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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
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.
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公开(公告)号：US10371009B2
公开(公告)日：2019-08-06
申请号：US15113543
申请日：2015-01-20
Applicant: SNECMA
Inventor： Mario Cesar De Sousa , Benoit Argemiro Matthieu Debray , Paul Moreau , Frederic Noel
Abstract: The invention relates to a turbomachine casing (1) comprising: a hub (2), an outer shroud (3), and yokes (11) projecting from the outer shroud (3), for attaching the housing (1), characterized in that it comprises at least one stiffener (10) extending between pairs of yokes (11) facing each other, and comprising a central part (18) and side arms (19) projecting from the central part (18).
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公开(公告)号：US20170108225A1
公开(公告)日：2017-04-20
申请号：US15391578
申请日：2016-12-27
Applicant: SNECMA
Inventor： Jacques Marcel Arthur BUNEL , Mario Cesar De Sousa , Gilles Ulryck
CPC classification number: F02C7/20 , F02C7/266 , F05D2220/32 , F05D2240/35 , F05D2260/99 , F23R3/06 , F23R3/60 , F23R2900/00005 , F23R2900/00012
Abstract: A device for mounting a spark plug in a combustion chamber of a gas turbine engine includes a chimney including a collar extending radially inwards, a washer fastened on an axial end of the chimney so as to project towards the inside of the chimney, and a bushing forming a spark plug guide and including an inner collar and an outer collar that are axially spaced apart from each other by a cylindrical portion. Each collar extends radially outwards. The bushing is floatingly mounted inside the chimney with its collars axially positioned between the collar of the chimney and the washer. The inner collar comes in operation to bear against the collar of the chimney. The outer collar presents an outside diameter (d1) greater than the inside diameter (d2) of the washer.
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4.发明申请GAS TURBINE ENGINE COMPRISING AN EXHAUST CONE ATTACHED TO THE EXHAUST CASING 有权气体涡轮发动机，包括排放在排气管上的排气公开(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
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。
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公开(公告)号：US10273904B2
公开(公告)日：2019-04-30
申请号：US14931604
申请日：2015-11-03
Applicant: SNECMA
Inventor： Benoit Argemiro Matthieu Debray , Mario Cesar De Sousa , Gregory Ghosarossian-Prillieux , Frederic Noel
Abstract: The invention relates to a fairing (37) for a mixer (28) of a nozzle (26) of a dual-flow turbomachine (20), said mixer being of an overall annular shape and extending along a longitudinal axis (24) of the turbomachine, said mixer comprising an upstream part (29) provided with a flange (31) extending radially toward the outside of the mixer, intended to be fastened to an exhaust casing (21) of the turbomachine, and a downstream part (33) forming a flow mixing area, the fairing (37) being of an overall annular shape and configured to extend around the upstream part (29) of the mixer (28) and to be attached to the flange (31) of said upstream part (29), the fairing being without means for fastening to the downstream part (33) of the mixer (28), in such a way as to connect the fairing (37) to the mixer (28) at a distance from the flow mixing area.
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Patent Agency Ranking
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
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).
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公开(公告)号：US09399952B2
公开(公告)日：2016-07-26
申请号：US13974849
申请日：2013-08-23
Applicant: SNECMA
Inventor： Mario Cesar De Sousa , Baghdad Achbari , Luc Henri Claude Daguenet , Benoit Debray
CPC classification number: F02C7/20 , F01D9/065 , F01D25/162 , F01D25/243 , F01D25/30 , F02K1/386 , F02K1/48 , F02K1/80 , F05D2230/60 , Y02T50/671 , Y10T29/49321
Abstract: A method for assembling a nozzle and an exhaust case of a turbomachine is disclosed. The exhaust case includes a hub and an outer ferrule connected to each other by a plurality of arms. The nozzle is attached to the outer ferrule of the exhaust case substantially at the trailing edges of the arms.
Abstract translation: 公开了一种用于组装涡轮机的喷嘴和排气箱的方法。 排气箱包括通过多个臂彼此连接的毂和外套圈。 喷嘴基本上在臂的后缘附接到排气箱的外套圈。
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公开(公告)号：US20160131077A1
公开(公告)日：2016-05-12
申请号：US14931604
申请日：2015-11-03
Applicant: SNECMA
Inventor： Benoit Argemiro Matthieu Debray , Mario Cesar De Sousa , Gregory Ghosarossian-Prillieux , Frederic Noel
CPC classification number: F02K1/40 , F01D25/243 , F02K1/386 , F02K1/48 , F02K3/04 , F02K3/06 , F05D2230/232 , F05D2250/311 , F05D2260/941 , Y02T50/671
Abstract: The invention relates to a fairing (37) for a mixer (28) of a nozzle (26) of a dual-flow turbomachine (20), said mixer being of an overall annular shape and extending along a longitudinal axis (24) of the turbomachine, said mixer comprising an upstream part (29) provided with a flange (31) extending radially toward the outside of the mixer, intended to be fastened to an exhaust casing (21) of the turbomachine, and a downstream part (33) forming a flow mixing area, the fairing (37) being of an overall annular shape and configured to extend around the upstream part (29) of the mixer (28) and to be attached to the flange (31) of said upstream part (29), the fairing being without means for fastening to the downstream part (33) of the mixer (28), in such a way as to connect the fairing (37) to the mixer (28) at a distance from the flow mixing area.
Abstract translation: 本发明涉及一种用于双流涡轮机（20）的喷嘴（26）的混合器（28）的整流罩（37），所述混合器具有整体环形形状，并且沿着纵向轴线（24）延伸 涡轮机，所述混合器包括设置有朝向混合器外部径向延伸的凸缘（31）的上游部分（29），用于紧固到涡轮机的排气外壳（21），以及形成 流动混合区域，整流罩（37）为整体环形，并且构造成围绕混合器（28）的上游部分（29）延伸并附接到所述上游部分（29）的凸缘（31） 整流罩没有用于紧固到混合器（28）的下游部分（33）的方式，以便将整流罩（37）连接到距离混合区域一定距离的混合器（28）。
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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
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.
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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
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.
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