WO2010055060A1 - A method of manufacturing a laminated part from fibre material - Google Patents

A method of manufacturing a laminated part from fibre material Download PDF

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Publication number
WO2010055060A1
WO2010055060A1 PCT/EP2009/064993 EP2009064993W WO2010055060A1 WO 2010055060 A1 WO2010055060 A1 WO 2010055060A1 EP 2009064993 W EP2009064993 W EP 2009064993W WO 2010055060 A1 WO2010055060 A1 WO 2010055060A1
Authority
WO
WIPO (PCT)
Prior art keywords
mould
mats
layers
fibre
rolls
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
Application number
PCT/EP2009/064993
Other languages
French (fr)
Inventor
Dennis André Børsting
Qinyin Zhou
Jacobus Johannes Van Der Zee
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.)
LM Wind Power AS
Original Assignee
LM Glasfiber AS
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
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Application filed by LM Glasfiber AS filed Critical LM Glasfiber AS
Priority to CN2009801451689A priority Critical patent/CN102216055A/en
Priority to BRPI0922036A priority patent/BRPI0922036B1/en
Priority to US13/128,869 priority patent/US9381705B2/en
Priority to EP09752349.2A priority patent/EP2362824B1/en
Publication of WO2010055060A1 publication Critical patent/WO2010055060A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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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
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • 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
    • B29C63/00—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/02—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material
    • 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
    • B29C63/00—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/22—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using layers or sheathings having a shape adapted to the shape of the article
    • 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
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/082—Blades, e.g. for helicopters
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/12—Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing

Definitions

  • the invention relates to a method of manufacturing fibre-reinforced parts, such as blades, for wind power plants whereby a number of layers of material comprising fibre, such as glass fibre mats, are arranged on a curved surface of an elongated open mould.
  • a manufacturing process is typically employed in which a part is moulded in two halves in each their open mould, wherein a coat e.g. of gelcoat is initially applied onto the interior surface of the open mould.
  • a number of layers of fibre material, or mats, are subsequently arranged in the mould, typically by hand, following which resin is applied, typically by injection into the closed mould, to attach the individual layers of fibre material to each other.
  • the resin can be applied to the layers manually by RTM (resin transfer moulding), VARTM (vacuum assisted resin transfer moulding) or other suitable methods.
  • the resin can be applied to the laminate layers prior to laying the layers (Prepeg). In the context of this, gelcoat will harden and form the surface of the product.
  • the layers are typically provided to the process as rolls comprising an "endless" length of material which are arranged on the mould and subsequently cut to fit the shape of the part to be manufactured.
  • Knitting and shaping (by cutting) the layers of fibre material within the interior of a mould is today a time-consuming and labour intensive process.
  • walkways may be arranged alongside and/or above the mould such that the workers are allowed to walk along the edge or periphery of the mould and/or above the mould in order to arrange and cut the layers of fibre material as required.
  • multiple layers of fibre material may be arranged on the mould and the layers are typically arranged on top of each other or next to each other possibly with overlapping edges.
  • the parts typically consist of as many as fifty or more layers of material, and the parts are typically build up from a main laminate provided in the centre of the mould.
  • the material is cut from the roll.
  • Manufacturing of parts having curvature throughout the length of the part, such as a wing for a wind power plant, may require very long cuts along the edges of the mould.
  • Moulds for manufacturing such parts may be very large, and the moulds are as a consequence expensive.
  • the time required for the arrangement of material on the mould should be kept at a minimum such that the form time (the time which a part occupies the mould) required by a part to be manufactured is kept at a minimum, thus increasing the overall productivity of the mould.
  • GB 2156729 A teaches a method of moulding reinforced materials where a pre-impregnated reinforcement material, such as a glass fibre mat, is applied to a moulding process.
  • the reinforcement material may be of "indefinite length", in which case a cutter will be needed for the process of laying up the laminate, or the mat can be provided to the process in pre-cut lengths, where the cuts are provided by a cutting station arranged in the vicinity of the mould. The cutting station is able to cut the material, prior to the material being arranged onto the mould, in a direction substantially transverse to the materials direction of conveyance.
  • the fibre material is preferably arranged substantially even and flush, which is why any developed dents, wrinkles or curls and the like should be smoothed out.
  • the lower layer incl. possible additional layers arranged below the lower layer, tend to move or slide within the mould causing the entire layup of fibre material to move away from an intended position within the mould.
  • any manipulation or handling of the material arranged on the mould should be kept at a minimum, which is why a process of manufacture is desired wherein the step of cutting the mats, while the mats are arranged on the mould, is eliminated.
  • each mat is arranged on the curved surface of the mould as pre-shaped mats having a form substantially corresponding to an intended area of application such that any need for further modification of or cutting in the mat is substantially eliminated.
  • the method according to the present invention substantially reduces the required form time required by the manufacturing of a part, and further, the method is able to reduce the efforts required by workers in order to lay up the mats.
  • the pre-shaped mats are rolled off or drawn from one or more rolls provided on a gangway or a cart adapted for conveyance along said elongated mould, the odds of damaging the layers during the layup is greatly reduced and the required manpower for the layup minimized.
  • the one or more rolls are arranged as a "revolver drum” comprising a number of rolls each comprising different pre-shaped mats, handling of, and access to the mats accommodated by the rolls are greatly optimized.
  • the pre-shaped mats constitute pre-cut mats cut from one or more rolls of material.
  • the pre-shaped mats are arranged on the mould according to a pattern of predetermined positions, layup speed as well as the quality of the final product is increased.
  • the predetermined positions constitute a pattern established on the mould by means of light.
  • the pre-shaped mats are provided from a device adapted to pre-cut an "endless" length of material drawn of a roll.
  • the pre-cut mats are rolled onto one or more rolls and in one or more layers.
  • the pre-shaped mats are provided with a form of identification, control and documentation of the layup is facilitated.
  • Figure 1 shows an open mould covered by a layer of fibre mats.
  • Figure 2 shows pre-shaped fibre mats.
  • Figure 3 shows an open mould
  • Figure 1 shows a principal top view of three juxtaposed lengths of fibre material 20 covering an open mould 1 having a curved surface 5 defined by the periphery 6.
  • the mould 1 and the periphery 6 of the curved surface 5 are illustrated by dotted lines.
  • the mould 1 may typically constitute an elongated mould having a length corresponding substantially to the length of the part or sub-part to be manufactured.
  • the material is cut along the edge or periphery 6 such that the length of material, upon being cut, fits an indented position within the mould 1.
  • one layer of material is typically made up from several sub-pieces being arranged, either side by side or with an overlap, on the mould 1.
  • Superjacent or overlying layers may be arranged on the mould 1 such that the lines or areas wherein subjacent or underlying layers meet are covered by the superjacent or overlying layer, in other words, the position of the matsl being arranged on the mould 1 may shift in directions substantially perpendicular to a longitudinal axis of the mould 1.
  • moulds for manufacturing components like blades for wind power plants and the like may be very large, typically in excess of 60 meters, and as many as 50 layers (stacked or piled) or more are arranged on the mould, the process of cutting the material is a tremendous task.
  • a main laminate having a relatively great thickness possibly as much as 50 mm or more and a width of about 800 mm may be arranged on the mould 1.
  • balsa wood may be interposed in order to obtain a desired distance between the layers of mats.
  • the balsa wood may also be subjects to the method of manufacture according to this specification.
  • Figure 2 shows pre-shaped fibre mats 10 prepared for being arranged onto a mould 1.
  • the pre-shaped mats 10 may be delivered from a sub supplier or manufactured at an adjacent manufacturing station.
  • the pre-shaped fibre mats 10 may be provided to the process as rolled unto one or more not shown rolls.
  • the rolls may constitute a "revolver drum” (not shown) configured for accommodating two or more rolls, such that fibre mats with varying properties and shaped, may be arranged onto the mould 1 without disturbing the process of laying up one or more layers of fibre material.
  • the pre-shaped mats may be provided with markings 11 facilitating layup of the mats on the mouldi .
  • the pre-shaped fibre mats 10 may be produced (fabricated or weaved) such that a particular shape is obtained, or as an equal alternative, cut in shape from a roll of material.
  • the means for establishing the cuts may constitute cut-rolls, knives/blades, laser, any type of blast-cutting, cutting forms and the like, and the process of pre-shaping the layers may constitute an automated and/or processor controlled process.
  • Figure 3 shows an empty and open mould 1.
  • the method of manufacturing a fibre reinforced part according to the present invention may comprise the step of establishing markings on the curved surface 5 of the mould 1 , or on mats arranged on the mould 1 , such as illustrated by the dotted lines 7.
  • the markings 7 may be established by lightning or illuminating means (not shown) incl. a laser, provided above the curved surface 5 of the mould 1.
  • a worker may align the material according to the markings 7, such that the intended position of the material on the mould 1 may relatively easily be obtained.
  • the lightning means may, for various purposes, be able to alter the markings, e.g. such that the markings 7 changes upon finalization of a layup.
  • Means for recording video or still pictures may be provided such the control and/or documentation of the process of laying up the material may be provided.
  • the lightning means as well as the camera may be controlled by a not shown processor, such as a computer.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

A method of manufacturing fibre-reinforced parts, such as blades, for wind power plants, whereby a number of layers (10) of material comprising fibre, such as glass fibre mats, are arranged on a curved surface (5) of an elongated (5) open mould (1) wherein each layer (10) of material is arranged on said curved surface (5) as pre-shaped mats (10) having a form substantially corresponding to an intended area of application such that any need for further modification of or cutting in said material is substantially eliminated.

Description

A method of manufacturing a laminated part from fibre material
According to one aspect, the invention relates to a method of manufacturing fibre-reinforced parts, such as blades, for wind power plants whereby a number of layers of material comprising fibre, such as glass fibre mats, are arranged on a curved surface of an elongated open mould.
Background
In the context of manufacturing fibre-reinforced parts, such as blades, for wind power plants, a manufacturing process is typically employed in which a part is moulded in two halves in each their open mould, wherein a coat e.g. of gelcoat is initially applied onto the interior surface of the open mould.
A number of layers of fibre material, or mats, are subsequently arranged in the mould, typically by hand, following which resin is applied, typically by injection into the closed mould, to attach the individual layers of fibre material to each other. The resin can be applied to the layers manually by RTM (resin transfer moulding), VARTM (vacuum assisted resin transfer moulding) or other suitable methods. Alternatively the resin can be applied to the laminate layers prior to laying the layers (Prepeg). In the context of this, gelcoat will harden and form the surface of the product.
The layers are typically provided to the process as rolls comprising an "endless" length of material which are arranged on the mould and subsequently cut to fit the shape of the part to be manufactured.
Arranging and shaping (by cutting) the layers of fibre material within the interior of a mould is today a time-consuming and labour intensive process. Depending of the size of the part to be manufactured, and thereby the size of the mould, walkways may be arranged alongside and/or above the mould such that the workers are allowed to walk along the edge or periphery of the mould and/or above the mould in order to arrange and cut the layers of fibre material as required.
During the layup of fibre material, combined efforts of several workers are required, as the fibre material is heavy and not easy manipulable. Some workers assist in the rollout of material, while other workers positioned along the edge of the mould, make sure that the layers are laid up correctly.
In order to secure a desired shape, visual appearance, strength and stability of the part to be manufactured, it is of outmost importance that the layers are arranged and cut correctly without dents or wrinkles and the like.
Depending on the application and structure of the part to be manufactured, multiple layers of fibre material may be arranged on the mould and the layers are typically arranged on top of each other or next to each other possibly with overlapping edges.
The parts typically consist of as many as fifty or more layers of material, and the parts are typically build up from a main laminate provided in the centre of the mould.
After a layer, which is provided from a roll, is arranged on the mould, the material is cut from the roll. Manufacturing of parts having curvature throughout the length of the part, such as a wing for a wind power plant, may require very long cuts along the edges of the mould.
Moulds for manufacturing such parts may be very large, and the moulds are as a consequence expensive. The time required for the arrangement of material on the mould should be kept at a minimum such that the form time (the time which a part occupies the mould) required by a part to be manufactured is kept at a minimum, thus increasing the overall productivity of the mould.
GB 2156729 A teaches a method of moulding reinforced materials where a pre-impregnated reinforcement material, such as a glass fibre mat, is applied to a moulding process. The reinforcement material may be of "indefinite length", in which case a cutter will be needed for the process of laying up the laminate, or the mat can be provided to the process in pre-cut lengths, where the cuts are provided by a cutting station arranged in the vicinity of the mould. The cutting station is able to cut the material, prior to the material being arranged onto the mould, in a direction substantially transverse to the materials direction of conveyance.
The fibre material is preferably arranged substantially even and flush, which is why any developed dents, wrinkles or curls and the like should be smoothed out. Further, as one layer is typically applied on top of a preceding layer, the lower layer incl. possible additional layers arranged below the lower layer, tend to move or slide within the mould causing the entire layup of fibre material to move away from an intended position within the mould. As a consequence, any manipulation or handling of the material arranged on the mould should be kept at a minimum, which is why a process of manufacture is desired wherein the step of cutting the mats, while the mats are arranged on the mould, is eliminated.
It is thus an object of the invention to provide a solution to the above drawbacks.
This is accomplished by the method of manufacturing a fibre-reinforced part as per the introductory part of this specification, wherein each mat is arranged on the curved surface of the mould as pre-shaped mats having a form substantially corresponding to an intended area of application such that any need for further modification of or cutting in the mat is substantially eliminated.
The method according to the present invention substantially reduces the required form time required by the manufacturing of a part, and further, the method is able to reduce the efforts required by workers in order to lay up the mats.
When, as stated in claim 2, the pre-shaped mats are rolled off or drawn from one or more rolls provided on a gangway or a cart adapted for conveyance along said elongated mould, the odds of damaging the layers during the layup is greatly reduced and the required manpower for the layup minimized.
When, as stated in claim 3, the one or more rolls are arranged as a "revolver drum" comprising a number of rolls each comprising different pre-shaped mats, handling of, and access to the mats accommodated by the rolls are greatly optimized.
According to one embodiment, the pre-shaped mats constitute pre-cut mats cut from one or more rolls of material.
When, as stated in claim 5, the pre-shaped mats are arranged on the mould according to a pattern of predetermined positions, layup speed as well as the quality of the final product is increased.
According to one embodiment, the predetermined positions constitute a pattern established on the mould by means of light.
According to one embodiment the pre-shaped mats are provided from a device adapted to pre-cut an "endless" length of material drawn of a roll. According to one embodiment, the pre-cut mats are rolled onto one or more rolls and in one or more layers.
When, as stated in claim 10, the pre-shaped mats are provided with a form of identification, control and documentation of the layup is facilitated.
Brief description of the figure
Figure 1 shows an open mould covered by a layer of fibre mats.
Figure 2 shows pre-shaped fibre mats.
Figure 3 shows an open mould.
Detailed description with reference to the figures
Figure 1 shows a principal top view of three juxtaposed lengths of fibre material 20 covering an open mould 1 having a curved surface 5 defined by the periphery 6. The mould 1 and the periphery 6 of the curved surface 5 are illustrated by dotted lines.
The mould 1 may typically constitute an elongated mould having a length corresponding substantially to the length of the part or sub-part to be manufactured.
According to today's methods of manufacturing fibre reinforced parts, one or more layers 20, which typically are unrolled from one or more rolls (not shown), are arranged on the mould 1 such that the curved surface 5 is covered. Upon at least one length of material being arranged such that the curved surface 5 is covered, the material is cut along the edge or periphery 6 such that the length of material, upon being cut, fits an indented position within the mould 1.
Due to a limited width of the material being provided to the mould 1 , one layer of material is typically made up from several sub-pieces being arranged, either side by side or with an overlap, on the mould 1.
Superjacent or overlying layers may be arranged on the mould 1 such that the lines or areas wherein subjacent or underlying layers meet are covered by the superjacent or overlying layer, in other words, the position of the matsl being arranged on the mould 1 may shift in directions substantially perpendicular to a longitudinal axis of the mould 1.
As can be seen in the figure, it will typically be necessary to cut along the entire periphery or edge 6 of the curved surface 5.
As the moulds for manufacturing components like blades for wind power plants and the like may be very large, typically in excess of 60 meters, and as many as 50 layers (stacked or piled) or more are arranged on the mould, the process of cutting the material is a tremendous task.
Although not shown in the figures, a main laminate having a relatively great thickness, possibly as much as 50 mm or more and a width of about 800 mm may be arranged on the mould 1.
Further, and not shown in the figures, between the mats, balsa wood may be interposed in order to obtain a desired distance between the layers of mats. The balsa wood may also be subjects to the method of manufacture according to this specification.
Figure 2 shows pre-shaped fibre mats 10 prepared for being arranged onto a mould 1. The pre-shaped mats 10 may be delivered from a sub supplier or manufactured at an adjacent manufacturing station.
The pre-shaped fibre mats 10 may be provided to the process as rolled unto one or more not shown rolls. The rolls may constitute a "revolver drum" (not shown) configured for accommodating two or more rolls, such that fibre mats with varying properties and shaped, may be arranged onto the mould 1 without disturbing the process of laying up one or more layers of fibre material.
The pre-shaped mats may be provided with markings 11 facilitating layup of the mats on the mouldi .
The pre-shaped fibre mats 10 may be produced (fabricated or weaved) such that a particular shape is obtained, or as an equal alternative, cut in shape from a roll of material.
The means for establishing the cuts may constitute cut-rolls, knives/blades, laser, any type of blast-cutting, cutting forms and the like, and the process of pre-shaping the layers may constitute an automated and/or processor controlled process.
Figure 3 shows an empty and open mould 1. The method of manufacturing a fibre reinforced part according to the present invention may comprise the step of establishing markings on the curved surface 5 of the mould 1 , or on mats arranged on the mould 1 , such as illustrated by the dotted lines 7. The markings 7 may be established by lightning or illuminating means (not shown) incl. a laser, provided above the curved surface 5 of the mould 1.
Upon a layer of material, pre-shaped of not, being arranged on the mould 1 , a worker may align the material according to the markings 7, such that the intended position of the material on the mould 1 may relatively easily be obtained.
The lightning means may, for various purposes, be able to alter the markings, e.g. such that the markings 7 changes upon finalization of a layup.
Means for recording video or still pictures may be provided such the control and/or documentation of the process of laying up the material may be provided.
The lightning means as well as the camera may be controlled by a not shown processor, such as a computer.
It must be understood that the invention as disclosed in the present description and figures can be modified or amended while continuing to be comprised by the protective scope conferred by the following claims.

Claims

Claims
1. A method of manufacturing fibre-reinforced parts, such as blades for wind power plants, whereby a number of layers (10) of material comprising fibre, such as glass fibre mats, are arranged on a curved surface (5) of an elongated open mould (1 ) characterized by that each layer (10) of material is arranged on said curved surface (5) as pre-shaped mats (10) having a form substantially corresponding to an intended area of application such that any need for further modification of or cutting in said material is substantially eliminated.
2. The method according to claim 1 wherein said pre-shaped mats (5) are rolled off or drawn from one or more rolls provided on a gangway or a cart adapted for conveyance along said elongated mould (1 ).
3. The method according to claim 2 wherein said one or more rolls are arranged as a "revolver drum" comprising a number of rolls each comprising different pre-shaped mats (10).
4. The method according to any of the preceding claims wherein said pre- shaped mats (5) constitute pre-cut layers cut from one or more rolls of material.
5. The method according to any of the preceding claims wherein said pre- shaped mats (5) are arranged on said mould according to a pattern of predetermined positions.
6. The method according to any of the preceding claims wherein said pre- shaped mats (5) are arranged on said mould according to a pattern of predetermined positions indicated on said mould (1 ), wherein said pattern are established on said mould (1 ) by means of light.
7. The method according to any of the preceding claims wherein said pre- shaped mats (5) are provided from a device adapted to pre-cut said material.
8. The method according to claim 7 wherein said pre-cut layers (5) are rolled onto one or more rolls and in one or more layers.
9. The method according to any of the preceding claims wherein said pre- shaped mats (5) are arranged on said form (1 ) according to markings provided on said pre-shaped mats (5).
10. The method according to any of the preceding claims wherein said pre- shaped mats (5) are provided with a form of identification.
PCT/EP2009/064993 2008-11-12 2009-11-11 A method of manufacturing a laminated part from fibre material Ceased WO2010055060A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CN2009801451689A CN102216055A (en) 2008-11-12 2009-11-11 A method of manufacturing a laminated part from fibre materia
BRPI0922036A BRPI0922036B1 (en) 2008-11-12 2009-11-11 method of making fiber-reinforced parts
US13/128,869 US9381705B2 (en) 2008-11-12 2009-11-11 Method of manufacturing a laminated part from fibre material
EP09752349.2A EP2362824B1 (en) 2008-11-12 2009-11-11 A method of manufacturing a laminated part from fibre material

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BRPI0922036B1 (en) 2020-01-28
US20110277929A1 (en) 2011-11-17
EP2362824A1 (en) 2011-09-07
US9381705B2 (en) 2016-07-05
CN102216055A (en) 2011-10-12
BRPI0922036A2 (en) 2015-12-22
EP2362824B1 (en) 2016-04-13

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