• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a fibrous texture (100) having a strip shape extending in a longitudinal direction (X) over a determined length (Lioo) between a proximal portion (110) and a distal portion (120) and in a direction lateral pattern (Y) over a given width (100) between a first lateral edge (101) and a second lateral edge (102), the fibrous texture having a three-dimensional or multilayer weave between a plurality of layers of warp yarns or strands; extending in the longitudinal direction and a plurality of layers of yarn or weft strands extending in the lateral direction, characterized in that a first portion (P1) of the fibrous texture present between the proximal portion (110) and a portion intermediate of the fibrous texture comprises carbon fiber weft strands or strands and that a second portion (P2) of the fibrous texture present between the intermediate portion and the portion distal comprises threads or strands of fiberglass frame.
    公开号:FR3070402A1
    申请号:FR1757977
    申请日:2017-08-30
    公开日:2019-03-01
    发明作者:Son Le Hong；Dominique Marie Christian Coupe；Martin Gabillon；Herve Grelin；Jean Noel Mahieu；Sylvain Moussillat；Jose Yann Mortier Roland；Frederic Raymond
    申请人:Safran Aircraft Engines SAS；
    IPC主号:
    专利说明:

    The present invention relates to a method for manufacturing a fibrous texture which can be used, in particular but not exclusively, to form the fibrous reinforcement of an aeronautical engine fan casing made of composite material.
    Invention background
    The manufacture of a composite material casing begins with the production of a fibrous texture in the form of a strip, the fibrous texture being produced by three-dimensional weaving between a plurality of layers of warp threads and a plurality of layers of weft threads. The fibrous texture thus obtained is wound over several turns on a mold or tool having the shape of the casing to be produced and maintained between the mold and segments forming a counter-mold so as to obtain a fibrous preform.
    Once the fibrous preform has been made, that is to say at the end of the winding of the fibrous texture, the tool carrying the fibrous preform is closed by counter molds and then transported to an oven or oven in wherein the densification of the preform by a matrix is carried out, the matrix being able in particular to be obtained by injection and polymerization of a resin in the fibrous preform.
    The crankcases must provide a retention function by retaining debris ingested inside the engine, or the blades or blade fragments projected by centrifugation, in order to prevent them from crossing the crankcase and reaching other parts of the aircraft.
    The casings of the prior art generally perform this function satisfactorily. However, it remains possible to further improve the mechanical resistance of certain casings on impact with a blade, when there is detachment of the latter and projection thereof on the housing.
    Subject and summary of the invention
    The invention relates, according to a first aspect, to a fibrous texture having a form of strip extending in a longitudinal direction over a determined length between a proximal part and a distal part and in a lateral direction over a determined width between a first edge lateral and a second lateral edge, the fibrous texture having a three-dimensional or multilayer weaving between a plurality of layers of warp threads or strands extending in the longitudinal direction and a plurality of layers of weft threads or strands extending in the lateral direction, characterized in that a first portion of the fibrous texture present between the proximal part and an intermediate portion of the fibrous texture comprises threads or strands of carbon fiber weft and in that a second portion of the texture fibrous present between the intermediate part and the distal part comprises weft threads or strands of e glass.
    The fibrous texture is intended to be wound in several turns in order to form a fibrous reinforcement of the casing of composite material. The first portion is intended to form the radially internal part of this fibrous reinforcement (first turns of the winding). The second portion is intended to form the radially external part of this fibrous reinforcement (last turns of the winding).
    The inventors have found that it is possible to improve the resistance of the casing to impact with a detached blade by imparting significant rigidity to the first turns of the fibrous reinforcement of this casing, and a deformable character to the last turns of this reinforcement, these latter turns being in fact the most stressed in deformation during impact.
    Thus, the fibrous texture according to the invention comprises carbon weft threads or strands in the first portion, intended to form the start of the winding and situated on the side of the impact with the blade, in order to impart rigidity. raised to this first serving. In addition, the fibrous texture according to the invention comprises son or strands of glass weft in the second portion, which is intended to form the outer layer or layers of the winding, in order to impart a significant elastic deformation capacity to this second portion, and thus being able to absorb the energy communicated by the dawn by deforming then being able to restore this energy at dawn by returning to its initial shape.
    The invention is therefore based on the use of two different materials, namely carbon and glass, located in particular areas of the fibrous reinforcement, in order to respond, in an optimal manner, to the stresses of the casing during an event of loss of dawn while limiting the mass of the latter.
    In an exemplary embodiment, the son or strands of glass fiber weft in the second portion are present on the side of an external face of the texture.
    The external face is intended to form the radially external face of the fibrous texture, once the latter is wound up to form the fibrous reinforcement of the casing.
    The inventors have found that, within a given turn of the winding, the part of the texture situated on the side of the external face was the most stressed in deformation upon impact with a detached blade.
    Thus, the fact of positioning the son or strands of glass weft on the side of this external face makes it possible to further improve the resistance of the casing to the deformation imposed upon impact with a detached blade.
    In an exemplary embodiment, only part of the weft threads or strands of the second portion are made of glass fibers, the other weft threads or strands of the second portion being made of carbon fibers.
    Having in the second portion a mixed presence of son or strands of glass weft and son or strands of carbon weft advantageously further improves the resistance of the housing to impact with a detached blade.
    In an exemplary embodiment, the fibrous texture further comprises yarns or strands of warp in glass fibers present on the side of an external face of the fibrous texture, the other yarns or strands of warp of the fibrous texture being in fibers of carbon.
    Adding wires or strands of glass chain makes it possible to further improve the resistance of the casing to the deformation imposed upon impact with a detached blade. The glass chain wires or strands are here located on the side of the external face which constitutes a region subjected to deformation, and the rest of the chain wires or strands is made of carbon. This makes it possible to further improve the deformability while maintaining a satisfactory level of rigidity in the fibrous reinforcement.
    In particular, the son or strands of glass fiber warp may be present in a central zone in the lateral direction situated behind the first and second lateral edges and which extends over a determined width less than the width of said fibrous texture. .
    The central zone is intended to be present opposite the blades and defines the retention zone of the casing to be obtained. The purpose of this crankcase retention zone is to retain debris, particles or objects ingested at the engine inlet, or the blades or blade fragments detached and projected radially by centrifugation against the crankcase.
    The son or strands of glass chain are in the latter case located in a region highly stressed in deformation, i.e. on the side of the outer face and in the central zone, and the rest of the son or strands of chain are made of carbon. This makes it possible to further improve the deformability while maintaining a satisfactory level of rigidity in the fibrous reinforcement.
    In an exemplary embodiment, the son or strands of carbon fibers and the son or strands of glass fibers present in the fibrous texture have a similar titer.
    Such a characteristic is advantageous because by using in the texture of strands or strands of similar size, the textile architecture is not significantly modified, which makes it possible to maintain a similar shrinking and of similar matrix pocket sizes in the composite casing. .
    The invention also relates to a fibrous aeronautical casing preform comprising a winding over several turns of a fibrous texture as described above, the first portion being located on the side of a radially internal face of the preform, and the second portion being located on the side of a radially outer face of the preform.
    The invention also relates to a gas turbine casing made of a composite material, comprising a fibrous reinforcement constituted by a fibrous preform as described above, and a matrix densifying the fibrous reinforcement.
    In an exemplary embodiment, said casing is a gas turbine fan casing.
    The invention also relates to an aeronautical gas turbine engine having a casing as described above.
    Brief description of the drawings
    Other characteristics and advantages of the invention will emerge from the following description, given without limitation, with reference to the appended drawings, in which:
    FIG. 1 is a schematic perspective view of a loom showing the three-dimensional weaving of a fibrous texture,
    FIG. 2 is a schematic perspective view of a fibrous texture in accordance with an embodiment of the invention,
    FIG. 3 is a cross section taken at the level of the first portion of the fibrous texture of FIG. 2 and showing a plane of weaving weave,
    FIG. 4 is a cross section taken at the level of the second portion of the fibrous texture of FIG. 2 and showing a plane of weaving weave,
    FIG. 5 is a schematic perspective view showing the winding of a fibrous texture on a shaping tool,
    FIG. 6 is a half view in axial section of a casing preform obtained by winding a fibrous texture as shown in FIG. 5,
    FIG. 7 is a sectional view showing the positioning of injection sectors on the preform of the casing of FIG. 6,
    FIG. 8 is a perspective view of an aeronautical engine in accordance with an embodiment of the invention,
    FIG. 9 is a cross-section taken at the level of the first portion of a variant of fibrous texture according to the invention and showing a plane of weaving weave, and
    - Figure 10 is a cross section taken at the second portion of this variant of fibrous texture and showing a weaving weave plane.
    Detailed description of embodiments
    The invention applies generally to fibrous textures intended for the manufacture of housings made of composite material, these housings comprising a barrel or a ferrule with annular flanges at their ends.
    As shown in FIG. 1, a fibrous texture 100 is produced in a known manner by weaving by means of a jacquard type loom 5 on which a bundle of warp threads or strands 20 has been placed in a plurality of layers, the warp threads being linked by weft threads or strands 30.
    The fibrous texture is produced by three-dimensional weaving. By "three-dimensional weaving" or "3D weaving" is meant here a weaving mode by which at least some of the weft threads link warp threads on several layers of warp threads or vice versa. The fibrous texture may have interlock weaving weave. By “interlock” weaving is meant here a weaving weave in which each layer of weft threads binds several layers of warp thread, with all the threads of the same weft column having the same movement in the plane of the armor. Other weaving weaves are possible.
    As illustrated in FIG. 2, the fibrous texture 100 has the shape of a strip which extends in length in a longitudinal direction X corresponding to the running direction of the warp threads or strands 20 and in width or transversely in a lateral direction Y between first and second lateral edges 101 and 102, the lateral direction Y corresponding to the direction of the wefts or strands
    30. The fibrous texture extends longitudinally over a determined length Lioo in the direction X between a proximal part 110 intended to form the beginning of the winding of a fibrous preform on a shaping tool and a distal part 120 intended to form the end of the winding of the fibrous preform.
    The fibrous texture also has a central zone 130 extending over a determined width 130 in the direction Y, the central zone 130 being intended to form the barrel or the shell of the casing. The central zone 130 is intended to be present opposite the blades and defines the retention zone of the casing to be obtained. The central zone 130 is set back from the first 101 and second 102 lateral edges and extends over a determined width Ibo less than the width Iwo of the texture 100. The central zone 130 is at an intermediate position between the first and second edges lateral 101 and 102. The central zone 130 is delimited between two lateral zones 140 and 150 each extending over a determined width, respectively Ii4o and liso, in the direction Y. The first lateral zone 140 extends between the first lateral edge 101 and the central zone 130. The second lateral zone 150 extends between the second lateral edge 102 and the central zone 130. Each of the lateral zones 140 and 150 is intended at least in part to form an annular flange of the casing.
    The length Lioo of the fibrous texture 100 is determined as a function of the circumference of the tooling or of the shaping mold so as to allow the production of a determined number of turns of the fibrous texture, for example four turns.
    The fibrous texture 100 comprises a first portion PI present between the proximal part 110 and an intermediate part PI of the fibrous texture (the intermediate part PI is visible in FIG. 7). The first portion PI is intended to form the first part of the winding forming the fibrous reinforcement of the casing (radially internal part of this winding, see FIG. 7 which shows the radial direction R). The intermediate part PI can be located at mid-length of the fibrous texture 100, or more generally between a quarter and three-quarter of the length of the fibrous texture 100, for example.
    The fibrous texture 100 further comprises a second portion P2, distinct from the first portion PI, and present between the intermediate portion PI and the distal portion 120. The second portion P2 is intended to form the second portion of the winding forming the reinforcement fibrous casing (radially outer part of this winding).
    FIGS. 3 and 4 each illustrate a plane of the interlock weaving weave of the fibrous texture 100 located respectively at the level of the first portion PI and of the second portion P2.
    The examples of armor planes illustrated in FIGS. 3 and 4 include 7 layers of weft and 8 layers of warp. In the interlock weave illustrated, a warp layer is formed by two adjacent warp half-layers offset from each other in the weft direction. There are therefore 16 half-layers of chain positioned in staggered rows. Each weft layer links 3 half layers of warp. One could also adopt a non-staggered arrangement, the warp threads of two adjacent chain layers being aligned on the same columns. Interlock type weaving weaves that can be used are described in document WO 2006/136755.
    As illustrated in FIG. 3, the first portion PI includes weft wires or strands of carbon fibers, denoted Te. All of the wefts or weft strands of the first portion PI may be made of carbon fibers.
    In the example illustrated, the fibrous texture comprises son or strands of chain of glass fibers, denoted Cv, as well as son or strands of chain of carbon fibers, denoted Ce.
    The son or strands of glass fiber chain Cv are present on the side of the external face F1 of the fibrous texture. This external face F1 is intended to form the radially external face of the fibrous preform, once the texture has been rolled up (see FIG. 7). In particular, son or strands of glass fiber chain Cv are present on the external face F1 of the fibrous texture. The son or strands of glass fiber chain Cv may be present at least in the central zone 130, which is the most mechanically stressed upon impact with a detached blade, in order to give this zone optimum deformability. The son or strands of Cv glass fiber chain may be present only in this central zone 130. As a variant, the son or strands of Cv glass fiber chain may be present in the central zone 130 and in the lateral zones 140 and 150.
    In the example illustrated, the other warp threads or strands of the fibrous texture are made of carbon fibers, and denoted Ce. These carbon fiber warp threads or strands These are, in particular, present on the side of the internal face F2 of the fibrous texture. This internal face F2 is intended to form the radially internal face of the fibrous preform, once the texture has been rolled up (see FIG. 7). In particular, carbon fiber warp threads or strands Ce are present on the internal face F2 of the fibrous texture. In this example, carbon fiber warp threads or strands are also present in the lateral zones 140 and 150.
    As illustrated in FIG. 4, the second portion P2 comprises weft son or strands of glass fibers, denoted Tv, and weft son or strands of carbon fibers Te. Thus, in the example illustrated, only part of the weft threads or strands of the second portion P2 are made of glass fibers, the other weft threads or strands of the second portion P2 being here made of carbon fibers. It is not, however, outside the scope of the invention when all the wefts or weft strands of the second portion are made of glass fibers. The glass fiber weft strands or strands Tv are present on the side of the external face F1 of the fibrous texture. In particular, weft threads or strands of glass fibers Tv are present on the external face F1 of the fibrous texture. The weft yarns or strands of carbon fibers Te are, in particular, present on the side of the internal face F2 of the fibrous texture.
    There is therefore an evolution in the nature of the wefts or strands when we move along the longitudinal direction X of the fibrous texture 100.
    We have just described an example in which the fibrous texture has an interlock weaving weave with 7 layers of weft and 8 layers of warp. It is not, however, outside the scope of the invention when the number of weft and warp layers is different, or when the fibrous texture has a weaving weave different from an interlock weave.
    As mentioned above, it is also advantageous for the carbon fiber wires or strands and the glass fiber wires or strands present in the fibrous texture to have a similar count. The | T2-T1 | / Tl may, for example, be less than or equal to 10%, where Tl designates the title of the carbon fiber wires or strands, T2 designates the title of the glass fiber wires or strands, and |. | denotes the absolute value.
    As illustrated in FIG. 5, a fibrous casing reinforcement is formed by winding on a mandrel 50 of the fibrous texture 100 described above, the fibrous reinforcement constituting a tubular fibrous preform complete with a casing forming a single piece. To this end, the mandrel 50 has an external surface 51 whose profile corresponds to the internal surface of the casing to be produced. The mandrel 50 also includes two flanges 52 and 53 to form parts of the fiber preform 62 and 63 corresponding to the flanges of the casing (the flanges 62 and 63 are visible in FIG. 6). The tower or towers located radially inward of the preform correspond to the first portion PI of the fibrous texture and the tower or towers located radially outward of the preform correspond to the second portion P2 of the fibrous texture.
    FIG. 6 shows a sectional view of the fibrous preform 60 obtained after winding of the fibrous texture 100 in several layers on the mandrel 50. The number of layers or turns depends on the desired thickness and the thickness of the texture fibrous. It is preferably at least equal to 2. In the example described here, the preform 60 comprises 4 layers of fibrous texture 100.
    Next, the fibrous preform 60 is densified by a matrix.
    The densification of the fibrous preform consists in filling the porosity of the preform, in all or part of the volume thereof, with the material constituting the matrix.
    The matrix can be obtained in a manner known per se according to the liquid method. The liquid method consists in impregnating the preform with a liquid composition containing an organic precursor of the matrix material. The organic precursor is usually in the form of a polymer, such as a resin, optionally diluted in a solvent. The fibrous preform is placed in a mold which can be sealed with a housing having the shape of the final molded part. As illustrated in FIG. 7, the fibrous preform 60 is here placed between a plurality of sectors 54 forming a counter mold and the mandrel 50 forming a support, these elements having respectively the external shape and the internal shape of the casing to be produced. Then, the liquid matrix precursor, for example a resin, is injected into the entire housing to impregnate the preform.
    The transformation of the precursor into an organic matrix, namely its polymerization, is carried out by heat treatment, generally by heating the mold, after elimination of the possible solvent and crosslinking of the polymer, the preform always being maintained in the mold having a shape corresponding to that of the part to be produced. The organic matrix can in particular be obtained from epoxy resins, such as, for example, the high performance epoxy resin sold, or liquid precursors of carbon or ceramic matrices.
    In the case of the formation of a carbon or ceramic matrix, the heat treatment consists in pyrolyzing the organic precursor in order to transform the organic matrix into a carbon or ceramic matrix according to the precursor used and the pyrolysis conditions. For example, liquid carbon precursors can be relatively high coke resins, such as phenolic resins, while liquid ceramic precursors, in particular SiC, can be polycarbosilane (PCS) resins or polytitanocarbosilane (PTCS) or polysilazane (PSZ). Several consecutive cycles, from impregnation to heat treatment, can be performed to achieve the desired degree of densification.
    The densification of the fiber preform can be carried out by the well-known transfer molding process called RTM ("Resin Transfer Molding"). In accordance with the RTM process, the fibrous preform is placed in a mold having the shape of the casing to be produced. A thermosetting resin is injected into the internal space defined between the piece of rigid material and the mold and which comprises the fibrous preform. A pressure gradient is generally established in this internal space between the place where the resin is injected and the evacuation orifices of the latter in order to control and optimize the impregnation of the preform by the resin.
    The resin used can be, for example, an epoxy resin. Resins suitable for RTM processes are well known. They preferably have a low viscosity to facilitate their injection into the fibers. The choice of the temperature class and / or the chemical nature of the resin is determined according to the thermomechanical stresses to which the part must be subjected. Once the resin has been injected into all of the reinforcement, it is polymerized by heat treatment in accordance with the RTM process.
    After injection and polymerization, the part is removed from the mold. The part is finally cut out to remove the excess resin and the chamfers are machined to obtain a casing 810 having a shape of revolution as illustrated in FIG. 8.
    The casing 810 shown in FIG. 8 is a casing of an aeronautical engine fan with a gas turbine 80. Such an engine, as shown very diagrammatically in FIG. 8, comprises, from upstream to downstream in the direction of the flow of gas flow, a blower 81 disposed at the inlet of the engine, a compressor 82, a combustion chamber 83, a high-pressure turbine 84 and a low-pressure turbine 85. The engine is housed inside a housing comprising several parts corresponding to different elements of the engine. Thus, the fan 81 is surrounded by the casing 810.
    FIGS. 9 and 10 show a variant of fibrous texture according to the invention, in which all of the wires or strands of chain are made of carbon (wires or strands of chain Ce).
    The fibrous texture comprises in its second portion P2 wires or strands of weft Tv made of glass, these latter are situated on the side of the external face F1 of the texture as in the embodiment described above. According to this illustrated example, the fibrous texture further comprises carbon weft threads or strands Te in the first portion PI and in the second portion P2. All the wefts or weft strands of the first portion PI are made of carbon, according to this example.
    权利要求:
    Claims (10)
    [1" id="c-fr-0001]
    1. Fibrous texture (100) having a stripe shape extending in a longitudinal direction (X) over a determined length (Lioo) between a proximal part (110) and a distal part (120) and in a lateral direction (Y ) over a determined width (lioo) between a first lateral edge (101) and a second lateral edge (102), the fibrous texture having a three-dimensional or multilayer weaving between a plurality of layers of warp threads or strands (20) s' extending in the longitudinal direction and a plurality of layers of weft threads or strands (30) extending in the lateral direction, characterized in that a first portion (PI) of the fibrous texture present between the proximal part (110) and an intermediate part (PI) of the fibrous texture comprises wefts or wefts (Te) made of carbon fibers and in that a second portion (P2) of the fibrous texture present between the intermediate part and the distal part comp all wefts or weft strands (Tv) made of glass fibers.
    [2" id="c-fr-0002]
    2. A fibrous texture (100) according to claim 1, in which the wefts or strands of weft (Tv) made of glass fibers in the second portion (P2) are present on the side of an external face (Fl) of the texture.
    [3" id="c-fr-0003]
    3. A fibrous texture (100) according to claim 1 or 2, in which only part of the weft threads or strands of the second portion (P2) are made of glass fibers, the other weft threads or strands of the second portion being carbon fiber.
    [4" id="c-fr-0004]
    4. fibrous texture (100) according to any one of claims 1 to 3, further comprising son or strands of chain (Cv) in glass fibers present on the side of an external face (Fl) of the texture, the other yarns or strands of warp of fibrous texture being made of carbon fibers.
    [5" id="c-fr-0005]
    5. A fibrous texture (100) according to claim 4, in which the son or strands of chain (Cv) made of glass fibers are present in a central zone (130) in the lateral direction situated behind the first and second lateral edges ( 101; 102) and which extends over a determined width (li 3 o) less than the width (lioo) of said fibrous texture.
    [6" id="c-fr-0006]
    6. Fibrous texture (100) according to any one of claims 1 to 5, in which the wires or strands (Ce; Te) of carbon fibers and the wires or strands (Cv; Tv) of glass fibers present in the fibrous texture have a similar title.
    [7" id="c-fr-0007]
    7. fibrous preform (60) of an aeronautical casing (810) comprising a winding over several turns of a fibrous texture (100) according to any one of claims 1 to 6, the first portion (PI) being located on the side of a radially internal face (F2) of the preform, and the second portion (P2) being located on the side of a radially external face (Fl) of the preform.
    [8" id="c-fr-0008]
    8. Carter (810) of a gas turbine made of a composite material, comprising a fibrous reinforcement constituted by a fibrous preform (60) according to claim 7, and a matrix densifying the fibrous reinforcement.
    [9" id="c-fr-0009]
    9. A housing (810) according to claim 8, wherein said housing is a gas turbine fan housing.
    [10" id="c-fr-0010]
    10. Aeronautical gas turbine engine (80) having a casing (810) according to claim 8 or 9.
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    同族专利:
    公开号 | 公开日
    FR3070402B1|2020-08-28|
    BR112020003874A2|2020-09-24|
    JP2020533494A|2020-11-19|
    CN111051585B|2022-01-28|
    EP3676431A1|2020-07-08|
    CA3073795A1|2019-03-07|
    US11230798B2|2022-01-25|
    WO2019043333A1|2019-03-07|
    US20200190711A1|2020-06-18|
    RU2020111479A3|2021-11-15|
    CN111051585A|2020-04-21|
    RU2020111479A|2021-09-30|
    EP3676431B1|2021-07-14|
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    FR3070402B1|2017-08-30|2020-08-28|Safran Aircraft Engines|WOVEN FIBROUS TEXTURE FOR THE FORMATION OF A CRANKCASE PREFORM|FR3070402B1|2017-08-30|2020-08-28|Safran Aircraft Engines|WOVEN FIBROUS TEXTURE FOR THE FORMATION OF A CRANKCASE PREFORM|
    CN112680864A|2020-12-11|2021-04-20|江苏恒力化纤股份有限公司|Fabric-enhanced rearview mirror and preparation method thereof|
    法律状态:
    2019-03-01| PLSC| Publication of the preliminary search report|Effective date: 20190301 |
    2019-07-22| PLFP| Fee payment|Year of fee payment: 3 |
    2020-07-21| PLFP| Fee payment|Year of fee payment: 4 |
    2021-07-22| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1757977|2017-08-30|
    FR1757977A|FR3070402B1|2017-08-30|2017-08-30|WOVEN FIBROUS TEXTURE FOR THE FORMATION OF A CRANKCASE PREFORM|FR1757977A| FR3070402B1|2017-08-30|2017-08-30|WOVEN FIBROUS TEXTURE FOR THE FORMATION OF A CRANKCASE PREFORM|
    RU2020111479A| RU2020111479A3|2017-08-30|2018-08-29|
    CN201880056793.5A| CN111051585B|2017-08-30|2018-08-29|Woven fiber structure for forming shell preform|
    PCT/FR2018/052117| WO2019043333A1|2017-08-30|2018-08-29|Woven fibrous structure for forming a casing preform|
    JP2020512613A| JP2020533494A|2017-08-30|2018-08-29|Woven fiber structure for forming casing preforms|
    EP18773796.0A| EP3676431B1|2017-08-30|2018-08-29|Woven fibrous structure for forming a casing preform|
    BR112020003874-1A| BR112020003874A2|2017-08-30|2018-08-29|fibrous structure, fibrous preform, gas turbine engine housing, and aircraft gas turbine engine.|
    CA3073795A| CA3073795A1|2017-08-30|2018-08-29|Woven fibrous structure for forming a casing preform|
    US16/642,767| US11230798B2|2017-08-30|2018-08-29|Woven fibrous structure for forming a casing preform|
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