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    METHOD FOR MANUFACTURING A HOLLOW VANE
    1.
    发明申请
    METHOD FOR MANUFACTURING A HOLLOW VANE 审中-公开
    制造中空帆的方法

    公开(公告)号：US20130164145A1

    公开(公告)日：2013-06-27

    申请号：US13723996

    申请日：2012-12-21

    申请人： Thierry Georges Paul PAPIN

    发明人： Thierry Georges Paul PAPIN

    IPC分类号： B23P15/04 ,  F01D5/18

    CPC分类号： B23P15/04 ,  F01D5/147 ,  F05D2230/236 ,  F05D2240/12 ,  Y02T50/671 ,  Y02T50/673 ,  Y10T29/49321

    摘要： A method for manufacturing a hollow structural turbomachine vane, the method including forming a first cavity in a first face of a first block; assembling by diffusion bonding the first block and a second block, the first face of the first block being positioned facing a second face of the second block, the first cavity thus forming a closed cavity; machining the block resulting from the assembly of the first block and the second block so as to obtain a vane including the closed cavity.

    摘要翻译： 一种中空结构涡轮机叶片的制造方法，该方法包括在第一块的第一面中形成第一空腔; 通过扩散接合第一块和第二块来组装，第一块的第一面被定位成面对第二块的第二面，因此第一腔形成闭合腔; 对由第一块和第二块的组装产生的块进行加工，以获得包括封闭腔的叶片。

    Turbine engine vane plate seal
    3.
    发明授权
    Turbine engine vane plate seal 有权
    涡轮发动机叶片板密封

    公开(公告)号：US09556745B2

    公开(公告)日：2017-01-31

    申请号：US14233549

    申请日：2012-07-17

    申请人： Thierry Georges Paul Papin ,  Lise Lacroix ,  Dominique Raulin

    发明人： Thierry Georges Paul Papin ,  Lise Lacroix ,  Dominique Raulin

    IPC分类号： F04D29/38 ,  F01D9/02 ,  F01D5/14 ,  F01D9/04 ,  F04D29/54

    CPC分类号： F01D9/02 ,  F01D5/147 ,  F01D9/041 ,  F04D29/542 ,  F05D2260/96 ,  Y10T29/49316

    摘要： A plate closes the main part of a vane in two parts. An internal cavity is closed by the plate. Around a bearing surface of the plate, a groove receives an elastic seal, and the outer edge of the plate extends over the groove to compress the seal and to establish excellent leak proofing. The position of the plate may be guaranteed by centring pins penetrating into holes adjacent to the seal and which it fills when the pins have been removed, which completes the closing of the cavity. The plate has application in particular to stationary gas guide vanes in turbine engines.

    摘要翻译： 板将两个部分的叶片的主要部分关闭。 内部腔体被板关闭。 在板的轴承表面周围，凹槽接收弹性密封件，并且板的外边缘在凹槽上延伸以压缩密封并且建立优异的防漏。 板的位置可以通过定位销穿过邻近密封件的孔来确保，并且当销已经被移除时填充它，这完成了空腔的关闭。 该板特别适用于涡轮发动机中的固定气体导向叶片。

    DISC BRAKE PISTON CAP AND DISC BRAKE EQUIPPED THEREWITH
    5.
    发明申请
    DISC BRAKE PISTON CAP AND DISC BRAKE EQUIPPED THEREWITH 有权
    DISC制动活塞和碟形刹车

    公开(公告)号：US20140193250A1

    公开(公告)日：2014-07-10

    申请号：US14233549

    申请日：2012-07-17

    申请人： Thierry Georges Paul Papin ,  Lise Lacroix ,  Dominique Raulin

    发明人： Thierry Georges Paul Papin ,  Lise Lacroix ,  Dominique Raulin

    IPC分类号： F01D9/02

    CPC分类号： F01D9/02 ,  F01D5/147 ,  F01D9/041 ,  F04D29/542 ,  F05D2260/96 ,  Y10T29/49316

    摘要： A plate closes the main part of a vane in two parts. An internal cavity is closed by the plate. Around a bearing surface of the plate, a groove receives an elastic seal, and the outer edge of the plate extends over the groove to compress the seal and to establish excellent leak proofing. The position of the plate may be guaranteed by centring pins penetrating into holes adjacent to the seal and which it fills when the pins have been removed, which completes the closing of the cavity. The plate has application in particular to stationary gas guide vanes in turbine engines.

    摘要翻译： 板将两个部分的叶片的主要部分关闭。 内部腔体被板关闭。 在板的轴承表面周围，凹槽接收弹性密封件，并且板的外边缘在凹槽上延伸以压缩密封并且建立优异的防漏。 板的位置可以通过定位销穿过邻近密封件的孔来确保，并且当销已经被移除时填充它，这完成了空腔的关闭。 该板特别适用于涡轮发动机中的固定气体导向叶片。

    Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a module
    6.
    发明授权
    Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a module 有权
    用于涡轮机壳体和壳体结构的结构和空气动力学模块包括多个这样的模块

    公开(公告)号：US08740556B2

    公开(公告)日：2014-06-03

    申请号：US13031893

    申请日：2011-02-22

    申请人： Thierry Georges Paul Papin ,  Alain Raffy ,  Dominique Raulin

    发明人： Thierry Georges Paul Papin ,  Alain Raffy ,  Dominique Raulin

    IPC分类号： F01D9/04

    CPC分类号： F01D9/041 ,  F01D11/008 ,  F01D25/162 ,  F05B2260/301 ,  F05D2240/12 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/673

    摘要： A structural and aerodynamic module including two blades each extending along a longitudinal axis, in which each blade includes a leading edge, a trailing edge, a radially inner edge, and a radially outer edge, is provided. The module also includes a radially inner platform mechanically connecting the radially inner edges of the two blades, and a radially outer platform mechanically connecting the radially outer edges of the two blades such that the two blades and the radially outer and inner platforms delimit a flow stream. The two blades and the platforms are made from a composite material and the two blades are fixed on the radially outer and inner platforms using screw-nut assemblies.

    摘要翻译： 包括两个叶片的结构和空气动力学模块，每个叶片沿着纵向轴线延伸，其中每个叶片包括前缘，后缘，径向内边缘和径向外边缘。 模块还包括机械连接两个叶片的径向内边缘的径向内部平台和径向外部平台，其机械地连接两个叶片的径向外边缘，使得两个叶片和径向外部和内部平台限定流动流 。 两个叶片和平台由复合材料制成，两个叶片使用螺母组件固定在径向外平台和内平台上。

    STRUCTURAL AND AERODYNAMIC MODULE FOR A TURBOMACHINE CASING AND CASING STRUCTURE COMPRISING A PLURALITY OF SUCH A MODULE
    9.
    发明申请
    STRUCTURAL AND AERODYNAMIC MODULE FOR A TURBOMACHINE CASING AND CASING STRUCTURE COMPRISING A PLURALITY OF SUCH A MODULE 有权
    用于包含这种模块的多样性的涡轮机壳和结构的结构和空气动力学模块

    公开(公告)号：US20110229326A1

    公开(公告)日：2011-09-22

    申请号：US13031893

    申请日：2011-02-22

    申请人： Thierry Georges Paul PAPIN ,  Alain Raffy ,  Dominique Raulin

    发明人： Thierry Georges Paul PAPIN ,  Alain Raffy ,  Dominique Raulin

    IPC分类号： F01D5/22

    CPC分类号： F01D9/041 ,  F01D11/008 ,  F01D25/162 ,  F05B2260/301 ,  F05D2240/12 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/673

    摘要： The invention relates to a structure and aerodynamic module comprising two blades each extending along a longitudinal axis, each blade each comprising a leading edge, a trailing edge, a radially inner edge and a radially outer edge, the module also comprising a radially inner platform mechanically connecting the radially inner edges of the two blades, and a radially outer platform mechanically connecting the radially outer edges of the two blades such that the two blades and the radially outer and inner platforms delimit a flow stream, the two blades and the platforms being made from a composite material and the two blades being fixed on the radially outer and inner platforms using screw-nut assemblies.

    摘要翻译： 本发明涉及包括两个叶片的结构和空气动力学模块，每个叶片沿着纵向轴线延伸，每个叶片各自包括前缘，后缘，径向内边缘和径向外边缘，该模块还包括机械地 连接两个叶片的径向内边缘，以及径向外部平台，机械地连接两个叶片的径向外边缘，使得两个叶片和径向外部和内部平台限定流动流，使两个叶片和平台被制成 并且使用螺母 - 螺母组件将两个叶片固定在径向外平台和内平台上。