GB2319205A - Process for the manufacture of a mould tool - Google Patents

Process for the manufacture of a mould tool Download PDF

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Publication number
GB2319205A
GB2319205A GB9623587A GB9623587A GB2319205A GB 2319205 A GB2319205 A GB 2319205A GB 9623587 A GB9623587 A GB 9623587A GB 9623587 A GB9623587 A GB 9623587A GB 2319205 A GB2319205 A GB 2319205A
Authority
GB
United Kingdom
Prior art keywords
bolster
layer
skin
tooling
shim
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.)
Granted
Application number
GB9623587A
Other versions
GB2319205B (en
GB9623587D0 (en
Inventor
Alan Roger Harper
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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
Application filed by Individual filed Critical Individual
Priority to GB9623587A priority Critical patent/GB2319205B/en
Publication of GB9623587D0 publication Critical patent/GB9623587D0/en
Publication of GB2319205A publication Critical patent/GB2319205A/en
Application granted granted Critical
Publication of GB2319205B publication Critical patent/GB2319205B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • B29C33/3842Manufacturing moulds, e.g. shaping the mould surface by machining
    • B29C33/3857Manufacturing moulds, e.g. shaping the mould surface by machining by making impressions of one or more parts of models, e.g. shaped articles and including possible subsequent assembly of the parts
    • 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
    • B29C33/56Coatings, e.g. enameled or galvanised; Releasing, lubricating or separating agents
    • B29C33/565Consisting of shell-like structures supported by backing material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2883/00Use of polymers having silicon, with or without sulfur, nitrogen, oxygen, or carbon only, in the main chain, as mould material

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

Mould tooling is manufactured by a process comprising (a) forming a skin layer 12 on the surface of a master pattern 11; (b) depositing a wax calibration layer 13 over the skin layer; (c) depositing a bolster layer 14 of heat insulating material over the calibration layer; (d) shrouding the exposed face of the bolster layer with a frame 15 and filling the thus formed plenum with aggregate 16 providing thermal insulation between the bolster layer and the bolster frame; (e) separating the pattern with the attached skin layer from the bolster assembly, removing the calibration layer 13 from the exposed surface of the bolster layer, applying mould release means to that surface and relocating the pattern and skin layer on the bolster assembly; (f) introducing shim-forming plastics material into the space between the skin layer and the bolster surface; (g) separating the pattern from the rest of the assembly and the skin layer and shim from the bolster assembly; (h) removing the release means from the bolster surface and (i) locating the skin on the shim in the bolster to provide the tool.

Description

TOOLING This invention relates to tooling. It is particularly concerned with the manufacture of moulding tools.
It is known to manufacture moulding tools in the form of composite moulds based on low mass heated or unheated high temperature composite skins with integral cores. The skins and cores are supported by way of shim profiled and suitably shaped steel frame bolsters.
A composite mould can make use of a metal faced mould. The metal can be deposited as a skin by metal spraying, sheet forming, casting or machining. By whatever means are used to provide a skin the metal thickness is kept to a minimum and is cradled in a well supported elastomeric material including an embedded heater. It is supported as a skin adapted for high temperature operation and steel support frames to provide for readily matchable mould sets.
As originally conceived solid bonding of the skin to the supporting frame reduced, if it did not actually prevent, allowance for movement between skin and frame to provide for a degree of relative movement between shin and frame arising from differential expansion due to different coefficients of thermal expansion between frame and skin.
According to one aspect of the present invention there is provided a process for the manufacture of tooling comprising the use of a thin skin mould supported in a bolster by way of an elastomeric shim over its entire undersurface which is in turn supported on an in-fill in the bolster wherein the thin skin is of at least one of the following: vacuum formed thermoplastic sheet; metal sheet however formed; cast metal skin; ceramic skin however formed; silicone or similar elastomeric matrix skin however formed; thermoset reinforced or un-reinforced skin however formed.
The skin can be of composite construction (that is to say of two or more layers) formed to receive the elastomeric shim.
An exemplary embodiment of the invention will now be described with reference to the accompanying drawings of a skin tooling process of which each figure is a section of a during a working step in the process. The steps proceed in sequence and chronological order.
Figure 1 show a prepared master pattern 11 for the manufacture of a bowl shaped object with a bowl region 11A, sides 11B and rim 11C.
Figure 2 shows the addition of a high temperature heat resistant thin skin 12 to the master pattern 11 in the form of a lamination to a thickness of 2 - 5 mm. In this case the skin is of thermoset material but, as will be touched on later, a wide variety of skin materials can be used typically depending on what product is to be moulded.
Figure 3 shows a calibration layer 13 (typically of wax) of some 2 - 3 mm thickness Figure 4 shows a bolster skin 14 incorporating a heating system (in this case an electric mesh heater). For a particular application this layer 14 can also include a cooling system.
Figure 5 shows a bolster frame 15 is the form of a box placed over encompassing the master pattern 11 along with skin 12, layer 13 and bolster skin 14.. With a more elaborate pattern or one with double curvature the frame 15 can be profiled in form to reduce in-fill volume. The bolster frame 15 includes dowels and clamp points 15A, 15B providing for accurate alignment of this portion of tooling with a complementary component to make up an accurately alignable mould set.
The bolster frame 15 is shuttered and filled with low cost filler aggregate 16. The in-fill has a high heat insulation value to maintain lower thermal mass. In this case low cost blown clay is used but other materials can be used such as glass balloons in a 'dry' matrix mix including air as further insulant.
Figure 6 shows the completed assembly inverted and with the pattern 11 removed together with skin 12 attached temporarily to the pattern around its periphery 12A.
The calibration layer 13 is then removed.
Figure 7 shows the pattern 11 with skin 12 attached by way of its periphery 12A to the pattern 11 having had a release agent deposited on inner side 14A of bolster skin 14. The pattern 11 with skin 12 is then replaced in the bolster frame 15. The frame 15 is clamped to hold the frame 15 in accurate registration with pattern 11.
Figure 8 shows the stage in the process where resin has been injected into the gap between the pattern 11 and the inner side 14A of the bolster skin 14 to create a bedding shim 17 between the released film bolster surface 14 and the rear 12A of the mould face skin 12.
Figure 9 shows the dis-assemby of the thrree main compontnes from one another in their final form. Pattern 11 is shown lifted clear with no attachments. Tailored skin 12 with its adhering bedding shim 17 is shown lifted clear of frame 15 with its bolster skin 12. The skin 12/shim 17 combination can be stored in a suitable support or restored to bolster frame 15 for use in production. Once the bedding shim 17 has cured it adheres to the skin 12 and the profiled bolster and frame 15 is released from the pattern 11 (Figure 9) to enable the skin with its adhering bedding shim 17 to be removed as a unit as shown in Figure 9.
In other embodiments the skin and bedding shim can be separated by one or more intermediate layers to provide a composite construction made up of one or more intermediate on which the skin and the bedding shim are mounted to serve as the outer faces.
The thin skin and its bedding shim are readily moved as a unit from the bolster and then be returned to it while providing for the ready and accurate re-alingment of the skin within the bolster.
The bolster 14 van be combined with another bolster equipped by measn of a similar tool so as to provide matching closed mould set.
A wide range of variants based on the above basic process are possible under the present invention.
1 During production use the edges of the skin 12 can be sealed to the edge of bolster 14 to provide for a vacuum lock to hold the skin to the matching bolster face. It is likely to be necessary for an upper mould of the thin skinned type to be positively retained in its bolster least it should fall out when the upper bolster is raised. This can be by a vacuum lock or by a material such as Velcro (RTM) mounted in recsses in the bolster to insure that the material does not cause local distortion of the thin skin.
2 When creating similar tooling skin from matching mould half the vacuum lock referred to in 1 above can be used to ensure that any slight distortion in a tailored skimmed face skin is not replicated in the second mould half skin.
3 The use of dry packed aggregate to in-fill the bolster provides for a much higher degree of thermal insulation to be applied to a mould face than has be possible heretofore. This renders the effect of operating any heating element net incorporated in for example layer 14 to be increased in efficiency. In addition a labyrinthine path can be created in the bolster directly behind the bolster face to provide for relatively simple and effective air cooling to be used rather than liquid cooling techniques (though liquid cooling may be appropriate and can be incorporated in a thin skin mould procees).
4 The locking shim 17 requires to be of low, is not zero, shrinkage so as not to distort the working skin when the shim cures.
5 For maximum output the working skins and their bedding shim can eadily be removed from their bolster and temporarily stored in holding jigs when, for example, gel coatings are being sprayed on or fibre packs are being inserted (or indeed both). These holding jigs can usefully incorporate heater cloths or nets to maintain background temperature whilst the production skin is out of the production bolster. In this way the loaded skin is prepared and ready at or near production temperatures.
6 The proposed process enables 'smart' tooling operations to be undertaken.
Typically after resin has been injected into the mould a consolidating pressure can be introduced between bolster and skin to provide for a fractional squeeze the sealed resin impregnated cavity.
The exemplary embodiment refers to the use of a skin of conventional thermoset resins laminated with reinforcements as generally used in the GRP/components industry. However this skin, designed to fit a shaped "solid bolster could be made from a variety of materials, and as such also made in a different way from my example. The following are offered by way of example: Thermoplastic sheet, vacuum formed; Metal sheet, panel beaten to shape or pressed into shape for example hydraformed; Metal shin, cast into shape; Ceramic skin, pour moulded or pressed into shape; Silicone or similar elastomeric matrix skin, cast, pressed or fabricated into shape; Thermoset reinforced or un reinforced skin, pressure injected into shape; Any suitable formable or mouldable material processed by whatever means into shape to form the mould skin.
The present invention provides for low cost tooling or mould construction by considering the possibilities arising from skin tooling rather than depending on existing solid conventional tooling build concepts.
Other features of the invention contrasting with existing processes include: the provision of a process providing for reduction in mould material cost; reduction in mould building labour cost; faster mould production; maintenance of high quality mould.part surface due to thin skin homgeneity.
The process also provides for a user of the process and moulds and tools produced by it in contrast to extsting systems: quicker first off moulding; multiple tooling faces without normal multiple costs; mould face renewal at low cost; less tooling capital outlay; higher production voulmes with little or no increased capital expenditure; greater capitalisation of tooling investment; and low cost skin renewal.

Claims (12)

CLAIMS 1A process for the manufacture of tooling comprising the use of a thin skin mould supported in a bolster by way of an elastomeric shim over the entire under surface of the mould which shim is in turn supported on an in-fill in the bolster wherein the thin skin is of at least one of the following: vacuum formed thermoplastic sheet; metal sheet however formed; cast metal skin; ceramic skin however formed; silicone or similar elastomeric matrix skin however formed; thermoset reinforced or un-reinforced skin however formed. 2 A process as claimed in Claim 1 wherein the thin skin is of composite construction, that is to say of two or more layers, formed to receive the elastomeric shim. 3 A process for the manufacture of tooling characterised by the steps of:
1 forming on a surface of a master pattern member a skin layer by casting or laminating of plastics material; the skin layer during this stage having an inner face contacting the member and an exposed outer face;
2 depositing on the exposed face of the skin layer a calibration layer of substantially uniform thickness of a material such as wax; the calibration layer during this step having an inner face contacting the skin and an exposed outer face;
3 depositing on the exposed face of the calibration layer a bolster layer of a heat insulating material optionally including means whereby the bolster layer can be heated or cooled or providing for both heating and cooling relative to ambient temperature;
4 shrouding the exposed face of the bolster layer by way of a bolster frame so as to provide between the exposed face of the bolster layer and an inner face of the bolster frame a plenum;
5 filling the plenum with an aggregate material providing for thermal insulation between the bolster layer and the bolster frame;
6 separating the pattern with the skin layer retained thereon from the assembled bolster frame, bolster layer and calibration layer;
7 removing the calibration layer to expose the inner face of the bolster layer;
8 provide a release means on the exposed inner surface of the bolster layer;
9 relocate the pattern with the skin layer retained thereon into the assembled bolster frame and bolster layer;
10 inject or otherwise locate in the volume left on removal of the calibration layer between the exposed face of the skin layer and the exposed inner surface of the bolster layer a plastics material to provide a locking shim reproducing the exposed face of the skin layer; and
11 separating the pattern from the remainder of the assembly when formation of the locking shim is complete;
12 A process as hereinbefore described with reference to the accompanying drawings.
12 removing the release means from the bolster layer;
13 locating the skin on the locking shim in the bolster to provide the tool comprising the skin layer releaseably mounted on the bolster layer by way of the locking shim and the bolster layer retained in the bolster frame.
4 A process as claimed in Claim 3 including the step of causing periphery of the skin layer to be sealed to a complementary region of the bolster layer to enable a pressure differential to be provided, such as by evacuation, to improve retention of skin layer on bolster layer.
5 A process as claimed in Claim 3 wherein the skin layer is retained in place on the bolster layer at least in part by the use of separable contact material such as 'Velcro' (RTM).
6 A process as claimed in any of preceding claims 3 to 5 wherein the skin layer is formed from a silicone based material.
7 An article of tooling manufactured by a process as claimed in any preceding claim when used in a production process.
8 An article of tooling as claimed in Claim 7 when used in conjunction with a further article of tooling also manufactured by a process as claimed in any of preceding claims 1 to 6.
9 An article of tooling as claimed in Claim 7 or 8 when used in conjunction with at least one further bolster member serving as a holding jig for the skin layer while the skin layer is released and outside the tool.
10 An article of tooling as claimed in Claim 9 wherein the or each furtehr bolster member is equipped with heating means to provide for heating of the skin when located on the furtehr bolster.
11 A component of plastics material manufactured by means of a tool manufactured by the process of Claims 1 to 6 or by an article of tooling as claimed in Claims 7 to 10.
GB9623587A 1996-11-13 1996-11-13 Tooling Expired - Fee Related GB2319205B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9623587A GB2319205B (en) 1996-11-13 1996-11-13 Tooling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9623587A GB2319205B (en) 1996-11-13 1996-11-13 Tooling

Publications (3)

Publication Number Publication Date
GB9623587D0 GB9623587D0 (en) 1997-01-08
GB2319205A true GB2319205A (en) 1998-05-20
GB2319205B GB2319205B (en) 2001-06-13

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999007532A2 (en) * 1997-08-08 1999-02-18 Ciba Specialty Chemicals Holding Inc. Metal-coated plastic mould tool
WO2001094089A1 (en) * 2000-06-06 2001-12-13 Plastech Thermoset Tectonics Limited Moulding tooling
EP1254751A1 (en) * 2001-05-03 2002-11-06 Puma Stampi di Bisonni Umberto & C.S.N.C. Casting process for the realisation of light moulds used to produce thermoformed articles
GB2435848A (en) * 2006-02-15 2007-09-12 Advanced Composites Group Ltd Mould skins
US7883657B2 (en) 2002-09-25 2011-02-08 Airbus Uk Limited Method for joining aircraft components
CN102873800A (en) * 2012-10-18 2013-01-16 山东双一集团有限公司 Method for carrying out vacuumized manufacturing on upper dies by using light resin transfer molding process
US11370149B2 (en) * 2017-07-18 2022-06-28 Frimo Group Gmbh Method for producing a negative skin, and tool

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB738403A (en) * 1951-12-21 1955-10-12 Philips Nv Improvements in or relating to methods of securing electrolytic deposited metal skins and matrices manufactured by such methods
GB900570A (en) * 1957-12-20 1962-07-11 Bristol Aeroplane Plastics Ltd Improvements relating to moulds
GB923321A (en) * 1958-07-11 1963-04-10 Oscar James Gagne Improvements in and relating to the production of metal clad articles
GB1245724A (en) * 1969-03-01 1971-09-08 Maria-Edith Leowald Moulds having electrodeposited moulding surfaces
EP0117985A2 (en) * 1983-02-07 1984-09-12 Alban Pütz Method of producing moulds for injection moulding, particularly tools for the injection moulding of plastic materials

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB738403A (en) * 1951-12-21 1955-10-12 Philips Nv Improvements in or relating to methods of securing electrolytic deposited metal skins and matrices manufactured by such methods
GB900570A (en) * 1957-12-20 1962-07-11 Bristol Aeroplane Plastics Ltd Improvements relating to moulds
GB923321A (en) * 1958-07-11 1963-04-10 Oscar James Gagne Improvements in and relating to the production of metal clad articles
GB1245724A (en) * 1969-03-01 1971-09-08 Maria-Edith Leowald Moulds having electrodeposited moulding surfaces
EP0117985A2 (en) * 1983-02-07 1984-09-12 Alban Pütz Method of producing moulds for injection moulding, particularly tools for the injection moulding of plastic materials

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999007532A2 (en) * 1997-08-08 1999-02-18 Ciba Specialty Chemicals Holding Inc. Metal-coated plastic mould tool
WO1999007532A3 (en) * 1997-08-08 1999-04-15 Ciba Geigy Ag Metal-coated plastic mould tool
WO2001094089A1 (en) * 2000-06-06 2001-12-13 Plastech Thermoset Tectonics Limited Moulding tooling
EP1254751A1 (en) * 2001-05-03 2002-11-06 Puma Stampi di Bisonni Umberto & C.S.N.C. Casting process for the realisation of light moulds used to produce thermoformed articles
US7883657B2 (en) 2002-09-25 2011-02-08 Airbus Uk Limited Method for joining aircraft components
GB2435848A (en) * 2006-02-15 2007-09-12 Advanced Composites Group Ltd Mould skins
CN102873800A (en) * 2012-10-18 2013-01-16 山东双一集团有限公司 Method for carrying out vacuumized manufacturing on upper dies by using light resin transfer molding process
CN102873800B (en) * 2012-10-18 2014-08-20 山东双一集团有限公司 Method for carrying out vacuumized manufacturing on upper dies by using light resin transfer molding process
US11370149B2 (en) * 2017-07-18 2022-06-28 Frimo Group Gmbh Method for producing a negative skin, and tool

Also Published As

Publication number Publication date
GB2319205B (en) 2001-06-13
GB9623587D0 (en) 1997-01-08

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20101113