ES2163525T3 - Maquina para montar un larguero de material compuesto. - Google Patents

Maquina para montar un larguero de material compuesto.

Info

Publication number
ES2163525T3
ES2163525T3 ES95930210T ES95930210T ES2163525T3 ES 2163525 T3 ES2163525 T3 ES 2163525T3 ES 95930210 T ES95930210 T ES 95930210T ES 95930210 T ES95930210 T ES 95930210T ES 2163525 T3 ES2163525 T3 ES 2163525T3
Authority
ES
Spain
Prior art keywords
loads
machine
mandrels
mandriles
platform
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
ES95930210T
Other languages
English (en)
Inventor
Donald A Jensen
Joel L Morphis
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2163525T3 publication Critical patent/ES2163525T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • 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
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/004—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore making articles by joining parts moulded in separate cavities, said parts being in said separate cavities during said joining
    • 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
    • B29C70/345—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 matched moulds

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Automatic Assembly (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)

Abstract

SE PRESENTA UNA MAQUINA (34) PARA SU USO EN EL MONTAJE DE UN LARGUERO (32) A PARTIR DE DOS CARGAS EN FORMA DE C (22), CADA CARGA DE CANAL SE ENCUENTRA REVESTIDA ALREDEDOR DE UN MANDRIL (20). LA MAQUINA INCLUYE UNA ARMADURA (36) QUE TIENE UNA PRIMERA PLATAFORMA (40) PARA SOPORTAR LOS MANDRILES Y LAS CARGAS EN FORMA DE C DE FORMA QUE LAS CARGAS EN FORMA DE C ESTEN ESPALDA CONTRA ESPALDA. UN YUNQUE EN FORMA DE U (48) CONECTADO A LA ARMADURA, PUEDE GIRAR ENTRE UNA POSICION DE AJUSTE QUE SE SUPERPONE A LOS MANDRILES Y A LAS CARGAS EN FORMA DE C Y UNA POSICION DESAJUSTADA ALEJADA DE LOS MANDRILES Y DE LAS CARGAS EN FORMA DE C. EL YUNQUE (48) INCLUYE UNA VEJIGA LATERAL (58) PARA COMPACTAR LAS CARGAS EN FORMA DE C UNA CONTRA LA OTRA PRESIONANDO LOS MANDRILES Y LAS CARGAS EN FORMA DE C ENTRE SI Y CONTRA UNA PARED DEL YUNQUE OPUESTA A LA VEJIGA LATERAL, Y UNA VEJIGA SUPERIOR (62) PARA ALINEAR LOS MANDRILES Y LAS CARGAS EN FORMA DE C COMPRIMIENDO LOS MANDRILES Y LAS CARGAS EN FORMA DE C CONTRA LA PLATAFORMA. LA MAQUINA INCLUYE ADEMAS UN MECANISMO DE ROTACION PARA MOVER LOS MANDRILES Y LAS CARGAS EN FORMA DE C DESDE LA PRIMERA PLATAFORMA A UNA SEGUNDA PLATAFORMA PARA GIRAR LOS MANDRILES Y LAS CARGAS EN FORMA DE C A TRAVES DE 180 (GRADOS) A MEDIDA QUE SE MUEVEN PARA INVERTIR LOS MANDRILES Y LAS CARGAS EN FORMA DE C REVESTIDAS SOBRE LOS MANDRILES. TAMBIEN SE INCLUYEN CON LA MAQUINA DISPOSITIVOS DE ALINEAMIENTO (42) PARA ALINEAR LOS EXTREMOS DE LOS MANDRILES Y DE LAS CARGAS EN FORMA DE C ENTRE SI.
ES95930210T 1994-08-31 1995-08-17 Maquina para montar un larguero de material compuesto. Expired - Lifetime ES2163525T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/299,925 US5538589A (en) 1994-08-31 1994-08-31 Composite stringer assembly machine

Publications (1)

Publication Number Publication Date
ES2163525T3 true ES2163525T3 (es) 2002-02-01

Family

ID=23156888

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95930210T Expired - Lifetime ES2163525T3 (es) 1994-08-31 1995-08-17 Maquina para montar un larguero de material compuesto.

Country Status (7)

Country Link
US (1) US5538589A (es)
EP (1) EP0777571B1 (es)
JP (1) JP3811739B2 (es)
AU (1) AU3367595A (es)
DE (1) DE69524106T2 (es)
ES (1) ES2163525T3 (es)
WO (1) WO1996006726A1 (es)

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US6470942B1 (en) * 2000-10-12 2002-10-29 Thermwood Corporation Pneumatic clamping apparatus and method thereof
JP3782072B2 (ja) * 2003-05-30 2006-06-07 川崎重工業株式会社 複合材型材の成形方法及び装置
US7249943B2 (en) 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
FR2863198B1 (fr) * 2003-12-04 2006-03-03 Airbus France Panneaux auto-raidis en composite pre-impregne et procedes de mise en place des elements de tels panneaux
FR2863197B1 (fr) * 2003-12-04 2006-03-03 Airbus France Procede de mise en place des elements d'un panneau auto-raidi en composite preimpregne
US7293737B2 (en) 2004-04-20 2007-11-13 The Boeing Company Co-cured stringers and associated mandrel and fabrication method
ITTO20040410A1 (it) * 2004-06-21 2004-09-21 Alenia Aeronautica Spa Procedimento per la fabbricazione di travi strutturali in composito per aeromobili.
US7588655B2 (en) * 2004-11-24 2009-09-15 The Boeing Company Mandrel with differential in thermal expansion to eliminate wrinkles in ply
US7357166B2 (en) 2004-11-24 2008-04-15 The Boeing Company Flexible mandrel for highly contoured composite stringer
US8632653B2 (en) * 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
GB0614087D0 (en) * 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
US7644491B2 (en) * 2006-10-17 2010-01-12 The Boeing Company Device for assembling composite structure incorporating flipper assemblies
US7788784B2 (en) * 2006-10-17 2010-09-07 The Boeing Company Method of assembling composite structure
US7694412B2 (en) * 2006-10-17 2010-04-13 The Boeing Company Moving a pair of mandrel cradles
US7814644B2 (en) 2006-10-17 2010-10-19 The Boeing Company Positioning assembly for composite structure
US7588711B2 (en) 2006-11-21 2009-09-15 The Boeing Company Method for forming a composite support beam
DE102007015518A1 (de) 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung von Profilteilen
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
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
US7754045B2 (en) 2007-11-14 2010-07-13 The Boeing Company Method and tools for fabricating composite beams
FR2927013B1 (fr) * 2008-01-31 2010-02-19 Airbus France Dispositif pour la fabrication d'une piece en materiau composite comprenant des toles de lissage a jonctions glissantes et procede de fabrication de toles de lissage a jonctions glissantes
WO2009097514A1 (en) * 2008-01-31 2009-08-06 Alliant Techsystems Inc. A stiffener tool positioning apparatus
US9090028B2 (en) * 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9238335B2 (en) * 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
GB0813161D0 (en) 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
GB0813146D0 (en) * 2008-07-18 2008-08-27 Airbus Uk Ltd Ramped stiffener and apparatus and method for forming the same
GB0813785D0 (en) * 2008-07-29 2008-09-03 Airbus Uk Ltd Method of manufacturing a composite element
US8312906B2 (en) * 2008-08-13 2012-11-20 Airbus Operations Gmbh Method and device for positioning stringers on an aircraft skin, in particular on a wing skin
US8815038B2 (en) 2008-10-01 2014-08-26 The Boeing Company Joining curved composite sandwich panels
US8834667B2 (en) * 2010-10-19 2014-09-16 The Boeing Company Method for joining sandwich truss core panels and composite structures produced therefrom
US8293051B2 (en) 2008-12-10 2012-10-23 The Boeing Company Method for producing composite laminates using a collapsible mandrel
US9296187B2 (en) 2008-12-10 2016-03-29 The Boeing Company Bagging process and mandrel for fabrication of elongated composite structure
US9662841B2 (en) 2009-11-10 2017-05-30 Orbital Atk, Inc. Radially extending composite structures
US8282757B2 (en) 2009-11-10 2012-10-09 Alliant Techsystems Inc. Automated composite annular structure forming
US8430984B2 (en) 2010-05-11 2013-04-30 The Boeing Company Collapsible mandrel employing reinforced fluoroelastomeric bladder
US8597015B2 (en) * 2010-12-15 2013-12-03 The Boeing Company Airfoil manufacturing system
US8776375B2 (en) * 2011-05-19 2014-07-15 The Boeing Company Aircraft structure for high capacity pull off
US8997642B2 (en) * 2011-08-08 2015-04-07 The Boeing Company Method for transporting, placing and compacting composite stiffeners
US9931807B2 (en) 2011-08-08 2018-04-03 The Boeing Company Flexible compactor with reinforcing spine
US8440045B2 (en) * 2011-09-14 2013-05-14 Sikorsky Aircraft Corporation Conformal deltoid noodle for a composite structure
DE102011056978A1 (de) * 2011-12-23 2013-06-27 Rehau Ag + Co Verfahren zur Herstellung eines Bauteils aus einem faserverstärkten Kunststoff¬material unter Verwendung eines Formwerkzeugs zum Formpressen und Formwerkzeug
ES2413189B1 (es) * 2012-01-10 2015-02-11 Manuel Torres Martínez Instalacion para fabricar larguerillos de fibra para estructuras aeroespaciales
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
US9409348B2 (en) 2013-02-04 2016-08-09 The Boeing Company Fabrication of stiffened composite panels
US9272767B2 (en) 2013-04-19 2016-03-01 The Boeing Company Compacting uncured composite members on contoured mandrel surfaces
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
EP2868464B1 (en) 2013-10-30 2019-03-13 Airbus Operations GmbH System and method of manufacturing composite modules
US9751256B2 (en) * 2014-01-20 2017-09-05 Lockheed Martin Corporation Joint molding apparatus
US9511520B1 (en) 2014-08-20 2016-12-06 The Boeing Company Method, apparatus and device for preventing vacuum bag wrinkling
US9701070B2 (en) 2014-11-06 2017-07-11 Lockheed Martin Corporation Mandrel forming for discrete wing skin stiffeners
ES2817003T3 (es) * 2015-04-10 2021-04-06 Leonardo Spa Procedimiento de fabricación de paneles reforzados de material compuesto mediante curado conjunto
GB201507519D0 (en) * 2015-05-01 2015-06-17 Vestas Wind Sys As Reinforcing Structure for a Wind Turbine Blade
US9713901B2 (en) * 2015-05-27 2017-07-25 The Boeing Company Method to reduce residual stress in an integrally-stiffened co-bonded structure
US10035300B2 (en) * 2015-06-23 2018-07-31 The Boeing Company System and method for manufacturing a stiffened composite structure
US10780655B2 (en) * 2015-10-28 2020-09-22 The Boeing Company Rotational tooling apparatus for layup and cure of composite stringers
DE102016125959A1 (de) * 2016-12-30 2018-07-05 Airbus Operations Gmbh Membranwerkzeug zum Umformen von Verstärkungsfaserlagen zu vorumgeformten T-förmigen Profilen
US11104113B2 (en) * 2017-04-19 2021-08-31 The Boeing Company Systems and methods for assembling elongate composite structures
GB2575102A (en) * 2018-06-29 2020-01-01 Airbus Operations Ltd Duct stringer with bulkhead

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US4816106A (en) * 1984-12-13 1989-03-28 Aeritalia Saipa - Gruppo Velivoli Da Trasporto Method for the controlled curing of composites
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Also Published As

Publication number Publication date
JP3811739B2 (ja) 2006-08-23
US5538589A (en) 1996-07-23
JPH10505016A (ja) 1998-05-19
EP0777571B1 (en) 2001-11-21
AU3367595A (en) 1996-03-22
EP0777571A1 (en) 1997-06-11
DE69524106T2 (de) 2002-04-11
WO1996006726A1 (en) 1996-03-07
DE69524106D1 (de) 2002-01-03

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