首页> 外国专利> Support wing profile for commercial aircraft; has profiled edge with skin parts and perpendicular ribs having planar elements connected between skin parts by rotating joints

Support wing profile for commercial aircraft; has profiled edge with skin parts and perpendicular ribs having planar elements connected between skin parts by rotating joints

机译:商用飞机的机翼轮廓;具有带皮肤部件的异型边缘和垂直肋,该肋具有通过旋转接头在皮肤部件之间连接的平面元件

摘要

The support wing profile (1) has a profiled edge (2) with two skin parts (10,20) extending from it and perpendicular ribs (5). The ribs have planar elements (30), which are arranged with their planar surfaces perpendicular to the profile edge and are rotated about joint axles (36,38) arranged in triangles parallel to the profile edge. The ribs have a flexible longitudinal structure (11,50) next to each skin part. Two joint axles of each planar element are connected to the longitudinal structure of one skin part and the other axle is connected to the longitudinal structure of the other part.
机译:支撑翼轮廓(1)具有轮廓边缘(2),该轮廓边缘具有从其延伸的两个蒙皮部分(10,20)和垂直肋(5)。肋具有平面元件(30),这些平面元件的平面垂直于轮廓边缘布置,并且绕着以平行于轮廓边缘的三角形布置的关节轴(36,38)旋转。肋在每个皮肤部位附近具有柔性纵向结构(11,50)。每个平面元件的两个关节轴连接到一个蒙皮部分的纵向结构,而另一根轴连接到另一蒙皮部分的纵向结构。

著录项

  • 公开/公告号DE19936721A1

    专利类型

  • 公开/公告日2001-02-15

    原文格式PDF

  • 申请/专利权人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT EV;

    申请/专利号DE1999136721

  • 发明设计人 PABSCH ARNO;

    申请日1999-08-06

  • 分类号B64C3/48;

  • 国家 DE

  • 入库时间 2022-08-22 01:10:22

相似文献

  • 专利
  • 外文文献
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