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Wing flap mechanism for adjusting an aerodynamic wing flap associated with a wing

机译:机翼襟翼机构,用于调节与机翼相关的空气动力学机翼襟翼

摘要

A pivoted flap mechanism for adjusting an aerodynamic pivotable flap associated with a wing, including: an actuating device including a gear device; a drive device including a drive arm that rotates about an axis, and which is structured and arranged to load the actuating device; and a flap support composed of a leading flap support portion and a trailing flap support portion. The aerodynamic pivotable flap is arranged on the flap support, and a steering arm of the gear device is swivellably coupled by a link to a part of the trailing flap support portion adjacent the leading flap support portion. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
机译:一种枢转襟翼机构,用于调节与机翼相关的气动可枢转襟翼,包括:致动装置,其包括齿轮装置;一种驱动装置,该驱动装置包括绕轴线旋转的驱动臂,该驱动臂的结构和布置为加载致动装置;襟翼支撑件由前襟翼支撑部分和后襟翼支撑部分组成。气动可枢转的襟翼布置在襟翼支撑件上,并且齿轮装置的转向臂通过连杆可旋转地联接到后襟翼支撑部分的与前襟翼支撑部分相邻的部分。本摘要既无意于定义本说明书中公开的发明,也无意以任何方式限制本发明的范围。

著录项

  • 公开/公告号DE102005016638B4

    专利类型

  • 公开/公告日2010-12-30

    原文格式PDF

  • 申请/专利权人 EADS DEUTSCHLAND GMBH;

    申请/专利号DE20051016638

  • 发明设计人

    申请日2005-04-11

  • 分类号B64C9/16;B64C13/24;

  • 国家 DE

  • 入库时间 2022-08-21 17:48:05

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