WO1998016376A1 - Pole and method for its manufacture - Google Patents

Pole and method for its manufacture Download PDF

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Publication number
WO1998016376A1
WO1998016376A1 PCT/DK1997/000431 DK9700431W WO9816376A1 WO 1998016376 A1 WO1998016376 A1 WO 1998016376A1 DK 9700431 W DK9700431 W DK 9700431W WO 9816376 A1 WO9816376 A1 WO 9816376A1
Authority
WO
WIPO (PCT)
Prior art keywords
pole
mandrel
polymer
composite fibres
plate
Prior art date
Application number
PCT/DK1997/000431
Other languages
Danish (da)
French (fr)
Other versions
WO1998016376A8 (en
Inventor
Thomas-Peter THØGERSEN
Original Assignee
Danomast Gt Glasfiber A/S
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 Danomast Gt Glasfiber A/S filed Critical Danomast Gt Glasfiber A/S
Priority to EP97943789A priority Critical patent/EP0930965A1/en
Priority to CA002269548A priority patent/CA2269548A1/en
Priority to AU45502/97A priority patent/AU4550297A/en
Publication of WO1998016376A1 publication Critical patent/WO1998016376A1/en
Priority to NO991730A priority patent/NO991730L/en
Publication of WO1998016376A8 publication Critical patent/WO1998016376A8/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00—Layered products having a non-planar shape
    • B32B1/08—Tubular products
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/36—Bending and joining, e.g. for making hollow articles
    • B29C53/38—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges
    • B29C53/40—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges for articles of definite length, i.e. discrete articles
    • B29C53/42—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges for articles of definite length, i.e. discrete articles using internal forming surfaces, e.g. mandrels
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping 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
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/0036—Heat treatment
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
    • E04H12/02—Structures made of specified materials
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/562—Winding and joining, e.g. winding spirally spirally
    • 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
    • B29L2009/00—Layered products
    • 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
    • B29L2031/766—Poles, masts, posts

Definitions

  • the invention concerns a pole made of a material which is mainly made up of a first component, such as glass, and of a second component, such as a polymer.
  • a typical example of such poles are flagpoles which earlier were normally made of wood. However, in the recent many years, wood as material for flagpoles has largely been replaced by other materials.
  • a material which has grown quite popular is glass-fibre reinforced polyester which is characterised by a number of outstanding properties .
  • Flagpoles made of this material in practice known as glass-fibre flagpoles, are thus light and at the same time very strong. They have a smooth, bright surface which is weather-resisting and dirt repelling, and unlike wooden flagpoles, they do not require recurrent maintenance such as painting or lacquering.
  • the flagpoles can be constructed in different ways, but normally the polyester in the pole is reinforced by several layers of tube-shaped fibres in the form of webs or mats which lie rather close together.
  • the flagpole can be adopted for manual laying up.
  • the glass fibre webs which in advance has been drenched with polyester, is thus laid round a mandrel.
  • Each layer is pressed by a groove roller to compress the web and press out the air in the web, before the next layer is laid up.
  • a pole such as a flagpole of glass-fibre reinforced polyester or of a similar fibre reinforced polymer, will be rather expensive due to the above-mentioned production-related circumstances.
  • the object of the invention is to provide a pole of the type mentioned in the opening paragraph and which is less expensive to manufacture than a pole made of glass-fibre reinforced polyester or a similar fibre reinforced polymer and which, at the same time, has just as good properties.
  • novel and unique features according to the invention whereby this is achieved, is the fact that the two components form part of the material as composite fibres formed by both components .
  • the composite fibres can enter into the material as rovings which consist of a large number of fibres, but at the embodiment preferred, these rovings can already be woven into a web of fibres .
  • the material of a pole is recyclable and can thereby be utilised again.
  • an advantage is furthermore obtained in that discarded poles and poles with manufacturing faults will no longer pollute the environment to the same extent as poles of e.g. glass-fibre reinforced polyester which are virtually imperishable.
  • the invention furthermore concerns a method of manufacturing a pole of a material which is mainly made up of a first component, such as glass, and a second component, such as a polymer.
  • the novel and unique features of this method is the fact that the two components make up composite fibres formed by both components, and that the pole is made of these composite fibres.
  • fig. 1 is a perspective view of a flagpole according to the invention
  • fig. 2 a - g are perspective views of successive process stages of a first embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1,
  • fig. 3 a - c are perspective views of successive process stages of a second embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1, and
  • fig. 4 a - c are perspective views of successive process stages of a third embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1.
  • Fig. 1 shows, diagonally from the end and in perspective, a flagpole 1 according to the invention.
  • the flagpole is, in this case, made up of a number of tube-shaped webs 2 which transversely lie close together.
  • the web is woven from rovings each consisting of a large number of fibres.
  • Each fibre is a composite fibre of two components, respectively glass and a polymer, such as polypropylene.
  • the flagpole can be manufactured in different ways as described in details in the following.
  • Fig. 2 a - g show a first method according to the invention of manufacturing a flagpole.
  • the flagpole is thus constructed round a rigid mandrel 3 of for example aluminium.
  • the mandrel has journals 4 for rotatable suspension in a pedestal (not shown) .
  • a web 5 is wound round the mandrel 3 until a layer 6 having mainly the diameter of the finished pole is formed.
  • the web 5 is of the above-mentioned type of composite fibres of glass and a polymer respectively, in the following, the polymer is assumed to be, as an example, polypropylene.
  • a flexible plate 8 is laid round the film 7.
  • the surface of the composite fibre layer 6 with the film 7 will be formed as an impression of the surface of the plate 8 facing the composite fibre layer.
  • flagpoles of an even, smooth surface are wanted, the surface being dirt repelling and easy cleanable, and the plate 8 must then have a correspondingly even, smooth surface .
  • an air permeable mat 9 is laid round the already laid layers 6, 7, 8, 9. Since the mat is air permeable, it allows confined air being evacuated.
  • the mandrel 3 with the layers 6, 7, 8, 9, 10 is placed in a furnace 11 at a temperature of e.g. 200°C.
  • the mandrel stays in the furnace for about 5 minutes during which the two thermoplastic polymers, in this example polypropylene and acrylic respectively, soften and assume the shape of the mandrel, simultaneously the composite fibres of the web 5 are joined whereby a solid, coherent layer 5 is formed, said layer is furthermore joined with the acrylic film 7.
  • the mandrel 3 with the layers 6, 7, 8, 9, 10 is then taken out of the furnace and cooled to a temperature where both the polypropylene and the acrylic transform into the solid phase, and finally, the different layers 8, 9, 10 and the mandrel 3 are removed from the now solid and joined layers 6, 7 which form the in fig. 2g shown finished flagpole 1.
  • Fig. 3 a, b, c show a second method according to the invention of manufacturing a flagpole.
  • the flagpole is constructed round a flexible mandrel 12 of for example thermostable silicone rubber.
  • the mandrel 12 is via a tube 13 with a valve 14 connected to a compressed-air source (not shown) .
  • a valve 14 By opening the valve 14, the flexible mandrel 12 is put under pressure.
  • a web 14 is wound round the mandrel 12 until a layer 15 having mainly the diameter of the finished pole is formed.
  • the web is of the same kind as the web 5 shown in fig. 2 a-g of composite fibres of glass and polymer, respectively.
  • the mandrel 12 with the composite fibres 15 is placed in a mould 16 of for example aluminium.
  • the mould 16 consists, in this case, of two halves 16 a, b which in fig. 3b are closed round the composite fibre layer 15 and the mandrel 12.
  • the valve 14 is now opened so that the flexible mandrel 12 expands and thereby presses the composite fibre layer 15 to abut against the inside of the mould chamber which has a shape corresponding to the shape of the finished flagpole.
  • the mould 16 is, in advance, heated to for example 150°C.
  • the mould is closed and the flexible mandrel 12 put under pressure, the mould is heated further to a temperature of 200°C and kept at this temperature for a sufficient period of time, for example 5 minutes, until the polymer softens and thereby assumes the shape of the mould chamber, at the same time as the composite fibres of the web 14 are joined.
  • the mould At the end of the standing time in the furnace, the mould is cooled to about 150°C at which point the plastic polymer transforms into the solid phase. The mould is then opened and the mandrel removed when the pressure has been released.
  • Fig. 4 a, b, c show a third method according to the invention of manufacturing a flagpole.
  • a plate is formed, as shown in fig. 4a, said plate consisting partly of web 19 which is of the same kind as the web 5 shown in fig. 2 a - g of composite fibres of glass and polypropylene respectively, and partly of an substratum in the form of a dyed acrylic-film 20 with an even, smooth surface .
  • the plate 18 may be formed under pressure at a temperature of for example 200°C and with a standing time of 5 minutes during which the polypropylene softens and the composite fibres of the web 19 are joined, simultaneously the acrylic-film 20 is joined with the composite fibres.
  • the plate 18 is then cooled to 80° - 120°C and curved, as shown in fig. 4a with the acrylic substratum at the outside, to a jacket 21 round a rigid mandrel 22 having the shape of the wanted cavity of the finished flagpole.
  • the two long sides 23 a,b of the wrapping 21 are joined by a weld 24 by means of a welding gun 25 after which the finished flagpole is pulled off the mandrel.
  • the flagpole is now the colour of the acrylic-film and has its even, smooth surface.
  • the joining of the long sides can also be done by means of other joining methods, for example bonding or hot melting, just as the seam can be a lap weld instead of a butt joint.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Thermal Sciences (AREA)
  • Materials Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Physics & Mathematics (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

A pole (1), for example a flagpole, is made of a material which is mainly made up of a first component, such as glass, and a second component, such as a polymer. The two components enter into the material as premade composite fibres formed by both components, in the form of a web (2) of rovings. The polymer is a thermoplastic polymer, for example polypropylene, and the pole is made of the composite fibres under heat stress which softens the polymer and thereby joins the composite fibres so that they, after cooling, assume fixed shape. In this way, for example a flagpole which is less expensive than a conventional flagpole of for example glass-fibre reinforced polyester and which, at the same time, has just as good properties, can be manufactured.

Description

Pole and method for its manufacture
The invention concerns a pole made of a material which is mainly made up of a first component, such as glass, and of a second component, such as a polymer.
A typical example of such poles are flagpoles which earlier were normally made of wood. However, in the recent many years, wood as material for flagpoles has largely been replaced by other materials. A material which has grown quite popular is glass-fibre reinforced polyester which is characterised by a number of outstanding properties .
Flagpoles made of this material, in practice known as glass-fibre flagpoles, are thus light and at the same time very strong. They have a smooth, bright surface which is weather-resisting and dirt repelling, and unlike wooden flagpoles, they do not require recurrent maintenance such as painting or lacquering.
The flagpoles can be constructed in different ways, but normally the polyester in the pole is reinforced by several layers of tube-shaped fibres in the form of webs or mats which lie rather close together.
Depending on batch sizes, more or less mechanical or manual methods of manufacturing the flagpole can be adopted. For manual laying up, the glass fibre webs, which in advance has been drenched with polyester, is thus laid round a mandrel. Each layer is pressed by a groove roller to compress the web and press out the air in the web, before the next layer is laid up.
Manufacturing a flagpole of glass-fibre reinforced polyester is therefore rather difficult and demanding work. In addition to this, the still not cured polyester gives off unhealthy vapours. The responsible authorities therefore demands that effective installations to exhaust the vapours and filter off unhealthy elements before the vapours are discharged into open air are installed at the working area.
A pole, such as a flagpole of glass-fibre reinforced polyester or of a similar fibre reinforced polymer, will be rather expensive due to the above-mentioned production-related circumstances.
The object of the invention is to provide a pole of the type mentioned in the opening paragraph and which is less expensive to manufacture than a pole made of glass-fibre reinforced polyester or a similar fibre reinforced polymer and which, at the same time, has just as good properties.
The novel and unique features according to the invention whereby this is achieved, is the fact that the two components form part of the material as composite fibres formed by both components . Thereby the demanding and expensive processes of the conventional methods of manufacturing fibre-reinforced polymer poles, e.g. polyester poles, are eliminated.
The composite fibres can enter into the material as rovings which consist of a large number of fibres, but at the embodiment preferred, these rovings can already be woven into a web of fibres .
When the polymer is a thermoplastic polymer, the material of a pole is recyclable and can thereby be utilised again. Thereby an advantage is furthermore obtained in that discarded poles and poles with manufacturing faults will no longer pollute the environment to the same extent as poles of e.g. glass-fibre reinforced polyester which are virtually imperishable. The invention furthermore concerns a method of manufacturing a pole of a material which is mainly made up of a first component, such as glass, and a second component, such as a polymer. The novel and unique features of this method is the fact that the two components make up composite fibres formed by both components, and that the pole is made of these composite fibres. By means of this method, for example a pole can now be manufactured in a quick and labour-saving way, and without the workers having to risk inhaling unhealthy vapours from the process.
The dependent claims 6 - 10 show advantageous methods according to the invention.
The invention will be explained in greater detail below, where only exemplary embodiments are described with reference to the drawing, in which
fig. 1 is a perspective view of a flagpole according to the invention,
fig. 2 a - g are perspective views of successive process stages of a first embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1,
fig. 3 a - c are perspective views of successive process stages of a second embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1, and
fig. 4 a - c are perspective views of successive process stages of a third embodiment of the method according to the invention of manufacturing the flagpole shown in fig. 1.
Fig. 1 shows, diagonally from the end and in perspective, a flagpole 1 according to the invention. The flagpole is, in this case, made up of a number of tube-shaped webs 2 which transversely lie close together. The web is woven from rovings each consisting of a large number of fibres. Each fibre is a composite fibre of two components, respectively glass and a polymer, such as polypropylene.
The flagpole can be manufactured in different ways as described in details in the following.
Fig. 2 a - g show a first method according to the invention of manufacturing a flagpole. In this method, the flagpole is thus constructed round a rigid mandrel 3 of for example aluminium. At its ends, the mandrel has journals 4 for rotatable suspension in a pedestal (not shown) .
In fig. 2a, a web 5 is wound round the mandrel 3 until a layer 6 having mainly the diameter of the finished pole is formed.
The web 5 is of the above-mentioned type of composite fibres of glass and a polymer respectively, in the following, the polymer is assumed to be, as an example, polypropylene.
In fig. 2b, a film 7 of a thermoplastic polymer, such as acrylic, is wrapped round the formed composite fibre layer 6. This film 7 is dyed in the wanted colour of the finished pole.
In fig. 2c, a flexible plate 8 is laid round the film 7. During the further processing, the surface of the composite fibre layer 6 with the film 7 will be formed as an impression of the surface of the plate 8 facing the composite fibre layer. Normally, flagpoles of an even, smooth surface are wanted, the surface being dirt repelling and easy cleanable, and the plate 8 must then have a correspondingly even, smooth surface . In fig. 2d, an air permeable mat 9 is laid round the already laid layers 6, 7, 8, 9. Since the mat is air permeable, it allows confined air being evacuated.
In fig. 2e, the layers 6, 7, 8, 9 are concluded with a vacuum tube 10 being put round them for compressing all the layers 6, 7, 8, 9 firmly round the mandrel when the tube is connected to a vacuum source (not shown) . Thereby, it is effectively ensured that the finished flagpole will assume the fixed form of the mandrel.
In fig. 2f, the mandrel 3 with the layers 6, 7, 8, 9, 10 is placed in a furnace 11 at a temperature of e.g. 200°C. The mandrel stays in the furnace for about 5 minutes during which the two thermoplastic polymers, in this example polypropylene and acrylic respectively, soften and assume the shape of the mandrel, simultaneously the composite fibres of the web 5 are joined whereby a solid, coherent layer 5 is formed, said layer is furthermore joined with the acrylic film 7.
The mandrel 3 with the layers 6, 7, 8, 9, 10 is then taken out of the furnace and cooled to a temperature where both the polypropylene and the acrylic transform into the solid phase, and finally, the different layers 8, 9, 10 and the mandrel 3 are removed from the now solid and joined layers 6, 7 which form the in fig. 2g shown finished flagpole 1.
Fig. 3 a, b, c show a second method according to the invention of manufacturing a flagpole. In this method, the flagpole is constructed round a flexible mandrel 12 of for example thermostable silicone rubber. The mandrel 12 is via a tube 13 with a valve 14 connected to a compressed-air source (not shown) . By opening the valve 14, the flexible mandrel 12 is put under pressure. In fig. 3a, a web 14 is wound round the mandrel 12 until a layer 15 having mainly the diameter of the finished pole is formed. The web is of the same kind as the web 5 shown in fig. 2 a-g of composite fibres of glass and polymer, respectively.
In fig. 3b, the mandrel 12 with the composite fibres 15 is placed in a mould 16 of for example aluminium. The mould 16 consists, in this case, of two halves 16 a, b which in fig. 3b are closed round the composite fibre layer 15 and the mandrel 12. The valve 14 is now opened so that the flexible mandrel 12 expands and thereby presses the composite fibre layer 15 to abut against the inside of the mould chamber which has a shape corresponding to the shape of the finished flagpole.
The mould 16 is, in advance, heated to for example 150°C. When the mould is closed and the flexible mandrel 12 put under pressure, the mould is heated further to a temperature of 200°C and kept at this temperature for a sufficient period of time, for example 5 minutes, until the polymer softens and thereby assumes the shape of the mould chamber, at the same time as the composite fibres of the web 14 are joined.
At the end of the standing time in the furnace, the mould is cooled to about 150°C at which point the plastic polymer transforms into the solid phase. The mould is then opened and the mandrel removed when the pressure has been released.
In fig. 3b, the finished flagpole 17 is taken out of the open mould 17.
Fig. 4 a, b, c show a third method according to the invention of manufacturing a flagpole.
In this case, a plate is formed, as shown in fig. 4a, said plate consisting partly of web 19 which is of the same kind as the web 5 shown in fig. 2 a - g of composite fibres of glass and polypropylene respectively, and partly of an substratum in the form of a dyed acrylic-film 20 with an even, smooth surface .
The plate 18 may be formed under pressure at a temperature of for example 200°C and with a standing time of 5 minutes during which the polypropylene softens and the composite fibres of the web 19 are joined, simultaneously the acrylic-film 20 is joined with the composite fibres.
The plate 18 is then cooled to 80° - 120°C and curved, as shown in fig. 4a with the acrylic substratum at the outside, to a jacket 21 round a rigid mandrel 22 having the shape of the wanted cavity of the finished flagpole.
Finally, the two long sides 23 a,b of the wrapping 21 are joined by a weld 24 by means of a welding gun 25 after which the finished flagpole is pulled off the mandrel. The flagpole is now the colour of the acrylic-film and has its even, smooth surface.
It is to be noted that the joining of the long sides can also be done by means of other joining methods, for example bonding or hot melting, just as the seam can be a lap weld instead of a butt joint.
In all the examples of the methods shown in the drawing and described above, it is assumed that webs of composite fibres is used in the manufacture. Within the scope of the invention, for example mats of composite fibres or composite fibres in the form of rovings can also be used depending on the circumstances .
When flagpoles are mentioned, it is further to be understood as an example, since the concept of the invention can also be applied to the manufacture of any kind of poles.

Claims

C l a i m s
1. Pole of a material which is mainly made up of a first component, such as glass, and a second component, such as a polymer, characterized in that the two components enter into the material as premade composite fibres made up of by both components .
2. Pole according to claim 1, characterized in that the premade composite fibres enter into the material as rovings.
3. Pole according to claim 1 or 2 , characterized in that the premade composite fibres enter into the material in the form of a web of rovings .
4. Pole according to claim 1, 2 or 3 , characterized in that the polymer is a thermoplastic polymer.
5. Method for the manufacture of a pole of a material which is mainly made up of a first component, such as glass, and a second component, such as a polymer, characterized in that the two components form a composite fibre which is formed by both components, and that the pole is made of these composite fibres.
6. Method according to claim 5, characterized in that rovings are made of the composite fibres, and that these rovings are woven into a web, and that the pole is made of this web.
7. Method according to claim 5 or 6 , characterized in that the polymer is a thermoplastic polymer, and that the pole is made of the composite fibres under heat stress.
8. Method according to claim 5, 6 or 7 and where the pole is hollow and the polymer thermoplastic, characterized in that a length of web woven from composite fibres in the shape of rovings is wound in a layer round a mandrel which has the shape of the cavity of the pole, that a film of a thermoplastic polymer, such as acrylic or polypropylene of the wanted colour of the pole, is wound round the formed fabric-layer, that a flexible plate which, at least on one of the sides, has a surface which corresponds with the finish of the pole, is laid up around the polymer film with said side facing the film, that an air permeable mat is laid up around the flexible plate, that a vacuum tube which is connected to a vacuum source is wrapped around the mat, thereby compressing the remainding layers firmly around the mandrel, that the in this way formed unit is heated for a sufficient period of time in for example a furnace, that the heated unit is subsequently cooled, and that the mandrel, the vacuum tube, the mat and the flexible plate are removed.
9. Method according to claim 5, 6 or 7 and where the pole is hollow and the polymer thermoplastic, c h a r a c t e r i z e d in that a length of web woven from composite fibres in the shape of rovings is wound in a layer round an elastomeric mandrel of for example silicone rubber, that the wrapped elastomeric mandrel is placed in a, to the wanted configuration of the pole, corresponding cavity in a hot mould, that the elastomeric mandrel is put under pressure by for example air, that the wrapped elastomeric mandrel is kept in the hot mould for a predetermined period, that the wrapped elastomeric mandrel is cooled in the mould, that the mould is opened and the mandrel is removed when the pressure has been released in the mandrel .
10. Method according to claim 5, 6 or 7 and where the pole is hollow and the polymer thermoplastic, characterized in that a plate is formed, under heat stress, of web woven from composite fibres in the form of rovings, said plate having mainly the same thickness as the wanted wall thickness of the pole and the same length as the finished pole, that the plate during cooling is folded round the mandrel which has the shape of the cavity of the pole, so that the long sides of the plate are brought close together or to touch each other, that the long sides are joined by means of for example bonding or welding, and that the mandrel is pulled out.
AMENDED CLAIMS
[received by the International Bureau on 10 March 1998 (10.03.98) ; original claims 1-10 replaced by amended claims 1-4 (.2 pages) ]
1 . Method for manufacturing a hollow pole of composite fibres which consist of at least a f irst component , such as glass , and a second component , such as a thermoplastic polymer , characterized in that the method comprises that the pole under thermal stress is formed of said composite fibres in the shape of a fabric around a mandrel .
2. Method according to claim 1, characterized in that said fabric is wound in a layer round a mandrel which has the shape of the cavity of the pole, that a film of a thermoplastic polymer, such as acrylic or polypropylene of the wanted colour of the pole, is wound round the formed fabric-layer, that a flexible plate which, at least on one of the sides, has a surface which corresponds with the finish of the pole, is laid up around the polymer film with said side facing the film, that an air permeable mat is laid up around the flexible plate, that a vacuum tube which is connected to a vacuum source is wrapped around the mat, thereby compressing the remaining layers firmly around the mandrel, that the unit, formed in this way, is heated for a sufficient period of time in for example a furnace, that the heated unit is subsequently cooled, and that the mandrel, the vacuum tube, the mat and the flexible plate are removed.
3. Method according to claim 1, characterized in that said fabric is wound in a layer around an elastomeric mandrel of for example silicone rubber, that the wrapped elastomeric mandrel is placed in a cavity, corresponding to the wanted configuration of the pole, in a hot mould, that the elastomeric mandrel is put under pressure by for example air, that the wrapped elastomeric mandrel is kept in the hot mould for a predetermined period, that the wrapped elastomeric mandrel is cooled in the mould, that the mould is opened and the mandrel is removed when the pressure has been released in the mandrel .
4. Method according to claim 1, characterized in that a plate is formed, under thermal stress, of said fabric, said plate having mainly the same thickness as the wanted wall thickness of the pole and the same length as the finished pole, that the plate during cooling is folded round the mandrel which has the shape of the cavity of the pole, so that the long sides of the plate are brought close together or to touch each other, that the long sides are joined by means of for example bonding or welding, and that the mandrel is pulled out.
PCT/DK1997/000431 1996-10-14 1997-10-08 Pole and method for its manufacture WO1998016376A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP97943789A EP0930965A1 (en) 1996-10-14 1997-10-08 Pole and method for its manufacture
CA002269548A CA2269548A1 (en) 1996-10-14 1997-10-08 Pole and method for its manufacture
AU45502/97A AU4550297A (en) 1996-10-14 1997-10-08 Stang og fremgangsmade til fremstilling af stangen
NO991730A NO991730L (en) 1996-10-14 1999-04-13 Rod and method of manufacture thereof

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DK1137/96 1996-10-14
DK113796 1996-10-14

Publications (2)

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WO1998016376A1 true WO1998016376A1 (en) 1998-04-23
WO1998016376A8 WO1998016376A8 (en) 1999-07-08

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AU (1) AU4550297A (en)
CA (1) CA2269548A1 (en)
NO (1) NO991730L (en)
PL (1) PL332630A1 (en)
WO (1) WO1998016376A1 (en)

Cited By (3)

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Publication number Priority date Publication date Assignee Title
US20120211978A1 (en) * 2011-02-23 2012-08-23 Gardiner Pole Systems Limited Pole Assembly
GB2565032A (en) * 2017-04-27 2019-02-06 James Dobberson Geoffrey Moulding procedure to incorporate flag material within a tubular spine for full visibility flag
WO2019214951A1 (en) * 2018-05-11 2019-11-14 Herone Gmbh Device and method for continuously blow molding fiber-reinforced thermoplastic hollow profiles having a constant or changing cross-section

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4101613A1 (en) * 2021-06-11 2022-12-14 EcoTelligent Oy Laminated wooden pole and its manufacturing method

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WO1992001885A1 (en) * 1990-07-19 1992-02-06 Wavin B.V. Composite pipe with one or more layers of strip material wound around an inner pipe and reel provided with such a composite pipe wound onto it
WO1995007428A1 (en) * 1993-09-06 1995-03-16 Neste Oy Thermoplastic composite pipe
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DE1779262A1 (en) * 1968-07-25 1971-10-07 Siempelkamp Gmbh & Co Process for the production of molded parts reinforced with glass fiber from thermoplastics and prepress material for this purpose
DE3226220A1 (en) * 1982-07-14 1984-01-26 Julius Cronenberg Ohg, 5760 Arnsberg Mould and process for manufacturing conical masts from glass fibre-reinforced plastic
WO1989000917A1 (en) * 1987-07-28 1989-02-09 Oy Nettec Ab A fibre reinforced tube element and a method for its manufacture
WO1989005229A1 (en) * 1987-12-09 1989-06-15 Quadrax Corporation Multi-directional, light-weight, high-strength interlaced material and method of making the material
EP0367661A1 (en) * 1988-10-28 1990-05-09 Vetrotex Saint-Gobain Method and apparatus for producing a thread or ribbon made of reinforcing fibres and an organic thermoplastic material
GB2237583A (en) * 1989-09-27 1991-05-08 Plastic Developments Ltd Fibre reinforced thermoplastic composites
WO1992001885A1 (en) * 1990-07-19 1992-02-06 Wavin B.V. Composite pipe with one or more layers of strip material wound around an inner pipe and reel provided with such a composite pipe wound onto it
WO1995007428A1 (en) * 1993-09-06 1995-03-16 Neste Oy Thermoplastic composite pipe
WO1996024413A1 (en) * 1994-12-20 1996-08-15 Radius Engineering, Inc. Composite pole

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120211978A1 (en) * 2011-02-23 2012-08-23 Gardiner Pole Systems Limited Pole Assembly
GB2565032A (en) * 2017-04-27 2019-02-06 James Dobberson Geoffrey Moulding procedure to incorporate flag material within a tubular spine for full visibility flag
GB2565032B (en) * 2017-04-27 2022-02-16 James Dobberson Geoffrey Moulding procedure to incorporate flag material within a tubular spine for full visibility flag
US11667068B2 (en) 2018-03-11 2023-06-06 Herone Gmbh Device and method for continuously blow molding fiber-reinforced thermoplastic hollow profiles having a constant or changing cross-section
WO2019214951A1 (en) * 2018-05-11 2019-11-14 Herone Gmbh Device and method for continuously blow molding fiber-reinforced thermoplastic hollow profiles having a constant or changing cross-section

Also Published As

Publication number Publication date
NO991730D0 (en) 1999-04-13
CA2269548A1 (en) 1998-04-23
EP0930965A1 (en) 1999-07-28
NO991730L (en) 1999-04-13
WO1998016376A8 (en) 1999-07-08
PL332630A1 (en) 1999-09-27
AU4550297A (en) 1998-05-11

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