公开(公告)号：US20160237840A1

公开(公告)日：2016-08-18

申请号：US15024752

申请日：2014-09-23

Applicant: SNECMA

Inventor： Mathieu Louis Jean Leduc ,  Pierre-Louis Alexander Carlos ,  Clement Roussille

IPC: F01D11/00 ,  F01D5/12 ,  F01D5/30

CPC classification number: F01D11/006 ,  F01D5/12 ,  F01D5/3015 ,  F01D11/001 ,  F05D2220/32 ,  F05D2240/30 ,  F05D2240/81 ,  F05D2300/6033 ,  Y02T50/672

Abstract: The invention concerns a rotary assembly for a turbomachine, comprising a disk of which the outer periphery is formed from an alternation of cavities and teeth (12), and blades extending radially from the disk and of which the roots (16) are engaged axially and held radially in the cavities of the disk. According to the invention, the teeth of the disk and the blade roots comprise, at the upstream and/or downstream axial ends of same, axial shoulders (74, 76) disposed circumferentially end-to-end in alternation and together forming a cylindrical surface (78) facing radially towards the inside of the disk.

Abstract translation: 本发明涉及一种用于涡轮机的旋转组件，其包括盘，其外周由空腔和齿（12）的交替形成，以及从盘径向延伸的叶片，根部（16）轴向地接合， 径向保持在盘的空腔中。 根据本发明，盘和叶根的齿在相同的上游和/或下游的轴向端部包括轴向肩部（74,76），其沿周向端对端交替设置并一起形成圆柱形表面 （78）径向朝向盘的内部。

公开(公告)号：US10267172B2

公开(公告)日：2019-04-23

申请号：US15024274

申请日：2014-09-23

Applicant: Snecma

Inventor： Mathieu Louis Jean Leduc ,  Pierre-Louis Alexandre Carlos ,  Clement Roussille

IPC: F01D5/08 ,  F01D5/22 ,  F01D5/30 ,  F01D11/00

Abstract: The invention concerns a rotary assembly for a turbomachine, comprising: a disc (16) having an external periphery having an alternation of slots (22) and teeth (20), blades (14) extending radially from the disc (16), and the roots (24) of which are engaged axially and held radially in the slots (22) of the disc, platforms (30) extending circumferentially from the blades (14) and which are arranged circumferentially end to end, opposite each other, axial sealing means upstream and/or downstream of an annular zone extending radially from the platforms (30) as far as the disc (16). According to the invention, the sealing means comprise radially an internal annular part (64) and an external annular part (66) structurally separate from each other, and the facing radial ends of which are adapted for a relative radial movements by sliding sealingly, only an absorption of the centrifugal forces of the external part (66) being provided rotationally by the platforms (30).

公开(公告)号：US20160222810A1

公开(公告)日：2016-08-04

申请号：US15024274

申请日：2014-09-23

Applicant: SNECMA

Inventor： Mathieu Louis Jean Leduc ,  Pierre-Louis Alexandre Carlos ,  Clement Roussille

IPC: F01D11/00 ,  F01D5/22 ,  F01D5/30 ,  F01D5/08

CPC classification number: F01D11/006 ,  F01D5/087 ,  F01D5/22 ,  F01D5/3007 ,  F01D5/3015 ,  F01D11/001 ,  F05D2220/323 ,  F05D2300/6033 ,  Y02T50/672

Abstract: The invention concerns a rotary assembly for a turbomachine, comprising: a disc (16) having an external periphery having an alternation of slots (22) and teeth (20), blades (14) extending radially from the disc (16), and the roots (24) of which are engaged axially and held radially in the slots (22) of the disc, platforms (30) extending circumferentially from the blades (14) and which are arranged circumferentially end to end, opposite each other, axial sealing means upstream and/or downstream of an annular zone extending radially from the platforms (30) as far as the disc (16). According to the invention, the sealing means comprise radially an internal annular part (64) and an external annular part (66) structurally separate from each other, and the facing radial ends of which are adapted for a relative radial movements by sliding sealingly, only an absorption of the centrifugal forces of the external part (66) being provided rotationally by the platforms (30).

Abstract translation: 本发明涉及一种用于涡轮机的旋转组件，包括：盘（16），其外周具有交替的槽（22）和齿（20），从盘（16）径向延伸的叶片（14） 根部（24）轴向接合并径向保持在盘的槽（22）中，平台（30）从叶片（14）周向延伸并且彼此相对地彼此端对端布置，轴向密封装置 在从平台（30）径向延伸到盘（16）的环形区域的上游和/或下游。 根据本发明，密封装置径向地包括内部环形部分（64）和在结构上彼此分离的外部环形部分（66），并且其相对的径向端部仅通过密封滑动适于相对径向移动 所述外部部件（66）的离心力的吸收由所述平台（30）旋转地设置。

公开(公告)号：US10662795B2

公开(公告)日：2020-05-26

申请号：US15024752

申请日：2014-09-23

Applicant: Snecma

Inventor： Mathieu Louis Jean Leduc ,  Pierre-Louis Alexandre Carlos ,  Clement Roussille

IPC: F01D11/00 ,  F01D5/30 ,  F01D5/12

Abstract: The invention concerns a rotary assembly for a turbomachine, comprising a disk of which the outer periphery is formed from an alternation of cavities and teeth (12), and blades extending radially from the disk and of which the roots (16) are engaged axially and held radially in the cavities of the disk. According to the invention, the teeth of the disk and the blade roots comprise, at the upstream and/or downstream axial ends of same, axial shoulders (74, 76) disposed circumferentially end-to-end in alternation and together forming a cylindrical surface (78) facing radially towards the inside of the disk.

公开(公告)号：US20140205463A1

公开(公告)日：2014-07-24

申请号：US14117507

申请日：2012-05-11

Applicant: SNECMA ,  HERAKLES

Inventor： Ivan Herraiz ,  Clement Roussille ,  Julien Mateo ,  Alain Allaria ,  Jean-Luc Soupizon

IPC: F01D5/28

CPC classification number: F01D5/282 ,  F01D5/225 ,  F05B2240/33 ,  F05D2240/307 ,  F05D2300/603 ,  Y02T50/672 ,  Y10T29/49337

Abstract: A turbine rotor includes a plurality of blades of composite material comprising fiber reinforcement densified by a matrix. Each blade comprises a blade body extending between an inner end having a blade root and an outer end forming the tip of the blade. The rotor also includes outer platform elements of composite material comprising fiber reinforcement densified by a matrix, each outer platform element including an opening in which the outer end of a blade is engaged. The portion of the outer end of each blade that extends beyond the outer platform element includes a slot or a notch for receiving a locking element.

Abstract translation: 涡轮转子包括复合材料的多个叶片，其包括由基体致密化的纤维增强材料。 每个叶片包括在具有叶片根部的内端和形成叶片的尖端的外端之间延伸的叶片体。 转子还包括复合材料的外平台元件，其包括由基体致密化的纤维增强材料，每个外平台元件包括开口，叶片的外端接合在该开口中。 每个叶片的外端部延伸超过外平台元件的部分包括用于接收锁定元件的槽或凹口。