公开(公告)号：US20180170563A1

公开(公告)日：2018-06-21

申请号：US15845330

申请日：2017-12-18

Applicant: Airbus Operations SAS ,  Airbus Operations SL

Inventor： Eric BOUCHET ,  Esteban MARTINO-GONZALEZ ,  Jerome COLMAGRO ,  Fernando INIESTA LOZANO ,  Julien MOULIS ,  Antoine ABELE

IPC: B64D27/20 ,  B64C1/16 ,  B64D27/26

CPC classification number: B64D27/20 ,  B64C1/061 ,  B64C1/16 ,  B64D27/14 ,  B64D27/26 ,  B64D2027/268 ,  B64D2033/0286 ,  Y02T50/44

Abstract: In order to reduce the congestion of the attachment means for aircraft engines in a secondary vein, a first fuselage frame has two side portions for supporting the engine, each associated with one of the two partly buried side engines, these portions being curved inwards so as to surround and follow the profile of the outer shroud of an intermediate case. The side portion is attached on this shroud through first and second attachment arrangements spaced apart from each other circumferentially, these arrangements being configured in order to allow absorption of the forces related to the torque along a longitudinal direction of the engine.

公开(公告)号：US20180066606A1

公开(公告)日：2018-03-08

申请号：US15693735

申请日：2017-09-01

Applicant: Airbus Operations (SAS)

Inventor： Olivier PAUTIS ,  Jerome COLMAGRO

IPC: F02K1/72 ,  F02K1/76

CPC classification number: F02K1/72 ,  F02K1/763 ,  F05D2260/50

Abstract: A thrust reverser system with a thrust reverser cascade and a reverser door with door segments laid out in a folded condition relatively to each other in an inactive configuration of the reverser system, and accommodated in an accommodation space located outside the secondary channel. Upon passing from the inactive configuration to the active configuration a rearward displacement of the cascade towards a nacelle aperture, released by an external movable nacelle cowl driven rearwards by the cascade, and a deployment of segments until they attain a deployed closing position within the secondary channel occurs simultaneously.

公开(公告)号：US20160152315A1

公开(公告)日：2016-06-02

申请号：US14952376

申请日：2015-11-25

Applicant: Airbus Operations S.L. ,  Airbus Operations SAS

Inventor： Esteban MARTINO GONZALEZ ,  Diego FOLCH CORTES ,  Pablo GOYA ABAURREA ,  Angel PASCUAL FUERTES ,  Sandra LINARES MENDOZA ,  Julien GUILLEMAUT ,  Eric BOUCHET ,  Jerome COLMAGRO ,  Jonathan BLANC

IPC: B64C1/06 ,  B64C3/32 ,  B64C1/12

CPC classification number: B64C1/061 ,  B64C1/06 ,  B64C1/12 ,  B64C1/16 ,  B64C1/26 ,  B64C3/32

Abstract: An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. The central element and the two lateral extensions are configured as an integrated piece.

Abstract translation: 一种包括适于位于机身周边内的中心元件的飞行器机身框架，以及从作为提升表面的纵向结构的一部分的中心元件的两侧突出到机身的周边外侧的两个侧向延伸部。 中心元件和两个横向延伸部被配置为一体的部件。