Part made from oxide/oxide composite material for 3-D reinforcing and method for manufacture of same

Abstract

A part made of oxide/oxide composite material includes fiber reinforcement constituted by a plurality of warp yarn layers and of weft yarn layers interlinked by three-dimensional weaving, with the spaces present between the reinforcing yarns being filled with a refractory oxide matrix. The fiber reinforcement presents a weave selected from the following weaves: interlock; multi-plain; multi-satin; and multi-serge, with warp and weft thread counts lying in the range 4 yarns/cm to 20 yarns/cm. The fiber reinforcement also presents a fiber volume fraction lying in the range 40% to 51%.

Claims

1. A part made of oxide/oxide composite material comprising fiber reinforcement constituted by a plurality of warp yarn layers and of weft yarn layers interlinked by three-dimensional weaving, with the spaces present between the reinforcing yarns being filled with a refractory oxide matrix; wherein the fiber reinforcement presents a weave selected from the following weaves: interlock; multi-plain; multi-satin; and multi-serge; and warp and weft thread counts lying in the range 4 yarns/cm to 20 yarns/cm, and wherein the fiber reinforcement presents a fiber volume fraction lying in the range 40% to 51%, and wherein spaces present between the yarns of the fiber reinforcement are of dimensions that are less than five times a maximum section of the yarns of the fiber reinforcement.

2. A part according to claim 1, wherein the part presents, in monotonic traction, at ambient temperature, and in the warp direction: a modulus of elasticity lying in the range 120 GPa to 170 GPa; a breaking deformation of not less than 0.35%; and a breaking stress greater than 250 MPa.

3. A part according to claim 1, wherein the yarns of the fiber reinforcement are made of fibers constituted by one or more of the following materials: alumina; mullite; silica; an aluminosilicate; and a borosilicate.

4. A part according to claim 1, wherein the material of the matrix is selected from: alumina; mullite; silica; an aluminosilicate; and an aluminophosphate.

5. A method of fabricating an oxide/oxide composite material part, the method comprising the following steps: forming a fiber texture by three-dimensional weaving of refractory oxide yarns; compacting said fiber texture; placing on one side of the fiber texture a slip containing a submicrometer powder of refractory oxide particles; establishing a pressure difference to force the slip to pass through the fiber texture; filtering a liquid of the slip that has passed through the fiber texture so as to retain the powder of refractory oxide particles inside said texture and to form a filled preform; drying the filled preform; and sintering the submicrometer powder of refractory oxide particles in order to form a refractory oxide matrix in the preform; wherein during the step of forming the fiber texture the yarns are woven with a weave selected from the following weaves: interlock; multi-plain; multi-satin; and multi-serge; with warp and weft thread counts lying in the range 4 yarns/cm to 20 yarns/cm, and in that, after the compacting step, said fiber reinforcement presents a fiber volume fraction lying in the range 40% to 51%, such that spaces present between the yarns of the fiber reinforcement are of dimensions that are less than five times a maximum section of the yarns of the fiber reinforcement.

6. A method according to claim 5, wherein the yarns of the preform are made of fibers constituted by one or more of the following materials: alumina; mullite; silica; an aluminosilicate; and a borosilicate.

7. A method according to claim 5, wherein the submicrometer particles are made of a material selected from: alumina; mullite; silica; an aluminosilicate; and an aluminophosphate.

8. A method according to claim 5, wherein the yarns of the fiber reinforcement comprise continuous fibers.

9. A part according to claim 1, wherein the yarns of the fiber reinforcement comprise continous fibers.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other characteristics and advantages of the invention appear from the following description of particular implementations of the invention, given as nonlimiting examples, and with reference to the accompanying drawings, in which:

(2) FIG. 1 shows a plane of a three-dimensional interlock weave in accordance with an embodiment of the fiber texture of the invention;

(3) FIG. 2 shows a plane of a three-dimensional multi-plain weave in accordance with an embodiment of the fiber texture of the invention;

(4) FIG. 3 shows a plane of a three-dimensional multi-satin weave in accordance with an embodiment of the fiber texture of the invention;

(5) FIG. 4 shows a plane of a three-dimensional multi-serge weave in accordance with an embodiment of the fiber texture of the invention;

(6) FIG. 5 is a diagrammatic view showing the infiltration of a fiber texture with refractory oxide particles by means of the SPS technique;

(7) FIG. 6 is a micro-graph of a section of a part made of oxide/oxide type material as fabricated in the prior art;

(8) FIGS. 7A, 7B, and 7C are micro-graphs of a part made of oxide/oxide composite material in accordance with the invention; and

(9) FIG. 8 is a diagram showing the design domain for the fiber texture of the invention.

DETAILED DESCRIPTION OF EMBODIMENTS

(10) The method of fabricating a part out of oxide/oxide composite material in accordance with the present invention begins by making a fiber texture that is to form the reinforcement of the part.

(11) In accordance with the invention, the fiber texture is made by three-dimensional weaving between a plurality of warp yarns and a plurality of weft yarns, the layers of warp yarns being interlinked by weft yarns using three-dimensional weaving corresponding to a weave selected from one of the following weaves: interlock; multi-plain; multi-satin; and multi-serge; and with warp and weft thread counts lying in the range 4 yarns/cm to 20 yarns/cm, the texture as obtained in this way then being contacted to present a fiber volume fraction lying in the range 40% to 51%, the yarns or fibers in the fiber texture each having a number of filaments lying in the range 400 filaments to 700 filaments. FIG. 8 shows the design domain D for the fiber texture according to the invention, the domain D defining the values that need to be presented by the parameters relating to the fiber texture of the invention.

(12) These characteristics of the fiber texture make it possible to ensure that there are no spaces between the yarns presenting a dimension greater than five times the maximum section of the yarns. Thus, once the matrix has been formed within the texture, the blocks of matrix that are present between the yarns of the texture present dimensions that are all less than five times the maximum section of the yarns, thereby making it possible to prevent cracks appearing in the final material of the part.

(13) The term matrix block is used herein to mean any continuous portion of matrix situated between two or more yarns. The term dimension of a matrix block is used herein to designate any length, width, depth, thickness, height, or indeed diameter of a matrix block, and in still more general manner any size that can be measured in a straight-line direction.

(14) The term thread count is used herein to designate the number of yarns per unit length in the warp direction and in the weft direction.

(15) The terms three-dimensional weaving and 3D weaving are used herein to designate a weaving technique in which at least some of the warp yarns interlink weft yarns over a plurality of weft layers.

(16) Throughout the specification below, and in all of the drawings, it is stated and shown by convention and for reasons of convenience that it is the warp yarns that are deflected from their paths in order to take hold of the weft yarns of one or more layers of weft yarns. Nevertheless, it is also possible for the roles to be interchanged between warp and weft, which must also be considered as being covered by the claims.

(17) The term interlock weave or fabric is used herein to mean a 3D weave in which each layer of warp yarns interlinks a plurality of layers of weft yarns, with all of the yarns in the same warp column having the same movement in the weave plane. FIG. 1 is a view of eight planes of an interlock weave having seven layers of warp yarns C.sub.1 and eight layers CT.sub.1 of weft yarns T.sub.1. In the interlock weave shown, a layer CT.sub.1 of warp yarns T.sub.1 is made up of two adjacent half-layers ct.sub.1 that are offset from each other in the warp direction. There are thus 16 half-layers of weft yarns in a staggered configuration. Each warp yarn C.sub.1 interlinks three half-layers of weft yarns. It would also be possible to adopt a weft arrangement that is not staggered, the weft yarns of two adjacent layers of weft yarns being aligned in the same columns.

(18) By way of example, the fiber texture of the invention may be made by 3D weaving using an interlock weave as shown in FIG. 1 with warp and weft thread counts of 8 yarns/cm, 10 yarns/cm, and 12 yarns/cm, or with a warp thread count of 12 yarns/cm and a weft thread count of 5 yarns/cm.

(19) The term multi-plain weave or fabric, is used herein to mean 3D weaving with a plurality of weft yarn layers in which the basic weave for each layer is equivalent to a conventional plain type weave, but with certain crosspoints of the weave that interlink the weft yarn layers. FIG. 2 shows a plane of multi-plain fabric in which the warp yarns C.sub.2 are occasionally diverted from their paths in a conventional 2D plane weave associated with a layer CT.sub.2 of weft yarns in order to take hold of a weft yarn T.sub.2 of a neighbouring layer, thereby forming particular plain crosspoints P.sub.T interlinking two adjacent weft yarn layers. At a particular plain crosspoint P.sub.T, the warp yarn the C.sub.2 passes around two weft yarns T.sub.2 situated in the same column in two adjacent weft layers CT.sub.2.

(20) By way of example, the fiber texture of the invention may be made by 3D weaving using a multi-plain weave as shown in FIG. 2 and with warp and weft thread counts of 20 yarns/cm.

(21) The term multi-satin weave or fabric is used herein to mean 3D weaving with a plurality of weft yarn layers in which the basic weave for each layer is equivalent to a conventional satin type weave, but with certain crosspoints of the weave that interlink the weft yarn layers. FIG. 3 shows a plane of a multi-satin fabric in which each warp yarn C.sub.3, with the exception of warp yarns situated at the surface of the texture, is diverted in alternation in one direction and in the other in order to take hold of one weft yarn T.sub.3 out of n of a first weft yarn layer CT.sub.3 and one weft yarn T.sub.3 out of n of a second weft yarn layer CT.sub.3 adjacent to the first, where n is an integer number greater than two, thereby interlinking two layers.

(22) By way of example, the fiber texture of the invention may be made by 3D weaving using a multi-satin weave as shown in FIG. 3 and with warp and weft thread counts of 10 yarns/cm.

(23) The term multi-serge weave or fabric is used herein to mean 3D weaving with a plurality of weft yarn layers in which the basic weave for each layer is equivalent to a conventional serge type weave, but with certain crosspoints of the weave that interlink the weft yarn layers. FIG. 4 shows a plane of a multi-serge fabric in which each warp yarn C.sub.4, with the exception of warp yarns situated at the surface of the texture, is deflected so as to take hold of pairs of weft yarns T.sub.4 of a weft yarn layer CT.sub.4 or of a plurality of adjacent weft yarn layers CT.sub.4.

(24) By way of example, the fiber texture of the invention may be made by 3D weaving using a multi-serge weave as shown in FIG. 4 and with warp and weft thread counts of 8 yarns/cm.

(25) The yarns used for weaving the fiber texture that is to form of the fiber reinforcement of the oxide/oxide composite material part may in particular be made of fibers constituted by any of the following materials: alumina; mullite; silica; an aluminosilicate; a borosilicate; or a mixture of a plurality of these materials.

(26) Once the fiber texture has been made, it is compacted so as to adjust its fiber volume content to a value lying in the range 40% to 51%. Compacting is performed using tooling 100 that is for use in depositing refractory oxide particles within the fiber texture as described below in detail. The texture 10 is compacted by means of a grid 140 that is perforated so as to pass the slip that is used during the following operation. The grid 140 is held pressed against the fiber texture by holder means, e.g. by screws (not shown in FIG. 5), at a position in the tooling 100 that corresponds to the compacting thickness Ec that it is desired to apply to the texture. When there is no expansion of the fiber texture after unmolding (i.e. after impregnating the texture by the SPS technique and then drying it), the final thickness of the part is equal to the compacting thickness Ec.

(27) The fiber volume fraction corresponds to the fraction of the total volume of the texture that is occupied by fibers within that total volume of the texture that is made. By way of example, with a fiber texture presenting the shape of a plane plate, the following parameters are used for calculating the fiber volume fraction:

(28) the length L of the texture;

(29) the width l of the texture;

(30) the thickness e of the texture

(31) the density d of the fibers; and

(32) the weight per unit area Ms of the texture.

(33) Specifically, the fiber volume fraction Tvf is equal to the fiber volume Vf divided by the total volume of the texture. The fiber volume Vf used is equal to the weight of the fibers used, i.e. Ms.Math.L.Math.l, Divided by the density d of the fibers, i.e.: Vf=Ms.Math.L.Math.l/d.

(34) Since the total volume of the fiber structure in the form of a plate is equal to L.Math.l.Math.e, the fiber volume fraction Tvf is calculated using the following formula:
Tvf=Ms/(e.d)(1)

(35) Consequently, when it is desired to obtain a fiber texture presenting a fiber volume fraction with a value lying in the range 40% to 51%, the compacting thickness of the fiber texture is adjusted so that, after compacting, it presents a thickness e that makes it possible to obtain a fiber volume fraction lying in the range 40% to 51%, the compacting thickness being determined as a function of the weight per unit area Ms of the texture and of the fiber density, as specified by formula (1).

(36) Particles of refractory oxide are then deposited within the fiber texture using the well-known technique of submicrometer powder suction (SPS). For this purpose, and as shown in FIG. 5, a fiber texture 10 made using one of the above-described 3D weaves, is placed in an enclosure 110 of tooling 100. A filter 120 is previously interposed between the bottom 111 of the enclosure 110 and the fiber texture 10, the bottom 111 including openings 1110. After placing the texture 10 in the enclosure 110, a slip 130 for forming a refractory oxide matrix in the texture is deposited on the top face of the fiber texture 10, i.e. the face of the texture that is opposite from its face facing the filter 120. The slip 130 corresponds to a suspension containing a submicrometer powder of refractory oxide particles. By way of example, the slip 130 may correspond to an aqueous suspension constituted by alumina powder having a mean particle size (D50) lying in the range 0.1 micrometers (m) to 0.3 m with a volume fraction lying in the range 27% to 42%, the suspension being acidified with nitric acid (pH lying in the range 1.5 to 4). In addition to alumina, the refractory oxide particles constituting the submicrometer powder could equally well be made of a material selected from mullite, silica, an aluminosilicate, and an aluminophosphate. The refractory oxide particles may also be mixed with particles of zirconium, rare earth oxides, or any other filler enabling specific functions to be added to the final material (carbon black, graphite, silicon carbide, etc.).

(37) After closing the enclosure 110 with a cover 112, a gas stream F.sub.1 made up of compressed air or nitrogen is introduced into the enclosure 110 via a duct 1120. The stream F.sub.1 serves to apply a pressure P.sub.1 that forces the slip 130 to penetrate into the texture 10. In combination with inserting the stream F.sub.1, pumping P, e.g. using a primary vacuum pump (not shown in FIG. 5), is performed from the outside of the bottom 111 of the enclosure 110 through the openings 1110 so as to force the slip 130 to migrate through the texture 10. The filter 120 is calibrated to retain the refractory oxide particles that are present in the slip while the liquid of the slip is discharged via the openings 1110. The refractory oxide particles thus become progressively deposited by sedimentation in the texture.

(38) This produces a fiber preform filled with refractory oxide particles, in this example alumina particles of the above-described type. The preform is then dried at a temperature lying in the range 35 C. to 95 C., and is then subjected to sintering heat treatment under air at a temperature lying in the range 1000 C. to 1200 C. in order to sinter the refractory oxide particles together, thereby forming a refractory oxide matrix in the preform. This produces a part made of oxide/oxide composite material having fiber reinforcement obtained by 3D weaving and not including cracks in the blocks of matrix present between the reinforcing yarns.

(39) FIG. 6 is a micro-graph of a section of a part 200 made of prior art oxide/oxide composite material, specifically in this example alumina fiber reinforcement densified by an alumina matrix with the fiber reinforcement 210 being formed by 3D weaving between weft yarn layers 211 and warp yarn layers 212 with an interlock weave, with warp and weft thread counts of 8 yarns/cm, and with a fiber volume fraction of 38%. The part 200 was fabricated in the same manner as that described above, i.e. by the SPS technique followed by drying and sintering of the filled preform. As can be seen in FIG. 6, the weave and the thread count defined for the fiber reinforcement 210 lead to blocks 221 of matrix 220 being formed in the material that present a dimension in at least one direction that is greater than five times the maximum section of the reinforcing yarns, in this example the section of a weft yarn 211. As can be seen in FIG. 6, since the size of the matrix blocks is not limited to less than five times the maximum section, cracks 230 have formed in the material. The presence of cracks 230, some of which even pass through the reinforcing yarns, significantly degrades the mechanical properties of the part 200.

(40) FIGS. 7A, 7B, and 7C are micro-graphs of a section in the warp direction (the long direction of the micro-graphs corresponds to the warp direction, and the high direction of the micro-graphs corresponds to the z direction) respectively of parts 300, 400, and 500 each made out of oxide/oxide composite material of the invention, namely in this example alumina fiber reinforcement densified by an alumina matrix.

(41) In FIG. 7A, the fiber reinforcement 310 of the part 300 in this example was formed by 3D weaving between weft yarn layers 311 and warp yarn layers 312 using a multi-satin weave presenting warp and weft thread counts of 10 yarns/cm and a fiber volume fraction of 43.4%.

(42) In FIG. 7B, the fiber reinforcement 410 of the part 400 in this example was formed by 3D weaving between weft yarn layers 411 and warp yarn layers 412 using an interlock weave presenting a warp thread count of 12 yarns/cm, a weft thread count of 5 yarns/cm, and a fiber volume fraction of 44.8%.

(43) In FIG. 7C, the fiber reinforcement 510 of the part 500 in this example was formed by 3D weaving between weft yarn layers 511 and warp yarn layers 512 using an interlock weave presenting warp and weft thread counts of 12 yarns/cm, and a fiber volume fraction of 43.5%.

(44) The parts 300, 400, and 500 were fabricated in the same manner as that described above, i.e. by the SPS technique followed by drying and sintering of the filled preform.

(45) The weaves, the thread counts, and the fiber volume fractions as defined for the fiber reinforcements 310, 410, and 510 led to respective blocks 321, 421, and 521 of matrix 320, 420, and 520 being formed in the material that present dimensions in all directions that are less than five times the maximum section of the reinforcing yarns. As can be seen in FIGS. 7A, 7B, and 7C, since the matrix blocks are limited in size to less than five times the maximum section of the reinforcing yarns, no cracks are present in the material. Consequently, the parts 300, 400, and 500 present mechanical properties that are much superior to the properties of the part 200.

(46) The table below gives the values obtained in terms of weight per unit area Ms, plate thickness e, density d (alumina fiber), and fiber volume fraction Tvf for the parts of FIGS. 6, 7A, 7B, and 7C.

(47) TABLE-US-00001 Part Texture Ms (g/m.sub.2) e (mm) d TVf Part 200 8/8 6667 4.5 3.9 38 (FIG. 6) interlock Part 300 10/10 5420 3.2 3.9 43.4 (FIG. 7A) multi-satin Part 400 12/5 5420 3.1 3.9 44.8 (FIG. 7B) interlock Part 500 12/12 5770 3.4 3.9 43.5 (FIG. 7C) interlock

(48) It can be seen that the part 200 a FIG. 6 is the only part that presents a fiber volume fraction that does not lie in the range 40% to 51%. It can also be seen that the part 200 is the only part that has cracks in its material as a result of the presence of matrix blocks presenting a dimension in at least one direction that is more than five times the maximum section of the reinforcing yarns.

(49) The method of the present invention enables oxide/oxide composite material parts to be fabricated from a three-dimensionally woven fiber texture and by using the SPS technique, which parts are thoroughly uniform throughout their volume and do not have cracks or pores. These parts in accordance with the invention present the following mechanical properties, measured in monotonic traction, at ambient temperature, and in the warp direction:

(50) modulus of elasticity lying in the range 120 GPa to 170 GPa;

(51) breaking deformation of not less than 0.35%; and

(52) breaking stress greater than 250 MPa.

(53) Although the 3D woven fiber reinforcement yarns of the oxide/oxide material of a part of the invention may be covered in an interphase, the method of the invention makes it possible to make oxide/oxide composite parts with 3D woven fiber reinforcement without interphase on the yarns, and naturally without cracks in the material.