某型发射装置弹射故障分析  

Ejection Fault Analysis of a Launcher

作　　者：齐慧英 范昊栋 吴文 张茂杉 QI Hui-ying;FAN Hao-dong;WU Wen;ZHANG Mao-shan(Wuhu TianHang Aero-Tech Co.,Ltd,Wuhu Anhui 241000,China)

机构地区：[1]芜湖天航装备技术有限公司,安徽芜湖241000

出　　处：《科技视界》2019年第11期251-252,共2页Science & Technology Vision

摘　　要：发射装置是一种飞机与导弹的连接枢纽,用于实现导弹的悬挂、运载和发射。在弹射试验过程中,会出现高温高压燃气释放异常现象。针对此现象,本文从故障状况、原因分析、定位故障、检查故障源和故障排除五大方面进行阐述。Launcher is a connecting hub between aircraft and missile, which is used to suspend, carry and launch missiles. During ejection test, abnormal gas release at high temperature and high pressure will occur. In view of this phenomenon, this article elaborates from five aspects : fault status, cause analysis, fault location, fault source checking and fault elimination.

关 键 词：发射装置 燃气推进器 弹射试验 

分 类 号：TJ768.2[兵器科学与技术—武器系统与运用工程]