ATE251546T1 - Verfahren zur herstellung einer mit versteifungsrippen versehenen platte aus verbundwerkstoff und mit diesem verfahren hergestellte platte - Google Patents
Verfahren zur herstellung einer mit versteifungsrippen versehenen platte aus verbundwerkstoff und mit diesem verfahren hergestellte platteInfo
- Publication number
- ATE251546T1 ATE251546T1 AT01450006T AT01450006T ATE251546T1 AT E251546 T1 ATE251546 T1 AT E251546T1 AT 01450006 T AT01450006 T AT 01450006T AT 01450006 T AT01450006 T AT 01450006T AT E251546 T1 ATE251546 T1 AT E251546T1
- Authority
- AT
- Austria
- Prior art keywords
- bladder
- bands
- fold
- mold
- sets
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 3
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
- 239000011347 resin Substances 0.000 abstract 3
- 229920005989 resin Polymers 0.000 abstract 3
- 239000000835 fiber Substances 0.000 abstract 2
- 230000002787 reinforcement Effects 0.000 abstract 2
- 238000007666 vacuum forming Methods 0.000 abstract 2
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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0067—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other
- B29C37/0075—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other using release 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
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
-
- 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
- B29C70/342—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 isostatic pressure
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0005798A FR2808472B1 (fr) | 2000-05-05 | 2000-05-05 | Procede de fabrication d'un panneau en materiau composite a bandes raidisseurs et panneau ainsi obtenu |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE251546T1 true ATE251546T1 (de) | 2003-10-15 |
Family
ID=8849955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT01450006T ATE251546T1 (de) | 2000-05-05 | 2001-05-03 | Verfahren zur herstellung einer mit versteifungsrippen versehenen platte aus verbundwerkstoff und mit diesem verfahren hergestellte platte |
Country Status (7)
| Country | Link |
|---|---|
| US (2) | US6746642B2 (de) |
| EP (1) | EP1151856B1 (de) |
| AT (1) | ATE251546T1 (de) |
| CA (1) | CA2346311C (de) |
| DE (1) | DE60100919T2 (de) |
| ES (1) | ES2208535T3 (de) |
| FR (1) | FR2808472B1 (de) |
Families Citing this family (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060198962A1 (en) * | 2005-03-02 | 2006-09-07 | Efim Kravetz | Method for producing extremely durable photographs and printed matter |
| US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
| US7943076B1 (en) * | 2005-05-03 | 2011-05-17 | The Boeing Company | Method of manufacturing curved composite structural elements |
| CN101448626B (zh) * | 2006-03-31 | 2012-02-22 | 空中客车西班牙运营有限责任公司 | 用可收缩模具制造复合材料结构的方法 |
| ES2560860T3 (es) * | 2006-03-31 | 2016-02-23 | Airbus Operations S.L. | Procedimiento de fabricación de estructuras de material compuesto con un utillaje colapsable |
| CN101801649A (zh) * | 2007-05-28 | 2010-08-11 | 空客运营有限公司 | 制造复合材料结构的方法和模具 |
| US8337163B2 (en) * | 2007-12-05 | 2012-12-25 | General Electric Company | Fiber composite half-product with integrated elements, manufacturing method therefor and use thereof |
| 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. |
| FR2928577B1 (fr) * | 2008-03-14 | 2011-11-25 | Airbus France | Procede de realisation d'un raidisseur evide en forme de omega et noyau pour la realisation d'un raidisseur evide en forme de omega |
| US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
| US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
| US9090028B2 (en) | 2008-04-17 | 2015-07-28 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
| US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
| FR2933379B1 (fr) * | 2008-07-07 | 2010-08-20 | Aerazur | Procede d'assemblage d'un tapis de degivrage et d'un blindage metallique sur une structure |
| US9327467B2 (en) | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
| US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | Mandrel for autoclave curing applications |
| DE102009060693A1 (de) * | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement |
| CA2804960A1 (en) | 2010-07-13 | 2012-01-19 | Learjet Inc. | Composite structure and method of forming same |
| US9333713B2 (en) | 2012-10-04 | 2016-05-10 | The Boeing Company | Method for co-curing composite skins and stiffeners in an autoclave |
| DE102013218520A1 (de) * | 2013-09-16 | 2015-03-19 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils, Faserverbundbauteil, sowie Strukturbauteil für ein Luft- oder Raumfahrzeug |
| US9656761B2 (en) | 2014-04-30 | 2017-05-23 | The Boeing Company | Lipskin for a nacelle and methods of making the same |
| US9938852B2 (en) | 2014-04-30 | 2018-04-10 | The Boeing Company | Noise attenuating lipskin assembly and methods of assembling the same |
| US9708072B2 (en) | 2014-04-30 | 2017-07-18 | The Boeing Company | Aircraft engine nacelle bulkheads and methods of assembling the same |
| US9604438B2 (en) | 2014-04-30 | 2017-03-28 | The Boeing Company | Methods and apparatus for noise attenuation in an engine nacelle |
| US20170094800A1 (en) * | 2015-09-28 | 2017-03-30 | Tactotek Oy | Method and arrangement for providing electrical connection to in-mold electronics |
| FR3043935B1 (fr) * | 2015-11-20 | 2018-02-23 | Geco Ingenierie | Procede et dispositif de moulage d'une piece composite, piece composite et embarcation |
| DE102015225467B4 (de) * | 2015-12-16 | 2019-12-19 | Airbus Defence and Space GmbH | Beschichtetes Verbundbauteil und Verfahren zum Herstellen eines beschichteten Verbundbauteils |
| CN105711109B (zh) * | 2016-03-23 | 2018-01-09 | 江苏恒神股份有限公司 | 一种采用双真空袋整体成型复合材料帽型加筋壁板的成型工艺 |
| US10793282B2 (en) | 2016-07-28 | 2020-10-06 | The Boeing Company | Liner assembly, engine housing, and methods of assembling the same |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3608052A (en) * | 1970-02-12 | 1971-09-21 | Texaco Inc | Method for fabricating fiber reinforced articles |
| GB1522432A (en) * | 1976-10-21 | 1978-08-23 | Ruggeri V | Method of moulding hollow stiffeners or lightweight laminates or wholly box girdered laminates in fibre reinforced plastics |
| US4304376A (en) * | 1977-12-05 | 1981-12-08 | The Boeing Company | Composite honeycomb core structures and single stage hot bonding method of producing such structures |
| US4250136A (en) * | 1979-10-22 | 1981-02-10 | Composite Technology Corporation | Method of forming a composite structure |
| US4675061A (en) * | 1985-09-24 | 1987-06-23 | Grumman Aerospace Corporation | Method for forming corrugated materials using memory metal cores |
| US4681724A (en) * | 1986-04-28 | 1987-07-21 | United Technologies Corporation | Removable irreversibly shrinking male mandrel |
| US4946526A (en) * | 1987-10-29 | 1990-08-07 | Ltv Aerospace And Defense Company | Method for compression molding of laminated panels |
| US4853172A (en) * | 1987-12-01 | 1989-08-01 | United Technologies Corporation | Method of fabricating tubular composite structures |
| US4902215A (en) * | 1988-06-08 | 1990-02-20 | Seemann Iii William H | Plastic transfer molding techniques for the production of fiber reinforced plastic structures |
| US4923545A (en) * | 1988-09-23 | 1990-05-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of insetting predesigned disbond areas into composite laminates |
| US5425986A (en) * | 1992-07-21 | 1995-06-20 | Masco Corporation | High pressure laminate structure |
| US5451377A (en) * | 1993-09-29 | 1995-09-19 | Rockwell International Corp. | Composite structures and methods of manufacturing such structures |
| USH1621H (en) * | 1995-01-31 | 1996-12-03 | The United States Of America As Represented By The Secretary Of The Navy | Offset corrugated panel with curved corrugations for increased strength |
| US5789060A (en) * | 1996-07-29 | 1998-08-04 | Specialty Cellular Products Company | Heat conduction honeycomb core |
| US6458309B1 (en) * | 1998-06-01 | 2002-10-01 | Rohr, Inc. | Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel |
-
2000
- 2000-05-05 FR FR0005798A patent/FR2808472B1/fr not_active Expired - Lifetime
-
2001
- 2001-05-01 CA CA002346311A patent/CA2346311C/fr not_active Expired - Lifetime
- 2001-05-03 EP EP01450006A patent/EP1151856B1/de not_active Expired - Lifetime
- 2001-05-03 ES ES01450006T patent/ES2208535T3/es not_active Expired - Lifetime
- 2001-05-03 AT AT01450006T patent/ATE251546T1/de not_active IP Right Cessation
- 2001-05-03 DE DE60100919T patent/DE60100919T2/de not_active Expired - Lifetime
- 2001-05-07 US US09/849,533 patent/US6746642B2/en not_active Expired - Lifetime
-
2004
- 2004-04-30 US US10/834,833 patent/US7790082B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US20040227276A1 (en) | 2004-11-18 |
| FR2808472B1 (fr) | 2003-02-28 |
| DE60100919D1 (de) | 2003-11-13 |
| CA2346311A1 (fr) | 2001-11-05 |
| EP1151856A1 (de) | 2001-11-07 |
| EP1151856B1 (de) | 2003-10-08 |
| FR2808472A1 (fr) | 2001-11-09 |
| CA2346311C (fr) | 2009-11-24 |
| US7790082B2 (en) | 2010-09-07 |
| DE60100919T2 (de) | 2004-08-19 |
| ES2208535T3 (es) | 2004-06-16 |
| US6746642B2 (en) | 2004-06-08 |
| US20010038170A1 (en) | 2001-11-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |