• 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 preform for curved composite stiffener for axisymmetric part such as a ferrule, comprising at least one core (5) and at least one sole (7, 9) curved around an axis of revolution (22) of said preform and defining a section substantially shaped "T" or "I normal profile". The preform according to the invention is remarkable in that: the core (5) comprises a plurality of warp threads (21) oriented circumferentially with respect to the axis of revolution (22) of the preform, and a plurality of weft yarns (23) oriented radially with respect to said axis, the sole (7, 9) comprises a plurality of warp threads (21) circumferentially oriented with respect to the axis of revolution (22) of the preform, and a plurality of weft yarns (23) substantially parallel to said axis.
    公开号:FR3025529A1
    申请号:FR1458493
    申请日:2014-09-10
    公开日:2016-03-11
    发明作者:Benjamin Provost；Julien Lorrillard；Bertrand Desjoyeaux；Michel Rognant
    申请人:Aircelle SA；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a preform for curved composite stiffener, a stiffener obtained with such a preform and an axisymmetrical part comprising such a stiffener, a method of manufacturing this preform and a mandrel adapted to implement said method.
    [0002] In order to produce resistant and light structural elements, in particular for the aeronautical field, it is known to prepare a dry fabric preform comprising, for example, carbon fibers, which is impregnated with a resin, in particular by a method of injection called "RTM" (Resin Transfer Molding). Thus, after curing to polymerize the resin, an element 10 is obtained comprising fibers whose density and orientation are adjusted locally, in order to obtain mechanical strength characteristics adapted to the forces applied to this part. In particular, using this technique, it is possible to produce a self-stiffened skin-shaped panel curved about an axis such as an axisymmetrical shell 15 or an axisymmetric shell sector, comprising at least one at least partially circumferential stiffener giving the rigidity to this skin: such skin can be used in particular in the manufacture of an aircraft engine nacelle. In some cases, the stiffening function is provided by an element having a constant cross-section substantially in the shape of "T", "n" (Pi) or "normal profile" (denoted by the acronym " IPN "), comprising a core (the vertical part of the T, Pi or IPN) and a sole (the extended base of the section of the T, Pi or IPN). For the realization of the assembly formed by the curved skin to stiffen and the stiffener, it is known to separately make the skin and the stiffener which are pre-cooked, then assembled by a mechanical connection or a bonding. Various methods of manufacturing curved stiffeners are known from the prior art. From the prior art, there is known a method of draping flat fabric coupons, which consists of draping the flattened folds of flat fabrics into the shape of the stiffener. However, this operation requires a large workforce, which results in draping time and significant manufacturing costs. In addition, many fabric coupons are needed, and the orientation of the fibers is not optimized. It is also known to drape shaped fabric coupons. This method consists in depositing on the sole of the panel tissue coupons made in shape defining the core. The advantage of this method is the good control of the orientation of the fibers, but the panel obtained is mechanically weak due to the assembly of the different preforms which generate discontinuities in the fibrous reinforcement. International application WO 2005/082605 also discloses a process for cracking and stretching the fiber. This process consists of making a preform having the section of the final geometry and then breaking the fiber and stretching some parts of this preform to give it a curved shape. However, neither the cracking process of the fiber nor the process of drawing the preform to give it its curved shape can be uniform over the entire woven preform. Also, breaking the continuity of the carbon fiber greatly weakens the mechanical properties of the fabricated part. International application WO 2013/088040 discloses a 3D weaving process by which a three-dimensional preform with localized loosening zones is obtained, allowing the preform to be unfolded in order to give it its "T" shaped section, " Pi "or" IPN "). These preforms nevertheless have the disadvantage of being straight and not being able to conform to a curvature. The present invention is intended to avoid these disadvantages of the prior art. The object of the present invention is to provide a dry curved textile preform with a "T", "Pi" or "IPN" shaped section, inexpensive to manufacture and optimized with respect to the stresses to which it is intended to to be subject. It proposes for this purpose a curved composite stiffener preform for axisymmetric part such as a ferrule, comprising at least one core and at least one sole curved about an axis of revolution of said preform and defining a substantially shaped section. "T" or "1 normal profile", said preform being remarkable in that: - the core comprises a plurality of warp threads oriented circumferentially with respect to the axis of revolution of the preform, and a plurality of 30 weft yarns oriented radially with respect to said axis, the soleplate comprises a plurality of warp yarns oriented circumferentially with respect to the axis of revolution of the preform, and a plurality of weft yarns substantially parallel to said axis. An advantage of this woven preform is that in a single operation, easily industrializable and fast, a continuous weaving of the core and the sole of the preform is obtained, which are then positioned on a tool with geometry 3025529 3 of the final piece including a retaining device in the form of the core of the stiffener such as a tool with a core or counter-shape and bladder, foam shape, etc., then impregnated with a resin, in order to constitute after cooking a very homogeneous whole.
    [0003] In the same way, the stiffener preform obtained can be directly injected with resin and then integrated into the support to which it must be assembled, which makes it possible to limit the number of handling of the preform, and consequently to optimize the cost and efficiency of the preform. manufacturing time of the axisymmetric part. According to one characteristic of the preform according to the invention, the core 10 comprises a zone for bonding layers of warp threads to one another by means of weft threads, and said at least one sole comprises at least one layer unwinding zone. of warp threads. Furthermore, the warp yarns of the sole of the preform have identical lengths, and the warp threads of the core of the preform have distinct lengths. The invention also relates to: a curved composite stiffener for axisymmetric part such as a shell, comprising at least one preform according to the invention; an axisymmetrical part such as a ferrule, reinforced by at least one stiffener according to the invention. The invention also relates to a method of manufacturing a curved composite stiffener preform for an axisymmetric component such as a ferrule, said preform having at least one core and at least one sole and defining a substantially T-shaped section or from "1 to normal profile", said method being remarkable in that said preform is made by a weaving method in the form of contour type, and in that it comprises the following steps aimed at: - calling the warp yarns directly at the output of a loom on a mandrel having at least one conical portion and at least one conical or cylindrical portion; inserting weft threads so as to define at least one tying zone and at least one unfolding zone of the warp son layers; - Unfolding the preform obtained to obtain said soul and said at least one sole. Thus, by providing for the use of a contour-shaped weave method for making a "T" or "IPN" stiffener preform, the preform is given the desired curvature directly at the output of the loom.
    [0004] In addition, a preform is obtained having a core and a sole intimately connected without having to bring the soul on the sole, which gives the piece obtained excellent mechanical properties, superior to those obtained by the processes. manufacturing known from the prior art.
    [0005] An advantage of this woven preform is that in a single operation which can be easily industrialized and rapidly obtained, a continuous weaving of the core and the sole of the preform which are then positioned on a tool with a geometry of the final piece including the retaining device in the form of the core of the stiffener, such as a tool with a core or against a form and a bladder, forms a foam, etc., and then impregnated with a resin, in order to constitute after cooking a very homogeneous whole. In the same way, the stiffener preform obtained can be directly injected with resin and then integrated into the support to which it must be assembled, which makes it possible to limit the number of handling of the preform, and consequently to optimize the cost and efficiency of the preform. manufacturing time of the axisymmetric part. The invention also relates to a mandrel adapted to implement the manufacturing method according to the invention, remarkable in that it has a non-rectilinear generator.
    [0006] In addition, the call mandrel according to the invention comprises at least one conical portion and at least one conical or cylindrical portion. Other features, objects and advantages of the present invention will appear on reading the following description and on examining the appended figures, in which: FIGS. 1a and 1b illustrate two stiffeners obtained by the method manufacturing the preform according to the invention, respectively having a section in the form of "T" and shaped "1 normal profile"; FIG. 2 shows the preform being woven by the manufacturing method according to the invention; FIG. 3 is a detailed view of FIG. 2 which illustrates a preform with a "normal profile" type section during manufacture; - Figure 4 shows a section of the preform of Figure 3 at the output of the craft; - Figure 5 illustrates a section of the preform of Figure 4, in the unfolded position; Figure 6 is a partial isometric view of the preform shown in Figure 5; - Figure 7 shows schematically the stiffener obtained by the preform with a section in the form of "1 normal profile"; FIGS. 8 to 10 are figures similar to FIGS. 3, 6 and 7, the illustrated preform having a section in the form of a "T", the core of the preform being situated inside the soleplate; - Figures 11 to 13 are similar to Figures 8 to 10, the core of the preform section "T" being located outside the sole; FIG. 14 illustrates a manufacturing variant of a preform with a "T" -shaped section, the core of the preform being situated outside the soleplate; - Figure 15 is a view similar to Figure 14, the core of the preform being located inside the sole; Figures 16 to 22 show schematically variants of weaving of the preform "1 normal profile"; - Figures 23 to 25 illustrate another alternative embodiment of the preform.
    [0007] Throughout the figures, identical or similar references represent identical or similar members or sets of members. In the present application, an axisymmetrical part supporting a stiffener is understood to mean any part whose three-dimensional geometric definition concerned with the stiffener and its integration with the part can be defined by a 2D section contained in a plane, and by an axis contained in this section. plane and not intercepting said 2D section, around which the 2D section is rotated to obtain, according to a given angular sector, an axisymmetrical ferrule sector, or a complete ferrule in the case where the angular sector has an angle of 360 ° .
    [0008] Referring to Figure la representing a stiffener 1 obtained by the method according to the invention, having substantially a section in the form of "T", bent around an axis. The weaving method according to the invention uses a contour-like weaving method known from the prior art, which process consists in winding the fibrous preform during weaving directly at the output of the loom onto a cylinder. called rotary call chuck.
    [0009] In the example shown, the stiffener has a flange 3 comprising two parts 3a, 3b, interconnected by a web 5 of the stiffener 1. In FIG. 1b, the stiffener 1 has substantially a cross-section of "1 to normal profile ", that is to say that the stiffener has two flanges 7, 5 9, each of the flanges comprising two parts 7a, 7b and 9a, 9b, interconnected by a core 5. Figure 2 shows a loom weaving machine 11 which continuously produces the preform, conforming to a mandrel 13 for the manufacture of a preform with a section of "normal profile" 1.
    [0010] As can be seen in more detail in FIG. 3, illustrating the preform being woven on the mandrel 13, the mandrel 13 according to the invention has a first cylindrical portion 15, a second conical portion 17 and a third cylindrical portion. 19, of greater diameter than the first cylindrical portion 15. Thus, the mandrel 13 according to the invention has a non-rectilinear generatrix 15, which may have inflection points. This particular geometry of the call mandrel 13 makes it possible not to consume the warp son in a uniform manner. Indeed, the amount of warp son called on the mandrel is a function of the relevant section of the mandrel call. The larger the cross-section of a mandrel portion, the greater the number of warp threads that will be called when the mandrel rotates. In other words, the points of a generator of the mandrel farthest from the axis of revolution of the mandrel call each rotation of the mandrel a greater amount of warp son relative to the points of said generator which are closer to the axis of revolution of the chuck. The first and third portions 15 and 19, cylindrical, have a profile for making the two flanges 7 and 9 of the preform. The second portion 17, conical, has a profile for making the core 5 of the preform according to the desired curvature. According to the invention, the loom continuously supplies directly-called warp yarns on the mandrel 13 located directly at the exit of the loom 30. Weft threads are inserted between the warp yarns as and when the warp threads advance by being called on the mandrel by the contour-shaped weaving method, in a weaving pattern for defining tying zones and warp layer dewaxing zones, as shown in FIG. Figure 4 to which reference is made here.
    [0011] As shown in this figure, two layers 18, 20 of warp 21 from the loom are directly called by the mandrel, and weft yarns 23 are inserted between the warp yarns as and when call the warp threads on the mandrel, so as to define a binding zone 25 of the warp son layers 21 between them by the weft yarns 23 and two deliage zones 27, 29 of the warp son layers. For a better understanding of the invention, these bonding and untightening zones 27, 29 are shown in FIG. 3 illustrating the preform being weaved on the mandrel 13.
    [0012] The binding zones 25 constitute, once the preform has been unfolded, shown in FIG. 5, the core 5 of the preform, whereas the loosening zones 27, 29 respectively form, once the preform has been unfolded, the two soles 7. and 9 of the preform, each comprising the two parts 7a, 7b and 9a, 9b. With reference to FIG. 6, it will be noted that the preform according to the invention obtained by contour-shaped weave is advantageously curved, directly at the output of the loom, thanks to the call mandrel. The core 5 of the preform comprises a plurality of warp yarns 21 circumferentially oriented with respect to an axis of revolution 22 of the preform, and a plurality of weft yarns 23 oriented radially with respect to said axis. The flanges 7 and 9 comprise for their part a plurality of warp threads oriented circumferentially with respect to the axis of revolution 22 of the preform, and a plurality of weft threads 23 parallel to said axis of revolution. These particular orientations of the weft threads and the warp threads of the web and the soles of the preform are obtained thanks to the non-rectilinear generatrix of the call mandrel, which makes it possible to produce a preform according to the invention having different lengths of warp threads in the core area and in the sole area. As shown in FIG. 6, the warp yarns 21 which constitute the soleplate 7 all have identical lengths, as do those constituting the soleplate 9, whereas those constituting the core 5 of the preform have different lengths. . The dry preform obtained, composed of dry carbon fibers, can then be impregnated with a resin, for example by one of the impregnation processes grouped under the name "LCM" (Liquid Composite Molding), which is known per se. This preform impregnated with resin is then placed in a baking oven in order to polymerize the resin.
    [0013] The polymerization step completes the manufacture of the stiffener 1 according to the invention, shown schematically in FIG. 7. The stiffener obtained comprises a core 5 and two flanges 7 and 9, and is intended to be mounted on a ferrule which can define a nacelle portion for 5 turbojet, and can for this purpose be assembled to a precut bent skin defining the ferrule, by mechanical connection or by bonding. The dry preform, composed of dry carbon fibers can also be assembled to a skin composed of fibers also dry so that the preforms of the skin and the stiffener are impregnated with resin during the same impregnation operation, thus allowing in this case the manufacture of a self-stiffened ferrule. In the same way, the polymerization step completes the manufacture of the self-stiffened curved skin according to the invention. Referring now to FIGS. 8 to 10, illustrating a so-called concave "T" -shaped preform, that is, the "T" -shaped stiffener core 15 is disposed at the inside of the curved sole, that is to say that the core is radially closer than the sole with respect to the axis of revolution of the preform. As defined in FIG. 1a, a "T" -shaped section stiffener has a core 5 and a sole 3 comprising two parts 3a, 3b. Such a "T" -shaped stiffener may comprise a web 5 within the concave sole 3, as shown in FIG. 10. The "T" -shaped section stiffener comprising a web 5 The inside of the sole 3 illustrated in this figure is obtained by the method of manufacturing the "T" shaped section preform shown in FIGS. 8 and 9, FIGS similar to FIGS. 3 and 6 showing the preform with a section in the form of a cross-section. "I in normal profile".
    [0014] As seen in more detail in FIG. 8, illustrating the preform being woven on the mandrel 13, the mandrel 13 now has a first conical portion 31 and a second cylindrical portion 33. The first portion 31, conical , has a profile for making the core 5 of the preform according to the desired curvature.
    [0015] The second portion 33, cylindrical, has a profile for making the sole 3 of the preform section substantially shaped "T". To do this, the weave pattern of the preform provides for making a stripping zone 35 of the warp son layers, made at the cylindrical portion 33 of the mandrel 13, while a binding zone 37 is performed on the conical portion 31 of the mandrel.
    [0016] FIGS. 11 to 13, to which reference is made now, are similar to FIGS. 8 to 10, the preform being this time of the "convex" type, that is to say that the stiffener core with a "T" shaped section is disposed outside the curved sole, that is to say that the core is radially further away than the sole, 5 with respect to the axis of revolution of the preform . As shown in Figure 11, the mandrel 13 now comprises a first cylindrical portion 39 and a second conical portion 41. The second portion 41, conical, has a profile for making the core 5 of the preform according to the desired curvature.
    [0017] The first portion 39, cylindrical, has a profile for making the sole 3 of the preform section substantially shaped "T". To do this, the weave pattern of the preform provides for producing a warp layer 43 of the warp layers, made at the cylindrical portion 39 of the mandrel 13, while a binding zone 45 is performed on the conical portion 41 of the mandrel. According to a variant shown in Figure 14, showing the preform being weaved on the mandrel 13 and the stiffener 1 obtained by this preform, the stiffener 1 may have an inclination at the sole. This inclination is obtained thanks to a particular geometry of mandrel 13, having two conical portions 44, 46, and thanks to a core 47 which is positioned during weaving in the dislocation zone 49 of the warp layers, between the two 3a, 3b parts intended to form the sole 3. The two conical portions 44 and 46 of the mandrel and the core 47 can create differences in consumption at the warp son called on the mandrel. From these 25 consumptions result different lengths of the warp son composing the entire preform and thus generating different curvatures for different parts of the preform, namely: the first part 3a of the sole, the second part 3b of the preform sole, and the core 5. This type of stiffener fits particularly to the outer portion 30 of a conical convex surface. As a variant shown in FIG. 15, the stiffener 1 is particularly suitable for the inner part of a concave conical surface. To this end, a mandrel 13 having two conical portions 51, 53 is used, and a core 55 is positioned during weaving 55 in the untied zone 57 of the warp son layers, between the two parts 3a, 3b intended to constitute the sole 3.
    [0018] The weave of the preform, illustrated in FIG. 4, represents two layers of warp yarns in the core of the preform, and a layer of warp yarns in the sole of the preform. This weaving method is a non-limiting example of the weaving envisaged, and several weaving variants are envisaged, represented in FIGS. 16 to 22. Of course, the invention is not limited to these binding methods, which are only given as examples of weaving. examples. As illustrated in FIG. 16, it is in particular possible to introduce two additional weft yarns 59, 61 at the level of the flanges 7 and 9 in order to achieve additional localized bonding at the meeting point of the plies of the soleplate, thereby permitting to strengthen the junction between the core 5 and the flanges 7, 9. Figures 17 to 20 illustrate a variant in which a single layer of warp son is provided in the core and in the sole of the preform. In Fig. 17, the preform has a constant warp yarn density in the web and in the sole. FIG. 18 is an alternative embodiment of the preform shown in FIG. 17, according to which two additional weft threads 63, 65 are introduced at the level of the flanges 7 and 9 in order to achieve additional localized bonding at the meeting point of the folds of the soleplate, which reinforces the junction between the core 20 5 and the flanges 7, 9. In the variant shown in Figure 19, the core 5 has a higher density of warp 21 son than in the variants preceding. This variant has the particularity of being made from a layer of uniform warp yarns in the comb of the loom.
    [0019] FIG. 20 illustrates an alternative embodiment of the weaving of FIG. 19, in which two additional weft threads 67, 69 are introduced at the level of the soles 7 and 9 in order to achieve additional localized binding at the meeting point of the folds of the sole, which reinforces the junction between the core 5 and the soles 7, 9.
    [0020] The weave variants shown in Figs. 21 and 22 illustrate a woven preform from a plurality of warp layers in the web 5 and in the flanges 7 and 9. In Fig. 21, four layers 71, 73 , 75, 77 of warp threads 21 are shown. Of course, the number of layers as well as their mode of binding are not limited to the representation of this figure.
    [0021] As a variant shown in FIG. 22, the preform with a "T" -shaped cross-section has a particular binding mode making it possible to optimize the management of the forces at the junction zone between the core 5 and the soleplate 3. According to a variant common to the weaving methods previously described, it is envisaged to add fabric pleats 79 at the level of the soles and / or folds of fabric 81 at the level of the core of the preform, as shown in FIGS. FIGS. 23 to 25. Thanks to the present invention, the mechanical performances of the "T" -shaped or "normal-profile" section stiffeners are substantially increased compared to the performances obtained by the methods used in the prior art. . Indeed, thanks to the manufacturing method according to the invention, the whole of the preform, that is to say the core and the sole (s), are manufactured in one piece, which allows obtain an intimate connection between the web and the sole (s) of the stiffener. Thanks to the method of manufacturing the contour-shaped woven preform, the orientation of the fibers of the preform is controlled and optimized. Indeed, the stiffener obtained is directly adapted to the curvature of the support on which it is assembled, without intermediate operation to give it its specific curvature, which reduces the number of manipulations on the preform. Thus, the manufacturing cost of a ferrule equipped with such a stiffener is advantageously reduced compared to the prior art. In addition, the contour-shaped weave method provides a repeatable and uniform fiber orientation technical solution, thereby reducing manufacturing time and cost and increasing mechanical performance. Finally, it goes without saying that the invention is not limited to only the embodiments of the preform obtained by the process according to the invention, described above solely as illustrative examples, but on the contrary it embraces all variants involving the technical equivalents of the means described and their combinations if they fall within the scope of the invention.
    权利要求:
    Claims (8)
    [0001]
    REVENDICATIONS1. Curved composite stiffener preform for an axisymmetric component such as a ferrule, comprising at least one core (5) and at least one sole (3, 7, 9) curved around an axis of revolution (22) of said preform and defining a section substantially in the form of "T" or "1 normal profile", said preform being characterized in that: - the core (5) comprises a plurality of warp threads (21) oriented circumferentially with respect to the axis of revolution (22) of the preform, and a plurality of weft threads (23, 59, 61, 63, 65, 67, 69) oriented radially with respect to said axis, - the sole (3, 7, 9 ) comprises a plurality of warp threads (21) circumferentially oriented with respect to the axis of revolution of the preform, and a plurality of weft threads (23, 59, 61, 63, 65, 67, 69) substantially parallel to said axis.
    [0002]
    2. Preform according to claim 1, characterized in that the core (5) comprises a bonding zone (25) of layers (18, 20) of warp threads between them by means of weft threads, and in that said at least one sole (3, 7, 9) comprises at least one loosening zone (27, 29) of layers (18, 20) of warp yarns.
    [0003]
    3. Preform according to one of claims 1 or 2, characterized in that the warp son (21) of the sole (3, 7, 9) of the preform have identical lengths, and in that the warp son (21) of the core (5) of the preform have distinct lengths.
    [0004]
    4. curved composite stiffener (1) for axisymmetric part such as a shell, characterized in that it comprises at least one preform according to one of claims 1 to 3. 30
    [0005]
    5. Axisymmetric piece such as a shell, characterized in that it is reinforced by at least one stiffener according to claim 4.
    [0006]
    6. A method of manufacturing a curved composite stiffener preform 35 for axisymmetrical part such as a shell, said preform having at least one core (5) and at least one sole (3, 7, 9) and defining a section 3025529 13 substantially in the form of "T" or "1 normal profile", said method being characterized in that said preform is made by an outline-type weaving method, and in that it comprises the following steps aimed at to: - call the warp threads (21, 71, 73, 75, 77) directly at the exit of a loom (11) on a mandrel (13) having at least one conical portion (17, 31, 41, 44, 46, 51, 53) and at least one conical or cylindrical portion; inserting weft threads (23, 59, 61, 63, 65, 67, 69) so as to define at least one bonding zone (25) and at least one untie zone (27, 29) of the layers (18, 59, 61, 63, 65, 67, 69) 20) of warp yarns; Unfolding the preform obtained so as to obtain said core (5) and said at least one sole (3, 7, 9).
    [0007]
    7. Mandrel call (13) adapted to implement the manufacturing method defined in claim 6, characterized in that it has a non-rectilinear generatrix 15.
    [0008]
    8. mandrel (13) according to claim 7, characterized in that it comprises at least one conical portion (17, 31, 41, 44, 46, 51, 53) and at least one conical or cylindrical portion.
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    同族专利:
    公开号 | 公开日
    US20170175308A1|2017-06-22|
    WO2016038301A1|2016-03-17|
    US10767288B2|2020-09-08|
    FR3025529B1|2017-07-14|
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    法律状态:
    2015-09-15| PLFP| Fee payment|Year of fee payment: 2 |
    2016-03-11| PLSC| Search report ready|Effective date: 20160311 |
    2016-08-10| PLFP| Fee payment|Year of fee payment: 3 |
    2017-08-24| PLFP| Fee payment|Year of fee payment: 4 |
    2018-03-02| CD| Change of name or company name|Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
    2018-09-07| PLFP| Fee payment|Year of fee payment: 5 |
    2019-08-20| PLFP| Fee payment|Year of fee payment: 6 |
    2020-08-19| PLFP| Fee payment|Year of fee payment: 7 |
    2021-08-19| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1458493A|FR3025529B1|2014-09-10|2014-09-10|PREFORM FOR CURVED COMPOSITE STIFFENER FOR AXISYMETRIC PIECE SUCH AS A VIROLE|FR1458493A| FR3025529B1|2014-09-10|2014-09-10|PREFORM FOR CURVED COMPOSITE STIFFENER FOR AXISYMETRIC PIECE SUCH AS A VIROLE|
    PCT/FR2015/052404| WO2016038301A1|2014-09-10|2015-09-10|Preform for a curved composite stiffener for an axisymmetric part such as a collar|
    US15/454,022| US10767288B2|2014-09-10|2017-03-09|Preform for a curved composite stiffener for an axisymmetric part such as a collar|
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