专利检索 ap:("Airbus Operations SAS" OR "Airbus Operations SL") AND inv:"Fernando INIESTA LOZANO" 第 1 页

1.

发明申请
REAR PORTION OF AN AIRCRAFT COMPRISING A FUSELAGE FRAME SUPPORTING TWO PARTLY BURIED ENGINES 审中-公开

公开(公告)号：US20180170563A1

公开(公告)日：2018-06-21

申请号：US15845330

申请日：2017-12-18

申请人： Airbus Operations SAS , Airbus Operations SL

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

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

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

摘要： 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.