公开(公告)号：US09789948B2

公开(公告)日：2017-10-17

申请号：US14448807

申请日：2014-07-31

申请人： Airbus Operations (S.A.S.)

发明人： Yannick Marin ,  Emilie Luche

IPC分类号： B64C1/12 ,  B64F5/10 ,  B64C1/06

CPC分类号： B64C1/12 ,  B64C1/061 ,  B64C1/068 ,  B64F5/10 ,  Y02P70/585 ,  Y10T29/4981 ,  Y10T29/49947

摘要： A system with attachment clips designed to fix an attachment element of an aircraft fuselage frame onto a fuselage skin and/or to stiffeners fitted onto this fuselage skin is provided. The system includes tooling elements arranged alternately with the clips such that they connect to each other, in order to reduce the fabrication time and cost of an aircraft fuselage.

公开(公告)号：US20150034763A1

公开(公告)日：2015-02-05

申请号：US14448768

申请日：2014-07-31

申请人： Airbus Operations (S.A.S.)

发明人： Yannick Marin ,  Damien Guilloteau ,  Emilie Luche

IPC分类号： B64C1/06

CPC分类号： B64C1/061 ,  B64C1/064 ,  Y10T29/49622

摘要： In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a tab for the fastening of the frame element onto the fuselage stiffener, with the tab being a single piece with the core and connected to the latter by a fold that delimits the opening.

摘要翻译： 为了减少制造飞机机身的时间和成本，本文公开的主题提供了一种飞机机身框架元件，其包括设置有用于机身加强件通过的至少一个通孔的芯体， 与每个开口相关联的用于将框架元件紧固到机身加强件上的突片，其中突片与芯部是单件式的，并且通过限定开口的折叠部与芯片连接。

公开(公告)号：US09745043B2

公开(公告)日：2017-08-29

申请号：US14448768

申请日：2014-07-31

申请人： Airbus Operations (S.A.S.)

发明人： Yannick Marin ,  Damien Guilloteau ,  Emilie Luche

IPC分类号： B64C1/00 ,  B64C1/06

CPC分类号： B64C1/061 ,  B64C1/064 ,  Y10T29/49622

摘要： In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a tab for the fastening of the frame element onto the fuselage stiffener, with the tab being a single piece with the core and connected to the latter by a fold that delimits the opening.

公开(公告)号：US09527606B2

公开(公告)日：2016-12-27

申请号：US14448779

申请日：2014-07-31

申请人： Airbus Operations (S.A.S.)

发明人： Yannick Marin ,  Damien Guilloteau

IPC分类号： B64C1/00 ,  B23P11/00 ,  B64F5/00 ,  B64C1/06 ,  B64C1/12

CPC分类号： B64F5/0009 ,  B64C1/061 ,  B64C1/12 ,  B64F5/10 ,  Y10T29/49826 ,  Y10T29/53978

摘要： To reduce the time and cost of manufacture of an aircraft fuselage, a tool for positioning mounting clamps to attach a fuselage frame element onto a fuselage skin and/or onto stiffeners is provided. Accordingly, the tool includes a ramp and several systems for holding clamps in position distributed along the ramp, where each system includes a mobile device for applying pressure to the clamp, together with an adjustment device coupled to the mobile device such that its separation from the ramp is adjustable.

摘要翻译： 为了减少制造飞机机身的时间和成本，提供了用于定位安装夹具以将机身框架元件附接到机身皮肤和/或加强件上的工具。 因此，该工具包括斜坡和几个系统，用于将夹具保持在沿着坡道分布的位置，其中每个系统包括用于向夹具施加压力的移动装置以及耦合到移动装置的调节装置，使得其与 斜坡可调。