WO2009150298A1 - A method to produce engineered composite articles comprising epoxy and carbon nano tubes - Google Patents
A method to produce engineered composite articles comprising epoxy and carbon nano tubes Download PDFInfo
- Publication number
- WO2009150298A1 WO2009150298A1 PCT/FI2009/050492 FI2009050492W WO2009150298A1 WO 2009150298 A1 WO2009150298 A1 WO 2009150298A1 FI 2009050492 W FI2009050492 W FI 2009050492W WO 2009150298 A1 WO2009150298 A1 WO 2009150298A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- mould
- epoxy
- film
- blade
- carbon nano
- Prior art date
Links
- 239000004593 Epoxy Substances 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims abstract description 28
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims abstract description 26
- 239000002041 carbon nanotube Substances 0.000 title claims abstract description 26
- 229910021393 carbon nanotube Inorganic materials 0.000 title claims abstract description 26
- 239000002131 composite material Substances 0.000 title claims abstract description 22
- 239000011347 resin Substances 0.000 claims abstract description 16
- 229920005989 resin Polymers 0.000 claims abstract description 16
- 238000004519 manufacturing process Methods 0.000 claims abstract description 14
- 239000003292 glue Substances 0.000 claims abstract description 8
- 239000011343 solid material Substances 0.000 claims abstract description 3
- 239000011162 core material Substances 0.000 claims description 21
- 239000000463 material Substances 0.000 claims description 10
- 239000007788 liquid Substances 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 9
- 239000003365 glass fiber Substances 0.000 claims description 8
- 239000007787 solid Substances 0.000 claims description 8
- 238000009472 formulation Methods 0.000 claims description 6
- 229920000647 polyepoxide Polymers 0.000 claims description 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 5
- 239000004952 Polyamide Substances 0.000 claims description 5
- 239000004917 carbon fiber Substances 0.000 claims description 5
- 239000003822 epoxy resin Substances 0.000 claims description 5
- 229920001169 thermoplastic Polymers 0.000 claims description 5
- 239000004416 thermosoftening plastic Substances 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 229920002647 polyamide Polymers 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 239000000047 product Substances 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 claims description 3
- 229920002725 thermoplastic elastomer Polymers 0.000 claims description 3
- 229920002803 thermoplastic polyurethane Polymers 0.000 claims description 3
- 239000004964 aerogel Substances 0.000 claims description 2
- 239000004411 aluminium Substances 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 239000012467 final product Substances 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 claims description 2
- 230000005923 long-lasting effect Effects 0.000 claims 1
- 239000012779 reinforcing material Substances 0.000 claims 1
- 230000002441 reversible effect Effects 0.000 claims 1
- 230000008901 benefit Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 150000002924 oxiranes Chemical class 0.000 description 4
- 239000004848 polyfunctional curative Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 239000006260 foam Substances 0.000 description 3
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 3
- 239000004800 polyvinyl chloride Substances 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 229920001187 thermosetting polymer Polymers 0.000 description 3
- VILCJCGEZXAXTO-UHFFFAOYSA-N 2,2,2-tetramine Chemical compound NCCNCCNCCN VILCJCGEZXAXTO-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- IISBACLAFKSPIT-UHFFFAOYSA-N bisphenol A Chemical compound C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 IISBACLAFKSPIT-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000000178 monomer Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 229920000768 polyamine Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 229920000915 polyvinyl chloride Polymers 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- BRLQWZUYTZBJKN-UHFFFAOYSA-N Epichlorohydrin Chemical compound ClCC1CO1 BRLQWZUYTZBJKN-UHFFFAOYSA-N 0.000 description 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- 239000004433 Thermoplastic polyurethane Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 125000003277 amino group Chemical group 0.000 description 1
- 229940106691 bisphenol a Drugs 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000004850 liquid epoxy resins (LERs) Substances 0.000 description 1
- 239000011344 liquid material Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- -1 reinforcement Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009745 resin transfer moulding Methods 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 239000012265 solid product Substances 0.000 description 1
- 229920006345 thermoplastic polyamide Polymers 0.000 description 1
- 239000004634 thermosetting polymer Substances 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
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
- B29C70/58—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y30/00—Nanotechnology for materials or surface science, e.g. nanocomposites
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/005—Reinforced macromolecular compounds with nanosized materials, e.g. nanoparticles, nanofibres, nanotubes, nanowires, nanorods or nanolayered materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G6/00—Devices for producing mechanical power from solar energy
- F03G6/02—Devices for producing mechanical power from solar energy using a single state working fluid
- F03G6/04—Devices for producing mechanical power from solar energy using a single state working fluid gaseous
- F03G6/045—Devices for producing mechanical power from solar energy using a single state working fluid gaseous by producing an updraft of heated gas or a downdraft of cooled gas, e.g. air driving an engine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/16—Fillers
- B29K2105/165—Hollow fillers, e.g. microballoons or expanded particles
- B29K2105/167—Nanotubes
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
- Y02E10/46—Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Definitions
- This invention relates to a method according to the preamble of claim 1.
- the technical field is characterized by the keywords: composites, thermosets, reinforcement, carbon fibers (CF) , carbon nano tubes (CNT), production of composites, windmill blades, propellers, sporting goods such as skis, automotive and industrial parts, production methods.
- the invention relates also to a windmill blade or similar composite article.
- Epoxy mixtures with CNT are known, in particular under the trade name Hybtonite® by the company Amroy (FI) . Descriptions can be found e.g. in the prior art WO 2006/040398 Al. Hybtonite® is already used in the manufacture of large wind mill blades and other composite articles. The production process for wind mill blades typically involves one mould into which solids are placed such as long glass fibers. Thereafter, a liquid epoxy formulation is pumped into the mould, and typically vacuum has to be applied to ensure that the liquid fills all empty spaces prior to heating up the complete mould.
- EP 1859920 Al discloses a method to vent residual gas through at least one venting duct which may contain a semi-permeable membrane.
- the usually employed technique to produce long composite articles such as windmill blades is (vacuum-assisted) resin transfer moulding (RTM) .
- RTM resin transfer moulding
- the wind mill blade is painted or gel-coated in order to provide a surface finish and to protect the structure from weather influences and sunlight.
- Epoxy or polyepoxide is a thermosetting polymer formed from reaction of an epoxide "resin” with polyamine “hardener”.
- Epoxy has a wide range of applications, including fiber-reinforced plastic materials and general purpose adhesives.
- Epoxy is a copolymer; that is, it is formed from two different chemicals. These are referred to as the "resin” and the “hardener”.
- the resin consists of monomers or short chain polymers with an epoxide group at either end. Most common epoxy resins are produced from a reaction between epichlorohydrin and bisphenol-A, though the latter may be replaced by similar chemicals.
- the hardener consists of polyamine monomers, for example Triethylenetetramine (TETA) . When these compounds are mixed together, the amine groups react with the epoxide groups to form a covalent bond. Each NH group can react with an epoxide group, so that the resulting polymer is heavily crosslinked, and is thus rigid
- curing The process of polymerization is called "curing", and can be controlled through temperature and choice of resin and hardener compounds; the process can take minutes to hours. Some formulations benefit from heating during the cure period, whereas others simply require time, and ambient temperatures.
- the costs for raw materials can be high.
- the costs for moulding are usually high because either pressure or vacuum equipment or both is needed in order first pump liquid raw material into the mould and to secondly ensure that no gas is trapped within the finished article.
- the surface quality and appearance of the finished article is often of low quality, and this requires after-work such as gel-coating or painting.
- the stability and mechanical properties, or the weight/strength ratio is insufficient.
- blades of extremely low weight such as weighing 2,5 kg or less for a blade length of 2 m are required. These are not available today.
- composite articles show a favorable life-cycle analysis (LCA) .
- LCA life-cycle analysis
- the object of this invention is to achieve an improved method for producing engineered composite articles comprising epoxy resins and carbon nano tubes. This object is achieved with the features described in accompanying claim 1.
- the traditional need for evacuating the mould or the need for transferring liquid resin using pressure pumps is obviated.
- the film is under any circumstances fully polymerized ("fully cured") .
- a good bonding is achieved because a) The film is highly compatible with the epoxy system, and/or b) Excess resin fills the film at least partly - whereas the resin, however, will not migrate through the whole film.
- the good compability means that the epoxy resin wets the surface of the film. This will be true for thermoplastic elastomer, polyamide, polyacryle, polyvinylchloride (PVC) , polystyrene, and many other thermoplastics or their mixtures. In other words compatibility is defined here in terms of surface tension. On the contrary silicone and water, or polyester to take a plastic, are NOT compatible.
- thermoplastic may need a pre-treatment for reaching said compability.
- PVC-layer isn't directly compatible with epoxy.
- PVC may be provide first a layer like paper, which is compatible both PVC and epoxy.
- the surface quality is given by the surface quality of the film, and by the contact between film and the mould halves. It is not expected that a gel coat or any further finishing step apart from trimming edges (where excess resin has left the mould) is needed.
- mould release agents are also obviated, alternatively non-fluorinated release agents can be used, thereby reducing costs and environmental performance.
- paraffinic waxes are suitable. Liquid epoxy resin will not permeate through such films and will therefore not adhere later to the mould surface.
- the films can be equipped directly with company logos or colour patterns.
- the film has also the function of enclosing the resin containing functionalized CNT. Without a film, there would be a risk of contamination of the mould with CNT, a rougher surface might result because resin/CNT would stick to the mould and create an irregular surface.
- windmill blades and similar composite articles are produced in the following manner: a mould is provided, equipped with a film which later shall at least partly form part of the windmill blade. The film is wetted with glue.
- the mould is further loaded with reinforcing structures such as glass fiber mats, light- weight core material and elements which allow the windmill blades to be connected to the rotor.
- the mould is closed whereby the core material may be oversized in comparison to the mould volume.
- the subsequent partial crushing of the core structure ensures that all remaining liquid epoxy fills all voids in the mould.
- the complete mould is heated until the material is cured. No mould evacuation is necessary. Also, the need for using pressure pumps to transfer liquid resin into the mould is obviated.
- Life-cycle analysis as the windmill blade contains less solid materials and more combustible materials, the product can be burned after use leaving less ash and solid products.
- Figure 1 presents open mould halves for receiving film and other required materials
- Figure 2 presents mould halves in a closing stage
- Figure 3 presents another mould in the heating phase
- a mould (10) comprising two mould halves (1) is provided which are connected by an axis (2), Fig. 1. Film and solid components and resin are laid into one mould half whereupon the mould (10) is closed for curing. Film (3) may cover both mould halves (1) .
- the film covers at least 50%, but preferably at least 90% of the surface of the open mould (10) .
- Thermoplastic, like polyamide of film has preferably high melting point and pre-treated to reach said compability. If multi-layer film is used, the outer layer is impermeable, while others allow unpolymerized epoxy migrate through to the outer layer.
- film (3) is used to fill at least part of the inner mould surface, ideally on both sides.
- Solid light-weight components (4) are used to fill the mould, as well as liquid resin (5) to fill voids and to provide binding between the solids and the film.
- the mould is closed as indicated by arrow (6) .
- the film (3) is impermeable at least to the extent that unpolymerized epoxy is prevented from migrating through the film to the mould.
- the film has preferably with excellent compatibility with and adhesion to epoxy resins.
- epoxy formulations containing functionalized Carbon Nano Tubes are used in amounts of at least 1% of the final product weight, such as at least 2% or such as at least 5% or more.
- Aerogel, honeycomb structures, or other materials of a specific weight not exceeding 100 kg/m 3 is used as light weight core material, preferably the specific weight not exceeding 60 kg/m 3 .
- the closed mould is heated to afford polymerisation or curing of the resin system used, Fig. 3.
- connectors (6) have been inserted. They extend well into the wind mill blade as indicated by extensions (7) .
- the outer part (6) may be detachable from the inner part (7) e.g. by a screw connection.
- film is forming an integral part of a rigid composite structure, and that a part of the film used in the composite is covering a part of the outer surface of the composite.
- the exceptional strength of film and its tolerance to defects such as mechanical damage helps to produce durable light-weight composites on the basis of sustainable raw materials.
- a mould is provided, ideally in two halves made of metal such as aluminium.
- the mould is equipped with a film or a foil which later at least partly forms an integral part of the composite.
- the film material may be e.g. a thermoplastic polyurethane or polyamide and may be e.g. 0,75 mm in thickness (generally each layer 0,2 - 1,0 mm) .
- the film may consist of more than one layer whereby the top layer can be removed after the moulding process and serves otherwise as protective film.
- Glue containing epoxy and functionalized CNT commercially available as Hybtonite®, is spread on the foil or the film.
- epoxy formulations contain preferably carbon nano tubes (CNT) with covalent bondings.
- the film may be partly porous or microporous such that liquid glue impregnates the film, such that a better adhesion is achieved between the film and the glue.
- Said porous or microporous film (3) which is used to cover the inner surfaces of the mould halves (1) has a thickness of at least 30 micrometer, but preferably at least 200 micrometer and most preferably 750 micrometer. It is made of thermoplastic urethane, thermoplastic elastomer or thermoplastic such as polyamide (particularly with melting point about 100 0 C) .
- thermoplastic urethane thermoplastic elastomer or thermoplastic such as polyamide (particularly with melting point about 100 0 C) .
- a laminate such as consisting of glass or carbon fiber, in the form of woven or non-woven laminate or pre-impregnated (pre-cured) structures is placed in the mould.
- a light weight core is placed in the mould.
- a bar which shall connect the core or the blade to the rotor of the wind power installation is placed in the mould in such a way that a good mechanical connection is achieved.
- the core may be cut out appropriately leaving space for the bar which in itself preferably is a cured glass fiber composite material.
- the said laminate structures or mats preferably cover the bar completely such that additional stability and fastening between the blade and the rotor is achieved.
- the core material is oversize compared with the mould volume such that closure of the mould leads to partial crushing of the core material. This is intentional as liquid material is pressed into remaining open spaces of the mould, and also a good cross- linking between the core and the thermosetting epoxy is achieved. Furthermore, any trapped air, or most of the trapped air, is pressed into the light weight core.
- the moulds may be held together by simple clamps.
- the closed moulds are heated e.g. for 30 min at 75-100 0 C whereby the lower temperature often results in a better surface quality.
- the blades may provided with stickers such as advertising emblems. Providing gel-coat or paint is only optionally and usually avoided due to the perfect surface of the film.
- the production process is highly economical and suitable for windmill blades of any length.
- the connecting bar i.e. the bar which connects the blade to the rotor of the wind power generator, may consist of pre-cured glassfiber and epoxy or similar hard material, and the connection to the rotor may be preferably by at least two metal rods having diameters of at least 10 mm for blades of 2 m length (and accordingly stronger for longer blades) .
- the solid bar is connected to the light weight core using glue such as containing epoxy and CNT.
- the blade can turn automatically away from the wind or expose only a minimum part of its surface to the wind. This can be achieved by fastening the rods into an arrangement which can rotate in the axis or parallel to the axis given by the long blade axis. Elastic components such as rubber parts or springs ensure that the blade is either moving away from the wind, or is returning to its default position of maximum wind power utilization.
Abstract
The invention relates to a method for producing composite articles containing epoxy and functionalized carbon nano tubes (CNT). The method comprises the following steps: a closable mould (10) is provided the mould having open and close positions, the inner parts of the open mould (10) is equipped with a film (3), which has compatibility with said epoxy and it is impermeable at least to the extent that resin is prevented from migrating through the film to the mould, the open mould (10) is further filled with glue containing epoxy and said functionalized carbon nano tubes, solid materials and elements enabling the mechanical connection to other machine elements, the mould (10) is closed and heated until the finished article is sufficiently stable.
Description
A METHOD TO PRODUCE ENGINEERED COMPOSITE ARTICLES COMPRISING EPOXY AND CARBON NANO TUBES
Background of the invention
Field of the invention
This invention relates to a method according to the preamble of claim 1. The technical field is characterized by the keywords: composites, thermosets, reinforcement, carbon fibers (CF) , carbon nano tubes (CNT), production of composites, windmill blades, propellers, sporting goods such as skis, automotive and industrial parts, production methods. The invention relates also to a windmill blade or similar composite article.
Description of the related art
Document US 3873654 presents a process of forming a rigid foam airfoil section. An oversized foam core is compressed between slit molds, which have partially cured epoxy-coated fibreglass cloth laid up in both halves of the molds. Thus, this assures a good bond between the cloth and foam core during the final curing process. Similar process has been presented in document US 4,639,284.
Epoxy mixtures with CNT are known, in particular under the trade name Hybtonite® by the company Amroy (FI) . Descriptions can be found e.g. in the prior art WO 2006/040398 Al. Hybtonite® is already used in the manufacture of large wind mill blades and other composite articles. The production process for wind mill blades typically involves one mould into which solids are placed such as long glass fibers. Thereafter, a liquid epoxy formulation is pumped into the mould, and typically vacuum has to be applied to ensure that the liquid fills all empty spaces prior to heating up the complete mould. EP 1859920 Al discloses a method to vent residual gas through at least one venting duct which may contain a semi-permeable membrane. The usually employed technique to produce long composite
articles such as windmill blades is (vacuum-assisted) resin transfer moulding (RTM) . After curing at elevated temperature, the wind mill blade is painted or gel-coated in order to provide a surface finish and to protect the structure from weather influences and sunlight.
Epoxy or polyepoxide is a thermosetting polymer formed from reaction of an epoxide "resin" with polyamine "hardener". Epoxy has a wide range of applications, including fiber-reinforced plastic materials and general purpose adhesives. Epoxy is a copolymer; that is, it is formed from two different chemicals. These are referred to as the "resin" and the "hardener". The resin consists of monomers or short chain polymers with an epoxide group at either end. Most common epoxy resins are produced from a reaction between epichlorohydrin and bisphenol-A, though the latter may be replaced by similar chemicals. The hardener consists of polyamine monomers, for example Triethylenetetramine (TETA) . When these compounds are mixed together, the amine groups react with the epoxide groups to form a covalent bond. Each NH group can react with an epoxide group, so that the resulting polymer is heavily crosslinked, and is thus rigid and strong.
The process of polymerization is called "curing", and can be controlled through temperature and choice of resin and hardener compounds; the process can take minutes to hours. Some formulations benefit from heating during the cure period, whereas others simply require time, and ambient temperatures.
Problems with prior art
Disadvantages of the compositions and the manufacturing process for wind mill blades and similar composites, are: The costs for raw materials can be high. The costs for moulding are usually high because either pressure or vacuum equipment or both is needed in order first pump liquid raw material into the mould and to secondly ensure that no gas is trapped within the finished article. The surface quality and appearance of the finished article is often of low quality, and this requires after-work such as gel-coating or painting. In particular the stability and mechanical properties, or
the weight/strength ratio is insufficient. In order to generate electricity from wind power especially at low wind speeds and with smaller installations such as cottage houses in the countryside, blades of extremely low weight such as weighing 2,5 kg or less for a blade length of 2 m are required. These are not available today.
Usually there is a need for mould release agents, which cause costs and environmental problem.
Finally, it is desirable that composite articles show a favorable life-cycle analysis (LCA) . After use, composite articles should contain high concentrations of materials, which either are biologically degradable, or combustible leaving a minimum amount of ash. From the foregoing it should be apparent that there is a need to provide methods to produce light weight windmill blades and composite articles at lower cost than possible today, combined with improvements in terms of LCA.
Summary of the invention The object of this invention is to achieve an improved method for producing engineered composite articles comprising epoxy resins and carbon nano tubes. This object is achieved with the features described in accompanying claim 1. The traditional need for evacuating the mould or the need for transferring liquid resin using pressure pumps is obviated.
The film is under any circumstances fully polymerized ("fully cured") . A good bonding is achieved because a) The film is highly compatible with the epoxy system, and/or b) Excess resin fills the film at least partly - whereas the resin, however, will not migrate through the whole film.
The good compability means that the epoxy resin wets the surface of the film. This will be true for thermoplastic elastomer, polyamide, polyacryle, polyvinylchloride (PVC) , polystyrene, and many other thermoplastics or their mixtures. In other words compatibility is defined here in terms of surface tension. On the contrary silicone
and water, or polyester to take a plastic, are NOT compatible.
Certain thermoplastic may need a pre-treatment for reaching said compability. For example, PVC-layer isn't directly compatible with epoxy. PVC may be provide first a layer like paper, which is compatible both PVC and epoxy.
The surface quality is given by the surface quality of the film, and by the contact between film and the mould halves. It is not expected that a gel coat or any further finishing step apart from trimming edges (where excess resin has left the mould) is needed.
The need for mould release agents is also obviated, alternatively non-fluorinated release agents can be used, thereby reducing costs and environmental performance. For example, to allow the easy release of polyolefin films from a mould surface, paraffinic waxes are suitable. Liquid epoxy resin will not permeate through such films and will therefore not adhere later to the mould surface. A further benefit is that the films can be equipped directly with company logos or colour patterns. The film has also the function of enclosing the resin containing functionalized CNT. Without a film, there would be a risk of contamination of the mould with CNT, a rougher surface might result because resin/CNT would stick to the mould and create an irregular surface.
In this invention, windmill blades and similar composite articles are produced in the following manner: a mould is provided, equipped with a film which later shall at least partly form part of the windmill blade. The film is wetted with glue. The mould is further loaded with reinforcing structures such as glass fiber mats, light- weight core material and elements which allow the windmill blades to be connected to the rotor. The mould is closed whereby the core material may be oversized in comparison to the mould volume. The subsequent partial crushing of the core structure ensures that all remaining liquid epoxy fills all voids in the mould. After closure of the mould, the complete mould is heated until the material is cured. No mould evacuation is necessary. Also, the need for using pressure pumps to transfer liquid resin into the mould is obviated.
Advantages
Advantages of the invention can be summarized as follows:
Improved mechanical properties: strength, elongation at break, elasticity, fatigue resistance, and the like are greatly improved when comparing articles of the same weight.
Low investment costs: the production process is cheaper because an investment in vacuum or pressure technology is not needed. The production process is not at all complex and does not require highly skilled workforce.
Life-cycle analysis: as the windmill blade contains less solid materials and more combustible materials, the product can be burned after use leaving less ash and solid products.
Brief description of Figures
Figure 1 presents open mould halves for receiving film and other required materials
Figure 2 presents mould halves in a closing stage Figure 3 presents another mould in the heating phase
Detailed description of preferred embodiments
The following description of a preferred embodiment shall only illustrate the principle of the invention and is not meant to be restrictive .
A mould (10) comprising two mould halves (1) is provided which are connected by an axis (2), Fig. 1. Film and solid components and resin are laid into one mould half whereupon the mould (10) is closed for curing. Film (3) may cover both mould halves (1) . The film covers at least 50%, but preferably at least 90% of the surface of the open mould (10) . Thermoplastic, like polyamide of film has preferably high melting point and pre-treated to reach said compability. If multi-layer film is used, the outer layer is
impermeable, while others allow unpolymerized epoxy migrate through to the outer layer.
Referring now to Fig. 2 film (3) is used to fill at least part of the inner mould surface, ideally on both sides. Solid light-weight components (4) are used to fill the mould, as well as liquid resin (5) to fill voids and to provide binding between the solids and the film. After filling, in this case the right mould half, the mould is closed as indicated by arrow (6) . The film (3) is impermeable at least to the extent that unpolymerized epoxy is prevented from migrating through the film to the mould. The film has preferably with excellent compatibility with and adhesion to epoxy resins.
Preferably epoxy formulations containing functionalized Carbon Nano Tubes (CNT) are used in amounts of at least 1% of the final product weight, such as at least 2% or such as at least 5% or more. Aerogel, honeycomb structures, or other materials of a specific weight not exceeding 100 kg/m3 is used as light weight core material, preferably the specific weight not exceeding 60 kg/m3.
The closed mould is heated to afford polymerisation or curing of the resin system used, Fig. 3. To allow fastening of the article (e.g. a wind mill blade), connectors (6) have been inserted. They extend well into the wind mill blade as indicated by extensions (7) . The outer part (6) may be detachable from the inner part (7) e.g. by a screw connection.
These examples shall only illustrate the principle of the invention and are not meant to be restrictive. The important features are that film is forming an integral part of a rigid composite structure, and that a part of the film used in the composite is covering a part of the outer surface of the composite. The exceptional strength of film and its tolerance to defects such as mechanical damage helps to produce durable light-weight composites on the basis of sustainable raw materials.
A mould is provided, ideally in two halves made of metal such as aluminium. The mould is equipped with a film or a foil which later
at least partly forms an integral part of the composite. The film material may be e.g. a thermoplastic polyurethane or polyamide and may be e.g. 0,75 mm in thickness (generally each layer 0,2 - 1,0 mm) .
In a variation, the film may consist of more than one layer whereby the top layer can be removed after the moulding process and serves otherwise as protective film. Glue containing epoxy and functionalized CNT, commercially available as Hybtonite®, is spread on the foil or the film. Thus, epoxy formulations contain preferably carbon nano tubes (CNT) with covalent bondings.
The film may be partly porous or microporous such that liquid glue impregnates the film, such that a better adhesion is achieved between the film and the glue.
Said porous or microporous film (3) which is used to cover the inner surfaces of the mould halves (1) has a thickness of at least 30 micrometer, but preferably at least 200 micrometer and most preferably 750 micrometer. It is made of thermoplastic urethane, thermoplastic elastomer or thermoplastic such as polyamide (particularly with melting point about 100 0C) . When the film is provided as multi-layer film, one or more of such layers improving the heat transfer from the mould, or one or more of such layers serving as protective films being detachable after formation of the product, this operation enables the production of windmill blades with optical structures such as logos at excellent surface quality
A laminate such as consisting of glass or carbon fiber, in the form of woven or non-woven laminate or pre-impregnated (pre-cured) structures is placed in the mould. A light weight core is placed in the mould. Preferably Divinycell® HP 60 having a specific weight of 60 kg m3 is used. A bar which shall connect the core or the blade to the rotor of the wind power installation is placed in the mould in such a way that a good mechanical connection is achieved. For this purpose, the core may be cut out appropriately leaving space for the bar which in itself preferably is a cured glass fiber composite material. The said laminate structures or mats preferably cover the
bar completely such that additional stability and fastening between the blade and the rotor is achieved. When the mould is fully loaded, the mould halves are closed.
In one embodiment, it is advantageous to build up the structure in one half of the mould and to cover the complete structure with the CAP film before the second (empty) half of the mould is placed onto the first half. Excess film may be cut off before or after heating. Preferably the core material is oversize compared with the mould volume such that closure of the mould leads to partial crushing of the core material. This is intentional as liquid material is pressed into remaining open spaces of the mould, and also a good cross- linking between the core and the thermosetting epoxy is achieved. Furthermore, any trapped air, or most of the trapped air, is pressed into the light weight core. The moulds may be held together by simple clamps.
The closed moulds are heated e.g. for 30 min at 75-100 0C whereby the lower temperature often results in a better surface quality. After production and removal from the mould, the blades may provided with stickers such as advertising emblems. Providing gel-coat or paint is only optionally and usually avoided due to the perfect surface of the film.
The production process is highly economical and suitable for windmill blades of any length.
The connecting bar, i.e. the bar which connects the blade to the rotor of the wind power generator, may consist of pre-cured glassfiber and epoxy or similar hard material, and the connection to the rotor may be preferably by at least two metal rods having diameters of at least 10 mm for blades of 2 m length (and accordingly stronger for longer blades) . Preferably the solid bar is connected to the light weight core using glue such as containing epoxy and CNT.
To avoid a too high load onto the blade at high wind speeds, it is preferable that the blade can turn automatically away from the wind
or expose only a minimum part of its surface to the wind. This can be achieved by fastening the rods into an arrangement which can rotate in the axis or parallel to the axis given by the long blade axis. Elastic components such as rubber parts or springs ensure that the blade is either moving away from the wind, or is returning to its default position of maximum wind power utilization.
Claims
1. A method to produce composite articles of an absolute length to maximum thickness ratio of at least 20:1 such as windmill blades, said articles containing polymerized epoxy and functionalized carbon nano tubes (CNT), said method comprising the following steps: a closable mould (10) is provided, the mould having open and close positions, the inner parts of the open mould (10) is equipped with a film (3) covering at least 50%, but preferably at least 90% of the surface of the open mould (10) , the open mould (10) is further filled with glue containing unpolymerized epoxy and said functionalized carbon nano tubes, solid materials such as glass or carbon fiber materials, laminates, light weight core material and elements enabling the mechanical connection to other machine elements such as a rotor, the mould (10) is closed and heated until epoxy has been polymerized and the finished article is sufficiently stable, such as at 75 - 100 0C for about 30 minutes, - characterized in that the film (3) has compatibility with said epoxy and it is impermeable at least to the extent that unpolymerized epoxy is prevented from migrating through the film to the mould.
2. A method according to claim 1, wherein aerogel, honeycomb structures, or other materials of a specific weight not exceeding 100 kg/m3 is used as light weight core material, preferably the specific weight not exceeding 60 kg/m3.
3. A method according to claim 1 or claim 2, wherein the mould (10) is filled with an excess of at least 1% (volume/volume) of light weight core material is used, and where the closure of the mould leads to a partial crushing of said light weight core material, said crushing enabling partly a better bonding of the light weight core to the epoxy resin, and enabling partly the filling of all empty spaces by liquid resin.
4. A method according to any of the preceding claims, wherein said epoxy formulations contains carbon nano tubes (CNT) with covalent bondings .
5. A method according to any of the preceding claims, wherein the optionally porous or microporous film (3) which is used to cover the inner surfaces of the mould halves (1) is having a thickness of at least 30 micrometer, but preferably at least 200 micrometer and most preferably 750 micrometer, and is made of thermoplastic urethane, thermoplastic elastomer or thermoplastic such as polyamide.
6. A method according to any of the preceding claims, wherein the film is provided as multi-layer film, where the outer layer is impermeable, while others allow unpolymerized epoxy migrate through to the outer layer.
7. A method according to claim 6, wherein one or more of such layers improving the heat transfer from the mould.
8. A method according to claim 6, wherein one or more of such layers are serving as protective films being detachable after formation of the product, said mode of operation enabling the production of windmill blades with optical structures such as logos at excellent surface quality.
9. A method according to any of the preceding claims, wherein epoxy formulations containing functionalized Carbon Nano Tubes (CNT) are used in amounts of at least 1% of the final product weight, such as at least 2% or such as at least 5% or more.
10. A method according to any of the preceding claims, wherein a solid bar, e.g. consisting of a cured glass or carbon fiber structure containing one or more, preferably two metal rods, is used to connect the light weight core of the windmill blade and the rotor of the wind mill.
11. A method according to claim 10 wherein, said solid bar is connected to the light weight core using glue such as containing epoxy and functionalized CNT.
12. A method according to any of the preceding claims, wherein the solid bar is covered during the production process with laminates, woven or non-woven mats of glass or carbon fibers, or cured or non- cured reinforcing materials ensuring adequate and long-lasting connection of the bar to the blade.
13. A method according to any of the preceding claims, wherein the rods which connect the windmill blade and the rotor are fastened in the rotor such that the blade can rotate in the axis or parallel to the axis given by the long axis of the blade, such that the blade can turn away from the wind at high wind speeds, whereby the rotation of the blade is reversible and controlled e.g. by elastic components such as springs .
14. A method according to any of the preceding claims, wherein the mould (10) has two halves (1) , preferably made of metal such as aluminium.
15. A windmill blade or similar composite article such as propeller, aeronautic, automotive or industrial part or the like made according to any of the preceding claims.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP09761853A EP2300219A1 (en) | 2008-06-10 | 2009-06-10 | A method to produce engineered composite articles comprising epoxy and carbon nano tubes |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FI20085570A FI20085570A0 (en) | 2008-06-10 | 2008-06-10 | A process for making technical composite products comprising epoxy resins and carbon nanotubes |
FI20085570 | 2008-06-10 |
Publications (1)
Publication Number | Publication Date |
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WO2009150298A1 true WO2009150298A1 (en) | 2009-12-17 |
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ID=39589334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/FI2009/050492 WO2009150298A1 (en) | 2008-06-10 | 2009-06-10 | A method to produce engineered composite articles comprising epoxy and carbon nano tubes |
Country Status (3)
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EP (1) | EP2300219A1 (en) |
FI (1) | FI20085570A0 (en) |
WO (1) | WO2009150298A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2493166A (en) * | 2011-07-26 | 2013-01-30 | Khalil Abu Al-Rubb | Sail-type turbine blade with buoyant structure, adjustable tip, flexible reinforcement, tip cap and uncovered non-working parts |
FR3066141A1 (en) * | 2017-05-12 | 2018-11-16 | Safran | PROCESS FOR MANUFACTURING COMPOSITE WORK WITH INTEGRATED EROSION RESISTANT COATING DURING MANUFACTURE |
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US3873654A (en) * | 1973-03-05 | 1975-03-25 | Robert G Smith | Process of forming a rigid foam airfoil section |
US4292101A (en) * | 1979-03-05 | 1981-09-29 | Reichert James B | Method of fabricating composite members |
EP0037987A2 (en) * | 1980-04-15 | 1981-10-21 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Method for the manufacture of foamed core-supported moulded articles such as wings, rotor blades, etc. of great dimension in length and width |
GB2105633A (en) * | 1981-08-28 | 1983-03-30 | Dowty Rotol Ltd | Foam-containing structures |
US4639284A (en) * | 1983-03-18 | 1987-01-27 | Societe Nationale Industrielle Aerospatiale | Process for manufacturing a variable pitch multi-blade propeller by molding resin-impregnated fails around a preform |
GB2237532A (en) * | 1989-11-02 | 1991-05-08 | United Technologies Corp | Moulding composite articles |
WO2005070647A1 (en) * | 2003-12-31 | 2005-08-04 | Collins & Aikman Products Co. | In mold lamination of decorative products |
WO2007127032A2 (en) * | 2006-04-25 | 2007-11-08 | Cytec Technology Corp. | One-part uv and abrasion resistant pigmented surfacing film composition for prepregs |
-
2008
- 2008-06-10 FI FI20085570A patent/FI20085570A0/en not_active Application Discontinuation
-
2009
- 2009-06-10 WO PCT/FI2009/050492 patent/WO2009150298A1/en active Application Filing
- 2009-06-10 EP EP09761853A patent/EP2300219A1/en not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3873654A (en) * | 1973-03-05 | 1975-03-25 | Robert G Smith | Process of forming a rigid foam airfoil section |
US4292101A (en) * | 1979-03-05 | 1981-09-29 | Reichert James B | Method of fabricating composite members |
EP0037987A2 (en) * | 1980-04-15 | 1981-10-21 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Method for the manufacture of foamed core-supported moulded articles such as wings, rotor blades, etc. of great dimension in length and width |
GB2105633A (en) * | 1981-08-28 | 1983-03-30 | Dowty Rotol Ltd | Foam-containing structures |
US4639284A (en) * | 1983-03-18 | 1987-01-27 | Societe Nationale Industrielle Aerospatiale | Process for manufacturing a variable pitch multi-blade propeller by molding resin-impregnated fails around a preform |
GB2237532A (en) * | 1989-11-02 | 1991-05-08 | United Technologies Corp | Moulding composite articles |
WO2005070647A1 (en) * | 2003-12-31 | 2005-08-04 | Collins & Aikman Products Co. | In mold lamination of decorative products |
WO2007127032A2 (en) * | 2006-04-25 | 2007-11-08 | Cytec Technology Corp. | One-part uv and abrasion resistant pigmented surfacing film composition for prepregs |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2493166A (en) * | 2011-07-26 | 2013-01-30 | Khalil Abu Al-Rubb | Sail-type turbine blade with buoyant structure, adjustable tip, flexible reinforcement, tip cap and uncovered non-working parts |
US10385825B2 (en) | 2011-07-26 | 2019-08-20 | Khalil Abu Al-Rubb | Turbine blade with adjustable tips |
FR3066141A1 (en) * | 2017-05-12 | 2018-11-16 | Safran | PROCESS FOR MANUFACTURING COMPOSITE WORK WITH INTEGRATED EROSION RESISTANT COATING DURING MANUFACTURE |
Also Published As
Publication number | Publication date |
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EP2300219A1 (en) | 2011-03-30 |
FI20085570A0 (en) | 2008-06-10 |
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