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公开(公告)号：US20070110913A1
公开(公告)日：2007-05-17
申请号：US11539044
申请日：2006-10-05
申请人： Jean-Michel FRANCHET , Jean-Francois Fromentin , Jean-Michel Quenisset , Carine Duda , Corinne Arvieu , Pierre Frayssines
发明人： Jean-Michel FRANCHET , Jean-Francois Fromentin , Jean-Michel Quenisset , Carine Duda , Corinne Arvieu , Pierre Frayssines
CPC分类号： C04B41/90 , B22F2998/00 , C04B41/009 , C04B41/4584 , C04B41/52 , C04B2111/00965 , C22C47/04 , C22C49/11 , C23C2/006 , C23C2/02 , C04B41/4531 , C04B41/5059 , C04B41/5001 , C04B41/5061 , C04B41/507 , C04B41/4523 , C04B41/5161 , C04B41/5133 , C04B14/386 , B22F2201/01 , B22F2202/07
摘要： The invention relates to a method for metallic coating of fibres by liquid technique, in which a fibre, coated with a material forming a diffusion barrier with the metal, is drawn through a liquid metal bath to be coated therewith. The method is characterized in that prior to the passage of the fibre into the bath, the fibre is coated with a compound wettable by the metal. The coating of the fibre by the metal is facilitated by the presence of the compound, forming an interface wettable by the metal.
摘要翻译： 本发明涉及一种通过液体技术对纤维进行金属涂覆的方法，其中涂覆有与金属形成扩散阻挡层的材料的纤维通过待涂覆的液态金属浴被拉伸。 该方法的特征在于，在纤维通过浴之前，纤维被可被金属润湿的化合物涂覆。 通过化合物的存在促进了金属对纤维的涂层，形成了被金属润湿的界面。
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公开(公告)号：US07687114B2
公开(公告)日：2010-03-30
申请号：US11539044
申请日：2006-10-05
申请人： Jean-Michel Patrick Maurice Franchet , Jean-Francois Fromentin , Jean-Michel Quenisset , Carine Duda , Corinne Arvieu , Pierre Eric Frayssines
发明人： Jean-Michel Patrick Maurice Franchet , Jean-Francois Fromentin , Jean-Michel Quenisset , Carine Duda , Corinne Arvieu , Pierre Eric Frayssines
CPC分类号： C04B41/90 , B22F2998/00 , C04B41/009 , C04B41/4584 , C04B41/52 , C04B2111/00965 , C22C47/04 , C22C49/11 , C23C2/006 , C23C2/02 , C04B41/4531 , C04B41/5059 , C04B41/5001 , C04B41/5061 , C04B41/507 , C04B41/4523 , C04B41/5161 , C04B41/5133 , C04B14/386 , B22F2201/01 , B22F2202/07
摘要： The invention relates to a method for metallic coating of fibers by liquid technique, in which a fiber, coated with a material forming a diffusion barrier with the metal, is drawn through a liquid metal bath to be coated therewith. The method is characterized in that prior to the passage of the fiber into the bath, the fiber is coated with a compound wettable by the metal. The coating of the fiber by the metal is facilitated by the presence of the compound, forming an interface wettable by the metal.
摘要翻译： 本发明涉及一种通过液体技术对纤维进行金属涂覆的方法，其中涂覆有与金属形成扩散阻挡层的材料的纤维通过待涂覆的液态金属浴被拉伸。 该方法的特征在于，在将纤维通入浴液之前，纤维被可被金属润湿的化合物涂覆。 通过化合物的存在促进了金属对纤维的涂层，形成了被金属润湿的界面。
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3.发明申请Process for manufacturing a component with an insert made of a composite consisting of a metal matrix and ceramic fibers 有权用由金属基体和陶瓷纤维组成的复合体制成的嵌件的制造方法公开(公告)号：US20070051455A1
公开(公告)日：2007-03-08
申请号：US11441156
申请日：2006-05-26
IPC分类号： B65H81/00
CPC分类号： C22C47/064 , B22F2998/00 , B23K11/0026 , B23K2101/34 , B23K2103/16 , C22C49/11 , Y10T29/49801 , Y10T29/49968 , B22F1/025
摘要： Process for manufacturing a component with an insert made of a composite comprising a metal matrix, within which ceramic fibers extend, the insert made of a composite being obtained from a plurality of coated filaments, each comprising a ceramic fiber coated with a metal sheath, characterized in that it comprises the manufacture of an insert with a step of winding a bundle or bonded sheet of coated filaments around a body of revolution perpendicular to the axis of rotation of said body. The insert is then subjected to a hot isostatic pressing step in a container. The process is applied to the manufacture of aeronautical turbomachine components.
摘要翻译： 制造具有由包含金属基质（其中陶瓷纤维延伸的）的复合材料制成的嵌件的组件的方法，由复合材料制成的插入件由多个涂覆的长丝获得，每个包括涂覆有金属护套的陶瓷纤维，其特征在于 因为它包括制造插入件，该插入件具有绕垂直于所述主体的旋转轴线的旋转体周围卷绕包裹的纤维束或粘合片材的步骤。 然后将该插入物在容器中进行热等静压步骤。 该过程适用于航空涡轮机组件的制造。
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公开(公告)号：US20080304959A1
公开(公告)日：2008-12-11
申请号：US12096663
申请日：2006-12-08
申请人： Joel Michel Daniel Benoit , Jean-Francois Fromentin , Valerie Chaumat , Olivier Gillia , Nikolas Eustathopoulos , Fiqiri Hodaj , Alexey Koltsov
发明人： Joel Michel Daniel Benoit , Jean-Francois Fromentin , Valerie Chaumat , Olivier Gillia , Nikolas Eustathopoulos , Fiqiri Hodaj , Alexey Koltsov
CPC分类号： C04B37/025 , B23K35/0244 , B32B2311/22 , C04B37/026 , C04B2235/5244 , C04B2235/5248 , C04B2237/08 , C04B2237/123 , C04B2237/125 , C04B2237/16 , C04B2237/341 , C04B2237/365 , C04B2237/38 , C04B2237/405 , F01D9/023 , F02K1/78 , F02K1/822 , F02K3/10 , F05D2230/237 , F05D2230/642 , F05D2300/2261 , F23M2900/05004 , F23R3/007 , Y02T50/67 , Y02T50/672 , Y02T50/675 , Y10T428/12326 , Y10T428/12507
摘要： An assembly between a metal piece and a ceramic material piece made of SiC and/or C based ceramic material. The assembly includes a stack structure including the following elements assembled together in pairs in this order, by brazing: the metal piece; a first intermediate piece; a second intermediate piece; and the ceramic material piece. The second intermediate piece is made of another ceramic material, that is chemically less reactive relative to metals than are SiC or C, and that presents a coefficient of expansion smaller than that of the material constituting the metal piece. The first intermediate piece is made of metal and can deform to compensate for expansion difference between the metal piece and the second intermediate piece. The assembly can be used in a turbomachine.
摘要翻译： 金属片和由SiC和/或C基陶瓷材料制成的陶瓷材料片之间的组件。 组件包括堆叠结构，其包括以下顺序组合成一对的元件，通过钎焊：金属片; 第一中间件 第二中间件 和陶瓷材料片。 第二中间件由另一种陶瓷材料制成，其比SiC或C在化学上相对于金属的反应性更小，并且其膨胀系数小于构成金属片的材料的膨胀系数。 第一中间件由金属制成并且可以变形以补偿金属片和第二中间件之间的膨胀差。 该组件可用于涡轮机。
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公开(公告)号：US20080307793A1
公开(公告)日：2008-12-18
申请号：US12096714
申请日：2006-12-08
CPC分类号： C04B37/023 , B32B2311/00 , C04B2235/96 , C04B2237/121 , C04B2237/122 , C04B2237/123 , C04B2237/363 , C04B2237/365 , C04B2237/385 , C04B2237/40 , C04B2237/597 , C04B2237/76 , C04B2237/88 , F01D9/023 , F02K1/12 , F02K1/78 , F02K3/10 , F05D2230/237 , F05D2250/611 , F05D2300/2261 , F05D2300/603 , F23R3/007 , Y02T50/672 , Y02T50/675 , Y10T29/4932 , Y10T403/213 , Y10T403/217 , Y10T428/24182
摘要： An assembly including a metal piece, a piece made of ceramic material, and at least one intermediate connection element assembled to each of the pieces by brazing. The intermediate connection element includes a deformable sheet presenting at least two flat zones brazed to respective ones of the pieces, the two flat zones being interconnected by a deformable zone presenting at least two free undulations oriented in alternation towards the metal piece and towards the piece made of ceramic material.
摘要翻译： 包括金属片，由陶瓷材料制成的片的组件和通过钎焊组装到每个片的至少一个中间连接元件。 中间连接元件包括可变形片材，其呈现钎焊到相应片段的至少两个平坦区域，两个平坦区域通过可变形区域相互连接，该可变形区域具有至少两个自由波动，所述至少两个自由起伏朝着金属片方向定向， 的陶瓷材料。
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6.发明申请公开(公告)号：US20070086896A1
公开(公告)日：2007-04-19
申请号：US11427106
申请日：2006-06-28
申请人： Caroline AUMONT , Sandrine Chatel , Bruno Dambrine , Didier Escure , Jean-Francois Fromentin , Jean-yves Guedou , Ludovic Molliex , Stephane Rousselin
发明人： Caroline AUMONT , Sandrine Chatel , Bruno Dambrine , Didier Escure , Jean-Francois Fromentin , Jean-yves Guedou , Ludovic Molliex , Stephane Rousselin
IPC分类号： F04D29/38
CPC分类号： C22C49/00 , F01D5/282 , F04D29/023 , F04D29/321 , F05D2230/237 , F05D2300/133 , F05D2300/2112 , F05D2300/2261 , F05D2300/6032 , F05D2300/614
摘要： A turbomachine rotor including at least one disk having a ring constituted, for example, by a winding of metal-coated silicon carbide or alumina yarn. According to the invention, the composite ring is received in a closed annular cavity, e.g. defining by machining a groove in an enlarged portion of the disk and closing the groove by means of an annular plate after the ring has been put into place.
摘要翻译： 涡轮机转子，其包括至少一个具有环的盘，例如由金属包覆的碳化硅或氧化铝纱的卷绕构成的环。 根据本发明，复合环被接收在封闭的环形空腔中，例如， 通过在盘的扩大部分中加工凹槽并且在环已经就位之后通过环形板来闭合凹槽来限定。
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7.发明授权公开(公告)号：US08177497B2
公开(公告)日：2012-05-15
申请号：US12096663
申请日：2006-12-08
申请人： Joel Michel Daniel Benoit , Jean-Francois Fromentin , Valerie Chaumat , Olivier Gillia , Nikolas Eustathopoulos , Fiqiri Hodaj , Alexey Koltsov
发明人： Joel Michel Daniel Benoit , Jean-Francois Fromentin , Valerie Chaumat , Olivier Gillia , Nikolas Eustathopoulos , Fiqiri Hodaj , Alexey Koltsov
IPC分类号： F01D25/24
CPC分类号： C04B37/025 , B23K35/0244 , B32B2311/22 , C04B37/026 , C04B2235/5244 , C04B2235/5248 , C04B2237/08 , C04B2237/123 , C04B2237/125 , C04B2237/16 , C04B2237/341 , C04B2237/365 , C04B2237/38 , C04B2237/405 , F01D9/023 , F02K1/78 , F02K1/822 , F02K3/10 , F05D2230/237 , F05D2230/642 , F05D2300/2261 , F23M2900/05004 , F23R3/007 , Y02T50/67 , Y02T50/672 , Y02T50/675 , Y10T428/12326 , Y10T428/12507
摘要： An assembly between a metal piece and a ceramic material piece made of SiC and/or C based ceramic material. The assembly includes a stack structure including the following elements assembled together in pairs in this order, by brazing: the metal piece; a first intermediate piece; a second intermediate piece; and the ceramic material piece. The second intermediate piece is made of another ceramic material, that is chemically less reactive relative to metals than are SiC or C, and that presents a coefficient of expansion smaller than that of the material constituting the metal piece. The first intermediate piece is made of metal and can deform to compensate for expansion difference between the metal piece and the second intermediate piece. The assembly can be used in a turbomachine.
摘要翻译： 金属片和由SiC和/或C基陶瓷材料制成的陶瓷材料片之间的组件。 组件包括堆叠结构，其包括以下顺序组合成一对的元件，通过钎焊：金属片; 第一中间件 第二中间件 和陶瓷材料片。 第二中间件由另一种陶瓷材料制成，其比SiC或C在化学上相对于金属的反应性更小，并且其膨胀系数小于构成金属片的材料的膨胀系数。 第一中间件由金属制成并且可以变形以补偿金属片和第二中间件之间的膨胀差。 该组件可用于涡轮机。
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8.发明申请BRAZED JOINT BETWEEN A TITANIUM-BASED METAL PART AND A CERAMIC PART BASED ON SILICON CARBIDE (SIC) AND/OR CARBON 有权基于钛金属部件和基于碳化硅（SIC）和/或碳的陶瓷部件之间的熔接公开(公告)号：US20090068004A1
公开(公告)日：2009-03-12
申请号：US12096489
申请日：2006-12-08
CPC分类号： C04B37/025 , B32B2311/18 , C04B37/026 , C04B2235/5244 , C04B2235/5248 , C04B2237/125 , C04B2237/36 , C04B2237/365 , C04B2237/38 , C04B2237/385 , C04B2237/403 , F01D5/284 , F01D9/023 , F01D9/041 , F02K3/10 , F05D2230/237 , F05D2300/13 , F05D2300/133 , F05D2300/211 , F05D2300/224 , F05D2300/2261 , F05D2300/603 , F23M2900/05004 , F23R3/007 , Y10T428/12576 , Y10T428/12736 , Y10T428/31678
摘要： The assembly comprises a stack structure made up of the following elements assembled together in pairs by brazing: the titanium-based metal piece (10); a first intermediate piece (11) suitable for deforming to accommodate differential expansion between the metal piece (10) and a piece (20) made of ceramic material based on silicon carbide and/or carbon; a second intermediate piece (12) that is rigid, having a coefficient of expansion close to that of said ceramic material piece (20) and made of aluminum nitride (AlN) or of tungsten (W); and the ceramic material piece (20).
摘要翻译： 该组件包括由以下元件组成的堆叠结构，所述元件通过钎焊成对组装在一起：钛基金属片（10）; 第一中间件（11）适于变形以适应金属片（10）和基于碳化硅和/或碳的由陶瓷材料制成的片（20）之间的不同膨胀; 具有与所述陶瓷材料片（20）的膨胀系数接近并且由氮化铝（AlN）或钨（W）制成的膨胀系数的第二中间件（12）; 和陶瓷材料片（20）。
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公开(公告)号：US09103215B2
公开(公告)日：2015-08-11
申请号：US13368671
申请日：2012-02-08
CPC分类号： F01D5/147 , B22F3/1055 , B22F5/009 , B22F5/04 , B22F7/06 , B33Y80/00 , F05D2230/30 , F05D2240/12 , F05D2300/43 , Y02P10/295 , Y02T50/671 , Y02T50/673 , Y10T29/49336
摘要： The invention relates to a method of producing a guide vane, the method comprising a step of fabricating at least a portion of a metal body of the guide vane by additive fabrication, with at least one outside surface thereof presenting a plurality of cavities; and a step of filling said cavities with a material of lower density than the metal body in order to form at least one substantially smooth airfoil surface.
摘要翻译： 本发明涉及一种制造导向叶片的方法，该方法包括以下步骤：通过添加制造来制造导向叶片的金属体的至少一部分，其至少一个外表面具有多个空腔; 以及通过具有比金属体低密度的材料填充所述空腔以形成至少一个基本上平滑的翼面表面的步骤。
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10.发明授权Turbomachine rotor including at least one disk reinforced by a composite ring 有权涡轮机转子包括由复合环增强的至少一个盘公开(公告)号：US07334999B2
公开(公告)日：2008-02-26
申请号：US11427106
申请日：2006-06-28
申请人： Caroline Aumont , Sandrine Chatel , Bruno Jacques Gerard Dambrine , Didier Rene Andre Escure , Jean-Francois Fromentin , Jean-yves Guedou , Ludovic Edmond Camille Molliex , Stephane Rousselin
发明人： Caroline Aumont , Sandrine Chatel , Bruno Jacques Gerard Dambrine , Didier Rene Andre Escure , Jean-Francois Fromentin , Jean-yves Guedou , Ludovic Edmond Camille Molliex , Stephane Rousselin
IPC分类号： F01D5/02
CPC分类号： C22C49/00 , F01D5/282 , F04D29/023 , F04D29/321 , F05D2230/237 , F05D2300/133 , F05D2300/2112 , F05D2300/2261 , F05D2300/6032 , F05D2300/614
摘要： A turbomachine rotor including at least one disk having a ring constituted, for example, by a winding of metal-coated silicon carbide or alumina yarn. According to the invention, the composite ring is received in a closed annular cavity, e.g. defining by machining a groove in an enlarged portion of the disk and closing the groove by means of an annular plate after the ring has been put into place.
摘要翻译： 涡轮机转子，其包括至少一个具有环的盘，例如由金属包覆的碳化硅或氧化铝纱的卷绕构成的环。 根据本发明，复合环被接收在封闭的环形空腔中，例如， 通过在盘的扩大部分中加工凹槽并且在环已经就位之后通过环形板来闭合凹槽来限定。
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