导弹发射箱发射导轨倾角偏差检测方法  

Obliquity Deviation Measuring Method of Launching Guide Track of Missile Launching Container

作　　者：赵耀辉[1] 胡秉飞[1] 高海波 李红英[1] 

机构地区：[1]中国兵器工业第五九研究所,重庆400039 [2]总装军代局驻重庆地区军代室,重庆400039

出　　处：《包装工程》2012年第7期137-139,145,共4页Packaging Engineering

摘　　要：提出了发射箱发射导轨倾角偏差的转换公式,给出了一种简易、快捷的发射导轨倾角偏差检测方法,并设计了专用的检测工装。最后,详细介绍了检测流程,并提出了检测结果的判定准则。A conversion formula of obliquity deviation of launching guide track of missile launching container was put forward. A simple and fast method of the obliquity deviation measurement was also given. The special measuring tool was designed. The particular measuring flow was introduced, and the judgment criterion for the measuring result was put forward.

关 键 词：导弹发射箱 发射导轨 检测 

分 类 号：TB482.2[一般工业技术—包装工程]