WO1991001871A1 - Procede et appareil de moulage - Google Patents
Procede et appareil de moulage Download PDFInfo
- Publication number
- WO1991001871A1 WO1991001871A1 PCT/GB1990/001149 GB9001149W WO9101871A1 WO 1991001871 A1 WO1991001871 A1 WO 1991001871A1 GB 9001149 W GB9001149 W GB 9001149W WO 9101871 A1 WO9101871 A1 WO 9101871A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- mould tool
- mat
- mould
- perforated
- 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.)
- Ceased
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
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/08—Deep drawing or matched-mould forming, i.e. using mechanical means only
- B29C51/082—Deep drawing or matched-mould forming, i.e. using mechanical means only by shaping between complementary mould parts
-
- 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
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/002—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor characterised by the choice of material
- B29C51/004—Textile or other fibrous material made from plastics fibres
-
- 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
Definitions
- This invention relates to a method of moulding and to apparatus for carrying out the method.
- EP-A-0229441 there is described a method of moulding in which a reinforcement structure, for example of a glass fibre material, is placed between male and female mould tool parts which together define a cavity defining the shape of the moulded article to be produced, and a quantity of a thermosetting resin is then introduced into the mould tool cavity.
- the mould tool parts are then urged towards each other thereby to disperse the thermosetting resin throughout the reinforcement structure.
- the noted steps are carried out at an elevated temperature, for example 55°C, which is maintained after final closing of the mould tool parts together, for a period sufficient to effect curing of the thermosetting resin, after which period the moulded article formed between the mould tool parts can be removed from the mould tool for use or storage for later use.
- preformed dry reinforcements have been produced, for subsequent use in the moulding process.
- the preforms are generally fibrous in nature and have a self-supporting shape that approximates to the shape of the finished article or have a shape which allows them to conform with other preforms before moulding of the finished article.
- preform preparation has often been labour intensive and have involved costly tooling.
- the preforms are manufactured by mechanical press tooling.
- the processes used have not been very flexible, since different match parts have to be produced for each separate reinforcing structure, to enable the presses to mould the required shape.
- the method of the present invention aims to overcome the disadvantages of the prior art by providing a flexible and inexpensive method of producing preformed reinforcement structures.
- the method does not involve elaborate apparatus and is flexible, the same apparatus being used for different mould tools to form a variety of different shaped preformed structures.
- a method of moulding a reinforcing structure for use in a subsequent moulding operation to form a moulded article comprising heating a fibrous mat coated with a thermoformable binder while located between the parts of a mould tool, which parts are precoated with a release agent; bringing the parts of the mould tool together using a vacuum with the mat between them, allowing the mould tool with the fibrous mat therein to cool and removing the moulded reinforcing structure thus formed from the mould tool.
- the present invention further provides a method of preforming a reinforcing structure for embodying in a subsequent moulding operation comprising the steps of; taking a fibrous mat embodying a thermoformable binder; raising the temperature of the mat to render the mat pliable; vacuum forming the mat in a mould tool defining the required shape; and allowing the mat to cool so that the mat becomes self-supporting with the shape defined by the mould tool before removing the mat from the mould tool.
- the fibrous mat can be a continuous filament fibre mat or a woven fibre mat.
- the fibrous mat is initially cut to a template.
- the mould tool is a two-part mould tool and one part of the two-part mould tool defines the required shape of a first side of the mat and the other part defines the required shape of a second side of the mat.
- the parts of the mould used in the method are preferably pre-coated with a PTFE release agent.
- the mat is heated in the mould tool before vacuum forming the mat within said mould tool in an oven.
- the vacuum forming is carried out by the steps of; placing the mat in the mould in a vacuum forming table, which vacuum forming table comprises a perforated table and a lid pivotally attached to said table, said lid comprising a frame and a flexible membrane spanning the area within the frame; bringing the lid and the table into contact; and evacuating the volume enclosed between the lid and the table such that pressure is applied to the mat to mould the mat to shape of the mould tool.
- the mould tool is a two-part mould tool
- the flexible membrane is drawn down on to the mould tool when the volume between the lid and the table is evacuated such that the two-parts of the mould tool are drawn together to mould the mat to shape of the parts.
- the mould tool used preferably comprises a perforated female mould part and a perforated male mould part.
- the perforated female mould is flexible and the male mould ⁇ is made rigid by bonding it to a supporting structure.
- the invention also provides moulding apparatus for use in carrying out a method as hereinbefore described, comprising a perforated mould tool in which the fibrous mat is received; means for heating said mould tool to pre-form the thermoformable material in the mould tool; and vacuum means adapted to receive the mould tool having the fibrous mat therein and operable without further heating to complete moulding of the fibrous mat in the mould tool to form the reinforcing structure.
- the perforated mould tool comprises mutually conforming male and female parts adapted to receive the fibrous mat therebetween.
- the mould tool is preferably of high thermal conductivity and is perforated with holes of up to 5mm diameter and separated from one another by a distance of up to 30 mm from centre to centre of adjacent holes.
- the mould tool can be formed by closing the tool around a prepared reinforcing structure.
- the vacuum means of the apparatus comprises a perforated table, a vacuum chamber disposed beneath said perforated table, a frame pivotally connected to the perforated table, flexible material attached to said frame and spanning the area within said frame and means for evacuating the volume enclosed between the frames and the table when perforated they are brought into contact.
- a reinforcing structure which can be used in a subsequent moulding process during which the reinforcing structure is impregnated with resin, to form a high quality moulded article.
- the invention provides a method of moulding a complete article which comprises initial steps as hereinbefore described and further comprises the steps of placing the moulded reinforcing stucture in a second mould tool of a plurality of parts; introducing thermosetting resin into the cavity defined by the second mould tool; urging the parts of the second mould tool together; curing the materials within the second mould tool; and removing the mould second tool parts after a time sufficient to allow curing of the thermosetting resin.
- Figure 1 shows a quantity of thermoformable material to be formed into a reinforcing structure by the method of the invention
- Figures 2 to 6 show steps in the manufacture of a reinforcing structure by the method of the invention.
- thermoformable material in the form of a sheet 10 of continuous filament fibre matting containing a thermoformable binder.
- a suitable thermoformable material is "UNIFILO U750".
- UNIFILO U750 is a trade mark of Vetrotex International used for a random mat of unchopped continuous glass strands held together with a b_ ier having medium solubility in styrene and other monomers.
- UNIFILO U750 uses a binder of powder polyester of medium solubility in styrene.
- UNIFILO U750 is supplied worldwide and is supplied in the U.S.A. by Certainteed Corporation. A number of such different materials are commercially available.
- Sheet 10 has been cut out according to a template (not shown) to be slightly oversized with respect to the reinforcing structure to be moulded.
- the sheet 10 is located between the rigid male and flexible female part 11 of a two-part, perforated mould tool.
- the female part 11 of the mould tool is then bought together with the loaded male part and, if necessary, clamped or locked to retain the sheet 10 between the mould parts.
- Both the male 12 and female 11 mould parts are perforated and therefore constitute perforated mould tooling. Both parts are pre-coated with a PTFE release agent to facilitate disassembly of the mould tool.
- the perforated mould tooling 11, 12 is placed in an oven and heated to a temperature at which the binder of the thermoformable sheet 10 softens.
- a minimum heating time to achieve a material temperature of 80 degrees Celsius is required. The actual temperature and heating time are determined by the thermoformable binder and type of fibre used in the thermoformable sheet 10, the thickness of the thermoformable sheet 10; and the thermal conductivity of the mould parts 11 and 12.
- thermoformable Sheet 10 pre-forms the thermoformable Sheet 10 to approximately the shape of the void between the male 12 and female 11 mould parts.
- the mould tooling 11, 12 containing the thermoformable sheet 10 is removed from the oven and placed on the lower part 13 of a vacuum forming table 14.
- the hinged lid 15 of the vacuum forming table is then closed, thereby switching on the vacuum pump (not shown) of the vacuum forming table 14 by means of a switch 16, which sustains a minimum vaccuum of 25in Hg (635mm Hg) .
- the lower part 12 of the vacuum forming table is perforated.
- a vacuum chamber is located below the lower part 13 of the table 14. The vacuum pump evacuates the vacuum chamber.
- the vacuum forming table operates without further heating of the mould tooling 11, 12 and thermoformable sheet 10 to draw the sheet 10 into close conformity with the void between the male 12 and female 11 mould parts.
- the vacuum pump is switched off and the mould tool is removed from the vacuum table and left to cool for between thirty seconds and a minute for most articles.
- the mould tool 11, 12 is removed from the vacuum forming table 14 and any protruding parts of the formed reinforcing structure 17 trimmed back to the joint between the male 12 and female 11 mould parts.
- the male and female mould parts are then separated to permit removal of the formed reinforcing structure 17 which can subsequently be used in a moulding process, for example, as described in the above noted EP-A-0229441, in the manufacture of a finished moulded article.
- the male 12 and female 11 parts of the mould tooling are preferably of high thermal conductivity to provide for rapid heating and cooling cycles.
- a suitable material for the mould parts has been found to be a polyester resin containing an aluminium filler. Mould tooling made from this material may itself be formed by closing the mould tool around an existing article which it is required to reproduce.
- a suitable pattern of perforations of the mould tooling is to provide 5mm diameter circular holes having their centres spaced 30mm from one another in a regular pattern over the parts 11, 12 of the mould tooling.
- the male part of the mould tooling is preferably rigid. The desired rigidity can be achieved by bonding a lightweight box structure to the underside of the male part of the tooling.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
L'invention prévoit un procédé qui sert à mouler une structure renforcée et destinée à un usage dans une opération de moulage ultérieure afin de former un article moulé. Le procédé consiste à chauffer une natte fibreuse (10) formée à partir de fibres qui sont maintenues ensemble au moyen d'un liant thermoformable lorsqu'ils se trouvent entre les éléments (11 et 12) d'un outil de moulage, lesquels éléments (11 et 12) sont revêtus d'une sous-couche d'agent de décollage; à réunir les éléments du moule au moyen d'un vide, la natte (10) se trouvant entre lesdits éléments; à permettre à l'outil de moulage, à l'intérieur duquel se trouve la natte fibreuse (10), de se refroidir, puis à enlever la structure renforçante moulée ainsi formée. Les éléments (11 et 12) du moule sont réunis en les plaçant dans une table de formage sous vide (14) puis en enlevant le volume enfermé entre la natte (10) traversant le cadre (15) et la partie inférieure (13) de la table (14) lorsque les deux entrent en contact l'une avec l'autre.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9201248A GB2254037B (en) | 1989-07-27 | 1992-01-15 | Moulding method and apparatus |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB898917142A GB8917142D0 (en) | 1989-07-27 | 1989-07-27 | Moulding method and apparatus |
| GB8917142.5 | 1989-07-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO1991001871A1 true WO1991001871A1 (fr) | 1991-02-21 |
Family
ID=10660697
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/GB1990/001149 Ceased WO1991001871A1 (fr) | 1989-07-27 | 1990-07-25 | Procede et appareil de moulage |
Country Status (3)
| Country | Link |
|---|---|
| GB (1) | GB8917142D0 (fr) |
| MY (1) | MY107064A (fr) |
| WO (1) | WO1991001871A1 (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999048670A1 (fr) * | 1998-03-26 | 1999-09-30 | Lear Corporation | Procede et appareil de moulage de garniture de toit de voiture |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB940407A (en) * | 1961-03-29 | 1963-10-30 | Ford Motor Co | Method of shaping a sheet material containing a heat deformable component |
| GB1024582A (en) * | 1961-07-05 | 1966-03-30 | Rodgers William | A method of manufacturing a synthetic resin moulding reinforced with fibrous material |
| US3559236A (en) * | 1969-12-02 | 1971-02-02 | Glass Reinforced Engineered Ma | Apparatus for molding plastic |
| DE1958110A1 (de) * | 1969-11-19 | 1971-05-27 | Metallgiesserei Und Schilderfa | Verfahren und Vorrichtung zur Herstellung von mattenartigen Gebilden |
| FR2258136A1 (en) * | 1974-01-22 | 1975-08-18 | Fontanille Jean Claude | Hot forming part of a garment containing synthetic material - by forcing into a mould using membrane controlled by fluid pressure |
| FR2567807A1 (fr) * | 1984-07-20 | 1986-01-24 | Bronzavia Sa | Procede pour la realisation de pieces en materiaux composites et dispositif pour la mise en oeuvre de ce procede et pieces obtenues par ce procede |
| US4608220A (en) * | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
| EP0229441A2 (fr) * | 1986-01-10 | 1987-07-22 | Group Lotus Plc | Procédé pour le moulage d'un produit |
| EP0243617A2 (fr) * | 1986-05-02 | 1987-11-04 | AlliedSignal Inc. | Procédé de fabrication de matériaux composites renforcés par des fibres |
| US4842787A (en) * | 1986-12-22 | 1989-06-27 | Xerkon, Inc. | High speed process for production of oriented structural yarn/polymer matrix composite structural parts |
-
1989
- 1989-07-27 GB GB898917142A patent/GB8917142D0/en active Pending
-
1990
- 1990-07-25 WO PCT/GB1990/001149 patent/WO1991001871A1/fr not_active Ceased
- 1990-07-26 MY MYPI90001258A patent/MY107064A/en unknown
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB940407A (en) * | 1961-03-29 | 1963-10-30 | Ford Motor Co | Method of shaping a sheet material containing a heat deformable component |
| GB1024582A (en) * | 1961-07-05 | 1966-03-30 | Rodgers William | A method of manufacturing a synthetic resin moulding reinforced with fibrous material |
| DE1958110A1 (de) * | 1969-11-19 | 1971-05-27 | Metallgiesserei Und Schilderfa | Verfahren und Vorrichtung zur Herstellung von mattenartigen Gebilden |
| US3559236A (en) * | 1969-12-02 | 1971-02-02 | Glass Reinforced Engineered Ma | Apparatus for molding plastic |
| FR2258136A1 (en) * | 1974-01-22 | 1975-08-18 | Fontanille Jean Claude | Hot forming part of a garment containing synthetic material - by forcing into a mould using membrane controlled by fluid pressure |
| FR2567807A1 (fr) * | 1984-07-20 | 1986-01-24 | Bronzavia Sa | Procede pour la realisation de pieces en materiaux composites et dispositif pour la mise en oeuvre de ce procede et pieces obtenues par ce procede |
| US4608220A (en) * | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
| EP0229441A2 (fr) * | 1986-01-10 | 1987-07-22 | Group Lotus Plc | Procédé pour le moulage d'un produit |
| EP0243617A2 (fr) * | 1986-05-02 | 1987-11-04 | AlliedSignal Inc. | Procédé de fabrication de matériaux composites renforcés par des fibres |
| US4842787A (en) * | 1986-12-22 | 1989-06-27 | Xerkon, Inc. | High speed process for production of oriented structural yarn/polymer matrix composite structural parts |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6146578A (en) * | 1997-10-09 | 2000-11-14 | Lear Corporation | Method for molding headliners |
| WO1999048670A1 (fr) * | 1998-03-26 | 1999-09-30 | Lear Corporation | Procede et appareil de moulage de garniture de toit de voiture |
Also Published As
| Publication number | Publication date |
|---|---|
| MY107064A (en) | 1995-09-30 |
| GB8917142D0 (en) | 1989-09-13 |
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