FR3018719B1 - Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procede - Google Patents
Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procedeInfo
- Publication number
- FR3018719B1 FR3018719B1 FR1452434A FR1452434A FR3018719B1 FR 3018719 B1 FR3018719 B1 FR 3018719B1 FR 1452434 A FR1452434 A FR 1452434A FR 1452434 A FR1452434 A FR 1452434A FR 3018719 B1 FR3018719 B1 FR 3018719B1
- Authority
- FR
- France
- Prior art keywords
- debouchant
- cavity
- carrying
- core used
- composite material
- 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
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/485—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling cores or mandrels
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1452434A FR3018719B1 (fr) | 2014-03-24 | 2014-03-24 | Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procede |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1452434A FR3018719B1 (fr) | 2014-03-24 | 2014-03-24 | Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procede |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3018719A1 FR3018719A1 (fr) | 2015-09-25 |
FR3018719B1 true FR3018719B1 (fr) | 2016-04-29 |
Family
ID=51014451
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1452434A Expired - Fee Related FR3018719B1 (fr) | 2014-03-24 | 2014-03-24 | Procede de consolidation d'elements en materiau composite pour former une piece en materiau composite comprenant une cavite debouchante et noyau utilise pour la mise en oeuvre dudit procede |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3018719B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10906210B2 (en) | 2017-01-25 | 2021-02-02 | The Boeing Company | Mandrel for composite part fabrication and repair |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4310138A (en) * | 1980-06-18 | 1982-01-12 | Johnston George S | Self-supporting shrinking mandrel |
US7293737B2 (en) * | 2004-04-20 | 2007-11-13 | The Boeing Company | Co-cured stringers and associated mandrel and fabrication method |
DE102006031326B4 (de) * | 2006-07-06 | 2010-09-23 | Airbus Deutschland Gmbh | Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031335B4 (de) * | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102009002697B4 (de) * | 2009-04-28 | 2014-02-27 | Airbus Operations Gmbh | Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
-
2014
- 2014-03-24 FR FR1452434A patent/FR3018719B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR3018719A1 (fr) | 2015-09-25 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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ST | Notification of lapse |
Effective date: 20221105 |