GB2345877A - Composite moulding method - Google Patents

Composite moulding method Download PDF

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Publication number
GB2345877A
GB2345877A GB9901394A GB9901394A GB2345877A GB 2345877 A GB2345877 A GB 2345877A GB 9901394 A GB9901394 A GB 9901394A GB 9901394 A GB9901394 A GB 9901394A GB 2345877 A GB2345877 A GB 2345877A
Authority
GB
United Kingdom
Prior art keywords
film
mould
preform
external surface
polyamide
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
GB9901394A
Other versions
GB2345877B (en
GB9901394D0 (en
Inventor
Geoffrey Michael Suter
Ronald John Dawson
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.)
GKN Technology Ltd
Original Assignee
GKN Technology 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 GKN Technology Ltd filed Critical GKN Technology Ltd
Priority to GB9901394A priority Critical patent/GB2345877B/en
Publication of GB9901394D0 publication Critical patent/GB9901394D0/en
Publication of GB2345877A publication Critical patent/GB2345877A/en
Application granted granted Critical
Publication of GB2345877B publication Critical patent/GB2345877B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • 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
    • B29C51/00Shaping 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
    • B29C51/16Lining or labelling
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/34Layered products comprising a layer of synthetic resin comprising polyamides
    • 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
    • B29C51/00Shaping 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
    • B29C51/08Deep drawing or matched-mould forming, i.e. using mechanical means only
    • B29C51/082Deep drawing or matched-mould forming, i.e. using mechanical means only by shaping between complementary mould parts
    • 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0809Fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2377/00Polyamides

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 cured component is made from laminated pre-preg by hot compression moulding in which a pre-form of the component 16 is separated from the mould surface by a film (17, 18) of polyamide or other thermoplastic material. The polyamide is incorporated into the component as the outer surface thereof.

Description

Composite Moulding Method This invention relates to a method of hot compression moulding. In such a method a preform of uncured polymeric material, e. g. of pre-preg laminates, is introduced into a heated mould in a press, the mould is closed and the material cured. The mould is typically heated to a temperature greater than 120 C. After curing the mould is opened and the cured article removed.
The polymeric material may be, for example, laminates of epoxy-impregnated glass fibre"pre- preg". Conventionally a release agent coating is applied to the mould tool before use so that the moulded article can be separated from the tool when the resin has cured sufficiently.
It is often necessary to clean the mould after each moulding cycle and periodically to re-coat the mould with release agent.
It is an object of the present invention to provide a method of compression moulding a component which reduces the moulding cycle time by enabling a partially cured blank to be removed from the mould after a shorter cure time than heretofore.
According to the invention we provide a method of making a cured component by hot compression moulding in which the external surface of a preform of laminated pre-preg is separated from the mould surface by a film of a polyamide or of another thermoplastic material which retains sufficient strength at the moulding temperature not to rupture and which adheres directly to the external surface of the preform, there being no release agent between said surface and the film, placing the preform in the mould so that said external surface is separated from the mould surface by said film, closing the mould and heating the latter to cure the prepreg and to incorporate the polyamide or other thermoplastic film into the cured article so that the film forms the external surface thereof.
It has heretofore been proposed to provide a shaped article by curing a pre-preg laminate by vacuum-bagging a blank in a polyamide film then autoclaving the bagged blank to cure it. The blank is wrapped in a release film before being bagged in the polyamide film and the air between the release film and the bag evacuated before the bag is autoclaved. After curing of the blank, the polyamide film is removed from the cured article. The release film ensures that the polyamide bag can be removed from the cured blank.
The present invention differs from the prior art in that the polyamide or other thermoplastic film is integrally incorporated into the preform or blank and forms the external surface thereof.
The method has various advantages. Since the polyamide or other thermoplastic film does not stick to the mould surface the partially cured preform can be removed from the mould sooner than heretofore because it is not necessary that the preform be cured to the stage at which the resin loses its adhesive properties.
Another feature of the method is that the preform may be wrapped in e. g. polyamide film and heated in an oven, e. g. a microwave oven, before being placed in the mould thus further reducing the mould cycle time.
Another feature is that the polyamide or other thermoplastic film can serve to bridge over clearances in complex tools with moving surfaces or ejection devices. This can prevent liquid resin from running down such clearances, curing and causing seizure.
The preform may be wrapped in thermoplastic film before being placed in the mould or a sheet of the film may be placed over the lower mould surface, the preform placed in the mould, another sheet of the film place over the preform and the mould closed. The essential point is that the preform is separated from the mould surface by the film.
It would be possible to include an adhesion promoter between the outer surface of the preform and the polyamide or other film.
The polyamide film may e. g. be nylon 6 or nylon 66 such as that known as Capran (TM) made by Allied Signal Inc. It may have a thickness of between 10 and 80ym, e. g. 50, um.
While in carrying out the method it may still be necessary to apply a release agent to the mould from time to time but this may not be necessary after every moulding cycle nor will it be necessary to clean the mould so frequently as heretofore.
The invention will now be described in detail by way of example with reference to the accompanying drawings in which: Figure 1 is a diagram illustrating the principle of the invention; Figure 2 is a diagram illustrating an embodiment in which the preform is wrapped in a film before being placed in the mould; Figure 3 is a diagram illustrating how the film may be applied to the mould rather than to the preform.
Referring first to Figure 1, a mould of a hot compression moulding machine is indicated at 10 and has an upper part 11 and a lower part 12. The upper part 11 has a shaped moulding surface 13 and the lower part 12 has a shaped moulding surface 14. There are ejectors 15 in the lower mould part 12.
A preform 16 is shown which is made of epoxy impregnated glass fibre pre-preg. A nylon film 17 is shown as separating the upper surface of the pre-preg from the mould surface 13 and a second sheet of nylon 18 is shown separating the lower surfaces of the preform from the mould surface 14. The nylon films 17 and 18 separate the faces of the preform from the mould surfaces.
To mould the required article, the mould parts are closed and heated to a temperature greater than 120 C. After moulding the mould parts are opened and the finished article removed, the nylon films 17 and 18 having been incorporated into and forming the surfaces of the article.
No release agent is used between the preform 16 and the films 17 and 18. Indeed an adhesion promoter may be used between the facing surfaces of the preform and the nylon film to improve the adhesion between the surface of the preform and the nylon film.
Since the nylon film does not adhere to the mould surfaces 13 and 14 it has been found that it is possible to remove the moulded article from the mould after a shorter time than would be the case if no nylon film 17 and 18 were used. The film 18 also prevents resin from the preform from leaking down into the ejectors 15, curing and causing the ejectors to stick.
Figure 2 shows a variation in which the preform 16 is wrapped in the sheets 17 and 18 of nylon film before it is put into the mould. In this case it is possible to heat the wrapped preform, e. g. in a microwave, before it is placed in the mould thus reducing the mould cycle time.
Figure 3 shows another variation where the nylon film 18 is placed on the surface 14 of the lower mould part 12, the preform 16 is then placed on the film 18, the film 17 is then placed over the preform and the mould then closed.
It will be noticed in all cases that the nylon films 17 and 18 isolate the faces of the preform 16 from the mould surfaces 13 and 14.
While it may still be necessary to use a mould release agent as conventionally used, this will not be needed as frequently as heretofore. Moreover the use of the nylon film means that the mould surfaces 13 and 14 will require less cleaning.
It will be seen that the invention provides a method of making a cured component which has advantages over those heretofore used and which provides the component with a protective coating of nylon. As has been described above, the nylon film may be replaced by another thermoplastic material which retains sufficient strength at moulding temperature not to rupture and which adheres directly to the external surface of the preform.

Claims (7)

  1. Claims 1. A method of making a cured component by hot compression moulding in which the external surface of a preform of laminated pre-preg is separated from the mould surface by a film of polyamide or of other thermoplastic material which retains sufficient strength at the moulding temperature not to rupture and which adheres directly to the external surface of the preform, there being no release agent between said surface and the film, placing the preform in the mould so that said external surface is separated from the mould surface by said film, closing the mould and heating the latter to cure the pre-preg and to incorporate the polyamide or other thermoplastic film into the cured article so that the film forms the external surface thereof.
  2. 2. A method according to Claim 1 wherein the preform is wrapped in said film before being placed in the mould.
  3. 3. A method according to Claim 2 wherein the preform is wrapped in said film and then heated before being placed in the mould.
  4. 4. A method according to Claim 1 in which the mould has upper and lower mould parts and wherein a sheet of said film is placed over the surface of the lower mould part, the preform is placed over said sheet, a second sheet of said film is placed over the preform and the mould parts are closed.
  5. 5. A method according to any preceding claim wherein an adhesion promoter is used between the outer surface of the preform and the film.
  6. 6. A method according to any preceding claim in which the film is nylon 6 or nylon 66.
  7. 7. A method substantially as herebefore described with reference to the accompanying drawings.
    7. A method according to any preceding claim wherein the film has a thickness of between 10 and 80ym.
    8. A method substantially as herebefore described with reference to the accompanying drawings.
    Amendments to the claims have been filed as follows 1. A method of making a cured component by hot compression moulding in which the external surface of a preform of laminated pre-preg is separated from the mould surface by a film of a polyamide which retains sufficient strength at the moulding temperature not to rupture and which adheres directly to the external surface of the preform, there being no release agent or adhesion promoter between said surface and the film, placing the preform in the mould so that said external surface is separated from the mould surface by said film, closing the mould and heating the latter to cure the pre-preg and to incorporate the polyamide film into the cured article so that the film forms the external surface thereof.
    2. A method according to Claim 1 wherein the preform is wrapped in said film before being placed in the mould.
    3. A method according to Claim 2 wherein the preform is wrapped in said film and then heated before being placed in the mould.
    4. A method according to Claim 1 in which the mould has upper and lower mould parts and wherein a sheet of said film is placed over the surface of the lower mould part, the preform is placed over said sheet, a second sheet of said film is placed over the preform and the mould parts are closed.
    5. A method according to any preceding claim in which the film is nylon 6 or nylon 66.
    6. A method according to any preceding claim wherein the film has a thickness of between 10 and 80ym.
GB9901394A 1999-01-23 1999-01-23 Composite moulding method Expired - Fee Related GB2345877B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9901394A GB2345877B (en) 1999-01-23 1999-01-23 Composite moulding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9901394A GB2345877B (en) 1999-01-23 1999-01-23 Composite moulding method

Publications (3)

Publication Number Publication Date
GB9901394D0 GB9901394D0 (en) 1999-03-10
GB2345877A true GB2345877A (en) 2000-07-26
GB2345877B GB2345877B (en) 2003-05-21

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB9901394A Expired - Fee Related GB2345877B (en) 1999-01-23 1999-01-23 Composite moulding method

Country Status (1)

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Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS592842A (en) * 1982-06-30 1984-01-09 宇部日東化成株式会社 Blank for forming coating fiber reinforced plastic product
JPH02235631A (en) * 1989-03-08 1990-09-18 Nec Corp Preparation of fiber reinforced composite material

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS592842A (en) * 1982-06-30 1984-01-09 宇部日東化成株式会社 Blank for forming coating fiber reinforced plastic product
JPH02235631A (en) * 1989-03-08 1990-09-18 Nec Corp Preparation of fiber reinforced composite material

Also Published As

Publication number Publication date
GB2345877B (en) 2003-05-21
GB9901394D0 (en) 1999-03-10

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Legal Events

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

Effective date: 20040123