公开(公告)号：US09328614B2

公开(公告)日：2016-05-03

申请号：US13980412

申请日：2012-01-10

申请人： Gilles Charles Casimir Klein ,  Jean-Michel Patrick Maurice Franchet ,  Gilbert Michel Marin Leconte ,  Dominique Magnaudeix

发明人： Gilles Charles Casimir Klein ,  Jean-Michel Patrick Maurice Franchet ,  Gilbert Michel Marin Leconte ,  Dominique Magnaudeix

IPC分类号： F01D5/14 ,  B21D53/78 ,  B23P15/04 ,  B23K15/00 ,  B23K15/06 ,  B23K20/02 ,  B23K26/00 ,  F04D29/02 ,  F04D29/32

CPC分类号： F01D5/147 ,  B21D53/78 ,  B23K15/0053 ,  B23K15/06 ,  B23K20/021 ,  B23K26/3584 ,  B23K2101/006 ,  B23K2101/045 ,  B23K2103/14 ,  B23P15/04 ,  F04D29/023 ,  F04D29/324 ,  F05D2230/42 ,  F05D2230/90 ,  F05D2240/303 ,  F05D2240/304 ,  F05D2300/13 ,  F05D2300/15 ,  F05D2300/174 ,  Y02T50/672 ,  Y10T29/49337

摘要： A metal reinforcing piece for mounting on a leading edge or trailing edge of a composite blade for a turbine engine is made by shaping two metal sheets, positioning them on either side of a core, assembling the two sheets together around the core under a vacuum, shaping them on the core by hot isostatic compression, and cutting them to separate the reinforcing piece and release the core. A predetermined roughness is given to at least a portion of the surface of the core and is transferred to a corresponding portion of an inside surface of the reinforcing piece by the hot isostatic compression.

摘要翻译： 用于安装在用于涡轮发动机的复合叶片的前缘或后缘上的金属加强件通过成形两个金属板，将它们定位在芯的任一侧上，在真空下将两个片组合在芯周围， 通过热等静压成型在​​芯上，并切割它们以分离加强件并释放芯。 对芯的表面的至少一部分施加预定的粗糙度，并且通过热等静压力将其转移到加强件的内表面的相应部分。

公开(公告)号：US20140208819A1

公开(公告)日：2014-07-31

申请号：US14238303

申请日：2012-08-09

申请人： Gilles Charles Casimir Klein ,  Jean-Michel Patrick, Maurice Franchet ,  Gilbet Michel, Marin Leconte ,  Dominique Magnaudeix

发明人： Gilles Charles Casimir Klein ,  Jean-Michel Patrick, Maurice Franchet ,  Gilbet Michel, Marin Leconte ,  Dominique Magnaudeix

IPC分类号： B21D53/78 ,  B21J13/02

CPC分类号： B21D53/78 ,  B21D22/22 ,  B21D43/003 ,  B21J13/02 ,  B21K3/04

摘要： A device for shaping a metal sheet by die stamping, the device including first and second trunnions configured to be fastened respectively to two opposite ends of a sheet, the sheet being configured to be shaped by die stamping, wherein the first and second trunnions define respective first and second bearing surfaces configured respectively to guide turning of the trunnions, the first bearing surface defining a peripheral groove around a pivot axis of the first trunnion while the second bearing surface is smooth along a pivot axis of the second trunnion.

摘要翻译： 一种用于通过模具冲压成形金属板的装置，该装置包括构造成分别固定在片材的两个相对端部的第一和第二耳轴，该片材被构造成通过模具冲压成形，其中第一和第二耳轴限定相应的 第一和第二轴承表面分别构造成引导耳轴的转动，第一支承表面围绕第一耳轴的枢转轴线限定周边凹槽，而第二支承表面沿着第二耳轴的枢转轴线是平滑的。

公开(公告)号：US08782887B2

公开(公告)日：2014-07-22

申请号：US13635502

申请日：2011-03-18

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein

IPC分类号： B21K3/04 ,  B23P15/04

CPC分类号： B23P15/04 ,  B21D53/78 ,  B23K20/021 ,  B23K2101/001 ,  F01D5/147 ,  F01D5/282 ,  F04D29/324 ,  F05D2230/236 ,  F05D2230/50 ,  F05D2230/60 ,  F05D2240/121 ,  F05D2240/122 ,  F05D2240/303 ,  F05D2240/304 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/49336 ,  Y10T29/49337

摘要： A method for producing a metal insert for protecting a leading or trailing edge of a compressor vane of an aeronautical machine made of a composite material, by stamping sheets and diffusion bonding between the sheets. The method includes: initially shaping the sheets by stamping to approximate the sheets to a shape of a suction side and pressure side of the insert; producing a core shaped inner cavity of the metal insert to be manufactured, one of the surfaces thereof reproducing an inner shape of the suction side of the insert and the other surface reproducing an inner shape of the pressure side of the insert; positioning the sheets around the core and securing the assembly; applying a vacuum and sealing the assembly by bonding; assembling the assembly by hot isostatic compression; cutting the assembly to extract the core and separate the insert; producing an outer profile of the insert by a final machining.

摘要翻译： 一种用于制造用于保护由复合材料制成的航空机械的压缩机叶片的前缘或后缘的金属插入件的方法，通过冲压片材和片材之间的扩散接合。 该方法包括：首先通过冲压来成形片材以将片材近似为插入物的吸力侧和压力侧的形状; 制造要制造的金属插入件的芯形内腔，其中一个表面再现插入件的吸入侧的内部形状，而另一个表面再现插入件的压力侧的内部形状; 将片材定位在芯部周围并固定组件; 施加真空并通过粘合密封组件; 通过热等静压压装配组件; 切割组件以提取芯部并分离插入件; 通过最终加工产生插入件的外部轮廓。

公开(公告)号：US20130008027A1

公开(公告)日：2013-01-10

申请号：US13635502

申请日：2011-03-18

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein

IPC分类号： B23P15/04

CPC分类号： B23P15/04 ,  B21D53/78 ,  B23K20/021 ,  B23K2101/001 ,  F01D5/147 ,  F01D5/282 ,  F04D29/324 ,  F05D2230/236 ,  F05D2230/50 ,  F05D2230/60 ,  F05D2240/121 ,  F05D2240/122 ,  F05D2240/303 ,  F05D2240/304 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/49336 ,  Y10T29/49337

摘要： A method for producing a metal insert for protecting a leading or trailing edge of a compressor vane of an aeronautical machine made of a composite material, by stamping sheets and diffusion bonding between the sheets. The method includes: initially shaping the sheets by stamping to approximate the sheets to a shape of a suction side and pressure side of the insert; producing a core shaped inner cavity of the metal insert to be manufactured, one of the surfaces thereof reproducing an inner shape of the suction side of the insert and the other surface reproducing an inner shape of the pressure side of the insert; positioning the sheets around the core and securing the assembly; applying a vacuum and sealing the assembly by bonding; assembling the assembly by hot isostatic compression; cutting the assembly to extract the core and separate the insert; producing an outer profile of the insert by a final machining.

摘要翻译： 一种用于制造用于保护由复合材料制成的航空机械的压缩机叶片的前缘或后缘的金属插入件的方法，通过冲压片材和片材之间的扩散接合。 该方法包括：首先通过冲压来成形片材以将片材近似为插入物的吸力侧和压力侧的形状; 制造要制造的金属插入件的芯形内腔，其中一个表面再现插入件的吸入侧的内部形状，而另一个表面再现插入件的压力侧的内部形状; 将片材定位在芯部周围并固定组件; 施加真空并通过粘合密封组件; 通过热等静压进行装配; 切割组件以提取芯部并分离插入件; 通过最终加工产生插入件的外部轮廓。

公开(公告)号：US20120234431A1

公开(公告)日：2012-09-20

申请号：US13512447

申请日：2010-12-15

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Richard Masson ,  Louis Salvat

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Richard Masson ,  Louis Salvat

IPC分类号： B65B13/28

CPC分类号： C22C47/068 ,  B21C47/18 ,  B21F15/06 ,  B21F15/08 ,  B21F15/10 ,  B21F23/005 ,  B22F3/002 ,  B22F3/15 ,  B22F2998/10 ,  B32B5/12 ,  B32B15/02 ,  B32B37/0084 ,  B32B37/142 ,  C22C47/20 ,  C22C49/11 ,  C22C47/04

摘要： A method for manufacturing a straight insert intended to be incorporated in a metal container by HIC includes placing coated wires in a rectilinear juxtaposition over a predefined length in a straight gutter-shaped tool and joining the coated wires together. The insert includes a bundle of coated wires that are joined together and have a predefined length. The wires are made from metal-coated ceramic fibers.

摘要翻译： 用于制造用于通过HIC并入金属容器的直插入件的方法包括将直线并排的直线并排放置在直沟槽形工具中的预定长度上并将涂覆的线连接在一起。 插入件包括一束连接在一起并具有预定长度的涂覆线。 电线由金属涂层的陶瓷纤维制成。

公开(公告)号：US08166910B2

公开(公告)日：2012-05-01

申请号：US12980942

申请日：2010-12-29

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Christian Garnier ,  Patrick Petitpas ,  Pierre Eric Frayssines ,  Mikael Dumont

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Christian Garnier ,  Patrick Petitpas ,  Pierre Eric Frayssines ,  Mikael Dumont

IPC分类号： B05C3/12

CPC分类号： C23C2/006 ,  C04B41/009 ,  C04B41/4584 ,  C04B41/52 ,  C04B41/88 ,  C04B41/90 ,  C04B2111/00982 ,  C04B41/5059 ,  C04B41/5001 ,  C04B41/4523 ,  C04B41/5133 ,  C04B14/386 ,  C04B14/324

摘要： A device used for a process of coating fibers with a metal by a liquid method is disclosed. In this process, a fiber is drawn through a bath of molten liquid metal so as to be coated with the molten liquid metal. The liquid metal bath is maintained in a crucible of the “levitation” type, which at least partly eliminates contact between the liquid metal and the crucible. The bath is fed with metal, during the process, by a metal powder.

摘要翻译： 公开了一种用于通过液体方法用金属涂覆纤维的方法的装置。 在该方法中，将纤维通过熔融液态金属浴浸渍以涂覆熔融液态金属。 将液态金属浴保持在“悬浮”型坩埚中，其至少部分地消除了液态金属和坩埚之间的接触。 在金属加工过程中，金属粉末通过金属进料。

公开(公告)号：US08084099B2

公开(公告)日：2011-12-27

申请号：US12124562

申请日：2008-05-21

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Christian Garnier ,  Patrick Petitpas ,  Pierre Eric Frayssines ,  Mikael Dumont

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Christian Garnier ,  Patrick Petitpas ,  Pierre Eric Frayssines ,  Mikael Dumont

IPC分类号： B05D1/18

CPC分类号： C23C2/006 ,  C04B41/009 ,  C04B41/4584 ,  C04B41/52 ,  C04B41/88 ,  C04B41/90 ,  C04B2111/00982 ,  C04B41/5059 ,  C04B41/5001 ,  C04B41/4523 ,  C04B41/5133 ,  C04B14/386 ,  C04B14/324

摘要： A process of coating fibers with a metal by a liquid method is disclosed. In this process, a fiber is drawn through a bath of molten liquid metal so as to coated with the latter, the liquid metal bath being maintained in a crucible of the “levitation” type, which at least partly eliminates contact between the liquid metal and the crucible. The bath is fed with metal, during the process, by a metal powder. Accordingly, the molten metal bath is fed in a simple and effective manner.

摘要翻译： 公开了一种通过液体方法用金属涂覆纤维的方法。 在此过程中，将纤维从熔融液体金属浴中拉出以涂覆该液体金属浴，将液态金属浴保持在“悬浮”型坩埚中，该坩埚至少部分地消除了液态金属与 坩埚。 在金属加工过程中，金属粉末通过金属进料。 因此，以简单有效的方式供给熔融金属浴。

公开(公告)号：US08871308B2

公开(公告)日：2014-10-28

申请号：US13322063

申请日：2010-04-20

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Gerald Sanchez

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Gerald Sanchez

IPC分类号： C23C2/00 ,  C04B41/45 ,  C04B41/00 ,  C04B41/88 ,  C22C47/04 ,  C23C2/24 ,  C23C2/38 ,  C04B111/00

CPC分类号： C04B41/4584 ,  B05D2203/30 ,  B05D2256/00 ,  B22F2999/00 ,  C04B41/009 ,  C04B41/88 ,  C04B2111/00931 ,  C04B2111/00982 ,  C22C47/04 ,  C23C2/003 ,  C23C2/24 ,  C23C2/38 ,  C04B41/4523 ,  C04B41/5133 ,  C04B14/46 ,  C04B14/4693 ,  C22B9/221

摘要： A method of coating ceramic material fibers in metal using a liquid technique and a device implementing the method. The method maintains a charge of molten metal in levitation in a substantially spherical shape inside a crucible and causes a tensioned ceramic material fiber to travel at a predetermined speed between a bottom pulley and a top pulley disposed on either side of the crucible such that a portion of fiber is immersed in the charge to be covered in a metal coating. During coating, the portion of fiber that is immersed in the charge is shifted as a function of the remaining volume of the charge such that the instantaneous height of fiber that is immersed in the charge remains substantially constant throughout the coating operation.

摘要翻译： 使用液体技术在金属中涂覆陶瓷材料纤维的方法和实现该方法的装置的方法。 该方法在坩埚内保持基本上球形的悬浮液中的熔融金属的电荷，并且使得张紧的陶瓷材料纤维以预定的速度行进在位于坩埚的任一侧的底部滑轮和顶部滑轮之间，使得部分 的纤维浸入电荷中以覆盖在金属涂层中。 在涂覆期间，浸入电荷中的纤维部分作为电荷的剩余体积的函数而移动，使得浸入电荷中的纤维的瞬时高度在整个涂覆操作中保持基本上恒定。

公开(公告)号：US08732920B2

公开(公告)日：2014-05-27

申请号：US13347108

申请日：2012-01-10

申请人： Gilbert Michel Marin Leconte ,  Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Dominique Magnaudeix

发明人： Gilbert Michel Marin Leconte ,  Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Dominique Magnaudeix

IPC分类号： B21K3/04

CPC分类号： B21D43/26 ,  B21D11/14 ,  B21D22/022 ,  B21D37/12 ,  B21D53/78 ,  B21J13/02 ,  B21K3/04 ,  B21K31/00 ,  Y10T29/37 ,  Y10T29/49336 ,  Y10T29/49996

摘要： The invention provides tooling and a method for hot forging pieces of sheet metal that are to form metal reinforcement mounted on the leading or trailing edge of a turbine engine blade, by means of bottom and top matrices each presenting a twisted elongate surface for use in shaping an initially plane piece of sheet metal, the shaping surface of the bottom matrix presenting a high portion, a low portion, and two end zones. The bottom matrix includes studs for positioning and guiding the piece, the studs being situated at the periphery of the corresponding shaping surface.

摘要翻译： 本发明提供了一种用于热锻金属片的工具和方法，所述金属片通过底部和顶部基体形成金属加强件，所述金属加强件安装在涡轮发动机叶片的前缘或后缘，每个底部和顶部基体均呈现出扭曲的细长表面，用于成型 初始平面的片状金属片，底部矩形的成形表面呈现高部分，低部分和两个端部区域。 底部矩阵包括用于定位和引导件的螺柱，螺柱位于相应的成形表面的周边。

公开(公告)号：US08684255B2

公开(公告)日：2014-04-01

申请号：US13637593

申请日：2011-03-30

申请人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Richard Masson ,  Louis Salvat

发明人： Jean-Michel Patrick Maurice Franchet ,  Gilles Charles Casimir Klein ,  Richard Masson ,  Louis Salvat

IPC分类号： B32B37/10 ,  D02G3/24 ,  D02G3/36

CPC分类号： C22C47/20 ,  B22F2998/10 ,  C22C47/04 ,  C22C47/06 ,  B22F3/15

摘要： A method of manufacturing an elongate insert configured to be integrated by CIC in a metal container, including coated yarns bonded together, the coated yarns being formed from metal-coated ceramic fibers. The method includes placing the coated yarns side by side in a bundle and pulling the fiber bundle through a shaping element so as to compact the fiber bundle transversely while forming the fiber bundle so as to have a defined cross section. A metal part incorporating a fibrous insert can be manufactured by the CIC technique.

摘要翻译： 一种制造细长插入件的方法，所述细长插入件构造成由CIC整合在金属容器中，包括粘合在一起的涂覆纱线，所述涂覆纱线由金属涂覆的陶瓷纤维形成。 该方法包括将包覆的纱线并排放置成束并将纤维束拉过成形元件，以便在形成纤维束时横向压实纤维束以具有限定的横截面。 包含纤维插入物的金属部件可以通过CIC技术制造。