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Improvements in or relating to wing ribs for aeroplanes

机译:飞机翼肋的改进或与之相关的改进

摘要

281,658. Fiat Soc. Anon. Nov. 30, 1926, [Conrention date]. Framework; planes and wings, construction of.- A wing rib consists of a rigid triangular truss structure built up of metal tubes of quadrangular cross section. The upper and lower booms 1, 2 are tubes of rectangular cross section whilst the bracing struts 3 are of square cross section with the exception of the rear strut 4 which comprises a strip having a strengthening corrugation 5. The lower joints of the struts are arranged closer together than the upper ones and intermediate vertical struts 10 are provided as a greater load acts upon the lower boom 2. The struts are connected to the booms by plates 6 and tubular rivets, the passages in which may be used as anchorage for bracing wires. Upper and lower plates 11, 12 and 14, 15, which embrace the booms 1, 2, provide seatings for the spars which are connected to outturned tongues 13, 16 on the plates : the spars thus act as further struts for the rib.
机译:281,658。菲亚特Soc。阿农1926年11月30日,[生效日期]。框架;飞机的机翼和机翼的构造。-机翼肋由刚性的三角形桁架结构组成,该结构由四边形截面的金属管构成。上部和下部吊杆1、2是矩形横截面的管,而支撑支柱3具有正方形横截面,除了后支柱4,后支柱4包括具有加强波纹5的条。支柱的下部接头被布置由于较高的载荷作用在下部吊杆2上,因此与上部吊杆相比,它们之间的距离更近,并且提供了中间的垂直支柱10。这些支柱通过板6和管状铆钉连接到吊杆,其中的通道可用作固定电线的锚固件。包围动臂1、2的上,下板11、12和14、15提供了用于梁的支座,该梁连接到板上的向外的舌状部13、16:梁因此用作肋的另外的支柱。

著录项

  • 公开/公告号GB281658A

    专利类型

  • 公开/公告日1928-06-14

    原文格式PDF

  • 申请/专利权人 FIAT SOCIETA ANONIMA;

    申请/专利号GB19270032038

  • 发明设计人

    申请日1927-11-28

  • 分类号B64C3/18;

  • 国家 GB

  • 入库时间 2022-08-24 09:52:39

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