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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 filamentos

Info

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
Application number
ES8602089A
Other languages
English (en)
Inventor
Albert R Mead
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Publication of ES2002367A6 publication Critical patent/ES2002367A6/es
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

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.
ES8602089A 1985-09-24 1986-09-23 Metodo de moldear materiales para darles forma ondulada y metodo de bobinar filamentos Expired ES2002367A6 (es)

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)

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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
RU2188126C2 (ru) * 2000-09-14 2002-08-27 Федеральное государственное унитарное предприятие "Обнинское научно-производственное предприятие "Технология" Способ изготовления формовочной оснастки из полимерного композиционного материала
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
US8808479B2 (en) 2004-06-04 2014-08-19 Cornerstone Research Group, Inc. Method of making and using shape memory polymer composite patches
US7981229B2 (en) * 2004-06-04 2011-07-19 Cornerstone Research Group, Inc Method of making and using shape memory polymer patches
US8721822B2 (en) 2004-06-04 2014-05-13 Cornerstone Research Group, Inc. Method of making and using shape memory polymer composite patches
DE602005020001D1 (de) * 2004-06-04 2010-04-29 Cornerstone Res Group Inc Hochgeschwindigkeitsfertigung unter verwendung von formgedächtnis-polymerverbundwerkstoffen
US7938923B2 (en) * 2004-06-04 2011-05-10 Cornerstone Research Group, Inc. Method of making and using shape memory polymer composite patches
ATE459465T1 (de) * 2005-08-17 2010-03-15 Saab Ab Verfahren zur herstellung eines verbundteils mit einem beschlagteil sowie dadurch hergestellter verbundteil
ES2335351T3 (es) * 2005-09-09 2010-03-25 Saab Ab Utilizacion de una herramienta helicoidal y procedimiento de fabricacion de un miembro de superficie que comprende al menos un miembro de refuerzo.
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

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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
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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
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US4198081A (en) * 1973-10-29 1980-04-15 Raychem Corporation Heat recoverable metallic coupling
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US3872573A (en) * 1973-12-19 1975-03-25 Raychem Corp Process and apparatus for making heat recoverable composite couplings
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GB1599999A (en) * 1977-01-24 1981-10-14 Raychem Ltd Heat-recoverable articles
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US4433567A (en) * 1981-11-12 1984-02-28 Grumman Aerospace Corporation Method for working holes

Also Published As

Publication number Publication date
JPS63501004A (ja) 1988-04-14
CA1286582C (en) 1991-07-23
WO1987001650A1 (en) 1987-03-26
EP0237566A1 (en) 1987-09-23
US4675061A (en) 1987-06-23
IL80130A0 (en) 1986-12-31
EP0237566A4 (en) 1988-04-18

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19981001