ES2545635T3 - Célula que incluye secciones limpia y sucia para fabricar piezas de material compuesto - Google Patents

Célula que incluye secciones limpia y sucia para fabricar piezas de material compuesto Download PDF

Info

Publication number
ES2545635T3
ES2545635T3 ES12741164.3T ES12741164T ES2545635T3 ES 2545635 T3 ES2545635 T3 ES 2545635T3 ES 12741164 T ES12741164 T ES 12741164T ES 2545635 T3 ES2545635 T3 ES 2545635T3
Authority
ES
Spain
Prior art keywords
section
dirty
clean
tool
positioning system
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.)
Active
Application number
ES12741164.3T
Other languages
English (en)
Inventor
Jeffrey L. Miller
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 ES2545635T3 publication Critical patent/ES2545635T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B29C73/00Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
    • B29C73/04Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • 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
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • 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
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/0227Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using pressure vessels, e.g. autoclaves, vulcanising pans
    • 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
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49801Shaping fiber or fibered material
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49995Shaping one-piece blank by removing material
    • 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
    • Y10T29/00Metal working
    • Y10T29/51Plural diverse manufacturing apparatus including means for metal shaping or assembling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
  • Woven Fabrics (AREA)

Abstract

Un procedimiento de uso de una célula (110) de fabricación para fabricar una pieza de material compuesto, comprendiendo la célula de fabricación una sección (130) limpia para llevar a cabo operaciones limpias que incluyen la laminación de fibras de refuerzo en una herramienta mandril, cumpliendo la sección limpia con los requisitos de sala limpia para procesar materiales compuestos no curados; una sección (120) sucia adyacente para llevar a cabo operaciones sucias que incluyen mecanizar el laminado después de curar; un sistema (140) de posicionamiento del efector final común que puede moverse entre las secciones limpia y sucia; y medios (180) para impedir que los contaminantes en la sección (120) sucia entren en la sección (130) limpia; comprendiendo el procedimiento: utilizar el sistema (110) de posicionamiento del efector final para construir una herramienta mandril en la sección (120) sucia; mover la herramienta mandril y el sistema (140) de posicionamiento del efector final a la sección (130) limpia; utilizar el sistema (140) de posicionamiento del efector final para depositar fibras de refuerzo en la herramienta; mover la herramienta a una sección (190) de curado y llevar a cabo el curado; mover la herramienta mandril y el sistema de posicionamiento del efector de nuevo a la sección sucia; mecanizar la pieza curada en la herramienta.

Description

imagen1
imagen2
imagen3
imagen4
imagen5
imagen6
imagen7

Claims (1)

  1. imagen1
ES12741164.3T 2011-07-12 2012-07-11 Célula que incluye secciones limpia y sucia para fabricar piezas de material compuesto Active ES2545635T3 (es)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201161507115P 2011-07-12 2011-07-12
US201161507115P 2011-07-12
US201113267876 2011-10-06
US13/267,876 US8887367B2 (en) 2011-07-12 2011-10-06 Cell including clean and dirty sections for fabricating composite parts
PCT/US2012/046303 WO2013009909A2 (en) 2011-07-12 2012-07-11 Cell including clean and dirty sections for fabricating composite parts

Publications (1)

Publication Number Publication Date
ES2545635T3 true ES2545635T3 (es) 2015-09-14

Family

ID=46598955

Family Applications (1)

Application Number Title Priority Date Filing Date
ES12741164.3T Active ES2545635T3 (es) 2011-07-12 2012-07-11 Célula que incluye secciones limpia y sucia para fabricar piezas de material compuesto

Country Status (9)

Country Link
US (1) US8887367B2 (es)
EP (1) EP2731784B1 (es)
JP (1) JP6025840B2 (es)
KR (1) KR101874664B1 (es)
CN (1) CN103826835B (es)
BR (1) BR112014000556B1 (es)
CA (1) CA2834546C (es)
ES (1) ES2545635T3 (es)
WO (1) WO2013009909A2 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
US8728262B2 (en) * 2011-07-12 2014-05-20 The Boeing Company Rapid fabrication of a composite part
US9381659B2 (en) * 2014-04-16 2016-07-05 The Boeing Company Automated apparatus for use in selectively cutting side walls of a honeycomb core
US9545759B2 (en) 2015-01-30 2017-01-17 CGTech Automated fiber placement with course trajectory compensation
US10265890B2 (en) 2015-04-10 2019-04-23 Channell Commercial Corporation Method of manufacturing a thermoset polymer utility vault lid
US9987659B2 (en) 2015-10-19 2018-06-05 United Technologies Corporation Nanotube enhancement of interlaminar performance for a composite component
JP6776200B2 (ja) 2017-07-20 2020-10-28 三菱重工業株式会社 ファスナ及び補修構造並びに損傷検出方法
NL2027426B1 (en) * 2021-01-26 2022-08-26 Boeing Co Edge trimming for moving-line fabrication of aircraft
EP4001129A1 (en) 2020-11-18 2022-05-25 The Boeing Company Edge trimming for moving-line fabrication of aircraft
CN117429090B (zh) * 2023-12-04 2024-04-30 哈尔滨远驰航空装备有限公司 机载多腔结构及其一体成型模具、方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB211659A (en) * 1923-01-11 1924-02-28 Quicksafe Mfg Co Improvements in or relating to can openers
US4292874A (en) 1979-05-18 1981-10-06 Baldwin Piano & Organ Company Automatic control apparatus for chords and sequences
GB2116594B (en) * 1982-02-09 1985-05-30 Glyndon Products Limited Machine installations
JPH06127497A (ja) * 1992-10-20 1994-05-10 Mitsubishi Heavy Ind Ltd ロケット発射装置
US5341918A (en) 1993-04-16 1994-08-30 Covert William J Article transfer device
JPH11235782A (ja) * 1998-02-23 1999-08-31 Matsushita Electric Works Ltd 金属箔張り積層板の製造方法
JP2000024971A (ja) * 1998-07-08 2000-01-25 Komatsu Ltd ワーク搬送ロボットの教示システム
US6506009B1 (en) * 2000-03-16 2003-01-14 Applied Materials, Inc. Apparatus for storing and moving a cassette
JP3608107B2 (ja) * 2000-10-19 2005-01-05 日精樹脂工業株式会社 塵埃飛散防止手段を備えた射出成形機
JP2003017376A (ja) * 2001-07-02 2003-01-17 Sanki Eng Co Ltd 半導体製造装置および半導体製造方法
WO2003026821A1 (en) * 2001-09-25 2003-04-03 Gerhard Jack K Apparatus and method for induction lamination of electrically conductive fiber reinforced composite materials
JP2004207279A (ja) * 2002-12-20 2004-07-22 Rorze Corp 薄板状物製造設備
US7103952B2 (en) * 2004-03-12 2006-09-12 The Boeing Company Engine loader and transporter apparatus and methods
US7341086B2 (en) * 2004-10-29 2008-03-11 The Boeing Company Automated fabric layup system and method
US7472736B2 (en) 2005-02-14 2009-01-06 The Boeing Company Modular head lamination device and method
DE102005053690A1 (de) * 2005-11-10 2007-05-31 Airbus Deutschland Gmbh Werkzeug, Anordnung und Verfahren zum Herstellen eines Bauteils, Bauteil
US8691037B2 (en) * 2006-12-14 2014-04-08 The Boeing Company Method for minimizing fiber distortion during fabrication of one-piece composite barrel section
ITTO20070507A1 (it) * 2007-07-11 2009-01-12 Alenia Aeronautica Spa Procedimento di fabbricazione di una struttura d'ala monolitica a profilo integrale
US8557074B2 (en) * 2008-02-27 2013-10-15 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
DE102008044069B3 (de) * 2008-11-26 2010-08-05 Airbus Deutschland Gmbh Formkörper zur Herstellung eines Faserverbundbauteils
US8844108B2 (en) * 2011-07-12 2014-09-30 The Boeing Company Large area repair of composite aircraft

Also Published As

Publication number Publication date
WO2013009909A3 (en) 2014-02-27
EP2731784A2 (en) 2014-05-21
CA2834546A1 (en) 2013-01-17
WO2013009909A2 (en) 2013-01-17
KR101874664B1 (ko) 2018-07-04
EP2731784B1 (en) 2015-06-10
BR112014000556B1 (pt) 2022-01-04
BR112014000556A2 (pt) 2020-10-27
CN103826835A (zh) 2014-05-28
JP2014525852A (ja) 2014-10-02
US8887367B2 (en) 2014-11-18
KR20140038400A (ko) 2014-03-28
CA2834546C (en) 2016-06-14
US20130014378A1 (en) 2013-01-17
JP6025840B2 (ja) 2016-11-16
CN103826835B (zh) 2016-02-03

Similar Documents

Publication Publication Date Title
ES2545635T3 (es) Célula que incluye secciones limpia y sucia para fabricar piezas de material compuesto
WO2013022534A3 (en) Method and device for transporting, placing and compacting composite stiffeners
ES2705334R1 (es) Método para inducir un bloque candidato de fusión y dispositivo que usa el mismo
BR112014000590A2 (pt) fabricação rápida de uma peça composta
BR112014003350A2 (pt) composto laminado termoplástico, estrutura de composto, composto laminado, e, método para formar um composto laminado
WO2014149428A3 (en) Method and apparatus for reducing ply wrinkling of composite laminates during forming
CL2009001591A1 (es) Metodo para reparar y reforzar una tuberia que comprende cubrir una seccion de tuberia con un enrollamiento de material compuesto, aislar la superficie externa del ambiente, aplicar una fuerza compresiva a dicha superficie externa y permitir que se cure efectivamente.
CL2012002295A1 (es) Dispositivo y metodo para imprimir superficies de paneles de material, en especial paneles de madera, que comprende medios para retener un panel de material en una posicion alineada, una unidad de impresion para imprimir una superficie del panel de material y medios para desplazar la unidad de impresion.
MX2016011866A (es) Unidad de recoleccion de muestras.
EP2532580A3 (en) Boron fiber reinforced structural components
FR2953812B1 (fr) Procede de reparation d'un fuselage d'aeronef
JP2014525852A5 (es)
CL2014002824A1 (es) Un metodo para fabricar un sistema de tuberia reforzada para transportar un fluido, comprende enfriar una tuberia de polietileno de alta densidad, envolver una cinta de fibra sobre la superficie de la tuberia, asegurar los extremos de la cinta, calentar la cinta y la tuberia, encajar las fibras tensas, adherir la cinta a la tuberia; y sistema asociado.
ITTO20110368A1 (it) Metodo e sistema di ispezione non distruttiva ad ultrasuoni, in particolare per strutture in materiale composito per applicazioni aeronautiche
FR2961740B1 (fr) Procede de fabrication d'un article en materiau composite
WO2015181374A3 (en) Underwater pipeline repair by automated composite lamination
DE112015004623A5 (de) Lagerträger aus faser-kunststoff-verbund
FR3018473B1 (fr) Procede de fabrication d'une plate-forme d'aube en materiau composite a joints integres pour soufflante de turbomachine
MX2015012220A (es) Laminados compuestos termoplásticos de alto desempeño y estructuras compuestas producidas a partir de los mismos.
ITMO20120233A1 (it) Metodo e dispositivo di fabbricazione di un articolo in vetro provvisto di un'ansa
CL2011000601A1 (es) Estructura de un composito de madera y metal unidos entre si por un agente de acoplamiento, en donde dicha estructura comprende un material de acoplamiento que contiene un material de metal y comprende por lo menos tres capas, y por lo menos las capas exteriores del material de acoplamiento contienen un polimero.
BR112016009559A2 (pt) Processo para a produção de partículas compósitas e uso das mesmas
IL249482B (en) Tools and methods to create a composite aircraft using steering mandrels
FR3010652B1 (fr) Procede de reparation d'un panneau composite
DK3831566T3 (da) Fremgangsmåde til adskillelse af lagene i flerlagsplastmaterialer