首页> 外国专利> Rib structure for a box of toru00c7u00e7o a wing or horizontal stabilizer of an aircraft, and the element enrijecedor vertical to a rib structure for a box of toru00c7u00e7o

Rib structure for a box of toru00c7u00e7o a wing or horizontal stabilizer of an aircraft, and the element enrijecedor vertical to a rib structure for a box of toru00c7u00e7o

机译:飞机机翼或水平稳定器的一盒托肋的肋结构,以及与一盒托的肋结构垂直的单元增强器

摘要

Rib structure for a box of toru00c7u00e7o a wing or horizontal stabilizer of an aircraft, and the element enrijecedor vertical to a rib structure for a box of toru00c7u00e7o. It described a fin or rib structure for a box of twist of a wing or stabilizer. The horizontal of an aircraft.The structure comprises a central element which extends between the front and the rear spar spar of the torsion box, a series of elements enrijecedores vertical arranged between a top and a bottom cowl cowl box of twist.The vertical enrijecedor element consists of a first lateral wing which extends in the direction of the front spar and a second lateral wing which extends in the direction of the rear spar. Such side extensions emerge from opposite sides of the body vertically and are connected side by side to the central part of the rib.
机译:用于飞机机翼或水平稳定器的一盒tor的肋结构,以及垂直于一盒tor的肋结构的元件增强器。它描述了用于机翼或稳定器的扭转盒的鳍或肋结构。飞机的水平方向。该结构包括一个在扭力箱的前翼梁和后翼梁之间延伸的中央元件,以及一系列在顶部和底部前围整流罩之间的垂直方向布置的垂直竖立的一系列元素。由沿前翼梁方向延伸的第一侧翼和沿后翼梁方向延伸的第二侧翼组成。这样的侧向延伸部从主体的相对侧竖直地出现并且并排连接到肋的中央部分。

著录项

  • 公开/公告号BRPI0800648A2

    专利类型

  • 公开/公告日2008-12-30

    原文格式PDF

  • 申请/专利权人 AIRBUS ESPANA S.L.;

    申请/专利号BR2008PI00648

  • 发明设计人 JUAN ZUNIGA SAGREDO;

    申请日2008-03-14

  • 分类号B64C3/18;

  • 国家 BR

  • 入库时间 2022-08-21 19:28:23

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号