AU618573B2 - Multi-directional, light-weight, high-strength interlaced material and method of making the material - Google Patents

Description

PCT

OPI DATE 05/07/89 AOJP DATE 27/07/89 APPLN. ID 29225 89 PCT NUMBER PCT/US88/04328 INTERNATIONAL-APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (51) International Patent Classification 4 (11) International Publication Number: WO 89/ 05229 B32B 1/08, 5/22, B65H 81/00 Al (43) International Publication Date: 15 June 1989 (15.06.89) (21) International Application Number: PCT/US88/04328 (74 ent JBS Ha ey, et al.; Fleit, Jatobsdn, &~~Wice, e Jelj Building, 400 Sev- (22) International Filing Date: 8 December 1988 (08.12.88) enth Street, Washington, DC 20004-2201 (US).

(31) Priority Application Number: 130,854 (81) Designated States: AT (European patent), AU, BE (European patent), BR, CH (European patent), DE (Eu- (32) Priority Date: 9 December 1987 (09.12.87) ropean patent), FR (European patent), GB (European patent), IT (European patent), JP, LU (Euro- (33) Priority Country: US pean patent), NL (European patent), SE (European patent).

(71) Applicant: QUADRAX CORPORATION [US/US]; 300 High Point Avenue, Portsmouth, RI 02857 Published With international search report.

(72) Inventors: CRAVEN, Paul, T. 177 Elmdale Road, Before the expiration of the time limit for amending the North Scituate, RI 02857 FISHER, Richard, A. claims and to be republished in the event of the receipt 375 Lloyd Avenue, Apt. 1-E, Providence, RI 02906 of amendments.

MacGOWAN, Andrew, J. 15 East Street, Newport, RI 02840 (US).

(54)Title: MULTI-DIRECTIONAL, LIGHT-WEIGHT, HIGH-STRENGTH INTERLACED MATERIAL AND METHOD OF MAKING THE MATERIAL (57) Abstract Continuous flat unidirectional flat ribbons which have been precut from an impregnated fiber reinforced-matrix composite tape so as to have a substantially greater width than thickness, are interlaced in over-and-under relationship in 0 degree and 90 degree directions into the form of a continuous, multi-directional seamless tube The tube (28) may be cut into tubular sections which then are subjected to temporary heat and pressure so that the matrix (63) fuses the interlaced ribbons (24) to form an integral tube The elongated seamless tube (28) also may be cut into planar sections (42, 44 or 44') and used to form integral members (42p, 44p or 46) of planar or contoured construction. The integral members (32, 42p, 44p, or 46) may be formed of a single layer of the interlaced material, or of laminated construction from multiple layers of the interlaced material, with the ribbons (24) of each layer either extending parallel, at an angle other than 0/90 degrees, aligned, or offset, with respect to the ribbons (24) in the other layer(s). The formed members (32, 42p, 44p, 46) may have interlaced ribbons (24) of different types and/or contain different types of fibers (62) in different sections of the members, to provide the members with different structural characteristics.

I i I-~ I" I Multi-directional, light-weight, high-strength interlaced material and method of making the material o. This invention relates to a multi-directional, *e light-weight, high-strength interlaced material and j 20 method of making the material, and more particularly to a multi-directional, light-weight, high-strength interlaced 1 material suitable for use in or for structural members in military and commercial aerospace and aircraft applications, as well as other commercial applications.

'25 In the past, high-strength structural members in I military and commercial aerospace and aircraft applications, as well as other commercial applications, have normally been constructed of various types of metals. In recent years, there has been a trend toward the use of fibre-reinforced plastic composite materials for this purpose, because of their various advantages.

For example, when compared to traditional structural metals such as steel, aluminum and titanium, fibrereinforced plastic composites are lighter, easier to use, stronger, less expensive, less subject to corrosion and more impact resistant. By way of illustration, carbon fibre 911010,gjnspe.013,29225.spe, 1 i^ I WO 89/05229 PCT/US88/04328 2 material impregnated with th'ermoplastic may be five times stronger than steel and 55% lighter than aluminum.

In general, fiber-reinforced plastic composites are formed by arranging continuous, light-weight, high-strength fibers, such as carbon, glass, boron, various high strength metals or various synthetic fibers, such as aromatic polyamides, and lesser strength fibers such as rayon or nylon, in side-by-side bundles or tows with the fibers extending longitudinally in one direction. The side-by-side fiber bundles or tows then are impregnated with a plastic matrix under simultaneous heat and pressure. Subsequently, the resultant fiber-reinforced plastic composite may be arranged in layers in sheet, or unidirectional tape, form which, when subjected to heat and pressure, form a fiber-reinforced plastic composite laminate.

Fiber-reinforced plastic composites are available in fiber-reinforced thermoset matrices or fiber-reinforced thermoplastics matrices. Fiber-reinforced thermosets are epoxy, vinylester or polyester-based, harden through an irreversible catalytic process and require a long curing cycle as part of the process through which they are fabricated into finished parts. Prior to use, fiber-reinforced thermosets have delicate shelf-life properties and require refrigeration. When WO 89/05229 PCT/US88/04328 3 cured, fiber-thermosets are strong and light-weight, but often brittle.

Fiber-reinforced thermoplastics, on the other hand, are a newer form of composite which, compared to fiber-reinforced thermosets, have significantly higher toughness and impact resistance, are processed at and can tolerate higher temperatures and have improved moisture and chemical resistance. Fiber-reinforced thermoplastics do not require refrigeration, have an unlimited shelf life and require only a short heat/cool cycle for curing. Unlike fiber-reinforced thermosets, fiber-reinforced thermoplastics are not hardened through a catalytic process and therefore can be reheated and reformed without undue detrimental effect, although they do require higher temperatures than fiber-reinforced thermosets to process them into finished parts. Further, fiber-reinforced thermoplastics tend to be stiff and boardy, and therefore generally are unable to conform to highly contoured molds at room temperature.

Fiber-reinforced thermoset composite unidirectional tapes have been used extensively for high strength structural aerospace/aircraft applications because all fibers, and therefore all the structural attributes of the material, are aligned in one direction. (To date, however, the processing of these tapes into finished parts has been too expensive 1

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I WO 89/05229 PCT/US88/04328 for most commercial applications.) Unidirectional tapes are laid in successive laminated layers at predetermined angles, to obtain the desired structural properties in a finished format of greater dimensions than the individual tapes. An example of such laminated fabrication is shown in U.S. Patent No.

3,946,127, to J.R. Eisenmann et al. Normally, the unidirectional tapes are processed by hand; however, for some larger parts, complex automated tape laying machines, having a cost on the order of one to three million dollars, may be used, although such machines for processing fiber-reinforced thermoplastic composite unidirectional tapes are still in the development stages.

Fabrication of parts from fiber-reinforced thermoplastic composite unidirectional tapes has followed the labor-intensive processes developed for fiber-reinforced thermoset composite unidirectional tapes. Fiber-reinforced thermoset tapes, however, are more suitable for these hand processes because, unlike fiber-reinforced thermoplastic tapes, they can be fabricated so that they remain tacky until cured and thus can be more easily held in position, whereas hand lay-up of fiber-reinforced thermoplastic tapes requires that each tape be tacked, welded or stitched in position before laying the next tape.

b WO 89/05229 PCr/US88/04328 Thus, a particular need exists for a light-weight and high-strength fiber-reinforced composite material which covers large areas economically without loss of the structural characteristics of unidirectional tapes and which can be fabricated automatically in a rapid, efficient and inexpensive manner.

obecsA Accordingly, a *pj1mdar---u-_poof this invention is to provide a new and improved multi-directional, light-weight and high-strength fiber-reinforced plastic composite material of this type, wherein the unidirectional fiber-reinforced plastic tapes initially are interlaced in over-and-under relationship in a 0 degree/90 degree configuration. The interlaced material, which may be fabricated automatically in a machine known as a composite material interlacer, subsequently is subjected to heat and pressure in single or multiple layers to form an integral structure.

In general, the weaving or braiding of yarns, strips or ribbons of material in the forming of various types of parts n: -For example, U.S. Patent No. 2,162,598 to H. N. Atwood discloses the forming of a composite shatterproof window glass in which glass strips or ribbons are passed throucih or immersed in a molten plastic bath, subsequently braided, woven or interwoven into a fabric, and then subjected to heat and pressure to unite and bond the plastic-coated strips together. Similarly, U.S. Patent No. 3,439,685 to M. I.

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WO 89/05229 pcT/Uss8/4328 6 Port et al discloses the weaving of flat plastic yarn and passing the woven yarn through heat rolls to bond the yarns slightly to prevent slippage therebetween.

U.S. Patent No. 3,974,313 to V. L. James discloses an energy absorbing blanket comprising layers of cloth woven from tapes formed from glass filaments, an aromatic polyamide or other materials, in various patterns, so that the tapes of the layers can move relative to one another to absorb energy, e.g., of a projectile. U.S. Patent No. 4,030,892 to L. I. Mendelsohn et al is directed to an electro-magnetic shield which may be woven from filaments including a glass metal alloy. U.S.

Patent No. 3,769,144 to J. Economy discloses a central layer of woven carbon cloth disposed between two outer reinforcing layers to form a quilted fabric for use in fabricating gas-impermeable protective clothing or gas masks. U.S. Patent No. 4,412,854 to G. K. Layden concerns a method of producing a fiber-reinforced material by painting a thermoplastic polymeric binder, containing glass powder, on woven carbon cloth, drying the resultant sheet, cutting the sheet to produce a plurality of preforms of a desired shape, stacking the preforms in a mold, initially warm-molding the preform to form an intermediate article, and then hot pressing the intermediate article to form a final article.

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r o s i Previously, there has been disclosure of the formation of tape yarns on a circular loom into a tubular member which may be used in that configuration, or may be cut longitudinally to form a sheet of planar material. For example, circular looms of this general type are shown in U.S. Patent No. 2,454,146 to G.E.

Ezbelent, U.S. Patent No. 3,719,210 to P.D. Emerson et al and U.S. Patent No. 3,871,413 to S. Torii.

Heretofore, however, the prior art has not provided a multi-directional, light-weight, high-strength fibrereinforced plastic composite material which can be fabricated in a rapid, efficient and inexpensive manner, and which can be used for forming parts of tubular, planar or contoured configuration, and a primary purpose of this invention is to provide such a material and a method of making the material.

According to a first aspect of the present invention there is provided a method of forming a multi-directional light-weight, high-strength material, which comprises the 20 steps of: providing a plurality of continuous ribbons some of which comprising continuous fibres impregnated with a matrix and extending longitudinally essentially in only one direction, the ribbons also having a greater width than thickness; and interlacing the continuous ribbons into over-andunder relationship in 0 degree and 90 degree directions to form a continuous, tubular-shaped, multi-directional, seamless interlaced material.

According to a second aspect of the present invention there is provided a multi-directional, lightweight, high-strength material, which comprises: a plurality of 0 degree and 90 degree flat ribbons interlaced in over-and-under relationship so that the ribbons have sets of respective opposed engaged flat surface portions; at least some of the 0 degree and 90 degree ribbons 911010,gjnspe.013,29225.spe,7 uL.- i._i i~ -8having continuous fibres extending in only 90 degree and 0 degree directions, respectively; and at least some of the 0 degree and 90 degree ribbons having been being pre-impregnated with a matrix so that substantially all of the continuous fibres of the respective ribbons are encapsulated in the matrix and substantially the entire surface area of each of the opposed engaged flat surface portions of each sat of said opposed engaged flat surface portions of the respective ribbons is coated with the matrix.

According to a third aspect of the present invention there is provided a multi-directional, light-weight, high-strength laminated material, which comprises: a first layer of 0 degree and 90 degree flat ribbons interlaced in over-and-under relationship; at least one additional layer of 0 degree and degree flat ribbons interlaced in over-and-under relationship; least some of the 0 degree and 90 degree ribbons 20 of each layer comprising continuous unidirectional fibres pre-impregnated with a matrix so that substantially all of the continuous fibres are encapsulated in the matrix, and the 0 degree and 90 degree ribbons of each layer having the continuous fibres extending in only 0 degree 25 and 90 degree directions, respectively, in that layer; :the layers of 0 degree and 90 degree ribbons being in superimposed relationship with respect to one another; and n: the 0 degree and 90 degree ribbons of each layer being integrally bonded to each other and the 0 degree and 90 degree ribbons of each adjacent layer by the matrix.

According to a fourth aspect of the present invention there is provided a multi-directional, lightweight, high-strength material, which comprises: a plurality of 0 degree and 90 degree flat ribbons I ~interlaced in over-and-under relationship so that the 911010,gjnspe.013,29225.spe,8 Vf: iii~r -xl-r~l ribbons have sets of respective opposed engaged flat surface portions; at least some of the 0 degree and 90 degree ribbons having fibres extending in only 0 degree and 90 degree directions, respectively; and at least some of the 0 degree and 90 degree ribbons having been being pre-impregnated with a matrix so that substantially all of the fibres of the respective ribbons are encapsulated in the matrix and substantially the entire surface area of each of the opposed engaged flat surface portions of each set of said opposed engaged flat surface portions of the respective ribbons is coated with the matrix.

According to a fifth aspect of the present invention there is provided a circular-machine-interlaced fabric of flat tapes of polymeric material reinforced with continuous filaments in both the warp and weft .:directions, said warp and weft tapes being interlaced in S:over-and-under symmetrical relationship with respect to a 20 plane of the fabric, with the warp and weft tapes having sets of opposed flat surface portions disposed in the plane of the fabric and the weft tapes extending at a slightly inclined angle to the warp tapes, and said warp and weft tapes having edges that are abutting substantially throughout the fabric.

4 *The continuous tubular-shaped interlaced seamless material may be cut into tubular sections of preselected lengths and each section subjected to temporary heat and pressure so that the plastic matrix fuses the interlaced warp and weft ribbons into an integral seamless tube.

The continuous tubular-shaped interlaced material also may be cut in a 0 degree/90 degree configuration or an angle into a planar strip or planar sections and used to form integral members of planar or contoured construction. Articles or members may be formed from a single layer of the interlaced material, or may be formed of laminated construction from multiple layers of the S911010,gjnspe.013,29225.spe,9 1 i~i: sV 4 -9amaterial, with the 0 degree and 90 degree ribbons of each layer either parallel with, at an angle, aligned or offset with respect to, the ribbons of the other layer(s). Preferably, the ribbons are formed so as to have a thickness of at least 2 mils so as to be of sufficient strength to withstand interlacing. The ribbons also preferably have a width of at least 1/8 inch so as to not be subject to overtwisting and so as to have a relatively flat, unkinked configuration when the ribbons are interlaced together. Ribbons having different types of reinforcing fibres or filaments, or metal ribbons, also may be interlaced into the material to provide different selected material characteristics.

Embodiments of the invention will now be described by way of example only with reference to the accompanying drawings in which:- 0* Figure 1 is a perspective schematic view of a fibre- 2 reinforced plastic composite tape which is used in 20 practicising an embodiment of the invention; Figure 2 is a schematical elevational view of a i. machine for the slitting and winding of fibre-reinforced plastic composite unidirectional ribbons from the tape shown in Figure 1; Figure 3 is a schematic elevational view of a machine for interlacing the unidirectional ribbons produced by the machine of Figure 2, into a multidirectional, fibre-reinforced plastic composite seamless tube in accordance with an embodiment of the invention; Figure 4 is a schematic cross-sectional view taken along the line 4-4 in Figure 3; 911010,gjnspe.013,29225.spe,10 f 11

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k i i PCT/US88/04328 Figure 5 is a perspective view of a portion of the material as it is being interlaced in the machine illustrated in Figures 3 and 4; Figure 6 is a partial plan view of a portion of a multi-directional, interlaced material in accordance with\the present invention; Figure 7 is a view similar to Figure 6 and illustrating an alternate interlaced configuration; Figure 8a is a photomicrograph, in cross-sectional view, of an 8-ply material formed from a plurality of superimposed layers of material having an interlaced configuration as shown in Figure 7, after being subjected to temporary heat and pressure; Figure 8b is a series of cross-sectional photomicrographs of the material shown in Figure 8a; Figure 9 is a side elevational view, as seen along the line 9-9 in Figure 3, illustrating the cutting of the fiber-reinforced plastic composite seamless tube of Figure 3 to form a tube section; Figure 10 is a partial plan view of the machine shown in Figure 3, illustrating the cutting of the fiber-reinforced plastic composite seamless tube of Figure 3 to form a planar strip;

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WO 89/05229 PCT/US88/04328 11 n Figure 11 is a perspective view of the interlaced tube section formed in Figure 9; Figure 12 is a perspective view of the interlaced tube section of Figure 11 after having been subjected to temporary heat and pressure to form an integral tube; Figure 13 is a schematic cross-sectional view of a heated pressure mold for forming the interlaced tube section of Figure 11 into the integral tube of Figure 12; Figure 14 is a schematic elevational view of a heated pressure roller mechanism or forming the elongated planar strip of the interlaced material formed in Figure 10, into a material of integral planar construction; Figure 15 is a schematic cross-sectional view of a heated pressure mold for forming a planar section of the interlaced material into a member of integral planar construction; Figure 16 is a perspective view of the planar member formed in Figure Figure 17 is a perspective exploded schematic view illustrating a plurality of planar sections of the interlaced material prior to being formed into an integral laminated member; *%r i

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12 Figure 18 is a view similar to Figure 17 showing the planar sections of Figure 17 after being formed into the integral laminated member; Figures 19a-19d are schematic views illustrating the use of a heated pressure mold for forming a planar section of the interlaced material into an integral member of contoured configuration; Figure 20 is a perspective view of the contoured member formed by the heated pressure mold of Figure 19; and Figure 21 is a schematic perspective view of a planar member formed from fibre-reinforced plastic composite unidirectional ribbons containing different types of fibres.

In general, the present embodiment involves initially slitting a fibre-reinforced plastic matriximpregnated composite unidirectional tape 22 (for example, 4-12'' wide), as illustrated in Figure 1, into .continuous unidirectional tapes or ribbons 24 of reduced 20 width, in a machine 25 as shown in Figure 2. The ribbons "I 24 then are interlaced in a machine 26 illustrated schematically in Figures 3-5, 9 and 10 into a continuous, multi-directional seamless tube d8 of interlaced material I or fabric which is of uniform diameter along its length I 25 and which subsequently is cut and formed into members or articles of different shapes.

C9 4 P-z 0 911010,gjnspe.0 1 3,29225.spe,12 .1 i r WO 89/05229 PCT/US88/04328 13 ti For example, the interlaced seamless tube 28 may be cut transversely to form a tube section 30%of uniform diameter and a preselected length, as shown in Figure 11, and the tube section then subjected to temporary heat and pressure, as illustrated in Figure 13, to form a tube member 32 of integral construction as shown in Figure 12. The interlaced seamless tube 28 also may be cut longitudinallyor diagonally on an angle) to form a continuous strip 42 (Figure 10), and then transversely to form a section 44 (Figure 15), of the interlaced material of flexible, essentially planar construction. The strip 42 or section 44 then is subjected to temporary heat and pressure, as is illustrated in Figures 14 and 15, respectively, to form an essentially planar material 42p or member 44p (Figure 16) of integral construction. In the alternative, a cut section 44' of the flexible interlaced planar material may be formed into an integral member 46 having a contoured configuration, as illustrated in Figures 19 and The members 32, 42p, 44p, and 46 may be formed in a single layer configuration, or as a multilayer laminated member 48, as illustrated in Figures 17 and 18. Further, the interlacing of the ribbons 24 may be accomplished so that a resultant member 52 (Figure 21) includes ribbons 24 containing fibers of different types, and/or different ribbon widths and/or U H N WO 89/05229 PcT/88/04328 14 different ribbon thicknesses, to provide different structural characteristics in preselected areas of the article.

It is contemplated that the t:nmay be practiced using either fiber-reinforced thermoplastic composites or fiber-reinforced thermoset composites. However, fiber-reinforced thermoplastic composites gene-.lly are preferred because many fiber-thermoset composites, as presently manufactured, have a tacky surface consistency to facilitate hand lay-up, which makes them unsuitable for slitting and interlacing, although the tackiness of certain fiber-reinforced thermoset composites can be eliminated by appropriate stabilization of the end product in the manufacturing process.

Even then, however, thermoset composites tend to be relatively soft and, as a result, have poor edge stability, so that dust particles tend to break off during the ribbon slitting operation and/or the resultant ribbons 24 tend to become damaged in the interlacing operation. In any event, both types of fiber-reinforced plastic composites may be used in practicing the invention, as noted previously.

Referring to Figures 1 and 2, initially the fiber-reinforced plastic composite ribbons 24 may be slit from a supply roll 54 of the fiber-reinforced plastic matrix-impregnated tape 22 by the ribbon slitting machine and wound up on respective take-up reels 58. The tape 22 is in ul i C, I Iti 4. 'i I WO 89/05229 15 PCT/US88/04328 the form of a side-by-side array of bundles or tows 60 (Figure 1) of continuous fibers 62 extending longitudinally in only one direction, that is, unidirectional, which have been pre-impregnated under heat and pressure with a plastic matrix 63.

The fibers 62 are of a light-weight and high-strength type, such as carbon, glass, or synthetic fiber. For example, a presently preferred fiber-reinforced plastic composite tape 22 is formed of AS4 carbon fibers available from the Hercules Aerospace Company of Magna, Utah, which have been impregnated with a thermoplastic sold by the Imperial Chemical Company of England, under the tradename "PEEK" (polyether-ether-etherketone). A presently preferred synthetic fiber is an aromatic polyamide manufactured by E.I. DuPont Company of Wilmington, Delaware, and sold under the trademark "Kevlar" particularly "Kevlar" 29, 49 and 149, impregnated with a thermoplastic sold by the Phillips Petroleum Company of Bartlesville, Oklahoma, under the trademark "RYTON". Glass fibers which may be used are available from Pittsburgh Plate Glass Company of Pittsburgh, Pennsylvania. Other fiber reinforcements which may be used include metal fibers such as cobalt, boron or ceramic fibers (in a ceramic or other type matrix), or other synthetic fibers such as nylon or rayon. Similar composites can be achieved with the same or similar fiber reinforcements impregnated with thermosetting plastics, as for example, i ~E;L. WO 89/05229 1 6 PCT/US88/04328 available from the Ferro Corporation, -Composites Division, Culver City, California. Impregnation of the fiber reinforcements also can be accomplished by independent impregnators of fibers, such as Baycomp, a division of Bay Mills Ltd., Burlington, Ontario, Canada, and Polymer Composites Inc., of Winona, Minnesota.

The fiber-reinforced plastic composite tape 22 is slit by the ribbon slitting machine 25 parallel to the one direction in which the fibers of the tape extend so that the slit ribbons 24 also are unidirectional, as noted above, that is, the continuous fibers thereof extend longitudinally of the ribbons. Accordingly, the resultant ribbons 24 have extremely high tensile strength in a longitudinal direction, but substantially limited tensile strength in a transverse direction. After being interlaced, however, the unidirectional ribbons 24 retain their individual structural characteristics, and cooperate to provide these same structural characteristics, including high tensile strength, to the resultant material in both the longitudinal and transverse directions of the interlaced material.

It is very important in the present -i-n--ta\that the unidirectional ribbons 24 be slit to a substantial width with respect to their thickness so that when the ribbons are interlaced, they resist overtwisting and produce an essentially \Li j; s/ I

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07 oy ^Ej~y ;i WO 89/05229 PCT/US88/04328 flat "unkinked" interlaced configuration. Otherwise, the ribbons 24 tend to behave like yarns of circular cross section, which, when interlaced, tend to twist in excess of 900 and/or have an undulating, "knuckled", or "kinked" configuration.

Such results should be avoided in the present invention since they produce material having a nonuniform surface, destroy the surface integrity of the fibers 62, and reduce the tensile strength of the ribbons in a longitudinal direction. Further, certain ribbons containing higher modulus reinforcement fibers, such as carbon, also may snap if twisted under stress, requiring stopping of the machine 26 and splicing of the ribbon broken ends, with uncertain consequences regarding the structural integrity of the interlaced material. Accordingly, the ribbons 24 preferably have a thickness of at least 2 mils so as to have sufficient strength to withstand interlacing, and a width of at least 1/8 inch to avoid overtwisting during the interlacing operation.

Further, the maximum thickness of the ribbons 24 is dependent primarily on the maximum ribbon thickness which can be thoroughly impregnated by the matrix 63, presently considered to be about 0.150 inch. It also is contemplated that ribbons 24 of up to about 3 inches in width can be fabricated by constructing an interlacing machine 26 which is sufficiently rugged to process ribbons of this size over an

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WO 89/05229 PCT/US88/04328 18 extended period. Preferably, the thickness of the ribbons 24 is in a range on the order of about 6 to about 40 mils, with a ribbon width on the order of about 1/8 to about 1/2 inch. Most preferred, however, is a ribbon thickness in a range of about 6 to about 18 mils, with a ribbon width in a range on the order of about 3/16 to about 3/8 inch, based on various factors, such as preserving hinging at ribbon cross-over points, efficient manufacturing rate and ease of subsequent formability.

The slitting-and-winding machine 25 may be of any suitable type, such as that available from the Independent Machine Company of Fairfield, 'New Jersey. Thus, as shown in Figure 1, the machine 25 comprises the tape supply roll 54 and a slitting mechanism 66 provided with a series of knives (not shown in detail) adjustable to different spacings for cutting ribbons 24 of different widths. As the fiber-plastic matrix-impregnated composite tape 22 is advanced through the machine to the left in Figure 2, the knives of the slitting mechanism 66 slit the tape to form a plurality five in Figure 2) of ribbons 24. Further, since an entire width of the tape 22 normally cannot be slit at one time, the remaining unslit width portion of the tape is wound up on one of the takeup reels 58 for future use as a new supply reel "54".

After the ribbons 24 have been slit and wound on the take-up reels 58, the reels are transferred to the interlacing LI It _i -LI Y: I I I ii il~ ii -19machine 26, which is of a type capable of interlacing the ribbons, which are flexible, but stiff and boardy in nature. For example, the machine 26 may be of a circular type as disclosed in U.S. Patent No. 4977933, which is exclusively licensed to the assignee of the subject application, and the subject matter of which, to the extent not inconsistent with this disclosure, is hereby incorporated by reference.

In this regard, referring to Figure 3, a plurality of the reels 58, designated 58a and containing 0 degree ribbons 24a, are mounted in supply stands 70 (only two shown) about the periphery of the circular machine 26, which includes a fixed support table 72 and a continuously rotating table 74 comprising one or more shuttles 76 (best shown in Figure each of which also carries one of the reels 58, designated 58b and containing a supply of 90 degree ribbon 24b. The 0 degree ribbons 24a are suitably guided, under tension and without excessive twist, to vertically extending 20 positions, as clearly disclosed in Figures 4 and adjacent a cylindrical vertical forming surface 80 (shown only in Figure 4) of a cylinder 82 about which the table 74 and the shuttles 76 rotate. More specifically, the 0 i degree ribbons 24a are brought into engagement with the 25 vertical forming surface 80 in tightly abutted relationship about an annular guide ring 84 disposed about the cylinder 82.

For each pass of one of the shuttles 76, each of the **o 0 degree ribbons 24a is preset into an upper or lower position with respect to the approaching shuttle by a respective one of a plurality of 0 degree ribbon setting mechanisms 86, depending on the interlacing pattern being used, to'define a 0 degree ribbon shed. The next rotating shuttle 76 then passes through the 90 degree ribbon shed defined by the 0 degree ribbon setting mechanism 86, and lays the 90 degree ribbon 24b on that shuttle, under tension and without twist, against the 911010,gjnspe,013,29225.spe, 19 0EN k F _L i.i.~ii. a.

degree ribbons 24a at the cylindrical vertical forming surface 80, as is best shown in Figure 5. In the disclosed interlacing machine 26, this accomplished by the 90 degree ribbon 24b passing from the 90 degree supply reel 58b about vertical guide posts 87 on the shuttle 76, and then horizontally under a lower surfuce of the guide ring 84, after which the ribbon turns 900 and becomes laid into vertical engagement with the portions of the 90 degree ribbons 24a behind the guide ring, as illustrated in Figures 4 and 5. As the shuttle 76 then clears each of the 90 degree ribbons 24a, the degree ribbon is again preset, if necessary, for the next shuttle pass.

As the shuttles 76 rotate to form the interlaced ribbon tube 28, the tube is advanced vertically upward in increments corresponding to one 90 degree ribbon width by a take-up mechanism 88 (Figure for the laying of the next 90 degree ribbon pass into the 0 degree ribbons 24a 2 in tightly abutted relationship with the preceding 20 degree ribbon. Thus, as is clearly shown in Figure the 90 degree ribbon 24b is interlaced with the 0 degree ribbons 24a in over-and-under symmetrical relationship with respect to a circular plane of the interlaced i material tube 28 and in a continuous smooth helically extending path, with the 90 degree ribbon extending across the 0 degree ribbons at a slightly inclined angle approximately, but slightly less than perpendicular, and thus also at a slightly inclined angle I *to the axis of the interlaced material tube) and with engaged mating surface portions of the 90 degree and 0 degree ribbons disposed in the circular plane of the interlaced material tube. In this way, the interlaced ribbon tube 28 can be formed on a continuous basis to a preselected diameter.

Referring to Figure 6, in forming the tube 28, the fibre-reinforced plastic composite ribbons 24a and 24b L1,1 may be interlaced in tightly abutted relationship into a 911010,gjnspe.013,29225.spe,20 1/ I -i -21 plain over-and-under pattern, in which each ribbon passes over and then under alternating ones of the ribbons extending approximately perpendicularly thereto.. (In Figure 6, "over" 0 degree ribbons 24a are shaded and "under" 0 degree ribbons are unshaded). In the alternative, other interlaced patterns also may be used.

For example, Figure 7 illustrates an interlaced pattern for a tube 28' 'n which each ribbon 24a and 24b passes over four other ribbons extending approximately perpendicularly thereto, then under one of the ribbons perpendicular thereto, and then over four more of the ribbons perpendicular thereto, etc., to form a "fiveharness interlace" in which the ribbons clearly have edges abutting substantially throughout the interlaced material or fabric. (In Figure 7, "over" 0 degree ribbons 24a are shaded and "under" 0 degree ribbons are unshaded; on the opposite side of the material, the :pattern is reversed). The pattern of Figure 7 enables 20the ribbons 24a and 24b to be interlaced in a flatter 20 configuration then the interlaced ribbons in the pattern of Figure 5, which can be advantageous from the standpoint of greater flexibility and 911010,gjnspe.013,29225.spe,21 ea/ ooo WO 89/05229 PCT/US88/04328 22 ability to conform the interlaced material to contoured mold surfaces, and improved structural characteristics tensile, compressive and shear strength) of the final product.

Further, while in Figures 6 and 7, the ribbons 24a and 24b are shown as being of uniform width, the ribbons may be of different widths, depending upon the intended use and desired characteristics of the interlaced material. Increasing the width of the -degree ribbons 24b also is advantageous from the standpoint of increasing the rate at which the interlaced material can be fabricated. Decreasing the width of the ribbons (either the 0 degree or 90 degree, or both) is advantageous from the standpoint of the ultimate formability of curved finished parts, such as the contoured member 46 in Figure The photomicrographs of Figures 8a and 8b are a cross-sectional view and a series of continuous cross sections, respectively, of a 0/90 degree, 8-ply consolidated laminate of interlaced ribbons 24 formed from AS4 continuous carbon fibers (Hercules Aerospace) impregnated with a PEEK plastic matrix 63 (Imperial Chemical Company), enlarged 80 times as seen in Figure 8a. The ribbons 24 had a thickness of approximately 6 mils and a width of 3/16 inch. As is best shown in Figure 8a, qo the -9-degree oriented fibers 62 appear as numerous small essentially white circles directed at the viewer. The 0 degree oriented fibers 62 run across the page and are S1 i 'i U~I~ 11 WO 89/05229 Per/US88104328 23 essentially white. The laminate was consolidated by means of a press applying heat and pressure simultaneously.

With further reference to Figure 8a, the gray matter in which the -\degree oriented fibers 62 are encapsulated is the PEEK plastic matrix 63. Matrix (resin) rich areas appear as solid gray with no white fibers. Voids, areas in which there is neither fiber 62 nor resin 63, appear as solid black areas. The darker colors which are interspersed in the 9-degree oriented fibers 62 resulted from an imperfect cross section cut, a cut at an angle other than exactly 0/90 degrees. The areas in which the 0 degree oriented fibers 62 "split" represents one of the 0 degree ribbons 24j rising over |o or under one of the -&degree ribbons 24b.

The photomicrographs of Figures 8a and 8b also illustrate that the fiber alignment of each ply is very straight, which is critical for maintaining the structural characteristics of the unidirectional ribbons 24a and 24b. In this regard, unlike composites woven from yarns of circular or essentially circular cross section, there is minimal "knuckle" or "kinking" to disrupt structural integrity.

In summary, with respect to Figures 8a and 8b, it is seen that, as a result of pre-impregnation of the fibers 62 WO 89/05229 24 PCT/US88/04328 before further processing of the unidirectional material, there is substantially complete encapsulation and "wetout" of the individual fibers, with the fibers being maintained essentially straight within their respective individual ribbons 24a and 24b. This is in contrast to a nonuniform fiber encapsulation or "wetout" which would be achieved by dipping, spraying or coating procedures after the material has been converted by conventional weaving, braiding, etc., in which the thermoplastic matrix 63 would be unable to penetrate the tightly packed fibers 62. Further, as a result of the interlaced ribbons 24 being of substantial width with respect to their thickness, no significant bending or kinking of the fibers 62 is produced at ribbon cross-over points so as to disrupt the straightness of the fibers. As L net result, the finished material has been found, unlike conventionally woven composite yarns and rovings, to retain, or actually improve, all of the structural characteristics of conventional structures currently formed from the laminated ribbons, with a significant increase in ease of fabrication, including substantially improved capability to form, and consequent reduction in fabrication expense.

With reference to Figure 3, the takeup mechanism 88 comprises a pair of opposed intermittently motor-driven pinch rolls 89 (only one shown in Figure 3) having end portions 89e WO 89/05229 PC/US8/04328 of reduced diameter so as not to crush or damage the stiff folded-over portions 28f of the seamless tube 28. Referring to Figure 9, when it is desired to produce tubular sections, such as the tubular section 30 (also shown in Figure 11), the seamless tube 28 may feed from the pinch rolls 89 onto a suitable conveyor or inclined plate 90, and subsequently be manually cut transversely into the tube section 30 to a desired length.

With reference to Figure 10, when it is desired to cut the seamless tube 28 into the planar strip 42, the tube is advanced from the pinch rolls 89 by a rotatably driven takeup cylinder or drum 91 past a motor-driven rotary knife 92, which cuts the tube longitudinally, to form the strip 42. As the strip 42 then proceeds to the takeup drum 91, the strip fans out into a planar configuration and then becomes wound up on the takeup drum.

After the continuous seamless tube 28 has been cut transversely to form the interlaced tube section 30 as shown in Figure 9, the interlaced tube section is temporarily subjected to heat and pressure to cause the plastic matrix 63 to melt and then coalesce to fuse the interlaced ribbons 24a, 24b into the integral tube 32 shown in Figure 11. For example, the interlaced tube section 30 may be placed in a heated pressure mold 93 comprising a teles iing inner mold member 94 and outer A 'I -v I i i WO 89/05229 PCrUS88/04328 26 split mold members 95, as shown in Figure 12. The mold members 94 and 95 then are temporarily heated under pressure to cause the desired melting of the plastic matrix 63, and permitted to cool so that the plastic matrix flows and forms the tube 32.

When the interlaced seamless tube 28 is slit longitudinally by the rotary cutter 92, to form the planar sheet 42 shown in Figure 10, the sheet 42 also may subsequently be formed into the elongated planar sheet 42p of integral construction, by subjecting the interlaced sheet to temporary heat and pressure. For example, referring to Figure 14, the interlaced planar sheet 42 may be passed from a supply roll 94 transposed takeup drum 91) to a takeup 96, through a pair of opposed heated pressure rolls 98 for this purpose. In the alternative, the interlaced planar sheet 42 may be further cut longitudinally'or diagonally, and then cut transversely, into sheet sections of desired sizes, as illustrated by the section 44 in Figure 15. The sections 44 can then be formed into planar sheets of integrated construction, such as walls, panels, covers, etc., as illustrated by the member 44p in Figure by placing each cut section in a mold 100 comprising upper and lower heated pressure mold members 102 and 104.

Similarly, as is illustrated in Figure 17, two or more interlaced planar sections 44a, 44b and 44c may be arranged in

SI

0 -27- 9 super:'mposed relationship and subjected to temporary heat and pressure to form the multiple layer, laminated member or structure 48 shown in Figure 18. The 0 degree and degree ribbons 24a and 24b in each of the sections or layers 44a, 44b and 44c may extend parallel to each other as illustrated by the layers 44a and 44c, or the 0 degree and 90 degree ribbons of at least one layer may extend at an angle other than approximately 0/90 degrees to the ribbons in the other layer(s) that is, an angle which is greater than the slightly inclined angle at which the 0 degree ribbons extend with respect to the 90 degree ribbons in each layer, as illustrated by the layer 44b, so that the structure 48 has multi-directional strength in more than the approximately 0 degree and 90 degree directions. The 0 degree and 90 degree ribbons 24a and/or 24b in the different layers 44a, 44b and 44c also may be offset with respect to one another, and additional partial layer sections added at selected locations, as for example, to provide additional strength or 20 reinforcement at those locations.

Referring to Figures 19a-19d and 20, a planar section 44' of interlaced material also may be subjected to temporary heat and pressure to form the tray member 46 of contoured construction in a pressure mold 100' having 25 upper and lower heated mold members 102' and 104', respectively. In this regard, the individual fibrereinforced plastic composite ribbons 24a and 24b, prior to being interlaced, while flexible, normally are relatively stiff and difficult to control during bending.

When interlaced as shown in Figures 6 and 7, however, 911010,gjnspe.013,29225.spe,27 -;a I i WO 89/05229 PCT/US88/04328 28 the interlaced ribbons 24a and 24b cooperate to hold one another together and provide a series of hinges in both 0 degree and 90 degree directions at successive ribbon cross-over points. Thus, the interlaced planar section 44' readily can be preheated, as shown in Figure 19a, to a temperature slightly above the melting/softening point of the plastic matrix 63, placed in the heated mold 100', and the heated mold 100' slowly closed to form the contoured tray member 46 having lower curved edges and shown in Figure Referring to Figure 21, where it is desired that a member have different structural characteristics in different parts, it is considered to be within the purview of the invention to produce the member 52 wherein the interlaced ribbons 24a and 24b (Figures 6 and 7) in different parts 52a, 52b and 52c of the member contain fibers 62 (Figure 1) of different types, where it is desired that the membe.r have different structural characteristics in the different parts.

Thus, in the forming of the interlaced seamless tube 28 (Figure by stopping the interlacing machine 26, selectively changing certain of the supply reels 58a and 58b, and splicing the new ribbons 24a and 24b thereon to the existing ribbons in the machine, the tube can be formed utilizing fiber-reinforced plastic composite ribbons 24 containing different types of the fibers 62, at selected positions along the length of the tube.

IL. 1- -L

I

WO 89/05229 PCT/US88, 04328 29 Subsequently, the thus formed interlaced seamless tube 28 is processed in a manner as above-described, to form the member 52 having the different fibers 62 in the respective portions 52a, b and c of the member, as illustrated in Figure 21.

While the foregoing description has been directed primarily to the interlacing of fiber-reinforced plastic composite ribbons 24 of particular types, into certain interlaced configurations, it is considered within the purview of the invention that variations in the type of ribbons, fibers and the interlaced configuration may be used, depending upon the requirements and uses for which the material is intended.

For example, the fibers 62 could be discontinuous fibers for certain applications, such as the forming of tubular pipes.

Further, with reference to Figures 6 and 7, selected ones of the 0 degree ribbons 24a may be of different types than the other 0 degree ribbons and/or the -9degree ribbons 24b. In qo this regard, the -8degree ribbons 24b or certain of the 0 degree ribbons 24a may be of thin metal or a metal alloy formed by slitting, ribbons containing encapsulated metal filaments, such as that available from American Cyanimid, Polymer Products Division, Wallingford Connecticut, cast ribbons containing cobalt powder and available from Ribbon Technology, Inc. of Gahanna, Ohio, ribbons including encapsulated graphite in a nickel coating and available from Mitsubishi Metals of Japan, or other ribbons in the form of encapsulated metal filaments or

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I=i~:qi WO 89/05229 PCT/US88/04328 metal powder. More particularly, all of the 0 degree ribbons 24a could be metal or metal-containing ribbons interlaced with fiber-reinforced, electrically insulating plastic composite ribbons in a five harness array as shown in Figure 7, or an eight harness array (wherein each ribbon passes over one and under seven other ribbons), respectively, to provide an electromagnetic shielding member formed primarily of metal on one side and primarily of electrically insulating composite material on the other.

In summary, a new and improved interlaced fiber-reinforced plastic matrix-impregnated composite material, in the form of the interlaced tube 28, which may be used to make various types of light-weight members having high-strength characteristics and suitable for use in military and commercial aerospace and aircraft applications, as well as other commercial applications, and a method of making the material in a rapid and efficient manner, has been disclosed. The tube 28 may be cut into tubular sections 30, as shown in Figure 11, and then subjected to temporary heat and pressure to form an integral tube 32 as shown in Figure 12. The tube 28 also may be cut and formed into a continuous strip 42p, as shown in Figure 14, or into planar sections 44 and used to form integral members 44p of planar construction, as shown in Figure 16, or contoured members 46, as shown in Figure 20. Planar sections, such as 44a, 44b and 44c, may be superimposed to form IL- i u i WO 89/05229 PCT/US88/04328 31 a multi-directional laminated structure 48 as shown in Figure 18, and formed members may contain different types of fibers and/or ribbons, to provide different structural characteristics, as illustrated by the member 52 in Figure 21.

It is to be understood that various other modifications, additions and alternative designs are, of course, possible in light of the above teachings. Therefore, it also should be understood at this time that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described hereinabove.

Claims (50)

1. A method of forming a multi-directional light-weight, high-strength material, which comprises the steps of: providing a plurality of continuous ribbons SoT e Ls\-itc\-\ comprising continuous fibers impregnated with a matrix and extending longitudinally essentially in only one direction, the ribbons also having a greater width than thickness; and interlacing sespc t a-ve=a4-=e4g the continuous ribbons into over-and-under relationship -Wi=-Ma-=h r-t :~ibbn in 0 degree and 90 degree directions to form a continuous, tubular-shaped, multi-directional, seamless interlaced material.

2. The method of claim 1, which comprises the additional step of: heating a portion of the continuous tubular-shaped, multi-directional, seamless interlaced material under pressure so that the matrix fuses the interlaced ribbons into an integral seamless tube.

3. The method of claim 2, wherein the matrix is a thermoplastic. WO 89/05229 PCT/US88/04328 33

4. The method of claim 2, wherein the matrix is a i thermosetting plastic. The method of claim 2, wherein the matrix is a ceramic.

6. The method as recited in claim 1, wherein the ribbons have a thickness of at least 2 mils and a width of at least 1/8 inch.

7. The method as recited in claim 6, wherein the ribbons have a thickness in a range *or fntbr' o of 2 to 150 mils and a thickness in a range on the order of 1/8 inch to 3 inches.

8. The method of claim 1, wherein ribbons containing at least two different types of fibers are A interlaced to form separate sections of the elongated, tubular- shaped, multi-directional, seamless interlaced material.

9. The method as recited in claim 1, wherein at least some of the ribbons include continuous carbon, glass, boron and/or ceramic fibers. The method as recited in claim 1, wherein at least some of the ribbons include continuous synthetic fibers.

11. The method as recited in claim 1, wherein at least some of the ribbons are solid metal ribbons.

12. The method as recited in claim 1, wherein at least some of the ribbons include metal powder and/or metal filaments. I 'y A WO 89/05229 PCT/US88/04328 34

13. The method at recited in claim 1, wherein a major portion of the 0 degree ribbons are formed of a first material and a major portion of the 90 degree ribbons are formed of a second material, and the ribbons are interlaced in a pattern so that a major portion of the one side of interlaced material is formed of the first material and a major portion of an opposite side of the interlaced material is formed of the second material.

14. The method as recited in claim 13, wherein one of the materials is metallic and the other material is electrically insulating. The method as recited in claim 1, wherein the ribbons are of different widths and/or different thicknesses.

16. The method as recited in claim 1, which comprises the additional step of: cutting the elongated tubular-shaped, multi-directional seamless interlaced material to form an essentially planar multi-directional interlaced material.

17. The method as recited in claim 16, which comprises the additional step of: heating the planar multi-directional interlaced material under pressure so that the matrix fuses the interlaced ribbons into an integral essentially planar member.

18. The method as recited in claim 16, which comprises the additional steos of: 1 VO 89/05229 PCT/US88/04328 positioning at least one layer of the essentially planar multi-directional interlaced material in engagement with a contoured molding surface; and heating the layer of the multi-directional interlaced material so that the matrix fuses the interlaced ribbons into an integral article having a contoured configuration.

19. The method as recited in claim 1, which comprises the additional steps of: arranging at least two layers of the multi-directional interlaced material in superimposed relationship; and heating the superimposed layers under pressure so that the matrix fuses the interlaced ribbons of the layers into an integral, laminated member. The method as recited in claim 19, wherein the interlaced ribbons of at least one layer extend at an angle other than 0/90 degrees to the interlaced ribbons of at least one other layer.

21. The method as recited in claim 19, wherein at least some of the ribbons in one layer are offset~with respect to some of the ribbons in at least one other layer.

22. The method as recited in claim 19, wherein at least some of the interlaced ribbons in at least one layer are WO 89/05229 PCT/US88/04328 36 of f of different e.ets-". han at least some of the interlaced ribbons in at least one of the other layers.

23. A method of forming a multi-directional light-weight, high strength material, which comprises the steps of: providing at least one plastic matrix-impregnated sheet of continuous high-strength fibers arranged longitudinally essentially in only one direction; slitting the plastic matrix-impregnated sheet of fibers parallel to the one direction into continuous ribbons having greater width than thickness; and interlacing 1-r-pc-et-c on 1 -e-F the continuous ribbons into over-and-under relationship a ai a'r in 0 degree and 90 degree directions to form a continuous, tubular-shaped, multi-directional, seamless interlaced material.

24. The method of claim 23, which comprises the additional step of: heating a portion of the multi-directional, seamless interlaced material under pressure so that the plastic matrix fuses the interlaced ribbons into an integral member. A multi-directional, light-weight, high- strength material, which comprises: a plurality of 0 degree and 90 degree flat ribbons interlaced in over-and-under relationship so that the II WO 89/05229 PCT/US88/04328 37 ribbons have sets of respective opposed engaged flat surface portions; at least some of the 0 degree and 90 degree qo ribbons having continuous fibers extending in only -9-\degree and 0 degree directions, respectively; and at least some of the 0 degree and 90 degree ribbons hainr- been being pre-impregnated with a matrix so that substantially all of the continuous fibers of the respective ribbons are encapsulated in the matrix and substantially the entire surface area of each of the opposed engaged flat surface portions of each set of said opposed engaged flat surface portions of the respective ribbons is coated with the matrix.

26. The material as recited in claim 25, wherein the matrix is a thermoplastic.

27. The material as recited in claim 25, wherein the matrix is a thermosetting plastic.

28. The material as recited in claim 25, wherein the matrix is a ceramic.

29. The material as recited in claim 25, wherein the ribbons have a thickness of at least 2 mils and a width of at least 1/8 inch, and the interlaced ribbons have an essentially flat, unkinked configuration. The material as recited in claim 29, wherein the ribbons have a thickness in a range on the order of 2 to IB PCT/US88/04328 WO 89105229 150 mils and a width in a range thg:d:c: of 1/8 inch to 3 inches.

31. The material as recited in claim 25, wherein at least some of the boron and/or ceramic

32. at least some of fibers.

33. at leasc some of

34. at least some of filaments. The the ribbons include continuous carbon, glass, fibers. material as recited in claim 25, wherein ribbons include continuous synthetic material as recited in claim 25, wherein ribbons are solid metal ribbons. material as recited in claim 25, wherein ribbons include metal powder and/or metal The the The the The material as recited in claim 25, wherein a major portion of the 0 degree ribbons are of a first material and a major portion of the 90 degree ribbons are of a second material interlaced in a pattern with a major portion of the first material on one side of the interlaced material and a major portion of the second material on an opposite side of the interlaced material.

36. The material as recited in claim 35, wherein the first material is metallic and the second material is electrically insulating. e~i I _I_ WO 89/05229 PCT/US88/04328 39

37. The material as recited in claim 25, wherein the material is of elongated tubular seamless construction.

38. The material as recited in claim 25, wherein the material is of flexible planar construction.

39. The material as recited in claim 25, wherein the matrix bonds the interlaced ribbons together and forms a material of integral construction. The material as recited in claim 39, wherein the integral material is of elongated tubular seamless construction.

41. The material as recited in claim 39, wherein the integral material is of planar construction.

42. The material as recited in claim 39 wherein the integral material is of contoured construction.

43. The material as recited in claim 39, wherein the integral material includes separate sections having interlaced ribbons formed of different types of continuous fibers.

44. A multi-directional, light-weight, high-strength laminated material, which comprises: a first layer of 0 degree and 90 degree flat ribbons interlaced in over-and-under relationship; at least one additional layer of 0 degree and degree flat ribbons interlaced in over-and-under relationship; -1 4. I I WO 89/05229 PCT/US88/04328 at least some of the 0 degree and 90 degree ribbons of each layer comprising continuous unidirectional fibers pre-impregnated with a matrix so that substantially all of the continuous fibers are encapsulated in the matrix, and the 0 degree and 90 degree ribbons of each layer having the continuous fibers extending in only 0 degree and 90 degree directions, respectively, in that layer; the layers of 0 degree and 90 degree ribbons being in superimposed relationship with respect to one another; and the 0 degree and 90 degree ribbons of each layer being integrally bonded to each other and the 0 degree and 90 degree ribbons of each adjacent layer by the matrix. A multi-directional, light-weight high-strength laminated material, as recited in claim 44, wherein the interlaced ribbons of at least one layer extend at an angle other than 0/90 degrees to the interlaced ribbons of at least one other layer.

46. A multi-directional, light-weight, high-strength laminated material, as recited in claim 44, wherein the interlaced ribbons of at least one layer are offset with respect to the interlaced ribbons of at least one other layer. I i Ca~- WO 89/05229 PCTUS88/04328 41

47. A multi-directional, light-weight, high-strength laminated material, as recited in claim 46, wherein at least some of the interlaced ribbons of at least one layer are of different construction than at least some of the interlaced ribbons of at least one of the other layers.

48. A multi-directional, light-weight, high-strength, integral flexible material, which comprises: a plurality of spaced continuous ribbons of continuous unidirectional fibers extending in interlaced over-and-under relationship in 0 degree and 90 degree directions, respectively; said elongated fibers in the 0 degree ribbons extending only in the 0 degree direction and the elongated fibers in the 90 degree ribbons extending only in the 90. degree direction; and a matrix bonding the ribbons of continuous unidirectional fibers, the matrix also impregnating the fibers of each ribbon and covering exterior surfaces of the ribbons to provide the integral flexible material.

49. The material of claim 48, wherein the matrix is a thermoplastic. The material of claim 48, wherein the matrix is a thermosetting plastic.

51. The material of claim 48, wherein the matrix is a ceramic. .i- -42-

52. A multi-directional, light-weight, high-strength material, which comprises: a plurality of 0 degree and 90 degree flat ribbons interlaced in over-and-under relationship so that the ribbons have sets of respective opposed engaged flat surface portions; at least some of the 0 degree and 90 degree ribbons having fibres extending in only 0 degree and 90 degree directions, respectively; and at least some of the 0 degree and 90 degree ribbons having been being pre-impregnated with a matrix so that substantially all of the fibres of the respective ribbons are encapsulated in the matrix and substantially the entire surface area of each of the opposed engaged flat surface portions of each set of said opposed engaged flat surface portions of the respective ribbons is coated with the matrix. oe ee

53. A circular-machine-interlaced fabric of flat tapes of polymeric material reinforced with continuous I filaments in both the warp and weft directions, said warp and weft tapes being interlaced in over-and-under symmetrical relationship with respect to a plane of the fabric, with the warp and weft tapes having sets of opposed flat surface portions disposed in the plane of the fabric and the weft tapes extending at a slightly inclined angle to the warp tapes, and said warp and weft D tapes having edges that are abutting substantially throughout the fabric.

54. A composite of the fabric of claim 53. The material as recited in claim 25, wherein the 0 degree ribbons are disposed in tightly abutted relationship, and the 90 degree ribbons are disposed in tightly abutted relationship. 911010,gjnspe.013,29225.spe,42 -43

56. A multi-directional, light-weight, high-strength laminated material, as recited in claim 44, wherein the 0 degree ribbons are disposed in tightly abutted relationship, and the 90 degree ribbons are disposed in tightly abutted relationship.

57. The material of claim 48, wherein the 0 degree ribbons are disposed in tightly abutted relationship, and the 90 degree ribbons are disposed in tightly abutted relationship.

58. The material of claim 52, wherein the 0 degree ribbons are disposed in tightly abutted relationship, and the 90 degree ribbons are disposed in tightly abutted relationship.

59. The fabric of claim 53, wherein the warp tapes are disposed in tightly abutted relationship, and the weft tapes are disposed in tightly abutted relationship. A composite of the fabric of claim 59. a.

61. A method of forming a multi-directional, light- weight, high-strength material substantially as hereinbefore described with reference to the accompanying drawings.

62. A multi-directional, light-weight, high-strength material substantially as hereinbefore described with reference to the accompanying drawings. DATED this 16th day of October 1991 Qyadrax Corporation By Its Patent Attorneys DAVIES COLLISON 911016,gnspe.013,29225.spe,43