Ltd | A wind turbine blade and a method of moulding a wind turbine blade tip section |
FR3037315B1 (fr) * | 2015-06-15 | 2017-07-07 | Critt Materiaux Polymeres Composites | Procede de realisation d'une aile d'aeronef en materiau composite, aile d'aeronef obtenue a partir de ce procede |
CN105035359B (zh) * | 2015-07-28 | 2017-03-08 | 中国运载火箭技术研究院 | 一种刚度递减的复合材料一体成型舵面结构及加工方法 |
FR3043010B1 (fr) | 2015-10-28 | 2017-10-27 | Coriolis Composites | Machine d'application de fibres avec systemes de coupe particuliers |
GB201522327D0 (en) * | 2015-12-17 | 2016-02-03 | Airbus Operations Ltd | Wing structure |
FR3048373B1 (fr) | 2016-03-07 | 2018-05-18 | Coriolis Group | Procede de realisation de preformes avec application d'un liant sur fibre seche et machine correspondante |
EP3219458B1 (de) * | 2016-03-14 | 2019-05-08 | Airbus Operations, S.L. | Verfahren und spritzgiesswerkzeug zur herstellung eines vorderkantenabschnitts mit hybrider laminarer strömungskontrolle für ein flugzeug |
GB2550403A (en) * | 2016-05-19 | 2017-11-22 | Airbus Operations Ltd | Aerofoil body with integral curved spar-cover |
GB201611788D0 (en) | 2016-07-06 | 2016-08-17 | Williams Grand Prix Eng Ltd | Manufacturing fibre-reinforced composite structures |
CN106182801A (zh) * | 2016-07-15 | 2016-12-07 | 西北工业大学 | 一种飞行器泡沫夹芯复合材料舵面成型方法 |
FR3056438B1 (fr) | 2016-09-27 | 2019-11-01 | Coriolis Group | Procede de realisation de pieces en materiau composite par impregnation d'une preforme particuliere. |
US10766594B2 (en) * | 2016-11-03 | 2020-09-08 | Continuous Composites Inc. | Composite vehicle body |
JP6949474B2 (ja) * | 2016-11-24 | 2021-10-13 | 三菱重工業株式会社 | 複合材及び複合材の成形方法 |
US11273899B2 (en) * | 2018-01-25 | 2022-03-15 | The Boeing Company | Wing rib, wing having wing rib, and method for manufacturing the same |
US10933595B2 (en) * | 2018-02-15 | 2021-03-02 | The Boeing Company | Laminated composite structures with interlaminar corrugations to improve impact damage resistance, and system and method of forming the same |
US10647407B2 (en) * | 2018-03-30 | 2020-05-12 | The Boeing Company | Wing flap with torque member and method for forming thereof |
US10759516B2 (en) * | 2018-03-30 | 2020-09-01 | The Boeing Company | Wing flap with torque member and method for forming thereof |
CN112512782B (zh) * | 2018-05-04 | 2023-05-05 | 泰普爱复合材料股份有限公司 | 用于风力涡轮机叶片制造的周边板 |
GB2575102A (en) * | 2018-06-29 | 2020-01-01 | Airbus Operations Ltd | Duct stringer with bulkhead |
RU186272U1 (ru) * | 2018-08-08 | 2019-01-15 | Михаил Борисович Жуков | Кессон крыла летательного аппарата |
CN109353024B (zh) * | 2018-09-03 | 2020-11-13 | 西安飞机工业(集团)有限责任公司 | 一种飞机副翼j型肋的复材成型方法 |
CN109229373B (zh) * | 2018-09-29 | 2020-07-03 | 中船重工(海南)飞船发展有限公司 | 一种全复合材料地效翼船的连接结构 |
US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
CN109532059A (zh) * | 2018-12-03 | 2019-03-29 | 江西洪都航空工业集团有限责任公司 | 一种中空薄壁翼型结构复合材料件的制作方法 |
US11038334B2 (en) * | 2019-01-14 | 2021-06-15 | The Boeing Company | Aircraft wing composite ribs having electrical grounding paths |
US10913548B2 (en) | 2019-01-14 | 2021-02-09 | The Boeing Company | Metallic fittings for coupling composite ribs to skin panels of aircraft wings |
US11279474B2 (en) | 2019-05-30 | 2022-03-22 | Ctlp, Llc | Composite twin beam main landing gear for an aircraft |
CN110510145A (zh) * | 2019-08-30 | 2019-11-29 | 中国民用航空飞行学院 | 一种三梁式复合材料机翼整体结构及其成型工艺方法 |
US11046420B2 (en) * | 2019-10-23 | 2021-06-29 | The Boeing Company | Trailing edge flap having a waffle grid interior structure |
JP7318112B2 (ja) * | 2020-03-23 | 2023-07-31 | 三菱重工業株式会社 | 繊維強化複合材成形方法および繊維強化複合材成形装置 |
CN112537435B (zh) * | 2020-11-20 | 2023-03-17 | 上海复合材料科技有限公司 | 具有高精度曲面大长径比的复合材料翼梁及其制备方法 |
GB2604141A (en) * | 2021-02-25 | 2022-08-31 | Airbus Operations Ltd | Aircraft wing with tubular fuel tanks |
CN113602477B (zh) * | 2021-07-26 | 2024-03-15 | 成都飞机工业(集团)有限责任公司 | 一种全复合材料的尾翼结构及其成型方法 |
US20230242243A1 (en) * | 2022-02-02 | 2023-08-03 | Rohr, Inc. | Resin pressure molded aerostructure with integrated metal coupling |
WO2023198267A1 (en) * | 2022-04-11 | 2023-10-19 | Dufour Aerospace Ag | Method for manufacturing an aerodynamic profile |
CN117073467B (zh) * | 2023-09-04 | 2024-07-26 | 北京爱思达航天科技有限公司 | 一种可载器件的轻质复合材料飞行翼及其制备方法 |
Family Cites Families (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1814556A (en) * | 1929-04-15 | 1931-07-14 | Jr John Brown Jewett | Airplane construction and method therefor |
FR1085142A (fr) | 1953-06-19 | 1955-01-27 | Sncase | Perfectionnements aux surfaces aérodynamiques et plus particulièrement aux pales d'hélicoptères |
US3641230A (en) * | 1969-01-21 | 1972-02-08 | Dura Fiber | Method for making prestressed laminated fiber glass structures |
US3764641A (en) * | 1971-01-08 | 1973-10-09 | A Ash | Method of forming irregularly shaped hollow articles using a variable stiffness mandrel |
US4126659A (en) * | 1976-07-09 | 1978-11-21 | Lockheed Aircraft Corporation | Method of making a hollow article |
US4084029A (en) * | 1977-07-25 | 1978-04-11 | The Boeing Company | Sine wave beam web and method of manufacture |
US4198018A (en) | 1978-03-13 | 1980-04-15 | The Boeing Company | Blended wing-fuselage frame made of fiber reinforced resin composites |
US4357193A (en) | 1979-05-21 | 1982-11-02 | Rockwell International Corporation | Method of fabricating a composite structure |
GB2102036B (en) | 1981-07-01 | 1984-12-05 | Rolls Royce | Method of manufacturing composite materials |
DE3428282C1 (de) * | 1984-08-01 | 1986-01-16 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn | Entfernbarer Kern zur Herstellung rohrfoermiger Strukturen aus Faserverbundwerkstoffen |
US4622091A (en) | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
US4760493A (en) * | 1985-09-30 | 1988-07-26 | The Boeing Company | Lightning protection system for composite material aircraft structures |
US4681724A (en) | 1986-04-28 | 1987-07-21 | United Technologies Corporation | Removable irreversibly shrinking male mandrel |
US4938824A (en) | 1987-01-23 | 1990-07-03 | Thiokol Corporation | Method for making a composite component using a transverse tape |
DE3707634C1 (en) | 1987-03-10 | 1988-07-07 | Messerschmitt Boelkow Blohm | Device for producing a plastic body |
US4808362A (en) | 1987-06-04 | 1989-02-28 | The Budd Company | Hollow reinforced fiber structure formed by resin transfer molding |
US5641366A (en) | 1988-01-20 | 1997-06-24 | Loral Vought Systems Corporation | Method for forming fiber-reinforced composite |
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 |
US5106568A (en) | 1991-11-15 | 1992-04-21 | Mcdonnell Douglas Corporation | Method and apparatus for vacuum bag molding of composite materials |
US5266249A (en) | 1992-01-02 | 1993-11-30 | Fusion Composites, Inc. | Method of forming a fiber reinforced plastic structure |
US5242523A (en) | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
GB9211263D0 (en) * | 1992-05-28 | 1992-07-15 | British Aerospace | Manufacture of articles from composite material |
US5332178A (en) * | 1992-06-05 | 1994-07-26 | Williams International Corporation | Composite wing and manufacturing process thereof |
JPH06255587A (ja) | 1993-03-09 | 1994-09-13 | Honda Motor Co Ltd | 航空機 |
DE4329744C1 (de) | 1993-09-03 | 1994-09-08 | Deutsche Forsch Luft Raumfahrt | Flügel mit Flügelschalen aus Faserverbundwerkstoffen, insbesondere CFK, für Luftfahrzeuge |
US5534203A (en) * | 1994-02-09 | 1996-07-09 | Radius Engineering, Inc. | Composite pole manufacturing process for varying non-circular cross-sections and curved center lines |
US5939007A (en) | 1994-08-31 | 1999-08-17 | Sikorsky Aircraft Corporation | Method for manufacture of a fiber reinforced composite spar for rotary wing aircraft |
US5683646A (en) * | 1995-05-10 | 1997-11-04 | Mcdonnell Douglas Corporation | Fabrication of large hollow composite structure with precisely defined outer surface |
US5958325A (en) | 1995-06-07 | 1999-09-28 | Tpi Technology, Inc. | Large composite structures and a method for production of large composite structures incorporating a resin distribution network |
US5655883A (en) * | 1995-09-25 | 1997-08-12 | General Electric Company | Hybrid blade for a gas turbine |
US5848765A (en) * | 1996-06-20 | 1998-12-15 | The Boeing Company | Reduced amplitude corrugated web spar |
US6217000B1 (en) * | 1996-10-25 | 2001-04-17 | The Boeing Company | Composite fabrication method and tooling to improve part consolidation |
WO1998032589A1 (en) | 1997-01-29 | 1998-07-30 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
US5875732A (en) | 1997-04-18 | 1999-03-02 | Husky Airboats | Method for production of boat hulls and boat hull construction |
FR2766407B1 (fr) | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
US6458309B1 (en) * | 1998-06-01 | 2002-10-01 | Rohr, Inc. | Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel |
JP2000006893A (ja) * | 1998-06-23 | 2000-01-11 | Fuji Heavy Ind Ltd | 複合材翼構造 |
JP2000043796A (ja) * | 1998-07-30 | 2000-02-15 | Japan Aircraft Development Corp | 複合材の翼形構造およびその成形方法 |
DE19836629C1 (de) * | 1998-08-13 | 1999-10-14 | Deutsch Zentr Luft & Raumfahrt | Aerodynamisches Flächentragwerk und Verfahren zu seiner Herstellung |
WO2000018566A1 (fr) | 1998-09-30 | 2000-04-06 | Toray Industries, Inc. | Structure creuse en resine renforcee par des fibres et son procede de fabrication |
DE69926143T2 (de) * | 1998-12-03 | 2006-04-27 | C-Mac Invotronics Inc., Montreal | Hilfsantrieb mit einer elektromagnetischen kupplungseinheit |
US6179945B1 (en) | 1998-12-30 | 2001-01-30 | Owens Corning Fiberglas Technology, Inc. | Process for filament winding composite workpieces |
US6190484B1 (en) * | 1999-02-19 | 2001-02-20 | Kari Appa | Monolithic composite wing manufacturing process |
US6510961B1 (en) * | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
US6513757B1 (en) * | 1999-07-19 | 2003-02-04 | Fuji Jukogyo Kabushiki Kaisha | Wing of composite material and method of fabricating the same |
-
2002
- 2002-06-20 US US10/175,722 patent/US6889937B2/en not_active Expired - Lifetime
-
2003
- 2003-06-19 CN CN03814457A patent/CN100575189C/zh not_active Expired - Fee Related
- 2003-06-19 WO PCT/US2003/019100 patent/WO2004000643A2/en active Application Filing
- 2003-06-19 AT AT03739169T patent/ATE493333T1/de not_active IP Right Cessation
- 2003-06-19 EP EP03739169A patent/EP1585664B1/de not_active Expired - Lifetime
- 2003-06-19 DE DE60335576T patent/DE60335576D1/de not_active Expired - Lifetime
- 2003-06-19 JP JP2004515852A patent/JP4607583B2/ja not_active Expired - Fee Related
- 2003-06-19 AU AU2003245544A patent/AU2003245544A1/en not_active Abandoned
- 2003-12-03 US US10/726,970 patent/US7445744B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE60335576D1 (de) | 2011-02-10 |
WO2004000643A2 (en) | 2003-12-31 |
US20030192990A1 (en) | 2003-10-16 |
EP1585664B1 (de) | 2010-12-29 |
AU2003245544A1 (en) | 2004-01-06 |
CN100575189C (zh) | 2009-12-30 |
JP2006512240A (ja) | 2006-04-13 |
WO2004000643A3 (en) | 2005-12-08 |
US6889937B2 (en) | 2005-05-10 |
EP1585664A2 (de) | 2005-10-19 |
US20040079838A1 (en) | 2004-04-29 |
EP1585664A4 (de) | 2007-09-12 |
CN1819947A (zh) | 2006-08-16 |
JP4607583B2 (ja) | 2011-01-05 |
WO2004000643A8 (en) | 2004-06-10 |
US7445744B2 (en) | 2008-11-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE493333T1 (de) | Einstückiger co-aushärtender verbundflügel | |
EP1539464A4 (de) | Verfahren zur montage einer einstückigen gleichzeitig gehärteten konstruktion | |
JP7299085B2 (ja) | テープ挟み込み型キャッププライを用いる複合ファブリック翼桁 | |
EP3000586B1 (de) | Verfahren zur Herstellung eines Verbundstoffmaterialteils mit einer Bahn und mindestens einem Flansch | |
WO2006118691A3 (en) | Composite skin and stringer structures and methods for forming the same | |
BRPI0516389A (pt) | processo para formar um artigo tridimensional conformado e aparelho | |
HK1115098A1 (en) | Method of manufacturing curved composite structural elements | |
EP2739847A1 (de) | Schaufelsegmentspitze einer windmühle und montageverfahren dafür | |
US20130149166A1 (en) | Formation of a core structure of a wind turbine rotor blade by using a plurality of basic core components | |
JP2010523397A5 (de) | ||
CN102230448A (zh) | 一种竹纤维增强复合材料的风力发电机叶片及制造方法 | |
CN106515170B (zh) | 一种双曲面蜂窝芯板的生产工艺和专用模具 | |
CN106426987A (zh) | 一种整体成形翼面结构成形方法 | |
EP2524794A1 (de) | Schaum- oder Wabenkern, Rotorblatt aus Schaum- oder Wabenkernen und Verfahren zur Herstellung solch eines Rotorblatts | |
GB871625A (en) | Rotor blade structure and method of molding same | |
CN205203353U (zh) | 一种复合材料主承力蜂窝夹芯结构 | |
US9718262B2 (en) | Roll forming composite components | |
CN111923443A (zh) | 一种风电叶片及其成型方法 | |
CN208438808U (zh) | 复合材料及其芯材 | |
CN215512471U (zh) | 一种一体成型复合材料壳体 | |
CN108894687A (zh) | 一种蜂窝结构人防门门扇及采用此门扇的复合材料人防门 | |
TW200635755A (en) | Method for mounting mark on composites and corresponding products | |
CN108248824A (zh) | 一种微小型无人机翼面前缘结构、成型模具及其制备方法 | |
CN208267303U (zh) | 一种高强度高硬度塑木地板 | |
CN206957030U (zh) | 一种钢骨架建材的双五面体叠加成型的六面体钢丝骨架框 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |