BRPI0823282A2 - Método de formação de um artigo compósito - Google Patents

Método de formação de um artigo compósito

Info

Publication number
BRPI0823282A2
BRPI0823282A2 BRPI0823282-2A BRPI0823282A BRPI0823282A2 BR PI0823282 A2 BRPI0823282 A2 BR PI0823282A2 BR PI0823282 A BRPI0823282 A BR PI0823282A BR PI0823282 A2 BRPI0823282 A2 BR PI0823282A2
Authority
BR
Brazil
Prior art keywords
forming
composite article
article
composite
Prior art date
Application number
BRPI0823282-2A
Other languages
English (en)
Inventor
Per Hallander
Mikael Peterson
Bjorn Weidmann
Tonny Nyman
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Publication of BRPI0823282A2 publication Critical patent/BRPI0823282A2/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
    • B29C70/30—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
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24132—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in different layers or components parallel

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
BRPI0823282-2A 2008-11-13 2008-11-13 Método de formação de um artigo compósito BRPI0823282A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE2008/051304 WO2010056164A1 (en) 2008-11-13 2008-11-13 Method of forming a composite article

Publications (1)

Publication Number Publication Date
BRPI0823282A2 true BRPI0823282A2 (pt) 2015-06-16

Family

ID=42170142

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0823282-2A BRPI0823282A2 (pt) 2008-11-13 2008-11-13 Método de formação de um artigo compósito

Country Status (5)

Country Link
US (1) US20110250381A1 (pt)
EP (1) EP2349686B1 (pt)
BR (1) BRPI0823282A2 (pt)
CA (1) CA2743331A1 (pt)
WO (1) WO2010056164A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9040142B2 (en) 2010-05-11 2015-05-26 Saab Ab Composite article comprising particles and a method of forming a composite article
EP2665595A1 (en) * 2011-01-21 2013-11-27 Saab AB A composite article and a method of forming a composite article
FR2987778B1 (fr) * 2012-03-12 2014-05-02 Airbus Operations Sas Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres
EP3000586B1 (en) 2014-09-26 2019-03-20 Airbus Operations, S.L. Method for manufacturing a composite material part comprising a web and at least one flange
US10213954B2 (en) * 2016-02-19 2019-02-26 The Boeing Company Natural path forming for composite material
US10913198B2 (en) 2017-10-19 2021-02-09 The Boeing Company Pyrometer control for hot drape formers
US10913215B2 (en) * 2019-05-09 2021-02-09 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919256B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US10919260B2 (en) * 2019-05-09 2021-02-16 The Boeing Company Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US12533856B2 (en) * 2023-08-30 2026-01-27 The Boeing Company Methods and tools for forming composite structures with preferable wrinkle configurations
CN117048079B (zh) * 2023-10-08 2024-01-05 哈尔滨远驰航空装备有限公司 一种树脂基复合材料挂架的成型方法及模具
CN117087199B (zh) * 2023-10-08 2024-01-19 哈尔滨远驰航空装备有限公司 复合材料梁体、成型方法及成型模具

Family Cites Families (24)

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US5110652A (en) * 1989-12-04 1992-05-05 Corning Incorporated Shaped fiber-reinforced ceramic composite article
US5431538A (en) * 1993-07-01 1995-07-11 United Technologies Corporation Hybrid composite flexbeam for a helicopter bearingless main rotor assembly
FR2718758B1 (fr) * 1994-04-18 1996-06-14 Aerospatiale Procédé et machine pour la réalisation d'une armature pour une pièce de matière composite.
US5614305A (en) * 1995-02-08 1997-03-25 Virginia Tech Intellectual Properties, Inc. Impact and perforation resistant composite structures
US7413694B2 (en) * 1999-12-07 2008-08-19 The Boeing Company Double bag vacuum infusion process
GB2381493B (en) * 2001-10-30 2005-08-24 Trysome Ltd Composite materials
US6814916B2 (en) * 2002-08-30 2004-11-09 The Boeing Company Forming method for composites
US7243055B2 (en) * 2004-01-28 2007-07-10 The Boeing Company Composite stacking sequence optimization for multi-zoned composites
ITTO20040198A1 (it) * 2004-03-23 2004-06-23 Alenia Aeronautica Spa Procedimento per la fabbricazione di una preforma secca di rinforzo per un elemento strutturale composito di un aeromobile
US7469735B2 (en) * 2005-08-03 2008-12-30 The Boeing Corporation Composite structural element fabricating device and method
ATE492392T1 (de) * 2005-10-17 2011-01-15 Saab Ab Verfahren zur herstellung eines gekrümmten gegenstands aus verbundwerkstoff sowie durch dieses verfahren hergestellter gegenstand
ES2314581T3 (es) * 2005-12-20 2009-03-16 Saab Ab Elemento de rigidizacion y procedimiento de fabricacion de un elemento de rigidizacion.
JP4677950B2 (ja) * 2006-03-31 2011-04-27 株式会社豊田自動織機 三次元繊維構造体及び複合材並びに三次元繊維構造体の製造方法
EP1840775A1 (en) * 2006-03-31 2007-10-03 Airbus Espana, S.L. Computer-aided method of obtaining a ply model of composite component
JP5161432B2 (ja) * 2006-05-01 2013-03-13 三菱重工業株式会社 複合材料製構造部材の成形方法
GB0614087D0 (en) * 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
DE102006035939B4 (de) * 2006-07-31 2012-02-23 Eads Deutschland Gmbh Verfahren zur Herstellung von Faserverbundbauteilen und Faserverbundbauteil
ES2392187T3 (es) * 2006-11-23 2012-12-05 Siemens Aktiengesellschaft Método para fabricar un material laminado reforzado con fibra, uso de este material laminado, pala de turbina eólica y turbina eólica que comprende este material laminado
EP1932652A1 (en) * 2006-12-11 2008-06-18 Saab Ab A method and apparatus for manufacturing a curved elongated structural element
DE102007015909A1 (de) * 2007-04-02 2008-10-09 Mt Aerospace Ag Verfahren zur Herstellung faserverstärkter Hohlkörper
US8449709B2 (en) * 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
ITTO20070557A1 (it) * 2007-07-27 2009-01-28 Alenia Aeronautica Spa Procedimento di fabbricazione di un elemento curvo in materiale composito
ES2443917T3 (es) * 2007-10-09 2014-02-21 Saab Ab Procedimiento y dispositivo para conformar un material compuesto

Also Published As

Publication number Publication date
EP2349686A1 (en) 2011-08-03
EP2349686A4 (en) 2016-09-28
US20110250381A1 (en) 2011-10-13
CA2743331A1 (en) 2010-05-20
WO2010056164A1 (en) 2010-05-20
EP2349686B1 (en) 2018-08-08

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2386 DE 27-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.