ES2002367A6 - Metodo de moldear materiales para darles forma ondulada y metodo de bobinar filamentos - Google Patents
Metodo de moldear materiales para darles forma ondulada y metodo de bobinar filamentosInfo
- Publication number
- ES2002367A6 ES2002367A6 ES8602089A ES8602089A ES2002367A6 ES 2002367 A6 ES2002367 A6 ES 2002367A6 ES 8602089 A ES8602089 A ES 8602089A ES 8602089 A ES8602089 A ES 8602089A ES 2002367 A6 ES2002367 A6 ES 2002367A6
- Authority
- ES
- Spain
- Prior art keywords
- base layer
- metal alloy
- memory metal
- layer
- cores
- 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
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
- 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
-
- 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
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
-
- 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
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
Abstract
METODO DE MOLDEAR MATERIALES PARA DARLES FORMA ONDULADA Y METODO DE BOBINAR FILAMENTOS, EN QUE SE DEPOSITA EN UN MOLDE UNA CAPA DE BASE DE HOJAS DE TELA IMPREGNADAS POR UN MATERIAL DE LIGADO. SE COLOCA UNA PLURALIDAD DE MACHOS HUECOS SEPARADOS PARALELOS, SOBRE LA CAPA DE BASE. LUEGO SE COLOCA UNA CAPA SUPERPUESTA SOBRE LOS MACHOS Y LA CAPA DE BASE, ESTANDO IMPREGNADA TAMBIEN LA CAPA SUPERPUESTA POR MATERIAL DE LIGADO. SE SOMETE EL CONJUNTO A CALOR Y TEMPERATURA. LUEGO SE SOMETE EL MACHO A UNA TEMPERATURA QUE PROVOCA SU ENCOGIMIENTO Y PERMITE SU RETIRADA. EL RESULTADO ES UNA CAPA DE BASE A LA QUE ESTA LIGADA LA CAPA SUPERPUESTA, PRESENTANDO LA CAPA SUPERPUESTA ONDULACIONES QUE AUMENTAN LA RESISTENCIA ESTRUCTURAL. EL FILAMENTO IMPREGNADO SE BOBINA ALREDEDOR DEL MOLDE.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/779,765 US4675061A (en) | 1985-09-24 | 1985-09-24 | Method for forming corrugated materials using memory metal cores |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2002367A6 true ES2002367A6 (es) | 1988-08-01 |
Family
ID=25117480
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES8602089A Expired ES2002367A6 (es) | 1985-09-24 | 1986-09-23 | Metodo de moldear materiales para darles forma ondulada y metodo de bobinar filamentos |
Country Status (7)
Country | Link |
---|---|
US (1) | US4675061A (es) |
EP (1) | EP0237566A4 (es) |
JP (1) | JPS63501004A (es) |
CA (1) | CA1286582C (es) |
ES (1) | ES2002367A6 (es) |
IL (1) | IL80130A0 (es) |
WO (1) | WO1987001650A1 (es) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4797085A (en) * | 1986-12-04 | 1989-01-10 | Aerojet-General Corporation | Forming apparatus employing a shape memory alloy die |
US4925611A (en) * | 1987-10-19 | 1990-05-15 | Usbi Company | Mold making method |
US4880583A (en) * | 1988-05-23 | 1989-11-14 | Shell Oil Company | Method for reduction of mold cycle time |
US5013507A (en) * | 1989-09-29 | 1991-05-07 | The Boeing Company | Method for producing an elongate passage within a component |
US5021109A (en) * | 1989-12-29 | 1991-06-04 | Xerox Corporation | Method of preparing a multilayered belt |
US5061428A (en) * | 1990-01-04 | 1991-10-29 | Davidson Textron Inc. | Method for plastic coating foam molding insert |
US5265456A (en) * | 1992-06-29 | 1993-11-30 | Grumman Aerospace Corporation | Method of cold working holes using a shape memory alloy tool |
FR2808472B1 (fr) * | 2000-05-05 | 2003-02-28 | Aerospatiale Matra Airbus | Procede de fabrication d'un panneau en materiau composite a bandes raidisseurs et panneau ainsi obtenu |
US6986855B1 (en) * | 2001-01-24 | 2006-01-17 | Cornerstone Research Group | Structural and optical applications for shape memory polymers (SMP) |
US7422714B1 (en) | 2001-01-24 | 2008-09-09 | Cornerstone Research Group, Inc. | Method of using a shape memory material as a mandrel for composite part manufacturing |
US20030051434A1 (en) * | 2001-09-20 | 2003-03-20 | Lockheed Martin Corporation | Composite structure and method for constructing same |
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 |
US7981229B2 (en) * | 2004-06-04 | 2011-07-19 | Cornerstone Research Group, Inc | Method of making and using shape memory polymer patches |
WO2005118248A2 (en) * | 2004-06-04 | 2005-12-15 | Cornerstone Research Group, Inc. | High speed manufacturing using shape memory polymer composites |
US8808479B2 (en) | 2004-06-04 | 2014-08-19 | Cornerstone Research Group, Inc. | Method of making and using shape memory polymer composite patches |
US8721822B2 (en) | 2004-06-04 | 2014-05-13 | Cornerstone Research Group, Inc. | Method of making and using shape memory polymer composite patches |
EP1755871B1 (en) * | 2004-06-04 | 2012-01-04 | Cornerstone Research Group, Inc. | Method of using shape memory polymer composite patches |
DE602005019725D1 (de) * | 2005-08-17 | 2010-04-15 | Saab Ab | Verfahren zur Herstellung eines Verbundteils mit einem Beschlagteil sowie dadurch hergestellter Verbundteil |
DE602005018207D1 (de) | 2005-09-09 | 2010-01-21 | Saab Ab | Verwendung eines spiralförmigen Werkzeugs und Verfahren zur Herstellung eines Flächenelements mit mindestens einem Versteifungsteil |
US20090095865A1 (en) * | 2006-05-01 | 2009-04-16 | Cornerstone Research Group, Inc. | Device for Securely Holding Objects in Place |
DE102006031335B4 (de) | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031336B4 (de) | 2006-07-06 | 2010-08-05 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt |
US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | Mandrel for autoclave curing applications |
US9327467B2 (en) * | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
GB2464739B (en) * | 2008-10-27 | 2013-02-13 | Ge Aviat Systems Ltd | Corrugated skins for aircraft and methods of their manufacture |
DE102010028981A1 (de) * | 2010-05-14 | 2011-11-17 | Röchling Automotive AG & Co. KG | Formveränderlicher Formkern, Formpressvorrichtung mit einem solchen Formkern und Formpressverfahren unter Verwendung eines solchen Formkerns |
US9333713B2 (en) | 2012-10-04 | 2016-05-10 | The Boeing Company | Method for co-curing composite skins and stiffeners in an autoclave |
US10239141B2 (en) | 2013-10-10 | 2019-03-26 | Rohr, Inc. | Forming a complexly curved metallic sandwich panel |
US10654230B2 (en) * | 2017-08-28 | 2020-05-19 | The Boeing Company | Methods of forming a cored composite laminate |
CN109822933B (zh) * | 2019-03-25 | 2020-09-11 | 大连理工大学 | 一种用于复合材料结构成型的磁场辅助加压方法 |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1349372A (en) * | 1920-08-10 | Method of making hollow bodies | ||
US1433728A (en) * | 1916-05-26 | 1922-10-31 | Westinghouse Electric & Mfg Co | Propeller |
US1281258A (en) * | 1917-02-13 | 1918-10-15 | B R Greenblatt | Contracting metal core for ring-molds. |
US2454719A (en) * | 1943-11-11 | 1948-11-23 | Studebaker Corp | Method of making cored laminated plastic sheets |
US3379591A (en) * | 1961-06-22 | 1968-04-23 | Richard C. Bradley | Filament winding of tubular articles with incorporation of cut lengths of roving during winding |
US4035007A (en) * | 1970-07-02 | 1977-07-12 | Raychem Corporation | Heat recoverable metallic coupling |
BE788517A (fr) * | 1971-09-07 | 1973-03-07 | Raychem Corp | Procede de dilatation sur mandrin a tres basse temperature |
US3913444A (en) * | 1972-11-08 | 1975-10-21 | Raychem Corp | Thermally deformable fastening pin |
US4012266A (en) * | 1972-08-21 | 1977-03-15 | Magee Donald L | Method and apparatus for filament winding on a corrugated form to produce a cylindrical corrugated glass fiber part |
US4001928A (en) * | 1973-01-04 | 1977-01-11 | Raychem Corporation | Method for plugging an aperture with a heat recoverable plug |
US4198081A (en) * | 1973-10-29 | 1980-04-15 | Raychem Corporation | Heat recoverable metallic coupling |
US3900939A (en) * | 1973-10-31 | 1975-08-26 | Combustion Eng | Method of plugging steam generator tubes |
US3872573A (en) * | 1973-12-19 | 1975-03-25 | Raychem Corp | Process and apparatus for making heat recoverable composite couplings |
US4338970A (en) * | 1975-06-16 | 1982-07-13 | Raychem Corporation | Recoverable sleeve |
US4172562A (en) * | 1976-12-23 | 1979-10-30 | Union Carbide Corporation | Process for winding filaments on a mandrel |
GB1599999A (en) * | 1977-01-24 | 1981-10-14 | Raychem Ltd | Heat-recoverable articles |
US4384913A (en) * | 1979-09-25 | 1983-05-24 | Ameron, Inc. | Mandrel for filament winding of plastic articles |
US4369934A (en) * | 1981-02-03 | 1983-01-25 | Spies Henry J | Helical filament winding apparatus |
US4374170A (en) * | 1981-11-09 | 1983-02-15 | Ford Motor Company | Room temperature cure polyester laminates |
US4433567A (en) * | 1981-11-12 | 1984-02-28 | Grumman Aerospace Corporation | Method for working holes |
JPS5973937A (ja) * | 1982-10-20 | 1984-04-26 | Toyota Motor Corp | 曲管ゴムホ−スの製造方法 |
JPS60139434A (ja) * | 1983-12-28 | 1985-07-24 | Toshiba Corp | 繊維強化プラスチツク成形型 |
-
1985
- 1985-09-24 US US06/779,765 patent/US4675061A/en not_active Expired - Fee Related
-
1986
- 1986-09-23 IL IL80130A patent/IL80130A0/xx unknown
- 1986-09-23 CA CA000518837A patent/CA1286582C/en not_active Expired - Lifetime
- 1986-09-23 ES ES8602089A patent/ES2002367A6/es not_active Expired
- 1986-09-24 JP JP61505174A patent/JPS63501004A/ja active Pending
- 1986-09-24 EP EP19860906166 patent/EP0237566A4/en not_active Withdrawn
- 1986-09-24 WO PCT/US1986/002012 patent/WO1987001650A1/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP0237566A1 (en) | 1987-09-23 |
EP0237566A4 (en) | 1988-04-18 |
CA1286582C (en) | 1991-07-23 |
JPS63501004A (ja) | 1988-04-14 |
US4675061A (en) | 1987-06-23 |
IL80130A0 (en) | 1986-12-31 |
WO1987001650A1 (en) | 1987-03-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 19981001 |