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1.发明公开
公开(公告)号：EP2416944A1
公开(公告)日：2012-02-15
申请号：EP10715988.1
申请日：2010-03-26
申请人： Snecma , Snecma Propulsion Solide
发明人： BLANCHARD, Stéphane, Pierre, Guillaume , BOUILLON, Eric , COUPE, Dominique , ILLAND, Hubert , ROUSSILLE, Clément
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 , F01D5/282 , Y02T50/672 , Y10T29/49321 , Y10T29/49325
摘要： The invention relates to a method for producing a turbomachine blade from a composite material, having an integrated platform and/or shroud. The method comprises the following steps: the three-dimensional weaving of a flexible fibrous blank as a single part comprising blade vane (220) and root (230) preform portions; the separate production of a blade platform (400) or blade shroud (500) element comprising a stiffened fibrous reinforcement, whereby at least one opening in the shape of the vane profile of the blade to be produced is formed in the platform or shroud element; the mounting of the platform or shroud element, by means of the opening therein, on the flexible fibrous blank, with deformation of the latter, for assembly with the fibrous blank; the forming of the fibrous blank with the assembled platform or shroud element in order to obtain a preform (200) having a shape similar to that of the blade to be produced; the setting of the shape of the preform in a former; and the introduction of a matrix in the preform in order to obtain a blade made from a composite material and having an integrated platform or shroud.
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公开(公告)号：EP2356085A1
公开(公告)日：2011-08-17
申请号：EP09803800.3
申请日：2009-12-02
申请人： Snecma Propulsion Solide , Snecma
CPC分类号： C04B41/52 , C04B41/009 , C04B41/90 , C04B2111/00344 , F01D5/288 , F05D2230/90 , F05D2300/21 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T428/31678 , C04B41/4535 , C04B41/4554 , C04B41/5059 , C04B41/5066 , C04B41/522 , C04B41/5064 , C04B41/4523 , C04B41/5096 , C04B41/515 , C04B41/5144 , C04B35/565 , C04B35/806
摘要： The invention relates to a method for smoothing a corrugated, rough surface of a part made from a ceramic matrix composite material. According to the invention, a ceramic coating is formed on the surface of the part by means of the following steps, namely: application (20) of a liquid composition on the surface of the part, said composition containing a ceramic precursor polymer and a solid refractory filler; crosslinking (40) of the polymer; and conversion (50) of the crosslinked polymer into ceramic by means of heat treatment. The method also includes the impregnation of the ceramic coating with a liquid metal composition (60).
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3.发明公开STRUCTURE FIBREUSE DE RENFORT POUR PIECE EN MATERIAU COMPOSITE ET PIECE LA COMPORTANT 审中-公开VERSTÄRKENDESFASERGEBILDEFÜREINEN VERBUNDWERKSTOFF SOWIE DAS FASERGEBILDE ENTHALTENDES BAUTEIL
公开(公告)号：EP1893399A2
公开(公告)日：2008-03-05
申请号：EP06778962.8
申请日：2006-06-21
申请人： SNECMA , Snecma Propulsion Solide
IPC分类号： B29C70/24
CPC分类号： D03D25/005 , B29C70/24 , B29C70/48 , B29L2031/3076 , B29L2031/7488 , B64C25/12 , F16C7/026 , F16C2326/43 , Y10T74/2142 , Y10T442/3195 , Y10T442/3203 , Y10T442/3211
摘要： A woven fibrous structure embodied in one piece, used for producing a composite material part and comprising an internal part or a core (72) and a part adjacent to the external surface thereof or a skin (74, 76), is formed by three-dimensional core weaving with at least one weave selected from interlock and multilayer weaves and by skin weaving with a weave which differs from the core weave and selected from a multilayer weave and a two-dimensional weave. It can be also formed by three-dimensional weaving with at least one core interlock weave (72) and weaving with a fabric-, satin or skin twill-type weave, wherein skin weaving is of a multilayer or two-dimensional type. .
摘要翻译： 该部分具有其中布置圆柱形自由空间（14）的两个端部（10a）和由中心和周边纤维预制件（13,11）实现的由复合材料制成的主体。 预制件由三维编织的碳纤维制成。 周边纤维预制件以保持在部件的端部的方式包围中心纤维预制件，其中预成型件（11）是其端部接合的条带。 自由空间适于接收另一部分的铰接轴。 还包括以下独立权利要求：（1）起落架，其包括具有杆（2）的支柱，用于制造机械部件的方法。
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公开(公告)号：EP2349687B1
公开(公告)日：2012-11-14
申请号：EP09797096.6
申请日：2009-11-26
申请人： Snecma Propulsion Solide , Snecma
CPC分类号： B29B11/16 , B29B11/02 , C04B35/52 , C04B35/565 , C04B35/6286 , C04B35/62868 , C04B35/62873 , C04B35/62897 , C04B35/806 , C04B35/83 , C04B2235/5244 , C04B2235/5252 , C04B2235/614 , C04B2235/94 , F01D5/282 , F01D17/20 , F05D2300/601 , F05D2300/6012 , F05D2300/614 , Y02T50/672 , Y10S427/10
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公开(公告)号：EP2414305A1
公开(公告)日：2012-02-08
申请号：EP10717696.8
申请日：2010-03-31
申请人： Snecma Propulsion Solide , Snecma
CPC分类号： C23C18/1216 , C03C3/087 , C03C8/00 , C04B41/009 , C04B41/5022 , C04B41/52 , C04B41/86 , C04B41/89 , C23C4/11 , F01D5/282 , F05D2230/311 , F05D2230/312 , F05D2230/90 , F05D2300/611 , Y02T50/67 , Y02T50/672 , Y02T50/673 , Y10T428/249924 , C04B41/4539 , C04B41/4554 , C04B41/5059 , C04B41/4527 , C04B41/522 , C04B35/565 , C04B35/806
摘要： A process for smoothing the surface of a part made from a ceramic matrix composite material having a rough and wavy surface. The process comprises depositing a refractory vitreous coating on the surface of the part (90), the vitreous coating essentially containing silica, alumina, baryte and lime.
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公开(公告)号：EP2349687A2
公开(公告)日：2011-08-03
申请号：EP09797096.6
申请日：2009-11-26
申请人： Snecma Propulsion Solide , Snecma
CPC分类号： B29B11/16 , B29B11/02 , C04B35/52 , C04B35/565 , C04B35/6286 , C04B35/62868 , C04B35/62873 , C04B35/62897 , C04B35/806 , C04B35/83 , C04B2235/5244 , C04B2235/5252 , C04B2235/614 , C04B2235/94 , F01D5/282 , F01D17/20 , F05D2300/601 , F05D2300/6012 , F05D2300/614 , Y02T50/672 , Y10S427/10
摘要： The invention relates to a complexly shaped composite material part including a three-dimensional, weaved, fibrous reinforcement densified by a matrix, and manufactured through a method comprising the following steps of: - three-dimensionally weaving a continuous, fibrous strip including a series of fibrous blanks (200) made of preforms having a plurality of parts to manufacture; - then cutting individual fibrous blanks into the strip, each blank (200) being made of a single part; - shaping a cut blank to obtain a fibrous preform having a shape corresponding to that of a part to be manufactured; - setting the preform in the desired shape; and – densifying the set preform through the formation of a matrix by gaseous-phase chemical infiltration.
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公开(公告)号：EP2118448A2
公开(公告)日：2009-11-18
申请号：EP08788003.5
申请日：2008-03-14
发明人： HABAROU, Georges , MATEO, Julien , BOUILLON, Eric
CPC分类号： F01D9/04 , F01D11/08 , F05D2240/11 , F05D2300/21 , F05D2300/603 , Y02T50/67 , Y02T50/672
摘要： The invention relates to a turbine ring assembly for a gas turbine, that comprises a full ring (10) made of a single piece and of a composite material having a ceramic matrix, a metal structure for holding the CMC ring including metal annular holders (20, 30) between which the CMC ring is provided while allowing for a differential expansion at least in the radial direction between the CMC ring and the annular holders, a means (40-42) for centring the CMC ring, and at least one member for rotatingly blocking the CMC ring about the axis thereof.
摘要翻译： 本发明涉及一种用于燃气轮机的涡轮环组件，其包括由单件制成的完整环（10）和具有陶瓷基体的复合材料，用于保持CMC环的金属结构，所述金属结构包括金属环形保持器（20 ，30），其间提供CMC环，同时允许至少在CMC环和环形保持器之间的径向方向上的膨胀膨胀，用于使CMC环对中的装置（40-42），以及至少一个用于 围绕其轴线旋转地阻挡CMC环。
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8.发明公开PROCEDE DE FABRICATION DE PIECE EN MATERIAU COMPOSITE A MATRICE CERAMIQUE ET PIECE AINSI OBTENUE 有权用于生产复合陶瓷矩阵的一部分，从而制造，部件
公开(公告)号：EP1851180A1
公开(公告)日：2007-11-07
申请号：EP06726195.8
申请日：2006-02-22
发明人： PHILIPPE, Eric , BERTRAND, Sébastien , BOUILLON, Eric , CAILLAUD, Alain , ICHARD, Jean-christophe 34 Rue Bir-hakeim , BAGAT, Robert
IPC分类号： C04B35/571 , C04B35/80 , C04B41/45 , C04B41/52 , C04B35/628 , C04B41/50
CPC分类号： C04B35/62873 , C04B35/565 , C04B35/571 , C04B35/6286 , C04B35/62863 , C04B35/62868 , C04B35/62884 , C04B35/62894 , C04B35/62897 , C04B35/806 , C04B2235/465 , C04B2235/5244 , C04B2235/80 , C04B2235/96 , Y10T428/265
摘要： The invention concerns a method whereby an intermediate phase coating is formed by chemical vapour infiltration (CVI) on the fibers constituting a fibrous preform, the intermediate phase coating comprising at least one internal embrittlement relief layer of the composite material, in contact with the fibers, and an external adherence layer with the ceramic matrix. The fibrous preform is then maintained in its shape with the fibers provided with an intermediate phase coating, and reinforced by being impregnated with a liquid composition containing a ceramic precursor, and transformation of the precursor into a reinforcing phase of ceramic matrix. The reinforced preform is then densified by a complementary ceramic matrix phase. No maintenance tools are required for forming the intermediate phase coating by CVI or for densifying after reinforcement by liquid process.
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公开(公告)号：EP1786586A1
公开(公告)日：2007-05-23
申请号：EP05778794.7
申请日：2005-06-22
CPC分类号： B23K1/20 , B23K1/08 , B23K2203/16 , C04B37/005 , C04B2235/428 , C04B2235/616 , C04B2237/08 , C04B2237/083 , C04B2237/16 , C04B2237/365 , C04B2237/38 , C04B2237/385 , C04B2237/52 , C04B2237/55 , C04B2237/592 , C04B2237/72 , Y10T156/10 , Y10T156/1062
摘要： The invention relates to a method for assembling two parts (10, 20) by soldering consisting in inserting a reinforcement (30) formed by a refractory fibrous texture between two surfaces (S10, S20) of jointable parts, wherein said reinforcement is brought at least partially into contact with a soldering composition (40), in subsequently carrying out a heat treatment for liquefying said soldering composition (40) in such a way that the molten soldering composition is capillary distributed along the totality of a soldering surface between two parts (10, 20) covered by the reinforcement.
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公开(公告)号：EP2118448B1
公开(公告)日：2010-08-18
申请号：EP08788003.5
申请日：2008-03-14
发明人： HABAROU, Georges , MATEO, Julien , BOUILLON, Eric
CPC分类号： F01D9/04 , F01D11/08 , F05D2240/11 , F05D2300/21 , F05D2300/603 , Y02T50/67 , Y02T50/672
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