Brief Description Of The Invention

A composition and process that results an expanded molded product from a resin composition possessed of predetermined orientation of expansion and cure. The composition comprises a thin layer containing m situ- expandable materials ranging from solid chemical blowing agents to thermoplastic particles containing expansion chemicals, and a thermosettable matrix resin. The layer has an essentially uniform density and thickness across its oreadth, and has the capacity of expansion in height, widtn and length directions. The layer is filled with insoluble and matrix-resm incompatible particles with an aspect ratio greater than 1 which particles are uniformly distributed and oriented m a pattern within the layer such that they nurture the orientation of expansion of the layer in favor of expansion in not more than two of the height, width and length directions in making the molded product.

Composites of the layer and syntactic foam and/or other products are made by thermally curing the matrix resin in the layers while the layer is in association with the syntactic foam and/or other products. During curing of the resin, whether the layer is composited or not, the in situ-expandable particles expand b\ volatilization and/or decomposition to form a uniform cellular resin structure with a predetermined dιrectιon(s) of expansion.

Background. To The Invention

Syncore®, sold by The Dexter Corporation, Adhesive & Structural Materials Division, Pittsburgh, CA 94565 U.S.A., is a syntactic foam film that takes the place of more expensive prepreg plies in stiffening critical structures. This isotropic foam is a composite material consisting of preformed microballoons in a thermosetting matrix resin. A wide variety of preformed microballoons and matrices can be combined to make SynCore® materials. Glass is the most common microballoon material of construction, but quartz, phenolic, carbon, thermoplastic ana metal coated preformed microballoons have been used. Epoxies curing at 350°F. (177°C.) and 250°F. (121°C.) are the most common thermosetting matrix resins, but matrices of bismaleimide (BMI) , phenolic, polyester, PMR-15 polyimide and acetylene-terminated resins have been used to produce SynCore® syntactic foams. As a result of the variety of materials that successfully make Syncore®, they are tailorable to a variety of applications. There is a version of SynCore® available that will co-cure with all known available heat-cured composite laminating resins. Syncore® allows sandwich core concepts to be useα in a thinner dimension than previously possible. The thickness limit on honeycomb cores is approximately 0.125 inch. Syncore® is available in 0.007 to 0.125 inch (0.18 mm to 3.2 mm) thicknesses but can be made in thinner or thicker sheet forms. Other core materials such as wood and sheet foam can be made thin, but are not αrapable and generally require an adhesive film to bond to the partner composite components. I addition, Syncore® possess excellent uniformity in thickness which provides the ability to assure quality for the composite n which it is used as a component. Syncore® is typically used to replace prepreg

plies where the intent is to increase stiffness by increasing thickness.

Designing with Syncore® is straightforward because all of the analysis methods that apply to other core materials such as honeycomb apply to it. Flexural stiffness of flat plates and beams increases as a cubic function of thickness allowing a lighter, stiffer lamination than could be made from prepreg plies alone. Since Syncore®, on a per volume basis, typically costs less than half of a comparable carbon prepreg, it also leads to a lower cost lamination. This is illustrated by the following:

1. Adding one ply of .020 inch Syncore® and eliminating one ply of prepreg does not change the weight or cost significantly, but nearly doubles the flexural rigidity.

2. Adding one ply of .020 inch Syncore® and eliminating three plies of prepreg sharply decreases the cost and weight with a small decrease in rigidity.

3. Adding one ply of .040 inch Syncore® and eliminating three plies of prepreg provides lower weight, cost and sharply increases rigidity.

4. The introduction of unidirectional tape allows a further increase in performance at lower cost and weight at nearly the same thickness.

5. A hybrid tape/fabric/Syncore® construction gives a very attractive set of weight ana cost savings coupled with a 3.4 times increase in flexural rigidity.

Syncore© has been recommended for thin composite structures in any application where flexural stiffness,

buckling, or minimum gauge construction is used. It has been shown to save weight and material cost in carbon fiber composites. It has been offered to save weight at approximately the same cost in the case of glass fiber composites. Illustrative applications are covered in U.S. Patents Nos . 4,861,649, patented August 28, 1989, and U.S. Patent No. 4,968,545, patented November 6, 1990.

The manufacturing methods for employing Syncore® are very similar to those used for prepregs. Because it is not cured, it is tacky and very drapable when warmed to room temperature and is easier to lay-up than a comparable prepreg ply. It can be supplied in supported forms with a light weight scrim to prevent handling αamage when it is frozen. It requires cold storage like prepregs, usually 0°F. (-17.7°C.) or below. The various Syncore® materials typically have a room temperature out- time that is much longer than their companion prepregs. Syncore® is less sensitive to cure cycle variations than prepreg making the controlling factor the composite cure cycle selection. It will cure void free under full vacuum or low (e.g. about 10 p.s.i.) autoclave pressure. It has been cured at up to about 150 p.s.i. without exn biting balloon crushing.

In a typical application, a sandwich of Syncore® and prepreg, such as a thicker layer of Syncore® between two thinner layers of prepreg, are held together under heat ana pressure to cure the structure into a strong panel. Typical sandwich constructions of this nature are shown in U.S. patents 4,013,810, 4,433,068 and 3,996,654. Sucn composite structures typically are produced m flat sheets and in separatable molds to obtain various desireα shapes .

Though Syncore® will cure void free under significant reduced pressure or when put under pressure, it would be desirable to avoid those costly conditions to achieve void reduction. It would be desirable to have a material that has the properties of Syncore® but achieves void free construction without costly full vacuum operations or low autoclave pressure systems. These methods are typically batch type operations that materially add to the cost of making the composite. There are certain applications in which it is desirable to have the properties of a uniform thin drapable syntactic foam film in processing the formation of a laminated composite, yet have the capacity to autogenously expand so as to fill any void space existing in the composite's structure so as to minimize the effects of macro and micro void defects at interlaminate interfaces .

These mterlaminar mterfacial micro or macro void spaces are magnified by the irregularity of the reinforcing layer of the composite structure. For example, if the composite is of a layer of prepreg- derived carbon fiber reinforced thermosetting resin material, oonded to a syntactic foam, such as a Syncore® thin uniform film, the layer containing the prepreg- derived material will have an irregularly shaped surface and the Syncore® layer will have a relatively smooth uniform surface. Though the Syncore® is tacky ana drapable, it is incapable of filling in all of the irregularities of the prepreg-derived layer. Applicaticr of a full vacuum or the use of a low pressure autoclave can be used to significantly reduce the void space, but complete avoidance of micro voids is not readily achievable. Also, conforming Syncore® to the irregular surface causes transfer of the irregularity tc the

opposite surface of the Syncore® film. Such surface irregularity transfer may be avoided by sandwiching the Syncore® film using heat and pressure, such repositions the film's matrix resin and the microspheres so that the film within the sandwiched structure loses its original uniformity.

It would be desirable to be able to adequately bond a syntactic foam thin film to an irregular surface ¹ and fill the defects in the surface without transferring the shape of the defects to the unbonded side of the film. It would also be desirable to be able to adequately bond a syntactic foam thin film to a surface and, without the use of vacuum or low pressure autoclaves, fill the micro voids with the syntactic foam without repositioning the film's matrix resin and microspheres.

An advantage of Syncore® for many applications resides m its uniformity of distribution of the microsphere throughout the matrix resin. Such microspheres remain essentially intact throughout the cure cycle. As a result, it is not possible to have the microspheres concentrate at one or more surfaces, or one or more other locations in the final composite. It would be desirable to have a drapable thin film, having the handling qualities of Syncore®, but which would allow the production of a syntactic foam having a controllable density gradient that accommodates specific enα use applications .

There are a number of applications in which a thin f lm syntactic foam could serve as a seal to preclude the passage of gases and liquids. In some applications, the

¹ Such a surface is one that may contain undulations, cracks, large pores, warpage. andthe like defects

seal could be subjected to abrasion forces. It would be desirable to have a thin film syntactic foam that can be applied in a manner that allows it to be a sealant to gas or liquid flow m a confined space and be able to withstand abrasive forces.

There is a body of technology directed to fabricating expandable thermoplastic resinous material. For example, U.S. Patent No. 2,958,905, patented November 8, 1960, is directed to a method of making foam structures from particulate expandable granular thermoplastic resinous material containing in the particles a blowing agent for further expansion of the particles. A considerable number of thermoplastic resins are described as suitable for this purpose. The blowing agents are the conventional ones recommended for that application. The expandable granular thermoplastic resinous material may be admixed with a thermosetting resin to generate on curing the exotherm needed to expand the expandable granular thermoplastic resinous material. The resulting mass can be poured into a mold to make a number of products. The patentees indicates that the expandable granular thermoplastic resinous material can be formed in the presence of non-expandable filler materials such as staple fibers from a variety of sources, and the mixture fed to a mold for forming an expanded product. The resulting foamed product may be designed to adhesively oond to a fabric layer for reinforcement of the foamed product. The density of the foamed product can be controlled by the amount of the expandable material feα to tne mold. According to the patentees, starting at column 12, lines 5 et seq., molded products are formed b- charging tne mold "with the expandable material m any desired manner including manual filling or pneumatic conveyance tnereof." Accordmσ to the description at

column 12 relating to Figures 3 and 4 (see column 12, lines 16-32) :

"a considerable occurrence of void and hollow spaces occurs between the charged expandable beads 21 m the mass to be fabricated, each of which (in the case of preexpanded material) is a foam structure containing a plurality of internal cells or open spaces. When the liquid exothermus substance is added between such interparticle voids, the heat from its spontaneous self reaction causes the beads to expand whereby, as illustrated in Figure 4, the expanded and fabricated particles 22 force out a substantial portion (and frequently most) of the exothermus substance excepting for a minor quantity of reacted material 23 which remains, frequently as an interlaced and interlinking network between the expanded particles to assist in holding the expanded, cellular foam particles together." (Emphasis added)

U.S. Patent No. 2,959,508, patented November 8, 1960, describes another variation of using expandable thermoplastic particles. In this patent, the unexpanded particles and the exothermus substance, such as an epoxy resin, are first mixed and then poured into the mold to form a composite foam of the two when the exothermus suαstance heats up the mixture and causes the blowing agent to volatilize. The patent also suggest the use of chemical blowing agents m combination with the use of expandable thermoplastic particles.

*-. commercial version of the expanded thermosetting resins is used for "core splicing." Core splicing involves the use of a tnin film epoxy resin intumescent adnesive of the pourable or film type that is maintained

Decween release surfaces, such as polyethylene film and

release paper then applied in this condition to the composite core structure for adhesive bonding of the structure. Expansion is effected by the presence of solid blowing agents in the resin composition. It splices together irregular surfaces. It is deposited on one surface to be bonded, and the other surface is brought into contact with the adhesive coating. Cure of the adhesive unifies the two parts. One such product is Hysol™ EA 9814NA, sold by The Dexter Corporation, Hysol Aerospace Products, Adhesives & Structural Materials Division, .

Thermosetting resins have had blowing agents incorporated in them (see U.S. Patent No. 3,322,700, patented May 30, 1967) to form expanded molded products and recently, such types of resin systems have included preformed microspheres in the formation of partial syntactic foam films. These expanded thermosets comprise a more open cellular structure unlike that of syntactic foams, and the inclusion of preformed microspheres does not alter that condition.

There are commercial molding processes that utilize tacky sheets of thermosetting resins and reinforcing material. One such process involves the compression molding of sheet molding compounds ("SMC") . In that process, a thermosetting polyester resin filleα w t staple glass fiber and low profile thermoplastics, are sheeted out and thickened into a pourable paste retained between release surfaces such as polyethylene film. Cnunks of the thickened paste are casually depositec around the surface of the mold by hand, and on clos nq the mold with neatmg, the paste is liquified and t, ana its fiber loading, are redistributed around the mold to fill it up and form the desired molded article. In otner wore, the chunks of sheets of SMC represent a convenient

way in which to add a liquifiable moldable material to the mold. This process is presently commercially practiced in a number of industries. Advantages of the process are the convenience of storing moldable mixture and the ease of loading a mold with the molding composition.

The Invention

This invention relates to the selective foamed expansion of thermosettable resin by uniformly incorporating througnout the resin, solid particles naving (l) an aspect ratio (i.e., ^{e g} ) greater than 1 width and (n) thermal stability at the temperature of expansion of the resin, m such a manner that the particles are oriented in the direction of their length, in one or two directions in the resin. The invention is directed to all manner of expandable thermosettable resins, particularly those of the type that form adhesive films and molded articles.

The invention relates to a composite chemical composition and process that results an expanded moldeα product. The composite chemical composition is a filled resin composition possessed of predetermined orientation cf expansion and cure. The composite resin composition is provided as a thin layer of a mixture of a tnermosettable matrix resin and in situ-expandable particulate materials ranging from solid chemical blowing agents to thermoplastic particles containing expansior cnemicals . The layer contains an essentially uniform αensity and tmckness across its breadth, and has the capacity of expansion in height, width and lengtn directions .

The layer is filled with insoluble and matrix-resin incompatible particles with an aspect ratio greater than 1 that defines a longitudinal axis (length) of the particles. The longitudinal axis of these particles are typically not greater than about one inch (2.54 cm.) , preferably not greater than about H inch (1.905 cm.), and most preferably, not greater than about H inch (1.27 cm.) . These particles are not mterbonded except to the extent held in the layer by the matrix resin or a component of the formulation including the matrix resin. These filler particles possess thermal stability at the temperature of expansion of the resin. This means that the surface [s] of the filler particles remain solid at the temperature of expansion of the resin. These filler particles constitute from about 2 weight percent to about 35 weight percent of the weight of the layer. The particles are uniformly distributed and oriented in a pattern and an amount within the layer such that they nurture the orientation of expansion of the layer in making the molded product. The orientation of expansion is in not more than two of the height, width and length directions. Thus, the orientation of expansion may be in one of height, width or length directions, or in height and width directions, or in height and length directions, or in width and length directions.

Cured composites are made by thermally curing the matrix resin in the layer. During curing of the resin, the particulate chemical blowing agent or the in situ- expandable thermoplastic particles expand by chemical αecomposition or volatilization, as the case may be, to form a uniform cellular resin structure witr ar orientation of expansion in not more than two of the height, width and lengtn directions. Expansion of the laver is most favorably oriented m tne directions normal

to the general orientation of the particulate filler. Thus, particles oriented in the length direction hamper expansion of the layer in that direction while facilitating expansion of the layer in the width and height directions. Orientation that is uniformly skewed between the length, width and height directions, not an objective of this invention, will achieve a more uniform expansion in all of those directions.

The invention encompasses a moldable thermosettable resin mass in the form of a layer with a width and/or length that is greater than its thickness, into which there are uniformly distributed a) discrete, incompatible in situ-expandable thermoplastic particles and/or a particulate chemical blowing agent in a thermosettable matrix resin; and b) unidirectionally or bidirectionally oriented, solid particles having an aspect ratio greater than 1 and whose longitudinal axis is not greater than about The resins are employed in two type of molding systems: In one, the resin is pourable mass containing the solid particles in an nonoriented condition, and upor introduction to mold, orientation of the solid particles is achieved. The pourable mass is formed into a layer in the mold before molding takes place. In the other, tne tnermosettable resin is provided as a nonpourable filr within which the particle are oriented as aforesaid that contains the capacity for m si tu expansion and can be deposited into the mold as such. In another embodiment, the layer of such materials, typically as a thin film, is used as an adhesive. In tn s emboαiment, the layer (or film) is place on one aαnerend, using standarα core splicing techniques, ana

W ^y vOυ 9v6o/1ι77 ² 23 ^J PCT/US95/16314

13

the other surface to be bonded in superimposed on the layer, followed by curing of the layer to effect a desired level of adhesion between the adherends. The invention is particularly desirable for core splicing of honeycomb cores.

This invention relates to an oriented particulate reinforced, thin, tacky film of incompatible m situ- expandable thermoplastic particles and/or particulate chemical blowing agents in a thermosettable matrix resin that contains an essentially uniform density and thickness across the breadth of the film. The invention is directed to an adhesive or moldable in situ-expandable composition in the form of a thin film that is not pourable yet can be easily dispensed in a uniform manner as an adhesive or within a mold and thereafter expanded without liquification to the dimensions, in the case of an adhesive application, of the space between adherend surfaces, or of the mold. In either case, the invention is to provide a cured expanded foam that may be syntactic and has an orientation of expansion in not more than two of the height, width and length directions. The m si t u- exoansion can be carried out without major redistribution cf the mass to form a foam thermoset (cured) article with a oredetermineα density pattern and a predetermined orientation of expansion.

This invention is also directed to moldable, m si t u- exυandable, films comprising a mass of m situ-expandable tnermoplastic particles of different expandabilities, uniformly distributeα in a matrix thermosetting resir that is incompatible with the thermoplastic polymer of the m situ-expandable particles. This incompatibility exists throughout the thermal in situ-expansion cycle in forming tne thermoset syntactic foam structure. During

this cycle, the incompatible expandable thermoplastic particles sufficiently softens while at the same time expansion agents therein volatilize so as to reform the particles into hollow microsphere whose outer walls comprise the thermoplastic polymer, forming closed icrocells. A significant advantage of the invention is the formation of thermoset syntactic foam films of uniformly distributed expanded closed-cell microspheres that have a density less than thermoset Syncore® containing preformed microspheres (not in situ-formed) , yet possesses comparable properties for replacing more expensive prepreg plies in stiffening critical structures.

This invention relates to a thin, uniform, tacky, non- pourable film of an incompatible mixture of in situ- expandable thermoplastic particles and/or particles of solid chemical blowing agents, that are dispersed in a thermosettable matrix resin containing oriented reinforcing particles uniformly dispersed therein that contain an aspect ratio in which the measurement of length to width of the particles exceeds 1 and whose longitudinal axis is not greater than about one inch (2.54 cm.) . The film can be accurately dispensed in a mold or deposited on an adherend without pouring and, upon subjecting the dispensed films to heat, obtaining a cured foam that possesses an expansion oriented in a direction lateral of the orientation of the particles. The invention also includes the ability to heat the dispensed film in the mold or on an adherend in a uneven manner to effect a thermal gradient on the adherend or in the mold and obtain a cured product having a density gradient throughout that is responsive to such thermal gradient. As a result of the invention, there may be obtained shaped foam structures possessing a favored

degree of expansion with stiffness and strength variability or uniformity depending on the end use application.

This invention relates to such an expandable film, which embodies a composition and process that results in an expanded adhesive or molded product possessed of predetermined expansion and cure m that predetermined expanded state. In this embodiment of the invention, the expanded molded or adhesive product that is possessed of predetermined expansion and cure in that predetermined expanded state is from a thin, tacky film of m situ-expandable (l) thermoplastic particles and/or (n) solid chemical blowing agent particles, in a thermosettable matrix resin that contains an essentially uniform density and thickness across the breadth of the film and contains insoluble and matrix-resm incompatible particles with an aspect ratio greater than 1 and a longitudinal axis is not greater than about one inch (2.54 cm.) uniformly distributed within the film and oriented in the film in a manner that nutures the direction of expansion of the film ιr making the adhesive or molded product, as the case may be.

Cured foam composites of the films are made by thermally curing the matrix resin in the films.

This invention is directed to a tacky and αrapable, non-pourable film having a uniform (±10%, preferably ±5%) thickness throughout, between about 1 millimeter to about

5.5 millimeters, that contains ( ) a continuous pnase of

16

a thermosetting matrix resin system and (11) a discontinuous phase of two classes of particles essentially uniformly distributed throughout the thermosetting matrix resin system. One particle category comprises either an m situ-expandable thermoplastic polymer containing an expansion agent therein, a solid chemical blowing agent or a mixture of the two. The other particle category is a matrix-resm incompatible solid of organic or inorganic origin that (a) is thermally non-shapable during molding of the film and (b) possesses an aspect ratio (i.e., ^lenZth ) of greater than one width ana whose longitudinal axis is not greater than about one inch (2.54 cm.) . This other category of particle is distributed throughout the continuous phase such that its length is oriented in a single direction. Both (I) and

(n are uniformly distributed throughout the film, so that upon expansion of the thermoplastic polymer or decomposition of the chemical blowing agent to create microcells in the film, the resulting film is a thermoset thin foam film the thickness of which is about 1.01, preferably about 1.1, to about 5.5 times greater, preferably to about 4.5 times greater, than the non- expanded film. In addition, because of the orientation of the other category of particles, expansion of the film ends up favoring one or two of the dimension of w dtn, height or lengtn.

A feature of the non-pourable, tacky and αrapabie films is that wπile their thicknesses are uniform, the resultant cured foam may vary considerably in terms of density and thιcκness because of curing conditions. It is desirable tnat the insoluble and matrix-resir incompatible particles with an aspect ratio greater thar 1 and a longitudinal axis is not greater than about one

inch (2.54 cm.) reside in the thin, non-pourable, drapable non-expanded uniform film in manner that allows, upon expansion by uniform application of heat throughout the film, while free of any confinement, the formation of an oriented expanded film having a uniform (±10%, preferably ±5%) density throughout. Another embodiment of the invention provides that the film have the capacity to expand in favor of one direction over another. That is accomplished by providing in the film as an uniformly distributed component, insoluble and matrix-resm incompatible particles with an aspect ratio greater than 1, as aforesaid, oriented in the film in a manner that nutures the direction of expansion of the film in ma ιng the foam product. A feature of the films of the invention is that the thermoplastic particle softens and the chemical blowing agent decompose, as the case may be, sufficiently for expansion at the temperature under which the thermosetting matrix resin undergoes cure. Since such thermosetting resins are curable to temperatures as high as 400°C, essentially all thermoplastic polymers are amenable for use as the thermoplastic particle component and all chemical blowing agents are similarly effective.

The invention allows the facile production of thermoset foams of unique conformance to and predetermined density and orientation within the moldeα volume of confinement of d) a conventional mold or (n between two adherend surfaces. The "molded volume of confinement" means that mold or adhesive space occuoieα by thermoset foams of the invention and physically encompassing the boundaries of the thermoset foam. Tne molded volume of confinement is restricted by metal olα surfaces or the adherend surfaces encompassing the mold volume within which expansion of the nonpourable, tacky

and drapable film occurs. The mold volume of confinement is also restricted by other materials to which the thermoset foam, such as a syntactic foam, of the invention adheres in the molding or adhesive operation, to form a composite structure. The other materials may be derived from thin metal films or foils (such as aluminum, steel, titanium, and the like), fabrics, prepregs, composites derived from molding prepregs, other fiber reinforced composites, preformed but uncured syntactic foams of other composition, and the like. In the typical case, expansion of the thin films or layers of the invention fill the molded volume of confinement whereas the other materials occupy no more of the mold's interior before cure as they do after cure. The invention encompasses a molding (including adhesive binding) process as well as molded (including adhesively bonded) products obtained from the molding process. The process comprises defining a molded volume of confinement (the mold with or without other materials therein) and a thermoset foam density for the resulting molded tnermoset foam. Then at least one layer of an amount of the non-pourable, tacky and drapable film having a uniform thickness, between about 1.0 millimeters to about 5.0 millimeters, that contains (i) a continuous phase of a thermosetting matrix resin system, (n) a discontinuous phase of particles of (a) an m situ- expandable thermoplastic polymer containing an expansion agent therein or (b) a solid chemical blowing agent, is deposited and distributed in the mold to achieve the defined density, and ( n) insoluble and matπx-resir incompatible particles with an aspect ratio less than 1 and a longitudinal axis that is not greater than about one inch (2.54 cm.) uniformly distributed within the film ana oriented in tne film m a manner that nutures the

direction of expansion of the film in making the molded product. Both (1), (11) and (m) are uniformly distributed throughout the film, so that upon expansion of the thermoplastic polymer into microcells in the film or decomposition of the solid chemical blowing agent into thermosetting resin lined microcells in the film, the resulting film is a thermoset thin film foam the thickness of which is about 1.01 to about 5.5 times greater, preferably about 1.1 to about 4.5 times greater, than the non-expanded film. It is possible to predetermine the uniformity and direction of expansion and the resulting density of the thermoset foam because both (I) and (n) are uniformly distributed throughout the film and (m) controls the direction of expansion, so that upon expansion of the thermoplastic polymer and/or decomposition of the chemical blowing agent into microcell formation, the resulting film is a thin film foar the thickness of which, as noted above, is greater than the non-expanded film. When sufficient energy is applied to the mold to advance the cure of the thermosetting matrix resin in the tacky and drapable film, to a temperature so as to sufficiently soften the thermoplastic particles and volatilize the expansion agent therein and/or cause the chemical blowing agent to decompose, a thermoset foam is produced. The mold cycle is completed when the desired density is achieved. Then the resulting molded product encompassing the foam is withdrawn from the mold or is left behind as part of the composite structure containing the adherend surfaces . As noted above, the thin and drapable in situ- expandable tacky films or the layers, as aforedefιneα, may be composited with other materials. A simple anc practical composite may be one which strengthens the film prior to expansion and conversion to the thermoset state.

The non-pourable, thin, drapable tacky films can be handled without supporting material. However, to avoid premature curing of the film and to assist its handling, it may be cold stored like prepregs, usually at 0°F. (- 17.7°C.) or below, and kept in that condition prior to use. Similar to the various Syncore® materials, the films of the invention typically have a room temperature out-time that is similar to the companion prepregs with which they would be molded. Because it is not cured, the film of the invention is tacky and very drapable when warmed to room temperature and is easier to lay-up than a comparable prepreg ply. It is desirable to make the film in supported forms with a lightweight scrim to prevent handling damage when it is frozen. In general, it will oe αesirable to affix the films to other, more durable thin layers that take handling better. For example, the non-pourable, thin, drapable, in situ-expandable films may be calendared to other layers, such as, to scrims, release paper, foils and plastic films. One convenient metnod of affixing handling materials to the films is to sandwich the film between plastic films. Adhesion of the film to the handling material typically relies on its tackiness. If the handling material is an open scrim, sucr as a woven, nonwoven or knitted scrim, the drapability of the film assists bonding because the film sags about the individual fibers or filaments of the fabric, and will mterbond through the opening in the scrim. However, as will be detailed below, such fabrics do not affect the orientation of expansion of the film. In addition, the films of the invention may be composited with a conventional syntactic and/or core splice type foam that comprises thin films of uniform thickness which contain rigid preformed microballoons uniformly dispersed in a resin matrix. The syntactic

foam composited with the in situ-expandable film may be any of the SynCore® syntactic foams with which it would co-cure.

In another embodiment of the invention, the thin and drapable tacky films of the invention may be composited with a layer of a prepreg and the composite deposited in a mold for forming a product of the invention. In that case, the prepreg/thin and drapable tacky film composite can be laid up in a mold in a variety of configurations to form a lightweight thermoset composite having good strength and stiffness.

In a further embodiment of the invention, the thin ana drapable tacky film of the invention may be composited with more than one layer of material. In particular, the composite may comprise a layer of the handling material and at least one layer of another material such as a preformed syntactic foam layer or a prepreg layer, or a combination of the two. Alternatively, the composite may comprise at least two layers of handling material, such as a layer of scrim and a layer of foil or two layer of foil or one layer of scrim and two layers of foil, or one layer of scrim and one layer of plastic, and the like.

A highly preferred embodiment of the invention comprises a thin and drapable tacky film or layer, eacn comprising a mass of staple thermoplastic fibers ana expandable thermoplastic non-fibrous particles and/or particulate chemical blowing agents uniformly distributed in a matrix containing a thermosetting resin that is incompatible with the thermoplastic polymer of the fibers and the expandable particles. In the case of the film, the matrix resin will be non-pourable. The thermoplastic fibers have a T-, or T _c that is greater than ' the cure temperature of tne matrix resin. The thermoplastic

polymer of the expandable particles soften and the expansion agent and the chemical blowing agent become volatile and decompose, as the case may be, at a temperature which is less than the cure temperature of the matrix resin. This fiber reinforced film preferably contains the fibers oriented in a direction within and on the surface of the film or layer that is essentially parallel to the film or layer's surface. The fibers may be wholly oriented in the length or width directions, or skewed between the two directions. When the film is expanded into a foam possessing the orientation described herein, the fibers at the surface to form a tough, abrasion resistant surface. This embodiment, in general, forms molded syntactic foams that possess unique surface abrasion resistance when compared with other syntactic foams . This embodiment provides foams suitable for aerospace applications, where the material needs to be tough to withstand erosion forces or impaction yet be lightweight, a universal requirement in aircraft applications.

An interesting embodiment of the invention involves scrolling the non-pourable, thin, drapable film, preferably while adhered to a scrim layer, into small diameter tubes about which are adhered prepreg layers containing carbon fiber reinforcement to form a composite tube containing a small hole in the center. Such composite tubes, when viewed cross-sectionally, have a αonut appearance. When the tube is cured, the hole lr the interior may be fully or partially filled with the expanded syntactic foam to provide a stiff inner core, along the lines described in U.S. Patent No. 4,968,545, patented November 6, 1990. The orientation of the particulate reinforcement car assure a αegree of expansion in a directior that minimizes stresses from

overlapped expanding film portions. Such a scrolled structure lends itself to manufacture of tubular constructions such a golf shafts and fishing rods.

Brief Description Of The Drawings Figure 1 is a schematic perspective (partially isometric) illustration of a calendaring system for making the m situ-expandable thin films of the invention .

Figure 2 is a schematic perspective (partially isometric) illustration of a variation of the calendaring system of Figure 1 which has means for including a supporting scrim layer in the thin film.

Figure 3 is a schematic perspective (partially isometric) illustration of a variation of the calendaring system of Figure 2 which has means for sandwiching a supporting scrim layer in the thin film.

Figure 4 is a schematic perspective (partially isometric) illustration of a variation of the calendaring system of Figure 1 which has means for including in the calendaring step a supporting scrim layer within the thin film.

Figure 5 is a schematic cross-sectional edge-view of the feed end of the calendaring operation of Figure , characterizing the particles of m situ-expandable thermoplastic polymer or the chemical blowing agent ana filler particles having an aspect ratio greater than 1, uniformly mixed in a thermosetting resin matrix.

Figure 6 is a schematic cross-sectional eαge-view of the calendaring operation of Figure 5, characterizing uniformly distributed staple fibers amongst the particles of m situ-expandable thermoplastic polymer or chemical

blowing agent distributed uniformly in the thermosetting resin matrix.

Figure 7 is an schematic edge-view of a thin film segment formed in the calendaring operation of Figure 6 illustrating the manner of orientation of the staple fibers in the thin film of matrix resin.

Figure 8 is a coating and calendaring operation suitable for making a layer of oriented into which is impregnated an m situ-expandable thermoplastic polymer distributed uniformly in a thermosetting resin matrix.

Figure 9 illustrate fiber laydown pattern obtained from a carding or garnettmg operation in which there are depicted options A, B, C and D for fiber orientation.

Figure 10 in an perspective end-view of a mold containing the thin film of the invention, suitable for forming molded pieces.

Figure 11 is a plan end-view of the mold of Figure 8.

Detailed Description Of The Invention

As note previously, syntactic foam films, such as Syncore®, are typically used in stiffness critical applications. The bending stiffness of a structure is proportional to the third power of thickness (T ³ ) . relatively slight fluctuation in thickness will result in a significantly large variation in stiffness. That art teaches us that controlling the film thickness is a crucial manufacturing parameter in making a molded composite structure from syntactic foams.

Space volume (foam cells) in thin uniform syntactic foam films such as Syncore® is achieved by substituting light hollow microspheres for the relatively dense matrix resin on a volume to volume basis. The amount of space

volume that can be achieved is limited by a physical barrier and a process obstacle.

The physical barrier occurs at maximum packing fraction. Recognizing that the objective involves packing spheres into a fixed volume, maximum packing occurs when point-to-point contacts are developed between adjacent/nearest packing spheres. Beyond this point, it is physically impossible to pack any additional spheres into this fixed volume. For monodispersed spheres, this represents about 64% of the packing volume. In commercially available multi-dispersed sphere systems, the weight reduction is limited by the particular system's packing fraction.

From a processing standpoint, adding glass microspheres to a matrix resin increases resin viscosity, similar to that of adding fillers or thixotropic agents to the resin. This viscosity increase is due to an interaction between the flowing resin and the surface of the sphere. In simplistic terms, as the resin moves past a sphere, it imparts an equal and opposite drag force on the surface of the sphere and develops a shear stress through the center of the sphere. Typically, the shear strength of hollow spheres is low and during processing the resin's viscosity increases proportionally to the volume of hollow spheres added. As a result of the proportional increase in shear stress caused by the resin's increased viscosity, sphere damage/fracture occurs. This shear stress is the primary cause of sphere damage/fracture during processing. Once the spheres are damaged, the weight saving advantage from the use of hollow spheres is negated.

This invention contemplates that these sphere related limitations are avoided by the use of expandable

thermoplastic particles and/or chemical blowing agents to m si t u generate microspheres from a thin film or layer to produce a thin (albeit thicker) foam film which is a syntactic foam when the particles are of the expandable thermoplastic type. These m situ-expandable thermoplastic and chemical blowing agent particles possess behavior and processing characteristics similar to pigments and fillers. The average particle size of the solid chemical blowing agent and the thermoplastic in situ-expandable particles are typically an order of magnitude, or more, smaller than the pre-expanded hollow sphere used in commercial thin film syntactic foams. For example, for a given volume, a significantly greater number of unexpanded particles may be added to a given volume of resin compared to the pre-expanded spheres. Since expansion takes place m si tu during the cure step, tne shear sensitivity of pre-expanded hollow spheres does not become a problem. This invention gives preference to the use of expandable thermoplastic particles as the means for achieving the syntactic foam structure. Their expansion is more controllable and more uniform.

PacKing of the expanded spheres is also more efficient Decause of in ≤itu-expansion. During cure, the matrix resin's viscosity, even though non-pourable at normal handling temperatures, such as at about room temperature (aoout 15-37°C.) or conventional handling temperatures (which can vary from application to application ) , decreases with increasing temperature and since the unexpandeα spheres are not in a point-to-point contact configuration, their environment is mobile and this allows each particle to expand within the film. This mobility results in a more densely mιcrosphere-pacκed lattice. However, m the general practice of the invention without the inclusion of solid insoluble

particles with an aspect ratio greater than 1, the film will be cut to the size of the mold or to the size of the adherend. As a result, because the expansion forces are three-dimensionally directed, this mobility is initially primarily in the upwardly z direction rather than in the laterally xy direction. As expansion takes place, the film's edge surfaces enlarge, so they expose more particles to heat through the edge surfaces. As a result, more of the particles at the edge surfaces initiate expansion so that a greater proportion of the particles continue to expand in the z direction.

The upward expansion is further magnified by having the film placed in the mold such that the edges of the film abut or essentially abut the wall or walls of the mold. The free expansion of the particles into microspheres is inhibited by the confining walls so that the internal expansion forces in the particles at the walls are directed more in the z direction initially. One might expect that the edges of the film would rise to greater heights in an otherwise vertical free expansion, but this is no. the typical case Free vertical expansion of the film results in a generally uniform rise the film. This means that the surfaces of the expanded film which eventually contact the walls of mold are essentially uniform in thickness resulting in a molded product of exceptional uniformity both in density but also in surface skin thickness at the edges and surfaces .

However, with packing of the solid, insoluble particles having an aspect ratio of greater that 1, in

the film or layer, expansion is altered. With sufficient of the particles in the film or layer, the m si tu expandable particles are faced with surfaces in the film or layer that resist expansion. The resistance to expansion is believed to occur because as the thermoplastic particles are heated and the vapors in the particles start to expand or the chemical blowing agent is decomposed leading to blowing of the film about the particles, thermoplastic particle surfaces or thermosetting resin adjacent to the expanding cell make contact with the solid, insoluble particles. Though the expansion is isometric at the point in contact, the expansion is restrained in the direction of the length of the particle because of the greater solid surface area and mass that the expansion has to transgress. As a result, expansion is more favored in a direction lateral of the solid particle' s surface direction, herein called the particle's surface longitude. With this occurring hundreds to thousands of times in the layer or film, expansion becomes inhibited in favor of the direction of orientation of the particle surface latitude or the direction lateral of the particle's surface direction. By shifting the latitude of the particles in the film or layer, one may control the orientation of expansion of the film or layer.

It has been determined that the particles' lengtr snould be limited in size m order to achieve orientation cf expansion of the layer or film. A continuous filament reinforcement structure, sucn as a continuous filament tow, or a woven or knitted fabric (wherein the fibers are continuous filament or twisted staple finer yarn) wnereir the fiorous matter is stable (and hence, immovable! will not proviαe tne necessary resistance to expansion that controls the orientation of expansion of the film or

layer as defined herein with respect to the invention. The expandable film or layer formulation residing between such continuous filaments or spun yarn has no confronting surface that impedes the expansion lateral of the orientation of the filamentary or yarn materials. However, in the case of cut fibers having a finite length such as 1" (2.54 cm.), the fiber presents a coiled or tangled end to the expanding microcell, and this larger mass of surface resists expansion in the longitudinal direction of the fiber. Consequently, shorter particulate matter possessing an aspect ratio greater than 1 resist expansion into the particle, thereby causing expansion to explode laterally of the orientatior of the particles . The film of the invention can be made in a number of ways and with a variety of resin systems to achieve the advantages herein set forth. The formulation of the film will be dictated by the specific end-use application of the film and the resultant molded or adhesive foam, as well as the method employed m making the film. Tnerefore, it is not intended that this description should be limited to any specific application and to any specific formulation and process of manufacture.

The thermosetting matrix resin suitable for use in the invention comprise those typically used in the manufacture of Syncore® syntactic foam. For example, epoxies curing at 350°F. (177°C.) and 250°F. (121°C.) are tne most common matrix resins, but matrices o: Dismaleimide (BMI) , phenolic, polyester, PMR-15 an acetylene terminated resins that have been used to produce SynCoreC products, are usable in the practice of the invention. however, the invention includes as wel-, other thermosetting resins; indeed, the mventior includes the familv cf thermosetting resins. Fcr

example, thermosetting resins from acrylics, polyurethanes, free-radically induced thermosetting resin, and the like, may also be used n the practice of the invention. As a result of such considerable choices in thermosetting resins, the thin m situ-expandable films of the invention are tailorable to making syntactic foams for a wide variety of applications.

Preferably, the invention embraces the use of thermosetting resins that find use in adhesive applications thereby providing the desired tackiness to the film. Such allows the thin film to be applied conveniently to any substrate and by virtue of the drapability of the film, have the film cling to the substrate throughout processing and cure, and configure to the substrate.

In one embodiment, as noted, the thin film is non- pourable and tacky. This condition can be achieved in a number of ways. Many thermosetting resins are solids at about 23°C. and many of them are liquids at this temperature. Both kinds of resins can be made non- pourable and tacky. For example, a resin which is solid and a resin which is liquid can be combined to form a mixed resin system that is non-pourable and tacky. In addition, a solid or liquid thermosetting resin can have incorporated m it a variety of diverse materials which will render the resin non-pourable at conventional handling temperature conditions and non-pourable ana tacKy at room temperature (about 15-37°C) . Conventional handling temperatures are defined as a temperature of oetween about -20°C. to about 43°C. ²

* This ranσe reflects the fact that material handling can reσuire lov te Dera _t ure storage to precluαe premature reaction of the tnermose ting resin system and relatively high temperatures Decause tne f lm may t>e useα on a hot factory floor.

Though the in situ-expandable thermoplastic particles or the solid chemical blowing agent will render a liquid thermosetting resin more viscous, they alone are not effective for making the film non-pourable. If the thermosetting resin is solid, it can be calendared into a film by melting the resin with heat under conditions that avoid condensation or addition of the resin to a thermoset condition (C-stage) . If the resin is a liquid, it can be blended with thixotropic agents, other solid resins and/or liquid or thermoplastic elastomeric modifiers to convert the resin from a liquid to a non- pourable and tacky material .

The typical thermosetting resin is an A-stage resin. In some cases, it may be desirable to utilize a B-stage resin but in the typical case, such is done in combination with an A-stage resin. Such B-stage resin will affect the viscosity of the resin formulation but they are not relied on to achieve the level of non- pourability for the most effective operation of the invention.

The same resins may be used to make the "layer" that contains the m situ-expandable particles and the insoluble particles. The layer in that case possesses all of the features herein described for making the non- pourable films, except the feature that creates non- pourability. The resin containing the in situ-expandable particles and the insoluble particles may be pourable, however, it is preferred that the resin loaded with the in situ-expandable particles be impregnated intc a fibrous mass that possesses the fibers in the desired orientation.

A preferred class of thermosetting resin in the practice of the invention are the epoxy resins. They are frequently based, inter alia, on one or more of diglycidyl ethers of bisphenol A (2,2-bιs(4- hydroxyphenyl)propane) or sym-tns(4- hydroxyphenyl)propane, tπs (4-hydroxyphenyl)methane, their polyepoxide condensation products, cycloaliphatic epoxides, epoxy-modifled novolacs (phenol-formaldehyde resins) and the epoxides derived from the reaction of epichlorohydrin with aniline, o-, m- or p-aminophenol, and methylene diamline.

The epoxy resins suitable in the practice of the invention include the various established thermosetting epoxy resins conventionally employed in making prepregs, especially carbon and graphite fiber reinforced prepregs. It is desirable that the epoxy resin be a low or lower viscosity version to facilitate film formation. Illustrations of suitable epoxy resins include, e.g., one or more of diglycidyl ethers of bisphenol A (2,2-bιs(4- hyαroxyphenyl) propane) , such a those of the following formula:

or sym-tris (4-hyαroxypnenyl)propane or trιs(-*- hydroxyphenyl)metnane, their polyepoxide condensation products, cycloaliohatic epoxides, epoxy-mod_flea novolacs (phenol-formaldehyde resins) of the formula:

wherein n is 0-1.8, preferably 0.1-0.5.

Other epoxy resins may be combined with the above epoxy resins or used alone. They include, e.g., 3,4- epoxy cyclohexyl methyl-3, -epoxy cyclohexane carboxylate, vinyl cyclohexene dioxide, 2-(3,4-epoxy cyclohexyl -5,5-spιro - 3,4-epoxy) cyclohexane - meta - dioxane, bis (3,4-epoxy cyclohexyl) adipate, and the like.

The epoxy resins of the invention are combined with nardeners which cure the resin to a thermoset condition. The preferred hardeners are amme compounds, ranging from αicyandiamide, to ureas, to aliphatic and aromatic amines. A preferred class of. hardeners are the aromatic amines encompassed by the formula:

Q is one or more of a divalent group such as -S0 ₂ -, -0-, - RR'C-, -NH-, -CO-, -CONH-, -OCONH-, and the like, R ana R' may each independently be one or more of hydrogen, pnenyl, alkyl of 1 to about 4 carbon atoms, alkenyi of 2 to about 4 caroon atoms, fluorine, cycloalkyl cf 3 tc aoout 8 carbon atoms, and the like, x_ may be 0 cr 1, _^ _ may be 0 or 1 and is 1 when > is 1, and z_ may be 0 or a positive integer, typically not greater than about 5.

34

Preferred hardeners are diamines of the formula:

Another preferred class of hardeners are the aliphatic amines such as the alkyleneamines . Illustrative of suitable alkyleneamines are the following :

Monoethanolamine Ethyl enediamine

N- ( 2-amιnoethyl ) ethanola ine Diethylenetria ine

Piperazme N- (2-aminoethyl ) pιpera2ine

Triethyienetetramine Tetraethylenepentamine

Pentaethylenehexa ine Diammoethylpiperazine

Piperazinoethylethylenediamme 4 -Amιnoethyltriethylenetetramme

Tetraethylenepentamine Ammoethylpiperazmoethyletnylened: amme

Piperazmoethyldiethylenetriamine and the like .

Another class of hardeners , but which can also be used as extender of the epoxy resin , are the higher molecular weight poly (oxyalkylene ) - polyamines such as those of the f ollowinα formulas :

CH, CH-

H-NCHCH.(OCH-CH) NH ₂ where y is 2-40

CH. CH- CH.

H.NCHCH-fOCH-CH), (OCH-CH ₂ ) _b (OCH-CH) _c NH- where a+c is about 2.5 and b

CH, is 8-45

CH-(OCH ₂ CH) -NH- CH ₃ CH-CCH-(OCH-CH) _y NH ₂ CH ₂ (OCH.CH)-N 'H"2 where x, y and z range from

CH, about 2-40

CH, ^CH - CH,

H ₂ NCHCH ₂ (OCH ₂ CH) _m NH(OCH ₂ CH) _t NH ₂ where m+t is about 82-86.

The hardener may be a monoamine such as aniline, para-aminophenol, and alkylated versions of them.

A further class of desirable hardeners are the reaction products of dialkylamines, such as dimethylamine, diethylamine, methylethylamine, di-n- propylamine, and the like, with a variety of mono and diisocyanates to form mono and diureas . Any of the polyisocyanates listed below may be so reacted for use as a hardener. Specific illustration of useful hardeners are those encompassed by the following formulas and descriptions:

ere R is a monovalen ic group; R' is alkyl' alkoxy, and the like is methylene, opylidene, ethylidene, covalent bond; and a i

Preferred urea hardeners are those that are the reaction products of dimethylamme with mixtures of 80% 2,4-tolylene dusocyanate and 20% 2,6-tolylene 5 dusocyanate, polymeric isocyanate, p-chlorophenyl isocyanate, 3, 4-dιchlorophenylιsocyanate or phenyl isocyanate .

The amount of hardener employed is usually stoichiometrically equivalent on the basis of one amme 0 group per epoxy group in the resin. If the epoxide is a triepoxide and the hardener is a diamine, then the molar ratio of hardener to epoxide would typically be about 2.5 3 or 0.83. A typical formulation would have a weight ratio of epoxy resin to hardener of about 3/2 to about 5 4/1. Where any of the hardeners serve primarily as extenders of the epoxide resin, then the amount of the hardener in the typical case will be less than that generally employed for hardening the epoxide. Mixtures the above hardeners and with other hardeners are withir C the contemplation of this invention.

Other reactive resin systems include the various thermosetting or thermosettable resins include tne bismaleimide (BMI), phenolic, polyester (especially tne unsaturated polyester resins typically usec m SKC

production) , PMR-15 polyimide and acetylene terminated resins are also suitable.

The urethane systems represent a typical non- engineering polymer for applications demanding less ^p erformance than, for example, the epoxy resin systems. They typically comprise the reaction of a polyisocyanate, a polyol, alone or with another active hydrogen compound, typically in the presence of a catalyst, such as an amine catalyst. However, in the practice of this invention, the polyurethane is a mixture of a blocked polyisocyanate, such as the reaction product of a mono-ol or monohydroxy phenolic compound with a polyisocyanate that is an organic polyisocyanate. This includes an organic compounds that contain at least two isocyanato groups and include the hydrocarbon diisocyanates (e.g., the alkylene diisocyanates and the arylene diisocyanates), as well as known triisocyanates and polymethylene poly (phenylene isocyanates) .

The blocked isocyanates are compounds of the formula:

is a monovalent anic group; is alkyl, halo, oxy, and the ιi e; a is 0-4

Illustrative polyisocyanates for use in making the blocked isocyanates are: methyiene bis (4-cyclohexyl 1,2-diιsocyanatoethane isocyanate)

I, 3-dιιsocvanatoorooane 1, 2-diisocyanatopropane

and mixtures thereof.

The preferred polyisocyanates are mixture of 80% 2,4- tolylenediisocyanate and 20% 2, 6-tolylenedιιsocyanate ana polymeric isocyanate. Tne blocked isocyanates comprise any of the above polyisocyanates reacted • with a monofunctional hydroxy containing compound. The resultant blocked polyisocyanate is unreactive towarαε

hydroxyl compounds at room temperature but, at elevated temperatures, will function as an isocyanate to crosslink the hydroxyl compounds to form the thermoset resin. For example, an adduct of tolylene diisocyanate and trimethylolpropane is first prepared in solution, followed by the addition of phenol to block the remaining isocyanate groups. Illustrative of such a blocked polyisocyanate is a phenol blocked toluene diisocyanate in cellosolve acetate sold by Mobay Chemical Co., as Mondur S. Such blocked isocyanates, when mixed with the polyols, provide a thermosetting polyurethane matrix resin that can form a tacky thin in situ-expandable film that is storable and curable on demand, in accordance with the invention. The polyols used in forming the polyurethane may be an organic diol, triol, tetraol, pentaol, and the like. Illustrative are the following compounds: ethylene glycol, diethylene glycol, triethylene glycol, tetraethylene glycol, 1, 2-propylene glycol, di-1,2- propylene glycol, tri-1, 2-propylene glycol, tetra-1,2- propylene glycol, 1, -butanediol, 1, 3-propanediol, and the like; or formed from by the alkoxylation of a starter polyol, such as the class of polyols characterized; or formed from reaction of the above diols, triols, etc., with caprolactone. The resulting ester polyols ("Tone's") are widely used in reactions with isocyanate. Desirable alkoxylated polyols are alkylene oxide adducts of a hydroxylated alcohols of the formula:

Z(OH) _> ι and preferably a "starter" diol, triol, tetraol and higher hydroxylated alcohols, of the formula:

Z (OH! ≥2-€

wherein Z is a polyvalent organic moiety, the free valence of which is 2-6 or greater, or an average value equal thereto, as the case may be.

Illustrative of suitable compounds embraced by the "starter" Z(OH)≥ ₂ -6 alcohol are the following: ethylene glycol, diethylene glycol, 1, 2-propylene glycol, polyethylene glycol, polypropylene glycol, glycerine, pentaerythritol, sorbitol, diether of sorbitol, annitol, diether of mannitol, arabitol, diether or arabitol, sucrose, mixtures thereof, and the like.

The starter Z(OK)≥ ₂ -6 is first reacted with 1,2-alkylene oxiαe m an amount and under conditions sufficient to convert its hydroxyl groups to hydroxyalkyl groups. The amount of 1,2-alkylene oxide reacted is sufficient to achieve the ultimate molecular weight of the alkoxylated polyol adduct . The molecular weight of the alkoxylated polyol adduct should be relatively high, preferably above about 4000 (number average) and, more preferably, above about 5000. The minimum molecular weight of the alkoxylated polyol adduct may be about 2000. The preferred 1,2-alkylene oxides are lower 1,2-alkylene cxiαes, such as ethylene oxide, 1, 2-propylene oxide, 1,2- butylene oxide, and the like. The resulting polyol may oe hydroxyethyl capped by reaction with 1,2-ethylene oxide to provide assurance of primary hydroxyl content in the polyol especially if the alkoxylated polyol adduct is subsequently coupled, not polymerized, with an organic polyisocyanate. Such alkoxylation reactions, with consequent adduct formation, is well known in the art. Adduct reactions may be base or acid catalyzed, with base catalyzation preferred.

The organic polyol may be a polyester polyol, such as a polyester of a dicarooxylic acid, acid haliαe or

anhydride and a polyol, such as those characterized above. In this case, it is desirable to allow the polymer to be hydroxyl terminated, and conventional procedures in the art are useful for this purpose. A polyol is also employed to produce the polyester. Such polyols include ethylene glycol, diethylene glycol, propylene glycol, dipropylene glycol, butylene glycols, neopentyl glycol, glycerol and 1, 1, 1-trιmethylolpropane .

Polyester resins usable as the thermosetting matrix resin, are typically reaction products of a dicarboxylic acid, acid halide or anhydride, with a polyhydric alcohol. The dicarboxylic acids or anhydrides that are employed to produce the polyester, either singly or in combination, include those that contain olefinic unsaturation, preferably wherein the olefinic unsaturation is alpha, beta- to at least one of the carooxylic acid groups, saturated aliphatic, heteroaliphatic and aromatic polycarboxylic acids, and the like. Such acids include maleic acid or anhydride, fumaric acid, methyl maleic acid, and itaconic acid (maleic acid or anhydride and fumaric acid are the most widely used commercially) , saturated and/or aromatic dicarboxylic acids or anhydrides such as phthalic acid or anhydride, terephthalic acid, hexahydrophthalic acid or anhydride, adipic acid, isophthalic acid, and "dimer" acid (i.e., dimenzed fatty acids) . They may be cureα b-j providing a polymerization initiator and low viscosity crosslinking monomers in the formulation. Where tne resin is a unsaturated polyester or vinyl ester, it is preferred that the monomers contain ethylenic unsaturation such that the monomer is copolymer-zable with the polyester and terminally unsaturated vinyl ester resins. Useful monomers include monostyrene, alky_ acrylates and methacrylates such as Cι- _:2 alkyl acrylates

and methacrylates, substituted styrenes such as α-methyl styrene, α-chlorostyrene, 4-methylstyrene, and the like, divmylbenzene, acrylonitrile, methacrylonitrile, and the like. Styrene is the preferred monomer in commercial practice today, although others can be used. Suitable polymerization initiators include t-butyl hydroperoxide, t-butyl perbenzoate, benzoyl peroxide, cumene hydroperoxide, methyl ethyl ketone peroxide, and others known to the art. The polymerization initiator is employed in a catalytically effective amount, such as from about 0.3 to about 2 to 3 weight percent, based on tne weight of polyester and the crosslinking monomer.

When desired, a thickening agent can also be employed the polyester thermosetting compositions. Such materials are known in the art, and include the oxides and hydroxides of the metals of Group I, II and III of tne Periodic Table . Illustrative examples of thickening aαents include magnesium oxide, calcium oxide, calcium n-ydroxide, zinc oxide, barium oxide, magnesium hydroxide and the like, including mixtures of the same. Thickening agents are normally employed in proportions of from about 0.1 to about 6 weight percent, based upon weight of the polyester resin and crosslinking monomer.

Particularly desirable materials for rendering the tnermosett g resin non-pourable are thixotropic agents and/or elastomer-type polymers that provide discrete elastomer phases (second phases) in the thermosetting resin matrix. Certain of these material may reduce, tc some finite degree, tne crosslinking density of the thermoset resin (C-stage) . Many of these materials introduce very favorable properties to the resulting thermoset resin. For example, a particularly desirable material for this purpose, is an elastomeπc polymer

containing soft and hard segments, the hard segments acting like or forming on processing, crosslinking of the elastomeric type. Some of these elastomenc types contain functional end groups which allow it to couple with complementary functional monomers or polymers to form the desired elastomer m si tu of the thermosetting resin and render it non-pourable and tacky, while toughening the cured resin. As a class, these elastomeric polymers act or are crosslmked yet are thermoprocessable, which when discretely provided in the matrix resin renders the resin non-pourable and tacky, and also toughens it.

One class of suitable elastomer-type thermoplastic ABS (acrylonιtrιle-1, -butadιene-styrene) block copolymers that are typically used as modifiers of other resin systems. They are characterized as having a wide range of properties though the preferred systems of the invention utilize copolymers that are high rubber types that, when compared to other copolymers of this type, have a relatively low tensile strength, low tensile modulus, higher impact resistance, low hardness and heat deflection temperature. Another elastomer that is found desirable are the carboxyl and amme terminated liquid butadiene acrylonitrile copolymers. Such copolymers may contain pendant carboxyl groups in the interior of the polymer structure through the inclusion of methacrylic or acrylic acid in the polymerization or through the hydrolysis of some of the pendant nitrile units. Such polymers react with the epoxy resin and as a result, the epoxy forms tne hard segment generating the elastomer properties .

Another class of block thermoplastic elastomers are Kraton™, available from Shell Chemical Company. These thermoplastic rubber polymers possess usable

thermoplastic properties. They can be softened and they flow under heat and pressure. They then recover their structures on cooling. The chemical make-up are of three discrete blocks of the linear or A-B-A type. They are available as styrene-butadiene-styrene (S-B-S) block copolymers, styrene-isoprene-styrene (S-B-S) block copolymers and styrene-ethylene/butylene-styrene (S-EB-S) block copolymers. They are characterized by styrene polymer endblocks and an elastomeric midblock. After processing, the polystyrene endblocks physically crosslink, locking the rubber network in place. This physical crosslinking is reversible on heating.

Another series of the Kraton™ thermoplastic rubbers are the diblock polymers in which one block is a hard thermoplastic and the other is a saturated soft elastomer. Illustrative of this series is Kraton™ G 1701, a diblock polymer of a hard polystyrene block and a saturated, soft poly (ethylene-propylene) block.

Other rubbers or elastomers include: (a) homopolymers or copolymers of conjugated dienes having a weight average molecular weight of 30,000 to 400,000 or higher as oescnoed m U.S. Pat. No. 4,020,036, in which tne conjugated dienes contain from 4-12 carbon atoms per molecule such as 1, 3-butadιene, isoprene, and the like; (b) epihalohydrm homopolymers, a copolymer of two or more epihalohydrm monomer, or a copolymer of ar epmalohyαrin monomer (s) witn an oxide monomer (s) having a numoεr average molecular weight (M _n ) which varies from aocut 800 to about 50,000, as described in U.S. Pat. No. 4,101,604; (d chloroprene polymers including homopolymers of chloroprene ana copolymers of chloroprene with sulfur and/or with at least one copolymeπzable orαan c monomer wnere chloroprene constitutes at least

50 weight percent of the organic monomer make-up of the copolymer as described in U.S. Pat. No. 4,161,471; (d) hydrocarbon polymers including ethylene/propylene dipolymers and copolymers of ethylene/propylene and at least one noncon ugated diene, such as ethylene/propylene/hexadiene/norbornadiene, as described U.S. Pat. No. 4,161,471; (e) conjugated diene butyl elastomers, such as copolymers consisting of from 85 to 99.5% by weight cf a C* -C-- isolefin combined with 15 to 0.5% by weight cf a conjugated multi-olefm having 4 to 14 carbon atoms, copolymers of lsobutylene and lsoprene where a major portion of the isoprene units combined therein have conjugated diene unsaturation as described in U.S. Pat. No. 4,160,759. Specific illustrations of suitable elastomeric polymers are the following:

1. hycar™ CTBN liquid reactive rubbers, carboxyl terminated butadiene-acrylonitrile copolymers sold by B. F. Goodrich. 2. Hycar™ CTBNX, similar to CTBN except that they contain internal pendant carboxyl groups, also supplieα oy E. F. Gooαricn.

3. Hycar™ ATBN, amine terminated butadiene- acrylonitrile copolymers sold by B. F. Goodrich. 4. K 1102-28:72 styrene:butadιene linear SBS polymer, available from Shell Chemical Company under the registered trademark "Kraton" 1102.

5. KDX 1118-30:70 styrene:butadiene copolymer containing 20% SES triblock and 80% SB diblock, available from Shell Cne ical Company under the registered trademark "Kratcr" DX 1118.

6. KG 1657-14:86 stryene:ethylene-butylene : styrene copolymer available from Shell Chemical Company under the registered trademark "Kraton" G1657.

7. S 840 A-Stereospeciflc 43:57 styrene-butadiene SB rubber available from Firestone Synthetic Rubber & Latex

Company under the registered trademark "Stereon" 840A.

8. SBR 1006-random 23.5:76.5 styrene:butadιene SB block copolymer rubber available from Goodrich Chemical Company under the registered trademark "Ameripol" 1006. 9. SBR 1502-Random 23.5:77.5 styrene :butadiene rubber available from Hules Mexicanos, or from Goodrich Rubber Company as "Ameripol" 1502.

10. Blendex™ modifier resins (e.g., 305, 310, 311, 336, 338 and 405) - ABS polymers sold by General Electric. Different varieties are available and their suitability depends on the properties sought.

Illustrative of thixotropic agents that can render a thermosettable resin non-pourable are high surface area fumed silicas and organosilyl blocked fumed silicas, and the like.

The thermoplastic polymer used in forming the in situ- expandable thermoplastic particles are readily prepared from a wide variety of materials. A number of patents refer to their manufacture. For example, U.S. Patent No. 3,615,972 describes their preparation by polymerizing the monomer of an aqueous dispersion of (1) organic monomeric materials suitable for polymerization to a thermoplastic resinous material having the desired physical properties,

(2) a liquid blowing or raising agent which exerts a little solvent action on the resulting polymer, and a quantity in excess of that wnicn is soluble ιr the polymer, ana (3 a αispersion stabilizing material whιc

is utilized to maintain the dispersion. The resulting solid spherical particles have a quantity of the liquid- blowing agent encapsulated in them as a distinct and separate phase. The thermoplastic polymers are formed by the polymerization of one or more of a variety of different types of alkenyl monomers, such as those of the formula:

R° CH ₂ =C-X

to form homopolymers or copolymers, such as random or ordered (including block) copolymers. In the above o formula, R may be hydrogen, alkyl, such as methyl, ethyl and the like, or halogen, such as chlorine, fluorine, bromine or iodine, and X may be an aromatic containing moiety bonded via an aromatic carbon atom, a carbonyl oxy ester moiety, halogen, cyano, oxycarbonyl ester, carboxyl, and the like. Illustrative of these monomers are those in which X is aromatic containing, such as styrene, o-methylstyrene, m-methylstyrene, p- methylstyrene, ethylstyrene, α-vmyl-xylene, α- chlorostyrene, α-bromostyrene, vinylbenzylchloride, p- tert . -butylstyrene, and the like. Also illustrative of these monomers are those in which X is a carbonyl oxy ester moiety to form acrylate monomers alone or in combination with the alkenyl aromatic monomers may also oe utilized. Such acrylate-type monomers include methyl methacrylate, ethyl acrylate, propyl acrylate, butyl acrylate, butyl methacrylate, propyl methacrylate, butyl methacrylate, lauryl acrylate, 2 - ethyl hexyl acrylate, c ethyl methacrylate, and the like. X and P may ce a halogen, such as chlorine, fluorine, bromine and iodine, tnereby to encompass the formation of copolymers of vinyl

chloride and v ylidene chloride, acrylonitrile with vinyl chloride, vinyl bromide, and similar halogenated vinyl compounds. X may be a cyano group and this includes polymers of acrylonitrile and methacrylonitrile. When X is an oxycarbonyl esters, such as the vinyl esters, such as, vinyl acetate, vinyl butyrate, vinyl stearate, vinyl laurate, vinyl myristate, vinyl propionate, and the like, are suitable polymeric components. One may also employ for specific purposes ethylenically unsaturateα copolymerizable acids such as acrylic acid, methacrylic aciα, itaconic acid, citraconic acid, maleic acid, fumaric acid, vmylbenzoic acid, and the like.

The thermoplastic polymers may also include copolymers (of the random or ordered varieties, especially blocked copolymers) of the monomers described above with a variety of hydrocarbon monomers, such as propylene, putene, and one or more dienes, such as:

• straight chain acyclic dienes such as: 1, -hexadιene, 1, 6-octadιene, and the like;

• branched chain acyclic dienes such as: 5-methyl-l, - nexadiene, ^Λ 13, 7-dιmethyl-l, 6-octadιene, 3, 7-dιmethyl- 1, 7-octadιene and the mixed isomers of dihydro- myrcene, dihydroocmene, and the like; • single ring alicyclic dienes such as: 1,4- cyclohexadiene, 1, 5-cyclooctadιene, 1,5- cyclododecaαiene, and the like;

• multi-ring alicyclic fuseα and bridged ring dienes such as: tetrahydromdene, methyltetrahydromdene, dicyclopentaαiene, bicyclo- (2, 2, 1) -hepta-2, 5-dιene, alkeny _^ , alkylidene, cycloaltenyl and cycloalkyliαene norbornenes such as 5-methylene-2-noroornene (MNBj , 5- etnviιαene-2-norbornene (ENB , 5-propyl-2-noroornen ,

5-isopropylidene-2-norbornene, 5- (4-cyclopentenyl) -2- norbornene, 5-cyclohexylidene-2-norbornene, and the like.

The thermoplastic polymer used in forming the in si tu -expandable thermoplastic particles may also be made from condensation type polymers, such as nylon-6,6; nylcn-6; nylon-4,6; polyester from polyethylene terephthalate;

Kevlar™ polyaramide; polycarbonates (viz., poly (2,2-bis

(1.4-oxyphenyl) propane carbonate)) ; polyarylates (viz., poly (2, 2-bis (1.4-oxyphenyl) propane terephthalate) ; polyimides; polyetherimides, such as Ultem™ ³ ; polysulfones (see U.S. Patents No. 4,175,175 and

4,108,837), such as Udel™ and Radel™ A-400 ⁴ ; the polyethersulfones (see U.S. Patents Nos . 4,008,203, 4,175,175 and 4,108,837), such as Victrex™ ⁵ ; polyarylsulfones; polyarylamideimides, such as Torlon™ ⁶ ; and the like.

A wide variety of blowing or raising agents may be incorporated within the polymerization system. They can be volatile fluid-forming agents such as aliphatic hydrocarbons including ethane, ethylene, propane, propylene, butene, isobutylene, neopentane, acetylene, hexane, heptane, or mixtures of one or more such aliphatic hydrocarbons having a molecular weight of a least 26 and a boiling point below the range of the

³ Available from General Electric Company, Plastics Business Group, Pittsfield, MA.

⁴ Manufactured by Amoco Performance Products Inc., Ridgefield, CT .

⁵ Available from ICI Advanced Materials, Wilmington, DE 19897 ^b Available from Amoco Chemical Company, Chicago, 111.

softening point of the resinous material when saturated with the particular blowing agent utilized.

Other suitable fluid-forming agents are the chlorofluorocarbons such as those described in U.S. 3,615,972 (column 4, lines 21-30) and tetraalkyl silanes such as tetramethyl silane, trimethylethyl silane, trimethylisopropyl silane and trimethyl-n-propyl silane. As pointed out in this patent, the boiling point of such foaming agents at atmospheric pressure should be about the same temperature range or lower than the softening point of the resinous material employed.

Blowing agents such as the Freons®, such as trichlorofluoromethane, hydrocarbons such as n-pentane, l-pentane, neo-pentane, butane, l-butane, azodicarbonamide are commonly suggested blowing agents found in these types of m situ-expandable particles. Typically, the unexpanded particles contain from about 3 to about 40 weight % blowing agent.

As pointed out in U.S. Patent No. 4,397,799, patented August 9, 1983, the particle size of the unexpanded particles, as well as the expanded microspheres can vary widely. Particle sizes for the unexpanded particles can range, for example, from about 1 μm to about 1 mm, preferably from about 2 μm to about 0.5 mm. One version of m s u-expandable particles are sold under the name

Expancel®, by Nobel Industries Sweden, Sundsvall, Sweder

(U.S. address: Mametta, GA 30062) . They range IΓ unexpanded particle size from about 5 μm to aoout 50 μ .

The particle diameters expand 2 to 5 times. Preferably, the m situ-expandable particles used have a mixed particle size of wide spread to achieve the best packing, on expansion, the syntactic molded foam. A particularly preferred in situ-expandable particle is

Expancel® 091 DU, which is believed to be a terpolymer of vinylidene chloride, acrylonitrile and methacrylonitrile containing 10-18 weight % isopentane, and possesses the following properties: average unexpanded particle size of about 12 μm with a spread of about 5-50 μm; true density (expanded in water at 100°C, kg/m ³ ) , <20 TMA - T (start) °C, 125-130; T(max) °C, -183; TMA- density, kg/m ³ , <17.

The chemical blowing agent particles (with a particle size ranging from, about 1 μm to about 1 mm, preferably from about 2 μm to about 0.5 mm) that can be incorporated are inorganic and organic solid compositions that typically decompose at a particular temperature to generate a volatile (gas) component that cause microcell formation in the thermosetting matrix resin. Typical inorganic blowing agents include the ammonium carbonates and bicarbonates, alkali metal carbonates and bicarbonates such as lithium carbonate, sodium carbonate, potassium carbonate, rubidium carbonate, cesium carbonate, lithium bicarbonate, sodium bicarbonate, potassium bicarbonate, rubidium bicarbonate, cesium bicarbonate, mixture of the carbonates and bicarbonates as well as mixtures of the alkali metal form of the carbonates and bicarbonates. These carbonates anc bicarbonates can be made to decompose at lower temperatures by incorporating organic carboxylic acids and acid anhydrides blowing agent accelerators into the formulation. Suitable organic carboxylic acids and anhydrides are citric acid, acetic acid and anhydride, maleic anhydride, There are a variety of chemical blowing agents sold under the name Celogen™ (Naugatuck Chemical Division of U.S. Rubber Company (Uniroyal) ) that include toluene sulfonyl hydrazide, toluene sulfonyl

semicarbazide, 5-phenyl tetrazole, azodicarbonamide, and the like, that are excellent chemical blowing agents suitable for the purposes of the invention. The chemical blowing agents may be employed in the formulations of the invention in amounts ranging from about 0.1 to about 3 parts by weight, preferably from about 0.5 to 2.0 parts by weight, of the thermosetting resin formulation.

The particles with the aspect ratio (i.e., ^length j width greater than one with a longitudinal axis not greater than about one inch (2.54 cm.), as noted above, may be inorganic or organic. The aspect ratio is desirably a value greater than 2, preferably, a value greater than 5, and most preferably, a value greater than ten. The aspect ratio of the particle may range from >1 to about 5xl0 ⁶ , desirably, from about 2 to about lxlO ⁶ , preferably, from about 5 to about 5xl0 ⁵ , and most preferably, from about 10 to about 1x10 ^s .

The particles may have a fibrous to non-fibrous nature. For example, the particles may be platelet-like or rod-like or filament, fiber or fibrid-like or whiskers, each possessing the desired aspect ratio. It is preferred that a width of the particle not exceeα about of the thickness of the layer or film.

100

Preferably, a width of the particle should not exceed

about of the thickness of the layer or film. The

500 preferred particles are cylindrical, or cylinder-like, and the width of the particles with that shape snould not

1 1 exceed about , preferably not exceed about —— ^• , tne

100 500 thickness of the layer or film.

These expansion-orienting particles may be present in the layer or film in amounts sufficient to affect the expansion characteristics of the layer or film. No hard and fixed amount will establish a priori a predefined expansion orientation of the layer or film because the nature of the particle plays such an important role in expansion characteristics and orientation. The amount present should be sufficient to assure the desired degree of expansion and orientation. Thus the minimum amount of expansion-orienting particles should be an amount that alters the direction of expansion of the layer or film during the curing and expansion stage. That amount may range from as little as about 2 weight percent to as high as about 60 weight percent, preferably from about 5 weight percent to about 35 weight percent.

The solid expansion-orienting particles may be inorganic materials including natural mineral particulates such as asbestos, mica, quartz, calcium carbonate, and the like; metal fibers and whiskers, such as iron, steel, copper, aluminum, tungsten, boron and the like fibers and whiskers; siliceous fibers such as glass fiber; carbon fibers such as graphite and carbon fibers, and the like; boron nitride fibers; silicon carbide fibers; titanium carbon fibers; and the like. The solid, expansion-orienting particle may be organic baseα materials including thermosetting or thermoplastic solid, expansion-orienting particles such as pitch based fibrids and fibers, phenol-formaldehyde, melamine-formalαehyde and urea-formalαehyde resin fillers, fibrids and fibers, and a host of Known fiber materials that proviαe reinforcing as well as expansion properties to the film or layer.

Such fibers, in addition to controlling expansion, provide reinforcement and toughness properties to the

molded syntactic foam product. Fibers that may be used in the practice of the invention may be any organic fiber that has a melting temperature (T _m ) greater than the cure temperature of the matrix resin in making the expanded molded syntactic foam. Also usable in the practice of this invention are fibrous type of structures, having an length aspect ratio of length greater than diameter ( ) , diameter that are made of amorphous polymers. For example, certain polysulfone fibers having a high T _g may be employed. In such a case, the polymer's T _g should be greater than the cure temperature of the matrix resin. Suitable fibers may be made from any of the performance and engineering plastics. For example, the fibers may be made from nylon-6,6; nylon-6; nylon-4,6; polyester from polyethylene terephthalate; polypropylene; Kevlar® polyaramide; polycarbonates (viz., poly (2,2-bis (1.4- oxyphenyl) propane carbonate)); polyarylates (viz., poly

[2 , 2-bis ( 1. -oxyphenyl) propane terephthalate) ; polysulfides (see U. S. Patent No. 3,862,095) ; polyimides; polyetherimides, such as Ultem® polyetheretherketones , such as Victrex® PEEK ^ε and polyetherketone or polyetherketoneketone, such Stilan€ PEK or PEKK. ⁹ ; polysulfones (see U.S. Patents No. 4,175,175 and 4,108,837) , such as Udel® and Radel© A-40C ¹⁰ ; the polyethersulf ones (see U.S. Patents Nos .

4,006,203, 4,175,175 and 4,108,837), such as Victrex®

Available from General Electric Company, Plastics Business Group, Pittsfieid, MA.

Available from ICI Advanced Materials, Wilmington, DE 1989 ^"

Available from Rayche Corporation

Manufactured bv Amoco Performance Products Inc., Ridgefielc, CT

PES ¹¹ ; polyarylsulfones; polyarylamideimides, such as Torlon® ¹² ; and the like.

The preferred fibers are those made from the engineering plastics, such as the polyarylethers which include the polyetherimides, the polyetheretherketones, the polyetherketones, the polyetherketoneketones, the polysulfones, the polyethersulfones, the polyarylsulfones, the polyarylamideimides, and the like. Particularly preferred fibers are those made from polyetheretherketones, polyetherimides, polyarylamides, polyarylamideimides, polysulfones, polyethersulfones and polycarbonates .

The fibers are typically in the form of short cut fibers, i.e., staple fibers, ranging from about 2.5 millimeters to about 13 millimeters. Longer fibers may be used and when they are used, they typically concentrate at or near the syntactic foam's surfaces, as a result of migration during expansion. The diameter of the fibers may range considerably. Preferably, the fiber diameter ranges from about 20 μm to about 70 μm, preferably from about 30 μm to about 60 μm.

A typical resin formulation comprises the following:

11 Available from ICI Advanced Materials, Wilmington, DΞ 19897

12 Available from. Amoco Chemical Company, Chicago, 111.

Preferred Formulation Percent By Weig _h t Percent

By Weight

Bispnenol A epoxy 40 to 80 60 to 75 resin. A preferred resin comprises a mixture of (a) a solid resin and a liquid resin that yield a soft, non-pourable, tacky, resin; or (b) a mixture of liquid resins that yield a soft, non-pourable, tacr.y resin; or (c) a mixture of a liquid

Sispnenol A epoxy resi and low molecular weight novolac epoxy resm.

An elastomer toughening 0 to 12 3 to 9 agent .

A desirable toughening agent may be a camoxylated butadiene acrylonitrile copolymer elastomer; an ABS block copolymer elastomer; and SBS block copolymer elastomer.

Hydroxyl extender for 0 to 20 4 to 12 tne epoxy resin (s) .

Tne preferred extender is Disphenol A.

Amme curing agent. 4 to 12 5 to 10

Preferred amme curing agents include aliphatic amines, alkylene oxide amines, aromatic amines and aromatic ureas.

Diluent. 0 to 2 0

A variety of conventional ether, Ketone, acetate, and tne like diluent may be added to facilitate compatibility. They are typically removeα by evaporation once the film is formed.

Tnermo _D last c fibers 3 to 20 6 to 14

The invention can be carried out with a variety of thermosetting resin formulations, using coupling agents and curing aids, as well as particulates having an aspect ratio of greater than 1. There are many different types of formulations that one may wish to explore to obtain special properties in addition to orientation of expansion as set forth herein. For example, the following is an epoxy resin system for core splice applications as a non-pourable film adhesive:

Part A: W .

C.E.N.™ 438 (Dow Chemical Co. ) 84.93

Reaction product of methylene diphenyl αnsocyanate and Terathane® 2900 (a oolybutylene ether glycol of 2900 MW sold by DuPont) in Epon® 825 diluent, as described in copending application Serial No.

08/349,876, filed on even date herewith. 14.99

Colorant 0.08

100.00

Part B:

Epon® 826 29.25

MY0510™ (Ciba Geigy) 9.75 , ' -Diaminodiphenyl sulfone 48.80

PN23 (A]inomoto Co. Inc.) 12.20

100.00

System

Part A 39.46

TS-720 Cab-O-Sil (Cabot) 4.00

A-187 Epoxy silane coupling agent

Glass microspheres, K25 (3M) 8.0

Expancel 091 DU 12.08

1/8" glass fiber, Ave . filament diameter, 7.80 micrometers, 15.8; Nominal bulk density, g/m ³ , 0.17 (731ED, OCF Corp. )

Part B 28.34

Total 100.08 It can be made as follows: Preheat Part A to 71°C, then add it to a preheated pot at 71 ^C C. Add colorant, mix for 5 minutes, then add Cab-O-Sil TS-720, and mix for

5 additional minutes. Add the A-187, mix for 10 minutes, followed by addition of the K25 microspheres, with mixing for an additional 10 minutes. This is followed by the addition of the Expancel 091 DU, mix for 10 minutes, and followed by the addition of the glass fiber, with mixing for 10 minutes. Add Part B, then mix for 5 minutes; scrape down the vessel, mix for another 10 minutes with a full vacuum pulled on the mixer.

Another epoxy resin system, made according to the above procedure, is the following:

% by

Weight

Part A D.E.N.™ 438 {Dow Chemical Co.) 75.00

Reaction product of methylene diphenyl 15.00 dusocyanate and Terathane® 2900 (a polybutylene ether glycol of 2900 MW sold by DuPont) in Epon®

825 diluent, as described in copending application

Serial No. (Attorney's Docket No. HY028), filed on even date herewith.

Araldite® ECN™ 1280 (Ciba Geigy) 10.00

Part B MY722 ^m (Ciba-Geigy) 50.00

DDS

Bisphenol A imidazole condensate with phenolic novolac 21.67

Svstem

Part A 52.62

Colorant 0.10

Cab-O-Sil® (TS-720 from Cabot) 5.0C

A-IS ^"7 ™ epoxy silane,

0.4C

K25 ¹ * ^* * glass microsphere, from 3M 9.8C

Expancel® 091DU (Nobel Industries Sweden) 9. C.

1/8" glass fiber, Ave. filament diameter, micrometers, 15.8; Nominal bulk density, g/m ³ , 0.17 .8~ (731ED, CCF Corp. )

Part B

10C

The following formulation is a typical adhesive formulation that is suitable for making the in situ- expandable pourable mass layer form of the invention containing oriented fibers throughout.

Part A

% by

Weight

Araldite LY9703 Bisphenol F- 13.98 resin (Ciba-Geigy)

D.E.N.™ 438 (Dow Chemical Co.) 10.35

Blendex® 311, a ABS toughener. 11.20

Epon® 828 11.20

Hycar® CTBN1300X9 5.57

Triphenylphosphine* Ethyl Iodide 0.10

Dihydroxynapthalene 2.24

Phenyl Novolac (TACTIX® 485) 28.01

D.E.N.™ 438 (Dow Chemical Co.) 10.35

Amorphous Silica (Cab-O-Sil®- 7.00 720)

Part B

Epon® 828 (Shell Chemical) 57.93

Trihydroxy benzoic acid (Gallic 25.55 acid)

Dimethyldichlorophenyl urea 10.23

(Diuron®)

Uniroyal blowing agent (Celogen® 5.79

O.T. )

Epon® 828 blue (colorant) 0.50

System

Part A

Part B

Nylon fibers, 1/10" uncrimped (1.8 denier)

100.00 Another epoxy resin system, particularly suitable for non-pourable film adhesive applications, may contain the following :

Raw Materials

D.E.N . ^•m 43i (Dow Chemical Co.) D.E.N.*™ 438 (Dow Chemical Co.) ECN1280™ (Ciba Geigy) A-187 Epoxy silane coupling agent o -°\

IGD 101 Balloons, (Emerson & Cumings)

TS-720

ExDancel 091 DU

1/4" Glass fibers

(added to resin first)

Part B Mill M x of 38 9

Dicyan iamide 33% Epon® 828 50 %

Omini cure 24 (CVC Chemicals) 17 % Total 4096 'his formulation was compounded as follows:

The three resins were blended at 82.2°C. for 45 minutes in a 5 gallon Ross mixer at speed number 2. Added fioers, mixed for 1/2 hour at 82.2°C. Added silane and balloons, mix 1/2 hour at 82.2°C. Added Amorphous Silica at 76.7°C, mix 1/2 hour. Added Expancel® 091 D and mix 1/2 hour at 73.9°C. Added part B to part A at 68.3°C. Mixed for 15 minutes, scraped down twice. Filmed on pilot plant filmer in a single orientation at 50 mil.

The films were made as follows: produceα each formulation ana filmed process temperature was 82.2 ^C C. until ready to film. Calendar rolls of the filmer were set at 65.55 ^G C. and filming was to 50 mils. Each formulation was converted to a 2 sσ. ft. of film. Each

film was cut into 2" x 2" squares for expansion testing. Used two ply to get 100 mil thick uncured. The five samples were cured in an oven with a heat-up rate of 60 minutes to 121.1°C. and held for 1/2 hour. The specimens were allowed to cool and the measurements were taken. The formulations were repeated with the following components provided or deleted to make the following five samples, for the heat expansion tests.

Material

Weight Percent

Resin without particles

Glass microspheres

Curing agent

Expancel 091 DU

PEEK, 900 denier, 1/10" staple cut fibers (non- cnmped) .

Glass Flakes (1/64" glass flakes)

Nylon Fibers (1/10" nylon 6,6 fibers (non-crimped))

Measurements cf new surface area compared to initial surface area of 4 square inches and comparisons of expanded height to the original 100 mil thickness are set forth in the followinα table.

Percent surface area

Percent height expansion from original 100 mil

700% 850% 850% 600% 530^

Percent height expansion is greater than surface area _19Q „ _{50Q% 42Q% 37Q% 31 Q B<>} expansion

Heiqht/surface area 1.94 5.00 4.25 3.75 3.79

Specimens #2 and #5 show a surface expansion that was greater in the "x" direction than the "y" direction. Both averaging 20% greater expansion in the "x" direction. The expansion rate being greater perpendicular to the direction of the fibers in the film.

Expansion Ratios ::1 8.5:1 8.5:1 7.0:1 6 3.1

Horizontal expansion from original 4 sq. in. _{36Q% 17Q% 2 Q Q % 16Q% 14Ql}

The expansion of the pourable in si t u expandable layer can be controlled by the rate at which expansion and cure takes place. Tnrough control of the rate of temperature build up to reach cure temperature, one may materially control the expansion of a layer of the expanαaole material. In this way, one can tailor the expansion to the mold, merely by selection of the time perioα of expansion. For example, there was prepared 2" x 2" pieces of unidirectional coresplice cut from the above sneets that were doubleα to 100 mil thickness for

expansion testing. Three expansion protocols were followed.

Rate of temperature

Protocols increase Nature of expansion.

1. 3°F./min heat up to Expansion was 1.5

121.1°C. to 1 height expansion

2. 6°F./min heat up to Expansion was 2.5

121.1°C. to 1 height expansion

9 F./mm heat up to Expansion was 3.5 121.1°C. to 1 height expansion

1., 2., 3. a) No expansion noted in film direction. b) to 2" side expansion c) Expansion was opposite film direction

These resin formulations are made by conventional mixing of the components in standard mixing equipment for viscous compositions. Good results have been obtained using a Ross® Double Planetary Mixer, provided with vacuum construction and jacketing to control temperature and deaerate the mixture. Mixing is typically effected by blending the resin, unexpanded particles, elastomer components, extenders, diluents, curing agent and fibers or other particles with an aspect ratio greater than 1 (these being added last), and vacuum pumping to remove entrained air. The temperature chosen is variable depending on the viscosity of the formulation. It may be desirable to separately mix the resin and the curing agent. In such a case, the formulation may be divided up to mix the resin with some portion of the formulation to effect a well dispersed condition and do the same with

the curing agent, and then combine the well dispersed mixes with the particle with the aspect ratio greater than 1 component and the unexpanded particles, so as to mix them all under conditions avoiding premature reaction. Sucn procedures are well within the skill of the art.

Calendaring of the resin formulation into the thin films of the invention is a desirable way of effecting orientation of the particle component. This is illustrated in the drawings. As shown m Figure 1, which is an isometric-like schematic illustration of a calendaring line 1 for calendaring a nonreinforced film, thermosetting matrix resin formulation (containing unexpanded, m situ-expandable particles) feed 3 is fed to nip rolls 5. Nip rolls 5 are calendar rolls spaced apart to the desired thickness of the film 7. It is αesirable in the practice of the invention to avoid drawing action of film 7 after extrusion formation by rolls 5. Rolls 5 may vary m width, wider rolls generating more throughput and narrower rolls providing more control over film thickness from edge to edge. Because this invention is concerned with films of essentially uniform thickness from edge to edge, and front to back, it is desirable to use calendar rolls that are less than about 36 inches wide. A convenient width is about 12 to about 18 inches. Manufacture of films meeting the specifications of this invention are easier at those widths. Because the viscosity of feed 3 is net excessive, one may look at the calendaring operation as a filming operation, akin to roller coating. The distance between rolls 5 is maintained by a force balance (not shown) between the hydraulic pressure pushing on the roll and tne off-setting matrix fluid pressure acting in tne opposite αirection to the roll

Once film 7 is formed, it is frequently desirable to reduce the matrix resin viscosity in the film. Temperature reduction of film 7 reduces viscosity which reduces flow within the film and thus helps to preserve its dimensions. This may be accomplished by passing film 7 over one or more chilled rollers 9, 13 and 15. If used as chilled rollers, they are typically internally cooled via internal jacketing, to temperatures from about 0°C. to about 25°C, sufficiently low enough to prevent any sagging or flow of the resin matrix. The chill rollers, by cooling the film, increase the resin's elastic modulus so that resin flow is decreased and film dimensional stability is maintained. In the configuration of Figure 1, roller 9 may be utilized as a chilled roller, a guide roller for alignment purposes and/or a take-up roller, as desired. For handling convenience, release paper or plastic (viz., polyethylene film) layers 12 and 14 may be applied to the outside surfaces of film 7, from their corresponding core rolls, under or over rolls 13 and 15, as may be the case, to form a sandwiched construction. The so protected film 19, as a sandwiched construction, is rolled up onto core 17.

Figure 2 shows another calendaring line, 21, which comprises feed 23 containing expandable particles, calendar rolls 25, film 27, rollers 29, 33 and 35, core and film 32, corresponding to feed 3, calendar rolls 5, film 7, rollers 9, 13 and 15, core and film 12, respectively, of Figure 1. What is different in Figure 2 is the use of a scrim layer 41, comprised of an open woven, nonwoven or knitted scrim construction, that is guided by roller 43 to roller 35 to be pressed into contact with film 27 by way of passage under roller 35.

This sandwiched construction is collected as roll 39 on core 37.

Figure 3 offers another calendaring line, 51, comprising feed 53, calendar rolls 55, film 57, rollers 59, 63 and 65, core and film 62, corresponding to feed 3, calendar rolls 5, film 7, rollers 9, 13 and 15, core and film 12, respectively, of Figure 1 and scrim layer 71, comprised of an open woven, nonwoven or knitted scrim construction, that is guided by roller 43 to roller 35 to be pressed into contact with film 27 by way of passage under roller 35. In line 51, the difference is the inclusion of an additional chiller roller 58 to control the viscosity of film 57, and a second film line, in order to form a two-layer film composite structure. The second film line comprises matrix feed 75, with unexpanded particles, that is formed into film 79 by calendar rolls 77, passed over chilled roller 82, guided and further cooled by guide and chilled roller 81. It is then merged into contact with scrim layer 71, film layer 61, and release layer 62 at roller 65, and the composite then passed over guide roller 83 to be taken up as composite film 69 on core 67.

The invention also contemplates the inclusion of one or more layers of a nonwoven fabric provided with a resir binder that is co-curable with the matrix resin. These added layers serve to enhance the impact and Duckling resistance of the composite structure. The nonwoven layer is typically provided as an outside layer, such as a substitute for release layer 62, to provide a support surface for the thin film.

The nonwoven structures may be formed from unspun or spun staple fibers having a length of from about 1/4 en tc aoout 3 inches by garnett g and crosslaymg,

airlaying on a rotating screen or on an endless tenter arrangement according to the procedure of U.S. 3,538,564, utilizing the apparatus of U.S. 3,345,231 and 3,345,232. The nonwoven structures may be resm impregnated by spraying the thermosetting resm as a solvent solution into the batting or scrim-like structures. Preferably, the nonwoven is first bonded with a low cost thermoplastic from a latex or water dispersion or with starch from an aqueous solution, dried to fix the fibers in the nonwoven structure, and then the nonwoven structure is impregnated with the thermosetting resm. The nonwoven can be supported by a scrim layer in much the same manner that the thin film is supported by one or more scrim layers 71. Figure 4 is a simpler and preferred method for making a scrim-supported composite. In line 101, scrim layer 103 is fed centered of the space between calendar rolls 107 and the thermosetting resm matrix feed 105 with the unexpanded particles is uniformly applied to both of the rolls so that there is an essentially equivalent amount on both sides of scrim film 103. At the same time, release layer 106, supplied from its core, is passed over one of the rolls 107 to form an outside release surface. This composite is passed over chilled and guide roller 111, to form sandwiched film 113 containing matrix resm with a thin inner scrim layer. The sandwiched film is passed over guide and chilled rollers 115 and 117 to oe collected as composite film 121 on core 119.

Figure 5 snows another way of forming a scrim composited film. In system 130, the scrim layer 103 is fed to the calendar rolls 107 with the matrix res feeα 105 shown to contain particles of in s tu-expanαable thermoplastic. In this system, outside release layers 121 and 133 are passed over calendar rolls 1C ^"7 to insure

that the film is formed between them. The resulting f lm can be cooled and collected as noted above.

In Figure 6, system 135 is the same as system 130 of Figure 5, except that the resin matrix 137 also contains short staple fiber with the thermal characteristics noted above. In the preferred case, the fiber length is about 1/4 inch. The mass is film-formed and the construction has the characteristics shown in Figure 7. In Figure 7, the film 139 comprises staple fibers 141 well dispersed in the non-pourable film. Also present in the film are the unexpanded, m situ-expandable thermoplastic particles . The fibers are caused to be oriented in the film more in the direction of flow of the matrix resm, consequently, more fibers will be found to be oriented parallel to the film's surfaces.

Figure 8 illustrates the coating impregnation of a web of staple fibers that have been carded or garnetted in the type of patterns shown m Figure 9. The web taken from a carder or garnetter or from a card crosslapper, with the fibers configured as shown in Figure 9, is rolled up into beam 161 and off loaded as layer 162 ano fed to coating impregnation system 160 through nip rolls 165 and 167. A supporting film 164, removed from roll 163, either a woven or nonwoven scrim and/or a release plastic film (e.g., polyethylene, polyester, nylon, poiyacetate, polypropylene, and the like), is fed to system 160, through nip rolls 165 and 167, mtc supporting contact with layer 162. The combination cf film 164 and layer 162, is passed under contacted o_ coating rollers 171 while being supported by rollers 1 ^" 2, to form composite layer 176. It is passed over guiαe roller 17 ^"7 and collected on roll 179. Coating rollers 171 are associated with ΞUPPIV coating rollers 169, wmc-

are fed the in situ-expandable layer for transfer to and impregnation of layer 162.

Figure 9 A shows the fiber alignment from a carder with the fibers uniformly aligned in the machine direction (the "T" direction) . Figure 9 B shows the machine direction (the "T" direction) and the fiber laydown deposited m a crosslapper such that the overlapped carded fibrous web are normal to each other. Figure 9 C shows the machine direction (the " " direction) and the crosslappmg of the carded or garnetted web at a more acute angle. Figure 9 D shows the same except that the carded or garnetted web is at an obtuse angle. In the case of web A, maximum expansion in the height and width directions are possible, with minimum expansion in the length direction. In the case of web B, as compared to web A, there is more expansion m the length direction and a similar expansion m the width direction, however, the maximum expansion will be in the height direction. In the case of C, the expansion the length direction will be greater that is the case witn B length direction, the same maximum expansion in the height direction and minimum expansion in the width direction. In the case with D, near maximum expansion will oe found in the length and width directions, and maximum expansion in the height direction. If the fibers are crimped, then the degree of expansion will be affected by the crimp. The greater the degree of crimp in the fiber, the lower the degree of expansion, regardless of direction. Molding of the films of the invention to produce molded syntactic foams is simple and straightforwarα . For example, as shown m Figures 10 and 11, a mold 142, shown as having an open end, is a split mold cf the

configuration shown. In this case, the mold is a slice of a cylinder. The mold defines the shape of the resulting syntactic foam. Mold 143 comprises arcuate top and bottom walls 145 and 149 and arcuate front and back walls 150 and 148, and sidewalls 146. The unexpanded film, as one or more layers 147 are cut to the shape and size of surface 149, and then laid onto that surface. The mold is then closed and heat is applied to the mold. The temperature to which the mold is heated is dependent upon several considerations, such as the temperature at which crosslinking of the thermosetting matrix res is initiated, the melting and/or second order transition temperature of the fiber, if present, the desired syntactic foam density if the blowing agent used in the particle overlaps the crosslinking temperature of the resm, and the like considerations. With the use of epoxy resins, the cure temperature is typically at 350°F. (17 ^"7 °C. ) or 250°F. (121°C. ) .

In the above noted processes, the release layers may be substituted for by other materials such as syntactic foams comprising rigid microballoons in a resm matrix comprises microballoons (microspheres) embedded in the uncured or partially cured matrix resm. In this case, the matrix resm may be any of the resins described above witn respect to the film of the invention. The most common of the microballoons are made of glass, but quartz, phenolic, carbon, thermoplastic and metal coateα microballoons are usable. A Syncore® is suitable for this purpose. The microballoons those syntactic foam films are synthetic hollov microspheres that comprise div dua- rouna spneres or bubbles having diameters whicn range from about 1 to about 500 microns, preferably about 1 tc

about 200 microns, with wall thicknesses of about 0.1 to about 20 microns. They typically possess densities ranging from about 0.1 to about 0.5 g./cc. The syntactic foam comprising the rigid microballoons in a resin matrix as a result have relatively low densities such as densities ranging from about 0.5 to about 0.7 g./cm. ³ . Glass is the most common microballoon material in these types of materials, but quartz, phenolic, carbon, thermoplastic and metal coated microballoons are suitably employable.

Such syntactic foam used in composites with the films of the invention may have a thickness ranging from about 0.007 to about 0.125 inch. Each such film would be uniform in thickness.