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1.
公开(公告)号:US11046414B2
公开(公告)日:2021-06-29
申请号:US16202762
申请日:2018-11-28
Applicant: Airbus Operations SAS
Inventor: Franck Batalla , Denis Soula , Javier Maqueda Lahoz
Abstract: In order to be able to reduce the time and cost required for final assembly of an aircraft, a junction rib designed for the wing-central wingbox junction comprises a central web and an upper flange and a lower flange which extend from the main web, on a first side, the main web having a junction surface arranged on a second side opposite the first side, the main web including rows of orifices opening on the second side in the junction surface and on the first side, comprising a first row of orifices and a third row of orifices formed in an upper part of the main web on either side of the upper flange, and a second row of orifices formed in a lower portion of the main web, each one of the rows of orifices comprising orifices in a free state.
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公开(公告)号:US20150175252A1
公开(公告)日:2015-06-25
申请号:US14566822
申请日:2014-12-11
Applicant: AIRBUS OPERATIONS SAS
Inventor: Franck Batalla , Denis Soula , Javier Maqueda Lahoz
CPC classification number: B64C3/182 , B23K20/129 , B64C1/26 , B64F5/10 , Y10T29/49622
Abstract: A method for producing a central wing box including an upper panel, a lower panel, a front longeron, a rear longeron and four corners, wherein at least one panel and one longeron are obtained from a single flat metal wall which is bent along a bending line at approximately 90° which corresponds to a corner connecting said panel to said longeron.
Abstract translation: 一种用于制造中央翼盒的方法,包括上板,下板,前长龙,后长龙和四角,其中从弯曲的单个平板金属壁获得至少一个板和一个纵梁 线对应于将所述面板连接到所述龙门的角部的大约90°。
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