首页> 外国专利> An adjustment system for moving a flap on a wing of an aircraft, a method of moving a flap on a wing of an aircraft, and an aircraft having a wing and at least one flap movably disposed thereon

An adjustment system for moving a flap on a wing of an aircraft, a method of moving a flap on a wing of an aircraft, and an aircraft having a wing and at least one flap movably disposed thereon

机译:一种用于在飞机机翼上移动襟翼的调节系统,在飞机机翼上移动襟翼的方法以及具有机翼和至少一个可移动地布置在其上的襟翼的飞机

摘要

Adjustment system (2) for moving a flap (4) on a wing (5) of an aircraft, comprising: - an adjusting lever (6) having a first end (8) and a second end (10), - a support lever (18) a first end (20) and a second end (22), - a drive unit (15) and - a support device (30), wherein the drive unit (15) is adapted to an adjustment element (14) along a first axis (16) the adjusting system (2), wherein the first end (8) of the adjusting lever (6) with the flap (4) is coupled and the second end (10) is pivotally coupled to the adjusting element (14), wherein the first end ( 20) of the support lever (18) is coupled to a pivot point (24) arranged on the adjustment lever (6), the pivot point (24) lying between the first end (8) and the second end (10) of the adjustment lever (6), wherein the second end (22) of the support lever (18) with a receiving device (28) of the support device (30) out is finally pivotably coupled to a second axis (32) defined by the receiving device (28), and wherein the supporting device (30) is adapted to move the receiving device (28) as needed such that the orientation of the second axis (32) is opposite the first axis (16) is changed.
机译:用于在飞机机翼(5)上移动襟翼(4)的调节系统(2),包括:-具有第一端(8)和第二端(10)的调节杆(6),-支撑杆(18)第一端(20)和第二端(22),-驱动单元(15)和-支撑装置(30),其中,驱动单元(15)沿其与调节元件(14)相适配调节系统(2)的第一轴(16),其中调节杆(6)的第一端(8)与活门(4)联接,第二端(10)可枢转地联接到调节元件( 14),其中支撑杆(18)的第一端(20)耦接到布置在调节杆(6)上的枢轴点(24),该枢轴点(24)位于第一端(8)和调节杆(6)的第二端(10),其中支撑杆(18)的第二端(22)伸出支撑装置(30)的接收装置(28),最后与第二轴(32)由接收装置(28)限定,并且其中分选装置(30)适于根据需要移动接收装置(28),使得第二轴线(32)的方向与第一轴线(16)相反。

著录项

  • 公开/公告号DE102014102283B4

    专利类型

  • 公开/公告日2017-06-29

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号DE201410102283

  • 发明设计人 TANNO ZANTZ;

    申请日2014-02-21

  • 分类号B64C13/38;

  • 国家 DE

  • 入库时间 2022-08-21 13:23:01

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