公开(公告)号：US09827610B2

公开(公告)日：2017-11-28

申请号：US14771785

申请日：2014-03-04

Applicant: SNECMA

Inventor： Guillaume Klein ,  Josserand Bassery ,  Sebastien Congratel ,  Raphael Dupeyre ,  David Mathieu ,  Ba-Phuc Tang

IPC: B22D25/02 ,  B22C9/22 ,  F01D5/22 ,  F01D9/02 ,  F01D11/08 ,  B23P15/02

CPC classification number: B22D25/02 ,  B22C9/22 ,  B23P15/02 ,  F01D5/225 ,  F01D9/02 ,  F01D11/08 ,  F05D2240/12 ,  F05D2240/55

Abstract: A method for producing a rotor vane (10) for a turbomachine, including producing a rough casting, the heel of which has a downstream lip (121) with a transverse increased thickness (130) such that the lip has an upstream surface (134) substantially parallel to an axis The method further includes machining said increased thickness so that the downstream lip has an upstream surface (138) inclined in relation to the axis.

公开(公告)号：US20160016227A1

公开(公告)日：2016-01-21

申请号：US14771785

申请日：2014-03-04

Applicant: SNECMA

Inventor： Guillaume Klein ,  Josserand Bassery ,  Sebastien Congratel ,  Raphael Dupeyre ,  David Mathieu ,  Ba-Phuc Tang

IPC: B22D25/02 ,  F01D11/08 ,  B22C9/22 ,  F01D9/02

CPC classification number: B22D25/02 ,  B22C9/22 ,  B23P15/02 ,  F01D5/225 ,  F01D9/02 ,  F01D11/08 ,  F05D2240/12 ,  F05D2240/55

Abstract: The invention relates to a method for producing a rotor vane (10) for a turbomachine, comprising a step consisting in producing a rough casting, the heel of which has a downstream lip (121) with a transverse increased thickness (130) such that the lip has an upstream surface (134) substantially parallel to the above-mentioned axis, said method comprising an additional step of machining said increased thickness so that the downstream lip has an upstream surface (138) inclined in relation to the above-mentioned axis.

Abstract translation: 本发明涉及一种用于制造用于涡轮机的转子叶片（10）的方法，包括一个步骤，该步骤包括制造粗铸件，其后端具有横向增加的厚度（130）的下游唇缘（121），使得 唇部具有基本上平行于上述轴线的上游表面（134），所述方法包括加工所述增加的厚度以使下游唇缘具有相对于上述轴线倾斜的上游表面（138）的附加步骤。

公开(公告)号：US09567861B2

公开(公告)日：2017-02-14

申请号：US14249851

申请日：2014-04-10

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Raphael Dupeyre ,  Guillaume Klein ,  David Mathieu ,  Ba-Phuc Tang ,  Denis Gabriel Trahot

IPC: F01D5/30 ,  F01D5/14 ,  F01D11/00

CPC classification number: F01D5/3015 ,  F01D5/147 ,  F01D5/3007 ,  F01D11/006 ,  F05D2240/30 ,  F05D2250/70 ,  Y02T50/671 ,  Y02T50/673

Abstract: A turbomachine vane for cooperating with a vane retention disk including a plurality of peripheral teeth, the vane including a shank including a neck and a bulb for cooperating with a socket of the disk so as to radially hold the shank in the socket, the socket being a space bounded by two successive teeth of the disk, a pole on top of the neck, including two side walls facing the active surface side of the vane and two side walls facing the passive surface side of the vane, each wall having a rib at a lower end of the pole, the rib extending in the direction of the side wall facing the wall and providing a function of holding the vane when the vane is retained in the disk.

Abstract translation: 一种用于与包括多个周缘齿的叶片保持盘配合的涡轮机叶片，所述叶片包括具有颈部的杆和用于与所述盘的插座配合的灯泡，以将所述柄径向地保持在所述插座中，所述插座为 由盘的两个连续的齿限定的空间，颈部顶部的极，包括面对叶片的有效表面侧的两个侧壁和面向叶片的被动表面侧的两个侧壁，每个壁具有肋 杆的下端，肋沿面向墙壁的侧壁的方向延伸，并且当叶片保持在盘中时提供保持叶片的功能。

公开(公告)号：US20150354381A1

公开(公告)日：2015-12-10

申请号：US14765816

申请日：2014-01-30

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Marion Chambre ,  Thomas Marchyllie ,  Bruno Richard ,  Romain Roullet ,  Denis Aydin

IPC: F01D9/04

CPC classification number: F01D9/041 ,  F01D11/001 ,  F01D21/045 ,  F01D25/246 ,  F05D2220/30 ,  F05D2230/10 ,  F05D2230/31 ,  F05D2230/64 ,  F05D2240/11 ,  F05D2240/57 ,  Y02T50/671 ,  Y02T50/673 ,  Y10T29/49325

Abstract: The invention concerns a fixed flow distribution blading (10) in a turbomachine, comprising two coaxial annular platforms that are internal (12) and external respectively, linked to each other by a plurality of radial blades (11), in which the internal annular platform (12) comprises an annular radial partition (120) and a blade support ring (121) extending to each side of an outer radial end of said partition (120), the blading (10) further comprising an annular sealing plate (20) mounted on the internal annular platform (12), on the upstream side of the radial partition relative to an airflow in the blading, the blading (10) being characterised in that the sealing plate (20) is mounted on the blade support ring (121), and in that it comprises a circumferential groove. The invention also concerns a method for producing such a blading and a turbomachine comprising such a blading.

Abstract translation: 本发明涉及一种涡轮机中的固定流量分布叶片（10），包括分别由内部（12）和外部分别由多个径向叶片（11）彼此连接的两个同轴环形平台，其中内部环形平台 （12）包括环形径向隔板（120）和延伸到所述隔板（120）的外径向端的每一侧的叶片支撑环（121），所述叶片（10）还包括环形密封板（20），所述环形密封板 在所述内部环形平台（12）上，相对于所述叶片中的气流在所述径向隔板的上游侧，所述叶片（10）的特征在于所述密封板（20）安装在所述叶片支撑环（121）上， 并且其包括圆周凹槽。 本发明还涉及一种用于生产这种叶片的方法和包括这种叶片的涡轮机。

公开(公告)号：US10024179B2

公开(公告)日：2018-07-17

申请号：US14762782

申请日：2014-01-22

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Marion Chambre ,  Bruno Richard ,  Romain Roullet

IPC: F01D9/02 ,  F01D11/00

Abstract: The invention relates to a fixed diffuser vanes assembly (10) for guiding flow through a turbomachine, comprising an internal annular platform (12) and a plurality of fixed vanes (11) which are mounted on this platform, the internal platform comprising a support plate (121) forming the base of said vanes, a radial annular partition (120) extending from the support plate toward an axis of the vanes assembly, and an internal ring (122) attached to the radial annular partition and having an internal surface on which an abradable material (123) is arranged, the vanes assembly being characterized in that the internal ring comprises at least one cut-out (1223) delimiting a tongue (1226), the tongue being bent to press against the radial annular partition (120). The invention also relates to a method of manufacturing such a vanes assembly and to a turbomachine incorporating such vanes.

公开(公告)号：US20150377044A1

公开(公告)日：2015-12-31

申请号：US14762782

申请日：2014-01-22

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Marion Chambre ,  Bruno Richard ,  Romain Roullet

IPC: F01D9/02

CPC classification number: F01D9/02 ,  F01D11/001 ,  F05D2230/237 ,  F05D2240/80

Abstract: The invention relates to a fixed diffuser vanes assembly (10) for guiding flow through a turbomachine, comprising an internal annular platform (12) and a plurality of fixed vanes (11) which are mounted on this platform, the internal platform comprising a support plate (121) forming the base of said vanes, a radial annular partition (120) extending from the support plate toward an axis of the vanes assembly, and an internal ring (122) attached to the radial annular partition and having an internal surface on which an abradable material (123) is arranged, the vanes assembly being characterized in that the internal ring comprises at least one cut-out (1223) delimiting a tongue (1226), the tongue being bent to press against the radial annular partition (120). The invention also relates to a method of manufacturing such a vanes assembly and to a turbomachine incorporating such vanes.

Abstract translation: 本发明涉及一种用于引导流过涡轮机的固定扩散器叶片组件（10），其包括安装在该平台上的内部环形平台（12）和多个固定叶片（11），所述内部平台包括支撑板 （121），形成所述叶片的基部;径向环形隔板（120），其从所述支撑板朝向所述叶片组件的轴线延伸;以及内环（122），其附接到所述径向环形隔板并具有内表面， 布置了可磨损材料（123），所述叶片组件的特征在于，所述内环包括限定舌部（1226）的至少一个切口（1223），所述舌部被弯曲以压靠所述径向环形隔板（120） 。 本发明还涉及一种制造这种叶片组件的方法以及结合这种叶片的涡轮机。

公开(公告)号：US10107116B2

公开(公告)日：2018-10-23

申请号：US14765816

申请日：2014-01-30

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Marion Chambre ,  Thomas Marchyllie ,  Bruno Richard ,  Romain Roullet ,  Denis Aydin

IPC: F01D9/04 ,  F01D11/00 ,  F01D21/04 ,  F01D25/24

Abstract: The invention concerns a fixed flow distribution blading (10) in a turbomachine, comprising two coaxial annular platforms that are internal (12) and external respectively, linked to each other by a plurality of radial blades (11), in which the internal annular platform (12) comprises an annular radial partition (120) and a blade support ring (121) extending to each side of an outer radial end of said partition (120), the blading (10) further comprising an annular sealing plate (20) mounted on the internal annular platform (12), on the upstream side of the radial partition relative to an airflow in the blading, the blading (10) being characterized in that the sealing plate (20) is mounted on the blade support ring (121), and in that it comprises a circumferential groove. The invention also concerns a method for producing such a blading and a turbomachine comprising such a blading.

公开(公告)号：US09638049B2

公开(公告)日：2017-05-02

申请号：US14228409

申请日：2014-03-28

Applicant: SNECMA

Inventor： Raphael Dupeyre ,  Damien Alquier ,  Sebastien Congratel ,  Guillaume Klein ,  David Mathieu ,  Ba-Phuc Tang ,  Denis Gabriel Trahot

IPC: F01D5/30 ,  F01D11/00 ,  F01D5/14

CPC classification number: F01D5/30 ,  F01D5/147 ,  F01D5/3007 ,  F01D11/006 ,  F01D11/008

Abstract: A turbine engine blade includes an airfoil connected by a platform to a middle radial wall extending axially and prolonged radially inwards by a blade root that is mountable in a slot of a disk, and the platform and the middle radial wall defining two lateral cavities situated on either side of the middle radial wall and opening out circumferentially to receive scaling members. The cavities are open downstream with two fins projecting on either side of the middle radial wall at downstream end of the middle radial wall, the fins coming to bear against two adjacent teeth of the disk between which the slot is formed. The downstream end of the middle radial wall includes a setback extending between at least one rib of the platform and the fins.

公开(公告)号：US20140308134A1

公开(公告)日：2014-10-16

申请号：US14249851

申请日：2014-04-10

Applicant: SNECMA

Inventor： Sebastien Congratel ,  Raphael DUPEYRE ,  Guillaume KLEIN ,  David MATHIEU ,  Ba-Phuc TANG ,  Denis Gabriel TRAHOT

IPC: F01D5/30

CPC classification number: F01D5/3015 ,  F01D5/147 ,  F01D5/3007 ,  F01D11/006 ,  F05D2240/30 ,  F05D2250/70 ,  Y02T50/671 ,  Y02T50/673

Abstract: A turbomachine vane for cooperating with a vane retention disk including a plurality of peripheral teeth, the vane including a shank including a neck and a bulb for cooperating with a socket of the disk so as to radially hold the shank in the socket, the socket being a space bounded by two successive teeth of the disk, a pole on top of the neck, including two side walls facing the active surface side of the vane and two side walls facing the passive surface side of the vane, each wall having a rib at a lower end of the pole, the rib extending in the direction of the side wall facing the wall and providing a function of holding the vane when the vane is retained in the disk.

Abstract translation: 一种用于与包括多个周缘齿的叶片保持盘配合的涡轮机叶片，所述叶片包括具有颈部的杆和用于与所述盘的插座配合的灯泡，以将所述柄径向地保持在所述插座中，所述插座为 由盘的两个连续的齿限定的空间，颈部顶部的极，包括面对叶片的有效表面侧的两个侧壁和面向叶片的被动表面侧的两个侧壁，每个壁具有肋 杆的下端，肋沿面向墙壁的侧壁的方向延伸，并且当叶片保持在盘中时提供保持叶片的功能。