公开(公告)号：US20150097342A1

公开(公告)日：2015-04-09

申请号：US14509276

申请日：2014-10-08

Applicant: SNECMA

Inventor： Serge Rene MORREALE ,  Arnaud Jean-Marie PIERROT

IPC: F01D11/04 ,  F16J15/447 ,  F01D11/02

CPC classification number: F01D11/04 ,  F01D11/02 ,  F01D11/025 ,  F16J15/164 ,  F16J15/40 ,  F16J15/447 ,  F16J15/4472 ,  F16J15/453

Abstract: One of the components (15), opposite a labyrinth seal (12), is arranged sliding on a conical interface (18) of its support (7, 19) and constructed from a material with different thermal expansions, so as to reduce the clearance with the component face to face (13, 14), at steady state, at high temperature. The sealing surface (25) may be assured by a circulation of oil.

Abstract translation: 与迷宫式密封件（12）相对的部件（15）中的一个被布置成在其支撑件（7,19）的圆锥形接口（18）上滑动并且由具有不同热膨胀的材料构成，以便减小间隙 与组件面对面（13,14）在稳定状态下处于高温下。 可以通过油的循环来确保密封表面（25）。

公开(公告)号：US20160305283A1

公开(公告)日：2016-10-20

申请号：US15099880

申请日：2016-04-15

Applicant: SNECMA

Inventor： Serge Rene MORREALE ,  Dominik IGEL

IPC: F01D25/18 ,  F01D25/16 ,  F16J15/00 ,  F16J15/3252 ,  F16J15/447 ,  F16J15/3268

CPC classification number: F01D25/183 ,  F01D11/02 ,  F01D25/16 ,  F02C7/28 ,  F05D2220/30 ,  F05D2240/55 ,  F05D2260/98 ,  F16J15/002 ,  F16J15/162 ,  F16J15/324 ,  F16J15/3252 ,  F16J15/3268 ,  F16J15/442 ,  F16J15/447

Abstract: A sealing device for a turbine engine bearing oil enclosure including a rotor shaft; an annular cover secured to an engine casing and arranged around the rotor shaft to co-operate therewith to define an oil enclosure that is to receive a bearing (8) rotatably supporting the rotor shaft relative to the engine casing; a labyrinth seal mounted on the rotor shaft facing one end of the cover; an annular rim mounted inside the cover; a dynamic annular gasket interposed radially between the rim and the rotor shaft; and a clip for axially blocking the rim inside the cover and including at least one latch passing radially through the rim and being received radially inside a groove formed in the cover, is provided.

Abstract translation: 一种用于涡轮发动机的密封装置，其具有包括转子轴的油封壳; 固定到发动机壳体上的环形盖，围绕转子轴布置以与其配合，以限定油封，该油封可容纳相对于发动机壳体可旋转地支撑转子轴的轴承; 安装在转子轴上的迷宫式密封件，其面向盖的一端; 安装在所述盖内的环形边缘; 动态环形垫片径向插入在轮​​辋和转子轴之间; 以及夹子，其用于轴向地阻挡所述盖内的轮辋并且包括至少一个通过所述轮辋径向穿过并且径向地容纳在形成在所述盖中的凹槽内的闩锁。

公开(公告)号：US20150300191A1

公开(公告)日：2015-10-22

申请号：US14646872

申请日：2013-11-27

Applicant: SNECMA

Inventor： Serge Rene MORREALE ,  Francois Jean COMIN ,  Arnaud Jean-Marie PIERROT

IPC: F01D11/00 ,  F16J15/32 ,  B23P19/04

CPC classification number: F01D11/001 ,  B23P19/04 ,  F01D11/003 ,  F05D2240/56 ,  F16J15/3268 ,  F16J15/3288

Abstract: An assembly forming a gasket for a turbomachine, includes a brush seal made of a plurality of sealing elastic bristles surrounding a core, a retaining ring including a recess to at least partly accommodate the brush seal, and a bearing cover, placed in contact with the brush seal to hold it in position against the retaining ring, the brush seal being located between the retaining ring and the bearing cover.

Abstract translation: 形成用于涡轮机的垫圈的组件包括由围绕芯部的多个密封弹性刷毛制成的刷子密封件，包括至少部分地容纳刷子密封件的凹部的保持环以及与该密封件接触的轴承盖 刷密封件将其保持在抵靠保持环的位置，刷密封件位于保持环和轴承盖之间。