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1. 发明授权

US08615877B2 Method of producing a nozzle or a divergent nozzle element made of a composite 有权
标题翻译：制造由复合材料制成的喷嘴或发散喷嘴元件的方法
公开(公告)号：US08615877B2
公开(公告)日：2013-12-31
申请号：US13054348
申请日：2009-07-13
申请人： François Charleux , Jean-Marie Parenteau , Bernard Delperier
发明人： François Charleux , Jean-Marie Parenteau , Bernard Delperier
IPC分类号： B21D53/00
CPC分类号： C04B35/806 , C04B35/565 , C04B35/83 , C04B2235/614 , C04B2235/616 , C04B2235/72 , C04B2235/722 , C04B2235/723 , F02K9/97 , F05D2300/601 , F05D2300/603
摘要： A fiber preform is obtained by conforming panels of fiber texture on a former having a surface that reproduces the shape desired for a surface of the nozzle or the nozzle divergent section that is to be made. The panels are bonded together via their mutually contacting edges. A consolidated fiber reinforcement is formed by shaping the fiber preform impregnated with a consolidation composition including a resin. The shaping of the fiber preform is performed between the former and a jacket applied against the impregnated fiber preform so as the consolidated fiber reinforcement has a fiber volume percentage of at least 35%, and a thickness of less than 5 mm over at least a major fraction of its axial dimension. The densification of the fiber reinforcement is continued by chemical vapor infiltration after pyrolyzing the resin so that once densified, a part is obtained that has practically the shape and the wall thickness of the nozzle or the nozzle divergent section that is to be made.
摘要翻译：通过在具有再现喷嘴的表面所需形状的表面或要制造的喷嘴发散部分的表面上使纤维织构的面板相符合来获得纤维预制件。面板通过相互接触的边缘粘合在一起。通过使浸渍有包含树脂的固化组合物的纤维预制件成形来形成固结的纤维增强材料。纤维预成型件的成型在前者和施加在浸渍的纤维预制件上的护套之间进行，因此固结的纤维增强材料的纤维体积百分比至少为35％，厚度小于5mm至少大于其轴向尺寸的分数。在热解树脂之后，纤维增强物的致密化继续通过化学气相渗透，使得一旦致密化，获得实际上具有实际上要形成的喷嘴或喷嘴发散部分的形状和壁厚的部分。

2. 发明授权

US08426326B2 Fiber reinforcing texture for making a composite material part 有权
标题翻译：用于制造复合材料部件的纤维增强纹理
公开(公告)号：US08426326B2
公开(公告)日：2013-04-23
申请号：US13494376
申请日：2012-06-12
申请人： Eric Bouillon , François Charleux , Caroline Louchet-Pouillerie , Rémi Bouvier , Dominique Coupe
发明人： Eric Bouillon , François Charleux , Caroline Louchet-Pouillerie , Rémi Bouvier , Dominique Coupe
IPC分类号： D03D3/00 , D03D3/06 , D03D11/00 , F04D29/30
CPC分类号： B32B5/08 , C08J5/047 , D03D25/005 , Y10T442/2984 , Y10T442/3195 , Y10T442/3203 , Y10T442/3211
摘要： A fiber reinforcing texture woven as a single part for fabricating a composite material part having an inner portion, or core, made by three-dimensional weaving with yarns made up from discontinuous fibers, and a portion adjacent to an outside surface, or skin, made by weaving with yarns made up from continuous filaments.
摘要翻译：作为制造复合材料部件的纤维增强织构，用于制造具有由不连续纤维构成的纱线的三维织造和与外表面相邻的部分或皮肤制成的内部或芯部的复合材料部件通过用连续长丝制成的纱线编织。

3. 发明申请

US20120196107A1 METHOD OF FABRICATING A THERMOSTRUCTURAL COMPOSITE MATERIAL PART, AND A PART OBTAINED THEREBY 有权
标题翻译：制备热结构复合材料部件的方法及其获得的部件
公开(公告)号：US20120196107A1
公开(公告)日：2012-08-02
申请号：US13441432
申请日：2012-04-06
申请人： Eric Philippe , Eric Bouillon
发明人： Eric Philippe , Eric Bouillon
IPC分类号： B32B7/02 , B32B18/00 , B82Y30/00
CPC分类号： C04B35/80 , C04B35/571 , C04B35/6286 , C04B35/62865 , C04B35/62873 , C04B35/62884 , C04B35/62894 , C04B35/62897 , C04B35/83 , C04B2235/5224 , C04B2235/5244 , C04B2235/5248 , C04B2235/5252 , C04B2235/5256 , C04B2235/614 , C04B2235/616 , Y10S427/10 , Y10T428/24975 , Y10T428/249928 , Y10T428/25 , Y10T428/265
摘要： The method comprises: using chemical vapor infiltration to form a first continuous interphase on the fibers of a fiber structure made of refractory fibers, the interphase having a thickness of no more than 100 nanometers; impregnating the fiber structure with a consolidation composition comprising a carbon or ceramic precursor resin; forming a fiber preform that is consolidated by shaping the impregnated fiber structure and using pyrolysis to transform the resin into a discontinuous solid residue of carbon or ceramic; using chemical vapor infiltration to form a second continuous interphase layer; and densifying the preform with a refractory matrix. This preserves the capacity of the fiber structure to deform so as to enable a fiber preform to be obtained that is of complex shape, while nevertheless guaranteeing the presence of a continuous interphase between the fibers and the matrix.
摘要翻译：该方法包括：使用化学气相渗透在由耐火纤维制成的纤维结构的纤维上形成第一连续相间，相间的厚度不超过100纳米; 用包含碳或陶瓷前体树脂的固化组合物浸渍纤维结构; 形成纤维预成型件，其通过成形浸渍的纤维结构并使用热解将树脂转变成碳或陶瓷的不连续的固体残余物来固结; 使用化学气相渗透形成第二连续相间层; 并用耐火基体致密化预制件。这保持了纤维结构变形的能力，以便能够获得具有复杂形状的纤维预制件，同时保证在纤维和基质之间存在连续的相间。

4. 发明申请

US20120087795A1 ROTOR FOR TURBOMACHINERY 有权
标题翻译：涡轮机转子
公开(公告)号：US20120087795A1
公开(公告)日：2012-04-12
申请号：US13267290
申请日：2011-10-06
申请人： Fabrice Noël Marcel GARIN , Romain Nicolas Lunel
发明人： Fabrice Noël Marcel GARIN , Romain Nicolas Lunel
IPC分类号： F01D5/22
CPC分类号： F01D11/008 , F05D2240/80
摘要： A rotor includes a disc, on which are fixed vanes, and platforms between these vanes. The rotor is particularly remarkable in that the platforms are fixed securely and tightly to the disc. To this end, the disc includes between two successive vanes an upstream stop projecting axially from the upstream surface, and each platform includes: a plate, a retaining groove extending axially and in which the upstream stop of the disc is engaged, an axial stop bearing axially against the upstream surface of the disc.
摘要翻译：转子包括在其上是固定叶片的圆盘和这些叶片之间的平台。转子特别显着，因为平台牢固地固定在盘上。为此，盘包括在两个相继的叶片之间，上游止挡件从上游表面轴向突出，并且每个平台包括：板，沿轴向延伸的保持槽，其中盘的上游止挡接合在其中，轴向止动轴承轴向地抵靠盘的上游表面。

5. 发明申请

US20120055609A1 METHOD FOR PRODUCING A TURBOMACHINE BLADE MADE FROM A COMPOSITE MATERIAL 有权
标题翻译：从复合材料制造涡轮叶片的方法
公开(公告)号：US20120055609A1
公开(公告)日：2012-03-08
申请号：US13263176
申请日：2010-03-26
申请人： Stephane Pierre Guillaume Blanchard , Eric Bouillon , Dominique Coupe , Hubert Illand , Clement Roussille
发明人： Stephane Pierre Guillaume Blanchard , Eric Bouillon , Dominique Coupe , Hubert Illand , Clement Roussille
IPC分类号： C04B35/64 , D03D3/00 , B32B7/08 , D03D1/00
CPC分类号： C04B35/64 , B29B11/16 , B29C70/24 , B29D99/0025 , B29L2031/08 , C04B35/524 , C04B35/571 , C04B35/62868 , C04B35/62873 , C04B35/62884 , C04B35/62897 , C04B35/806 , C04B2235/5244 , C04B2235/5252 , C04B2235/5256 , C04B2235/616 , D03D25/005 , F01D5/282 , Y02T50/672 , Y10T29/49321 , Y10T29/49325
摘要： A method of fabricating a composite-material turbomachine blade having platform incorporated therein includes separately making a blade platform element that comprises rigidified fiber reinforcement and that has a shape close to that of a platform of the blade to be fabricated, with at least one opening being formed through the platform element. The opening has the shape of the profile of the airfoil of the blade to be fabricated. Three-dimensional weaving is used to make a flexible fiber blank as a single piece that includes blade airfoil-and-root preform portions. The platform element is engaged, via its opening, on the flexible fiber blank while deforming it so as to assemble the platform element with the fiber blank. The fiber blank is shaped together with the platform element assembled thereon to obtain a blade preform of a shape that is close to the shape of the blade to be fabricated. After shaping, the blade preform is consolidated in its shape in a shaper. Additionally, final densification of the consolidated blade preform is performed in order to obtain a composite-material blade having an incorporated platform.
摘要翻译：制造具有并入其中的平台的复合材料涡轮机叶片的方法包括分别制造包括刚性纤维增强件并且具有接近待制造的叶片的平台的形状的叶片平台元件，其中至少一个开口通过平台元件形成。开口具有要制造的叶片的翼型的形状。使用三维编织将柔性纤维坯料制成包括叶片翼型和根部预制件部分的单件。平台元件通过其开口接合在柔性纤维坯料上，同时变形，以便将平台元件与纤维坯料组装。纤维坯料与组装在其上的平台元件一起成形，以获得接近待制造的刀片形状的形状的刀片预制件。在成形之后，刀片预成型件以整形器固结成其形状。此外，为了获得具有并入的平台的复合材料刀片，进行固结刀片预成型件的最终致密化。

6. 发明授权

US08092276B2 Method of fabricating a part made up of a plurality of thin-walled tubes and having a surface of revolution 失效
标题翻译：制造由多个薄壁管组成并具有旋转表面的部件的方法
公开(公告)号：US08092276B2
公开(公告)日：2012-01-10
申请号：US12330711
申请日：2008-12-09
申请人： Jean-Pierre Maumus , Rémi Bessette
发明人： Jean-Pierre Maumus , Rémi Bessette
IPC分类号： B24C1/04
CPC分类号： B26F3/004 , B24C1/045 , B24C3/18
摘要： The invention relates to a method of fabricating a part including at least one face in the form of a surface of revolution from a structure made up of a plurality of thin-walled hollow bodies. In order to ensure that cutting takes place without damaging the walls and/or the bonds between the walls of the hollow bodies, the part is machined in the structure by means of a water jet. More precisely, during machining, the structure is attacked with a jet of water under pressure that is directed tangentially relative to the outer envelope of said at least one face to be made in the form of a surface of revolution.
摘要翻译：本发明涉及一种制造部件的方法，该部件包括从由多个薄壁中空体构成的结构的旋转表面形式的至少一个面。为了确保在不破坏壁和/或中空体的壁之间的结合的情况下进行切割，部件通过水射流在结构中加工。更准确地说，在加工过程中，结构受到压力下的水射流的冲击，相对于所述至少一个面的外包层以切向形式定向成旋转表面。

7. 发明授权

US08034273B2 Method of producing a fibrous layer for the manufacture of a preform of a composite part 有权
标题翻译：制造复合部件的预成型体的纤维层的制造方法
公开(公告)号：US08034273B2
公开(公告)日：2011-10-11
申请号：US12298249
申请日：2007-04-25
申请人： Joëlle Lalande , Frédéric Ballion , Dirk Feltin
发明人： Joëlle Lalande , Frédéric Ballion , Dirk Feltin
IPC分类号： B29C45/02 , B29C69/00
CPC分类号： B29C70/34 , B29C70/24 , B29C70/30 , B29C70/543 , B29C70/545 , F02K9/97 , F05D2300/2102 , F05D2300/224 , F05D2300/614 , Y10T428/24124
摘要： The invention provides a method of making a fiber ply for forming a preform of a composite part in the form of a body of revolution having a non-developable surface, the method being characterized in that it comprises the steps consisting in: defining an annular space (23) with first and second canvases (20, 21) respectively defining an inner periphery and an outer periphery thereof; placing fibers between the canvases (20, 21) by placing the fibers in the annular space in at least one direction and by holding said fibers on the canvases by stitching; implementing circular connection stitching in the vicinity of the inner periphery of the annular space (23); and cutting out the fiber ply as made in this way in the annular space (23) in order to extract it from the canvases.
摘要翻译：本发明提供一种制造纤维帘布层的方法，用于形成具有不可展开表面的具有旋转体形式的复合部件的预成型件，该方法的特征在于包括以下步骤：限定环形空间（23）具有分别限定其内周和外周的第一和第二帆布（20,21）; 通过将纤维沿至少一个方向放置在环形空间中并通过缝合将所述纤维保持在帆布上，将纤维放置在帆布（20,21）之间; 在环形空间（23）的内周附近实施圆形连接缝合; 并且在环形空间（23）中切割出如此制造的纤维层，以便将其从帆布中提取出来。

8. 发明申请

US20100111678A1 TURBINE RING ASSEMBLY FOR GAS TURBINE 有权
标题翻译：用于气体涡轮机的涡轮环组件
公开(公告)号：US20100111678A1
公开(公告)日：2010-05-06
申请号：US12531113
申请日：2008-03-14
申请人： Georges Habarou , Julien Mateo , Eric Bouillon
发明人： Georges Habarou , Julien Mateo , Eric Bouillon
IPC分类号： F01D11/08 , D04H18/00
CPC分类号： F01D9/04 , F01D11/08 , F05D2240/11 , F05D2300/21 , F05D2300/603 , Y02T50/67 , Y02T50/672
摘要： A turbine ring assembly for a gas turbine, the assembly comprising a complete ring (10) forming a single piece of ceramic matrix composite material (CMC), a metal structure for supporting the CMC ring having metal annular supports (20, 30) between which the CMC ring is placed while allowing differential expansion at least in a radial direction between the CMC ring and the annular supports, means (40-42) for centering the CMC ring, and at least one element for preventing turning of the CMC ring about its axis.
摘要翻译：一种用于燃气轮机的涡轮环组件，该组件包括形成单片陶瓷基复合材料（CMC）的完整环（10），用于支撑具有金属环形支撑件（20,30）的CMC环的金属结构 CMC环被放置，同时至少在CMC环和环形支撑件之间的径向方向上进行不同的膨胀，用于使CMC环对中的装置（40-42）以及用于防止CMC环绕其旋转的至少一个元件轴。

9. 发明授权

US07691440B2 Method and installation for the densification of substrates by means of chemical vapor infiltration 有权
标题翻译：通过化学气相渗透使基材致密化的方法和安装
公开(公告)号：US07691440B2
公开(公告)日：2010-04-06
申请号：US10475464
申请日：2003-01-14
申请人： Bruno Bernard , Stéphane Goujard , Sébastien Bertrand
发明人： Bruno Bernard , Stéphane Goujard , Sébastien Bertrand
IPC分类号： C23C16/00
CPC分类号： C23C16/045 , C04B35/83 , C23C16/455 , C23C16/45578 , Y10S427/10
摘要： A method of densifying porous substrates by chemical vapor infiltration comprises loading porous substrates for densification in a loading zone of an enclosure (10), heating the internal volume of the enclosure, and introducing a reagent gas into the enclosure though an inlet situated at one end of the enclosure. Before coming into contact with substrates (20) situated in the loading zone, the reagent gas admitted into the enclosure is preheated, at least in part, by passing along a duct (30) connected to the gas inlet and extending through the loading zone, the duct being raised to the temperature inside the enclosure, and the preheated reagent gas is distributed in the loading zone through one or more openings (33) formed in the side wall (32) of the duct, along the duct.
摘要翻译：通过化学气相渗透致密化多孔基材的方法包括在壳体（10）的装载区域中加载多孔基材用于致密化，加热外壳的内部体积，并且通过位于一端的入口将反应气体引入外壳的外壳。在与位于装载区域中的基板（20）接触之前，允许进入外壳的反应气体至少部分地通过连接到气体入口并延伸穿过装载区域的管道（30）进行预热，所述管道升高到所述外壳内部的温度，并且所述预热的反应气体沿着所述管道通过形成在所述管道的侧壁（32）中的一个或多个开口（33）分布在所述装载区域中。

10. 发明授权

US07658062B2 Gas generator and turbojet fitted with such a generator for starting 有权
标题翻译：燃气发电机和涡轮喷气发动机配有这样的发电机起动
公开(公告)号：US07658062B2
公开(公告)日：2010-02-09
申请号：US10994192
申请日：2004-11-19
申请人： Laurent Soulie , Roger Fischer
发明人： Laurent Soulie , Roger Fischer
IPC分类号： F02C3/26
CPC分类号： F01D19/00 , F02C7/272 , F42B3/04 , Y02T50/672
摘要： A gas generator comprises a casing forming a ring or a ring portion and housing a pyrotechnic charge, the casing including at least one vent for ejecting the gas produced during combustion of the charge. Because of its ring design, the gas generator is easy to integrate in the structure of a rotary machine. In particular, it can constitute a starter device for a turbojet.
摘要翻译：气体发生器包括形成环或环部并且容纳烟火装药的壳体，所述壳体包括用于喷射在燃料燃烧期间产生的气体的至少一个排气口。由于其环形设计，气体发生器易于集成在旋转机器的结构中。特别地，它可以构成涡轮喷气发动机的起动装置。

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