BRPI0821382A2 - método para reforço de um componente de fibra composto e uma parte de vácuo e disposição para produção de um componente composto de fibra reforçada - Google Patents

método para reforço de um componente de fibra composto e uma parte de vácuo e disposição para produção de um componente composto de fibra reforçada

Info

Publication number
BRPI0821382A2
BRPI0821382A2 BRPI0821382A BRPI0821382A BRPI0821382A2 BR PI0821382 A2 BRPI0821382 A2 BR PI0821382A2 BR PI0821382 A BRPI0821382 A BR PI0821382A BR PI0821382 A BRPI0821382 A BR PI0821382A BR PI0821382 A2 BRPI0821382 A2 BR PI0821382A2
Authority
BR
Brazil
Prior art keywords
composite fiber
component
reinforcing
disposing
producing
Prior art date
Application number
BRPI0821382A
Other languages
English (en)
Inventor
Luebbering Christian
Lengsfeld Hauke
Brandenburg Roland
Original Assignee
Airbus Operations Gmbh
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 Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0821382A2 publication Critical patent/BRPI0821382A2/pt

Links

Classifications

    • 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
    • B29C70/443—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 and impregnating by vacuum or injection
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/40—Plastics, e.g. foam or rubber
    • B29C33/405—Elastomers, e.g. rubber
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/46—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles using fluid 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • 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
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
    • B29K2707/04—Carbon

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Nonwoven Fabrics (AREA)
  • Laminated Bodies (AREA)
BRPI0821382A 2007-12-20 2008-11-17 método para reforço de um componente de fibra composto e uma parte de vácuo e disposição para produção de um componente composto de fibra reforçada BRPI0821382A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US840107P 2007-12-20 2007-12-20
DE102007061431A DE102007061431B4 (de) 2007-12-20 2007-12-20 Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils
PCT/EP2008/065699 WO2009080410A1 (de) 2007-12-20 2008-11-17 Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteils

Publications (1)

Publication Number Publication Date
BRPI0821382A2 true BRPI0821382A2 (pt) 2017-05-23

Family

ID=40689613

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821382A BRPI0821382A2 (pt) 2007-12-20 2008-11-17 método para reforço de um componente de fibra composto e uma parte de vácuo e disposição para produção de um componente composto de fibra reforçada

Country Status (10)

Country Link
US (2) US8137499B2 (pt)
EP (1) EP2219853B1 (pt)
JP (1) JP2011506149A (pt)
CN (1) CN101932433B (pt)
AT (1) ATE553911T1 (pt)
BR (1) BRPI0821382A2 (pt)
CA (1) CA2707932A1 (pt)
DE (1) DE102007061431B4 (pt)
RU (1) RU2480336C2 (pt)
WO (1) WO2009080410A1 (pt)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007061431B4 (de) 2007-12-20 2013-08-08 Airbus Operations Gmbh Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils
DE102007062872A1 (de) * 2007-12-28 2009-07-09 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Profils aus Faserverbundwerkstoff
DE102009001075A1 (de) * 2009-02-23 2010-09-09 Airbus Deutschland Gmbh Verfahren zum zumindest teilweise Nachbearbeiten oder Ersetzen eines Versteifungselementes einer Faserverbundstruktur und zugehörige Anbindvorrichtung
DE102009029575B4 (de) 2009-09-18 2011-06-22 Airbus Operations GmbH, 21129 Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils
DE102009059720B4 (de) * 2009-12-18 2012-04-12 Airbus Operations Gmbh Vorrichtung zur Herstellung einer aus Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug
DE102010062871A1 (de) * 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Infusionsverfahren und Aufbau eines Infusionsverfahrens
DE102011015014A1 (de) * 2010-11-10 2012-05-10 Waldemar Piekenbrink GFK - Modell- und Formenbau, Produktions- und Vertriebs GmbH Vakuumhauben-Vorrichtung
DE102011006047B4 (de) 2011-03-24 2014-01-23 Airbus Operations Gmbh Verfahren sowie Vorrichtung zum Herstellen eines Faserverbundbauteils
DE102011014999A1 (de) * 2011-03-25 2012-09-27 Waldemar Piekenbrink GFK - Modell- und Formenbau, Produktions- und Vertriebs GmbH Beheizbare Vakuumhauben-Vorrichtung
US9969131B2 (en) * 2011-06-22 2018-05-15 The Boeing Company Automated ply layup system
US8985174B2 (en) * 2011-08-26 2015-03-24 The Boeing Company Integrally stiffened, reusable vacuum bag and method of making the same
DE102011114206A1 (de) 2011-09-23 2013-03-28 Daimler Ag Handhabungssystem und Handhabungsverfahren für Faseranordnungen
ES2626352T3 (es) * 2013-05-30 2017-07-24 Airbus Operations S.L. Herramienta híbrida para curar piezas de material compuesto
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
JP6170347B2 (ja) * 2013-06-07 2017-07-26 三菱航空機株式会社 繊維強化プラスチック構造体の製造方法および金型
JP6220162B2 (ja) * 2013-06-07 2017-10-25 三菱航空機株式会社 繊維強化プラスチック構造体の製造装置および製造方法
EP2871045A1 (en) * 2013-11-06 2015-05-13 Airbus Operations GmbH Arrangement and method for producing a composite material component
DE102015211671A1 (de) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren und Vorrichtung zur Herstellung eines Bauteils unter Verwendung einer Vakuumfolie
JP6563284B2 (ja) * 2015-09-11 2019-08-21 三菱重工業株式会社 繊維強化プラスチック成型品の製造装置及びその製造方法
CN106696304A (zh) * 2016-11-23 2017-05-24 安徽佳力奇碳纤维科技股份公司 一种碳纤维复合材料抽真空装置及其抽真空的方法
RU2675563C1 (ru) * 2017-11-30 2018-12-19 Федеральное государственное бюджетное образовательное учреждение высшего образования "Саратовский государственный технический университет имени Гагарина Ю.А." (СГТУ имени Гагарина Ю.А.) Способ изготовления армированной волокном термопластичной композитной структуры с воздействием ультразвука и СВЧ электромагнитного поля
JP7114266B2 (ja) * 2018-02-13 2022-08-08 三菱重工業株式会社 複合材料の製造方法および繊維基材
FR3092785B1 (fr) * 2019-02-19 2021-03-12 Airbus Operations Sas procédé de formage d’un film d’ensachage sous vide comprenant la formation de nervures par flambage du film
US11701801B2 (en) * 2019-03-04 2023-07-18 The Boeing Company Caul plate with feature for separating from composite part
DE102019114710A1 (de) * 2019-05-31 2020-12-03 Airbus Operations Gmbh Vorrichtung und Verfahren
US20230100087A1 (en) * 2020-06-17 2023-03-30 Mitsubishi Heavy Industries, Ltd. Jig and composite material processing method
US11840361B1 (en) 2022-08-15 2023-12-12 The Boeing Company Magnetic handling systems for hat stringers and related methods

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3145698A1 (de) 1981-11-19 1983-05-26 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zum fertigen von bauteilen aus faserverstaerkten werkstoffen
US4451321A (en) * 1983-02-16 1984-05-29 Shatterproof Glass Corporation Flexible vacuum bag
US4822651A (en) * 1985-08-30 1989-04-18 Newsom Cosby M Vacuum diaphragm device
DE3605256C1 (de) * 1986-02-19 1991-03-28 Dornier Gmbh Verfahren zur Herstellung von ebenen oder schalenfoermig gekruemmten Bauteilen aus faserverstaerkten Kunststoffen
US5217669A (en) 1987-09-08 1993-06-08 United Technologies Corporation Method for forming complex composite articles
DE3739753A1 (de) * 1987-11-24 1989-06-08 Dornier Gmbh Verfahren zum herstellen von bauteilen aus faserverstaerkten kunststoffen
JPH0517211Y2 (pt) * 1987-12-21 1993-05-10
JP2647530B2 (ja) * 1990-03-20 1997-08-27 三菱重工業株式会社 複合材一体成形用形状保持装置
CA2056224A1 (en) * 1990-12-19 1992-06-20 Terry Martin Boustead Conformal composite molding
JP3193064B2 (ja) * 1991-04-22 2001-07-30 富士重工業株式会社 複合材料の一体成形方法
JP2666878B2 (ja) * 1992-12-28 1997-10-22 株式会社パイロット 焼結体製造における成形方法及び焼結体
US5709893A (en) * 1995-06-06 1998-01-20 The Boeing Company Breathable tooling for forming parts from volatile-emitting composite materials
US5716488A (en) * 1996-08-26 1998-02-10 The Boeing Company Reusable vacuum bag for making laminated articles
JPH10146898A (ja) * 1996-11-15 1998-06-02 Honda Motor Co Ltd 繊維強化複合材の成形方法
DE10013409C1 (de) * 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US6551091B1 (en) * 2000-09-14 2003-04-22 The Boeing Company Flexible inflatable support structure for use with a reusable compaction bag
JP4713780B2 (ja) * 2001-07-27 2011-06-29 富士重工業株式会社 補強パネルの製造方法
US7147818B1 (en) * 2002-05-16 2006-12-12 The United States Of America As Represented By The Secretary Of The Army Process and apparatus for improved composite fiber volume fraction and dimensional stability by removal of accumulated excess resin using the vacuum assisted resin transfer molding (VARTM) process
US6851945B2 (en) * 2002-12-11 2005-02-08 Northrop Grumman Corporation Seal-less reusable vacuum bag
CN101351327B (zh) * 2005-12-29 2013-01-16 空中客车西班牙运营有限责任公司 具有嵌入的预固化模具的复合结构的制造工艺
CA2635651C (en) * 2005-12-30 2012-05-29 Airbus Espana, S.L. Method for producing panels of composite materials with u-shaped stiffening elements
DE102007061431B4 (de) 2007-12-20 2013-08-08 Airbus Operations Gmbh Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils

Also Published As

Publication number Publication date
DE102007061431B4 (de) 2013-08-08
EP2219853A1 (de) 2010-08-25
ATE553911T1 (de) 2012-05-15
WO2009080410A1 (de) 2009-07-02
US20100314042A1 (en) 2010-12-16
CN101932433B (zh) 2014-04-16
CA2707932A1 (en) 2009-07-02
DE102007061431A1 (de) 2009-06-25
CN101932433A (zh) 2010-12-29
EP2219853B1 (de) 2012-04-18
US8137499B2 (en) 2012-03-20
JP2011506149A (ja) 2011-03-03
US20120152461A1 (en) 2012-06-21
RU2010122661A (ru) 2012-01-27
RU2480336C2 (ru) 2013-04-27

Similar Documents

Publication Publication Date Title
BRPI0821382A2 (pt) método para reforço de um componente de fibra composto e uma parte de vácuo e disposição para produção de um componente composto de fibra reforçada
WO2010039547A3 (en) Reinforced internal composite structures
BR112014015544A2 (pt) Pré-impregnado, método de processamento de pré-impregnado e material compósito reforçado por fibra
BR112014017646A8 (pt) Pré-impregnado, métodos para produzir um pré-impregnado, e de fabricação de um membro estrutural de material compósito reforçado com fibra, e, uso de um pré-impregnado
BR112013024886A2 (pt) pré-impregnado, material compósito reforçado com fibra e método para fabricação de um material compósito reforçado com fibra
WO2011151710A3 (en) Structure of fiber-reinforced composite material-made component part, and production method for the component part
GB2447964B (en) Moulding material
BR112016030776A8 (pt) pré-forma, e, métodos para fabricação de uma estrutura compósita e para fabricação de fitas fibrosas secas para deposição de fitas automatizada
BRPI0909269A2 (pt) Pré-impregnado para fabricar um material compósito reforçado com fibra, método para fabricar um membro estrutural alongado de material compósito reforçado com fibra, e, uso de um pré-impregnado
WO2011116030A3 (en) Recycled composite materials and related methods
PL2121264T3 (pl) Trzpień łopaty helikoptera, sposób wykonania trzpienia oraz sposób formowania łopaty wirnika helikoptera
WO2010083840A3 (en) Method of manufacturing a wind turbine blade by embedding a layer of pre-cured fibre reinforced resin
WO2013022534A3 (en) Method and device for transporting, placing and compacting composite stiffeners
FR2898539B1 (fr) Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises
WO2012064443A3 (en) Methods and systems for forming integral composite parts with a smp apparatus
EP2662202A3 (en) A method for the manufacture of a fibre composite component, a supporting core, and also a fibre composite component
BR112013020426A2 (pt) processo e sistema para fabricação de produtos de material compósito, assim como produtos fabricados com este processo ou sistema
ATE554913T1 (de) Verfahren zur herstellung von mehreren faserverbundbauteilen
ATE492247T1 (de) Verfahren zur herstellung einer orthese
IN2015DN02281A (pt)
IN2013CN00729A (pt)
WO2013093053A3 (en) Improvements in or relating to fibre reinforced materials
ATE483918T1 (de) Konstruktionsvorrichtung zur verbesserung der stabilität einer struktur hinsichtlich temperaturbedingter ausdehnungen
ATE477914T1 (de) Vakuumiervorgang zur verwendung bei einem verfahren zur herstellung einer verbundstruktur
BRPI0816672A2 (pt) Processo para a fabricação de um componente de compósito de fibras.

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]