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    PROCESS FOR MANUFACTURING A METAL PART REINFORCED WITH CERAMIC FIBRES
    11.
    发明申请
    PROCESS FOR MANUFACTURING A METAL PART REINFORCED WITH CERAMIC FIBRES 有权
    用陶瓷纤维增强金属部件的工艺

    公开(公告)号：US20110107579A1

    公开(公告)日：2011-05-12

    申请号：US13002514

    申请日：2009-07-03

    申请人： Patrick Dunleavy ,  Richard Masson

    发明人： Patrick Dunleavy ,  Richard Masson

    IPC分类号： B23P17/00

    CPC分类号： C22C47/04 ,  B22F2998/00 ,  C22C47/20 ,  F16C7/02 ,  F16C2220/00 ,  Y10T29/49 ,  Y10T29/4932 ,  Y10T29/49801 ,  Y10T29/49826 ,  B22F3/15

    摘要： The invention relates to a process for manufacturing a metal part reinforced with ceramic fibres, in which: at least one housing (10A) for an insert is machined in a metal body (10) having an upper face (10B); at least one insert (11) formed from ceramic fibres in a metal matrix is placed in the housing; the insert is covered with a cover; a vacuum is created in the interstitial space around the insert and said space is hermetically sealed under vacuum; the assembly, namely the metal body with the cover, is treated by hot isostatic pressure; and said treated assembly is machined in order to obtain said part. The process is characterized in that the cover comprises an element (12) covering the insert (11) in the slot and projecting from the upper face, and a sheet (14) covering the upper face with said element (12). In particular, the insert (11) is straight and the housing for the insert in the metal body forms a straight slot.

    摘要翻译： 本发明涉及一种用陶瓷纤维增强的金属部件的制造方法，其中：在具有上表面（10B）的金属体（10）中加工用于插入件的至少一个壳体（10A） 将由金属基体中的陶瓷纤维形成的至少一个插入件（11）放置在壳体中; 插入物被盖子覆盖; 在插入件周围的间隙空间中产生真空，并且所述空间在真空下气密密封; 组装，即具有盖的金属体，通过热等静压处理; 并且对所述经处理的组件进行加工以获得所述部件。 该方法的特征在于，盖包括覆盖槽中的插入件（11）并从上表面突出的元件（12）和覆盖上表面的所述元件（12）的片（14）。 特别地，插入件（11）是直的，并且用于插入物在金属体中的壳体形成直槽。

    Method for manufacturing a structural part made of a composite material and including a radially oriented double yoke
    12.
    发明授权
    Method for manufacturing a structural part made of a composite material and including a radially oriented double yoke 有权
    用于制造由复合材料制成并包括径向取向的双轭的结构件的方法

    公开(公告)号：US09387623B2

    公开(公告)日：2016-07-12

    申请号：US14236688

    申请日：2012-08-06

    申请人： Richard Masson ,  Thierry Rougier ,  Patrick Dunleavy

    发明人： Richard Masson ,  Thierry Rougier ,  Patrick Dunleavy

    IPC分类号： B29C70/68 ,  B29C65/72 ,  B29C70/54 ,  B29C70/86 ,  B29C70/22 ,  B29C70/24 ,  B64C25/60 ,  F16C7/02 ,  B29K105/08 ,  B29C70/48

    CPC分类号： B29C65/72 ,  B29C70/222 ,  B29C70/24 ,  B29C70/48 ,  B29C70/543 ,  B29C70/865 ,  B29C2791/001 ,  B29K2105/0827 ,  B64C25/60 ,  F16C7/026 ,  F16C2326/43

    摘要： A method of fabricating an aircraft landing gear rocker beam comprising a body having a clevis (24) with two lugs (19, 21) parallel to a direction that is radial relative to the body, the method comprising the steps of: forming a first mandrel; applying one or more first braided fiber layers (11) on the first mandrel; fitting a second mandrel element on the assembly as constituted in this way, the second mandrel element extending between the two lugs (19, 21) of the clevis (24) that is to be formed; applying one or more second braided fiber layers (17) on the assembly as constituted in this way; injecting resin into the various layers (11, 17) and polymerizing the resin; and machining the resulting workpiece blank in order to cut away a region of the second braided layers (17) in order to separate the two lugs (19, 21) of the clevis (24) from each other.

    摘要翻译： 一种制造飞机起落架摇摆梁的方法，包括具有平行于相对于主体径向的方向的两个凸耳（19,21）的U形夹（24）的本体，所述方法包括以下步骤：形成第一心轴 ; 在第一心轴上施加一个或多个第一编织纤维层（11）; 在所述组件上装配第二心轴元件，如此构成，所述第二心轴元件在要形成的所述U形夹（24）的两个凸耳（19,21）之间延伸; 在组件上施加一个或多个第二编织纤维层（17），如此构成; 将树脂注入各层（11,17）并聚合树脂; 以及加工所得到的工件坯件，以便切除第二编织层（17）的区域，以将U形夹（24）的两个凸耳（19,21）彼此分开。

    METHOD FOR MANUFACTURING AN ARM IN COMPOSITE MATERIAL COMPRISING A TRANSVERSAL BEARING DESIGNED TO RECEIVE A FIXED OR ROTATING SHAFT
    13.
    发明申请
    METHOD FOR MANUFACTURING AN ARM IN COMPOSITE MATERIAL COMPRISING A TRANSVERSAL BEARING DESIGNED TO RECEIVE A FIXED OR ROTATING SHAFT 有权
    用于制造包含设计用于接收固定或旋转轴的横向轴承的复合材料中的ARM的方法

    公开(公告)号：US20130098539A1

    公开(公告)日：2013-04-25

    申请号：US13637291

    申请日：2011-03-24

    申请人： Richard Masson ,  Patrick Dunleavy

    发明人： Richard Masson ,  Patrick Dunleavy

    IPC分类号： F01L1/18

    CPC分类号： F01L1/18 ,  B29C70/222 ,  B29C70/24 ,  B29C70/48 ,  B29C70/545 ,  B29C70/86 ,  B29L2031/06 ,  B60G2206/7101 ,  D04C3/48 ,  F16C7/026

    摘要： The invention relates to a method for manufacturing an arm (16) in composite material, this arm comprising a main body incorporating a bearing (22) designed to receive a shaft passing through it transversely, this method comprising the steps of: manufacturing a hub (11) by winding reinforcing fibres around a generally tubular support (12); manufacturing at least one sleeve (14); attaching the hub (11) to one end of the sleeve (14) and transversely to the sleeve (14) in order to form a mandrel; applying one or more layers of braided reinforcing fibres (21) around this mandrel with a machine for braiding reinforcing fibres (19); injecting and polymerizing resin into the layer or layers of braided fibres (21). The invention applies notably to an arm forming an undercarriage rocker arm of an aircraft.

    摘要翻译： 本发明涉及一种用于制造复合材料中的臂（16）的方法，该臂包括主体，该主体结合有轴承（22），该轴承设计成横向穿过轴的轴承（22），该方法包括以下步骤： 通过将增强纤维缠绕在大致管状的支撑件（12）周围; 制造至少一个套筒（14）; 将轮毂（11）附接到套筒（14）的一端并横向于套筒（14），以形成心轴; 使用用于编织增强纤维（19）的机器在该心轴周围施加一层或多层编织增强纤维（21）; 将树脂注入和聚合成编织纤维层（21）。 本发明特别适用于形成飞机底盘摇臂的臂。

    METHODS FOR PRODUCING A PART MADE FROM A COMPOSITE MATERIAL, OBTAINED BY DEPOSITING LAYERS OF REINFORCING FIBERS URGED ONTO A MANDREL
    14.
    发明申请
    METHODS FOR PRODUCING A PART MADE FROM A COMPOSITE MATERIAL, OBTAINED BY DEPOSITING LAYERS OF REINFORCING FIBERS URGED ONTO A MANDREL 审中-公开
    用于生产由复合材料制成的部件的方法，通过将加强在纤维上的纤维层沉积成层

    公开(公告)号：US20120279635A1

    公开(公告)日：2012-11-08

    申请号：US13511750

    申请日：2010-12-16

    申请人： Richard Masson ,  Patrick Dunleavy ,  Bertrand Desjoyeaux

    发明人： Richard Masson ,  Patrick Dunleavy ,  Bertrand Desjoyeaux

    IPC分类号： B29C70/32

    CPC分类号： B29C70/32 ,  B29C53/566 ,  B29C53/70 ,  B29C53/8083 ,  B29C70/222 ,  B29C70/48 ,  B29C70/543 ,  B29K2307/00 ,  B29L2023/22

    摘要： The invention relates to a method of fabricating a composite material part in which one or more layers of braided, or woven, or indeed draped reinforcing fibers are applied onto a mandrel having the general shape of a body of revolution. After one or more layers have been applied onto the mandrel, an operation is performed of winding at least one tie helically around and along the assembly constituted by the mandrel and each layer of reinforcing fibers that it carries, so as to press each layer of reinforcing fibers against the mandrel. The invention relates to fabricating composite material parts such as beams, connecting rods, or arms made out of carbon fibers.

    摘要翻译： 本发明涉及一种制造复合材料部件的方法，其中将一层或多层编织或织造或实际上覆盖的增强纤维施加到具有旋转体的大体形状的心轴上。 在一个或多个层已经施加到心轴上之后，执行一个操作，该方法是将由至少一个螺旋部分螺旋地缠绕在其周围并且沿着由心轴及其所携带的每层增强纤维构成的组件，以便按压每层增强 针对心轴的纤维。 本发明涉及制造复合材料部件，例如由碳纤维制成的梁，连杆或臂。

    Apparatus Comprising an End Fitting Connected to a Body
    16.
    发明申请
    Apparatus Comprising an End Fitting Connected to a Body 有权
    包括连接到身体的端部接头的设备

    公开(公告)号：US20120163905A1

    公开(公告)日：2012-06-28

    申请号：US13392439

    申请日：2010-08-24

    申请人： David Bond ,  Paul Trowbridge ,  Andrew Smith ,  Richard Masson ,  Patrick Dunleavy

    发明人： David Bond ,  Paul Trowbridge ,  Andrew Smith ,  Richard Masson ,  Patrick Dunleavy

    IPC分类号： B23P11/00 ,  F16B11/00

    CPC分类号： B29C70/86 ,  B29C53/585 ,  B29C70/30 ,  B29C70/48 ,  B29L2031/75 ,  F16C7/026 ,  Y02T50/43 ,  Y10T29/49826 ,  Y10T403/37 ,  Y10T403/47 ,  Y10T403/475

    摘要： An apparatus includes a fitting connected to a body. The fitting has an engagement portion including a channel formed into a peripheral surface of it and an axis. The body includes an axial layer provided around at least some of the peripheral surface of the engagement portion of the end fitting and a hoop layer provided around the axial layer at a location corresponding to at least some of the channel so as to urge at least some of the axial layer into a portion of the channel. The channel is arranged such that at least some of it defines a pathway that is non-orthogonal with respect to the axis of the fitting, such that at least some of the surface area of the channel defines a load bearing surface for the transfer of torque between the fitting and body when a rotational force is applied to one of them.

    摘要翻译： 一种装置包括连接到主体的配件。 该配件具有接合部分，该接合部分包括形成其周边表面的通道和轴线。 主体包括围绕端部配件的接合部分的周边表面中的至少一些设置的轴向层，以及围绕轴向层设置的环向层，所述环向层位于对应于至少一些通道的位置处，以便至少推动一些 的轴向层进入通道的一部分。 通道布置成使得其中的至少一些限定了相对于配件的轴线非正交的路径，使得通道的至少一些表面区域限定用于转矩的承载表面 当对其中一个施加旋转力时，在配件和主体之间。

    METHOD FOR MANUFACTURING A COMPOSITE MATERIAL CONNECTING ROD HAVING REINFORCED ENDS
    17.
    发明申请
    METHOD FOR MANUFACTURING A COMPOSITE MATERIAL CONNECTING ROD HAVING REINFORCED ENDS 有权
    复合材料制造方法连接加固钢筋的方法

    公开(公告)号：US20120103502A1

    公开(公告)日：2012-05-03

    申请号：US13264650

    申请日：2010-04-15

    申请人： Richard Masson ,  Patrick Dunleavy

    发明人： Richard Masson ,  Patrick Dunleavy

    IPC分类号： B29C70/24

    CPC分类号： B29C70/48 ,  B29C70/222 ,  B29C70/32 ,  B29C70/86 ,  B29L2031/75

    摘要： In the field of aviation, a method of fabricating a composite-material rod. The method comprises a first step of fabricating a mandrel comprising a sleeve of composite material and solid inserts of composite material secured to the ends of said sleeve to constitute a rigid whole. Then, one or more layers of braided fibers are applied around the mandrel by using a fiber-braiding machine. Next, a resin is injected into the layers of braided fibers so as to establish cohesion rigidly bonding the braided fiber layers and at least the ends of the mandrel in order to form a rod body out of composite material having reinforced ends. Finally, respective holes are drilled at each end of the rod body, each hole passing through the layers of braided fibers and also through the corresponding insert.

    摘要翻译： 在航空领域，制造复合材料棒的方法。 该方法包括制造心轴的第一步骤，所述心轴包括复合材料的套筒和固定到所述套筒的端部以构成刚性整体的复合材料的实心插入件。 然后，使用纤维编织机将一层或多层编织纤维施加在心轴周围。 接下来，将树脂注入到编织纤维层中，以便建立刚性结合编织纤维层和至少芯棒端部的内聚力，以便从具有加强端部的复合材料形成杆体。 最后，在杆体的每个端部钻出相应的孔，每个孔穿过编织纤维层并且还穿过相应的插入件。

    Method for manufacturing an arm in composite material comprising a transversal bearing designed to receive a fixed or rotating shaft
    18.
    发明授权
    Method for manufacturing an arm in composite material comprising a transversal bearing designed to receive a fixed or rotating shaft 有权
    用于制造复合材料中的臂的方法，包括设计成接收固定或旋转轴的横向轴承

    公开(公告)号：US08980032B2

    公开(公告)日：2015-03-17

    申请号：US13637291

    申请日：2011-03-24

    申请人： Richard Masson ,  Patrick Dunleavy

    发明人： Richard Masson ,  Patrick Dunleavy

    IPC分类号： B29C70/24 ,  B29C70/48 ,  B29C70/86 ,  F01L1/18 ,  B29C70/22 ,  B29C70/54 ,  D04C3/48 ,  F16C7/02 ,  B29L31/06

    CPC分类号： F01L1/18 ,  B29C70/222 ,  B29C70/24 ,  B29C70/48 ,  B29C70/545 ,  B29C70/86 ,  B29L2031/06 ,  B60G2206/7101 ,  D04C3/48 ,  F16C7/026

    摘要： The invention relates to a method for manufacturing an arm (16) in composite material, this arm comprising a main body incorporating a bearing (22) designed to receive a shaft passing through it transversely, this method comprising the steps of: manufacturing a hub (11) by winding reinforcing fibers around a generally tubular support (12); manufacturing at least one sleeve (14); attaching the hub (11) to one end of the sleeve (14) and transversely to the sleeve (14) in order to form a mandrel; applying one or more layers of braided reinforcing fibers (21) around this mandrel with a machine for braiding reinforcing fibers (19); injecting and polymerizing resin into the layer or layers of braided fibers (21). The invention applies notably to an arm forming an undercarriage rocker arm of an aircraft.

    摘要翻译： 本发明涉及一种用于制造复合材料中的臂（16）的方法，该臂包括主体，该主体结合有轴承（22），该轴承设计用于容纳横向穿过该轴的轴承，该方法包括以下步骤： 通过将增强纤维缠绕在大致管状的支撑件（12）周围; 制造至少一个套筒（14）; 将轮毂（11）附接到套筒（14）的一端并横向于套筒（14），以形成心轴; 使用用于编织增强纤维（19）的机器在该心轴周围施加一层或多层编织增强纤维（21）; 将树脂注入和聚合成编织纤维层（21）。 本发明特别适用于形成飞机底盘摇臂的臂。