ES2098521T3 - Un procedimiento para formar y consolidar una estructura de resina reforzada con fibras. - Google Patents
Un procedimiento para formar y consolidar una estructura de resina reforzada con fibras.Info
- Publication number
- ES2098521T3 ES2098521T3 ES92916155T ES92916155T ES2098521T3 ES 2098521 T3 ES2098521 T3 ES 2098521T3 ES 92916155 T ES92916155 T ES 92916155T ES 92916155 T ES92916155 T ES 92916155T ES 2098521 T3 ES2098521 T3 ES 2098521T3
- Authority
- ES
- Spain
- Prior art keywords
- southern
- consolidating
- fibers
- procedure
- forming
- 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 - Lifetime
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
- B29D23/00—Producing tubular articles
-
- 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
- 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
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
-
- 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
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/243—Partially cured
-
- 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
- B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
- B29L2031/601—Multi-tubular articles, i.e. composed of a plurality of tubes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Reinforced Plastic Materials (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
LAS ESTRUCTURAS COMPUESTAS DE RESINA REFORZADA CON FIBRAS SE ENDURECEN Y SE CONSOLIDAN COMPLETAMENTE MIENTRAS SE COMPENSA LA COMPACTACION INICIAL INCOMPLETA DEL PREIMPREGNADO ENTRE LOS NUCLEOS, Y EL CRECIMIENTO TERMICO DEL MANDRIL QUE DISTRIBUYE LOS NUCLEOS SEPARADOS FORMANDO LA ESTRUCTURA ALREDEDOR DE UNA FORMA DE ALEACION DE METAL SUJETA AL MANDRIL EN EL QUE EL COEFICIENTE DE EXPANSION TERMICA DE LA ALEACION DE METAL ES MAYOR QUE EL DEL MANDRIL.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/735,841 US5125993A (en) | 1991-07-25 | 1991-07-25 | Method for forming and consolidating a fiber reinforced resin structure |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2098521T3 true ES2098521T3 (es) | 1997-05-01 |
Family
ID=24957411
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES92916155T Expired - Lifetime ES2098521T3 (es) | 1991-07-25 | 1992-07-24 | Un procedimiento para formar y consolidar una estructura de resina reforzada con fibras. |
Country Status (10)
Country | Link |
---|---|
US (1) | US5125993A (es) |
EP (1) | EP0595959B1 (es) |
JP (1) | JPH06509292A (es) |
KR (1) | KR100214396B1 (es) |
AU (1) | AU2393692A (es) |
BR (1) | BR9206288A (es) |
CA (1) | CA2113622A1 (es) |
DE (1) | DE69217953T2 (es) |
ES (1) | ES2098521T3 (es) |
WO (1) | WO1993001925A1 (es) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5429693A (en) * | 1994-05-09 | 1995-07-04 | The United States Of America As Represented By The Secretary Of The Air Force | Method of making a prestressed composite materials |
US5716677A (en) * | 1996-03-21 | 1998-02-10 | Ohio Aerospace Institute | Protective coatings for polyimide composites |
US5795524A (en) * | 1996-03-29 | 1998-08-18 | Basso, Jr.; Robert J. | Process for producing composite tubular parts |
FR2760399B1 (fr) * | 1997-03-06 | 1999-05-07 | Hispano Suiza Sa | Procede de fabrication de pieces creuses en materiau composite |
CA2253037C (en) * | 1997-11-12 | 2004-11-02 | Sakura Rubber Co., Ltd. | Method of manufacturing structure by using biodegradable mold |
AU2230499A (en) | 1998-01-16 | 1999-08-02 | Maverick Corporation | Low-toxicity, high-temperature polyimides |
DE10210517B3 (de) * | 2002-03-09 | 2004-01-29 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Bauteiles in Faserverbundbauweise |
EP1473131A3 (de) * | 2003-04-30 | 2007-01-03 | Airbus Deutschland GmbH | Verfahren zum herstellen textiler vorformlinge aus textilen halbzeugen |
US7166251B2 (en) * | 2004-12-01 | 2007-01-23 | The Boeing Company | Segmented flexible barrel lay-up mandrel |
JP5738033B2 (ja) * | 2011-03-28 | 2015-06-17 | 三菱重工業株式会社 | 複合材構造体の成形方法 |
DE202013004692U1 (de) | 2013-05-22 | 2013-06-14 | Weinor Gmbh & Co. Kg | Markise mit Spannsystem |
JP5777789B1 (ja) * | 2014-10-30 | 2015-09-09 | 三菱重工業株式会社 | 人工欠陥材料及びfrp構造体の製造方法 |
DE102014017949A1 (de) | 2014-12-05 | 2016-06-09 | Weinor Gmbh & Co. Kg | Markise mit Gegenzugsystem |
DE102015000671A1 (de) | 2015-01-23 | 2016-07-28 | Weinor Gmbh & Co. Kg | Markise mit Gewebe-Gegenzugsystem |
US20160214283A1 (en) * | 2015-01-26 | 2016-07-28 | General Electric Company | Composite tool and method for forming composite components |
CN109605780B (zh) * | 2018-11-20 | 2021-02-19 | 航天时代飞鸿技术有限公司 | 一种无人机复合材料结构整体成型的方法 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2755216A (en) * | 1952-08-16 | 1956-07-17 | Douglas Aircraft Co Inc | Process for forming a multi-ducted shell |
FR1111380A (fr) * | 1954-11-02 | 1956-02-27 | Renault | Panneaux en matières plastiques |
US3165569A (en) * | 1960-04-18 | 1965-01-12 | Air Logisties Corp | Method and apparatus for thermal expansion molding |
CH530249A (de) * | 1971-10-22 | 1972-11-15 | Liechti Fritz Dipl Ing Dr | Verfahren zur Herstellung von Formteilen aus Kunststoffen mit komplizierten Aussparungen und Hohlräumen |
US4187271A (en) * | 1977-04-18 | 1980-02-05 | Owens-Corning Fiberglas Corporation | Method of making same |
US4155970A (en) * | 1977-11-04 | 1979-05-22 | Mcdonnell Douglas Corporation | Method for making a hollow composite using a destructible core |
US4167430A (en) * | 1978-04-28 | 1979-09-11 | General Dynamics Corporation | Method for fabricating a composite bonded structure |
JPS54156080A (en) * | 1978-05-31 | 1979-12-08 | Nitto Electric Ind Co Ltd | Manufacture of pipe connection member in tubular module |
US4474636A (en) * | 1981-11-06 | 1984-10-02 | Qo Chemicals, Inc. | Fabrication of composite articles |
GB2190724B (en) * | 1986-04-16 | 1990-08-08 | Courtaulds Plc | Composite element |
-
1991
- 1991-07-25 US US07/735,841 patent/US5125993A/en not_active Expired - Fee Related
-
1992
- 1992-07-24 DE DE69217953T patent/DE69217953T2/de not_active Expired - Fee Related
- 1992-07-24 ES ES92916155T patent/ES2098521T3/es not_active Expired - Lifetime
- 1992-07-24 CA CA002113622A patent/CA2113622A1/en not_active Abandoned
- 1992-07-24 EP EP92916155A patent/EP0595959B1/en not_active Expired - Lifetime
- 1992-07-24 JP JP5503026A patent/JPH06509292A/ja active Pending
- 1992-07-24 BR BR9206288A patent/BR9206288A/pt not_active Application Discontinuation
- 1992-07-24 KR KR1019940700212A patent/KR100214396B1/ko not_active IP Right Cessation
- 1992-07-24 AU AU23936/92A patent/AU2393692A/en not_active Abandoned
- 1992-07-24 WO PCT/US1992/006060 patent/WO1993001925A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
CA2113622A1 (en) | 1993-02-04 |
BR9206288A (pt) | 1994-08-02 |
DE69217953T2 (de) | 1997-07-10 |
EP0595959A1 (en) | 1994-05-11 |
WO1993001925A1 (en) | 1993-02-04 |
JPH06509292A (ja) | 1994-10-20 |
AU2393692A (en) | 1993-02-23 |
US5125993A (en) | 1992-06-30 |
DE69217953D1 (de) | 1997-04-10 |
EP0595959B1 (en) | 1997-03-05 |
KR100214396B1 (ko) | 1999-09-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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