ATE493333T1 - Einstückiger co-aushärtender verbundflügel - Google Patents

Einstückiger co-aushärtender verbundflügel

Info

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
Application number
AT03739169T
Other languages
English (en)
Inventor
Craig Simpson
Mike Allman
Steven Tuttle
Larry Ashton
Original Assignee
Rocky Mountain Composites Inc
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 Rocky Mountain Composites Inc filed Critical Rocky Mountain Composites Inc
Application granted granted Critical
Publication of ATE493333T1 publication Critical patent/ATE493333T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/20Integral or sandwich constructions
    • 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
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/006Degassing moulding material or draining off gas during moulding
    • B29C37/0064Degassing moulding material or draining off gas during moulding of reinforced material
    • 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
    • B29C70/40Shaping 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
    • B29C70/443Shaping 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
    • 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure
    • 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
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80Component parts, details or accessories; Auxiliary operations
    • B29C53/8008Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
    • B29C53/8016Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80Component parts, details or accessories; Auxiliary operations
    • B29C53/8008Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
    • B29C53/8066Impregnating
    • 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
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076Aircrafts
    • B29L2031/3085Wings
    • 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
    • Y10S264/90Direct 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
    • Y10S264/904Maintaining 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)
AT03739169T 2002-06-20 2003-06-19 Einstückiger co-aushärtender verbundflügel ATE493333T1 (de)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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WO2004000643A2 (en) 2003-12-31
US20030192990A1 (en) 2003-10-16
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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

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