COMPOSITE MATERIAL COMPRISING PRE-IMPREGNATED WOVEN FIBERS

Abstract

A material of pre-impregnated woven fibers for a part is in the form of a fibrous mat having at least one layer of several pieces of fibrous fabric pre-impregnated with resin. At least one portion of the fabric has a low-shrinkage contexture. The pieces of fabric are positioned parallel with the plane (X, Y) of the fibrous mat and orientated in different directions in the plane (X, Y).

Claims

1. A pre-impregnated woven fiber material in a form of a fibrous mat comprising at least one layer of a plurality of pieces of fibrous fabric pre-impregnated with resin, wherein the pieces of fibrous fabric pre-impregnated with resin are positioned parallel to a plane of the fibrous mat and are oriented in different directions in the plane.

2. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric pre-impregnated with resin are oriented in the different directions such that each area of 2 cm.sup.2 of the fibrous mat comprises across a thickness at least 4 distinct directions of fibers forming angles of more than 15 therebetween.

3. The pre-impregnated woven fiber material according to claim 1, wherein the entire fibrous fabric pre-impregnated with resin forming the fibrous mat has a shrinkage of less than 5%.

4. The pre-impregnated woven fiber material according to claim 1, wherein a ratio between a length and a thickness of the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat is between 60 and 250.

5. The pre-impregnated woven fiber material according to claim 4, wherein the ratio between the length and the thickness of the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat is between 80 and 200.

6. The pre-impregnated woven fiber material according to claim 5, wherein the ratio between the length and the thickness of the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat is between 100 and 180.

7. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat have a width greater than a quarter of a length of the pieces of fibrous fabric.

8. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat have a width greater than half of a length of the pieces of fibrous fabric.

9. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat have a width equal to a length of the pieces of fibrous fabric.

10. The pre-impregnated woven fiber material according to claim 1, wherein the fibrous mat has an average surface mass at least 2 times greater than a surface mass of the fibrous fabric pre-impregnated with resin and less than 10 times the surface mass of the fibrous fabric pre-impregnated with resin.

11. The pre-impregnated woven fiber material according to claim 1, wherein the fibrous mat has an average surface mass between 1 kg/m.sup.2 and 3 kg/m.sup.2.

12. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric are impregnated with a thermosetting polymer resin adapted to be crosslinked by a thermocompression operation.

13. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric are impregnated with a thermoplastic polymer resin adapted to be solidified by a thermocompression step.

14. The pre-impregnated woven fiber material according to claim 1, wherein the pieces of fibrous fabric pre-impregnated with resin of the fibrous mat have a triangular, rectangular, or hexagonal shape.

15. The pre-impregnated woven fiber material according to claim 1 further comprising pre-impregnated unidirectional fiber lap pieces.

16. A part made of a composite material formed by thermocompression of at least one pre-impregnated woven fiber material in a form of a fibrous mat according to claim 1.

17. The pre-impregnated woven fiber material according to claim 1, wherein at least one portion of the fibrous fabric pre-impregnated with resin forming the fibrous mat has a shrinkage of less than 5%.

Description

DRAWINGS

[0043] In order that the disclosure may be well understood, there will now be described various forms thereof, given by way of example, reference being made to the accompanying drawings, in which:

[0044] FIG. 1 represents a mat roll according to the present disclosure;

[0045] FIG. 2 is a detail view of the mat constituted by a stack of fabric pieces according to the present disclosure;

[0046] FIG. 3 is a transparent detail view of the mat of FIG. 2 with arrows representative of the orientations of fibers according to the present disclosure;

[0047] FIGS. 4a to 4f illustrates possible forms of parts made from the material according to the present disclosure.

[0048] The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.

DETAILED DESCRIPTION

[0049] The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.

[0050] FIG. 1 shows a partially unwound roll of fibrous mat 2 according to the present disclosure.

[0051] The mat is constituted by fabric pieces 3 of fibers pre-impregnated with a matrix or resin disposed parallel to the plane (X, Y) of the mat.

[0052] The fabric pieces 3 are stacked on top of each other and are disposed parallel to the plane (X, Y).

[0053] The matrix may be a thermosetting resin, in particular epoxy, or a thermoplastic resin such as PEI, PAEK, PA, PEEK, among others, or a ceramic precursor.

[0054] The fibers may be carbon fibers, glass fibers, Kevlar fibers, ceramic fibers such as SiC (silicon carbide) or alumina oxides or the like.

[0055] Optionally, the fibers are called continuous fibers, that is to say rovings constituted by sets of parallel or twisted continuous filaments.

[0056] According to another variant, the fibers are called discontinuous fibers, that is to say rovings constituted by a filament aggregate of finite length held together by twisting and/or sizing and/or taping. For example, it may comprise Verranne type glass fibers or cracked fibers type carbon fibers (stretch broken fibers).

[0057] The fabrics may be of one single type of fibers or of combinations of fibers intertwined according to patterns such as canvas, twill, satin or braiding, or else stacked according to different directions and sewn (NCF).

[0058] Advantageously, the fibers are crossed and intertwined according to two perpendicular directions and in one form in substantially identical proportions according to each of the two directions.

[0059] The fibers inside the fabric pieces 3 are disposed substantially parallel to the plane (X, Y).

[0060] According to another variant, the fibrous mat may be a combination of pre-impregnated fiber fabric pieces and pre-impregnated unidirectional fiber lap pieces meeting similar geometrical characteristics, the fibers capable of being of the same nature or of different nature as previously described.

[0061] The fabrics are characterized by low-shrinkage contextures such as twill 22, twill 31, satin of 5 or of 8.

[0062] The term fabrics having low-shrinkage contextures, means contextures in which the corrugations of the threads, or rovings, of one direction of the fabric crossing the rovings of the other direction of the fabric impart a slight relief in thickness to the fabric.

[0063] Such a feature is obtained, on the one hand, using rovings having an envelope section of the filaments, which make up the rovings or threads, substantially ellipsoidal and very flattened, and in one form by a weave pattern of the fabric in which most of the weft rovings pass over at least two warp rovings such as twill 22, twill 31, satin of 5 or of 8.

[0064] Such textures then have a shrinkage of less than 5%. In one form, the shrinkage is less than 2%. In a further form, the shrinkage is less than 0.7%.

[0065] Thus, the fabrics offer, on the one hand, good mechanical properties in the plane, and have good deformation capacities by unstraining the fibers between the warp and weft directions during the compression of the material.

[0066] Advantageously, thanks to these contextures, the fabrics of pre-impregnated fibers have an apparent thickness in the initial state smaller than 200% of the thickness of the associated fabric piece after thermocompression. For example, in one form, the pre-impregnated fiber fabric has an initial thickness smaller than 170% of the thickness of the fabric piece after thermocompression.

[0067] FIG. 2 shows a detail of an example of a fibrous mat 2 having a stack with superposition of several layers of several fabric pieces 3 oriented according to different directions in the plane (X, Y) and the pieces partially covering each other.

[0068] The fabric pieces 3 have a polygonal shape and in one form have a quadrilateral shape.

[0069] In another form, the fabric pieces 3 have a triangular or rectangular or hexagonal shape.

[0070] The dimensions of the fabric pieces 3 are such that the ratio between their largest length and the thickness of the fabric layer of the fibrous mat 2 is substantially comprised between 60 and 250.

[0071] In one form, the fabric pieces 3 have a length at least 80 times greater than the thickness of the woven fibers lap.

[0072] In another form, the fabric pieces 3 have a length at least 100 times greater than the thickness of the woven fiber lap.

[0073] The dimensions of the fabric pieces 3 are such that the ratio between their largest length and their width is less than or equal to 4.

[0074] In one form, the width of the fabric pieces 3 of the fibrous mat 2 is greater than half their length.

[0075] In another form, the width of the fabric pieces 3 of the fibrous mat 2 is substantially equal to their length.

[0076] The fabric pieces 3 are cut in fabrics as previously defined. They have a surface mass of dry fabric comprised between 0.160 kg/m.sup.2 and 0.6 kg/m.sup.2.

[0077] The fabric pieces 3 are impregnated with a thermosetting or thermoplastic resin according to a resin/fiber volume ratio comprised between 0.35 and 0.55.

[0078] The fibrous mat 2 constituted from these fabric pieces 3 is characterized in that the fabric pieces 3 are disposed in the plane of the fibrous mat 2 or substantially parallel to the plane of the fibrous mat 2.

[0079] The fibrous mat 2 has a surface mass ranging from 1 to 3 kg/m.sup.2. Its surface mass is at least greater than 2 times the surface mass of the constituent fabric, and less than 10 times the surface mass of the constituent fabric, and in one form, the surface mass of the fibrous mat 2 is between 3 and 8 times the surface mass of the constituent fabric.

[0080] The fibrous mat 2 has a random distribution of the fabric pieces 3 in the plane of the fibrous mat 2, resulting in random orientations of the main directions of the fibers of each fabric piece 3 in the plane of the mat and an overlap of the fabric pieces 3 therebetween.

[0081] FIG. 3 shows an example of a fibrous mat 2, highlighting in transparency the different fabric pieces 3 and the respective orientations of the fibers of each individual piece.

[0082] The fabric pieces 3 are disposed parallel to the plane of the fibrous mat 2, providing step by step coverages between the fabric pieces 3. The orientations of the fabric pieces 3 and the overlap of pieces at least two by two in the plane of the mat allow obtaining, in any square area of at least 1.4 cm inside (2 cm.sup.2), at least 4 distinct directions of fibers forming angles of more than 15 therebetween.

[0083] As shown in the dotted square 9 in FIG. 3, the fibers inscribed inside the dashed square 9 are in multiple directions, herein more than 4. Considering fibers of two fabric pieces 3 in this dotted square 9, it is possible to find two fabric pieces 3 forming an angle of up to 45.

[0084] Because each fabric piece 3 itself includes two directions of fibers substantially perpendicular to each other, the fibrous mat 2, in this dotted square 9, has fiber orientations in so many directions parallel to the plane of the mat, which provides homogenized properties of stiffness and substantially isotropic resistance in this plane.

[0085] The material according to the present disclosure enables in particular the making of parts according to the manufacturing method described in FIGS. 4a to 4f.

[0086] It comprises a cutting step (FIG. 4b or 4b bis) of at least one flank of the fibrous mat 4 or blank in the fibrous mat 2 formed by the fabric pieces 3.

[0087] The manufacturing method alternatively comprises a stack of several flanks of fibrous mat 4 or blanks.

[0088] The manufacturing method alternatively comprises a preforming step (FIG. 4c bis) of the fibrous mat flanks 4 or of the stack of fibrous mat flanks 4.

[0089] The manufacturing method alternatively comprises a step of assembling the preforms obtained in the previous step (FIG. 4c bis).

[0090] The implementation comprises a step (FIG. 4c or 4d bis) of arranging the flanks of fibrous mat 4 or blanks, or preforms or preform assembly in a mold 5, 6.

[0091] The manufacturing method comprises a step (FIG. 4d or 4e) of thermocompressing the flanks of fibrous mat 4 or blanks, or preforms or preform assembly to form a woven fiber based composite part 1.

[0092] The mold 5, 6 is closed and a compression and a thermal cycle are applied on the material to compact it and make it creep/deform, in the directions 7 or 8 represented in FIGS. 4d and 4e respectively, to fill the volume of the imprint of the mold 5, 6.

[0093] The compression may be uni-axial or multi-axial depending on the closure kinematics of the tooling/mold.

[0094] In one form, the compression directions are locally perpendicular or substantially perpendicular to the plane of the flanks of the fibrous mat 4, blanks or preforms.

[0095] A polymerization thermal cycle is carried out when the resin is a thermosetting or solidification resin when the resin is a thermoplastic resin.

[0096] The thermocompression step may be carried out in an autoclave or by press molding, and in one form is carried out by applying pressures of at least 80 to 100 bars on the material.

[0097] The manufacturing method comprises a step of demolding (FIG. 4f) the woven fiber based composite part 1.

[0098] Alternatively, the manufacturing method then comprises a step of shrinking and/or machining the woven fiber based composite part 1.

[0099] Alternatively, the manufacturing method includes the hybridization of flanks of fibrous mat 4 or preforms cut in one or more of the variants of the fibrous mat 2 previously described, and/or with unidirectional continuous or discontinuous fiber laps, and/or with woven continuous fiber laps.

[0100] Thanks to the mat according to the present disclosure, after thermocompression of the material, a coverage of the fabric pieces 3 therebetween is obtained on the parts with constant or variable thickness, providing a proper homogeneity of the mechanical properties of stiffness and strength in any direction of the plane of the mat, thus providing a proper transfer of the forces/loads.

[0101] The present disclosure enables the conservation of several fiber orientations in the plane. The mechanical performances are maintained even for a part made of a pre-impregnated woven fiber material 1 with a very low thickness (equivalent to at least 1 time the thickness of the fabric piece 3). An almost isotropic material is obtained.

[0102] Depending on the length of the fibrous material flanks 4 (long or short), the thermocompression will induce a creeping starting from the center in the direction 8 (perpendicular to the plane of the flank when it is long (FIG. 4e)) or according to the direction 7 (short flank (FIG. 4d)).

[0103] After thermocompression, composite materials are obtained, with high mechanical properties and providing these same properties in the planes of the layers including the thin areas of these molded parts.

[0104] Depending on the distribution of the fibrous material flanks 4 in the mold 5, 6 (shape, stacks), the resin substantially creeps during the compression step.

[0105] As a general rule, upon the creeping during the thermocompression, it is desirable to have a viscosity of the resin which allows maintaining the desired resin/fiber stoichiometric ratio. In the case of very thin piece thickness, close to once the thickness of the fabric, it is possible to promote the desired creeping of the resin, by generating higher compaction pressures.

[0106] In the case of a part made of a pre-impregnated woven fiber material 1 having progressive and/or thin thicknesses, the creeping of the fabric pieces 3 or relative displacement of the latter relative to each other during the thermocompression, allows filling the total volume of the imprints 5, 6 of the mold.

[0107] An exemplary form is described below.

[0108] The mat of fabric piece(s) (or fibrous mat 2) is made from carbon fiber fabric(s) with a surface mass of about 280+/30 g/m.sup.2.

[0109] The fibers are made of carbon called high-strength or intermediate-modulus carbon and woven according to a low-shrinkage contexture of the type satin of 5 or twill of 2.

[0110] The fabric is impregnated with an epoxy thermosetting resin to form a pre-impregnated material having a mass rate comprised between about 70% of fibers and 30% of resin and 60% of fibers and 40% of resin.

[0111] The woven fiber lap intended to form the pre-impregnated fabric which will be cut into pieces to form the fabric pieces 3, has a compressed thickness of about 0.28 mm.

[0112] In the initial state, the pre-impregnated woven fiber fabric piece 3 or lap has an average thickness of 0.42 mm.

[0113] The impregnated fabric is cut into substantially square pieces of 35 mm side (i.e. 125 times the nominal thickness of the fabric) to form fabric pieces 3.

[0114] The fabric pieces 3 are disposed randomly in orientation and position on a planar surface, at an average of 3200 pieces/m.sup.2 leading to the obtainment of a fabric piece mat with an average surface mass of 1.5 kg/m.sup.2 in which there are, on average, 5 layers of fabric pieces 3.

[0115] This pre-impregnated woven fiber material being implemented into one single layer in a tooling, heated so that the matrix reaches a viscosity low enough to enable the pieces to slip relative to each other, such as for example less than 100 poises and more than 20 poises, and subjected to a pressure through the closure of the tooling, a pressure which may reach from 20 bars up to several hundred bars, can allow for part thicknesses ranging from about 0.5 mm to about 4 mm.

[0116] The mechanical properties of the molded material have elasticity moduli in the two main directions of a part surface in the range of 30 to 45 GPa and a mechanical tensile strength in the direction of the part plane higher than 300 MPa.

[0117] Unless otherwise expressly indicated herein, all numerical values indicating mechanical/thermal properties, compositional percentages, dimensions and/or tolerances, or other characteristics are to be understood as modified by the word about or approximately in describing the scope of the present disclosure. This modification is desired for various reasons including industrial practice, material, manufacturing, and assembly tolerances, and testing capability.

[0118] As used herein, the phrase at least one of A, B, and C should be construed to mean a logical (A OR B OR C), using a non-exclusive logical OR, and should not be construed to mean at least one of A, at least one of B, and at least one of C.

[0119] The description of the disclosure is merely exemplary in nature and, thus, variations that do not depart from the substance of the disclosure are intended to be within the scope of the disclosure. Such variations are not to be regarded as a departure from the spirit and scope of the disclosure.