FR2963273B1 - Procede de fabrication d'un panneau raidi en materiau composite - Google Patents
Procede de fabrication d'un panneau raidi en materiau compositeInfo
- Publication number
- FR2963273B1 FR2963273B1 FR1056264A FR1056264A FR2963273B1 FR 2963273 B1 FR2963273 B1 FR 2963273B1 FR 1056264 A FR1056264 A FR 1056264A FR 1056264 A FR1056264 A FR 1056264A FR 2963273 B1 FR2963273 B1 FR 2963273B1
- Authority
- FR
- France
- Prior art keywords
- panel
- stiffener
- mdash
- composite material
- raidi
- 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
-
- 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
- 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
- B29C33/50—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 elastic or flexible
- B29C33/505—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 elastic or flexible cores or mandrels, e.g. inflatable
-
- 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
- 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
- B29D99/0017—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs with filled hollow ridges
-
- 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)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1056264A FR2963273B1 (fr) | 2010-07-29 | 2010-07-29 | Procede de fabrication d'un panneau raidi en materiau composite |
US13/186,801 US9114574B2 (en) | 2010-07-29 | 2011-07-20 | Method for manufacturing a stiffened panel of composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1056264A FR2963273B1 (fr) | 2010-07-29 | 2010-07-29 | Procede de fabrication d'un panneau raidi en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2963273A1 FR2963273A1 (fr) | 2012-02-03 |
FR2963273B1 true FR2963273B1 (fr) | 2014-01-03 |
Family
ID=43805703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1056264A Active FR2963273B1 (fr) | 2010-07-29 | 2010-07-29 | Procede de fabrication d'un panneau raidi en materiau composite |
Country Status (2)
Country | Link |
---|---|
US (1) | US9114574B2 (fr) |
FR (1) | FR2963273B1 (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008062477B3 (de) | 2008-12-16 | 2010-03-25 | Airbus Deutschland Gmbh | Verfahren, System und Formwerkzeug zum Herstellen von Bauteilen aus Faserverbundwerkstoffen |
FR2963272B1 (fr) * | 2010-07-29 | 2012-08-17 | Airbus Operations Sas | Procede de fabrication d'un panneau raidi en materiau composite |
US9399510B2 (en) * | 2014-08-20 | 2016-07-26 | The Boeing Company | Hat stringer closeout fitting and method of making same |
US10899103B2 (en) | 2016-11-03 | 2021-01-26 | Anthony A. DUPont | Isogrid stiffening elements |
ES2954328T3 (es) * | 2017-07-25 | 2023-11-21 | Subaru Corp | Plantilla de moldeo de materiales compuestos y método de moldeo de materiales compuestos |
CN110001084A (zh) * | 2019-05-21 | 2019-07-12 | 陕西理工大学 | 飞机尾鳍的内高压成形模具及成形方法 |
GB2609030B (en) * | 2021-07-19 | 2023-11-22 | Safran Nacelles | Assembly structure and process for manufacturing a composite part with controlled geometry |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1054218A (fr) | 1950-12-15 | 1954-02-09 | Ciba Geigy | Procédé pour la préparation de solutions de 2-aminonaphtalène dans des solvants organiques |
US5484277A (en) * | 1989-12-26 | 1996-01-16 | Mcdonnell Douglas Corporation | Mandreless molding system |
US7052572B2 (en) * | 2001-08-01 | 2006-05-30 | Fuji Jukogyo Kabushiki Kaisha | Method for manufacturing a structure |
FR2899837B1 (fr) * | 2006-04-18 | 2010-09-17 | Latecoere | Panneau en materiau composite et procede de realisation de ce panneau |
DE102006031334A1 (de) * | 2006-07-06 | 2008-01-10 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
FR2963272B1 (fr) * | 2010-07-29 | 2012-08-17 | Airbus Operations Sas | Procede de fabrication d'un panneau raidi en materiau composite |
-
2010
- 2010-07-29 FR FR1056264A patent/FR2963273B1/fr active Active
-
2011
- 2011-07-20 US US13/186,801 patent/US9114574B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2963273A1 (fr) | 2012-02-03 |
US9114574B2 (en) | 2015-08-25 |
US20120024468A1 (en) | 2012-02-02 |
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