EP0730519A1 - Giessverfahren und vorrichtung und damit hergestellte produkte - Google Patents

Giessverfahren und vorrichtung und damit hergestellte produkte

Info

Publication number
EP0730519A1
EP0730519A1 EP95902848A EP95902848A EP0730519A1 EP 0730519 A1 EP0730519 A1 EP 0730519A1 EP 95902848 A EP95902848 A EP 95902848A EP 95902848 A EP95902848 A EP 95902848A EP 0730519 A1 EP0730519 A1 EP 0730519A1
Authority
EP
European Patent Office
Prior art keywords
mould
bag
inner core
mould bag
core tool
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.)
Withdrawn
Application number
EP95902848A
Other languages
English (en)
French (fr)
Inventor
Alan Roger Harper
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.)
Individual
Original Assignee
Individual
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
Priority claimed from GB9324345A external-priority patent/GB2284173A/en
Application filed by Individual filed Critical Individual
Publication of EP0730519A1 publication Critical patent/EP0730519A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/38Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/3821Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process composed of particles enclosed in a bag
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/44Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48Moulds 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
    • B29C33/50Moulds 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
    • B29C33/505Moulds 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/44Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48Moulds 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/76Cores

Definitions

  • This invention relates to a method of fabricating an inner core tool for casting, an inner core tool fabricated by the method, a moulding method using such an inner core tool and the products resulting from such use. It is particularly concerned with the casting of hollow items in plastics material such as a glass reinforced polymer.
  • a moulding is made in one piece using a foam core which is slightly smaller than the required outside dimension of the finished component.
  • This foam core is wrapped with glass fibre and placed in a two piece mould. The mould is closed and resin injected to flow between the foam core and the inner mould faces so impregnating the glass fibre. Once the resin has cured the two piece mould is then split apart and the hollow moulding removed.
  • a problem with this process is the cost of manufacturing the foam core and the weight of the core which adds to the weight of the finished product.
  • the method of fabricating an inner core tool is characterised by the further step of incorporating within the mould bag an expanding device so that in use as an inner mould tool for a lost core moulding process the rigidified inner mould tool can be subjected to internal pressurisation by way of the expansion device so as to urge the mould bag outwardly into contact with material juxtaposed with the mould bag.
  • the expansion device comprises a subsidiary inflatable bag; or a capsule containing a pressurised gas, the capsule having a closure adapted to vent the capsule within the mould bag in a controlled manner.
  • the step of causing the mould bag to be drawn into contact with the working surface the or each raised region provides for the creation of a channel in an outer surface of the mould bag by incorporating at least one raised region on the working surface.
  • the step of causing the bag to be drawn into contact with the working surface is achieved by the application of a sub-atmospheric pressure to the working surface by way of ducts through the walls of the mould.
  • the step of filling the interior of the mould bag is undertaken with the interior at substantially atmospheric pressure.
  • the step of filling the interior of the mould bag at least in part with particles involves particles of a substantially similar size.
  • the step of filling the interior of the mould bag at least in part with particles involves the use of particles which vary in size so that the largest are at least twice the size of the smallest.
  • the filling step includes the introduction of non-particulate material which is in filamentary or sheet form.
  • an inner core tool characterised in that it is fabricated according to the method of the first aspect or any preceding preferred version thereof.
  • the inner core tool includes a flexible heater element adapted for heating so as to supply heat as preliminary step of a moulding process in which the inner core tool is to be used.
  • the moulding method for producing a moulded component is characterised by an intermediate step, during or following the step of introducing into the plenum volume polymerisable material, wherein the inner core tool is caused to inflate to enhance contact pressure between particles and the inner side of the mould bag and so between the exterior of the mould bag and material located in the plenum volume.
  • a moulded component fabricated by the use of a lost core inner tool according to the second aspect or the first preferred version thereof.
  • a moulded component fabricated by way of the moulding method of the first aspect.
  • the inner core tool of the present invention is accurately located in a mould.
  • the bag and its filling are separately removed from a cured moulded component through a small aperture provided in the hollow component: the particulate material, being very free flowing, can be poured out and the bag, which can be of thin film, is also readily removed through the aperture.
  • the proposed system provides a number of advantages over existing systems. There is no sacrificial component in the method (except possibly the mould bag which in any event is inherently cheap); no heating is required to remove the core; accurate reproduction of the finished product is facilitated as no significant shrinkage takes place during the evacuating step; an evacuated core is readily obtained at room temperature using low cost tooling; there is no limitation on the size of the evacuated core that can be fabricated and used; and due to the low density of the particulate materials available (such a micro balloons) the weight of the evacuated core is significantly lower than that of the previously known wax or low melt point metal.
  • Figures 1 to 4 is a rigid mould being used to form a rigidified mould bag
  • Figure 5 shows a completed rigidified mould bag located in a working mould for the manufacture of a hollow component
  • Figure 6 shows a moulded hollow component resulting from the working mould of Figure 5.
  • FIGs 1 to 4 variously show the preparation and use of a rigidified mould to produce a hollow moulded component.
  • Split case mould 11 is made up of sections 12, 13 hinged along one side to enable the sections 12, 13 to be hinged apart to give access to interior 14 of the mould 11.
  • Port 15 provides for access to the interior 14 of the mould.
  • Seal 16 bounds moulding surfaces 12 A, 13A once the sections 12, 13 are hinged shut as shown in Figure 1.
  • the moulding surfaces 12A. 13A serve to provide an accurate reproduction of an external surface of a hollow component to be manufactured by way of the mould 11.
  • a number of vacuum ports 16 are provided through the walls of the sections 12, 13 to enable a sub-atmospheric pressure to be applied to the interior 14.
  • Mould 11 is shown closed with a thin walled mould bag 17 hanging in interior 14 of the mould. Interior 18 of the bag 17 communicates with the outside of the mould 13 by way of filling neck 19.
  • Ports 16 in walls of the mould 11 provide for a sub-atmospheric pressure to be applied to cause the outer surfaces of mould bag 17 to be drawn into contact with, and so conform closely to, the moulding surfaces 12A, 13 A. If necessary this effect can be enhanced by provision of a slight overpressure to the interior 18 by way of the neck 19.
  • Figure 3
  • the micro spheres form a mass M which during the filling operation behaves in the manner of a liquid.
  • the mass M is shown filling the interior 18 of the bag 17 to the extent that the bag 17 is fully supported in the vicinity of the mould surface 12 A, 13.
  • a vacuum is applied to the interior 18 of the bag 17 to withdraw air to a sufficient extent to cause the micro balloons forming the mass M to agglomerate to cause the mass M, and so the mould bag 17, to cohere into a rigid component.
  • the filling neck 19 in then sealed off as shown in Figure 4 to preserve low pressure in the interior of the bag 17.
  • the rigidified bag 17 obtained as described in connection with Figure 4 is removed from the mould 11 and has pre-formed glass fibre reinforcement 60 wrapped around it and is then located in the interior 61 of a working mould 62 and aligned to provide a casting plenum 63 between the outside of the bag 17 and inside moulding surface 64. Resin is then injected into the casting plenum 63 to immerse the reinforcement 60 and thereafter having cured form the required hollow fabrication F.
  • the fabrication F is removed from the working mould 62 and aperture 65 is prepared at one end.
  • the bag 17 is cut to vent the interior of the mould bag 17 to atmosphere by way of the atmosphere. This serves to allow the micro balloons making up the mass M to separate slightly from one another and revert to a liquid like behaviour. Consequently the small micro-balloons are readily poured out of the bag 17 by way of aperture 65. Once the micro-balloons have been removed the bag 17 can be withdrawn also. As a result the fabrication F is left hollow. If necessary a filling cap or other closure can be provided for the aperture 65.
  • the exemplary embodiment represents a cheap and readily undertaken method of manufacturing hollow fabrications.
  • the method is readily undertaken without a need for highly trained manufacturing staff and lends itself to production line use and readily provides for both small and large scale production requirements.
  • the exemplary embodiment makes use of a filling of particles of substantially uniform size.
  • the filling can comprise other elements.
  • it can be of particulate material of different sizes.
  • smaller particles can be used for the outer layer of the tool to provided for particularly close conformity of the inner tool surface with the surface to be moulded from when manufacturing the inner core tool and so providing for a high definition of surface for the inner tool in that region.
  • the inner part of the filling is then taken up by particles of larger or much larger size.
  • the filling can include other forms of material such as filamentary or sheetlike material. The only requirement is that whatever filling material is used it must be capable of being withdrawn form the inner core tool through the aperture.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
EP95902848A 1993-11-26 1994-11-28 Giessverfahren und vorrichtung und damit hergestellte produkte Withdrawn EP0730519A1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB9324345 1993-11-26
GB9324345A GB2284173A (en) 1993-02-06 1993-11-26 Collapsible core tool for lost-core moulding
PCT/GB1994/002599 WO1995014563A1 (en) 1993-11-26 1994-11-28 Casting method and apparatus and products thereof

Publications (1)

Publication Number Publication Date
EP0730519A1 true EP0730519A1 (de) 1996-09-11

Family

ID=10745752

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95902848A Withdrawn EP0730519A1 (de) 1993-11-26 1994-11-28 Giessverfahren und vorrichtung und damit hergestellte produkte

Country Status (4)

Country Link
EP (1) EP0730519A1 (de)
AU (1) AU1194595A (de)
BR (1) BR9408141A (de)
WO (1) WO1995014563A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK1109657T4 (da) 1998-07-03 2014-02-10 Siemens Ag Fremgangsmåde til fremstilling af lukkede kompositstrukturer og formapparatur til brug ved fremgangsmåden
SE0200278D0 (sv) * 2002-01-31 2002-01-31 Saab Ab Urtagbar kärna
FR2898539B1 (fr) * 2006-03-20 2008-05-23 Eads Ccr Groupement D Interet Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises
FR2898538A1 (fr) * 2006-03-20 2007-09-21 Eads Ccr Groupement D Interet Procede de realisation de structures de formes complexes en materiaux composites
DE102006031336B4 (de) * 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
DE102006031325B4 (de) 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031335B4 (de) 2006-07-06 2011-01-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031323B4 (de) * 2006-07-06 2010-07-15 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031334A1 (de) 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102012216830A1 (de) * 2012-09-19 2014-03-20 Wobben Properties Gmbh Verfahren zur Herstellung von Windenergieanlagen-Rotorblättern, sowie zur Herstellung eines Formkerns hierfür
EP3159129A1 (de) * 2015-10-22 2017-04-26 Evonik Röhm GmbH Herstellung von komplexen schaum-/ oder sandwichholstrukturen mittels eines formkerns

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2517902A (en) * 1944-08-31 1950-08-08 George C Luebkeman Molding process and means
DE2832566A1 (de) * 1978-07-25 1980-02-07 Bayer Ag Verfahren zur herstellung von hohlkoerpern
JPS5967007A (ja) * 1982-10-11 1984-04-16 Aisin Seiki Co Ltd 樹脂成形用中子の製造方法
US4855011A (en) * 1986-12-12 1989-08-08 United Technologies Corporation Isostatic self-contained bond or mold tool
FR2640188B1 (fr) * 1988-12-14 1991-04-05 Peugeot Procede de realisation par moulage avec noyau extractible d'une piece creuse en matiere plastique et en particulier d'une piece presentant une contre-depouille
FR2649916A1 (fr) * 1989-07-18 1991-01-25 Ferrer Erick Moule universel a surfaces de moulage adaptables pour le moulage de matieres plastiques, ceramiques ou autres materiaux

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9514563A1 *

Also Published As

Publication number Publication date
WO1995014563A1 (en) 1995-06-01
BR9408141A (pt) 1997-08-12
AU1194595A (en) 1995-06-13

Similar Documents

Publication Publication Date Title
US3358062A (en) Molding method for making sealed articles
US3187069A (en) Making foamed articles
US4743481A (en) Molding process for articles having an irregular shaped internal passage
EP0476742B1 (de) Verfahren zum Schlickergiessen von Gegenständen, wie Kunstleder od. dgl., mit zwei oder mehr Farben aus thermoplastischen, Wärmehärterbaren oder elastomeren Kunststoffen in Pulverform und Vorrichtung zur Durchführung des Verfahrens.
US3629030A (en) Method for forming a mandrel and fabricating a duct thereabout
WO1995014563A1 (en) Casting method and apparatus and products thereof
JP5686194B2 (ja) 繊維強化プラスチック構造体の成形方法と車両用ホイール
GB2292332A (en) Moulding process and apparatus
US5639416A (en) Method of molding precision parts
GB2284173A (en) Collapsible core tool for lost-core moulding
JPH06166112A (ja) 皮付き発泡体の成形方法
CN105690791A (zh) 一种易脱模的筒形复合材料结构件整体成型方法
JPS63249616A (ja) 樹脂成形方法
JPS625048B2 (de)
JPH08142060A (ja) 中子の製造方法とその中子及び成形金型
JPS62225309A (ja) 筒状予備形成材の射出型成形の方法と装置
JP4287058B2 (ja) 大容積の容器を製造する方法及び装置
US3566449A (en) Apparatus for molding plastic foam
JP2681730B2 (ja) 皮付き発泡体の成形方法
EP0733330A1 (de) Isolierbehälter aus synthetischem Harz und Verfahren zur Herstellung eines solchen Behälters
JPH0216017A (ja) 流動性反応混合物から成形部品を製造するための方法および金型
JPH06328550A (ja) 複合成形体及びその製造方法
JPS6222351Y2 (de)
JP2784704B2 (ja) 皮付き発泡体の成形装置
JPS61181617A (ja) 樹脂成形品の成形方法

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19960626

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES FR GB IT NL

17Q First examination report despatched

Effective date: 19970822

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19980603