公开(公告)号：US09951650B2

公开(公告)日：2018-04-24

申请号：US14547525

申请日：2014-11-19

Applicant: SNECMA

Inventor： Frederic Noel ,  Benoit Argemiro Matthieu Debray ,  Mario Cesar De Sousa ,  Gregory Ghosarossian-Prillieux ,  Nicolas Pommier

IPC: F01D25/16 ,  F02C7/06 ,  F01D25/18 ,  F16C33/76 ,  F16C35/04 ,  F16C35/067

CPC classification number: F01D25/162 ,  F01D25/18 ,  F02C7/06 ,  F05D2220/323 ,  F05D2230/232 ,  F05D2240/50 ,  F16C33/76 ,  F16C35/045 ,  F16C35/067

Abstract: The invention relates to a turbomachine bearing support (1) supporting at least one bearing and extending according to a longitudinal principal axis of the turbomachine and comprising: a truncated part (11) having a diameter increasing from upstream to downstream; a flange part (12) which extends from the truncated part (11) as far as the bearing (5, 6) to which it is fixed by an axial flange (121), and having at its downstream end a radial internal flange (17) fixed to an oil inlet cover defining with the bearing (5, 6) an oil inlet container (170); oiled air clearance ducts (71) projecting downstream relative to the flange part (12) and on the oil inlet container (170) and to the other side upstream of the flange part (12) directly radially externally relative to the axial flange (121).

公开(公告)号：US10006307B2

公开(公告)日：2018-06-26

申请号：US14903266

申请日：2014-07-07

Applicant: SNECMA

Inventor： Benoit Debray ,  Gregory Ghosarossian-Prillieux ,  Mario De Sousa ,  Nicolas Pommier ,  Frederic Noel

IPC: F01D25/16 ,  F01D25/24 ,  F01D25/30 ,  F01D9/02 ,  F02C7/20 ,  F02K1/04

CPC classification number: F01D25/243 ,  F01D9/02 ,  F01D25/162 ,  F01D25/30 ,  F02C7/20 ,  F02K1/04 ,  F05D2220/323 ,  F05D2230/10

Abstract: The present invention relates to a turbine engine casing (1), in particular a turbojet exhaust casing, including at least one hoop (2) and at least one flange (3, 4) at least partially defining one end of said hoop (2), and at least one cap (5) positioned at least partially on the outer surface of the hoop (2), said cap (5) including a bore (6) capable of receiving an element for fastening the casing (1) to a bracket, the flange including an access cut-out (7a) substantially coaxial with the bore (6) of said at least one cap (5), said access cut-out (7a) enabling access to the bore (6), the access cut-out (7a) being provided at a release cut-out (7b) which is wider than the flange (3, 4) and constitutes a recess on said release cut-out (7b). The invention also relates to a turbine engine including a casing (1) and to a method for machining the latter according to the present invention.

公开(公告)号：US09897011B2

公开(公告)日：2018-02-20

申请号：US14403305

申请日：2013-06-20

Applicant: SNECMA

Inventor： Mario Cesar De Sousa ,  Baghdad Achbari ,  Benoit Argemiro Matthieu Debray ,  Sylvain Pichon ,  Gregory Ghosarossian-Prillieux ,  Frederic Noel ,  Nicolas Pommier ,  Mathieu Ange Poisson

IPC: F02C1/00 ,  F02C7/32 ,  F01D25/24 ,  F02K1/04 ,  F02K1/80 ,  F01D25/30

CPC classification number: F02C7/32 ,  F01D25/24 ,  F01D25/30 ,  F02K1/04 ,  F02K1/80 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/91

Abstract: An assembly including an exhaust casing and an exhaust cone for a gas turbine engine, each including an axial annular flange, the two flanges being inserted into one another, one being radially external and the other radially internal, and held together by a mechanical attachment, and the assembly further including a guide by which, during operation of assembling the annular flanges to each other, the exhaust cone is in a predetermined angular position relative to the exhaust casing.

公开(公告)号：US20150152788A1

公开(公告)日：2015-06-04

申请号：US14403305

申请日：2013-06-20

Applicant: SNECMA

Inventor： Mario Cesar De Sousa ,  Baghdad Achbari ,  Benoit Argemiro Matthieu Debray ,  Sylvain Pichon ,  Gregory Ghosarossian-Prillieux ,  Frederic Noel ,  Nicolas Pommier ,  Mathieu Ange Poisson

IPC: F02C7/32 ,  F01D25/30

CPC classification number: F02C7/32 ,  F01D25/24 ,  F01D25/30 ,  F02K1/04 ,  F02K1/80 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/91

Abstract: An assembly including an exhaust casing and an exhaust cone for a gas turbine engine, each including an axial annular flange, the two flanges being inserted into one another, one being radially external and the other radially internal, and held together by a mechanical attachment, and the assembly further including a guide by which, during operation of assembling the annular flanges to each other, the exhaust cone is in a predetermined angular position relative to the exhaust casing.

Abstract translation: 一种包括用于燃气涡轮发动机的排气罩和排气锥的组件，每个包括轴向环形凸缘，两个凸缘彼此插入，一个在径向外部，另一个径向内部，并通过机械附件保持在一起， 并且所述组件还包括引导件，通过所述引导件，在将所述环形凸缘彼此组装的操作期间，所述排气锥体相对于所述排气外壳处于预定的角度位置。

公开(公告)号：US09970320B2

公开(公告)日：2018-05-15

申请号：US14439998

申请日：2013-10-22

Applicant: SNECMA

Inventor： Mario Cesar De Sousa ,  Frederic Noel ,  Nicolas Pommier ,  Olivier Renon

IPC: F01D25/16 ,  F01D25/24 ,  F01D25/28 ,  F01D9/04

CPC classification number: F01D25/162 ,  F01D9/04 ,  F01D25/243 ,  F01D25/28

Abstract: An exhaust housing hub of a turbomachine, including a connecting wall and an inner channel wall, the connecting wall connecting the inner channel wall to inner attachment flanges, wherein a radial section of the connecting wall is curved and can be formed, as required, as a single component with the inner channel wall, the hub also including a series of ribs extending radially between the connecting wall and the inner channel wall.

公开(公告)号：US09932857B2

公开(公告)日：2018-04-03

申请号：US15037642

申请日：2014-11-18

Applicant: SNECMA

Inventor： Frederic Noel ,  Benoit Argemiro Matthieu Debray ,  Mario Cesar De Sousa ,  Gregory Ghosarossian-Prillieux ,  Nicolas Pommier

IPC: F01D25/16 ,  F02C7/06 ,  F01D25/18 ,  F16C33/76 ,  F16C35/04 ,  F16C35/067

CPC classification number: F01D25/162 ,  F01D25/18 ,  F02C7/06 ,  F05D2220/323 ,  F05D2230/232 ,  F05D2240/50 ,  F16C33/76 ,  F16C35/045 ,  F16C35/067

Abstract: A bypass engine bearing holder (1) that holds an upstream bearing (6) and defines, with said upstream bearing, an oil chamber (100) and an air chamber (200), comprising a frusto-conical portion (11) defining an upstream bearing chamber (160) and a downstream inner chamber (150), and includes an outer collar (13) connected, by a weld (135), to a flange (15) that extends outward from the frusto-conical portion (11). The outer collar (13) has a sealable gimlet (131) engaging with the upstream bearing (6) such as to seal the oil chamber (100). The bearing holder (1) includes a plurality of oil recovery ducts (8) leading to the downstream inner chamber (150) and to the upstream bearing chamber (160). The oil recovery ducts (8) lead to the upstream bearing chamber (160), downstream from the weld (135) of the outer collar (13) on the flange (15), the weld (135) of the outer collar (13) being axisymmetric.

公开(公告)号：US20150285098A1

公开(公告)日：2015-10-08

申请号：US14439998

申请日：2013-10-22

Applicant: SNECMA

Inventor： Mario Cesar De Sousa ,  Frederic Noel ,  Nicolas Pommier ,  Olivier Renon

IPC: F01D25/16 ,  F01D25/24

CPC classification number: F01D25/162 ,  F01D9/04 ,  F01D25/243 ,  F01D25/28

Abstract: The invention relates to an exhaust (1) housing (1) hub (2) of a turbomachine, comprising a connecting wall (22) and an inner channel wall (20), the connecting wall (22) connecting the inner channel wall (20) to inner attachment flanges (24), wherein a radial section of the connecting wall (22) is curved and can be formed, as required, as a single component with the inner channel wall (20), the hub also comprising a series of ribs (28) extending radially between the connecting wall (22) and the inner channel wall (20).

Abstract translation: 本发明涉及一种包括连接壁（22）和内通道壁（20）的涡轮机（1）的外壳（1）轮毂（2），连接壁（22）将内通道壁（20 ）连接到内部附接凸缘（24），其中连接壁（22）的径向部分是弯曲的并且可以根据需要形成为具有内部通道壁（20）的单个部件，毂还包括一系列 在连接壁（22）和内通道壁（20）之间径向延伸的肋（28）。