BR0302957B1 - processo e dispositivos para a fabricação de componentes reforçados de fibra. - Google Patents

processo e dispositivos para a fabricação de componentes reforçados de fibra.

Info

Publication number
BR0302957B1
BR0302957B1 BRPI0302957-3A BR0302957A BR0302957B1 BR 0302957 B1 BR0302957 B1 BR 0302957B1 BR 0302957 A BR0302957 A BR 0302957A BR 0302957 B1 BR0302957 B1 BR 0302957B1
Authority
BR
Brazil
Prior art keywords
fiber
manufacture
devices
fiber reinforced
reinforced components
Prior art date
Application number
BRPI0302957-3A
Other languages
English (en)
Other versions
BR0302957A (pt
Inventor
Thomas Lippert
Hans-Wolfgang Schroeder
Franz Stadler
Stefan Utecht
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 filed Critical
Publication of BR0302957A publication Critical patent/BR0302957A/pt
Publication of BR0302957B1 publication Critical patent/BR0302957B1/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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
    • B29C70/547—Measures for feeding or distributing the matrix material in the reinforcing structure using channels or porous distribution layers incorporated in or associated with the product
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
BRPI0302957-3A 2002-01-31 2003-01-23 processo e dispositivos para a fabricação de componentes reforçados de fibra. BR0302957B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10203975A DE10203975C1 (de) 2002-01-31 2002-01-31 Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen
PCT/DE2003/000177 WO2003064143A1 (de) 2002-01-31 2003-01-23 Verfahren und vorrichtungen zur herstellung von faserverstärkten bauteilen

Publications (2)

Publication Number Publication Date
BR0302957A BR0302957A (pt) 2004-07-06
BR0302957B1 true BR0302957B1 (pt) 2012-05-15

Family

ID=7713509

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0302957-3A BR0302957B1 (pt) 2002-01-31 2003-01-23 processo e dispositivos para a fabricação de componentes reforçados de fibra.

Country Status (8)

Country Link
US (1) US7931458B2 (pt)
EP (1) EP1469986B1 (pt)
AT (1) ATE332799T1 (pt)
BR (1) BR0302957B1 (pt)
CA (1) CA2473777C (pt)
DE (2) DE10203975C1 (pt)
ES (1) ES2262978T3 (pt)
WO (1) WO2003064143A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10305544A1 (de) * 2003-02-10 2004-08-26 Tuhh-Technologie-Gmbh Mehrschichtfolie zur Herstellung von Faserverbundwerkstoffen
DE10342867B4 (de) * 2003-09-15 2008-05-29 Eurocopter Deutschland Gmbh Verfahren zur Herstellung eines wasserlöslichen Formkerns
DK176490B1 (da) * 2006-03-03 2008-05-13 Lm Glasfiber As Fremgangsmåde og polymerforsyningsindretning til brug ved vakuuminfusion
EP2160287B1 (en) 2007-06-29 2012-11-28 Lm Glasfiber A/S A method for producing a composite structure and a composite structure
FR2936735B1 (fr) * 2008-10-06 2010-10-15 Airbus France Procede de fabrication d'une piece en materiau composite avec une forme concave, notamment une section en u et dispositif pour sa mise en oeuvre.
DE102008055771C5 (de) † 2008-11-04 2018-06-14 Senvion Gmbh Rotorblattgurt
DK2295235T3 (da) * 2009-08-20 2013-07-29 Siemens Ag Fiberforstærket plaststruktur og fremgangsmåde til fremstilling af den fiberforstærkede plaststruktur
US8636252B2 (en) 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same
US8940213B2 (en) * 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
DE102010025068B4 (de) 2010-06-25 2016-07-28 Airbus Defence and Space GmbH Vorrichtung und Verfahren zur Herstellung von faserverstärkten Bauteilen
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
CN103796875B (zh) * 2011-09-14 2016-09-14 宝马股份公司 车轮的轮辋和具有该轮辋的车轮
US10226902B2 (en) 2011-12-13 2019-03-12 Low & Bonar B.V. Flow medium
US9199419B2 (en) 2012-10-31 2015-12-01 The Boeing Company System and method for facilitating fluid movement in close-molded composite parts
WO2015013012A1 (en) 2013-07-26 2015-01-29 Learjet Inc. Composite material incorporating water ingress barrier
DE102013012762B4 (de) * 2013-07-31 2017-05-04 Mt Aerospace Ag Verfahren zur Herstellung von Faserverbundgehäusen mit integrierter Isolation
DE102015005492B4 (de) 2015-04-30 2023-05-04 Airbus Defence and Space GmbH Fließhilfe für einen Infusionsaufbau sowie Infusionsaufbau und Verfahren zum Infiltrieren eines Fasermaterials
FR3047196B1 (fr) * 2016-02-02 2018-09-28 Coriolis Group Procede de realisation de preformes tridimensionnelles par formage de preformes initiales avec des voiles

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2124130B (en) * 1982-07-24 1985-11-27 Rolls Royce Vacuum moulding fibre reinforced resin
US5464337A (en) * 1991-03-27 1995-11-07 The Charles Stark Draper Laboratories Resin transfer molding system
US5904972A (en) * 1995-06-07 1999-05-18 Tpi Technology Inc. Large composite core structures formed by vacuum assisted resin transfer molding
US5576030A (en) * 1995-10-02 1996-11-19 Lockheed Corporation Apparatus for fabricating composite parts
US6818159B2 (en) * 2000-03-17 2004-11-16 Deutsches Zentrum Fuer Luft-Und Raumfahrt E.V. Process for the production of a composite consisting of a fiber reinforced material
DE10013409C1 (de) 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US6630095B2 (en) * 2001-08-01 2003-10-07 Lockheed Martin Corporation Method for making composite structures

Also Published As

Publication number Publication date
BR0302957A (pt) 2004-07-06
WO2003064143B1 (de) 2003-09-25
CA2473777A1 (en) 2003-08-07
DE10203975C1 (de) 2003-01-23
US20050031720A1 (en) 2005-02-10
EP1469986A1 (de) 2004-10-27
DE50304213D1 (de) 2006-08-24
ATE332799T1 (de) 2006-08-15
CA2473777C (en) 2010-07-27
ES2262978T3 (es) 2006-12-01
WO2003064143A1 (de) 2003-08-07
EP1469986B1 (de) 2006-07-12
US7931458B2 (en) 2011-04-26

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 23/01/2003, OBSERVADAS AS CONDICOES LEGAIS.

B25D Requested change of name of applicant approved
B25G Requested change of headquarter approved