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公开(公告)号:US09346533B2
公开(公告)日:2016-05-24
申请号:US13419791
申请日:2012-03-14
CPC分类号: B64C3/185 , B64C3/187 , B64C3/34 , B64D2211/00 , Y10T29/49826 , Y10T403/32861
摘要: An aircraft wing includes a rib attached by a joint to a tubular spar that varies in cross sectional shape during flight. The joint includes a ring attached to the tubular spar, and pivot pins connecting the ring with the rib. The pivot pins allow relative movement between the rib and the tubular spar as the tubular spar varies in cross sectional shape.
摘要翻译: 飞机机翼包括通过接头附接到在飞行中横截面形状变化的管状翼梁的肋。 接头包括附接到管状翼梁的环和连接环与肋的枢轴销。 当管状翼梁的截面形状变化时,枢轴销允许肋和管状翼梁之间的相对移动。
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公开(公告)号:US20130240671A1
公开(公告)日:2013-09-19
申请号:US13419791
申请日:2012-03-14
CPC分类号: B64C3/185 , B64C3/187 , B64C3/34 , B64D2211/00 , Y10T29/49826 , Y10T403/32861
摘要: An aircraft wing includes a rib attached by a joint to a tubular spar that varies in cross sectional shape during flight. The joint includes a ring attached to the tubular spar, and pivot pins connecting the ring with the rib. The pivot pins allow relative movement between the rib and the tubular spar as the tubular spar varies in cross sectional shape.
摘要翻译: 飞机机翼包括通过接头附接到在飞行中横截面形状变化的管状翼梁的肋。 接头包括附接到管状翼梁的环和连接环与肋的枢轴销。 当管状翼梁的截面形状变化时,枢轴销允许肋和管状翼梁之间的相对移动。
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