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Helicopter trim tab angle adjuster and measurer - has clasp connected to tab and rotatable relative to a disc fast to rotor blade

机译:直升机护板翼片角度调节器和测量器-扣环连接到翼片,可相对于固定在转子叶片上的圆盘旋转

摘要

The adjuster and measurer for the angle of incidence of trimming tabs on the rotor baldes of helicopters has a reference disc which can be laid fast onto the rotor blade, and a calsp, rotatable w.r.t. the reference disc, which can be connected to the trimming tab such that the position of the tab can be read off from a scale fitted to the reference disc. Preferably, the disc is semicircular and has an angle scale. The clasp has a slot engaging around the tab and bears a sector-shaped disc whose edge is U-shaped and slidingly embraces the semicircular edge of the reference disc. One shank of the U has a pointer which covers the scale. The angle can be measured simultaneously with the bending process.
机译:直角调整片在直升飞机旋翼秃顶上的入射角的调节器和测量器具有一个可快速放置在旋翼桨叶上的基准盘,以及一个可旋转的尖头旋转轴。参考盘,可以将其连接到修整凸耳,以便可以从安装到参考盘的刻度尺上读取凸耳的位置。优选地,盘是半圆形的并且具有角度刻度。扣具具有接合在凸片周围的狭槽,并带有扇形盘,该扇形盘的边缘为U形并可滑动地包围参考盘的半圆形边缘。 U的一个柄上有一个指针,它覆盖了刻度尺。可以在弯曲过程中同时测量角度。

著录项

  • 公开/公告号DE000002358205C3

    专利类型

  • 公开/公告日1976-07-08

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE2358205A

  • 发明设计人

    申请日1973-11-22

  • 分类号B64C27/54;

  • 国家 DE

  • 入库时间 2022-08-23 02:09:26

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