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1.发明授权公开(公告)号：US08707669B2
公开(公告)日：2014-04-29
申请号：US13395219
申请日：2010-09-13
CPC分类号： F16C7/02 , Y10T74/2142 , Y10T74/2144 , Y10T156/1052
摘要： The present invention relates to a method of fabricating a metal link rod (6) that is longitudinally reinforced in its thickness by fiber reinforcement (2), the method comprising the following steps: making a metal blank including at least one longitudinal housing (11, 12) leading into an edge face of the blank; inserting fiber reinforcement (2) in the housing; connecting the fiber reinforcement to the blank by metal diffusion around the fibers of the fiber reinforcement (2); and finishing the blank in order to obtain a link rod (6). The invention also provides a link rod having a metal matrix in which reinforcing fibers are embedded that extend on either side of a longitudinal axis (X) of the link rod, the fibers leading into an edge face of the link rod.
摘要翻译： 本发明涉及一种制造金属连杆（6）的方法，该金属连杆通过纤维增强件（2）在其厚度上纵向增强，该方法包括以下步骤：制造金属坯料，其包括至少一个纵向壳体（11， 12）进入坯料的边缘面; 将纤维增强件（2）插入壳体中; 通过在纤维增强件（2）的纤维周围的金属扩散将纤维增强材料连接到坯料上; 并整理坯料以获得连杆（6）。 本发明还提供一种具有金属基体的连杆，其中嵌入增强纤维，其在连杆的纵向轴线（X）的两侧延伸，纤维通向连杆的边缘面。
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2.发明授权Assembly for the manufacture of a hollow mechanical part by diffusion bonding and superplastic forming, use of such an assembly and process for manufacturing such a mechanical part 有权通过扩散接合和超塑性成型制造中空机械部件的组件，使用这种组件和制造这种机械部件的方法公开(公告)号：US07255260B2
公开(公告)日：2007-08-14
申请号：US10803957
申请日：2004-03-19
IPC分类号： B23K39/00
CPC分类号： B21D26/055 , B23K20/18 , B23K2101/001 , Y10T29/49339
摘要： A method for manufacturing an assembly including a stack of at least two primary parts, the primary parts being joined together around their periphery with the exception of a place forming a passage so as to define between the two of them a cavity, and the primary parts having, facing the cavity, at least one face that is covered, in a pattern, with a stop-off product containing a binder that can be thermally degraded, and a sealed reservoir having an open end, the end being joined in a sealed manner to the passage in the stack so as to allow communication between the internal space of the reservoir and the cavity, the reservoir being placed under a partial vacuum, this being produced so as to be non-deformable at the temperature and at the pressure at which the diffusion bonding of the said stack takes place.
摘要翻译： 一种用于制造包括至少两个主要部分的叠层的组件的方法，所述主要部件围绕其周边连接在一起，除了形成通道的位置之外，以便在其中的两个之间限定空腔，并且所述主要部件 具有面向空腔的至少一个表面，其以图案被覆盖有包含可以被热降解的粘合剂的停止产品，以及具有开口端的密封容器，所述端部以密封方式接合 到堆叠中的通道以允许储存器的内部空间和空腔之间的连通，储存器被放置在部分真空下，其被制造成在温度和压力的温度下不可变形 发生所述堆叠的扩散接合。
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公开(公告)号：US20050005445A1
公开(公告)日：2005-01-13
申请号：US10847863
申请日：2004-05-19
CPC分类号： F01D5/147 , B23K20/023 , B23K2101/001 , B23P15/04 , Y10T29/4932 , Y10T29/49339
摘要： The invention relates to a method of manufacturing a hollow blade for turbine engine comprising a foot and a rotor blade, the method comprising a production stage of two external parts (14) as well as an assembling stage via diffusion bonding of these two external parts so as to obtain a blade preform. According to the invention, the production stage of the two external parts comprises, for each of these parts, the following operations: the making via forging of a primary element (28) constituting at least a rotor blade part of the external part; the making via forging of at least a secondary element (34) intended to form at least partially a foot part of the external part; and the assembling of each secondary element (34) onto the primary element so as to obtain the external part.
摘要翻译： 本发明涉及一种制造用于涡轮发动机的中空叶片的方法，其包括脚和转子叶片，所述方法包括两个外部部件（14）的生产阶段以及通过这两个外部部件的扩散接合的组装阶段 以获得刀片预制件。 根据本发明，对于这些部件中的每一个，两个外部部件的制造阶段包括以下操作：构成至少构成外部部件的转子叶片部分的主要元件（28）的制造; 至少通过锻造形成用于至少部分地形成外部部分的脚部的次要元件（34）的制造; 以及将每个次要元件（34）组装到主元件上以便获得外部部件。
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公开(公告)号：US6132526A
公开(公告)日：2000-10-17
申请号：US213247
申请日：1998-12-17
申请人： Thierry Eric Carisey , Dipankar Banerjee , Jean-Michel Franchet , Ashok Kumar Gogia , Alain Lasalmonie , Tapash Kumar Nandy , Jean-Loup Strudel
发明人： Thierry Eric Carisey , Dipankar Banerjee , Jean-Michel Franchet , Ashok Kumar Gogia , Alain Lasalmonie , Tapash Kumar Nandy , Jean-Loup Strudel
摘要： A titanium-based intermetallic alloy having a high yield stress, a high creep resistance and sufficient ductility at ambient temperature has the following chemical composition as measured in atomic percentages:Al, from 16 to 26; Nb, from 18 to 28; Mo, from 0 to 2; Si, from 0 to 0.8; Ta, from 0 to 2; Zr, from 0 to 2; and Ti as the balance to 100; with the condition that Mo+Si+Zr+Ta>0.4%.Production, working and heat-treatment ranges adapted to the intended use of the material are also defined.
摘要翻译： 具有高屈服应力，高抗蠕变性和在环境温度下具有足够延展性的钛基金属间合金具有按原子百分比测量的以下化学组成：Al，16至26; Nb，从18到28; Mo，0〜2; Si，0〜0.8; Ta，0〜2; Zr，0〜2; 和Ti为平衡为100; 条件是Mo + Si + Zr + Ta> 0.4％。 还定义了适合材料预期用途的生产，加工和热处理范围。
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5.发明授权Method for making a composite metal part having inner reinforcements in the form of fibers, blank for implementing same and metal part thus obtained 有权制造复合金属部件的方法，所述复合金属部件具有纤维形式的内部增强件，用于实现其的坯料和由此获得的金属部件公开(公告)号：US08776343B2
公开(公告)日：2014-07-15
申请号：US13509022
申请日：2010-11-24
摘要： During implementing a composite metal part by compaction of an insert having reinforcing fibers in a metal body or container, gas used for compaction may enter the cavity formed in the container for receiving the insert between a lid covering the insert and the container, which can prevent or degrade compaction and diffusion welding of fiber sheaths of the insert therebetween and/or with walls of the cavity. To solve this problem, the present method includes initiating isostatic compaction by a phase including raising and maintaining temperature, followed by a phase including hot-feeding pressurized gas, and machining an assembly to obtain the part. The temperature raising phase includes a diffusion pre-welding of material rigidly connecting the pressure-adjusted walls of the lid and the container. The method can be used for designing parts having a tensile and compression resistance, such as parts for aircraft landing gear.
摘要翻译： 在通过在金属体或容器中压制具有增强纤维的插入件来实现复合金属部件时，用于压实的气体可以进入形成在容器中的空腔中，用于在覆盖插入件的盖子和容器之间接收插入件，这可以防止 或降低其间的插入物的纤维鞘和/或腔的壁的压实和扩散焊接。 为了解决这个问题，本方法包括通过包括升温和保持温度的相进行等静压缩，接着是包括加热加压气体的相，并加工组件以获得部件。 升温阶段包括将盖的压力调节壁和容器刚性连接的材料的扩散预焊接。 该方法可用于设计具有拉伸和抗压缩性的部件，例如用于飞机起落架的部件。
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6.发明授权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：US07987574B2
公开(公告)日：2011-08-02
申请号：US11441156
申请日：2006-05-26
CPC分类号： C22C47/064 , B22F2998/00 , B23K11/0026 , B23K2101/34 , B23K2103/16 , C22C49/11 , Y10T29/49801 , Y10T29/49968 , B22F1/025
摘要： A process for manufacturing a component with an insert made of a composite is disclosed. The composite includes a metal matrix, within which ceramic fibers extend. The insert is made of a composite which is obtained from a plurality of coated filaments, each filament includes a ceramic fiber coated with a metal sheath. The process includes 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： 公开了一种制造具有由复合材料制成的插入件的部件的方法。 复合材料包括金属基体，陶瓷纤维在其中延伸。 该插入物由多个涂覆的长丝获得的复合材料制成，每个细丝包括涂有金属护套的陶瓷纤维。 该方法包括绕垂直于所述主体的旋转轴线的旋转体围绕卷绕或粘合的涂覆丝的片材。 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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7.发明授权Process for manufacturing a tubular component with an insert made of a metal matrix composite 有权用金属基复合材料制成的插入件制造管状部件的方法公开(公告)号：US07507935B2
公开(公告)日：2009-03-24
申请号：US11420615
申请日：2006-05-26
IPC分类号： B23K26/00
CPC分类号： C22C47/064 , B22F2998/00 , B23K20/021 , B23K20/233 , B23K2101/06 , B23K2103/14 , C22C49/11 , Y10T29/49801 , B22F1/025
摘要： A process for manufacturing a tubular component with an insert made of a metal matrix composite, within which ceramic fibers extend, includes a draping step, in which a bonded sheet of coated filaments is draped around a metal mandrel. Each filament includes a ceramic fiber coated with a metal sheath, and the filaments are bonded by spot welds.
摘要翻译： 用陶瓷纤维延伸的由金属基复合材料制成的插入件制造管状部件的方法包括一个悬垂步骤，其中涂覆的长丝的粘合片围绕金属心轴覆盖。 每个灯丝包括涂覆有金属护套的陶瓷纤维，并且灯丝通过点焊接合。
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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：US20060269746A1
公开(公告)日：2006-11-30
申请号：US11420648
申请日：2006-05-26
申请人： Jean-Michel Franchet , Gilles Klein , Louis Salvat
发明人： Jean-Michel Franchet , Gilles Klein , Louis Salvat
CPC分类号： C22C47/064 , B22F2998/00 , B23K26/22 , B23K2101/16 , B23K2101/34 , B23K2103/16 , B23K2103/172 , C22C49/11 , Y10T428/2913 , Y10T428/2918 , Y10T428/2933 , Y10T428/294 , Y10T428/2956 , Y10T428/2958 , B22F1/025
摘要： Process for manufacturing a coiled insert of coated filaments, each filament comprising a ceramic fiber coated with a metal sheath, characterized in that it includes a step of winding a sheet of coated filaments onto a piece, in which step, at the start of winding, a metal shim for catching the internal part of the insert is coiled and, at the end of winding, a metal shim for catching the external part of the insert is coiled. The process is applied to the manufacture of aeronautical turbomachine components.
摘要翻译： 用于制造涂覆长丝的盘绕插入件的方法，每个细丝包括涂覆有金属护套的陶瓷纤维，其特征在于，其包括将一片涂覆的长丝卷绕到一块上的步骤，在该步骤中，在卷绕开始时， 用于捕获插入件的内部的金属垫片被卷绕，并且在卷绕结束时，用于捕获插入件的外部部分的金属垫片被卷绕。 该过程适用于航空涡轮机组件的制造。
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10.发明申请Hollow fan blade for turbine engine and method of manufacturing such a blade 审中-公开用于涡轮发动机的空心风扇叶片及其制造方法公开(公告)号：US20050002786A1
公开(公告)日：2005-01-06
申请号：US10847860
申请日：2004-05-19
摘要： The invention relates to a method of manufacturing a single-piece hollow fan blade for turbine engines comprising a foot (2) extended by a rotor blade (4) in a radial direction, the method comprising the following stages: making via forging of a single-piece fan blade (1) with a plurality of inserts; and eliminating of the inserts so as to obtain a plurality of recesses (16) in this blade. The invention also relates to such a blade (1) fitted with a plurality of recesses (16) each extending substantially and radially along a curved central line (18).
摘要翻译： 本发明涉及一种用于涡轮发动机的单片中空风扇叶片的制造方法，其包括在径向方向上由转子叶片（4）延伸的脚部（2），该方法包括以下步骤：通过锻造单个 风扇叶片（1）具有多个插入件; 并且消除刀片以便在该刀片中获得多个凹槽（16）。 本发明还涉及装配有多个凹槽（16）的这种刀片（1），每个凹槽基本上沿着弯曲的中心线（18）径向延伸。
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