FR2988324B1 - Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede - Google Patents
Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procedeInfo
- Publication number
- FR2988324B1 FR2988324B1 FR1252662A FR1252662A FR2988324B1 FR 2988324 B1 FR2988324 B1 FR 2988324B1 FR 1252662 A FR1252662 A FR 1252662A FR 1252662 A FR1252662 A FR 1252662A FR 2988324 B1 FR2988324 B1 FR 2988324B1
- Authority
- FR
- France
- Prior art keywords
- frame
- section
- manufacturing
- strip
- face
- 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 - Fee Related
Links
Classifications
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- 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
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/02—Bending or folding
- B29C53/08—Bending or folding of tubes or other profiled members
- B29C53/086—Bending or folding of tubes or other profiled members bending radially, i.e. deformig the cross-section of the tube
-
- 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
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- 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
-
- 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
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/462—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
- B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
-
- 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
- B29K2101/00—Use of unspecified macromolecular compounds as moulding material
- B29K2101/12—Thermoplastic materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
- B29L2031/005—Profiled members, e.g. beams, sections having a profiled transverse cross-section for making window frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
Abstract
L'invention concerne un procédé pour la fabrication d'un cadre comprenant une section extrudée selon un contour guide, laquelle section comprend une semelle et une âme s'étendant en section selon des directions concourantes et perpendiculaires au contour guide, caractérisé en ce qu'il comprend les étapes consistant à : a. réaliser une préforme fibreuse, dite chaussette, de section tubulaire par un procédé de tressage ; b. aplatir la section tubulaire de ladite chaussette et appliquer celle-ci , telle une bande (200'), selon une première partie (210) de la largeur de ladite bande sur la première face (310) d'un outillage (300) comportant deux faces (3120, 320) concourantes dont l'intersection est parallèle au contour guide ; c. rabattre la deuxième partie (220) de ladite bande (200') sur une face (320) de l'outillage concourante de la première face ; d. consolider la préforme ainsi réalisée par sa combinaison avec une résine polymère. L'invention concerne également un hublot, notamment pour aéronef obtenu par un tel procédé.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1252662A FR2988324B1 (fr) | 2012-03-23 | 2012-03-23 | Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede |
PCT/EP2013/055497 WO2013139714A2 (fr) | 2012-03-23 | 2013-03-15 | Procédé pour la fabrication d'un cadre de hublot en matériau composite a renfort fibreux et hublot obtenu par un tel procédé |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1252662A FR2988324B1 (fr) | 2012-03-23 | 2012-03-23 | Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2988324A1 FR2988324A1 (fr) | 2013-09-27 |
FR2988324B1 true FR2988324B1 (fr) | 2014-04-25 |
Family
ID=47884360
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1252662A Expired - Fee Related FR2988324B1 (fr) | 2012-03-23 | 2012-03-23 | Procede pour la fabrication d'un cadre de hublot en materiau composite a renfort fibreux et hublot obtenu par un tel procede |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2988324B1 (fr) |
WO (1) | WO2013139714A2 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2781182T3 (es) * | 2015-11-05 | 2020-08-31 | Airbus Operations Sl | Procedimiento de fabricación de una cuaderna circundante de abertura para un fuselaje de aeronave, y cuaderna |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004025381B4 (de) * | 2004-05-24 | 2014-01-23 | Airbus Operations Gmbh | Fensterrahmen für Flugzeuge |
BR112012006935B1 (pt) | 2009-10-01 | 2020-01-14 | Albany Eng Composites Inc | pré-forma tecida tridimensional, compósito reforçado de fibra, métodos de formação de pré-forma tecida tridimensional e de compósito reforçado com fibra |
RU2550860C2 (ru) * | 2009-10-01 | 2015-05-20 | Олбани Энджиниэрд Композитс, Инк. | Тканая заготовка, композитный материал, и способ их изготовления |
FR2964062B1 (fr) * | 2010-08-31 | 2012-08-24 | Messier Dowty Sa | Procede de fabrication d'un organe mecanique en materiau composite ayant une tenue mecanique accrue |
-
2012
- 2012-03-23 FR FR1252662A patent/FR2988324B1/fr not_active Expired - Fee Related
-
2013
- 2013-03-15 WO PCT/EP2013/055497 patent/WO2013139714A2/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2013139714A2 (fr) | 2013-09-26 |
FR2988324A1 (fr) | 2013-09-27 |
WO2013139714A3 (fr) | 2013-12-19 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 5 |
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RN | Application for restoration |
Effective date: 20190703 |
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FC | Decision of inpi director general to approve request for restoration |
Effective date: 20190709 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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ST | Notification of lapse |
Effective date: 20211105 |