GB2073648A - Vacuum bagging - Google Patents

Vacuum bagging Download PDF

Info

Publication number
GB2073648A
GB2073648A GB8109317A GB8109317A GB2073648A GB 2073648 A GB2073648 A GB 2073648A GB 8109317 A GB8109317 A GB 8109317A GB 8109317 A GB8109317 A GB 8109317A GB 2073648 A GB2073648 A GB 2073648A
Authority
GB
United Kingdom
Prior art keywords
base
membrane
ribbing
vacuum
framework
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
GB8109317A
Other versions
GB2073648B (en
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.)
Cytec Process Materials Keighley Ltd
Original Assignee
Aerovac Systems Keighley Ltd
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 Aerovac Systems Keighley Ltd filed Critical Aerovac Systems Keighley Ltd
Priority to GB8109317A priority Critical patent/GB2073648B/en
Publication of GB2073648A publication Critical patent/GB2073648A/en
Application granted granted Critical
Publication of GB2073648B publication Critical patent/GB2073648B/en
Expired 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3607Moulds for making articles of definite length, i.e. discrete articles with sealing means or the like
    • 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
    • B29C33/30Mounting, exchanging or centering
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping 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
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic 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)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

A method and apparatus is disclosed for forming a vacuum bag for moulding composite articles which comprises a base 10, triangular section ribbing 12 fixed to the base and about its perimeter, a stretchable membrane 14 of elastomeric material such as silicone rubber held within a framework 16 and able to form a seal with the ribbing 12. The framework 16, which may be a T-section aluminium frame, may be fastened to the base 10 by means of clips thereby forming a seal between the ribbing 12 and the stretchable member 14 allowing a vacuum to be drawn, e.g. by means of vacuum points 18 between the membrane, the ribbing and the base. Once the vacuum is drawn and the membrane conforms closely to the article to be moulded placed on the base 10, the whole is transferred to an autoclave curing. <IMAGE>

Description

SPECIFICATION Vacuum bagging This invention relates to a method and apparatus useful in the production of carbon fibre composite materials, glass reinforced Plastics, laminates and the like by the vacuum bagging system.
Vacuum bagging is a term used to describe a method of producing pressure on the various components in a carbon fibre composite material, glass reinforced plastics material, metal/metal bonds and other composite materials while these are cured, usually by means of heating in an autoclave. The method may also be used in the production of various parts useful in the aircraft industry by bonding laminates and honeycomb sections.
Previously the normal method which has been used involves "laying up" the component together with layers of release sheets, bleeder cloths, air bleed ropes, rubber compression sheets and the like, on a metal base plate, covering the whole with an impervious sheet of flexible plastics material. The latter has to be securely sealed to the base plate generally by means of a special putty and adhesive tapes to allow a vacuum to be drawn inside the bag. The bag is draped over the contours of the component and slack material has to be secured by adhesive tapes to prevent drainage by air movement when the lay-up is in the autoclave. To ensure a good lay-up and an efficient vacuum seal, the process needs careful workmanship and takes considerable time to operate.Further, after curing in the autoclave, the vacuum bag must be removed from the special putty, which entails considerable cleaning up of the base plate and the bag itself often must be replaced.
The invention seeks to provide a method and apparatus capable of achieving the same end result but without needing putty in a very much quicker time and with greater reliability.
According to the present invention there is provided an apparatus for forming a vacuum bag which comprises a base, ribbing fixed to the base about its perimeter, stretchable membrane held within a framework and able to form a seal with the said ribbing, means for fastening the framework to the base thereby forming a seal between the ribbing and the stretchable membrane, and means for forming a vacuum between the membrane the ribbing and the base.
In one embodiment, the base may be a rigid base plate, e.g. a metal plate, but in another embodiment the base may itself be a stretchable membrane held within a framework.
The invention further provides a method of moulding which comprises placing an item to be moulded on a base having ribbing fixed thereto about its perimeter, locating a stretchable membrane held in a framework over the item on the base, fixing the framework to the base thereby forming a seal between the stretchable membrane and the ribbing, drawing a vacuum between the membrane, the ribbing and the base plate, and curing the article.
Preferably, curing is carried out by heating the bagged lay-up, for example in an autoclave.
Consequently, the material from which the various components are made are of necessity capable of standing curing temperatures without degradation. The preferred material for the membrane is an elastomeric silicone rubber sheet having high elongation and tear-strength properties and being capable of continued service at 4000 F. Similarly the ribbing which forms the seal with the membrane is also of a silicone rubber material.
The membrane is attached to a framework, for example an aluminium T-section framework, so that the membrane may be handled easily. This is especially important when the apparatus used is capable of taking relatively large lay-ups. The membrane, within its frame, can easily be placed in its correct position over the base and the membrane firmly attached to the base by clipping the frame to the base. The ribbing will normally be indented somewhat from the perimeter of the base so that it forms a seal with the membrane within the perimeter of the base and the framework carrying the membrane. The rigid framework has the further advantage that it secures the perimeter of the membrane while the vacuum is drawn thus dispensing with the need for separate adhesive tape and the like which was formally used in these circumstances.
The invention will be described further, by way of example, with reference to the accompanying drawings, in which~ Figure 1 is a perspective view of a base of one embodiment of~the invention; Figure 2 is a perspective view of a membrane suitable for use with the base of Figure 1; Figure 3 is a perspective view of a second embodiment of the invention: and Figure 4 is a cross-section, on an enlarged scale, of the ribbing used.
Referring to Figures 1 and 2, the apparatus comprises an aluminium base plate 10 having a sealing rib 12 located about its perimeter, and spaced in somewhat from the perimeter. The rib 12, as can be seen from Figure 4, is basically triangular in cross-section and its upper apex has been rounded off. An article to be moulded is laid up within the perimeter of the ribbing 12 on the base plate 10. A membrane 14 of flexible silicone rubber having high elongation and tear-strength properties is attached to a T-section aluminium frame 1 6 by means of an appropriate RTV adhesive. The membrane 14 contains two vacuum points 18, to which a vacuum extraction line can be attached. In use, the article to be moulded is placed on the base plate 10 and the membrane 14 placed over the article.Generally, the framework 16 of the membrane is co-extensive with the dimensions of the base plate 10 and, when the membrane 14 is in position over the base plate 10, the framework 16 surrounds the rib 12, which is of sufficient height to contact the membrane 14.
The framework 16 is clipped at various points to the base 10 holding it securely fixed thereto. This has the effect of ensuring that the rib 12 contacts the membrane 14 completely around its periphery forming a sealing contact therewith. The centre of the membrane of course conforms to the shape of the laid-up composite placed on the base plate. A vacuum is then drawn between the base, the rib 12 and the membrane 14 by means of a vacuum extract pipe attached to either or both of the vacuum points 18 when the membrane 14 will conform exactly to the contours of the lay-up. The cross-sectional shape of the rib 12 ensures that as the vacuum is drawn, the membrane 14 conforms closely to the rib in sealing contact therewith, as shown most clearly in Figure 4.On removing the vacuum extract pipes, the vacuum within the apparatus is maintained, and excellent vacuum integrity can be maintained for a long period of time. The apparatus is then transferred to an autoclave set at the correct temperature for curing the article for a time sufficient to effect cure. If desired, thermo-couples or the like may be inserted into the apparatus to ensure that the temperature in a vicinity of the composite is correct.
Referring now to Figure 3, the base 10 here is replaced by a second membrane held within a framework 20 co-extensive with the framework 16. The second membrane contains a rib 12 sealed to it just within the periphery of the framework 20 by means of a suitable RTV adhesive. The two frameworks 16 and 20:may be clamped to each other by means of a clamping strip 22 with the article to be moulded between the two membranes. When the two frameworks 16 and 20 are clamped together the sealing rib on the lower membrane contacts the membrane 14 in a sealing manner similar to that described with reference to Figures 1 and 2 above, and when the vacuum is drawn the membranes-mould themselves to the contours of the article and form a vacuum tight seal about the# rib 12. As before, the apparatus can be taken to an autoclave for heat curing.
As is normal, the composite to be moulded may be laid-up using layers of reinforced resin, release sheets, bleeder cloths, air bleed ropes, rubber compression sheets and the like as wiith conventional vacuum bag moulding.
If the article to be moulded is of unusual shape, the membrane may be made from an uncured silicone rubber moulded to the shape required and then fully cured before being inserted in the framework 14.
When the embodiment of the type shown in Figure 3 is used, it may often be desirable to provide stiffening in the form of cross members 24.
Vacuum monitoring connection points can be inserted into the membrane or the tool base as required. Generally however self-sealing connectors are used so that once the vacuum has been applied the vacuum pipes rnay-be removed without loss of vacuum within the apparatus. As before, thermo-couple leads may be led into the apparatus through the seal rib.
Using the above system, the use of conventional film and acrylic putty is eliminated and the membranes used have an extended life.
The location of the membrane within a framework enables the top frame to be clipped into position on the base very quickly compared with the skilled and laborious job of setting up the diaphragm with putty and adhesive tape under the previous method. Further, the base need not be cleaned after a moulding operation since putty is no longer used. Finally, the sealing of the membrane about the ribbing used in the apparatus of the invention is extremely good and vacuum integrity can be maintained at a higher level and for longer periods than hitherto possible.

Claims (17)

1. An apparatus for forming a vacuum bag which comprises a base, ribbing fixed to the base about its perimeter, a stretchable membrane held within a framework able to form a seal with the said ribbing, means for fastening the framework to the base thereby forming a seal between the ribbing and the stretchable membrane, and means for forming a vacuum between the membrane, the ribbing and the base.
2. An apparatus according to claim 1 in which the base is a rigid plate.
3. An apparatus according to claim 2 in which the base is aluminium plate.
4. An apparatus according to claim 1 in which the base is a stretchable membrane held within a framework.
5. An apparatus according to claim 4 in which the ribbing is fixed to the stretchable membrane comprising the base about its perimeter.
6. An apparatus according to any of the preceding claims in which the ribbing is triangular in cross-section.
7. An apparatus according to any preceding claim in which the membrane is formed from an elastomeric silicone rubber sheet having high elongation and tear-strength properties.
8. An apparatus according to any preceding claim in which th-e means of fastening the framework to the base comprises clips.
9. An apparatus as claimed in any one of claims 1 to 7 in which the means for fastening the membrane to the base comprises a clamping strip.
10. An apparatus according to any preceding claim in which the means for forming a vacuum between the membrane, the ribbing and the base comprises one or more vacuum points set into the membrane.
1 An apparatus according to claim 10 in which the or each vacuum point comprises a selfsealing valve. -
12. An apparatus for forming a vacuum bag substantially as hereinbefore described with reference to-and as illustrated in Figures 1, 2 and 4, or Figures 3 and 4 of the accompanying drawings
13. A method of moulding which comprises placing an item to be moulded on a base having a ribbing fixed thereto about its perimeter, locating stretchable membrane held in a framework over the item on the base, fixing the framework to the base thereby forming a seal between the stretchable member and the ribbing, drawing a vacuum be#tween the membrane, the ribbing and the base plate, and curing the article.
14. A method according to claim 13 in which the curing is carried out by heating the bagged assembly in an autoclave.
15. A method according to either of claims 1 3 - or 14 in which the item to be moulded comprises a lay-up of carbon fibre composite materials, glass reinforced plastics materials, or laminates.
16. A method according to any of claims 13 to 15 in which the membrane is firmly attached to the base by clipping the frame to the base.
17. A method of moulding substantially as hereinbefore described with reference to and as illustrated in Figures 1, 2 and 4, or Figures 3 and 4 of the accompanying drawings.
GB8109317A 1980-04-11 1981-03-25 Vacuum bagging Expired GB2073648B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8109317A GB2073648B (en) 1980-04-11 1981-03-25 Vacuum bagging

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8012051 1980-04-11
GB8109317A GB2073648B (en) 1980-04-11 1981-03-25 Vacuum bagging

Publications (2)

Publication Number Publication Date
GB2073648A true GB2073648A (en) 1981-10-21
GB2073648B GB2073648B (en) 1983-07-06

Family

ID=26275144

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8109317A Expired GB2073648B (en) 1980-04-11 1981-03-25 Vacuum bagging

Country Status (1)

Country Link
GB (1) GB2073648B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0175510A2 (en) * 1984-09-18 1986-03-26 Aerovac Systems (keighley) Limited Vacuum bagging
EP0330972A2 (en) * 1988-02-29 1989-09-06 Siemens Nixdorf Informationssysteme Aktiengesellschaft Autoclave laminating device for multilayered ciruit boards
US4882118A (en) * 1985-04-01 1989-11-21 Short Brothers Plc Method and apparatus for molding fiber reinforced resin matrix composite material
GB2232631A (en) * 1989-01-13 1990-12-19 Spacesaver Signs Making flat plates
US5807593A (en) * 1996-07-10 1998-09-15 The Boeing Company Vacuum bag not requiring disposable breathers
US5993184A (en) * 1998-02-05 1999-11-30 The Boeing Company Magnetic fairing bars for bonding tools
EP1162055A1 (en) * 2000-06-10 2001-12-12 Westland Helicopters Limited Vacuum membrane moulding of a layered composite material
EP2942182A1 (en) * 2014-05-06 2015-11-11 Airbus Operations GmbH Method and system for applying a film to a plastic work piece that is to be cured, and a method for producing a plastic work piece

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0175510A2 (en) * 1984-09-18 1986-03-26 Aerovac Systems (keighley) Limited Vacuum bagging
EP0175510A3 (en) * 1984-09-18 1987-10-28 Aerovac Systems Keighley Ltd Vacuum bagging
US4882118A (en) * 1985-04-01 1989-11-21 Short Brothers Plc Method and apparatus for molding fiber reinforced resin matrix composite material
EP0330972A2 (en) * 1988-02-29 1989-09-06 Siemens Nixdorf Informationssysteme Aktiengesellschaft Autoclave laminating device for multilayered ciruit boards
EP0330972A3 (en) * 1988-02-29 1991-09-18 Siemens Nixdorf Informationssysteme Aktiengesellschaft Autoclave laminating device for multilayered ciruit boards
GB2232631A (en) * 1989-01-13 1990-12-19 Spacesaver Signs Making flat plates
US5807593A (en) * 1996-07-10 1998-09-15 The Boeing Company Vacuum bag not requiring disposable breathers
US5993184A (en) * 1998-02-05 1999-11-30 The Boeing Company Magnetic fairing bars for bonding tools
EP1162055A1 (en) * 2000-06-10 2001-12-12 Westland Helicopters Limited Vacuum membrane moulding of a layered composite material
US6723272B2 (en) 2000-06-10 2004-04-20 Westland Helicopters Limited Moulding process
EP2942182A1 (en) * 2014-05-06 2015-11-11 Airbus Operations GmbH Method and system for applying a film to a plastic work piece that is to be cured, and a method for producing a plastic work piece
DE102014106319A1 (en) * 2014-05-06 2015-11-12 Airbus Operations Gmbh Method and system for applying a film to a provided for curing plastic workpiece and method for producing a plastic workpiece
US10343384B2 (en) * 2014-05-06 2019-07-09 Airbus Operations Gmbh Method and system for applying a film to a plastic work piece that is to be cured, and a method for producing a plastic work piece

Also Published As

Publication number Publication date
GB2073648B (en) 1983-07-06

Similar Documents

Publication Publication Date Title
US4681651A (en) Vacuum bag sealing system
JP6262842B2 (en) Method and apparatus for reducing layer wrinkles in a composite laminate during molding
CN108943768B (en) Flexible vacuum attachment of objects to complex surfaces
EP1162055B1 (en) Vacuum membrane moulding of a layered composite material
CA2787188C (en) Integrally stiffened, reusable vacuum bag and method of making the same
US4836765A (en) Molding apparatus for composite materials
EP2371523A1 (en) A method and a device for repairing parts of composite material of an aircraft
US20080083493A1 (en) Reusable mechanical fastener and vacuum seal combination
US9707705B2 (en) Vacuum bag processing of composite parts using a conformable vacuum bag assembly
RU2008116590A (en) METHOD AND DEVICE FOR ADHESIVE COMPONENTS TO COMPOSITE FORMED PRODUCT
JP6541976B2 (en) System and method for vacuum bagging composite parts
CA2802877C (en) Supporting profiled element, method for producing a supporting profiled element, and use of said supporting profiled element in a method for producing a reinforced vehicle fuselage component
GB2073648A (en) Vacuum bagging
EP0175510B1 (en) Vacuum bagging
US4824513A (en) Silicone rubber vacuum bag tool
JP2006212877A (en) Pressure bag, its manufacturing method, molding method of composite material molded product using pressure bag
US4732639A (en) Vacuum bagging apparatus
US5425628A (en) Pressure bag for tool core
EP0358510A2 (en) Apparatus and method for making composite materials
US7306761B2 (en) Method of manufacturing composite sandwich structures
US10343384B2 (en) Method and system for applying a film to a plastic work piece that is to be cured, and a method for producing a plastic work piece
US20140158282A1 (en) device for the manufacture of a bonded component from fibre-reinforced plastics, and also a method
CA3020773C (en) Systems and methods for applying vacuum pressure to composite parts
Smith et al. Basic Principles for Tooling Design and Inspection
JPS61104829A (en) Frp molding process

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee