公开(公告)号：US20200182087A1

公开(公告)日：2020-06-11

申请号：US16695631

申请日：2019-11-26

Applicant: Airbus Operations S.A.S.

Inventor： Mathieu Belleville ,  Jérome Colmagro

IPC: F01D25/12 ,  B64D27/24 ,  B64D27/16 ,  B64D33/08

Abstract: An engine assembly with an electric motor that includes a cooling system of which a heat sink portion is arranged in an exhaust cone downstream of the fan driven by the electric motor, that is designed to effect thermal exchanges with a wall of the exhaust cone. Such an electric rear fan arrangement with boundary layer ingestion enables a cold air flow coming from the fan when the engine assembly is in operation to be used to cool the different components of the engine assembly.

公开(公告)号：US09796142B2

公开(公告)日：2017-10-24

申请号：US14706660

申请日：2015-05-07

Applicant: Airbus Operations (S.A.S.)

Inventor： Denis Soula ,  Jérome Colmagro ,  Matthieu Plet

IPC: B29C70/52 ,  B29C35/02 ,  B29D99/00 ,  B29C70/44 ,  B29C70/46 ,  B29C70/54 ,  B29C70/68 ,  B29C70/86 ,  B29C65/00 ,  F16C7/02 ,  B29L31/06

CPC classification number: B29C70/523 ,  B29C35/0277 ,  B29C66/5324 ,  B29C66/5344 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/73754 ,  B29C66/73941 ,  B29C70/446 ,  B29C70/462 ,  B29C70/52 ,  B29C70/545 ,  B29C70/68 ,  B29C70/865 ,  B29D99/0003 ,  B29D99/0046 ,  B29L2031/06 ,  B29L2031/3076 ,  F16C7/026 ,  Y02T50/43 ,  B29K2063/00 ,  B29K2307/04

Abstract: The manufacture of structural elements for aircraft requires the use of complex and costly methods, particularly in the case of parts of elongate overall shape and variable thickness or cross section made of composite material. The disclosure herein proposes to overcome this problem by a method that allows the manufacture of a structural part from a preform made of composite material of simple shape obtained by pultrusion and of one or more reinforcing elements made of composite material and secured by cocuring with the preform to a region of this preform which region is to be reinforced.

公开(公告)号：US11421548B2

公开(公告)日：2022-08-23

申请号：US16695631

申请日：2019-11-26

Applicant: Airbus Operations S.A.S.

Inventor： Mathieu Belleville ,  Jérome Colmagro

IPC: F01D25/12 ,  B64D27/16 ,  B64D27/24 ,  B64D33/08

Abstract: An engine assembly with an electric motor that includes a cooling system of which a heat sink portion is arranged in an exhaust cone downstream of the fan driven by the electric motor, that is designed to effect thermal exchanges with a wall of the exhaust cone. Such an electric rear fan arrangement with boundary layer ingestion enables a cold air flow coming from the fan when the engine assembly is in operation to be used to cool the different components of the engine assembly.

公开(公告)号：US20150321429A1

公开(公告)日：2015-11-12

申请号：US14706660

申请日：2015-05-07

Applicant: Airbus Operations (S.A.S.)

Inventor： Denis Soula ,  Jérome Colmagro ,  Matthieu Plet

IPC: B29C70/52

CPC classification number: B29C70/523 ,  B29C35/0277 ,  B29C66/5324 ,  B29C66/5344 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/73754 ,  B29C66/73941 ,  B29C70/446 ,  B29C70/462 ,  B29C70/52 ,  B29C70/545 ,  B29C70/68 ,  B29C70/865 ,  B29D99/0003 ,  B29D99/0046 ,  B29L2031/06 ,  B29L2031/3076 ,  F16C7/026 ,  Y02T50/43 ,  B29K2063/00 ,  B29K2307/04

Abstract: The manufacture of structural elements for aircraft requires the use of complex and costly methods, particularly in the case of parts of elongate overall shape and variable thickness or cross section made of composite material. The disclosure herein proposes to overcome this problem by a method that allows the manufacture of a structural part from a preform made of composite material of simple shape obtained by pultrusion and of one or more reinforcing elements made of composite material and secured by cocuring with the preform to a region of this preform which region is to be reinforced.

Abstract translation: 用于飞机的结构元件的制造需要使用复杂和昂贵的方法，特别是在细长整体形状和可变厚度或由复合材料制成的横截面的部分的情况下。 本文的公开内容旨在通过一种方法来克服这个问题，该方法允许从由拉挤成型获得的简单形状的复合材料制成的预成型件和由复合材料制成的一个或多个增强元件制成的结构部件，并通过与预成型件共同固化而固定 到该预制件的该区域要被加强的区域。