[go: up one dir, main page]

GB2126148A - Mould making - Google Patents

Mould making Download PDF

Info

Publication number
GB2126148A
GB2126148A GB08303688A GB8303688A GB2126148A GB 2126148 A GB2126148 A GB 2126148A GB 08303688 A GB08303688 A GB 08303688A GB 8303688 A GB8303688 A GB 8303688A GB 2126148 A GB2126148 A GB 2126148A
Authority
GB
United Kingdom
Prior art keywords
pattern
mould
wax
resin material
synthetic resin
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Withdrawn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
GB08303688A
Other versions
GB8303688D0 (en
Inventor
Ivan John Birch
Michael John Jago
Keith Leonard Mitchell
John Edwin Guest
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB08303688A priority Critical patent/GB2126148A/en
Publication of GB8303688D0 publication Critical patent/GB8303688D0/en
Publication of GB2126148A publication Critical patent/GB2126148A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns
    • B22C9/043Removing the consumable pattern

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

A method of removing polystyrene foam from a composite polystyrene/wax pattern in a mould is described using superheated steam. The polystyrene foam shrinks on heating to allow expansion of the wax. The pattern shown in Figure 1 comprises large volume runners and risers 2, 4 which are made from expanded polystyrene foam while the pattern 6 requiring higher accuracy is made from wax. In an alternative embodiment a pattern comprises expanded polystyrene around which wax is injected in a die to form a coating. <IMAGE>

Description

SPECIFICATION Mould making This invention relates to the making of moulds for the casting of components.
In the conventional "lost wax" process of making a mould there is first fabricated a wax structure consisting of a representation of the component to be cast, together with the necessary feeder and runner passages required for casting. A body of refractory ceramic material such as Silica with a chemical binding agent is then built up around the wax structure and the wax is removed or "lost" (e.g. by heating so as to melt the wax) to leave a mould with internal cavities defining the component and feeder and runner passages.
Difficulties arise in the handling of such wax structures because of their high overall weight, since the volumes required for the feeder and runner passages may, especially in the case of components having larger cross-sectional areas, or in multi-component moulds, be relatively large in order to minimise the introduction of undesirable properties in the material of the finished component.
It has been proposed that, in order to facilitate handling of structures for defining mould cavities, the portions of the structure which may have a large volume and do not require such high dimensional stability and such good surface finish as the component portion (e.g. the feeder and runner passage portions) be made from an expanded synthetic resin material such as expanded polystyrene which is considerably lighter than wax. However, the use of polystyrene as part of a structure in this way has been hindered by the difficulty of removing it from the mould.
It has been proposed to use a chemical solvent to remove the polystyrene but the required solvents are chlorinated hydrocarbons which are hazardous to use since they are toxic and often inflammable. It has also been proposed to vaporise the polystyrene from the mould when pouring the molten material to cast the component, but this is not possible where wax has to be removed from the mould since the wax must be removed before the mould is used for casting. It has also been proposed that the polystyrene be burnt out of the mould when the mould is fired, but again this is not desirable where the mould contains wax since the wax expands and may crack the mould.
It is one object of the present invention to provide a method of removing an expanded synthetic resin material from a mould whereby the above disadvantages may be overcome.
Another problem which arises with the use of an expanded synthetic resin material, such as expanded polystyrene, is the difficulty of securely attaching the wax patterns which form the casting cavities, to the polystyrene runner system.
It is a further object of the invention to provide a lightweight composite mould pattern including an expanded synthetic resin material to which additional wax pattern can be securely attached by conventional methods.
In accordance with the invention as claimed in the appended claims, synthetic resin material, which either wholly or partially forms a pattern for a casting mould, is removed from a casting mould by subjecting the mould to a superheated steam environment.
We have found that the expanded synthetic resin material, and in particular expanded polystyrene, shrinks to a fraction of its volume when contacted by superheated steam. This reduction in volume allows room for any wax parts of a composite pattern material to expand without cracking the surrounding mould material and thus makes possible the provision of lightweight composite moulds using both wax and expanded synthetic resin materials.
A preferred lightweight material is expanded polystyrene and this can be used in various forms, for example a foam, or a plurality of small beads held together in a binder.
The pressure and temperature of the superheated steam are not critical since expanded polystyrene shrinks significantly at temperatures above 1 00 C. For rapid removal of both wax and polystyrene, however, it is preferable to use superheated steam at elevated pressure and this is conveniently carried out in a steam autoclave.
When the expanded polystyrene has shrunk in volume to an acceptable extent, usually down to a small compact lump, it may be removed bodily from the mould, or the mould may be further subjected to the high pressure steam environment to evaporate it completely from the mould.
Alternatively, the remaining compact lump of polystyrene can be left in the mould to be vaporised when the mould is fired to sinter it before casting.
In one preferred form of composite wax and synthetic resin mould, expanded polystyrene is used as a lightweight chill around which a conventional wax pattern material is injected in a die to form a runner system. Additional wax patterns of the desired cast article can then be simply joined to the wax outer surface of the runner by a conventional technique of using a hot knife to melt the surfaces to be joined.
Examples of the present invention, including composite patterns and a method of removing them from casting moulds, will now be more particularly described with reference to the accompanying drawings in which: Figures 1 and 2 illustrate one form of composite pattern for casting turbine blades for gas turbine engines, and, Figures 3 and 4 illustrate an alternative form of composite pattern for casting other components for a gas turbine engine.
Referring now to Figures 1 and 2, there is shown a lightweight composite pattern for making a mould for casting turbine blades. The pattern consists of four vertical runners 2 interconnected at their bases by horizontal runners 4 and 5 at the base and top respectively and all of which are made from expanded polystyrene foam formed into a die of appropriate shape. Attached to the runner system are eight wax patterns 6 of turbine blades. The wax patterns are attached by melting the surfaces of the patterns and pressing them into position, or by means of a wax or other resin adhesive.
In order to provide a smooth surface on the runner and to aid in the attachment of the wax patterns 6, it may be dip-coated in a suitable resin or wax, or may be placed in a further die into which wax is injected to provide a thin, smooth coating over its surfaces. Preferably one surface of the polystyrene forming the horizontal runner 4 is left uncoated for ease of removal of the polystyrene.
In order to form a casting mould from the composite pattern, it is coated in conventional manner (e.g. by dipping) with a slurry of refractory ceramic material (e.g. Silica in a suitable binder) which is built up in layers and dried.
In order to remove the pattern, the mould is placed in a steam autoclave so that the uncoated surface of the expanded polystyrene is exposed to superheated steam at a temperature of approximately 1 700C and a temperature of 7 bars.
At this temperature and pressure the expanded polystyrene rapidly shrinks down to a small fraction of its expanded size allowing room for expansion of the wax portions of the pattern as the wax heats up to its melting temperature, and allowing a passage for the melted wax to run out of the mould. Any polystyrene remaining in the mould may either be physically removed, or the mould may be left in the autoclave until the polystyrene completely evaporates. Alternatively, the polystyrene may be left in the mould to be burned out when the mould is fired.
The temperature and pressure of the steam in the autoclave may vary widely, the main criteria being that the steam should cause shrinking of the polystyrene before significant heating and expansion of the wax takes place through the mould walls. The optimum for any pattern arrangement can be simply established by experiment.
Figures 3 and 4 show a different composite pattern in which expanded polystyrene is used as a lightweight chill to reduce the weight of a runner system of relatively large dimensions. In this arrangement the runner system includes a pouring cup 10 feeding horizontal runners 12 down each side and transverse runners 14. The runners are arranged to feed three casting cavities.
This pattern is made first by forming a chill in a die from expanded polystyrene beads held together in a low temperature binder and subsequently placing the chill in a second die and injecting wax into the die to surround the chill on all but one surface to a thickness of about 0.0625 in. The surface left uncoated is usually the surface 1 5 which forms the opening of the pouring cup 10.
The casting cavities are defined by wax patterns (not shown) which are joined to the runner system at the three square surfaces 1 6.
Recesses 18, 20 are formed in the surfaces 1 6 into which projections on the wax patterns fit for location of the wax pattern on the runner system.
Because the surface of the runner is wax, it is a simple matter to join the wax pattern to the square surfaces 1 6 by a conventional hot knifing technique.
To form a casting mould from this lightweight composite pattern, it is simply invested in ceramic slurry as is common practice. The pattern is removed, as described above, by placing the dried mould in an autoclave and exposing the polystyrene to superheated steam at appropriate temperature and pressures (e.g. 1 700C and 7 bars), whereupon it shrinks down to a fraction of its volume and allows the wax first of all to expand on heating and then to run out.

Claims (12)

1. A method of making a casting mould comprising the steps of: making a pattern for defining a cavity in the mould, said pattern being formed wholly or in part from an expanded synthetic resin material.
coating the pattern with refractory material leaving part of the pattern surface exposed, and, removing the pattern, characterised in that the step of removing the pattern includes subjecting the mould containing the pattern to a superheated steam environment to shrink the expanded synthetic resin material.
removing the pattern, characterised in that the step of removing the pattern includes subjecting the mould containing the pattern to a superheated steam environment to shrink the expanded synthetic resin material.
2. A method as claimed in Claim 1 and in which the expanded synthetic resin material comprises polystyrene foam.
3. A method as claimed in Claim 1 and in which the expanded synthetic resin material comprises beads of expanded polystyrene in a binder.
4. A method as claimed in Claim 1 and in which the mould is subjected to superheated steam until the expanded resin material has reduced in volume to the extent that it can be physically removed from the mould.
5. A method as claimed in Claim 4 and in which the mould is further subjected to superheated steam until the resin material has completely vaporised.
6. A method as claimed in Claim 1 and in which the pattern is a composite pattern comprising a portion made from an expanded synthetic resin material and a portion made from wax joined together.
7. A method as claimed in Claim 6 and in which the portion made from an expanded synthetic resin material is coated with a wax or resin material to which the portion made from wax is joined.
8. A composite pattern for making a casting mould comprising a portion made from wax and a portion made from an expanded synthetic resin material joined together.
9. A composite pattern for making a casting mould comprising a portion made from an expanded synthetic resin material and coated with wax.
10. A composite pattern as claimed in Claim 8 or Claim 9 and in which the expanded synthetic resin material is polystyrene.
11. A method of making a casting mould substantially as hereinbefore particularly described with reference to the accompanying drawings.
12. A composite pattern for making a casting mould substantially as hereinbefore particularly described with reference to the accompanying drawings.
GB08303688A 1982-02-18 1983-02-10 Mould making Withdrawn GB2126148A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08303688A GB2126148A (en) 1982-02-18 1983-02-10 Mould making

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8204795 1982-02-18
GB08303688A GB2126148A (en) 1982-02-18 1983-02-10 Mould making

Publications (2)

Publication Number Publication Date
GB8303688D0 GB8303688D0 (en) 1983-03-16
GB2126148A true GB2126148A (en) 1984-03-21

Family

ID=26282013

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08303688A Withdrawn GB2126148A (en) 1982-02-18 1983-02-10 Mould making

Country Status (1)

Country Link
GB (1) GB2126148A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4651799A (en) * 1986-01-30 1987-03-24 Hitchiner Manufacturing Co., Inc. Vented casting molds and process of making the same
GB2213762A (en) * 1987-12-22 1989-08-23 Steel Castings Res Manufacture of ceramic shell moulds
US4940072A (en) * 1989-05-31 1990-07-10 Air Products And Chemicals, Inc. Removing pattern material from investment casting molds
EP0499486A3 (en) * 1991-02-14 1992-10-14 E.I. Du Pont De Nemours And Company Investment casting method and pattern material
US7204296B2 (en) 2004-07-26 2007-04-17 Metal Casting Technology, Incorporated Method of removing a fugitive pattern from a mold

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB948197A (en) * 1961-07-20 1964-01-29 Monsanto Chemicals Production of shell moulds
GB1023829A (en) * 1963-07-16 1966-03-23 Monsanto Chemicals Production of shell moulds
GB1034617A (en) * 1965-03-13 1966-06-29 Ford Motor Co Methods of making cores for castings
GB1048720A (en) * 1963-12-04 1966-11-16 Rolls Royce Improvements in or relating to shell moulds for castings
GB1076198A (en) * 1966-02-09 1967-07-19 Meehanite Metal Corp Improved casting method
GB1125124A (en) * 1965-09-06 1968-08-28 Howe Sound Company Superalloy Improved mould and methods for its production and for its use in precision casting
GB1233889A (en) * 1969-06-06 1971-06-03

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB948197A (en) * 1961-07-20 1964-01-29 Monsanto Chemicals Production of shell moulds
GB1023829A (en) * 1963-07-16 1966-03-23 Monsanto Chemicals Production of shell moulds
GB1048720A (en) * 1963-12-04 1966-11-16 Rolls Royce Improvements in or relating to shell moulds for castings
GB1034617A (en) * 1965-03-13 1966-06-29 Ford Motor Co Methods of making cores for castings
GB1125124A (en) * 1965-09-06 1968-08-28 Howe Sound Company Superalloy Improved mould and methods for its production and for its use in precision casting
GB1076198A (en) * 1966-02-09 1967-07-19 Meehanite Metal Corp Improved casting method
GB1233889A (en) * 1969-06-06 1971-06-03

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4651799A (en) * 1986-01-30 1987-03-24 Hitchiner Manufacturing Co., Inc. Vented casting molds and process of making the same
GB2213762A (en) * 1987-12-22 1989-08-23 Steel Castings Res Manufacture of ceramic shell moulds
US4940072A (en) * 1989-05-31 1990-07-10 Air Products And Chemicals, Inc. Removing pattern material from investment casting molds
EP0499486A3 (en) * 1991-02-14 1992-10-14 E.I. Du Pont De Nemours And Company Investment casting method and pattern material
US7204296B2 (en) 2004-07-26 2007-04-17 Metal Casting Technology, Incorporated Method of removing a fugitive pattern from a mold

Also Published As

Publication number Publication date
GB8303688D0 (en) 1983-03-16

Similar Documents

Publication Publication Date Title
US4434835A (en) Method of making a blade aerofoil for a gas turbine engine
US5176864A (en) Lost wax process utilizing a high temperature wax-based material
US4617977A (en) Ceramic casting mould and a method for its manufacture
US4691754A (en) Method for forming castings having inserts
JPH1029053A (en) Production of alloy structural body and alloy casting mold
US4655276A (en) Method of investment casting employing microwave susceptible material
JP2001511719A (en) Metal perfect dense mold and method of forming parts
JPH0214137B2 (en)
US4682643A (en) Method of producing molded parts and casting pattern therefor
GB2126148A (en) Mould making
JP3133077B2 (en) Ceramic mold forming method using thermoreversible material
US4356859A (en) Lost wax feeder and runner systems
US3254379A (en) Expendable molding shape for precision casting
US3114948A (en) Investment casting apparatus and method
JP4059937B2 (en) Investment casting to produce castings with enhanced surface finish
US4071372A (en) Silicon nitride NGV&#39;s and turbine blades
US4736786A (en) Method for improving stength of gasifiable patterns
US2495276A (en) Process for making multipiece molds
US6120713A (en) Method of making a casting mould having a cellular structure
EP1037723B1 (en) Method of forming a ceramic mold
JP3552298B2 (en) Mold for hot impeller casting
GB2312184A (en) Making a durable sand mould
WO1979000795A1 (en) Aperture forming member for gasifiable patterns
EP0668117A2 (en) Investment casting method and apparatus
JPH07214236A (en) Mold manufacturing method

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)