BR112016014735A2 - Processo para a estampagem de um disco compósito com matriz termoplástica não consolidada - Google Patents
Processo para a estampagem de um disco compósito com matriz termoplástica não consolidadaInfo
- Publication number
- BR112016014735A2 BR112016014735A2 BR112016014735A BR112016014735A BR112016014735A2 BR 112016014735 A2 BR112016014735 A2 BR 112016014735A2 BR 112016014735 A BR112016014735 A BR 112016014735A BR 112016014735 A BR112016014735 A BR 112016014735A BR 112016014735 A2 BR112016014735 A2 BR 112016014735A2
- Authority
- BR
- Brazil
- Prior art keywords
- disc
- thermoplastic matrix
- stamping process
- stamping
- unconsolidated
- Prior art date
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
-
- 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
- B29C70/345—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 matched moulds
-
- 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
- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/005—Surface shaping of articles, e.g. embossing; Apparatus therefor characterised by the choice of material
-
- 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
- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/02—Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing
- B29C59/026—Surface shaping of articles, e.g. embossing; Apparatus therefor by mechanical means, e.g. pressing of layered or coated substantially flat surfaces
-
- 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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/386—Automated tape laying [ATL]
-
- 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
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the 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
- 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
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during 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
- B29K2071/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone or derivatives thereof, as moulding material
-
- 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
- B29K2871/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone or derivatives thereof, as mould material
-
- 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
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0041—Crystalline
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Robotics (AREA)
- Textile Engineering (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Abstract
PROCESSO PARA A ESTAMPAGEM DE UM DISCO COMPÓSITO COM MATRIZ TERMOPLÁSTICA NÃO CONSOLIDADA. A presente invenção refere-se a um processo para a realização, por estampagem a quente, de uma peça compósita de reforço fibroso contínuo em uma matriz termoplástica, caracterizado pelo fato de comportar as etapas que consistem em: a) obter um disco (160) que compreende uma estratificação de camadas que consistem em camadas (110) unidirecionais de fibras pré-impregnadas de um polímero termoplástico; b) aquecer ao ar livre o disco (160) a uma temperatura superior ou igual à temperatura de fusão do polímero que constitui a matriz; c) estampar o disco (160).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1363575 | 2013-12-24 | ||
FR1363575A FR3016314B1 (fr) | 2013-12-24 | 2013-12-24 | Procede et dispositif pour l’estampage d’un flan composite a matrice thermoplastique non consolide |
PCT/EP2014/079340 WO2015097301A1 (fr) | 2013-12-24 | 2014-12-24 | Procédé et dispositif pour l'estampage d'un flan composite à matrice thermoplastique non consolidé |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112016014735A2 true BR112016014735A2 (pt) | 2017-08-08 |
BR112016014735B1 BR112016014735B1 (pt) | 2021-12-28 |
Family
ID=50179851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112016014735-9A BR112016014735B1 (pt) | 2013-12-24 | 2014-12-24 | Processo para a estampagem de um disco compósito com matriz termoplástica não consolidada |
Country Status (8)
Country | Link |
---|---|
US (1) | US10773470B2 (pt) |
EP (1) | EP3096940B1 (pt) |
JP (1) | JP6722589B2 (pt) |
BR (1) | BR112016014735B1 (pt) |
CA (1) | CA2934952C (pt) |
ES (1) | ES2881218T3 (pt) |
FR (1) | FR3016314B1 (pt) |
WO (1) | WO2015097301A1 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10479029B2 (en) * | 2015-01-16 | 2019-11-19 | The Boeing Company | Composite forming apparatus |
US10375950B2 (en) * | 2015-12-07 | 2019-08-13 | Valent Biosciences Llc | Concentrated gibberellin solution formulations |
US10583617B2 (en) | 2016-11-28 | 2020-03-10 | General Electric Company | Automatic systems and methods for stacking composite plies |
DE102020206058A1 (de) | 2020-05-13 | 2021-11-18 | Ford Global Technologies, Llc | Verbindungselement, Bauteil aus einem Kompositwerkstoff und Verfahren zur Herstellung eines Bauteils aus einem Kompositwerkstoff |
KR102472506B1 (ko) * | 2021-07-02 | 2022-12-01 | 한국항공우주산업 주식회사 | 복합재 제조 방법 |
FR3134333B3 (fr) | 2022-04-11 | 2024-04-19 | Daher Aerospace | Outillage d’estampage à mobilités multiples |
FR3140570A1 (fr) * | 2022-10-05 | 2024-04-12 | Daher Aerospace | système pour l’estampage d’un flan composite thermoplastique épais |
FR3142117A1 (fr) | 2022-11-23 | 2024-05-24 | Daher Aerospace | Procédé pour l’intégration d’un raidisseur à une pièce composite à matrice thermoplastique |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8406869D0 (en) * | 1984-03-16 | 1984-04-18 | Alcan Int Ltd | Forming fibrethermoplastic composites |
JP3250901B2 (ja) * | 1994-02-07 | 2002-01-28 | 三井化学株式会社 | 繊維補強樹脂シートの積層体の製造方法 |
WO2004103669A2 (en) * | 2003-05-21 | 2004-12-02 | Brown Machine, Llc. | Closed loop oven control system and method |
FR2863543B1 (fr) * | 2003-12-16 | 2007-11-02 | Airbus France | Procede de formage par estampage a chaud de pieces de tolerie complexes en materiau composite et outillage pour sa mise en oeuvre |
FR2905891B1 (fr) * | 2006-09-15 | 2008-12-05 | Airbus France Sa | Procede de fabrication d'un panneau en materiau composite thermoplastique |
FR2922276B1 (fr) | 2007-10-12 | 2012-05-04 | Airbus France | Jonction triedre en materiau composite et procede de fabrication d'une telle jonction |
FR2929167B1 (fr) | 2008-03-27 | 2010-04-23 | Airbus France | Procede de fabrication d'un flan en materiau composite thermoplastique, outillage de fabrication associe et application du procede a la realisation de pieces de structure d'aeronef |
DE102008020347B4 (de) * | 2008-04-23 | 2012-03-15 | Airbus Operations Gmbh | Vorrichtung zur Herstellung eines Bauteils und Verfahren |
FR2942600A1 (fr) * | 2009-02-27 | 2010-09-03 | Airbus France | Procede de compactage en cote finie d'une piece composite thermoplastique a fibres continues |
US8158245B2 (en) * | 2009-09-24 | 2012-04-17 | Cytec Technology Corp. | Thermoplastic composites and methods of making and using same |
DE102010013131A1 (de) * | 2009-12-21 | 2011-06-22 | REHAU AG + Co., 95111 | Verfahren zur Herstellung von endlosfaserverstärkten Formteilen aus thermoplastischem Kunststoff sowie Kraftfahrzeugformteil |
JP5968600B2 (ja) * | 2011-06-14 | 2016-08-10 | 三菱レイヨン株式会社 | 繊維強化熱可塑性樹脂成形品とその製造方法、および複合体とその製造方法 |
JP2013018858A (ja) * | 2011-07-11 | 2013-01-31 | Toray Ind Inc | 予備成形体およびその製造方法 |
GB201117796D0 (en) * | 2011-10-14 | 2011-11-30 | Victrex Mfg Ltd | Polymeric materials |
FR2987304B1 (fr) * | 2012-02-29 | 2018-03-02 | Daher Aerospace | Procede de formage par estampage d'un materiau composite thermoplastique a renfort fibreux continu |
FR2987307B1 (fr) | 2012-02-29 | 2017-02-10 | Daher Aerospace | Procede et dispositif pour le compactage et la consolidation d'un panneau composite de forte epaisseur a matrice thermoplastique |
-
2013
- 2013-12-24 FR FR1363575A patent/FR3016314B1/fr active Active
-
2014
- 2014-12-24 ES ES14824847T patent/ES2881218T3/es active Active
- 2014-12-24 CA CA2934952A patent/CA2934952C/fr active Active
- 2014-12-24 US US15/107,425 patent/US10773470B2/en active Active
- 2014-12-24 WO PCT/EP2014/079340 patent/WO2015097301A1/fr active Application Filing
- 2014-12-24 BR BR112016014735-9A patent/BR112016014735B1/pt active IP Right Grant
- 2014-12-24 JP JP2016561080A patent/JP6722589B2/ja active Active
- 2014-12-24 EP EP14824847.9A patent/EP3096940B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
ES2881218T3 (es) | 2021-11-29 |
WO2015097301A1 (fr) | 2015-07-02 |
EP3096940B1 (fr) | 2021-04-21 |
JP6722589B2 (ja) | 2020-07-15 |
JP2017503691A (ja) | 2017-02-02 |
FR3016314A1 (fr) | 2015-07-17 |
FR3016314B1 (fr) | 2016-04-15 |
BR112016014735B1 (pt) | 2021-12-28 |
US10773470B2 (en) | 2020-09-15 |
CA2934952A1 (fr) | 2015-07-02 |
CA2934952C (fr) | 2022-06-07 |
EP3096940A1 (fr) | 2016-11-30 |
US20170001383A1 (en) | 2017-01-05 |
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B06A | Patent application procedure suspended [chapter 6.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 24/12/2014, OBSERVADAS AS CONDICOES LEGAIS. |