DE60036234D1 - Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung - Google Patents

Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung

Info

Publication number
DE60036234D1
DE60036234D1 DE60036234T DE60036234T DE60036234D1 DE 60036234 D1 DE60036234 D1 DE 60036234D1 DE 60036234 T DE60036234 T DE 60036234T DE 60036234 T DE60036234 T DE 60036234T DE 60036234 D1 DE60036234 D1 DE 60036234D1
Authority
DE
Germany
Prior art keywords
making
same
wing structure
composite
fiber composite
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60036234T
Other languages
English (en)
Other versions
DE60036234T2 (de
Inventor
Kazuaki Amaoka
Takayuki Nagao
Atsushi Harada
Naoya Takizawa
Sano Hideyuki
Yasuhiro Toi
Megumi Hiraki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Subaru Corp
Original Assignee
Fuji Jukogyo KK
Fuji Heavy Industries Ltd
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
Priority claimed from JP20445199A external-priority patent/JP4187878B2/ja
Priority claimed from JP22163799A external-priority patent/JP4316057B2/ja
Priority claimed from JP27850099A external-priority patent/JP4316067B2/ja
Application filed by Fuji Jukogyo KK, Fuji Heavy Industries Ltd filed Critical Fuji Jukogyo KK
Application granted granted Critical
Publication of DE60036234D1 publication Critical patent/DE60036234D1/de
Publication of DE60036234T2 publication Critical patent/DE60036234T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/32Shaping 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 on a rotating mould, former or core
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/462Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/20Integral or sandwich constructions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24281Struck out portion type
    • Y10T428/24289Embedded or interlocked

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Transportation (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE60036234T 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung Expired - Lifetime DE60036234T2 (de)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
JP20445199 1999-07-19
JP20445199A JP4187878B2 (ja) 1999-07-19 1999-07-19 航空機の複合材翼およびその製造方法
JP22163799A JP4316057B2 (ja) 1999-08-04 1999-08-04 複合材翼
JP22163799 1999-08-04
JP27850099 1999-09-30
JP27850099A JP4316067B2 (ja) 1999-09-30 1999-09-30 複合材翼およびその成形方法

Publications (2)

Publication Number Publication Date
DE60036234D1 true DE60036234D1 (de) 2007-10-11
DE60036234T2 DE60036234T2 (de) 2008-05-21

Family

ID=27328363

Family Applications (3)

Application Number Title Priority Date Filing Date
DE60020456T Expired - Lifetime DE60020456T2 (de) 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung
DE60044407T Expired - Lifetime DE60044407D1 (de) 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung
DE60036234T Expired - Lifetime DE60036234T2 (de) 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung

Family Applications Before (2)

Application Number Title Priority Date Filing Date
DE60020456T Expired - Lifetime DE60020456T2 (de) 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung
DE60044407T Expired - Lifetime DE60044407D1 (de) 1999-07-19 2000-07-18 Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung

Country Status (3)

Country Link
US (2) US6513757B1 (de)
EP (3) EP1070661B8 (de)
DE (3) DE60020456T2 (de)

Families Citing this family (110)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US7681835B2 (en) * 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
JP4574086B2 (ja) * 2001-09-03 2010-11-04 富士重工業株式会社 複合材翼の製造方法および複合材翼
GB0122050D0 (en) * 2001-09-13 2001-10-31 Bae Systems Plc Composite material structure
US7053971B2 (en) * 2002-07-17 2006-05-30 Citzen Watch Co., Ltd. Liquid crystal display panel
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
BRPI0407749A (pt) * 2003-02-24 2006-02-14 Bell Helicopter Textron Inc enrijecedores de contato para envoltórios estruturais
US6896841B2 (en) * 2003-03-20 2005-05-24 The Boeing Company Molding process and apparatus for producing unified composite structures
US7037568B1 (en) 2003-07-15 2006-05-02 Rogers Terry W Joining member for mechanically joining a skin to a supporting rib
US7638084B2 (en) * 2004-03-19 2009-12-29 Frankel Kenneth A Methods for forming fiber reinforced composite parts having one or more selectively positioned core, structural insert, or veneer pieces integrally associated therewith
US7387277B2 (en) 2004-12-29 2008-06-17 The Boeing Company Aircraft wing composed of composite and metal panels
US7398586B2 (en) * 2005-11-01 2008-07-15 The Boeing Company Methods and systems for manufacturing a family of aircraft wings and other composite structures
WO2007091990A2 (en) * 2006-01-11 2007-08-16 The Boeing Company Aircraft wing composed of composite and metal panels
US7517198B2 (en) 2006-03-20 2009-04-14 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
GB0611804D0 (en) * 2006-06-14 2006-07-26 Airbus Uk Ltd Improved aircraft component
GB0614087D0 (en) 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
GB0615104D0 (en) * 2006-07-28 2006-09-06 Airbus Uk Ltd Aircraft wing box and manufacture thereof
FR2906218B1 (fr) * 2006-09-21 2009-05-15 Airbus France Sas Raidisseur autostabilise autorisant une reprise d'elements
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
EP1918193A1 (de) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrierte Verbundhaut für Flugzeug-Midbox-Hebeoberflächen
GB0621952D0 (en) * 2006-11-03 2006-12-13 Airbus Uk Ltd A stringer for an aircraft wing and a method of reinforcing thereof
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
WO2008132251A1 (es) * 2007-04-30 2008-11-06 Airbus España, S.L. Cajón de torsión multilarguero integrado de material compuesto
ES2330180B1 (es) * 2007-06-28 2010-09-14 Airbus España S.L. Cajon de torsion multilarguero rigidizado.
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
GB0712549D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Improvements in elongate composite structural members
GB0712553D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Composite panel stiffener
US8016970B2 (en) * 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
GB0717690D0 (en) * 2007-09-11 2007-10-17 Blade Dynamics Ltd Wind turbine blade
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
CN201225330Y (zh) * 2008-06-24 2009-04-22 陈清辉 木质吊扇叶片
ES2371401B1 (es) * 2008-06-27 2012-11-07 Airbus Operations, S.L. Estructura de superficie sustentadora de aeronave.
GB0813146D0 (en) * 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
GB0813161D0 (en) 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
DK3276162T3 (da) 2008-12-05 2020-05-04 Vestas Wind Sys As Effektive vindmøllevinger, vindmøllevingestrukturer og associerede systemer og fremgangsmåder til fremstilling, samling og anvendelse
RU2560194C2 (ru) * 2009-05-28 2015-08-20 Сосьете Лоррен Де Констрюксьон Эронотик Композитная конструктивная панель задней кромки элемента летательного аппарата
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.
ES2392617B1 (es) * 2010-01-15 2013-11-21 Airbus Operations S.L. Disposición de unión de los cajones laterales de un estabilizador horizontal de cola con un cajón central tubular y procedimiento de fabricación de dicho cajón.
GB201000878D0 (en) * 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
DE102010003114A1 (de) * 2010-03-22 2011-09-22 Repower Systems Ag Stegverbindung
US8192169B2 (en) * 2010-04-09 2012-06-05 Frederick W Piasecki Highly reliable, low cost wind turbine rotor blade
FR2960179A1 (fr) * 2010-05-20 2011-11-25 Airbus Operations Sas Piece structurale composite a rigidite evolutive
US9500179B2 (en) 2010-05-24 2016-11-22 Vestas Wind Systems A/S Segmented wind turbine blades with truss connection regions, and associated systems and methods
FR2962409B1 (fr) * 2010-07-09 2012-09-21 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
US20120012242A1 (en) * 2010-07-14 2012-01-19 Spirit Aerosystems, Inc. Method and system for material placement over radiused edges
US8348196B2 (en) 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint
US8317483B2 (en) * 2010-12-15 2012-11-27 General Electric Company Wind turbine rotor blade
JP5851699B2 (ja) 2011-02-10 2016-02-03 三菱重工業株式会社 大型構造物の組み立てに用いる組立治具
DE102011007235A1 (de) 2011-04-12 2012-10-18 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung eines Faserverbundbauteils und Faserverbundbauteil
US8262362B2 (en) 2011-06-08 2012-09-11 General Electric Company Wind turbine blade shear web with spring flanges
US20130011605A1 (en) * 2011-07-05 2013-01-10 Israel Aerospace Industries Ltd. Manufacture of articles formed of composite materials
US8257048B2 (en) 2011-07-19 2012-09-04 General Electric Company Wind turbine blade multi-component shear web with intermediate connection assembly
US8235671B2 (en) 2011-07-19 2012-08-07 General Electric Company Wind turbine blade shear web connection assembly
US8393871B2 (en) * 2011-07-19 2013-03-12 General Electric Company Wind turbine blade shear web connection assembly
DE112011105793T5 (de) 2011-11-01 2014-09-04 General Electric Company Rotorblätter für Windkraftanlagen mit abdeckungsunterstützter Verklebungskonfiguration und zugehöriges Klebeverfahren
US9458823B2 (en) 2011-12-12 2016-10-04 General Electric Company Wind turbine blade shear web connection assembly
US9017510B2 (en) 2011-12-13 2015-04-28 The Boeing Company Method and apparatus for fabricating large scale integrated airfoils
US9481444B2 (en) * 2012-09-12 2016-11-01 The Boeing Company Passive load alleviation for aerodynamic lift structures
WO2014068572A2 (en) 2012-11-01 2014-05-08 Israel Aerospace Industries Ltd. Manufacture of integrated structures formed of composite materials
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
ES2606591T3 (es) * 2012-11-21 2017-03-24 Airbus Operations S.L. Un cajón de torsión optimizado para 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
IL223443A (en) 2012-12-04 2014-06-30 Elbit Systems Cyclone Ltd Buildings from composite materials with integral composite connectors and manufacturing methods
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
US8983171B2 (en) 2012-12-26 2015-03-17 Israel Aerospace Industries Ltd. System and method for inspecting structures formed of composite materials during the fabrication thereof
US8973871B2 (en) 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US20140272312A1 (en) 2013-03-13 2014-09-18 Gulfstream Aerospace Corporation Aircraft component and method of making an aircraft component
US9470205B2 (en) 2013-03-13 2016-10-18 Vestas Wind Systems A/S Wind turbine blades with layered, multi-component spars, and associated systems and methods
US9638048B2 (en) * 2013-03-15 2017-05-02 Bell Helicopter Textron Inc. Systems and methods of constructing composite assemblies
US20150203187A1 (en) * 2013-04-02 2015-07-23 The Boeing Company Continuously Curved Spar and Method of Manufacturing
GB201307066D0 (en) * 2013-04-18 2013-05-29 Airbus Operations Ltd Winglet and braided composite spar
CN103204236B (zh) * 2013-04-24 2015-07-01 哈尔滨飞机工业集团有限责任公司 一种用于直升机的多用途外挂装置
US9506452B2 (en) * 2013-08-28 2016-11-29 General Electric Company Method for installing a shear web insert within a segmented rotor blade assembly
US10723438B2 (en) 2013-08-30 2020-07-28 Bell Helicopter Textron Inc. System and methods of constructing composite assemblies
US9751256B2 (en) * 2014-01-20 2017-09-05 Lockheed Martin Corporation Joint molding apparatus
RU2549043C1 (ru) * 2014-04-17 2015-04-20 Открытое акционерное общество "Национальный институт авиационных технологий" (ОАО НИАТ) Кессон крыла, армированный полимерным композиционным материалом
US9745954B2 (en) 2014-04-30 2017-08-29 General Electric Company Rotor blade joint assembly with multi-component shear web
US10518516B2 (en) 2014-10-31 2019-12-31 The Boeing Company Method and system of forming a composite laminate
FR3030443B1 (fr) * 2014-12-18 2016-12-09 Airbus Operations Sas Procede de fabrication d'un caisson central de voilure integrant au moins un longeron intermediaire et caisson central de voilure ainsi obtenu
CN104494808B (zh) * 2014-12-23 2017-01-04 无锡透平叶片有限公司 一种易于钛合金锻件高筋成形的结构
CN104554704B (zh) * 2015-01-27 2016-09-28 新誉集团有限公司 可横向组装的大展弦比机翼结构及其组装方法
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
GB2550403A (en) * 2016-05-19 2017-11-22 Airbus Operations Ltd Aerofoil body with integral curved spar-cover
RU168933U1 (ru) * 2016-08-25 2017-02-28 Российская Федерация от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Оснастка для изготовления крыла летательного аппарата
US10717512B2 (en) * 2016-11-03 2020-07-21 Continuous Composites Inc. Composite vehicle body
ES2764122T3 (es) * 2016-12-02 2020-06-02 Airbus Operations Sl Integración del borde de ataque de un estabilizador de aeronave con el cajón de torsión y el fuselaje
NL2018263B1 (nl) * 2017-01-31 2018-08-16 Fibercore Ip Bv Aerodynamisch of hydrodynamisch blad uit gelaagd materiaal
US10519927B2 (en) 2017-02-20 2019-12-31 General Electric Company Shear web for a wind turbine rotor blade
US11511847B2 (en) 2017-03-28 2022-11-29 The Boeing Company Skin panel of composite material having an internal grid
CN107128508B (zh) * 2017-04-21 2019-11-15 陕西飞机工业(集团)有限公司 一种平直机翼成型方法
US10570879B2 (en) 2017-05-23 2020-02-25 General Electric Company Joint assembly for a wind turbine rotor blade with flanged bushings
US10544776B2 (en) 2017-07-27 2020-01-28 General Electric Company Injection method and device for connecting and repairing a shear web
US10563636B2 (en) 2017-08-07 2020-02-18 General Electric Company Joint assembly for a wind turbine rotor blade
CN108177360A (zh) * 2017-12-25 2018-06-19 航天神舟飞行器有限公司 无人机复合材料机翼整体壁板的成型工装及其成型方法
GB2573285A (en) * 2018-04-27 2019-11-06 Airbus Operations Ltd Composite spar for a wing structure
US11247429B2 (en) 2018-05-10 2022-02-15 Raytheon Company Bonding assembly system including timed bladder system
CN109606636A (zh) * 2018-11-02 2019-04-12 中国航空工业集团公司西安飞机设计研究所 一种通用飞机方向舵复合材料翼尖结构及制造方法
RU192695U1 (ru) * 2019-06-10 2019-09-26 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" (КНИТУ-КАИ) Крыло беспилотного летательного аппарата из композиционного материала
US11613219B2 (en) 2019-06-11 2023-03-28 The Boeing Company Energy subsystems integrated into structural components of an aircraft
US11530026B2 (en) * 2019-06-11 2022-12-20 The Boeing Company Energy subsystems integrated into structural components of an aircraft
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
ES2953735T3 (es) * 2019-12-11 2023-11-15 Airbus Operations Slu Borde de salida para una superficie de elevación integrada multilarguero de material compuesto y método de fabricación de dicho borde de salida
CN112339986B (zh) * 2020-09-22 2022-10-25 成都飞机工业(集团)有限责任公司 一种蒙皮骨架一体中温快速成型复合材料结构及方法
AT524687B1 (de) * 2021-05-27 2022-08-15 Facc Ag Verfahren zum Verschweißen von Faser-Kunststoff-Verbund-(FKV)-Bauteilen und Stabilisierungsvorrichtung
EP4095031A1 (de) * 2021-05-28 2022-11-30 Airbus Operations GmbH Verfahren zur herstellung einer strukturellen komponente eines fahrzeugs und strukturelle komponente
FR3128896A1 (fr) * 2021-11-10 2023-05-12 Benoît Matte Armature pour structure en matériau composite, et structure en matériau composite comprenant une telle armature
US20230211572A1 (en) * 2022-01-04 2023-07-06 Rohr, Inc. Component with monolithic structure having blind interface joint

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2032283A1 (de) * 1969-07-04 1971-03-25 Hawker Siddeley Aviation Ltd , King ston upon Thames, Surrey (Großbritannien) Groß Tragwerk, insbesondere Haupt bauteil eines Flugzeugs
US3995081A (en) * 1974-10-07 1976-11-30 General Dynamics Corporation Composite structural beams and method
US4051289A (en) * 1976-04-12 1977-09-27 General Electric Company Composite airfoil construction
US4331495A (en) * 1978-01-19 1982-05-25 Rockwell International Corporation Method of fabricating a reinforced composite structure
US4452657A (en) * 1982-09-15 1984-06-05 The Boeing Company Composite integral web stiffening method
WO1985001489A1 (en) * 1983-09-29 1985-04-11 The Boeing Company High strength to weight horizontal and vertical aircraft stabilizer
US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
US4671470A (en) * 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
US4749155A (en) * 1985-09-30 1988-06-07 The Boeing Company Method of making wing box cover panel
US5087187A (en) * 1990-03-09 1992-02-11 United Technologies Corporation Apparatus for molding hollow composite articles having internal reinforcement structures
US7126096B1 (en) * 1991-04-05 2006-10-24 Th Boeing Company Resistance welding of thermoplastics in aerospace structure
US5332178A (en) * 1992-06-05 1994-07-26 Williams International Corporation Composite wing and manufacturing process thereof
AT398064B (de) * 1992-07-01 1994-09-26 Hoac Austria Flugzeugwerk Wr N Kunststoff-verbundprofil, insbesondere flügelholm für den flugzeugbau
DE4315600C2 (de) * 1993-05-11 1996-07-25 Daimler Benz Aerospace Airbus Tragstruktur für eine aerodynamische Fläche
US5547629A (en) * 1994-09-27 1996-08-20 Competition Composites, Inc. Method for manufacturing a one-piece molded composite airfoil
DE19528664C2 (de) * 1995-08-04 1997-07-31 Joachim Heyse Tragkörper aus einem Verbundwerkstoff
US6217000B1 (en) * 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
JPH10258463A (ja) * 1997-03-19 1998-09-29 Fuji Heavy Ind Ltd 複合材の小骨およびその成形方法
US6173925B1 (en) * 1998-04-16 2001-01-16 Daimlerchrysler Ag Skin-rib structure
JP2000006893A (ja) * 1998-06-23 2000-01-11 Fuji Heavy Ind Ltd 複合材翼構造
US6190484B1 (en) * 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process

Also Published As

Publication number Publication date
DE60036234T2 (de) 2008-05-21
EP1070661A3 (de) 2003-03-05
EP1555204A1 (de) 2005-07-20
US20020195524A1 (en) 2002-12-26
EP1070661B8 (de) 2005-07-20
US6561459B2 (en) 2003-05-13
EP1806285B1 (de) 2010-05-12
EP1070661A2 (de) 2001-01-24
DE60044407D1 (de) 2010-06-24
DE60020456T2 (de) 2005-10-13
EP1555204B1 (de) 2007-08-29
EP1070661B1 (de) 2005-06-01
DE60020456D1 (de) 2005-07-07
US6513757B1 (en) 2003-02-04
EP1806285A1 (de) 2007-07-11

Similar Documents

Publication Publication Date Title
DE60044407D1 (de) Flügelstruktur aus Verbundfaserwerkstoff und Verfahren zu dessen Herstellung
DE60008501D1 (de) Wabenkernmaterial für verbundwerkstoffstrukturen und verfahren zu dessen herstellung
DE69733530D1 (de) Flexibler verbundstoff ohne klebstoff und verfahren zu seiner herstellung
DE69934463D1 (de) Cellulosischer Verbundwerkstoff und Verfahren zu dessen Herstellung
DE69814454D1 (de) Verbundwerkstoff mit elastischen abschnitten und verfahren zu seiner herstellung
DE60041725D1 (de) Röhrenförmige Stent-Graft-Kompositvorrichtung und Verfahren zu ihrer Herstellung
DE60106698D1 (de) Faser aus anorganischem Material und Verfahren zu deren Herstellung
ATE379971T1 (de) Disinfektionsmittel und verfahren zu dessen herstellung
DE69819755D1 (de) Leicht zu öffnende verpackung sowie verfahren zur herstellung derselbe
DE60127239D1 (de) Verbundstoff mit feuerverzögernden eigenschaften und verfahren zu seiner herstellung
DE50004342D1 (de) Verbundlaminat und verfahren zu seiner herstellung
DE69824761D1 (de) Faserstruktur und verfahren zu seiner herstellung
ATE288577T1 (de) Ladeluftkühler und verfahren zu dessen herstellung
DE60018049D1 (de) Ionisationsstab und verfahren zu dessen herstellung
DE60024801D1 (de) Polyurethanharnstofffasern und verfahren zu ihrer herstellung
DE60014701D1 (de) Zusammensetzungen aus zellstofffasern und verfahren zu deren herstellung
ATE198977T1 (de) Einbügelbarer einlagestoff und verfahren zu dessen herstellung
ATE250686T1 (de) Vliesverbund, verfahren zu dessen herstellung und dessen verwendung
DE69832822D1 (de) Beschichtete langfaserige verstärkungsverbundstruktur und verfahren zu deren herstellung
DE50010354D1 (de) Verbundteil und verfahren zu dessen herstellung
DE69905326T2 (de) Sollerschlitz und Verfahren zu dessen Herstellung
ATA75297A (de) Dekorlaminat und verfahren zu seiner herstellung
DE60044573D1 (de) Mit Gewinde versehenes Befestigungselement und Verfahren zu dessen Herstellung
DE69724921D1 (de) Freitragender Ausleger und Verfahren zu dessen Herstellung
DE59703243D1 (de) Cellulose-gebundenes faservlies und verfahren zu dessen herstellung

Legal Events

Date Code Title Description
8364 No opposition during term of opposition