DE3341564A1 - Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung - Google Patents

Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung

Info

Publication number
DE3341564A1
DE3341564A1 DE19833341564 DE3341564A DE3341564A1 DE 3341564 A1 DE3341564 A1 DE 3341564A1 DE 19833341564 DE19833341564 DE 19833341564 DE 3341564 A DE3341564 A DE 3341564A DE 3341564 A1 DE3341564 A1 DE 3341564A1
Authority
DE
Germany
Prior art keywords
fiber
reinforced plastic
stringers
surface component
outer skin
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.)
Granted
Application number
DE19833341564
Other languages
German (de)
English (en)
Other versions
DE3341564C2 (https=
Inventor
Branko Dipl.-Ing. 2000 Hamburg Sarh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE19833341564 priority Critical patent/DE3341564A1/de
Priority to DE8484112270T priority patent/DE3462111D1/de
Priority to EP84112270A priority patent/EP0142697B1/de
Priority to US06/670,472 priority patent/US4633632A/en
Priority to JP59240868A priority patent/JPS60128097A/ja
Publication of DE3341564A1 publication Critical patent/DE3341564A1/de
Priority to US06/932,686 priority patent/US4717330A/en
Application granted granted Critical
Publication of DE3341564C2 publication Critical patent/DE3341564C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
    • B21J15/142—Aerospace 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
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/58—Winding and joining, e.g. winding spirally helically
    • B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/68—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels with rotatable winding feed member
    • B29C53/70—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels with rotatable winding feed member and moving axially
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • 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
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B29C2791/00—Shaping characteristics in general
    • B29C2791/001—Shaping in several steps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
DE19833341564 1983-11-17 1983-11-17 Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung Granted DE3341564A1 (de)

Priority Applications (6)

Application Number Priority Date Filing Date Title
DE19833341564 DE3341564A1 (de) 1983-11-17 1983-11-17 Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung
DE8484112270T DE3462111D1 (en) 1983-11-17 1984-10-12 Shaped-surface structural elements, especially for aircraft, and device for manufacturing them
EP84112270A EP0142697B1 (de) 1983-11-17 1984-10-12 Gekrümmtes Flächenbauteil, insbesondere für Luftfahrzeuge und Vorrichtung zu dessen Herstellung
US06/670,472 US4633632A (en) 1983-11-17 1984-11-09 Structural component having a curved wall and apparatus for making such structural component
JP59240868A JPS60128097A (ja) 1983-11-17 1984-11-16 特に飛行機用の彎曲した面構造体およびこれを造るための装置
US06/932,686 US4717330A (en) 1983-11-17 1986-11-18 Apparatus for making a structural component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833341564 DE3341564A1 (de) 1983-11-17 1983-11-17 Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung

Publications (2)

Publication Number Publication Date
DE3341564A1 true DE3341564A1 (de) 1985-05-30
DE3341564C2 DE3341564C2 (https=) 1987-06-19

Family

ID=6214554

Family Applications (2)

Application Number Title Priority Date Filing Date
DE19833341564 Granted DE3341564A1 (de) 1983-11-17 1983-11-17 Gekruemmtes flaechenbauteil, insbesondere fuer luftfahrzeuge und vorrichtung zu deren herstellung
DE8484112270T Expired DE3462111D1 (en) 1983-11-17 1984-10-12 Shaped-surface structural elements, especially for aircraft, and device for manufacturing them

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE8484112270T Expired DE3462111D1 (en) 1983-11-17 1984-10-12 Shaped-surface structural elements, especially for aircraft, and device for manufacturing them

Country Status (4)

Country Link
US (2) US4633632A (https=)
EP (1) EP0142697B1 (https=)
JP (1) JPS60128097A (https=)
DE (2) DE3341564A1 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013222106A1 (de) * 2013-10-30 2015-05-13 Airbus Operations Gmbh Aushärtungswerkzeug für Schalenbauteile und Verfahren zum Aushärten von Schalenbauteilen

Families Citing this family (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3605256C1 (de) * 1986-02-19 1991-03-28 Dornier Gmbh Verfahren zur Herstellung von ebenen oder schalenfoermig gekruemmten Bauteilen aus faserverstaerkten Kunststoffen
DE3614618A1 (de) * 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm Schalenstruktur aus faserverstaerktem kunststoff
US5022845A (en) * 1989-04-25 1991-06-11 Hercules Incorporated Segmented mandrel for forming composite articles
ES2146140B1 (es) * 1996-10-15 2001-04-01 Torres Martinez M Maquina para el soporte y mecanizado de piezas.
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6217000B1 (en) 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
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
ES2131479B1 (es) * 1997-11-10 2000-03-01 Torres Martinez M Util y proceso de ensamblaje para soldadura laser.
US6149851A (en) * 1998-04-30 2000-11-21 Alliant Techsystems Inc. Tooling apparatus and method for producing grid stiffened fiber reinforced structures
US6026883A (en) * 1998-04-30 2000-02-22 Alliant Techsystems, Inc. Self-contained apparatus for fiber element placement
US6050315A (en) * 1998-04-30 2000-04-18 Alliant Techsystems Inc. Method and apparatus for producing fiber reinforced structures
ES2169620B1 (es) 1999-01-22 2003-11-01 Torres Ingenieria De Procesos Util para el montaje de secciones del fuselaje de aeronaves.
JP4316059B2 (ja) * 1999-08-06 2009-08-19 富士重工業株式会社 複合材翼の製造方法
US7228611B2 (en) * 2003-11-18 2007-06-12 The Boeing Company Method of transferring large uncured composite laminates
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7293737B2 (en) * 2004-04-20 2007-11-13 The Boeing Company Co-cured stringers and associated mandrel and fabrication method
US7182293B2 (en) 2004-04-27 2007-02-27 The Boeing Company Airfoil box and associated method
FR2882681B1 (fr) * 2005-03-03 2009-11-20 Coriolis Composites Tete d'application de fibres et machine correspondante
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
US8601694B2 (en) * 2008-06-13 2013-12-10 The Boeing Company Method for forming and installing stringers
FR2894869B1 (fr) * 2005-12-20 2009-10-09 Airbus France Sas Procede de fabrication d'un fuselage d'aeronef en materiau composite
US7639542B2 (en) 2006-05-15 2009-12-29 Apple Inc. Maintenance operations for multi-level data storage cells
GB0616406D0 (en) * 2006-08-17 2006-09-27 Airbus Uk Ltd A platform
WO2008025860A1 (es) * 2006-08-31 2008-03-06 Airbus España, S.L. Componentes tubulares para fuselajes aeronauticos y procedimientos y utiles para su fabricacion
FR2906008B1 (fr) * 2006-09-15 2008-11-07 Airbus France Sa Eclisse de lisses et dispositif de jonction orbitale
US7635106B2 (en) 2006-11-30 2009-12-22 The Boeing Company Composite shear tie
DE102007003275B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Schalenelement als Teil eines Flugzeugrumpfes
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
FR2913365B1 (fr) * 2007-03-06 2013-07-26 Coriolis Composites Attn Olivier Bouroullec Tete d'application de fibres avec systemes de coupe de fibres particuliers
FR2913366B1 (fr) * 2007-03-06 2009-05-01 Coriolis Composites Sa Tete d'application de fibres avec systemes de coupe et de blocage de fibres particuliers
DE102007019821B4 (de) 2007-04-26 2012-11-22 Airbus Operations Gmbh Strukturelement eines Flugzeugrumpfs
US8043458B2 (en) * 2007-06-21 2011-10-25 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
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
FR2946024B1 (fr) * 2009-05-27 2011-07-22 Airbus France Installation de realisation d'un troncon de fuselage d'aeronef.
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
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
ES2370324B1 (es) * 2009-08-17 2012-07-04 Aritex Cading, S.A. Planta para el montaje de alas de avión con equipo de gradas flexibles reconfigurables.
FR2958875B1 (fr) * 2010-04-20 2017-07-07 Snecma Dispositif de fabrication d'un carter en materiau composite et procede de fabrication mettant en oeuvre un tel dispositif
DE102010020368B4 (de) * 2010-05-12 2015-12-03 Airbus Operations Gmbh Verfahren und Werkzeug zur Bestückung einer Rumpfschale mit einem Fensterrahmen
US9126374B2 (en) 2010-09-28 2015-09-08 Russell B. Hanson Iso-grid composite component
DE102010043415B4 (de) 2010-11-04 2015-04-09 Airbus Operations Gmbh Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung
DE102011010539A1 (de) * 2011-02-07 2012-08-09 Airbus Operations Gmbh Aufrüstvorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpftonne für ein Luftfahrzeug
GB201120994D0 (en) * 2011-12-07 2012-01-18 Airbus Uk Ltd Integral stiffener
US8851422B2 (en) * 2012-08-28 2014-10-07 The Boeing Company Bonded composite aircraft wing
JP6239272B2 (ja) * 2013-06-04 2017-11-29 三菱航空機株式会社 繊維強化プラスチック部材の成形方法および成形装置
EP2878435B1 (en) * 2013-11-28 2018-07-18 Airbus Operations, S.L. Method for manufacturing an integrated composite trailing edge
US9676126B2 (en) * 2013-12-16 2017-06-13 Lockheed Martin Corporation Open-face molding
US9597843B2 (en) 2014-05-15 2017-03-21 The Boeing Company Method and apparatus for layup tooling
FR3034338B1 (fr) 2015-04-01 2017-04-21 Coriolis Composites Tete d'application de fibres avec rouleau d'application particulier
GB201507519D0 (en) * 2015-05-01 2015-06-17 Vestas Wind Sys As Reinforcing Structure for a Wind Turbine Blade
FR3043010B1 (fr) 2015-10-28 2017-10-27 Coriolis Composites Machine d'application de fibres avec systemes de coupe particuliers
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
US11331867B2 (en) 2016-08-23 2022-05-17 Textron Innovations, Inc. Nested manufacturing of composite structures
FR3056438B1 (fr) 2016-09-27 2019-11-01 Coriolis Group Procede de realisation de pieces en materiau composite par impregnation d'une preforme particuliere.
FR3070623B1 (fr) 2017-09-04 2020-10-09 Coriolis Composites Procede de realisation d’une piece en materiau composite par aiguilletage oriente d’une preforme
US11358348B2 (en) * 2019-01-02 2022-06-14 The Boeing Company Mold insert for use with a mandrel for forming a composite structure
DE102019114710A1 (de) * 2019-05-31 2020-12-03 Airbus Operations Gmbh Vorrichtung und Verfahren
AT522965B1 (de) * 2020-01-10 2021-04-15 Robert Jaeger Vorrichtung und Verfahren zur Bildung großvolumiger, hohlkörperförmiger Faserverbund-Bauteile
CN111152476A (zh) * 2020-01-17 2020-05-15 精功（绍兴）复合材料技术研发有限公司 一种超大型筒体缠绕成型模具
US11648739B2 (en) * 2020-06-04 2023-05-16 Safran Aircraft Engines Rtm injection mold and method using asymmetric anti-pinching sectors
CN112125673B (zh) * 2020-09-17 2022-08-09 中航复合材料有限责任公司 一种基于先驱体浸渍裂解工艺制备直角形长桁的方法
US12043005B2 (en) * 2021-02-04 2024-07-23 Lockheed Martin Corporation Mandrel support system and method
US12611823B2 (en) 2022-12-13 2026-04-28 The Boeing Company In-tool compaction for composite structures

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003552A1 (de) * 1980-01-31 1981-08-06 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flaechenbauteil, insbesondere fuer luftfahrzeuge

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1802815A (en) * 1928-01-25 1931-04-28 Commercial Shearing Tunnel-liner form
US2298839A (en) * 1939-10-30 1942-10-13 Porter William Alfred Form for concrete arch constructions
GB711282A (en) * 1951-04-24 1954-06-30 W & J R Watson Ltd Improvements in or relating to shuttering for casting concrete
US3058704A (en) * 1958-01-16 1962-10-16 Johnson & Johnson Laminated adhesive sheeting for aircraft
FR1345076A (fr) * 1962-10-24 1963-12-06 Sud Aviation Perfectionnement aux structures à revêtement mince renforcé par des éléments longitudinaux et transversaux
US3590590A (en) * 1969-03-03 1971-07-06 Petar Steva Vujasinovic Tunnel building
US3976269A (en) * 1974-12-19 1976-08-24 The Boeing Company Intrinsically tuned structural panel
US4171999A (en) * 1976-12-01 1979-10-23 Allen John D Method of fabricating a tank by joining wall sections with fiber reinforced joiner panels
AT381546B (de) * 1981-05-20 1986-10-27 Patenver Ag Traeger fuer schalungskonstruktionen fuer rundgebaeude
US4450661A (en) * 1981-09-30 1984-05-29 The Boeing Company Composite structures window belt and method of making
US4448628A (en) * 1982-07-14 1984-05-15 Stott Rexeene S Segmental mandrel for making wound filament structures
US4557090A (en) * 1983-10-07 1985-12-10 Keller Sr Robert R Curvilinear structural insulating panel and method of making the same

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003552A1 (de) * 1980-01-31 1981-08-06 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flaechenbauteil, insbesondere fuer luftfahrzeuge

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013222106A1 (de) * 2013-10-30 2015-05-13 Airbus Operations Gmbh Aushärtungswerkzeug für Schalenbauteile und Verfahren zum Aushärten von Schalenbauteilen
US9592640B2 (en) 2013-10-30 2017-03-14 Airbus Operations Gmbh Method for curing shell components

Also Published As

Publication number Publication date
US4717330A (en) 1988-01-05
JPH0425198B2 (https=) 1992-04-30
EP0142697B1 (de) 1987-01-21
US4633632A (en) 1987-01-06
EP0142697A1 (de) 1985-05-29
DE3462111D1 (en) 1987-02-26
DE3341564C2 (https=) 1987-06-19
JPS60128097A (ja) 1985-07-08

Similar Documents

Publication Publication Date Title
EP0142697B1 (de) Gekrümmtes Flächenbauteil, insbesondere für Luftfahrzeuge und Vorrichtung zu dessen Herstellung
DE69100380T2 (de) Struktur und Verfahren zur Herstellung eines Flugzeugrumpfs.
EP2046564B1 (de) Verfahren zur Herstellung von mehreren Faserverbundbauteilen
DE69324312T2 (de) Anlage zur Herstellung von kohlefaserverstärkten Strukturen und Verfahren zur Herstellung, für Anwendungen im aeronautischen Bereich
DE102009060706B4 (de) Verfahren sowie Vorrichtung zur Herstellung einer Versteifungsstruktur für ein Flugzeugrumpfsegment sowie eine Versteifungsstruktur
EP2229273B1 (de) Verfahren und vorrichtung zur herstellung röhrenförmiger strukturbauteile
DE19832441C1 (de) Verfahren zur Herstellung einer stringerversteiften Schale in Faserverbundbauweise
DE68904601T2 (de) Faserverstaerktes spant, insbesondere eines luftfahrzeugrumpfs, und sein herstellungsverfahren.
DE102007003275B4 (de) Schalenelement als Teil eines Flugzeugrumpfes
DE602004009516T2 (de) Selbstverstärkte Verbundplatten aus Prepreg und Verfahren zur Positionierung von Teilen solcher Platten
DE3806594C2 (de) Abnehmbarer oder schwenkbarer Bauteil zum Verkleiden von Öffnungen im Rumpf eines Flugzeuges sowie Verfahren zur Herstellung des Bauteiles und Vorrichtung zur Durchführung des Verfahrens
EP2419325B1 (de) Spant und verfahren zur herstellung eines solchen spants
WO2018029240A1 (de) Gurt aus vorgefertigten elementen mit gelege und ein verfahren zu seiner fertigung
DE3003552A1 (de) Flaechenbauteil, insbesondere fuer luftfahrzeuge
DE102007041282A1 (de) Sandwichbauteilanordnung mit einem L-förmigen oder T-förmigen Element und Verfahren zur Herstellung derselben
DE1951310A1 (de) Leichtgewichtiges Verbundgebilde
EP3656527B1 (de) Fertigungsverfahren sowie verformbare konstruktionsplatte zum formlosen herstellen eines faserverstärkten formteils, insbesondere eines bootsrumpfs
DE102011010539A1 (de) Aufrüstvorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpftonne für ein Luftfahrzeug
DE102005030939A1 (de) Verfahren zur Herstellung eines im Wesentlichen schalenförmigen Bauteils
DE102014221356B4 (de) Baugruppe mit Einzelkomponenten aus einem faserverstärkten Verbundmaterial
EP1011963A1 (de) Verfahren zum herstellen von ausschnitten in faserverbund-sandwichstrukturen und dadurch hergestellter ausschnitt
DE102007015516B4 (de) Kunststoff-Faser-Verbundbauteil in Form eines Profils mit über die Länge variierendem Profilquerschnitt
DE102009057006A1 (de) Vorrichtung und Verfahren zur Herstellung eines gekrümmten Verbundbauteils sowie Verbundbauteil
DE3107838C2 (de) Verfahren zur Herstellung von Doppelmantel-Kunststoffrohren
DE102007004313B4 (de) Verfahren zur Herstellung eines Bauteils für ein Luft- oder Raumfahrzeug

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee