CA2237359A1 - Thermosetting polymers for composite and adhesive applications - Google Patents

Thermosetting polymers for composite and adhesive applications Download PDF

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Publication number
CA2237359A1
CA2237359A1 CA002237359A CA2237359A CA2237359A1 CA 2237359 A1 CA2237359 A1 CA 2237359A1 CA 002237359 A CA002237359 A CA 002237359A CA 2237359 A CA2237359 A CA 2237359A CA 2237359 A1 CA2237359 A1 CA 2237359A1
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reactant
bismaleimides
bismaleimide
composition
resin
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CA002237359A
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French (fr)
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Jack Boyd
Albert Kuo
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Cytec Technology Corp
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/12Unsaturated polyimide precursors
    • C08G73/125Unsaturated polyimide precursors the unsaturated precursors containing atoms other than carbon, hydrogen, oxygen or nitrogen in the main chain
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/12Unsaturated polyimide precursors
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/12Unsaturated polyimide precursors
    • C08G73/123Unsaturated polyimide precursors the unsaturated precursors comprising halogen-containing substituents
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/12Unsaturated polyimide precursors
    • C08G73/124Unsaturated polyimide precursors the unsaturated precursors containing oxygen in the form of ether bonds in the main chain
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/243Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2379/00Characterised by the use of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing nitrogen with or without oxygen, or carbon only, not provided for in groups C08J2361/00 - C08J2377/00
    • C08J2379/04Polycondensates having nitrogen-containing heterocyclic rings in the main chain; Polyhydrazides; Polyamide acids or similar polyimide precursors
    • C08J2379/08Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors

Abstract

Thermosetting polymers with high temperature capability and superior oxidative stability for composite and adhesive applications are disclosed. These polymers are ideally suited for adhesives and RTM, resin film infusion, and prepreg methods to make polymer matrix, fiber reinforced composite parts.

Description

CA 022373~9 1998-0~-11 THERMOSETTING POLYMERS FOR COMPOSITE AND ADHESIVE APPLICATIONS
Techni~l Field This invention relates to heat curable bismaleimide resin systems and the preparation thereof. More particularly, the subject invention relates to the preparation of bismaleimide resins in which the bisl"~'~ c reactants are slurry mixed at relatively low temperature into the remaining resin system component.
The subject invention further relates to specific, solid diamine bismalci."iie resin reactant reacted with a liquid propenyl ben~opl1enone co-reactant to produce a thermosetting polymer. The resulting polymer has an unusually low weight loss during thermal treatment at high temperature.
k~round of the Invention Bismalei,nk3e resins are important resins in commerce for various uses, including fiber reinforced composite and structural adhesives. However, bismaleimide resins, while possessing high strength at elevated temperatures, tend to be somewhat brittle.
Accordingly, it is common to modify the bismalei., '~s with additional comonomers to improve impact ,~si;jl~nce.
Curable mixtures based on aromatic bismalci."ides and propenyl compounds are known, for example, from H.~. Stenzenberger et al. ("Slel,zenberger"), relating to various curable resins from bismaleimide and alkenyl phenyl hydroxy ether, and laminated articles produced from said resin as ~licclosed in U.S. Patent Nos. 4,871,821, 4,917,954, 4,789,704, 4,939,305 and 5,120,824. The cor, '..~alion of a bislllalci.l,ir!e and a propenyl compound by slurry mixing is not ~licclosed in any of the Stenzenberger patents.
Certain curable mixtures containing a bismaleimide and a propenyl compound are disclosed in A. Kramer, U.S. Patent No. 5,013,804 ("Kramer"). Although various aromatic bismalei.-,-des are contemplated, no ~lisclosllre~ either as teaching or suggestion using methylenedian!' ~e bismaleimide, is provided. Ad-lilionally, Kramer discloses a fusion process for bringing together a bismaleimide compound and a propenyl compound. Kramer does not teach or suggest the thermosetting polymer made, and the making thereof, using slurry mixing.
The process of slurry mixing bismaleimide resins is ~isclosed in L. Repecka, U.S.
Patent No. 5,003,018 ("Repecka"~. Certain aromatic bismaleimides in combination with liquid co-reactants, like o,o'-diallylbisphenol A, are disclosed. However, there is no CA 022373~9 1998-0~-11 disclosure for using a benzophenone as the liquid co-reactant. All of the above mentioned patents are incorporated herein by reference.
Many comonomers are physically incompatible with the bismaleimide resins because following initial formulation at elevated temperatures, the bismaleimide5 component may crystallize during processing. The large crystals which then form result in a resin system which is heterogeneous, difficult to pl~ cess and which may be prone to microcracking when used to prepare carbon fiber reinforced composites. In such a resin system, the bismale;...:la components are physically compatible, adhesives and prepregs prepared therefrom by the conventionally prepared systems often do not have 10 the drape and tack desired of them.
As a result, there is a need in this technical area for a bismaleimide resin that has a high temperature capability, superior oxidative stability, and acceplt,ble tack and drape to make composite parts.
Summary of the Invention It has been surprisingly discovered that bismaleimide polymer systems made using specific bismaleimide components, specific co-reactant components as curing agents in an opli",i~ed formula and a slurry mixing technology, provides systems having unexpectedly improved thermal and oxidative stability when formed into composites adhesives, etc. Specifically, the novel formulation of the present invention comprises a thermosettable curable resin composition pr~par~d by slurry mixing a compositioncomprising a solid diamine bismaleimide resin reactant and a liquid propenyl benzophenone co-reactant in which the reactant and co-reactant are present in a weight ratio of substantially about 1:1. This particular composition has a decreased weight loss upon thermal aging and the tack and drape necessary to make composite parts.
This invention also relates to a process for preparing a thermosettable curable resin composition by slurry mixing a powdered bisl"alei.l,ide resin reactant into a liquid co-reactant which has been heated to between 50~C and 150~C.
Description of the Preferred Frnbodiments The process of the subject invention involves the slurry mixing of one or more solid bismaleimide monomers with the other resin system components. After cooling the bism-~lei."ide resin systems thus obtained, very fine bismalei.~,ide particles in the form of a stable dispersion are present. Upon standing, substantial crystallization of additional bismaleimide will not occur. The resulting heat-curable resin system is thus uniform and homogeneous.

CA 022373~9 1998-0~-11 In this ap,t~licalion, the solid bismaleimide monomers may alternatively be described to include as a "specific bismaleimide component," "a solid reactant" and "solid aromatic diamine bismaleimide resin reactant."
The liquid co-reactant may be described to include a "curing agent", a "propenyl5 compound", a "liquid homogeneous benzophenone co-reactant" and an "incompatlble comonomer~s)."
The term "resin col,lposilion" as used herein refers to a heat-curable resin composition in its final form. The composition may contain one or more reactive monomers and/or comol1omers, curing agents, any necessary catalysts, and optionally 10 filler, rheology control agents, tackifiers, tougheners, diluents, dyes, and pigments, but exclusive of fiber reinforcement.
The term "incor ,paliLle comonomer(s)" as used herein refers to comonomers and other ingredients which, when present, would allow cryst~ tion of a particular bismaleimide component upon cooling a melt of such components. The incompatible 15 comonomer may thus com,~ e one or more additional components having chemical functionalities other than maleimide, as well as other bismiJ~ llide comonomers.For example, it might be found that homogeneous melt of specific quantities of aparticular bisrr~ci."ide monomer and a comonmple, might not present a problem with regard to crystallization of the bismalei.~,de on cooling. However, when a second 20 bismalei", c~e, or when more of the first bismaleimide are added to the melt, substantial crystallization might occur under the same condilions. The resulting cryst~ tionin-~;czltes incompatibility, in the sense used by the inventor, between the added bismaleimide and the other ingredients. Such incompatibility is most likely to result when high concenll~lions of bismaleil- :les are utilized, particularly when high25 concentrations of a single or limited number of bismaleimides are utilized.
The use of slurry mixing in the preparation of bisl,-alei.-,icle resin systems containing incompatible components is but one mode of practicing the subject invention.
This mode is important when large quantities of crystalline bismaleimides are contained in the resin formulation, as such formulations, when prepared by fully dissolving, are 30 frequently very difficult to process. The slurry mixing process has been found to be useful whether or not the overall resin system components are compatible. Such resin system may result when a compatible rather than an incompatible comonomer is utilized. An example of the latter might be the use of a bismaleimide monomer and a cyanate-functional comonomer.

CA 022373~9 1998-0~-11 WO 97/18254 E'CT/US96/1749g Slurry mixing is merely an aid in preparing the resin of the invention. It should be noted that slurry mixing is n~ required for good resistance to oxicl~tion. Good resistance to oxidalion is a function of the monomers, not the process for preparation.
However, for prepreg and adhesive applications, the invention will most likely be 5 practical using slurry mixing. In other ap,. l - -' ons, for example, resin transfer molding (RTM), slurry mixing may not be needed.
The resin system, upon cooling, will generally not show the presence of large orsubstantial amounts of crystals. In some cases, the resin system may have the appearance of a solid solution or glass. Yet despite the uniform appearance, these 10 uncured resin systems frequently possess virtually no tack, and often are highly brittle.
Surprisingly, when the same components are slurry mixed, the resulting resin system has excellent tack and drape.
The terrn "a weight ratio of substantially about 1:1" as used herein relates to the weight ratio of the solid reactant and the liquld co-reactant, but not diluents or other 15 polymer components. The solid reactant is generally present in a weight ratio of about 1:1 with the liquid co-reactant. The term "substantially about" as used herein indicates that the ratio may vary to a limited extent and would still be considered a part of the present invention. The weight ratio may vary from about 1:1.5 solid rea~ uid co-reactant to about 1.5:1 solid reactant:liquid co-reactant. rl~r~r~bly, however, the weight 20 ratio is about 1:1 solid reactant:liquid co-reactant.
The term "decreased weight loss" as used herein relates to a comparison of the weight loss of cured composites after the composites have been heat treated. Thermal aging is used to determine the effect of the resin and the composite materials after dormant treatment with heat over a period of time in air. It is expected that a certain 25 component of the resin and composite will be oxidized during the aging process.
Correlation can be made in the stability of a particular composite structure by comparing the weight loss from the composite structure after thermal aging. Generally, thermal aging takes place over a period of time at a particular temperature. For purposes of this invention, the time for such aging may range from one day to several years. For test 30 purposes, the time of thermal aging used was from three weeks to nine weeks. For purposes of this invention, the temperature in which the thermal aging was evaluated ranges from about 200~C to 300~C, with a preferred temperature ranging from 220~C to 280~C. These times and temperatures are used for an accelerated evaluation of composite.

CA 022373~9 l998-0~-ll The claimed heat-curable resin systems of the subject invention contain (excluding inorganic fillers, fibers and non-bismaleimide and co-reactant resin materials) from between about 20 to 80 percent by weight of one or more solid bismalei.~ 'ereactants. Preferably, the solid bismaleimide co-reactants are present from between 5 about 40 to 60 percent by weight of the total resin composition. The claimed heat-curable system also con~a;"s from between about 20 to 80 percent by weight of one or more co-reactants (excluding inorganic fillers, fibers and non-bismaleimide and co-reactant resin materials). Preferably, the liquid co-reactants are present from between about 40 to 60 percent by weight of the total resin composition. P~efer~i,ly, the 10 bismaleimide reactant and the liquid co-reactant have a high amount of aromatic groups.
Bismaleimide of certain structures have unexpectedly been found to have significantly improved oxidative stability.
Most preferably, the solid reactant and the liquid co-reactant is greater than about 70 percent and close to 100 percent total weight of the composition upon curing.
15 The comonomer may include the liquid co-reactant. However, in this invention, the comonomer, other than the liquid co-reactant, is about 20 percent total weight or less of the composition upon curing. As a most preferred example of this invention, MDA-BMI
(as a solid reactant) is combined with PPB (as a liquid co-reactant) in a 1:1 weight ratio, the combined weight of which is close to 100 percent total weight of the composition 20 upon curing. Also, the solid bismaleimide is preferred to have a mean size of less than 100 ,um, preferably less than 20 ~um, relative to the liquid coreactant and comonomer at a temperature such that a substantial portion of the solid bismaleimide does not dissolve in the liquid portion.
A number of suitable bismaleimide monomers exists. The common feature for 25 this monomer is that it must be highly aromatic and preferably have more than one aromatic group. Groups connecting to the aromatic ring can be methylene, isGpropylidene, oxygen, sulfone or sulfide. Such bismalei.n ~'es when used in the invention have been found to have markedly improved oxidative stability as a result of thermal aging in air. Pendant aliphatic groups are detrimental, for example, methyl, 30 ethyl, n-propyl, i-propyl and the like. However, the presence of methylene groups in the solid reactant tends to increase stabiiity of the aromatic nucleus against oxidation. For the purpose of this invention, methylene dianiline bismaleimide (MDA-BMI) is preferred.
Other preferred solid bismaleimide reactants of this invention include bis(aminophenoxyphenyl)propane bismaleimide (BAPP-BMI), oxydianiline bismaleimides 35 (ODA-BMI), bis(aminophenoxy)benzene bismaleimides (APB-BMI), CA 022373~9 lsss-o~-ll Wo 97/18254 PCT/US96/l 7499 diaminodiphenylsulfone bismaleimides (DADS-BMI), diaminodiphenylisopropylidines,diaminodiphenylketones, diaminodiphenyl sulfides, diaminodiphenyl hexafluoroisopropylidines, bis(diaminodiphenylisopropylidine)benzenes, toluene dianiline (TDA), p-phenylenediamine, m-phenylenediamine, and the like. Certain commercially 5 available eutectic mixtures of BMI monomers conl~ i"g methylene dianiline-bismaleimide (MDA-BMI), toluene dianiline bismalei.";cle (TDA-BMI) and trimethylenehexamethylenediamine-bismaleimide, and the like are not as stable to the thermal aging process.
Wholly aliphatic bismaleimides, for example, hexamethylenediamine-10 bismaleimides can be used in small amounts to increase tack as long as the thermalaging properties are still acceptable.
The bismaleimide monomers are well known to those skilled in the art, and are generally prepared by the reaction of maleic anhydride, or sl~hstihlt~d maleic anhydride, with a suitable diamine. Both aromatic and aliphatic diamines ara suitable for the 15 preparation of the bismaleimide. Suitable diamines for the preparation of bismaleimides also include other aromatic diamines such phenylenediamine, diaminodiphenylsulfones, diaminodiphenylisopropylidenes, diaminodiphenylketones, diaminodiphenyloxides and diaminodiphenylsulfides.
Bismaleimides derived from diamines containing heteroatoms are also useful, for 20 example those derived from amino terminated polyethersulfones, polyetherketones, polyetherketoneketones, polyetheretherketones and similar oligomers as prepared in accordance with U.S. Patent No. 4,175,175, as well as amino terminated polyoxyalkylene polyethers, amino terminated N,N-dialkylpiperidines, and the like.
Also useful are polyaminobismaleimide prepolymers which may be prepared 25 through the reaction of a stoichiometric excess of one or more bismaleimides with a di-or polyamine. Such polyaminobismaleimides or related products may also be prepared in situ by including in the resin system, one of the aforementioned diamines, preferably one of the diaminodiphenylsulfones.
Preferred comonomers are the alkenylphenols and alkenyloxyphenyls. Suitable 30 are, for example, o,o'-diallyl- and o,o'-dipropenylbisphenols such as o,o'-diallyl- and o,o'-dipropenylbisphenol A, bisphenol F and/or bisphenol S. Also suitable are the alkenylphenol- and alkenyloxyphenyl terminated dicyclopentadienes. The latter are prepared by first forming the phenolated dicyclopentadiene precursor as taught in lJ.S.
Pat. No. 3,536,734. The precursor is then reacted with the requisite alkenylhalide such 35 as allyl chloride or propenyl chloride in the presence of base to form the allyl or propenyl CA 022373~9 1998-0~-11 ether. These ethers may be used as such or may be isomerized through Claisen rearrangement to the ortho 5l~hstit~ted phenol. Various other comonomers are described in U.S. Pat. No. 5,003,018, which are incorporated herein by reference.
The resin system of the subject inventions may contain one or more 5 comonomers. These comonomers may be comonomers which react with the bismaleimide monomers, or which react with themselves or with other comonomers or may be the same or a different bismalei.lli ~e resin in liquid form. Such comonomers include, for example, those ~~iccussed in U.S. Pat. Nos. 4,100,140 and 4,035,345, which are incorporated herein by reference. Allylnadicimide resins, epoxy resins, di- and 10 polyamines, cyanate resins, unsaturated polyester resins, and alkenylphenol-terminated oligomeric tougheners similar to those disclosed in European published ~ppli-- ~ion 230,741 are useful. Silicone rubbers may also be utilized as comonomers, particularly those ler,l,;llated with maleimide, epoxy, vinyl and amino groups. In addition to such comonomers, the resin systems of the subject invention may also inciude engineering 15 thermopl~tic tougheners, particularly polyimides, polyetherimides, polyetherketones, polyarylenesulfides, polyarylenesulfones, polyethersulfones, and the like. Such thermopl~tic tougheners should have glass transition temperatures, Tg, in excess of about 100~C.
Suitable epoxy comonomer resins are disclosed in the treatise Handbook of 20 Epoxy Resins, I\/lcGraw-Hill, Inc., 1967. Examples of such resins are the bisglycidyl ethers of the bisphenols, particularly bisphenol A, bisphenol F and bisphenol S. Also sllit~l-lE are the various phenolic and crescli~ novolac-type resins, as well as the various glycidoxy amines and aminophenols, particularly N,N,N',N'-tetrakis~glycidyl)-4,4'-diaminodiphenylmethane and N,N,O-tris~glycidyl)4-aminophenol. Epoxy resin based on 25 the glycidyl ethers of the various dihydroxynaphthalenes and phenolated dicyclopentadienes are also sllit:~lE.
Cyanate functional comonomers are also useful. Such monomers are prepared by the reaction of cyanogen chloride or bromide with a diol or polyol. Examples of suitable diols include the bisphenols, the tetramethylbisphenols, other cyanates30 commercially available and in the literature, resorcinol, the hydroxyalkcyanurates and isocyanurates and the like. Such cyanate systems are well known to those skilled in the art, and are commercially available from a number of sources. Their preparation is also well known, and may be accomplished by the methods proposed in U.S. Pat. No.
4,546,131. Cyanate resins might need a catalyst.

CA 022373~9 1998-0~-11 The resin systems of this invention may also include other components, some of which may also affect the compatibility of the bismaleimide monomers. Catalysts are generally present, for example, in amounts of from Q.01 percent to about 5.0 percent by weight. P,~fer,.acJ catalysts include triphenylphosphine, the various tertiary amines, 5 i,., '-7oles, or diamines. The comonomers may require a catalyst for their polymerization. The system may also contain various dyes, pigments, fillers and rheology control agents. These additional components are well known to those skilled in the art.
A radical inhibitor has been found useful to stabilize the resin and prepreg. One 10 inhibitor, hydroquinone, is particularly advantageous. The prepreg keeps tack longer with 0.05% hydroquinone, and therefore hydroquinone is used in most commercial applications. Hydroquinone at 0.05% also increases 150~C gel time by 50% or moreafter room temperature storage in MDA/propenyl phenoxy benzene compositions, which is useful in most applications, especially resin transfer molding applicalions.
The resin systems of the subject invention are preferably prepared by dispersingthe bismaleimide into the compatible liquid co-reactant in such a manner that a uniform dispersion is obtained. The process of forming such dispersions is termed "slurry mixing" and may be accomplished through several means. Some of these means are described below, while other equivalent means will readily suggest themselves to those 20 skilled in the art of resin formulating.
In order to form a stable dispersions of this invention, the average particle size (by volume) of the solid bismalei." -'8 component must be kept below 100 ,um, preferably, below 50 ,um. The bismaleimide particle size may be obtained throughtraditional methods of size reduction, for example, by precipitation from solution, airjet 25 milling, three-roll milling or high-shear mixing. Preferably, the desired particle size is achieved through jet milling.
The liquid phase of the resin system may be defined as that portion of the resinsystem exclusive of the solid bismaleimide particles or other components. The liquid phase may also, in certain cases, contain compatible comonomers and liquid or 30 dissolved bismalei.,li~es. The liquid phase should have a low glass transition temperature, the value of which is dependent upon the particular ap,~ on.
By the term "liquid comonomer" is meant those components of the total resin system which, during the slurry mixing process, constitute the continuous phase. These components may be liquids, preferably viscous liquids, at room temperature. Examples 35 of such liquid comonomers suitable for formulation in this invention includes eutectic CA 022373~9 1998-0~-11 blends of bismaleimides, other resin systems such as resorcinol diglycidylether (RDGE), cis-stilbene (C-STIL), trans-stilbene (T-STIL), diallylbisphenol A (DABA), various epoxy and cyanate resins.
The liquid co-reactant can be monofunctional or bi-functional. Generally, it is 5 preferred to have a high ratio of aromatic moieties to other groups. Examples of preferable bi-functional liquid co-reactants include but not limited to 4,4'-bis[0-(1-propenyl)-phenoxy]benzophenone (UPPB") and 2,6-bis[0-(1-propenyl)phenoxy]pyridine ~"PPP"). Monofunctional co-reactants having only one alkenyl group are also a part of the preferred e,nbodi"lent. Such substances in general, have lower molecular weight 10 compared to substances with two alkenyl groups, and hence, lower viscosity which will impart prepreg tack. The monofunctional co-reactants can also have a high ratio of aromatic to aliphatic groups, thus do not reduce oxidative stability. It is generally preferable to have primarily a bi-functional curing agent because monofL"~clional curing agents tend to reduce the bonding in the molecular network and can reduce Tg. An15 example of a monofunctional modifier is (3-allyl-2-hydroxylphenyl) benzene.
The liquid phase preferably has a Tg of about room temperature or less. These low Tgs are desirable in order that the product, when in adhesive film or prepreg form, may have adequate tack and drape. If the viscosity or Tg of the liquid phase is too low, it may be raised to higher values by dissolving a portion of the bismalei"l;de into the 20 other components in the traditional manner. Care must be taken to avoid dissolving so much bismaleimide at higher temperatures that the iow temperature solubility is appreciably exceeded, as under these conditions bismaleimide may crystallize out. This cryst~ tion is promoted by the presence of dispersed, solid bismaleimide in the finished resin system which may serve as nucleation sites for cryst~" 'icn. If only 25 minor amounts of cryst~lli7~tit~n take place, the nonhomogeneity thus produced may be attenuated by further processing, such as three-roll milling. However, if substantial amounts of crystallization takes place, the product must be reworked or scrapped.
In the most preferred embodiment of this invention, slurry mixing of the resin system is accon,plished by dispersing the required quantity of bismaleimide in fine 30 particle form, preferably as less than 50 ,um particles, into the liquid phase. The slurry mixing generally takes place at a modestly elevated temperature, preferably from 30~C
to about 150~C, but below the temperature at which the particular bismalei.~ 'e is soluble or miscible with the remaining components. At these relatively low temperatures, only a minor portion of the bismalci."-~e, if any, will dissolve into the 35 continuous phase despite the small particle size of the bismaleimide.

CA 022373~9 1998-0~-11 Conventional high shear mixing equipment may be utilized. The cure catalyst may also be added at this stage. The uniform dispersion thus obtained may be proceeded on a three-roll mill, or may be directly coated onto silicone release paper for use as an adhesive or as a hot melt prepregging resin. Matrix resins prepared by this technique are particularly suit~ls for carbon/graphite and glass fiber applications.
For the purpose of this invention, where highest oxidative stability is not necessary, mixtures of less oxidatively stable co-reactants with bismaleimides is also a preferable part of this invention. For example, mixtures of (4,4'-bis~0-(1-propenyl)phenoxy]benzophenone) (PPB) and (2,6-bis[0-(1-propenyl)phenoxy]benzophenone) (PPP), or PPP and diallylbisphenol A (DABA) may be particularly suitable in some Applic~lions.
A preferred embodiment is that a substantial portion of the solid bismaleimide remain in solid form. The term "substantial portion" is best defined in terms of the amount of solid bisrr '~ ;e which does dissolve during the slurring mixing process when practiced by adding fine particle size bismaleimide to the liquid coingredients.
This portion must be such that following the slurry mixing process, the resin film or prepreg prepared from the heat-curable resin system has the desired tack and drape, and that substantial crys~i~ tion of the solid bismaleimide component(s) does not occur.
For example, in many systems, the portion of solid bismaleimide which dissolves during mixing and prepreg manufacture will be close to zero weight percent, and is generally less than about 20 weight percent of the total solid bismalei.~,i.le component added. However, in some cases, an appreciable amount of solid bismaleimide whichremains In solid form wiil vary along with the other system components. Preferably, the amount of solid bismaleimide which dissolves during slurry mixing will not appreciably exceed the storage temperature solubility of that particular bismaleimide. The "substantial amount" of bismale;~l.ide remaining in solid form may, in some cases, be as low as 10 weight percent of added solid bismaleimide, but is generally and preferably much higher.
Various prophetic examples that clarifies the term "substantial portion" are found in U.S. Pat. No. 5,003,018, which is incorporated herein by reference.
A less preferable means of slurry mixing the components in accordance with the subject invention is to heat the bismalci."-x'e component above its melting point and add it slowly to the continuous phase under conditions of high shear. The mixing may be cooled down to a temperature below the melting point of the bismaleimide either before .
CA 022373~9 1998-0~-11 the start of iiquid bismalei.l) ~'e addition, during the course of the addition, or following the addition. However, it is necessary that the high shear conditions be maintained during the addition and cooling processes in order that the desired bismaleimide fine particles size may be maintained. This method is impractical when using bismaleimides 5 with a particularly high melting points. It is also not of use, and therefore not within the scope of this invention when the liquid system is prone to supercooling. Under these conditions, a meP~t~hle resin system, initially containing no solid bismaleimidedispersed therein, will be retained.
In another, less preferred method, the solid bi~llal0imide is added in the form of 10 relatively coarse particle to the continuous phase under high shear such that the shear forces result in rapid size reduction to a range below 20 i~m, preferably from 1 to 5 ,um.
Shear mixers suitable to create the desired conditions are available commercially.
When using such high shear mixers, the resin mixtures must often be cooled, as the heat buildup which results from the high energy shear conditions would otherwise raise 15 the temperature of the resin by an undesirably high amount. The temperature must be kept appreciably below the temperature at which complete solubility of the solidbi~,.llal~imide would result.
A further means of practicing the subject invention is to first fuse together at least a portion the resin ingredients, including a portion of the total bismaleimide component, 20 in a conventional manner. Then, the additional solid bismaleimide is added at a lower temperature, either as fine particles of suitable size, or as larger particles followed by in situ size reduction, for example by using the high shear mixing technique previously described.
The mixing temperature is critical to the optimal use of the process of the subject 25 invention. This temperature should be as low as is practical for the resin components involved. For example, if suitable high torque mixers are available, slurry mixing of bismaleimides into even highly viscous comonomers may be accomplished at room temperature or below. However, it is frequently desirable to elevate the mixing temperature by a modest amount. With comonomers which are solid at room 30 temperature or too highly viscous, elevated temperature or too highly viscous, elevated temperatures may be necessary. The most desirable temperature may easily be determined by one of ordinary skill in the art.
The slurry mixing method described below is used to improve processing, increase "tack" and increase room temperature storage stability. The solid monomer 35 (solid reactant) remained as solids in a slurry. This method is also a necessary CA 022373~9 1998-0~-11 component of the invention as the resin could not be made without slurry mixing and still have good prepreg tack and drape and slurry mixing gives the impregnated fibers (prepreg) good room temperature storage stability.
The procedures for conducting the weight loss test consisted of preparing test 5 specimens 5 cm x 12.5 cm from the cured test panels. These test specimens werewei~l ~Led and then allowed to stand in an air circulating oven at 232~C or 260~C. The specimens were weighted after 6 weeks for weight loss due to oxi~tion. The percent weight loss was c~lu)l~t3d by dividing the weight after 6 weeks aging by the initial weight and subtracting from 100. The data is reported in the Table. The test was10 analyzed by comparing the weight loss of the various composites. The less the weight loss the more oxidatively stable the composite.
The following specific examples are intended to illustrate certain aspects of the present invention; they are not to be construed as li"~ lions thereof.
F~rnple 1 PPB with 0.1% hydroquinone ("HQ") was heated at 120~C until complete solution was achieved. 50 parts (w/w) of PPB with HQ were heated to between 70~C to 95~C
followed by addition of 50 parts (w/w) of the ground MDA-BMI and 0.05 parts (w/w) hydroquinone. The hydroquinone was heated at 121 ~C until all hydroquinone had dissolved. This "slurry" mixture was stirred until homogeneous. This pre-polymer resin 20 at 70~C to 95~C was metered onto silicone release paper then pressed (impregnated) into T-300 3K 70P Type carbon fiber fabric. The resin content was 30-35% the balance being carbon fiber. This impregnated fabrics were stacked 12 plies thick. Test panels were prepared by placing the stacks into a "vacuum bag" followed by heating in an autoclave at 85 psi at 227 for 6 hours. The test specimens were cut from the panels 25 and tested in weight loss according to the procedures described below in the test section. The weight loss of the cured composite at 232~C is 68% and at 260~C is 1 .62%.

CA 022373~9 1998-0~-11 Example 2 (Comparative) 40 parts (w/w) of DABA and 0.15 parts of TPP were heated to between 70~C to 95~C followed by addition of 60 parts (w/w) of the ground MDA-BMI. This "slurry"mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer 5 resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 2.14% and at 260~C is 4.53%.
~xan~rle 3 (Comparative) 25 parts (w/w) of PPB with 0.1% hydroquinone (HQ) and 25 parts (w/w) DABA
were heated to between 70~C to 95~C followed by addition of 50 parts (w/w) of the ground MDA-BMI. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example i. The weight loss of the cured composite at 232~C is 1.22% and at 260~C is 2.g9%.
Example 4 47.5 parts (w/w) of PPB with HQ and 5 parts (w/w) of RDGE were heated to between 70~C to 95~C followed by the addition of 47.5 parts (w/w) of the ground MDA-BMI. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin.
This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.91 %
and at 260~C is 1.74%.
F,~ple 5 50 parts (w/w) of PPB with HQ and 10 parts (w/w) of CPMI were heated to between 70~C to 95~C followed by addition of 40 parts (w/w) of the ground MDA-BMI.
This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.65% and at 260~C is 2.58 %.

CA 022373~9 1998-0~-11 Example 6 40 parts (w/w) of PPB with HQ and 10 parts (w/w) of CPMI were heated to between 70~C to 95~C followed by addition of 50 parts (w/w) of the ground MDA-BMI.
This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured co,.,posile at 232~C is 0.73 % and at 260~C is 1.57%.
FY~mple 7 45 parts (w/w) of PPB with HQ and 5 parts (w/w) of C-STIL were heated to between 70~C to 95~C followed by addition of 60 parts (w/w) of the ground MDA-BMI.
This "slurry'' mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.64% and at 260~C is 1.50 %.
FY~rnple 8 40 parts (w/w) of PPB with HQ and 10 parts ~w/w) of T-STIL were heated to between 70~C to 95~C followed by addition of 50 parts (w/w) of the ground MDA-BMI.
This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.75% and at 260~C is 1.83 %.
Example 9 40 parts (w/w) of PPB with HQ and 10 parts (w/w) of TPE were heated to between 70~C to 95~C followed by addition of 50 parts (w/w) of the ground MDA-BMI.
This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.69 % and at 260~C is 1.72 %.
Example 10 (Comparative) 50 parts (w/w) of PPB with HQ were heated to between 70~C to 9~~C followed by addition of 50 parts (w/w) of the ground TDA-BMI. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 2.47 % and at 260~C is 7.63 %.

CA 022373~9 1998-0~-11 F~mple 11 (ComDarative) 50 parts (w/w) of PPB with HQ were heated to between 70~C to 95~C followed by addition of 50 parts of (w/w) of the ground BMI-MP. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 1.60 % and at 260~C is 3.17%.
FY~rnple 12 50 parts (w/w) of PPB with HQ were heated to between 70~C to 95~C followed by addition of 30 parts (w/w) of ground MDA-BMI and 20 parts (w/w) of ground BAPP-BMI. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin.
This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.79 %
and at 260~C is 1.64 %.
Example 13 50 parts (w/w) of PPB with HQ were heated to between 70~C to 95~C followed by addition of 40 parts (w/w) of ground MDA-BMI and 10 parts (w/w) of ground BAPP-BMI. This "slurry" mixture was stirred until homogenous to make the pre-polymer resin.
This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.79 %
and at 260~C is 1.58 %.
FY~mple 14 49.5 parts (w/w) of PPB with HQ and 1 part (w/w) of hydroquinone were heated to between 70~C and 95~C followed by addition of 49.5 parts (w/w) of ground MDA-BMI.
This "slurry" mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weight loss of the cured composite at 232~C is 0.72 % and at 260~C is 1.62%.
~xample 15 (Comparative) 60 parts (w/w) of C-796 were heated to between 70~C to 95~C until homogenous followed by addition of 40 parts (w/w) of PPB with HQ. This mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weightloss of the cured composite at 232~C is 1.12 % and at 260~C is 2.54%.

CA 022373~9 1998-0~-11 Fxample 16 (Comparative) 60 parts (w/w) of C-353A were heated to between 70~C to 95~C until homogenous followed by addition of 40 parts (w/w) of PPB with HQ. This mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example t.
The weight loss of the cured composite at 232~C is 1.12 % and at 260~C is 2.54%.Example t7 50 parts (w/w) of C-353A were heated to between 70~C to 95~C until homogenous followed by addition of 50 parts ~w/w) of PPB with HQ. This mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example t.
The weight loss of the cured composite at 232~C is 0.97 % and at 260~C is 2.18 %.
FY~rnple 18 (Comparative) 50 parts (w/w) of PPP were heated to between 70~C to 95~C followed by addition of 50 parts (w/w) of the ground MDA-BMI. This "slurry" mixture was stirred untilhomogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same way as in Example 1. The weightloss of the cured composite at 232~C is t.38 % and at 260~C is 10.78.
F~rnple 19 25 parts ~w/w) of PPP and 25 parts of PPB were heated to between 70~C to 95~C rollowed by addition of 50 parts (w/w) of the ground MDA-BMI. This "slurry"mixture was stirred until homogenous to make the pre-polymer resin. This pre-polymer resin was then metered, impregnated, autoclave cured and tested the same as in Example 1. The weight loss of the cured composite at 232~C is 0.94 % and at 260~C is 2.32 %.

CA 022373~9 1998-0~-11 TABLE

EXAMPLE BMI NON-BMI Weight loss Weight Loss at COMPONENTSCOMPONENTSat 232~C (%)1 260~C

MDA-BMI50 PPB 50 0.68 1.62 2C MDA-BMI60 DABA 40 2.14% 4.53%
(0.15% TPP) 3C MDA-BMI50 DABA 2!~ 1.22 2.99 4 MDA-BMI PPB 47.6 0.91 1.74 47.5 RDGE 5 MDA-BMI40 PPB 50 0.65 2.58 6 MDA-BMI50 PPB 40 0.73 (1)1.57 7 MDA-BMI50 PPB 45 0.64 1.50 8 MDA-BMI50 PPB 40 0.75 1.83 g MDA-BMI50 PPB 40 0.69 1.72 10C TDA-BMI50 PPB 50 2.47 7.63 llC BMI-MP 50 PPB 50 1.60 3.17 12 MDA-BMI30 PPB 50 0.79 1.64 15 13 MDA-BMI40 PPB 50 0.79 1.58 14 MDA-BMI PPB 49.5 0.72 1.62 49.5 HYDRO 1.0 15C C-796 60 PPB 40 1.12 2.54 16C C-353A 60 PPB 40 1.12 2.54 17 C-353A 50 PPB 50 0.97 2.18 20 19C MDA-BMI50 PPP 50 1.38 10.78 18 MDA-BMI50 PPB 25 0.94 2.32 Six weeks aging at the indicated temperature It will be appreciated that variations and modifications to the products and methods can be made by the skilled person without departlng from the spirit or scope of the invention as defined in the appended claims.

Claims (7)

WHAT IS CLAIMED IS:
1. A thermosettable, curable, resin composition prepared by slurry mixing, the composition comprising A. a solid alkylene dianiline bismaleimide resin selected from the group consisting of methylene dianiline bismaleimide, bis(aminophenoxyphenyl)propane bismaleimide, oxydianiline bismaleimides, bis(aminophenoxy)benzene bismaleimides, diaminodiphenylsulfone bismaleimides, diaminodiphenylisopropylidine bismaleimides, diaminodiphenylketone bismaleimides, diaminodiphenyl sulfide bismaleimides, diaminodiphenylhexafluoroisopropylidine bismaleimides and bis(diaminodiphenylisopropylidine)benzenes bismaleimides; and B. a liquid propenyl benzophenone co-reactant;the reactant and co-reactant present in a weight ratio of substantially about 1:1 in which the composition after curing has a decreased weight loss upon thermal aging.
2. The composition of claim 1 wherein said benzophenone co-reactant is 4,4'-bis(o-propenylphenoxy)benzophenone.
3. The composition of claim 1 wherein said reactant and co-reactant comprises greater than about 70 percent total weight of reactive components in said composition upon curing.
4. A process for preparing a thermosettable curable resin composition which comprises A. slurry mixing a powdered methylene dianaline bismaleimide resin reactant into a curing agent; and B. combining the reactant-curing agent mixture into a liquid homogeneous benzophenone co-reactant which has been heated to between 50°C and 150°C.
5. A thermosettable, curable, resin composition for composite or adhesive applications comprising A. a solid alkylene dianiline bismaleimide resin selected from the group consisting of methylene dianiline bismaleimide, bis(aminophenoxyphenyl)propane bismaleimide, oxydianiline bismaleimides, bis(aminophenoxy)benzene bismaleimides, diaminodiphenylsulfone bismaleimides, diaminodiphenylisopropylidine bismaleimides, diaminodiphenylketone bismaleimides, diaminodiphenyl sulfide bismaleimides, diaminodiphenyl hexafluoroisopropylidine bismaleimides and bis(diaminodiphenylisopropylidine)benzene bismaleimides; and B. a liquid benzophenone co-reactant;the reactant and co-reactant present in a weight ratio of substantially about 1:1 in which the composition after curing has a decreased weight loss upon thermal aging.
6. The composition of claim 5 wherein said benzophenone co-reactant is 4,4'-bis(o-propenylphenoxy)benzophenone .
7. The composition of claim 5 wherein said reactant and co-reactant comprises greater than about 70 percent total weight of reactive components in said composition upon curing.
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