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1.
公开(公告)号:US20180170563A1
公开(公告)日:2018-06-21
申请号:US15845330
申请日:2017-12-18
发明人: Eric BOUCHET , Esteban MARTINO-GONZALEZ , Jerome COLMAGRO , Fernando INIESTA LOZANO , Julien MOULIS , Antoine ABELE
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.
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2.
公开(公告)号:US20190160606A1
公开(公告)日:2019-05-30
申请号:US16199795
申请日:2018-11-26
摘要: A device for manipulating a hollow shaft configured to create a pivot link between a first element and a second element. The manipulation device comprises a cylindrical body having a diameter variable by radial contraction or radial expansion of the cylindrical body, a module for controlling the diameter of the cylindrical body configured so that the diameter of the cylindrical body has alternatively at least a first diameter suitable for the cylindrical body to be displaced in the hollow shaft and a second diameter suitable for the cylindrical body to be blocked in the hollow shaft. The cylindrical body comprises an end configured to protrude from the hollow shaft when the cylindrical body is blocked in the hollow shaft. The manipulation device allows the alignment of the orifices due to the end configuration of the cylindrical body.
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