首页> 外国专利> Connecting unit for force transmission between flap drive and flap at e.g. airfoil wing, of e.g. fixed wing aircraft, has middle section arranged between two sections, where unit is designed as strap from fiber composite material

Connecting unit for force transmission between flap drive and flap at e.g. airfoil wing, of e.g. fixed wing aircraft, has middle section arranged between two sections, where unit is designed as strap from fiber composite material

机译:用于在襟翼驱动器和襟翼之间传递力的连接单元,例如机翼,例如固定翼飞机,中间部分位于两部分之间,其中单元由纤维复合材料制成带状

摘要

The unit (10) has a middle section (18) arranged between two sections (14, 16), where the unit is fixedly and respectively connected with a flap drive and a flap (12) over the sections (14, 16). The section (14) is fixedly and directly connected with a flap contour of the flap in a lifting direction, where the unit is designed as a strap from a fiber composite material. The middle section is guided over a flap contour area (20) in the lifting direction.
机译:单元(10)具有布置在两个部分(14、16)之间的中间部分(18),其中该单元固定地并分别在部分(14、16)上与挡板驱动器和挡板(12)连接。区段(14)在提升方向上与襟翼的襟翼轮廓固定且直接地连接,其中该单元被设计成由纤维复合材料制成的带。中间部分在升起方向上越过襟翼轮廓区域(20)。

著录项

  • 公开/公告号DE102007012984A1

    专利类型

  • 公开/公告日2008-09-18

    原文格式PDF

  • 申请/专利权人 EUROCOPTER DEUTSCHLAND GMBH;

    申请/专利号DE20071012984

  • 发明设计人 WAGNER ALOIS;

    申请日2007-03-14

  • 分类号B64C3/38;B64C9;B64C27/615;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:22

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