Aircraft tail rod straightening device
The utility model discloses an aircraft tail rod straightening device. The device comprises stamping equipment of a pressure head and a bottom plate capable of being mounted on a working table of thestamping equipment, vertical plates are arranged at the two ends of the bottom plate in the length di...
Saved in:
Main Authors | , , , , , |
---|---|
Format | Patent |
Language | Chinese English |
Published |
30.06.2020
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | The utility model discloses an aircraft tail rod straightening device. The device comprises stamping equipment of a pressure head and a bottom plate capable of being mounted on a working table of thestamping equipment, vertical plates are arranged at the two ends of the bottom plate in the length direction, idler wheels used for bearing the tail rod are correspondingly arranged on the two vertical plates, a concave groove is formed between the two idler wheels along the upper end faces of the vertical plates, a pressing rod used for straightening the tail rod is installed on a pressing head of the stamping equipment, and a measuring device is arranged on one side of each vertical plate. The straightening device is simple in structure and convenient to use, straightening errors and straightening time can be reduced, and working efficiency is improved.
本实用新型公开了一种飞行器尾杆校直装置,包括压头的冲压设备和可安装在冲压设备工作台面上的底板,沿底板长度方向两端设有立板,沿底板长度方向两端设有立板,在两立板上对应设有用于承托尾杆的滚轮,沿立板的上端面两滚轮之间设置有凹型槽,冲压设备的压头上安装有校直尾杆的压杆,立板的一侧设置有测量装置。本实用新型结构简单使用方便、可以 |
---|---|
Bibliography: | Application Number: CN201920887043U |