DE60100919D1 - Verfahren zur Herstellung einer mit Versteifungsrippen versehenen Platte aus Verbundwerkstoff und mit diesem Verfahren hergestellte Platte - Google Patents

Verfahren zur Herstellung einer mit Versteifungsrippen versehenen Platte aus Verbundwerkstoff und mit diesem Verfahren hergestellte Platte

Info

Publication number
DE60100919D1
DE60100919D1 DE60100919T DE60100919T DE60100919D1 DE 60100919 D1 DE60100919 D1 DE 60100919D1 DE 60100919 T DE60100919 T DE 60100919T DE 60100919 T DE60100919 T DE 60100919T DE 60100919 D1 DE60100919 D1 DE 60100919D1
Authority
DE
Germany
Prior art keywords
panel
bladder
bands
fold
mold
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
DE60100919T
Other languages
English (en)
Other versions
DE60100919T2 (de
Inventor
Michel Buge
Eric Rambaud
Alain Porte
Bruno Legeay
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 SAS filed Critical Airbus Operations SAS
Publication of DE60100919D1 publication Critical patent/DE60100919D1/de
Application granted granted Critical
Publication of DE60100919T2 publication Critical patent/DE60100919T2/de
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
    • B29D99/001—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
    • 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
    • B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0067—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other
    • B29C37/0075—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other using release sheets
    • 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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
DE60100919T 2000-05-05 2001-05-03 Verfahren zur Herstellung einer mit Versteifungsrippen versehenen Platte aus Verbundwerkstoff und mit diesem Verfahren hergestellte Platte Expired - Lifetime DE60100919T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0005798A FR2808472B1 (fr) 2000-05-05 2000-05-05 Procede de fabrication d'un panneau en materiau composite a bandes raidisseurs et panneau ainsi obtenu
FR0005798 2000-05-05

Publications (2)

Publication Number Publication Date
DE60100919D1 true DE60100919D1 (de) 2003-11-13
DE60100919T2 DE60100919T2 (de) 2004-08-19

Family

ID=8849955

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60100919T Expired - Lifetime DE60100919T2 (de) 2000-05-05 2001-05-03 Verfahren zur Herstellung einer mit Versteifungsrippen versehenen Platte aus Verbundwerkstoff und mit diesem Verfahren hergestellte Platte

Country Status (7)

Country Link
US (2) US6746642B2 (de)
EP (1) EP1151856B1 (de)
AT (1) ATE251546T1 (de)
CA (1) CA2346311C (de)
DE (1) DE60100919T2 (de)
ES (1) ES2208535T3 (de)
FR (1) FR2808472B1 (de)

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US20060198962A1 (en) * 2005-03-02 2006-09-07 Efim Kravetz Method for producing extremely durable photographs and printed matter
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US7943076B1 (en) * 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
WO2007113344A1 (es) * 2006-03-31 2007-10-11 Airbus España, S.L. Procedimiento de fabricacion de estructuras de material compuesto con un utillaje colapsable de material inerte
EP2006076B1 (de) * 2006-03-31 2015-11-18 Airbus Operations S.L. Verfahren zur herstellung von verbundmaterialstrukturen mit zusammenklappbaren werkzeugen
BRPI0721694A2 (pt) * 2007-05-28 2013-02-13 Airbus Operations Sl procedimento e ferramenta para a fabricaÇço de estruturas reforÇadas a partir de materiais compostos
US8337163B2 (en) * 2007-12-05 2012-12-25 General Electric Company Fiber composite half-product with integrated elements, manufacturing method therefor and use thereof
FR2928295B1 (fr) * 2008-03-07 2017-12-08 Duqueine Rhone Alpes Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante.
FR2928577B1 (fr) * 2008-03-14 2011-11-25 Airbus France Procede de realisation d'un raidisseur evide en forme de omega et noyau pour la realisation d'un raidisseur evide en forme de omega
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
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
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
FR2933379B1 (fr) * 2008-07-07 2010-08-20 Aerazur Procede d'assemblage d'un tapis de degivrage et d'un blindage metallique sur une structure
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
DE102009060693A1 (de) * 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement
US20130115429A1 (en) 2010-07-13 2013-05-09 Learjet Composite structure and method of forming same
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
DE102013218520A1 (de) * 2013-09-16 2015-03-19 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils, Faserverbundbauteil, sowie Strukturbauteil für ein Luft- oder Raumfahrzeug
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9656761B2 (en) 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
US9708072B2 (en) 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same
US9604438B2 (en) 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
WO2017055685A1 (en) * 2015-09-28 2017-04-06 Tactotek Oy Method and arrangement for providing electrical connection to in-mold electronics
FR3043935B1 (fr) * 2015-11-20 2018-02-23 Geco Ingenierie Procede et dispositif de moulage d'une piece composite, piece composite et embarcation
DE102015225467B4 (de) * 2015-12-16 2019-12-19 Airbus Defence and Space GmbH Beschichtetes Verbundbauteil und Verfahren zum Herstellen eines beschichteten Verbundbauteils
CN105711109B (zh) * 2016-03-23 2018-01-09 江苏恒神股份有限公司 一种采用双真空袋整体成型复合材料帽型加筋壁板的成型工艺
US10793282B2 (en) 2016-07-28 2020-10-06 The Boeing Company Liner assembly, engine housing, and methods of assembling the same

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US3608052A (en) * 1970-02-12 1971-09-21 Texaco Inc Method for fabricating fiber reinforced articles
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US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel

Also Published As

Publication number Publication date
US7790082B2 (en) 2010-09-07
EP1151856A1 (de) 2001-11-07
US6746642B2 (en) 2004-06-08
DE60100919T2 (de) 2004-08-19
FR2808472B1 (fr) 2003-02-28
ATE251546T1 (de) 2003-10-15
CA2346311C (fr) 2009-11-24
ES2208535T3 (es) 2004-06-16
FR2808472A1 (fr) 2001-11-09
CA2346311A1 (fr) 2001-11-05
EP1151856B1 (de) 2003-10-08
US20040227276A1 (en) 2004-11-18
US20010038170A1 (en) 2001-11-08

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