FR2995244B1 - Procede de realisation d'un profile en materiau composite presentant un angle rentrant a partir d'un empilage de couches de fibres - Google Patents
Procede de realisation d'un profile en materiau composite presentant un angle rentrant a partir d'un empilage de couches de fibresInfo
- Publication number
- FR2995244B1 FR2995244B1 FR1258369A FR1258369A FR2995244B1 FR 2995244 B1 FR2995244 B1 FR 2995244B1 FR 1258369 A FR1258369 A FR 1258369A FR 1258369 A FR1258369 A FR 1258369A FR 2995244 B1 FR2995244 B1 FR 2995244B1
- Authority
- FR
- France
- Prior art keywords
- stack
- making
- composite material
- fiber layers
- material profile
- 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
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
- B29C70/28—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
- B29C70/549—Details of caul plates, e.g. materials or shape
-
- 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
- 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
- B29D99/0003—Producing profiled members, e.g. beams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/0288—Controlling heating or curing of polymers during moulding, e.g. by measuring temperatures or properties of the polymer and regulating the process
-
- 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
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/0872—Prepregs
-
- 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
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
-
- 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.]
- Y10T428/24628—Nonplanar uniform thickness material
- Y10T428/24636—Embodying mechanically interengaged strand[s], strand-portion[s] or strand-like strip[s] [e.g., weave, knit, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258369A FR2995244B1 (fr) | 2012-09-07 | 2012-09-07 | Procede de realisation d'un profile en materiau composite presentant un angle rentrant a partir d'un empilage de couches de fibres |
US14/013,872 US9840063B2 (en) | 2012-09-07 | 2013-08-29 | Method for producing a profile that has a re-entrant angle in a composite material from a stack of layers of fibres |
CN201310407133.6A CN103660309B (zh) | 2012-09-07 | 2013-09-09 | 用于以叠层纤维的复合材料生产具有凹角的型材的方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258369A FR2995244B1 (fr) | 2012-09-07 | 2012-09-07 | Procede de realisation d'un profile en materiau composite presentant un angle rentrant a partir d'un empilage de couches de fibres |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2995244A1 FR2995244A1 (fr) | 2014-03-14 |
FR2995244B1 true FR2995244B1 (fr) | 2014-10-10 |
Family
ID=47137904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1258369A Active FR2995244B1 (fr) | 2012-09-07 | 2012-09-07 | Procede de realisation d'un profile en materiau composite presentant un angle rentrant a partir d'un empilage de couches de fibres |
Country Status (3)
Country | Link |
---|---|
US (1) | US9840063B2 (fr) |
CN (1) | CN103660309B (fr) |
FR (1) | FR2995244B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9211679B1 (en) | 2013-05-03 | 2015-12-15 | The Boeing Company | Systems and methods of forming a skin for a composite structure and composite structures including the same |
US9663247B2 (en) | 2015-02-27 | 2017-05-30 | The Boeing Company | Systems, methods, and vacuum chucks for transferring flexible elongate bodies |
US10005234B2 (en) * | 2015-10-29 | 2018-06-26 | The Boeing Company | Devices, systems, and methods for compacting a charge of composite material across an edge |
CN108883586B (zh) * | 2016-04-06 | 2020-10-09 | 罗尔斯·罗伊斯公司 | 用于制造复合部件的方法 |
KR102473358B1 (ko) | 2017-03-16 | 2022-12-06 | 더 보잉 컴파니 | 경화된 복합재 부품을 정의하기 위해 제1 열경화성 복합재와 제2 열경화성 복합재를 일체접합하는 방법 |
RU2762099C2 (ru) * | 2017-03-16 | 2021-12-15 | Зе Боинг Компани | Система и способ отверждения термореактивного композита до заданного состояния отверждения |
WO2019049411A1 (fr) * | 2017-09-06 | 2019-03-14 | 株式会社Subaru | Dispositif de mise en forme de préforme |
CN111619138B (zh) * | 2020-05-27 | 2021-09-24 | 大连理工大学 | 一种激光辅助原位成形热塑性复合材料结构件的回弹变形抑制方法 |
US12049047B2 (en) * | 2020-06-17 | 2024-07-30 | Mitsubishi Heavy Industries, Ltd. | Jig and composite material processing method |
IT202000028046A1 (it) * | 2020-11-23 | 2022-05-23 | Leonardo Spa | Metodo e dispositivo per la fabbricazione di un elemento strutturale in materiale composito con profilo a z |
US11752708B2 (en) | 2021-09-10 | 2023-09-12 | The Boeing Company | Uncured composite structures, cured composite structures, and methods of curing uncured composite structures |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2173144B (en) * | 1985-04-02 | 1989-08-09 | Rolls Royce Plc | Moulding of composite materials |
US5123985A (en) * | 1986-09-02 | 1992-06-23 | Patricia Evans | Vacuum bagging apparatus and method including a thermoplastic elastomer film vacuum bag |
JP2807891B2 (ja) * | 1989-02-28 | 1998-10-08 | 三菱レイヨン株式会社 | プリプレグ及びその製造法 |
US5145621A (en) * | 1990-04-20 | 1992-09-08 | General Electric Company | Crossover mold tool for consolidating composite material |
US5597435A (en) * | 1992-12-24 | 1997-01-28 | General Electric Company | Method using restrained cauls for composite molding |
US5348602A (en) * | 1993-06-08 | 1994-09-20 | General Electric Company | Method for making a bonded laminated article bend portion |
US7622066B2 (en) * | 2004-07-26 | 2009-11-24 | The Boeing Company | Methods and systems for manufacturing composite parts with female tools |
US7306450B2 (en) * | 2004-09-29 | 2007-12-11 | The Boeing Company | Apparatuses, systems, and methods for manufacturing composite parts |
US8691137B2 (en) * | 2009-03-04 | 2014-04-08 | The Boeing Company | Method of molding partus using a tool sleeve for mold die |
US20080060755A1 (en) * | 2006-09-13 | 2008-03-13 | General Electric Corporation | composite corner and method for making composite corner |
ITTO20070294A1 (it) * | 2007-05-03 | 2008-11-04 | Alenia Aeronautica Spa | Procedimento di fabbricazione di un pezzo in materiale composito con sezione a z |
ITTO20070659A1 (it) * | 2007-09-20 | 2009-03-21 | Alenia Aeronautica Spa | Procedimento di fabbricazione di un elemento strutturale curvilineo in materiale composito avente una sezione aperta complessa. |
US7754045B2 (en) * | 2007-11-14 | 2010-07-13 | The Boeing Company | Method and tools for fabricating composite beams |
CN101186707A (zh) * | 2007-11-15 | 2008-05-28 | 重庆长安汽车股份有限公司 | 一种汽车上用的玻璃纤维多层织物增强环氧树脂复合材料 |
CN101254652B (zh) * | 2007-12-28 | 2010-04-21 | 西安交通大学 | 制造树脂基复合材料构件的原位固结纤维铺放方法及装置 |
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. |
US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US8585952B2 (en) * | 2009-06-12 | 2013-11-19 | Alliant Techsystems Inc. | Pressure molded preform process for composite structures |
US8771575B2 (en) * | 2011-07-27 | 2014-07-08 | Dieffenbacher GmbH Maschinen- und Anlagenbau | Methods and systems for forming reinforced composite articles having variable thickness corners |
CN102529113B (zh) * | 2011-12-27 | 2014-04-09 | 成都飞机工业(集团)有限责任公司 | 复合材料构件转角间隙的填充方法 |
FR2987779A1 (fr) * | 2012-03-12 | 2013-09-13 | Airbus Operations Sas | Procede de realisation d'une piece en materiau composite et outillage pour sa mise en oeuvre |
-
2012
- 2012-09-07 FR FR1258369A patent/FR2995244B1/fr active Active
-
2013
- 2013-08-29 US US14/013,872 patent/US9840063B2/en active Active
- 2013-09-09 CN CN201310407133.6A patent/CN103660309B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
US9840063B2 (en) | 2017-12-12 |
CN103660309A (zh) | 2014-03-26 |
FR2995244A1 (fr) | 2014-03-14 |
US20140072775A1 (en) | 2014-03-13 |
CN103660309B (zh) | 2017-09-01 |
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