FR2942165B1 - Procede de fabrication d'un panneau raidi en materiau composite - Google Patents

Procede de fabrication d'un panneau raidi en materiau composite

Info

Publication number
FR2942165B1
FR2942165B1 FR0950973A FR0950973A FR2942165B1 FR 2942165 B1 FR2942165 B1 FR 2942165B1 FR 0950973 A FR0950973 A FR 0950973A FR 0950973 A FR0950973 A FR 0950973A FR 2942165 B1 FR2942165 B1 FR 2942165B1
Authority
FR
France
Prior art keywords
raidi
panel
manufacturing
composite material
composite
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
FR0950973A
Other languages
English (en)
Other versions
FR2942165A1 (fr
Inventor
Philippe Blot
Dominique Guittard
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
Priority to FR0950973A priority Critical patent/FR2942165B1/fr
Priority to PCT/FR2010/050254 priority patent/WO2010092309A1/fr
Publication of FR2942165A1 publication Critical patent/FR2942165A1/fr
Application granted granted Critical
Publication of FR2942165B1 publication Critical patent/FR2942165B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0027—Cutting off
    • 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
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
    • 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
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/243—Partially cured
FR0950973A 2009-02-16 2009-02-16 Procede de fabrication d'un panneau raidi en materiau composite Active FR2942165B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0950973A FR2942165B1 (fr) 2009-02-16 2009-02-16 Procede de fabrication d'un panneau raidi en materiau composite
PCT/FR2010/050254 WO2010092309A1 (fr) 2009-02-16 2010-02-15 Procede de fabrication d'un panneau raidi en materiau composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0950973A FR2942165B1 (fr) 2009-02-16 2009-02-16 Procede de fabrication d'un panneau raidi en materiau composite

Publications (2)

Publication Number Publication Date
FR2942165A1 FR2942165A1 (fr) 2010-08-20
FR2942165B1 true FR2942165B1 (fr) 2016-01-29

Family

ID=41226219

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0950973A Active FR2942165B1 (fr) 2009-02-16 2009-02-16 Procede de fabrication d'un panneau raidi en materiau composite

Country Status (2)

Country Link
FR (1) FR2942165B1 (fr)
WO (1) WO2010092309A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2991228B1 (fr) * 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
FR2999970B1 (fr) 2012-12-20 2015-06-19 Airbus Operations Sas Procede de realisation d'une preforme textile a fibres continues par circulation d'un flux de gaz chaud a travers un ensemble fibreux
EP3007969B1 (fr) * 2013-06-10 2020-01-01 Saab Ab Procédéde fabrication de peau composite renforcée par des lisses et dispositif
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3014841B1 (fr) 2013-12-17 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage
FR3015431B1 (fr) 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
FR3116755A1 (fr) 2020-11-30 2022-06-03 Airbus Operations (S.A.S.) Procédé de fabrication d’un panneau raidi comprenant des renforts avec des extrémités biseautées et panneau raidi obtenu à partir dudit procédé
FR3130189B1 (fr) 2021-12-14 2024-04-12 Airbus Operations Sas Dispositif de fabrication d’un panneau raidi permettant de maîtriser la géométrie dudit panneau raidi et procédé de fabrication d’un panneau raidi utilisant ledit dispositif

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2440831A1 (fr) * 1978-11-07 1980-06-06 Dassault Avions Panneaux a base de fibres a haute resistance, particulierement applicables a la construction des avions
US4492607A (en) * 1983-02-22 1985-01-08 Rockwell International Corporation Method for producing integrally stiffened fiber reinforced plastic panels
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
FR2863197B1 (fr) 2003-12-04 2006-03-03 Airbus France Procede de mise en place des elements d'un panneau auto-raidi en composite preimpregne
ATE463335T1 (de) * 2005-12-20 2010-04-15 Saab Ab Verfahren zur herstellung eines zum versteifen eines schalenstrukturs konfigurierten länglichen strukturelementes und verfahren zur herstellung eines steifen schalenstrukturs mit wenigstens einem integrierten länglichen versteifungselement

Also Published As

Publication number Publication date
WO2010092309A1 (fr) 2010-08-19
FR2942165A1 (fr) 2010-08-20

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Legal Events

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CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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