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1. 发明授权

EP2433860B1 Aircraft rib-spar joint 有权
标题翻译： Rippen-HolmverbindungfürFlugzeug
公开(公告)号：EP2433860B1
公开(公告)日：2017-03-01
申请号：EP11180571.9
申请日：2011-09-08
申请人： Airbus Operations Limited
发明人： Bestwick, Richard , Grant, Scott
IPC分类号： B64C1/06 , B64C3/18 , B64F5/00
CPC分类号： B64C3/187 , B64C3/185 , B64F5/10 , Y10T29/49622 , Y10T29/4978 , Y10T29/53978 , Y10T408/55

2. 发明公开

EP2433860A3 Aircraft rib-spar joint 有权
标题翻译： RippenholmverbindungfürFlugzeug
公开(公告)号：EP2433860A3
公开(公告)日：2016-03-16
申请号：EP11180571.9
申请日：2011-09-08
申请人： Airbus Operations Limited
发明人： Bestwick, Richard , Grant, Scott
IPC分类号： B64C1/06 , B64C3/18 , B64F5/00
CPC分类号： B64C3/187 , B64C3/185 , B64F5/10 , Y10T29/49622 , Y10T29/4978 , Y10T29/53978 , Y10T408/55
摘要： A method of forming a rib-spar joint during assembly of an aircraft wing, the method comprising: providing a spar with a fixedly attached rib post, the rib post having a first coordination feature; providing a rib having a web with a first tooling feature; providing a tooling component having a second tooling feature for cooperating with the first tooling feature, a second coordination feature for cooperating with the first coordination feature, and a plurality of drill bushings; fixedly attaching the tooling component to the rib web by aligning the first and second tooling features; aligning the rib with the spar by aligning the first and second coordination features; drilling fastener holes in the rib and the rib post off the drill bushings of the tooling component; removing the tooling component from the rib web; and fastening the rib to the rib post using the fastener holes to form a rib-spar joint. The method may be applied to form front and/or rear rib-spar joints.
摘要翻译：一种在飞行器机翼的组装期间形成肋 - 翼梁接头的方法，所述方法包括：提供具有固定附接的肋柱的翼梁，所述肋柱具有第一协调特征; 提供具有带有第一工具特征的网的肋; 提供具有用于与所述第一工具特征配合的第二工具特征的模具部件，用于与所述第一协调特征配合的第二协调特征以及多个钻套筒; 通过对准第一和第二工具特征将工具组件固定地附接到肋腹板; 通过对准第一和第二协调特征使肋与翼梁对准; 在所述肋和所述肋中钻紧所述紧固件孔，从所述工具部件的所述钻套筒中脱出; 从所述肋腹板上移除所述加工部件; 并使用所述紧固件孔将所述肋条紧固到所述肋柱上以形成肋 - 翼梁接头。该方法可以应用于形成前肋和/或后肋骨接头。

3. 发明公开

EP2433860A2 Aircraft rib-spar joint 有权
标题翻译：飞机肋骨铁路连接
公开(公告)号：EP2433860A2
公开(公告)日：2012-03-28
申请号：EP11180571.9
申请日：2011-09-08
申请人： Airbus Operations Limited
发明人： Bestwick, Richard , Grant, Scott
IPC分类号： B64C1/06 , B64C3/18 , B64F5/00
CPC分类号： B64C3/187 , B64C3/185 , B64F5/10 , Y10T29/49622 , Y10T29/4978 , Y10T29/53978 , Y10T408/55
摘要： A method of forming a rib-spar joint during assembly of an aircraft wing, the method comprising: providing a spar with a fixedly attached rib post, the rib post having a first coordination feature; providing a rib having a web with a first tooling feature; providing a tooling component having a second tooling feature for cooperating with the first tooling feature, a second coordination feature for cooperating with the first coordination feature, and a plurality of drill bushings; fixedly attaching the tooling component to the rib web by aligning the first and second tooling features; aligning the rib with the spar by aligning the first and second coordination features; drilling fastener holes in the rib and the rib post off the drill bushings of the tooling component; removing the tooling component from the rib web; and fastening the rib to the rib post using the fastener holes to form a rib-spar joint. The method may be applied to form front and/or rear rib-spar joints.

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