Patent Application
20240010828
This application claims priority to and the benefit of European Patent Application No. 22275092.9, filed Jul. 8, 2022, the entire content of which is incorporated herein by reference.
The present disclosure provides a polymer matrix composite comprising a (meth)acrylate polymer matrix, a halogenated organic flame retardant, an inorganic flame retardant synergist, and fibrous reinforcement; a method of preparing the polymer matrix composite; and a composition for use in the method.
Polymer matrix composites (PMCs) are a class of material formed of fibres dispersed in a polymer matrix. PMCs are used in a variety of sectors to produce various components. For example, PMCs are used to fabricate panel bodies, doors, drive shafts, leaf springs, bumpers and race vehicle bodies in the automotive sector, to fabricate primary and secondary structural components, such as main cabin seat backs, seat pans and seat back legs, for passenger airbuses, space shuttles, military aircraft, and satellite systems in the aerospace sector, to fabricate boat/marine body components using fibre glass PMCs, kayaks and canoes in the marine sector, to fabricate footwear, sports components and equipment in the sports equipment sector, to fabricate medical implants, devices for orthopaedics, body parts for MRI scanners, tables for X-rays, and prosthetics in the bio-medical sector, to fabricate electrical panels, printed circuit boards, switch-gear, electrical connectors and insulators in the electrical sector, to fabricate storage containers for chemicals, high pressure containers, valves and pump housing, and for the restoration of bridges and in equipment such as booms, blades for windmills, and cranes.
PMCs used in certain applications, e.g. the aerospace sector, may be required to be lightweight and ideally strong and low in cost. For this reason, it would be attractive to use (meth)acrylate PMCs, such as PMMA-based PMCs, in such applications. PMMA-based PMC seating products can be manufactured using traditional thermoset processes like resin infusion. However, for safety reasons, PMCs used in sectors such as the aerospace sector must also comply with relevant fire standards, such as Federal Aviation Regulations, Section 25.853, but PMMA-based PMCs are highly flammable.
The present disclosure provides a composition for forming a (meth)acrylate polymer and a method of forming a PMC therefrom which complies with the relevant fire standards, thereby enabling (meth)acrylate polymer-based PMCs to be used in the aerospace sector.
Viewed from a first aspect, the present disclosure provides a composition comprising monomers to form a (meth)acrylate polymer, a halogenated organic flame retardant, and an inorganic flame retardant synergist.
The aforementioned components of the composition, or the composition itself, may be used in a method for preparing a polymer matrix composite.
Thus, viewed from a further aspect, the present disclosure provides a method of preparing a polymer matrix composite, said method comprising:
Polymer matrix composites (PMCs) comprising a (meth)acrylate polymer matrix, a halogenated organic flame retardant, an inorganic flame retardant synergist, together with fibrous reinforcement are also disclosed, and may be prepared via the method described herein.
Thus, viewed from a further aspect, the present disclosure provides a polymer matrix composite comprising and/or formed from a (meth)acrylate polymer matrix, a halogenated organic flame retardant, an inorganic flame retardant synergist, and fibrous reinforcement. Articles comprising and formed from the PMC described herein form a further aspect of the disclosure.
It will be readily appreciated by the skilled person that the various optional and preferred features of certain aspects of the disclosure as described herein may be applicable to other aspects of the disclosure. For example, features disclosed in connection with each of the composition, article and PMC may be applicable to each other and to the method, and vice versa.
The present disclosure provides a composition comprising:
The terms “monomer” and “polymerizable compound” may be used interchangeably. Thus, a further aspect of the present disclosure provides a composition comprising:
The monomers to form a (meth)acrylate polymer and polymerizable (meth)acrylate compounds are materials which can be polymerized to form a (meth)acrylate polymer and combinations thereof, i.e. they may be, or comprise, acrylate monomers and combinations thereof. While the monomers and compounds will be described primarily as (meth)acrylates, this should be understood to include the equivalent (meth)acrylic acids.
The monomers are polymerizable (meth)acrylate compounds, and thus oligomers are also included, provided they are polymerizable to form a (meth)acrylate polymer.
The monomers and compounds may be di(meth)acrylates, tri(meth)acrylates or tetra(meth)acrylates.
The terms “monomers to form a (meth)acrylate polymer” and “polymerizable (meth)acrylate compounds” encompass polymerizable alkyl (meth)acrylate compounds, e.g. alkyl methacrylates, alkyl acrylates, or a combination thereof.
The monomers may be in the form of what may be termed a “resin” or “resin-formulation”, e.g. the monomers may be a resin or resin formulation comprising acrylate monomers such as methyl (meth)acrylate monomers or in the form of a (meth)acrylate monomer based resin or resin formulation. In some embodiments, the monomer or polymerizable compound may be an acrylate resin, or an acrylate system in a monomeric or oligomeric state with a viscosity suitable for resin infusion. Suitable viscosities for the monomer or polymerizable compound are 2 to 1000 mPa·s, e.g. 5 to 800 mPa·s, e.g. 10 to 500 mPa·s.
As used herein, the term “(meth)acrylate” can refer to methacrylate and/or acrylate. The alkyl group of alkyl (meth)acrylates may be C1-22, optionally C1-12, optionally C1-6, optionally C1-3, alkyl groups, e.g. methyl, ethyl or propyl. Suitable monomers include methyl (meth)acrylate, ethyl (meth)acrylate and propyl (meth)acrylate. Combinations of (meth)acrylate monomers may also be used.
In some embodiments, the monomers are or comprise methyl methacrylate (MMA). The (meth)acrylate polymer to be formed can be poly methylmethacrylate (PMMA).
In some embodiments, the (meth)acrylate polymer is a thermoplastic (meth)acrylate polymer, and thus the monomers are monomers for forming a thermoplastic (meth)acrylate polymer.
The term “PMMA” denotes a polymer comprising, or consisting of, methyl methacrylate (MMA) repeat units. Examples of the polymer include:
To form a copolymer, e.g. a PMMA copolymer, a mixture of monomers, i.e. a monomer mixture, is used. The mixture may include methyl methacrylate (MMA) in an amount from 70% to 99.7%, optionally from 80% to 99.7%, optionally from 90% to 99.5%, by weight, and from 0.3 to 30%, optionally from 0.3% to 20%, optionally from 0.3% to 10%, optionally from 0.5% to 10%, by weight of at least one monomer having at least one ethylenic unsaturation that can copolymerize with methyl methacrylate. Such monomers include styrene, alpha-methylstyrene, acrylic and methacrylic acids and alkyl(meth)acrylates in which the alkyl group has from 1 to 12 carbon atoms, such as methyl acrylate, ethyl acrylate or ethyl, butyl or 2-ethylhexyl (meth)acrylate. The comonomer may be an alkyl acrylate in which the alkyl group has from 1 to 4 carbon atoms.
The composition of the present disclosure may comprise more than one type of monomer.
For example, the monomer part of the composition (which may be a resin formulation) may comprise 50-100%, 60-95, 70-90, 70-80, of an acrylate monomer as described herein, e.g. methylmethacrylate, with any remainder being comonomers or other additives.
In some embodiments, the monomer or compound is any compound capable of polymerising with itself of other compounds to form a poly(meth)acrylate e.g. polymethylmethacrylate.
Monomer compositions such as Elium®, e.g. Elium® 150, Elium® 151 O, or Elium® 151 SA by Arkema may be used as the monomers of the present disclosure. Elium® is a registered trademark of Arkema S.A., located in Colombes, France.
The monomer part of the composition of the present disclosure may be a multi-component resin system, e.g. where two or more resin formulations (i.e. monomers/compounds as described herein) are mixed, e.g. in a 1:1 weight ratio prior to polymerisation. An example is Elium® 151 O/SA, which is a two-component resin system which is mixed in a 1:1 ratio by weight to form a methacrylate polymer.
In some embodiments, the glass transition temperature (Tg) of the (meth)acrylate polymer is above 80° C., for example when taking the onset of storage modulus from DMA as the Tg.
The monomers may be present in an amount of greater than or equal to 50 wt. % of the composition (i.e. at least 50 wt. % of the composition is monomers/resin formulation), greater than or equal to 60 wt. % of the composition, greater than or equal to 70 wt. % of the composition, greater than or equal to 80 wt. % of the composition, or greater than or equal to 90 wt. % of the composition, or greater than or equal to 95 wt. % of the composition. In some embodiments, the amount of monomers, in relation to the composition as a whole, is up to and including 60, 70, 80, 90, 95, or 99 wt. %. In some embodiments, the amount of monomers, in relation to the composition as a whole, is 60-85 or 65-80 wt. %.
The monomers may be present in an amount of greater than or equal to 50 wt. % of the total combined amount of monomers and halogenated organic flame retardant (i.e. at least 50 wt. % of the combined amount of the monomers and halogenated organic flame retardant is monomers/resin formulation), greater than or equal to 60 wt. % of the total combined amount of monomers and halogenated organic flame retardant, greater than or equal to 70 wt. % of the total combined amount of monomers and halogenated organic flame retardant, greater than or equal to 80 wt. % of the total combined amount of monomers and halogenated organic flame retardant, or greater than or equal to 90 wt. % of the total combined amount of monomers and halogenated organic flame retardant, or greater than or equal to 95 wt. % of the total combined amount of monomers and halogenated organic flame retardant. In some embodiments, the amount of monomers, in relation to the total combined amount of monomers and halogenated organic flame retardant, is 65-85 wt. %, e.g. 70-80 wt. %. In some embodiments, the amount of monomers, in relation to the total combined amount of monomers and halogenated organic flame retardant, is up to and including 99 wt. %.
The halogenated organic flame retardant may be non-polymerizable, for example, it may be or comprise a polymer, e.g. a halogenated polymeric organic flame retardant. In particular, the halogenated organic flame retardant may be or comprise a chlorinated or a brominated polymer, i.e. a chlorinated or a brominated polymeric organic flame retardant. The flame retardant is a compound capable of increasing the fire-resistance of the material to which it is added, in this case the (meth)acrylate polymer.
The halogenated, e.g. brominated, polymer may have a halogen, e.g. bromine, content of between 45 and 60 wt. %, optionally between 50 and 60 wt. %.
In some embodiments, the halogenated organic flame retardant is a halogenated, e.g. brominated, aromatic polymer. In some embodiments, suitable halogenated organic flame retardants include halogenated, e.g. brominated, epoxy polymers.
In some embodiments, the halogenated polymer comprises a bisphenol group, e.g. the halogenated polymer is a tetrabromobisphenol polymer or derivative.
Examples of suitable brominated organic flame retardants include the following and combinations thereof:
Further examples of suitable brominated flame retardants are F-2016, F-2100, F-2100H, F-2100L, F-2400, F-2400E, F-2400H, F-3020, F-3060, F-3100, FR-1025, and FR-803P, which are available from ICL.
In some embodiments, the flame retardant may be, or comprise, a brominated polymer with one or more of the following repeating units:
In some embodiments, the retardant may be one of the following:
As is well known in the field of polymers, “n” above is used to indicate a typical integer of repeat units of a polymer.
In some embodiments, the flame retardant is 2,2′-[(1-methylethylidene)bis[2,6-dibromo-4,1-phenylene)oxymethylene]]bisoxirane polymer with 2,2′,6,6′-tetrabromo-4,4′-iso-propylidenediphenol and 2,4,6-tribromophenol (CAS Number 135229-48-0), sold under the trade name Texfron 4002 @).
Alternatively, or additionally, suitable brominated polymers include poly brominated benzylacrylate, such as poly(pentabromobenzyl) acrylate, brominated polystyrene, polydibromostyrene, or any combinations thereof.
The inventors have found that halogenated polymeric flame retardants, e.g. brominated polymers such as Texfron 4002 @, do not affect the Tg (glass transition temperature) of the acrylate polymer, and thus of the final composite part, whereas undesirable changes to the Tg, e.g. lowering of the Tg, have been found for phosphorus-based flame retardants. In some embodiments, the flame retardant is substantially free from phosphorus.
The halogenated organic flame retardant may be present in the composition in an amount of up to and including 40 wt. %, or up to and including 35 wt. %, or up to and including 30 wt. %, or up to and including 25 wt. %, or up to and including 20 wt. %, or up to and including 15 wt. %, or up to and including 10 wt. %, or up to and including 5 wt. %, based on the total weight of the composition. In some embodiments, the amount of halogenated organic flame retardant in relation to the composition as a whole is at least 5 wt. %, at least 10 wt. % or at least 15 wt. %. In some embodiments, the amount of halogenated organic flame retardant in relation to the composition as a whole is 2 to 40 wt. %., e.g. 5 to 30 wt. %., e.g. 15 to 30 wt. %.
The halogenated organic flame retardant may be present in the total combined amount of monomers and halogenated organic flame retardant in an amount of up to and including 40 wt. %, or up to and including 35 wt. %, or up to and including 30 wt. %, or up to and including 25 wt. %, or up to and including 20 wt. %, or up to and including 15 wt. %, or up to and including 10 wt. %, or up to and including 5 wt. %, based on the total combined amount of monomers and halogenated organic flame retardant. In some embodiments, the amount of halogenated organic flame retardant in relation to the total combined amount of monomers and halogenated organic flame retardant is at least 5 wt. %, at least 10 wt. % or at least 15 wt. %. In some embodiments, the amount of halogenated organic flame retardant in relation to the total combined amount of monomers and halogenated organic flame retardant is 2 to 30 wt. %., e.g. 5 to 30 wt. %., e.g. 15 to 30 wt. %, e.g. 20 to 30 wt. %.
The ratio between the weight of monomer and the weight of halogenated organic flame retardant may be from 20:1 to 1:1, or from 15:1 to 1:1, or from 10:1 to 1;1, or from 9:1 to 1:1, or from 8:1 to 1:1, or from 7:1 to 1:1, or from 6:1 to 1:1, of from 5:1 to 1:1, or from 4:1 to 1:1, or from 3:1 to 1:1, or from 2:1 to 1:1, in particular from 6:1 to 2:1.
The inorganic flame retardant synergist may be selected from metal oxides, borates, silicates, stannates, organometallics, or combinations thereof. Suitable metal oxides include iron oxide, tin oxide, zinc oxide, aluminium trioxide, alumina, antimony trioxide, antimony pentoxide, bismuth oxide, molybdenum trioxide, tungsten trioxide, or any combination thereof. Suitable borates include zinc borate. Suitable silicates include antimony silicates. Suitable stannates include zinc stannate, zinc hydroxystannate, or combinations thereof. Suitable organometallics include ferrocene.
In some embodiments, the inorganic flame retardant synergist is antimony trioxide and/or antimony pentoxide. In some embodiments, the inorganic flame retardant synergist is antimony trioxide.
The inorganic flame retardant synergist may be present in the composition in an amount of up to and including 20 wt. %, or up to and including 15 wt. %, or up to and including 10 wt. %, or up to and including 5 wt. %, or up to and including 4 wt. %, or up to and including 3 wt. %, or up to and including 2 wt. %, or up to and including 1 wt. %, based on the total weight of the composition. In some embodiments, the amount of inorganic flame retardant synergist in relation to the composition as a whole is at least 0.5 wt. %. In some embodiments, the amount of inorganic flame retardant synergist in relation to the composition as a whole is 0.5 to 15 wt. %., e.g. 5 to 10 wt. %, e.g. 3 to 10 wt. %., e.g. 3-6 wt. %.
The ratio between the weight of halogenated organic flame retardant and the weight of inorganic flame retardant synergist may be from 20:1 to 1:1, or from 15:1 to 1:1, or from 10:1 to 1;1, or from 9:1 to 1:1, or from 8:1 to 1:1, or from 7:1 to 1:1, or from 6:1 to 1:1, of from 5:1 to 1:1, or from 4:1 to 1:1, or from 3:1 to 1:1, or from 2:1 to 1:1, in particular from 10:1 to 2:1, in particular 5:1.
The inorganic flame retardant synergist may be in the composition (and optionally also in the PMC disclosed herein) in the form of particles.
Without wishing to be bound by theory, it is thought that, when used in a composite material such as the PMC herein described, the inorganic flame retardant synergist and the halogenated organic flame retardant (e.g. brominated polymer) work in combination to reduce the flammability of the composite material. For example, when the inorganic flame retardant synergist is antimony trioxide and the flame retardant is a brominated polymer, the antimony trioxide accelerates the debromination of the flame retardant. HBr released from the brominated polymer in a fire reacts with the antimony trioxide to form SbBr3 and water. The resulting SbBr3 is volatile and imparts better flame compliance to the composite material by flame radical scavenging in the gas phase.
In a particular embodiment, the inorganic flame retardant synergist is antimony trioxide and the flame retardant is 2,2′-[(1-methylethylidene)bis[2,6-dibromo-4,1-phenylene)oxymethylene]]bisoxirane polymer with 2,2′,6,6′-tetrabromo-4,4′-iso-propylidenediphenol and 2,4,6-tribromophenol.
In an embodiment, the flame retardant is Texfron 4002@.
In addition to the monomer, flame retardant and synergist, the composition may comprise further components or additives, such as anti-dripping agents, heat stabilizers, weather stabilizers, lubricants, inorganic fillers, coupling agents, light stabilizers, antioxidants, dyes, pigments, anti-static agents, release agents, dispersants, inorganic fibres, parting agents, fluidizing agents, viscosity control agents, and any combination thereof. In some embodiments, the monomer, flame retardant and synergist form at least 80 wt. %, 90 wt. % or 95 wt. % and up to 99 wt. % or 100 wt. % of the composition.
The composition may comprise a radical initiator, also termed a catalyst. The catalyst may be a peroxide catalyst. The radical initiator may be chosen from diacyl peroxides, peroxy esters, dialkyl peroxides, peroxyacetals or azo compounds. Radical initiators which may be suitable are, for example, isopropyl carbonate, dibenzoyl peroxide, benzoyl peroxide, lauroyl peroxide, caproyl peroxide, dicumyl peroxide, tert-butyl perbenzoate, tert-butyl per(2-ethylhexanoate), cumyl hydroperoxide, 1,1-di(tert-butylperoxy)-3,3,5-trimethyl-cyclohexane, tert-butyl peroxyisobutyrate, tert-butyl peracetate, tert-butyl perpivalate, amyl perpivalate, tert-butyl peroctoate, azobisisobutyronitrile (AIBN), azobisiso-butyramide, 2,2′-azobis(2,4-dimethylvaleronitrile) or 4,4′-azobis(4-cyanopentanoic), or any combination thereof. In a particular embodiment, the radical initiator is dibenzoyl peroxide.
The catalyst may be present in an amount of up to and including 5 wt. % of the composition (i.e. up to and including 5 wt. % of the composition is catalyst), up to and including 4 wt. % of the composition, up to and including 3 wt. % of the composition, up to and including 2 wt. % of the composition, up to and including 2.5 wt. % of the composition, up to and including 1.5 wt. % of the composition, up to and including 1 wt. % of the composition, or up to and including 0.5 wt. % of the composition. In some embodiments, the amount of catalyst is from 1.5 to 3.0 wt. % or 2.0 to 2.5 wt. % of the composition.
The catalyst may be present in an amount of up to and including 5 wt. % of the total combined weight of monomers, up to and including 4 wt. % of the total combined weight of monomers, up to and including 3 wt. % of the total combined weight of monomers, up to and including 2 wt. % of the total combined weight of monomers, up to and including 2.5 wt. % of the total combined weight of monomers, up to and including 1.5 wt. % of the total combined weight of monomers, up to and including 1 wt. % of the total combined weight of monomers, or up to and including 0.5 wt. % of the total combined weight of monomers. In some embodiments, the amount of catalyst is from 2.5 to 3.0 wt. % of the total combined weight of monomers.
The content of radical initiator, with respect to the monomer content of the composition, may be from 0.05 to 5% by weight, optionally between 0.1 and 4% by weight, optionally between 0.5 and 3.5% by weight, optionally between 1 and 3% by weight, optionally between 2 and 3% by weight.
The composition may comprise a chain-limiting agent. This may serve to control the molecular weight of the eventual polymer. The chain-limiting agent may be γ-terpinene or terpinolene. The content of chain-limiting agent may be between 0 and 2500 ppm by weight, optionally between 0 and 1500 ppm by weight with respect to the monomer content of the composition.
In some embodiments, the above-mentioned composition may be combined with fibrous reinforcement, e.g. fibres, e.g. those described herein with respect to the method and composite, for example the one dimensional fibres, thus forming a mixture of the fibrous reinforcement and the composition as herein described. In such embodiments, the weight ratio of the fibrous reinforcement to the composition may be 60:40 to 80:20, for example 65:35 to 75:25. Further features of the fibrous reinforcement are discussed in connection with the method.
The composition is suitable for use in the production of polymer matrix composites in which the composition forms a polymer matrix for fibrous reinforcement.
The present disclosure therefore also provides a method of preparing a polymer matrix composite, said method comprising:
The composition which is contacted with the fibrous reinforcement in the method described herein may contain other components, e.g. catalysts/radical initiators, and/or chain-limiting agents, as discussed herein in relation to the composition.
The fibrous reinforcement may be present in an amount of at least 20% by weight, optionally at least 40% by weight, optionally at least 50% by weight, or optionally at least 55% by weight or optionally at least 60% by weight, or optionally at least 70% of fibrous reinforcement based on the total weight of the composition plus the fibrous reinforcement, i.e. the monomers, flame retardant, synergist, fibrous reinforcement, and any other components. The fibrous reinforcement may be present in an amount of up to 99% by weight, optionally at most 95% by weight, optionally at most 90% by weight, optionally at most 80% by weight, or optionally at most 70% by weight.
In an embodiment, the fibrous reinforcement may be present in an amount of 50-90 wt. %, e.g. 60-80 wt. %, e.g. 62-67 wt. % based on the total weight of the monomers, flame retardant, synergist, fibrous reinforcement, and any other components. In an embodiment, the fibrous reinforcement may be present in an amount of 70-75 wt. % based on the total weight of the monomers, flame retardant, synergist, fibrous reinforcement, and any other components. In an embodiment, the fibrous reinforcement is or comprises carbon fibres which are present in an amount of 60-70 wt. %, e.g. 62-67 wt. % based on the total weight of the monomers, flame retardant, synergist, fibrous reinforcement, and any other components. In an embodiment, the fibrous reinforcement is or comprises glass fibres which are present in an amount of 70-80 wt. %, e.g. 70-75 wt. % based on the total weight of the monomers, flame retardant, synergist, fibrous reinforcement, and any other components.
The fibrous reinforcement can have different forms and dimensions, i.e. those typical of fibrous reinforcement for PMCs. In an embodiment, the fibrous reinforcement may be fibres, e.g. discontinuous fibres. The fibrous reinforcement comprises, or is formed from, fibres and/or fibrous materials described herein and can be one dimensional, two dimensional or three dimensional. The fibrous reinforcement can be in the form of a preform, i.e. a structure comprising fibres shaped to form a particular component. In some embodiments, the preform is a fabric preform.
One dimensional fibres include linear long fibres. The fibres may be discontinuous or continuous. The fibres may be arranged randomly or as a continuous filament parallel to each other. A fibre is defined by its aspect ratio, which is the ratio between length and diameter of the fibre. The fibres may have an aspect ratio of at least 1000, optionally at least 1500, optionally at least 2000, optionally at least 3000 and optionally at least 5000.
Two dimensional fibrous reinforcement includes fibrous mats or non-woven reinforcements or woven roving or bundles of fibres, which can also be braided.
Three dimensional fibrous reinforcement includes stacked or folded fibrous mats or non-woven reinforcements or bundles of fibres or mixtures thereof, e.g. an assembly of the two dimensional form in the third dimension.
In some embodiments, the fibrous reinforcement is in the form of a preform, e.g. a two or three dimensional preform, e.g. a fabric preform. The preform may comprise different layers of fabric. The fibres in the fabric of the preform can be continuous, chopped, woven, braided, discontinuous, uniaxially arranged, or otherwise configured as known in the art. The fabric of the preform is formed from fibres as herein described, e.g. E glass, carbon fibres, or combinations thereof. The fibres can have diameters of 6 to 30 micrometres.
Synthetic fibres include polymeric fibres, for example made of polyamide (aliphatic or aromatic), polyester, polyvinylalcohol, polyolefins, polyurethanes, polyvinylchloride, polyethylene, unsaturated polyesters, epoxy resins, vinylesters, or any combination thereof.
Synthetic fibres also include glass fibres, for example of type E, R or S2, carbon fibres, boron fibres or silica fibres. The fibres may be E glass fibres. In an embodiment, the carbon fibre can be Zoltek PX35 NCF 500 gsm 0/900 127 cm Tricot Pillar Stitch. In an embodiment, the glass fibre can be biaxial 39-EX-600-1270 fabric (E glass, biaxial, 600 gsm, +/−45°).
Exemplary fibres include carbon fibres, graphene fibres, carbon nanotube fibres, metal fibres, ceramic fibres (e.g. SiC, Si3N4, SiOC, Al2O3), glass fibres, E-glass, S2 glass, aramid fibres, e.g., KEVLAR®, polyethylene fibres, e.g., ultra-high molecular weight polyethylene fibre (e.g. Dyneema® or SPECTRA®), coated carbon fibres (e.g., BN coated carbon fibres, BN/SiC coated carbon fibres), carbon fibres with a surface converted to SiC, coated SiC fibres, liquid crystal polymers (e.g. Vectran®, an aromatic polyester produced by polycondensation of 4-hydroxybenzoic acid and 6-hydroxynaphthalene-2-carboxylic acid), ultra-high molecular weight polypropylene fibre, poly(p-phenylene-2,6-benzobisoxazole) fiber (Zylon®), nylon or combinations thereof. In some embodiments, the fibres are carbon fibres, glass fibres, or ceramic fibres, or combinations thereof. In some embodiments, the fibres are carbon fibres or glass fibres, e.g. E glass fibres. Fibres can be continuous, chopped, woven, braided, discontinuous, uniaxially arranged, or otherwise configured as known in the art.
The polymerization step, i.e. polymerization of the monomers to form the polymer matrix, takes place subsequent to the contacting step. As the polymerization of the monomers takes place in the presence of the inorganic flame retardant synergist, halogenated organic flame retardant, and fibrous reinforcement, it may be termed “in-situ polymerization”. By the term “in-situ polymerization” as used herein is denoted that the final polymerization of the monomers to form the (meth)acrylate polymer takes place around, or in the presence of, the fibrous reinforcement in order to obtain directly the PMC. The polymerization step of the method disclosed herein therefore takes place after the composition and fibrous reinforcement have been combined.
The monomers, halogenated organic flame retardant, and inorganic flame retardant synergist and other components (e.g. catalysts/radical initiators, and/or chain-limiting agents) used in the method are as described herein, e.g. in relation to the composition. The matrix is the polymer matrix formed by polymerisation of the monomers and forms the matrix in the PMCs described herein. “Polymer matrix” encompasses “polymer-based matrix” as certain other components of the composition can also be present, for example the flame retardant and the synergist, for example, dispersed in the matrix.
The contacting step may be a wetting step. In the contacting, e.g. wetting, step, the one or more fibrous reinforcement and the monomers or composition are brought into contact. The contacting step may be effected by use of a vacuum. In some embodiments, the monomers or composition infiltrate the fibrous reinforcement. In some embodiments, a vacuum is used to assist the infiltration of the monomers or composition into the fibrous reinforcement. Polymerization of the monomers is then carried out.
The polymerization step may be carried out using known techniques for forming polymer matrix composites. The polymerization method for obtaining the (meth)acrylate polymer matrix may be radical polymerization, anionic polymerization or photopolymerization. The polymerization step may also be termed a curing step. The polymerization or curing may be performed by known methods, for example by means of a heated tool. The heated tool may be maintained at a temperature between 20 and 60° C., for example between 45 and 60° C. The tool may be formed of aluminium.
The contacting step involves contacting or wetting the fibrous reinforcement with the composition as herein described. In such embodiments, the method may further comprise a step of preparing the composition prior to contacting the fibrous reinforcement with it. For example, the inorganic flame retardant synergist and the halogenated organic flame retardant may be dissolved or dispersed into the monomers, e.g. monomers in liquid form, before the contacting step. Suitable methods for this step include shear mixing, and the liquid monomers may be heated.
Several methods may be used to prepare three dimensional PMCs. These methods include lamination, pultrusion, infusion, vacuum bag moulding, pressure bag moulding, autoclave moulding, resin transfer moulding (RTM), reinforced reaction injection moulding (R-RIM) and variants thereof, press moulding, filament winding, compression moulding or wet lay-up. All of these methods comprise the steps of contacting the fibrous reinforcement with the composition (or the monomers, flame retardant, synergist and any other components, separately or in combination) before the polymerization step. The additives may be dissolved or dispersed into the composition.
The composition may be mixed such that the non-monomer components are uniformly dispersed in the monomers, prior to contacting the composition with the fibrous reinforcement. In this way, the non-monomer components, i.e. the flame retardant, the synergist and any other components may be uniformly dispersed throughout the polymer matrix of the resulting composite.
Techniques such as resin infusion and resin transfer moulding are convenient and low-cost manufacturing methods which can be carried out at ambient temperatures. However, these methods require resins with suitable viscosities, e.g. less than 200 mPa·s, and are typically used for thermosets. The compositions described herein can be used as resins in resin infusion and resin transfer moulding techniques. The inventors have surprisingly found that using the compositions as described herein, which comprise monomers, facilitates use of these methods as the composition can have the desired viscosity characteristics for these methods, as well as improved flame resistance in the resulting composite.
In a particular embodiment, the method involves resin infusion. In the infusion method, the composition is aspired into the fibrous reinforcement present in a mould, e.g. by application of a slight vacuum. The fibrous reinforcement is infused and at least partially, e.g. completely, wetted by the composition. After a period of time since the introduction of the composition to the mould has elapsed, for example 0.5-2 hours, the resulting PMC can be demoulded.
In a particular embodiment, the method involves resin transfer moulding. Resin transfer moulding is a method using a two sided mould set which forms both surfaces of the PMC. The lower side is a rigid mould. The upper side can be a rigid or flexible mould. Flexible moulds can be made from composite materials, silicone or extruded polymer films such as nylon. The two sides fit together to produce a mould cavity. In resin transfer moulding, the fibrous reinforcement is placed into this cavity and the mould set is closed prior to the introduction of the composition comprising monomers to form a (meth)acrylate polymer matrix, an inorganic flame retardant synergist, and a halogenated organic flame retardant (and other components such as those mentioned herein with regard to the composition). In resin transfer moulding, the method by which the composition is introduced to the fibrous reinforcement in the mould cavity can include vacuum infusion. This process can be performed at either ambient (e.g. 10° C. to 60° C. or 20 to 50° C.) or elevated temperature, e.g. up to 200° C., optionally from 50° C. to 160° C., optionally from 50° C. to 100° C., optionally from 50° C. to 80° C. After a period of time since the introduction of the composition to the mould has elapsed, for example 0.5-2 hours, the resulting PMC can be demoulded.
In some embodiments, the steps of contacting and polymerizing (or curing) take place in a mould. The PMC thus formed can be removed from the mould, i.e. demoulded, after 0.5-2 hours, i.e. 0.5-2 hours after the introduction of the composition to the mould.
In some embodiments, the method of preparing the polymer matrix composite is resin transfer moulding or resin infusion.
Manufacturing PMMA-based PMCs using infusion or resin transfer moulding can provide a cost reduction of 70% compared to existing materials, improved recyclability compared to existing materials, which leads to an increased sustainability within the product life cycle.
In an embodiment, the contacting, e.g. wetting, step of the fibrous reinforcement is made in a closed mould, by resin transfer moulding or by infusion.
Optionally, the contacting, e.g. wetting, step of the fibrous reinforcement and the preparation of the composite material take place in the same mould, which is a closed mould. Using the same closed mould avoids the transfer of the material after contacting, e.g. wetting, and polymerizing in a closed mould ensures a good distribution of heat, which helps to provide a satisfactory yield of polymerization.
The mould may be opaque towards visible and ultraviolet radiation at least on one side.
A closed mould will avoid and reduce the evaporation of the monomer and protect the environment.
In some embodiments, the monomers and/or the composition are liquid at 25° C.
The PMC component formed by the above method can be post-processed by thermoforming or melt blending of the PMC component to achieve a new shape after the initial processing. The PMC can also be adhered to another material, for example, a polymeric, metallic, ceramic, or composite material. Adhesives may be applied to join the PMC to the further material. Alternatively, welding may be used to join the PMC to the further material.
Suitable steps for forming the composites of the invention by a vacuum assisted resin infusion process are outlined below. These are for the purposes of example only and are non-limiting:
Example Procedure for Vacuum Assisted Resin Infusion Process for Making PMC Plaques or
Parts:
Preparation of Composition
Preparation of Composite Part
A PMC produced by a method as herein described forms a further aspect of the present disclosure.
The present disclosure therefore also provides a polymer matrix composite (PMC) or PMC component, for example as manufactured by the method disclosed herein, comprising a (meth)acrylate polymer matrix, a halogenated organic flame retardant, an inorganic flame retardant synergist, and fibrous reinforcement.
The (meth)acrylate polymer matrix, halogenated organic flame retardant, inorganic flame retardant synergist, and fibrous reinforcement are as described herein with relation to the composition and the method.
The fibrous reinforcement may be present in the PMC or PMC component in an amount of 50-90 wt. %, e.g. 60-80 wt. %, e.g. 62-67 wt. % based on the total weight of the PMC. In an embodiment, the fibrous reinforcement may be present of an amount of 70-75 wt. % based on the total weight of the PMC.
In an embodiment, the fibrous reinforcement is, or is formed from, carbon fibres which are present in an amount of 60-70 wt. %, e.g. 62-67 wt. % based on the total weight of the PMC. In an embodiment, the fibrous reinforcement is, or is formed from, glass fibres which are present in an amount of 70-80 wt. %, e.g. 70-75 wt. % based on the total weight of the PMC.
In some embodiments, the (meth)acrylate polymer matrix, i.e. that formed by the polymerization, is formed of PMMA.
The PMC may be formed into components which have a laminate structure. These components may be formed by bonding together by lamination several layers or sheets of the PMC. The thickness of the laminate component can be 0.5-3 mm, optionally 1-2 mm.
Typically, thinner laminates (i.e. less than 2 mm in thickness) are more susceptible to failing flame tests. However, laminates of 1-2 mm in thickness which are formed from the PMC of the present disclosure, which contain both an inorganic flame retardant synergist and a halogenated organic flame retardant as described herein, have improved fire resistance characteristics and reduced weight, and are thus particularly suitable for use in aerospace applications, e.g. cabin products such as seats.
The PMC of the present disclosure may be used to manufacture an article, for example, a seat component such as a seat back, seat pan, seat back legs, seat back frame, or tray tables. The article, or a part thereof may be formed directly by the method, e.g. when a mould is used, or the composite of the present disclosure may subsequently be used in the manufacture of an article or part thereof. Articles comprising, or formed from, the PMC described herein form a further aspect of the disclosure. Such articles include those mentioned herein, for example, aerospace components, particularly interior cabin articles such as seating parts, e.g. seat backs, seat pans or seat back legs.
In some embodiments, e.g. for aircraft interior applications, the glass transition temperature (Tg) of the polymer matrix composite is at least 28° C. above the maximum operating temperature (MOT) or maximum storage temperature (whichever is greater) of the article. In some embodiments, the glass transition temperature is above 80° C., for example when taking the onset of storage modulus from DMA as the Tg.
A series of carbon laminate PMCs panels were prepared by resin infusion. The carbon laminate PMC panels were formed from a carbon fabric preform with several plies which are adhered together by a PMMA polymer matrix. Elium® 150 (Arkema) was used as the monomers. The brominated polymer Texfron 4002@ was added in Tests 2-13 as a flame retardant, and an inorganic flame retardant synergist (ATO, i.e. antimony trioxide) was added in Tests 6-13.
Three 12×3 inch coupons were extracted from the PMC panels. These coupons were conditioned for 24 hours prior to testing. The thickness of the carbon laminates is shown in Table 1.
The carbon laminate PMCs were subjected to a flammability test (vertical burn 12 s, VB12 s) according to Federal Aviation Regulations, Section 25.853. Burn length is measured in inches and flame time is measured in seconds. To pass the test, burn length must be below 8 inches and flame time must be below 15 s.
The results show that the Elium®-based composite parts burn continuously after removing the flame; in other words, when Elium® alone is used, the composite parts do not pass the flame test. Adding Texfron 40020 to the Elium® 150 formulation achieves desired compliance for laminates with a thicker cross-section.
The addition of an inorganic flame retardant synergist, in this case ATO, enables laminates with a thinner cross-section to also achieve a pass in the flame test. The results show improvements in terms of “Burn Length” for thinner cross-section laminates with ATO, even with reduced amount of Texfron 4002@.
References to “comprises” and/or “comprising,” should be understood to also encompass “consist(s) of”, “consisting of”, “consist(s) essentially of” and “consisting essentially of”.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
It will be readily appreciated by the skilled person that the various optional and preferred features of the disclosure as described above may be applicable to all the various aspects of the disclosure discussed.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
| Number | Date | Country | Kind |
|---|---|---|---|
| 22275092 | Jul 2022 | EP | regional |
