FR3088029B1 - Procede de drapage de plis pre-impregnes - Google Patents
Procede de drapage de plis pre-impregnes Download PDFInfo
- Publication number
- FR3088029B1 FR3088029B1 FR1860190A FR1860190A FR3088029B1 FR 3088029 B1 FR3088029 B1 FR 3088029B1 FR 1860190 A FR1860190 A FR 1860190A FR 1860190 A FR1860190 A FR 1860190A FR 3088029 B1 FR3088029 B1 FR 3088029B1
- Authority
- FR
- France
- Prior art keywords
- extending
- edges
- corner
- ply
- junction portion
- 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
- 238000000034 method Methods 0.000 title abstract 2
- 239000011159 matrix material Substances 0.000 abstract 1
- 239000002243 precursor Substances 0.000 abstract 1
- 238000007493 shaping process Methods 0.000 abstract 1
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
- B29C70/06—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
- B29C53/04—Bending or folding of plates or 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
- B29C70/28—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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/56—Tensioning reinforcements before or during shaping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
- Treatment Of Fiber Materials (AREA)
Abstract
L'invention concerne un procédé de drapage d'au moins un pli fibreux (100) pré-imprégné d'un précurseur d'une matrice sur un outillage de mise en forme (200) comprenant une face principale (210) et des première et deuxième faces latérales (220, 230) s'étendant perpendiculairement les unes par rapport aux autres et se réunissant en un coin de valise (240). Chaque pli comporte un premier bord (111) s'étendant suivant une première direction (A) et un deuxième bord (112) s'étendant suivant une deuxième direction (B) perpendiculaire à la première direction (A), les premier et deuxième bords (111, 112) étant respectivement plaqués sur les première et deuxième faces latérales (220, 230) de l'outillage de mis en forme en déformant une portion de jonction (120) entre lesdits bords sur le coin de valise (240). Chaque pli comprend une portion de sur-longueur (130) s'étendant le long d'une partie des premier et deuxième bords (111, 112) au niveau de leur portion de jonction (120), une ou plusieurs forces de tractions (FT1) étant exercés sur la portion de sur-longueur lors de la déformation de la portion de jonction (120) sur le coin de valise (240).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1860190A FR3088029B1 (fr) | 2018-11-06 | 2018-11-06 | Procede de drapage de plis pre-impregnes |
PCT/FR2019/052612 WO2020094965A1 (fr) | 2018-11-06 | 2019-11-05 | Procede de drapage de plis pre-impregnes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1860190A FR3088029B1 (fr) | 2018-11-06 | 2018-11-06 | Procede de drapage de plis pre-impregnes |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3088029A1 FR3088029A1 (fr) | 2020-05-08 |
FR3088029B1 true FR3088029B1 (fr) | 2020-11-27 |
Family
ID=66676576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1860190A Active FR3088029B1 (fr) | 2018-11-06 | 2018-11-06 | Procede de drapage de plis pre-impregnes |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3088029B1 (fr) |
WO (1) | WO2020094965A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113752588B (zh) * | 2020-06-03 | 2022-07-01 | 上海飞机制造有限公司 | 一种飞机隔框的制造方法 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4129959A1 (de) * | 1991-09-10 | 1993-03-11 | Menzolit Gmbh | Verfahren und fasermatte zur herstellung eines faserverstaerkten kunststoff-formteils sowie ein kunststoff-formteil |
US8263205B2 (en) * | 2009-09-17 | 2012-09-11 | Hexcel Corporation | Method of molding complex composite parts using pre-plied multi-directional continuous fiber laminate |
DE102012109231B4 (de) * | 2012-09-28 | 2018-01-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Integrale Verstärkungselemente |
FR3004732B1 (fr) | 2013-04-18 | 2015-05-08 | Herakles | Outillage de maintien, chargement et installation pour la densification de preformes poreuses de revolution |
JP6588691B2 (ja) * | 2014-07-18 | 2019-10-09 | 東洋炭素株式会社 | C/cコンポジット製成形体、その製造方法、及びc/cコンポジット製成形体を用いた熱処理用冶具 |
-
2018
- 2018-11-06 FR FR1860190A patent/FR3088029B1/fr active Active
-
2019
- 2019-11-05 WO PCT/FR2019/052612 patent/WO2020094965A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR3088029A1 (fr) | 2020-05-08 |
WO2020094965A1 (fr) | 2020-05-14 |
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