公开(公告)号：US20150300208A1

公开(公告)日：2015-10-22

申请号：US14452959

申请日：2014-08-06

Applicant: SNECMA

Inventor： Bruno Albert BEUTIN ,  Nuria LLAMAS CASTRO ,  Bruna RAMOS

IPC: F01D25/32 ,  F01D25/24

CPC classification number: F01D25/32 ,  B01D45/16 ,  F01D25/24 ,  F02C7/05 ,  F02C7/052 ,  F02C7/055 ,  F02K3/062 ,  F02K3/072 ,  F05D2220/30

Abstract: Turbine engine (110) having a nacelle (126) comprising, upstream, an air intake fairing (126a) and an element (140) for deflecting foreign objects which defines with said fairing an air intake flow path for supplying air to two coaxial flow paths, namely a radially inner and a radially outer flow path, said outer flow path being defined by a hub housing (152) and scoops, said hub housing (152) and said scoops (144) being installed downstream of the element (140) for deflecting objects, characterised in that each scoop comprises two independent portions, namely an upstream portion (144a) borne by the hub housing (152) and a downstream portion (144b) borne by the nacelle (162).

Abstract translation: 具有机舱（126）的涡轮发动机（110）包括在进气整流装置（126a）和元件（140）的上游，用于偏转用所述整流罩限定的异物，用于将空气供给到两个同轴流路 ，即径向内部和径向外部流动路径，所述外部流动路径由轮毂壳体（152）和铲斗限定，所述轮毂壳体（152）和所述铲斗（144）安装在所述元件（140）的下游，用于 偏转物体，其特征在于，每个铲斗包括两个独立的部分，即由轮毂壳体（152）承载的上游部分（144a）和由机舱（162）承载的下游部分（144b）。

公开(公告)号：US20160032755A1

公开(公告)日：2016-02-04

申请号：US14775292

申请日：2014-02-25

Applicant: SNECMA

Inventor： Bruno Albert BEUTIN ,  Carmen ANCUTA ,  Lambert Olivier, Marie DEMOULIN

IPC: F01D15/12 ,  F01D5/02 ,  F01D25/24 ,  F01D25/28 ,  F16H57/025 ,  F16H57/03

CPC classification number: F01D15/12 ,  F01D5/02 ,  F01D25/24 ,  F01D25/28 ,  F02C7/32 ,  F05D2220/30 ,  F05D2220/36 ,  F05D2250/38 ,  F05D2260/40311 ,  F16H57/025 ,  F16H57/03

Abstract: A gearbox for driving equipment of a turbomachine, including a substantially V-shaped box having two arms joined together by a joining part, the arms containing gear trains joined together at the joining part, and an attachment to the turbomachine. The attachment include a mechanism for insetting and/or for attaching the joining part and a suspension device of the arms.

Abstract translation: 一种用于驱动涡轮机的设备的齿轮箱，包括具有通过接合部分连接在一起的两个臂的大致V形的箱体，在接合部分处连接在一起的齿轮系的臂以及与涡轮机的连接。 附件包括用于插入和/或用于附接臂的连接部分和悬挂装置的机构。

公开(公告)号：US20160376990A1

公开(公告)日：2016-12-29

申请号：US15103177

申请日：2014-12-11

Applicant: SNECMA

Inventor： Carmen ANCUTA ,  Bruno Albert BEUTIN

IPC: F02C7/14 ,  F02C7/36

CPC classification number: F02C7/14 ,  F02C7/32 ,  F02C7/36 ,  F05D2250/38 ,  F05D2260/213 ,  F05D2260/4031 ,  Y02T50/675

Abstract: Aircraft turbomachine comprising at least one heat exchanger (40) and a gearbox (10) in a V-shaped overall configuration and comprising two lateral arms (20) joined together by a central joining piece, the heat exchanger being mounted between the arms of the gearbox.

Abstract translation: 包括至少一个热交换器（40）和V形整体构造的齿轮箱（10）的飞行器涡轮机，包括通过中心连接件连接在一起的两个侧臂（20），该热交换器安装在 变速箱