火箭推进2017，Vol.43Issue(2)：40-46,7.
火箭发动机试验紧急关机过程分析与改进
Analysis and improvement of emergency shutdown process in rocket engine test
庄建 1李琪琪 1王智超1
作者信息
- 1. 北京航天试验技术研究所,北京100074
- 折叠
摘要
Abstract
Emergency shutdown key processes in liquid rocket engine test are studied in this paper.The current commonly-used modes and methods of emergency shutdown in the liquid rocket engine test are expounded.The factors influencing the condition interpretation response time of automatic emergency shutdown are analyzed in theory and verified in experiment.The response time indicators of the emergency shutdown system were obtained.In order to solve the delay time problem of emergency shutdown,the ways and concrete solutions to shorten the condition interpretation response time of emergency shutdown are put forward.The method was verified repeatedly in actual test system.The correctness and stability of the procedure are assessed,which provides a certain reference basis for large data acquisition and analysis of fault diagnosis system response time.关键词
火箭发动机试验/自动紧急关机/条件判读/故障分析Key words
rocket engine test/automatic emergency shutdown/condition interpretation/fault analysis分类
航空航天引用本文复制引用
庄建,李琪琪,王智超..火箭发动机试验紧急关机过程分析与改进[J].火箭推进,2017,43(2):40-46,7.
