首页> 外国专利> A WING LEADING EDGE DEVICE AND A WING HAVING SUCH A WING LEADING EDGE DEVICE

A WING LEADING EDGE DEVICE AND A WING HAVING SUCH A WING LEADING EDGE DEVICE

机译:机翼领先的边缘设备和机翼具有机翼领先的边缘设备

摘要

A wing leading edge device is proposed, comprising a flow body having a front side, which is delimited by a first spanwise edge and a second spanwise edge, a back side, which is delimited by the first spanwise edge and the second spanwise edge, a front skin arranged on the front side, a back skin arranged on the back side, and at least one stiffening arrangement between the front skin and the back skin in the region of the first spanwise edge, wherein the front skin extends continuously and free from interruptions between the first spanwise edge and the second spanwise edge and covers the at least one stiffening arrangement.
机译:提出了一种机翼​​前缘装置,其包括流动体,该流动体具有由第一翼展方向边缘和第二翼展方向边缘界定的前侧,由第一翼展方向边缘和第二翼展方向边缘界定的后侧。在前侧上布置有前蒙皮,在后侧上布置有后蒙皮,并且在第一翼展方向边缘的区域中在前蒙皮和后蒙皮之间的至少一个加强结构,其中前蒙皮连续地延伸并且没有中断在第一翼展方向边缘和第二翼展方向边缘之间,并覆盖至少一个加强装置。

著录项

  • 公开/公告号EP3702268A1

    专利类型

  • 公开/公告日2020-09-02

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20200159994

  • 发明设计人 BENSMANN STEFAN;ERBAN MARCUS;FEES MARTIN;

    申请日2020-02-28

  • 分类号B64C9/22;B64C9/24;B64F5/10;

  • 国家 EP

  • 入库时间 2022-08-21 11:39:20

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